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KEMENTERIAN PERHUBUNGAN
DIREKTORAT JENDERAL PERHUBUNGAN UDARA
PERATURAN DIREKTUR JENDERAL PERHUBUNGAN UDARA
NOMOR : KP 294 TAHUN 2017
TENTANG
PETUNJUK TEKNIS
PERATURAN KESELAMATAN PENERBANGAN SIPIL BAGIAN 8900-6.1
{STAFF INSTRUCTION PART 8900-6.1)
TENTANG PEMERIKSAAN PESAWAT UDARA [AIRCRAFT INSPECTION)
DENGAN RAHMAT TUHAN YANG MAHA ESA
Menimbang
Mengingat
DIREKTUR JENDERAL PERHUBUNGAN UDARA,
a. bahwa Peraturan Menteri Pehubungan Nomor
PM 98 Tahun 2015 Tentang Peraturan Keselamatan
Penerbangan Sipil Bagian 21 (Civil Aviation Safety
Regulation Part 21) Tentang Prosedur Sertifikasi Untuk
Produk dan Bagian-Bagiannya (Certification Procedures
for Product and Parts) mengatur tentang inspeksi
terhadap produk pesawat udara;
b. bahwa "dalam rangka memberikan panduan bagi
pelaksanaan pemeriksaan pesawat udara (aircraft
inspection) oleh Inspektur Penerbangan perlu disusun
suatu petunjuk teknis;
c. bahwa berdasarkan pertimbangan sebagaimana
dimaksud pada butir a dan b, perlu menetapkan
Peraturan Direktur ' Jenderal Perhubungah Udara
tentang Petunjuk Teknis Peraturan Keselamatan
Penerbangan Sipil Bagian 8900-6.1 (Staff Instruction Part
8900-6.1) tentang Pemeriksaan Pesawat Udara (Aircraft
Inspection);
1. Undang-Undang Republik Indonesia Nomor 1 Tahun
2009 tentang Penerbangan (Lembaran Negara Republik
Indonesia Tahun 2009 Nomor 1, Tambahan Lembaran
Negara Republik Indonesia Nomor 4956);
2. Peraturan Presiden Nomor 7 Tahun 2015 tentang
Organisasi Kementerian Negara (Lembaran Negara
Republik Indonesia Tahun 2015 Nomor 5);
3. Peraturan Presiden Nomor 40 Tahun 2015 tentang
Kementerian Perhubungan (Lembaran Negara Republik
Indonesia Tahun 2015 Nomor 75);
4. Peraturan Menteri Perhubungan Nomor PM 59 Tahun
2015 Tentang Kriteria, Tugas dan Wewenang Inspektur;
5. Peraturan Menteri Perhubungan Nomor PM 189 Tahun
2015 tentang Organisasi dan Tata Keija Kementerian
Perhubungan;
6. Peraturan Menteri Perhubungan Nomor PM 98 Tahun
2015 Tentang Peraturan Keselamatan Penerbangan
Sipil Bagian 21 {Civil Aviation Safety Regulation Part 21)
Tentang Prosedur Sertifikasi Untuk Produk dan Bagian-
Bagiannya {Certification Procedures for Product and
Parts);
7. Peraturan Menteri Perhubungan Nomor PM 61 Tahun
2017 Tentang Perubahan Keempat Atas Peraturan
Menteri Perhubungan Nomor PM 28 Tahun 2013
Tentang Peraturan Keselamatan Penerbangan Sipil
Bagian 121 Tentang Persyaratan-Persyaratan Sertifikasi
dan Operasi Bagi Perusahaan Angkutan Udara yang
Melakukan Penerbangan Dalam Negeri, International
dan Angkutan Udara Niaga Tidak Berjadwal;
8. Peraturan Menteri Perhubungan Nomor 63 Tahun 2017
Tentang Perubahan Kesepuluh Atas Keputusan Menteri
Perhubungan Nomor KM 18 Tahun 2001 Tentang
Persyaratan-Persyaratan Sertifikasi dan Operasi Bagi
Perusahaan Angkutan Udara Niaga Untuk Penerbangan
Komuter dan Charter;
MEMUTUSKAN
Menetapkan : PERATURAN DIREKTUR JENDERAL PERHUBUNGAN
UDARA TENTANG PETUNJUK PELAKSANAAN PERATURAN
KESELAMATAN PENERBANGAN SIPIL BAGIAN 8900-6.1
(STAFF INSTRUCTION PART 8900-6.1) TENTANG
PEMERIKSAAN PESAWAT UDARA {AIRCRAFT INSPECTION)
Pasal 1
Memberlakukan Petunjuk Teknis Peraturan Keselamatan
Penerbangan Sipil Bagian 8900-6.1 (Staff Instruction Part
8900-6.2) Tentang Pemeriksaan Pesawat Udara (Aircraft
Inspection) sebagaimana tercantum dalam Lampiran yang
merupakan bagian tak terpisahkan dari Peraturan ini.
Pasal 2
Sejak berlakunya peraturan ini, maka Volume 2
Chapter 224 dan Chapter 225 Lampiran Peraturan Direktur
Jenderal Perhubungan Udara Nomor SKEP/44/III/2010
Tentang Staff Instruction 8300 (SI 8300) Airworthiness
Inspector's Handbook dicabut dan dinyatakan tidak
berlaku.
Pasal 3
Direktur Kelaikudaraan dan Pengoperasian Pesawat Udara
mengawasi Pelaksanaan Peraturan ini.
Pasal 4
Peraturan ini mulai berlaku sejak tanggal ditetapkan,
Ditetapkan : Jakarta
Pada tanggal : 11 OKTOBER 2017
DIREKTUR JENDERAL PERHUBUNGAN UDARA
ttd
Dr. Ir. AGUS SANTOSO, M.Sc
aslinya, Mla Mgian hukum
k/
UNAt
■ ^DAH Pt/p^AMA sflPT/ (IV/a)
NIP. 19680704 199503 2 001
LAMPIRAN PERATURAN DIREKTUR JENDERAL PERHUBUNGAN UDARANOMOR : KP 294 Tahun 2017TANGGAL : 11 Oktober2017
Staff Instruction
SI 8900 - 6.1
AIRCRAFT INSPECTION
Amendment : 0
Date : October 2017
REPUBLIC OF INDONESIA - MINISTRY OF TRANSPORTATION
DIRECTORATE GENERAL OF CIVIL AVIATION
JAKARTA - INDONESIA
J51 rUKlVl OyUU-D.l
OCTOBER 2017
AMENDMENT RECORD LIST
Amendment
No.Issue Date REFERENCE
Original Issue OCX 2017 -
SI FORM 8900-6.1
OCTOBER 2017
1. PURPOSE :
FOREWORD
This Staff Instruction on Aircraft Inspection isprepared for use and guidance of DGCA inspectorsand applicant dealing with DGCA for performingaircraft inspection to issuance Certificate ofAirworthiness (Original or Recurrent). It isdesigned to provide foundation for promotingsafety through proactive safety oversight system.The provision of this staff instruction shall applyto the aircraft inspection activities on both,original and recurrent of issuance airworthinesscertificate domestic and foreign aircraft operators.
All subject matters pertaining to aircraftinspection activities, procedures, functions andresponsibilities of DGCA are covered in this StaffInstruction.
2. REFERENCES :
3. CANCELLATION
4. AMENDMENT ;
This Staff Instruction should be used in
accordance with the applicable regulations.
SI 8300 Amdt. 4 Volume 2, Chapter 224, datedMarch 25*^, 2010 is canceled.
SI 8300 Amdt. 4 Volume 2, Chapter 225, datedMarch 25^, 2010 is canceled.
The amendment of this Staff Instruction shall be
approved by the Director General of Civil Aviation.
DIRECTOR GENERAL OF CIVIL AVIATION
signed
Dr. Ir. AGUS SANTOSO M. Sc
^suai aslinyavpaLab^gian hukum
LDAH PtlRNAMA SARI■^^Peiribfna / (IV/a)
NIP. 19680704 199503 2 001
IV
SI 8900-6.1
OCTOBER 2017
TABLE OF CONTENT
. AMENDMENT RECORD LIST i
FOREWORD ii
TABLE OF CONTENTS iii
CHAPTER I - INTRODUCTION 1
1. Aircraft Inspection 1
2. Purpose 1
CHAPTER II - AIRCRAFT INSPECTION POLICY 4
1. General 4
2. The Aircraft Inspection 4
3. The Physical Inspection Involves the Completion of DetailedChecklists and encompasses 4
4. Function of Directorate of Airworthiness and Aircraft Operations
(DAAO) for Aircraft Inspection in Issuing Airworthiness Certificate of
Aircraft (C of A) 19
5. Function of DGCA Regional Office 20
6. Function of Airworthiness Inspector Assigned for The Aircraft 20
Inspection
CHAPTER III - AIRCRAFT INSPECTION PROCEDURES 21
1. Aircraft Inspection And Related Processes - Overview 21
2. General instructions - Aircraft Inspection 21CHAPTER IV - AIRCRAFT INSPECTION FINDINGS 23
1. General 23
2. Findings - Categorization 23
CHAPTER V - FOLLOW UP ACTIONS 24
1. Aircraft Inspection - Follow-up Actions 24
2. Actions Resulting From An Inspection 243. Aircraft Grounded By DGCA Inspection Team 244. Generation And Distribution Of Aircraft Inspection Findings 24
5. Further Follow Up 24
CHAPTER VI - MONITORING OF AIRCRAFT INSPECTION DEFICIENCIES 25
1. Monitoring Deficiencies by DGCA (DAAO Office) 25
2. Review at DGCA (DAAO office) 253. Safety Related Issues 25
4. Records 25
APPENDIX 1 - QUALIFICATION AND TRAINING OF RAMP INSPECTOR 26
1. Competencies of the Inspector 26
2. Qualifications of the Inspector 263. Aircraft Certification Training 26
APPENDIX 2 - DGCA REFERENCES FOR AIRCRAFT INSPECTIONS
GUIDANCE 27
1. PART I General Data 27
2. PART II Aircraft Status 28
3. PART III Aircraft Inspection 32
SI 8900-6.1
OCTOBER 2017
4. PART IV Functional Check 45
5. PART V Ground Run and Test Flight 46
APPENDIX 3 - AIRCRAFT INSPECTION CHECKLIST 47
Instruction to complete Aircraft Inspection Checklist (DGCA Form 21.40) 47
Aircraft Inspection Checklist 49
SI 8900-6.1
OCTOBER 2017
CHAPTER I
INTRODUCTION
1. Aircraft inspection
Aircraft Inspections are planned inspections carried out to verify thecompliance of laid down standards and regulations prior issuing anairworthiness certificate ( Original or Recurrent ). This inspection iscarried out by a DGCA inspector as per standard checklist.
No aircraft may be operated unless a Certificate of Airworthiness hasbeen issued to that aircraft. DGCA is responsible to perform inspectionand test do determined its compliance with airworthiness standards.Standard Certificate of Airworthiness is issued to aeroplane certificatedin the transport, normal, utility, acrobatic, commuter categoiy and tohelicopter certificated in normsd and transport category, and to airshipand manned free balloon. Special Certificate of Airworthiness is issuedto aircraft operated in the limited, restricted, experimental and specialflight permit.
Refer to Staff Instruction SI 21-02, Original certification covers theinitial issuance of standeird or special airworthiness certificates.Recurrent certification applies to the issuance of standard or specialairworthiness certificates for aircraft that previously have been issuedan airworthiness certificate.
This Staff Instruction is prepared for use and guidance of DGCAinspectors for performing original and recurrent certification of aircraft.
2. Purpose
The purpose of the aircraft inspection is to determine its compliancewith airworthiness standard.
The aircraft inspection performed during original and recurrentcertification must be in accordance with the followings:
a. Original CertiHcationOriginal certification covers the initial issuance of standard orspecial airworthiness certificates and approvals, including export foraircraft and aeronautical products for aircraft holding a Republic ofIndonesia type design as follows:1) Aircraft or related products (new or used) that have not left the
original product manufacturer's quality control system.2) Aircraft or related products for which an DGCA airworthiness
certificate or approval has never been issued. Examples include:(a) All provisional Airworthiness Certificates and amendmentsthereto.
(b) All experimental certificates and amendments thereto,including amateur-built aircraft which are new or have beensubjected to a major change.
(c) Limited airworthiness certificates.(d) Aircraft manufactured to other than Republic of Indonesia,
requirements imported to the Republic of Indonesia.
SI 8900-6.1
OCTOBER 2017
3) Aircraft that previously have been issued an airworthinesscertificate and presented for certification in another category orclassification, for example; aircraft converted from standard torestricted for the first time or from a special airworthinesscertificate to standard for the first time.
4) Aircraft that have undergone changes to the type design andrequire flight testing, for example, under an experimentalcertificate for the purpose of showing compliance with regulationsincluding, as applicable, the issuance or reissuance of a standardairworthiness certificate.
5) Prototype or test articles to be used for design evsduation for TC orSTC purposes. This includes parts or installation approvals.
6) Aircraft with an DGCA-approved type design that have undergonea model change, as listed on the airworthiness certificate, andrequire a conformity inspection before issuance of an amendedairworthiness certificate.
7) Aircraft manufactured to a Indonesian ■ TC (TC Validation) andexported from a country with which the ROI has a bilateralagreement, when accompanied by an Export C of A from abilateral civil aviation authority (CAA). The CAA's Export C of Amust contain a statement from that CAA stating that the aircraftconforms to the type design approved under Indonesian TypeCertificate and is in a condition for safe operation.
8) Issuance of special flight permits for aircraft that previously havenot been issued an airworthiness certificate.
b. Recurrent Certification.
The term recurrent certificationll applies to the issuance of standardor special airworthiness certificates or approvals for the following:1) Aircraft that previously have been issued an airworthiness
certificate except those listed in paragraphs 2 a. 3) through 8) ofthis Staff Instruction.
2) Issuance of special flight permits for aircraft which have beenissued an airworthiness certificate.
3) Export certification or approval of aeronautical products orarticles that previously have been issued an airworthinesscertificate or approval.
4) Issuance of airworthiness certificates, except experimental andprovisional, for aircraft with certificates that have expired, beensurrendered, or been revoked.
5) Changes to operating limitations.6) Issuance of experimental certificates for research and developmentand exhibition which have expired.
7) ROI manufactured aircraft returning to the ROI. which werepreviously issued an airworthiness certificate or an Export C of Ain the R.I.
8) Aircraft manufactured to a Indonesian TC (TC Validation) andexported from a country with which the ROI has a bilateralagreement, when accompanied by an Export C of A from abilateral civil aviation authority (CAA). The CAA's Export C of Amust contain a statement from that CAA stating that the aircraftconforms to the type design approved under Indonesian TypeCertificate and is in a condition for safe operation.
SI 8900-6.1
OCTOBER 2017
Aircraft Inspection is concerned with the aircraft documents and theconditions of aircraft. The applicable requirements for these inspectionsare:
i. CASR Part 21, Part 91, Part 121, Part 135, Part 43, Part 39 andothers related CASR.
ii. Aircraft Manufacture Manual (Maintenance Manual, StructuralRepair Manual, Aircraft Weight 8b Balance Manual, Illustrated PartCatalog, Wiring Diagram Manual, etc).
iii. Aircraft delivery documentation, including build standards,components status, inspection and test;
iv. Operator Manual, including Maintenance Program, ReliabilityProgram, Continuous Airworthiness and Surveillance Program;
V. Aircraft document, including damage record, repair record,alteration record, Component Status, AD/SB status, etc.
Original and Recurrent certification of aircraft must be filed with IMSISdatabase.
Aircraft Inspection for issuance airworthiness certificate must beperformed at least 3 (three) working days for document and physicalcheck.
SI 8900-6.1OCTOBER 2017
CHAPTER II
AIRCRAFT INSPECTION POLICY
1. GENERAL
DGCA is responsible to cariy out the inspection for issuanceAirworthiness Certificate of aircraft (C of A).
2. THE AIRCRAFT INSPECTION
A. The DGCA Airworthiness Inspector will conduct inspection ofaircraft to check the aircrafts physic and aircraft document.Purpose of inspection is determining whether the aircraft conformsto the type design, any modification or repairs have been carriedout in accordance to approved data, and to ensure the aircraft isin a condition for safe operation (refer to CASR 21.183(c)).
B. The applicant must prepare an aircraft for inspection by the DGCAinspector on an agreed date.
3. THE PHYSICAL INSPECTION INVOLVES THE COMPLETION OF
DETAILED CHECKLISTS, AND ENCOMPASSES
The items to be checked by the DGCA inspector divided by 2 (two)categories, document check and physical check.
A. Document check
The document to be checked by the DGCA inspector duringaircraft inspection are summarized as:
a. Part I General Data
DGCA inspector must check
l.A. Aircraft Make Model:
Nationality Ss Registration Marks; Registration Number;Serial Number; A/C Category; Mfg. Year; Operator; TC/TCValidation Number ( Rev/Date); MTOW; No OF SEAT;TCDS; total time, current inspection, last inspection (tsn/csn ); aircraft utilization during one year ( year/hours/ cycles).
I.E. Engine Make & Model
(S/N, TSN, CSN, TBO, Remaining)
I.e. Propeller /Rotor Make & Model
(S/N, TSN, CSN, TBO, Remaining)
l.D. APU Make & Model
SI 8900-6.1
OCTOBER 2017
(S/N, TSN, CSN, TBO, Remaining)
I.E. Landing Gear :
Nose L/G, Left Main L/G, Right Main L/G (P/N, S/N, TBO,Remaining)
b. Part II Aircraft Status
DGCA inspector must check
II.A. Aircraft document and manual
II.A. 1. Certificate of Registration,II.A.2. Certificate of Airworthiness,II.A.3. Insurance,II.A.4. Maintenance manual,II.A.5. Weight and balance manual,II.A.6. Wiring diagram manual,II.A.7. Structure repair manual,II.A.8. Illustrated part catalog,II.A.9. Aircraft flight manual/ pilot operating handbook,II.A. 10. Flight crew operating handbook,II.A. 11. Quick reference handbook,II.A. 12. Master MEL and/or MEL,II.A. 13. Noise certificate,II.A. 14. Aircraft aeronautical station license.
II.B. Logbook and test reportII.B.l. Aircraft flight/ maintenance log,II.B.2. Deferred item list (ie, HIL, CDL, DMI, DDR),II.B.3. Airframe, engine, propeller,II.B.4. Compass wing and data report,II.B.5. Weight and balance report,II.B.6. Altimeter and static system test report,II.B.7. ATC transponder test report and mode Stransponder
encoding,II.B.8. VOR inspection for IFR andII.B.9. ELT test report.
II.C. Aircraft inspection and maintenance reportsII.C.l. Statement of build standard (new aircraft) from
manufacturer,II.C.2. Statement of accident/incident from the last
operator (if any),II.C.3. Approved maintenance program (Doc. No,
revision, date),II.C.4. Inspection work package for compliance,
annual/100 Hrs inspection, structuralinspection program, corrosion protection controlprogram, non routine inspection,
II.C.5. Component status (OC, CM, HT), life limitedpart (for bridging ref AC 121-1),
SI 8900-6.1
OCTOBER 2017
II.C.6. Airworthiness directives, alert service bulletingstatus,
II.C.7. Damage and repair status and work packagereport,
II.C.8. Alteration/modification status and workpackage and
II.C.9. Service difficulty report.
B. Physical check
The physical check performed by the DGCA inspector duringaircraft inspection are summarized as:
c. Part III Aircraft Inspection
DGCA inspector must check:
III.A. External Visual InspectionIII.A.l. Landing gear/ skid and wheel well areaIII.A. 1.1. Data plate, pacards and marking;III.A. 1.2. Sign of corrosion, wear, chafing lines or
wires;III.A.l.3. Structural integrity of gears and doors for
cracks, dents, other obvious damage,III.A. 1.4. Sign of leaks (struts, actuators valves, tube
and hose),III.A. 1.5. Wheel installation and safety locking device,III.A.l.6. Tire condition,III.A. 1.7. Brake installation for security, wear,
condition and leaks,III.A. 1.8. Skids and floats for security and condition,III.A. 1.9. Steering mechanism for security, wear, and
condition,III.A. 1.10. Brake pin indicator for minimum length,III.A. 1.11. Torque links for security and excessive play,III.A. 1.12. Fairing for security and missing fasteners,III.A. 1.13. Lighting for condition,III.A. 1.14. Main gear static discharge.
III.A.2. Fuselage and EmpenageIII.A.2.1. Identification Plate (CASR 45.11)
a. Aircraft
It must be secured to the aircraft fuselage
exterior so that it is legible to a person on the
ground, and must be either adjacent to and aftof the rearmost entrance door or on the
fuselage surface near the tail surfaces;
b. Manned Free Balloons
It must be secured to the balloon envelope and
must be located, if practicable, where it is
legible to the operator when the balloon is
inflated. In addition, the basket and heater
SI 8900-6.1
OCTOBER 2017
assembly must be permanently and legiblymarked with the manufacturer's name, part
number (or equivalent), aind serial number (orequivalent).
c. Power Parachute and Weight Shift Control
It must be secured to the aircraft fuselage
exterior so that it is legible to a person on theground.
d. Additional Identification Plate (Nationality &Registration Marks) CASR 45.30)It must be secured to the aircraft in a
prominent position near pilot's entrance;
III.A.2.2. Nationality 86 registration marks and national
flag for legibility, location and size, and othermarking requirements (casr 45.21, 45.22,
45.23, 45.24, 45.25. 45.27, 45.29),
III.A.2.3. Structure for cracks, corrosion, dents, rubbing
and other obvious damages,
III.A.2.4. Exterior exit markings and exterior emergency
lighting and escape route (casr 121.310,
135.349),
III.A.2.5. Drain holes for obstruction stain or other sign
of leaks,
III.A.2.6. Radome, pitot tubes, static ports, stall
warning, windshield, wiper, sensors, antennas,
for condition, security 86 corrosion,
III.A.2.7. Loose/missing improper fasteners,
III.A.2.8. Elevators, rudder and tabs for obvious damage,
cracks, corrosions, rubbing and excessive play,
III.A.2.9. Fire discharge dishes for indication,
III.A.2,10. Lavatory (evidence of fresh blue water streaks).
III.A.3. Auxiliaiy Power Unit
III.A.3.1. Identification plate,
IILA.3.2. Door for security and missing/loose fastener;
III.A.3.3. Any indication of wear, leak, chaffing line, wire;
III.A.3.4. Fire extinguisher and sensor.
III.A.4. Wings and Pylon
III.A.4.1. All lights for general condition and broken
lenses,
ni.A.4.2. Structure for cracks, corrosion, dents and
other damage;
III .A. 4.3. Fuel caps for security
III.A.4.4. Wing tip for general condition and damage
SI 8900-6.1
OCTOBER 2017
III .A. 4.5. Anti/de-icing devices for condition and damageIII.A.4.6. Leading edge for dents, abrasion, obvious
damage, and stall warning for functioncondition
III.A.4.7. Leading edge devices, rubber boots, wiring,hoses, for condition and leak
IILA.4.8. Evidence of fuel leaks;
IILA.4.9. Flaps, flaps track and flaps well for cracks,corrosion, leaks, abrasion, dents,
delamination, and condition of connectors,
wiring, lines and hoses
IILA.4.10. Aileron and tabs for obvious cracks, corrosion,
dents, delimination, excessive play
IILA.4.11. Static discharge for condition;
nLA.4,12. Access panels/hatch/inspection door for
security
11I.A.5. Power Plants
III.A. 5.1. Engine identificarion plate (casr 45.11);
IILA.5.2. Fan blade, turbine blade, and sensors for
damage,
111 .A. 5.3. Engine mount, cowling and pylons,
IIl.A.5.4. Cowling 86 doors for security and missing/loose
fasteners,
IILA.5.5. Inlet cowl for dents, corrosion aind abrasion,
IILA.5.6. Acoustic, access panel for security, dents,
corrosion, delimination and crack,
IILA.5.7. Reverse doors for stowage security and leaks,
III .A. 5.8. Exhaust for turbine/tail pipe damage and
leaks,
lll.A.5.9. Fire extinguisher bottle gauge for security and
correct pressure.
II1.A.6. Propeller/ Rotor
ni.A.6,1. Propeller/rotor identification plate;
III.A.6.2. Propeller blade and deicer boots, for dent,
crack, deterioration, delamination and general
condition;
III.A.6.3. Drive shaft, yoke, swash plate, rotor head for
wear, dent, crack, deterioration, delamination
and general condition;
III .A. 6.4. Spinner for cracks and dent;
III.A.6.5. Main rotor blades, for secured, wear, obvious
damage, and general condition (including colorcodes);
IIl.A.6.6. Tail rotor for secured, wear, obvious damage,
and general condition;
10
SI 8900-6.1
OCTOBER 2017
III.A.6.7. Tail rotor gearbox, drive shaft and oil level for
securily, cracks, damage, leaks and general
condition.
III.B Interior Inspection
III.B. 1. Lavatory fire protection;
III.B. 1.1. Each lavatory in the airplane must be equipped
with a smoke detector system or equivalentprovides a warning light in the cockpit or
provides a warning light or audio warning inthe passenger cabin readily detected by a flightattendant
III.B. 1.2. Each lavatory in the airplane must be equippedwith a built-in fire extinguisher and capable of
automatic discharge, for each disposalreceptacle for towels, paper, or waste located inthe lavatory
III.B.2. Emergency Equipment and Additional
Emergency Equipment (CASR 91.207, 91.533, CASR 121.309, CASR 121.310, CASR121 App. A, CASR 135.349)
note: Each item of emergency and flotationequipment:
(1) Must be inspected regularly, and soindicated date of last inspection;
(2) Must be readily accessible to the crew;
(3) Must be clearly identified and clearly markedto indicate its method of operation; and
When carried in a compartment or container,must be marked on the compartment orcontainer, the date of last inspection
III.B.2.1. Hand Fire Extinguisher
Note:
a. At least two of the required hand fire
extinguisher installed in passenger carryingairplanes must contain Halon 1211 (CASR121.309) or equivalent extinguisher agent.
b. At least one of the required hand fireextinguisher installed in passenger carryingairplanes must contain Halon 1211 (CASR135.349)
c. For individual Certificate of Airworthiness is
first issued on or after 31 December 2016
11
SI 8900-6.1
OCTOBER 2017
shall not be of a type listed in the 1987Montreal Protocol (Annex A, Group 11.)
1. Halon 1211
2. Halon 1301
3. Halon 2402
A. At least one hand fire extinguisher must beconveniently located for use:
i. in each galley compartment
ii. in each class E cargo compartment
iii. on the flight deck
B. In passenger compartment, at least oneHalon 1211 (CASR 121.309)
III.B.2.2.
7 - 30 at least one
o
1
CO
at least two
61-200 Minimum 3 ea
201-300 Minimum 4 ea
301-400 Minimum 5 ea
401-500 Minimum 6 ea
Firs§R}dTfiP,^ust
> 600 Minimum 8 ea
In passenger compartment
(CASR 135.349)
> 9 at least one
In passenger compartment
(CASR 91.533)
oOC
t
at least one
> 30 at least two
0-50 Minimum 1 ea
51-150 Minimum 2 ea
151-250 Minimum 3 ea
to the crew, stored seci
12
SI 8900-6.1
OCTOBER 2017
> 250 Minimum 4 ea
> 9 pax seat (CASR 135. 349)
First Aid Kit, must be readily acessible to thecrew, stored securely, free form dust, moisture
and temperature (CASR 91.533)
o o o muminiM1
ea
101 -200
muminiM2
ea
201 - 300
muminiM3
ea
301 - 400
muminiM4
ea
401 - 500
muminiM5
ea
>500
muminiM6
ea
III.B.2.3. Emergency Medical Kit (check contain in
accordance with appendix A)
At least one (CASR 121 Appendix A)
In airplanes for which a flight attendant is
required ( CASR 135.349)
III.B.2.4. Crash Axe
a. Each airplane accommodating more than 19
passengers (CASR 91.533)
b. Each airplane operated under CASR 135that has a lockable non frangible door
separating the flight deck from the
passenger cabin (CASR 135.349)
c. Each airplane operated under CASR 121
(CASR 121.309)
III.B.2.5. Megaphone (CASR 91.533, 121.309)
III.B.2.6.
61 -99 1 ea (rearward)
> 992 ea (forward 8b
rearward)
Emergency Exit (CASR 91.607, CASR 135.349,
CASR 121.310)
a. Interior Emergency Exit marking, placement
and legibility
b. Lighting for interior emergency exit marking
13
SI 8900-6.1
OCTOBER 2017
c. Emergency exit operating handles andinstruction
d. Emergency exit access, must beunobstructed
III.B.2.7. Portable lights, ensure available for each flightattendant seat and accesible from each fight
attendant seat (CASR 91.205, CASR 121.310,
CASR 135.357)
III.B.2.8 Protective Breathing Equipment (CASR
121.337)
a. One in flight deck
b. One PBE is required for each hand fireextinguisher located for use in a galley
c. One PBE is required for each hand fire
extinguisher in pax compartment (located
within 3 feet from hand firex)
d. One for use in each Class A, B, and E cargo
compartment
III.B.2.9 Portable Oxygen (CASR 121.333)
III.B.2.10 Emergency Locator Transmitter, type 406
(CASR 91.207).
Note: If the aircraft installed with fixed and
deployable automatic type transmitters, it
must be attached to the airplane as far aft as
practicable
a. Type of ELT
Automatic Fixed (AF)
Automatic Portable (AP)
Automatic Deployable (AD)
Survival (S)
b. < 20 passenger seat at least one (automatic)
Record ELT Battery due:
c. > 19 passengers for which the individual
certificate of airworthiness is first issued
after 1 July 2008 at least two (one of whichshall be automatic)
Record ELT Battery due:
and
d. ELT annual inspection (after the lastinspection) for:
(i) Proper installation
(ii) Battery corrosion
(iii) Operation of the controls and crashsensor
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The presence of a sufficient signal radiatedfrom its antenna
e. ELT encoding
III.B.3. Emergency Equipment for Overwater Operation(CASR 91, 207, 91.223, CASR 121.309,121.339, CASR 135.349, 135.351, 135.355)
III.B.4. Miscellaneous Equipment (CASR 121.313,
135.321)
III.B.4.1. Spare of protective fuse or bulb (if installed)III.B.4.2. A windshield wiper or equivalent for each pilot
station
III.B.4.3. Two independent static pressure systems
III.B.4.4. A means to monitor from the flight deck side of
the door the area outside the flight deck door(except for cargo)
III.B.4.5. Door between the passenger and pilot or crewrest compartments, for transport category
and/or cargo operation with a mtow in excess
of 45.500 kg or with a passenger seatinggreater than 60
III.B.4.6. A placard on each door of access to a an
emergency exit, to indicate that it must be
open during takeoff and landing
III.B.5. Passenger Information (CASR 121.317)
III.B.5.1. Passenger information marking and placard in
Bahasa or Bilingual (Bahasa - English) (CASR21.29 a.3)
a. Fasten seat belt sign or placard is visible
from each passenger seat
b. No smoking sign or placard, in cabin and
lavatory
III.B.6. Public Address System
III.B.6.1. Public Address System (more than 19 pax)(CASR 121.318, CASR 135.331)
(note: Transport category manufactured afterDecember 1996)
III.B.7. Crewmember Interphone SystemIII.B.7.1. Crewmember Interphone System (more than 19
pax) (CASR 121.319, CASR 135.333)
III.B.8. Passenger Briefing Card
III.B.8.1. Passenger Briefing Card (CASR 91.537(b),
CASR 121.503(b), CASR 135.107(b)
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III.B.9. Seats, Safety Belts, Shoulder Harnesses, andChild Restraint Systems (CASH 121.311,CASK 135.119, CASK 91.521)
III.B.9.1. Passenger seats, seat belts,cushion/upholstery materials, armrest forcondition, reclining mechanism for properoperations
III.B.9.2. Exit seat, check table, reclining mechanism tomake sure not blocking emergency exit ( CASK121.585, 135.121)
III.B.9.3. Child Restraint System, check for securityIII.B.9.4. At each flight deck station equipped with a
combined safety belt and shoulder harness,
check for security
III.B.IO. Cargo and Bagggage Compartment (CASR121.221)
III.B.10.1. Fire precaution
a. Class "A" (All parts of the compartment areeasily accesible and fire therein would beready discernible to a crew member)
There must be a hand fire extinguisher
available for each Class A compartment.
b. Class "B" (Enough access for crew memberto reach all the compartment and no smoke,
flame or extingushing agent enter thecompartment occupied by crew or
passanger)
(1) It must have a separate approved smokeor fire detector system to give warning atthe pilot or flight engineer station
(2) There must be a hand fire extinguisheravailable for the compartment
(3) It must be lined with fire resistantmaterial
c. Class "C" (Not conform with requirementClass A, B, D or E)
1. It must have a separate smoke or firedetector system to give warning at thepilot or flight engineer station
2. It must have an approved built-in fireextinguishing system controlled from thepilot or flight engineer station
3. It must be designed to exclude hazardousquantities of smoke, flames, orextinguishing agents from entering into
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any compartment occupied by the crew orpassenger
4. It must have ventilation and draft
controlled so that the extinguishing agentprovided can control any fire that maystart in the compartment
5. It must be lined with fire resistant
material
d. Class "D" (Designed and constructed that afire occuring therein will be completelyconfined without endargingthe safety of theairplane or occupants)
1. It must have a means to exclude
hazardous quantities of smoke, flames,or noxious gases from entering anycompartment occupied by the crew orpassengers
2. Ventilation and drafts must be controlled
within each compartment
3. It must be completely lined with fireresistant material
e. Class "E" for Cargo only
1. It must be completely lined with fireresistant material
2. It must have a separate system of anapproved type smoke or fire detector togive warning at the pilot or flightengineer station
3. It must have a means to shut off the
ventilating air flow to or within thecompartment and the controls for thatmeans must be accessible to the flightcrew in the crew compartment
4. It must have a means to exclude
hazardous quantities of smoke, flames,or noxious gases from entering the flightcrew compartment
III.B.10.2. Check cargo door for leaks, damage andgeneral condition
III.B.10.3. Smoke detectors for damage
III.B. 10,4. Lighting is operable and protective cover isinstalled
III.B.10.5. Flooring and pallet system for generalcondition
III.B.10.6. Placard of weight limitation for availability andlegibility
III.B. 10.7. A 9G cargo net for condition (if applicable)
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III.C. COCKPIT INSPECTION
INSTRUMENT, EQUIPMENT MARKING, PLACARD ARE
CORRECTLY INSTALLED AND LEGIBLE.
III.C.l. Instrument for VFR (day) (CASR 91.205)
III.C. 1.1. Airspeed indicator
III. C. 1.2. Altimeter
III.C. 1.3 Magnetic Direction Indicator
III.C. 1.4. A tachometer for each engineIII.C. 1.5 A cylinder head temperature indicator for each
air cooled eng.
III.C. 1.6. Oil in temperature indicator for each engineIII.C. 1.7. A fuel quantity indicator for each fuel tank
III.C. 1.8. An oil pressure indicator for each engine
III.C, 1.9. A manifold pressure indicator for each engineIII.C. 1.10. Landing gear position indicator, if the aircraft
has a retractable landing gear
III.C.2. Instrument for IFR (CASR 91.205), specified
requirement VFR (day)III.C,2.1. Gyroscopic rate of turn indicator
III.C.2.2. Slip/Skid indicator
III.C.2.3. Sensitive altimeter adjustable for barometric
pressure
III.C.2.4. Clock
III.C.2.5. Gjrroscopic pitch and bank indicator (AH)
III.C.2.6. Gyroscopic direction indicator (directional gyroor equivalent)
1II.C.3. Flight and Navigation Instrument (CASR
121.305)
III.C.3.1. An airspeed indicating system with heated pitottube
III.C.3.2. Two sensitive pressure altimeter
III.C.3.3. Clock
III,C.3.4. A free air temperture indicator
III.C.3.5. Gyroscopic pitch and bank indicator (AH)III.C.3.6. Gjn-oscopic rate and turn indicator combined
with an integral skip/skid indicator (turn andbank indicator)
III.C.3.7. Gjrroscopic direction indicator (dyrectional gyroor equivedent)
III.C.3.8. A magnetic compass
III.C.3.9. A vertical speed indicator (rate of climb
indicator)
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III.C.3.10. Two Gyroscopic pitch and bank indicator (AH)or :
Third Gyroscopic pitch and bank indicator (AH)
for:
(i). turbojet ,or
(ii). turbo prop having pax seat >30 or payload> 7500 lbs
III.C.4. Engine Instrument (CASR 121.307)
III.0.4.1. Oil in temperature indicator for each engine
III.C.4.2. A fuel pressure indicator for each engine
III.C.4.3. A means for indicating fuel quantity for each
fuel tank
III.C.4.4. An oil pressure indicator for each engine
III.C.4.5. An oil quantity indicator for each oil tank
III.C.4.6. An independent fuel pressure warning devicefor each engine or a master warning device for
all engines
III.0.5. Flight and navigation Instrument (CASR
135.305)
III.0.5.1. Two independent airspeed indicating systemIII.0.5.2. Two independent sensitive altimeter systemin.0.5.3. Clock
II1.0.5.4. A free air temperature indicator
III.0.5.5. Gyroscopic direction indicator (directional gyro
or equivalent)
III. 0.5.6. A magnetic compass
III.0.5.7. Gyroscopic pitch and bank indicator (AH)III.0.5.8. Vertical speed indicator (rate of climb indicator)
IIl.C.5.9. Two Gyroscopic pitch and bank indicator (AH)for turbojet and turbo prop.
III.0.5.10. Third Gjnroscopic pitch and bank indicator (AH)
for turbojet
III.0.6. Engine Instrument (CASR 135.317)III.0.6.1. A tachometer for each engineIII.0.6.2. A carburetor air temperature indicator for each
engine
III.0.6.3. A cylinder head temperature indicator for each
air cooled eng.
III.0.6.4. Oil in temperature indicator for each engineIII.0.6.5. A fuel pressure indicator for each engine111.0.6.6. A fuel flowmeter or fuel mixture indicator for
each engine not equipped with an automaticaltitude mixture control
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III.C.6.7, A means for indicating fuel quantity for eachfuel tank
III.C.6,8. An oil pressure indicator for each engine
III.C.6.9. An oil quantity indicator for each oil tankIILC.6.10. An independent fuel pressure warning device
for each engine or a master warning device for
all engines
III.C.6.11. A device for each reversible propeller
III.C.6.12. A manifold pressure indicator for each engine
III.C.7. Navigation and Radio Communication
(CASR 91.205, CASR 91.175CASR, 91.215,
CASR 121.99, CASR 121.349, CASR
135.309, CASR 135.311, CASR 121.345,)III.C.7.1. HF
III.C.7.2. VHP
III.C.7.3. ATC Trainsponder
III.C.7.4. VOR
III.C.7.5. DME
III.C.7.6. ILS
III.C.8. EQUIPMENTS
III.C.8.1. Weather Radar (CASR 121.357, 135.315)
III.C.8.2. 1. TCAS (CASR 91.227)
Turbine, MTOW>33.000 lbs (15.000 Kg) for
which the individual Airworthiness
Certificate is first issued after 31 December
2015, shall be equipped with TCAS II
2. TCAS (CASR 121.356)
a. Turbine, MTOW>33.000 lbs (15.000 Kg),TSO 119a, version 6,04A Enhance or
equivalent installed before May 1, 2003
TSO 119b, version 7.1 or a later or
equivalent
b. Combi airplane PaxlO - 30 seat TCAS I
TSO 118
c. Piston, MTOW>33.000 lbs TCAS I TSO
118
III.C.8.3. TAWS (CASR 121.354, CASR 135.319)
TSO C-151Class A or equivalent for >9 pax
TSO C-151Class B or equivalent for 6-9 pax
CASR 91.229
MTOW > 5700 kg or Pax seat >9
TSO C-151 or equivalent
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OCTOBER 2017
III.C.8.4. GPS/INS/Doppler Radar/ONS/IRS or FMS(CASR 121.355, CASR 121.358)
III.C.8.5. Low altitude windshear system (CASR121.352)
Aeroplanes (except turboprop) manufactured
after 2 January 1991, must be equipped with
either an approved airborne windshear warning
&i flight guidance system, an approved airborne
detection & avoidance system, or combination
of these systems
III.C.8.6. Pitot Heat Indicating System (CASR 121.342,
CASR 135.325)
AH transport category aicraft (CASR 121.342)>20 pax (CASR 135.325)
III.C.8.7. Flight Data Recorder, check for applicability
and type of FDR CASR 91.233 and Appendix E(Airplane), F (Helicopter)
AIRPLANE
i All airplane first issue of C of A on or after
IJanuaiy 1989 with maximum certificated
take-off mass more than 27.000 kg (Type IFDR)
ii All airplane first issue C of A on or after 1
Jan. 1989 with maximum certificated take
off mass more than 5.700 kg, up to andincluding 27.000 kg (Type II FDR)
iii All airplane first issue of C of A after 1
January 2005 with maximum certificated
take-off mass more than 5.700 kg (Type LA)iv All turbine engine airplane first issue of C of
A on or after 1 January 2016 with a seating
configuration of more than 5 passenger seatand maximum certificated take-off mass of
5700 kg or less (Type II)HELICOPTER
i AH helicopters first issued of C of A on or
after 1 January 2016 with maximum
certificated take-off mass more than 3180
kg (Type IVA)ii AH helicopters first issued of C of A on or
after 1 January 1989 with maximum
certificated take-off mass more than 7000
kg or having a passanger seatingconfiguration of more than 19 (Type IV)
Record ULB Battery due:
Annual read out for required number of
parameter to be recorded and quality(measurement range, recording interval,accuracy, resolution)
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OCTOBER 2017
Calibration for 5 year or at least 2 year in
accordance with
manufacturer recommendation
III.C.8.8. CVR/CARS (CASR 91.235)
AIRPLANE
i All turbine-engine airplanes, for which the
individual certificate of airworthiness was
first issued on or after 1 January 2016, with
a seating configurations of more than five
passenger seats and a maximum certificated
take-off mass of 5 700 kg or less shall be
equipped with either a CVR or a CARS
ii All turbine-engine airplanes for a maximum
certificated take-off mass of over 5 700 kgfor which the individual certificate of
airworthiness was first issued on or after 1
January 2016 and required to be operated
by more than one pilot shall be equippedwith a CVR
iii All airplanes of a maximum certificated
take-off mass of over 27 000 kg for whichthe individual certificate of airworthiness is
first issued on or after 1 January 1987 shallbe equipped with a CVR
HELICOPTER
i All helicopters of a maximum certificated
take-off mass of over 7 000 kg for which the
individual certificate of airworthiness is first
issued on or after 1 January 1987 shall be
equipped with a CVR. For helicopters notequipped with an FDR, at least main rotor
speed shall be recorded on the CVR
ii All helicopters of a maximum certificated
take-off mass of over 7 000 kg for which the
individual certificate of airworthiness was
first issued before 1 January 1987 shall beequipped with a CVR. For helicopters notequipped with an FDR, at least main rotor
speed shall be recorded on the CVR
From 1 January 2016, a magnetic tape & wireshall be discontinued, and capable of two
hours recordingFrom 1 January 2016, all CVR shall be capableof retaining the information recorded during atleast the last two hours of their operation
Record ULB Battery, due:
Annual Examination
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IILC.9. Lighting (CASR 91.209, CASR 121.323,
CASR 135.307)
III.C.9.1. Instrument light
III.C.9.2. Anti Collision light
III.C.9.3. Position/Navigation light
III.C.9.4. Two Landing light
IILC.9.5. Taxi light
III.C.9.6. Logo light
III.C.9.7. Cabin light (ceiling, windows, service, entry,
exit, etc.)
d. Part IV Functional Check
DGCA Inspector must check :
IV.A Aircraft SystemIV. A. 1. Flight control system
rV.A.2. Recording system (FDR, CVR)IV.A.3. Fire precaution (engine, APU, cargo)IV.A.4. Smoke detector system (lavatory, cargo)IV.A.5. Public address system and interphone systemIV.A.6. Pitot heat indicating systemIV.A.7. Lighting (nav. Light anti-collision light,
instrument light, landing light, emergeny light,passenger information light)
IV.A. 8. ELTtest
IV.A.9. Other applicable systems.
IV. B. Communication
IV.B.l. HF, VHF, ATC transponder
IV.C. Navigation;
IV.C. 1. ADF, VOR, DME, ILS;
IV,C.2. Weather radar;
IV.C.3. TAWS TSO C151 class A and windshear;IV.C.4. TCAS;
IV.C.5. GPS/INS/IRS/FMS.
e. Part V Ground Run and Test Flight
DGCA Inspector must check :
V. 1. Ground run and test flight conducted
according to test plane;V.2. Ground run and test result;V.3. Test flight result.
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OCTOBER 2017
4. FUNCTION OF DIRECTORATE OF AIRWORTHINESS AND
AIRCRAFT OPERATIONS (DAAO) FOR AIRCRAFT INSPECTION IN
ISSUING AIRWORTHINESS CERTIFICATE OF AIRCRAFT (C OF
A)
The DGCA (DAAO Office) shall have following function to ensurecompliance of the Aircraft inspection programme:• To plan Aircraft Inspection Annualy for Indonesia aircraft
registered.
• To designate Airworthiness Inspector to conduct AircraftInspection.
• To maintain Inspector Training and Experience meet withrequirement as per Staff Instruction SI 8900-1.3 Inspector TrainingSystem.
• To maintain report of aircraft inspection in DGCA (DAAO Office)and notify the findings of aircraft inspection to the operators.
• To ensure follow up actions.
• To ensure that root cause analysis is carried out by the operators toprevent repeat findings.
• To organize regular meetings with all airworthiness inspectors tomaintain a high standard of quality relating to:
o any changes/updates to the aircraft inspection procedures,
o feedback on quality issues with regard to aircraft inspectionreports e.g. incorrect entry's, mistakes, omissions, etc.,
• To carry out analysis of findings operator wise and finding wise andinitiate action for improvement if required.
• To initiate investigation depending upon seriousness of findingsreported and initiate enforcement action as per enforcement policyand procedures on the basis of investigation report if required.
DAAO coordination for aircraft inspection is performed by Sub-Directorate Maintenance for coordination of the program. To facilitatethe implementation of aircraft inspection activities a coordinatedapproach is needed at DAAO. The monitoring of the aircraft inspectionshall be done similarly as other surveillance activities. The recordsshould be stored in the DAAO IMSIS data base system.
5. FUNCTION OF DGCA REGIONAL OFFICE
The DGCA Regional Office shall have following function to ensurecompliance of the aircraft inspection programme:
• Regional office received order from DAAO to perform aircraftinspection, according to DAAO annualy plan.
• To designate airworthiness inspector to conduct aircraft inspection.
• To maintain Inspector Training and Experience meet withrequirement as per Staff Instruction SI 8900-1.3 Inspector TrainingSystem.
• To report of aircraft inspection to DGCA (DAAO Office) and notify thefindings of aircraft inspection to the operators.
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SI 8900-6.1
OCTOBER 2017
• To ensure follow up actions.
• To maintain in the DAAO IMSIS database aircraft inspection recordperformed by their regional office.
6. FUNCTION OF AIRWORTHINESS INSPECTOR ASSIGNED FOR THEAIRCRAFT INSPECTION
Airworthiness inspectors assigned for the aircraft inspection mustensure that the aircraft inspections are carried out efficiently followingthis Staff Instruction as per applicable check list and report generatedand submitted to the respective Inspector office (DAAOOffice or DGCA Regional Office).
CHAPTER III
AIRCRAFT INSPECTION PROCEDURES
1. Aircraft Inspection and Related Processes - Overview
Aircraft Inspection
Finding(s)
Corrective action
Issue 0 of A
a. The inspection process consists of different elements like thepreparation of the inspection, the determination of which items needto be inspected and which standards to use. General guidance onthe DGCA regulation references are placed at Appendix 2.
b. There are three different categories of findings, depending on theimpact the finding has on the safety of the aircraft and/or itsoccupants. Chapter 4 of this Staff Instructions provides guidance onthe categorization of findings.
c. Based on the outcome of the inspection and subsequentcategorization, follow-up actions as detailed in Chapter 5 shall betaken.
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SI 8900-6.1
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2. General Instructions - Aircraft Inspection
a. The main elements of the aircraft inspection are check generaldata, check aircraft status, perform physical aircraft inspection alsowitness of functional check, ground run and test flight (if necessary).
b.The inspection shall be as comprehensive as possible within thetime and resources available. The checklist to be used for carryingout the aircraft inspection (DGCA Form 21-40) is given at the StaffInstruction SI Form - 01.
c. The general principle shall be that the aircraft inspection,applicant must provide the available aircraft to inspect by DGCAinspector in sufficient time.
d. The applicant must prepare an aircraft for inspection by the DGCAinspector, the physical aircraft inspection time required by theDGCA inspector is at least 4 hours.
e. All findings during the physical aircraft inspection process must benotified to the accompan3dng operator's representative.
f. When conducting functional check, ground run and test flight, theoperator's representative must provide personnel who have training,licensed and experienced on the inspected aircraft.
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SI 8900-6.1
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CHAPTER IV
AIRCRAFT INSPECTION FINDINGS
1. General
Aircraft inspection aims at assessing the compliance with theapplicable standards of an aircraft used in operations. A non-compliance found during an inspection is called a finding.
Findings found during original and recurrent inspection must becompleted prior issuance of particular certificate.
Processing findings:
1. Issued letter to the operator
2. Received corrective action from operator
3. Communicate with operator
2. Findings - Categorization
If during the inspection it is established that a certain situation is notin compliance with the relevant standards, this is then considered afinding. For each inspection item, 3 (three) categories of possibledeviations from the standards have been defined. The findings arecategorized as below according to the seriousness and perceivedinfluence on flight safely.
Minor : Category 1 finding is considered to have a minorinfluence on safety.
SigniHcant : Categoiy 2 finding may have a significant influence onsafety
Major : Category 3 finding may have a major influence onsafety.
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SI 8900-6.1
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CHAPTER V
FOLLOW UP ACTIONS
1. Aircraft Inspection - Follow-up Actions
Follow up actions will be taken after the aircraft inspection. The follow-up actions may be distinguished in two stages. The first stage is thefollow-up action directly resulting from the findings, the second stage isthe monitoring and follow-up of any correspondence, sent out to theoperator.
2. Actions Resulting From An Inspection
Based on the results of the inspection and on how the findings havebeen categorized, following common follow-up actions may be used inorder of the seriousness of the findings.
1. Aircraft grounded by DGCA inspector
2. Corrective actions before issued the Airworthiness Certificate (C ofA)
3. No remarks
3. Aircraft Grounded By DGCA Inspection Team
If the category 3 (major) findings that have been established during theAircraft Inspection concern damage of a nature such that the aircraft isno longer airworthy, this has to be communicated immediately to theoperator. Although the first contact may be, as a matter of urgency,accomplished by telephone, it is advisable to use writtencommunication procedures.
An aircraft is grounded in a situation where the category 3 (three) majorfindings are not corrected by the operator before flight. Because thesafety of the aircraft and its occupants is at stake, the aircraft has to beprevented from resuming its flight and has to be ̂ grounded' until thesafety hazard is removedr
4. Generation And Distribution Of Aircraft Inspection Findings
The inspection report shall be generated after finalization of findings.The reports along with the findings shall be uploaded on IMSISdatabase. The Aircraft Inspection report along with findings shall bedistributed to operator.
The DGCA Regional Office should ensure the proper distribution ofAircraft Inspection Reports on Operators, with a copy to DGCA (DAAOOffice).
5. Further Follow Up
Any follow-up communication from the operators and the authoritiesshould be acknowledged and they should be informed about the closureof findings. Any request for clarification should equally be responded bythe DGCA (DAAO Office or Regional Office). The feedback or
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SI 8900-6.1
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clarifications from the DGCA (DAAO Office or Regional Office) should beperformed within 30 working days.
Findings should remain "open" as long as no satisfactory response ofthe operator. Findings could be closed if a re-inspection confirms thatthe appropriate corrective action was taken.
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CHAPTER VI
MONITORING OF AIRCRAFT INSPECTION DEFICIENCIES
1. Monitoring Deficiencies by DGCA (DAAO Office)
All deficiencies observed during aircraft inspection carried out by thevarious regional offices are required to be forwarded in a prescribedPerforma to the DGCA (DAAO Office) after the inspection.
2. Review at DGCA (DAAO office)
The review meeting for the compliance of aircraft inspection deficienciesis held at DGCA (DAAO Office), under the chairmanship of the Directorof Airworthiness and Aircraft Operations (DAAO).
The review of the aircraft maintenance program will be also carried outin the surveillance meeting. All major findings shall be discussed in themeeting to take a view on the action to be taken against the concernedorganization/operator/personnel.
3. Safety Related Issues
All , DGCA Airworthiness Inspector assigned for the Aircraft Inspectionshall report potential safety related issues reported during aircraftinspections and propose coordinated actions to the DAAO office whennecessary to address the problem.
Utilization of safety related information, necessaiy corrective actionsand appropriate effective preventive measures shall be initiated byDGCA to promote safety.
4. Records
All records related to Aircraft Inspection and follow up actions shall bemaintained at DGCA office and DGCA Regional Office. Soft copy of datashall be also maintained in IMSIS Database.
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APPENDIX 1
QUALIFICATION AND TRAINING OF INSPECTOR
1. Competencies of the Inspector
To cany out Aircraft Inspection in the most effective and efficientmanner, appropriate qualified and competent inspectors should bedeputed to cany out the task. This Chapter describes the trainingrequirements to reach the established level of competencies ofinspectors for this purpose. The DGCA (DAAO Office and RegionalOffice) should ensure that inspectors are competent to carry out thetasks assigned to them and that they are aware of the consequence oftheir actions for aviation safety.
2. Qualifications of the Inspector
The DGCA Inspector should meet the following qualification andexperience requirements:
a) Should have received initial and recurrent training as per StaffInstruction SI 8900-1.3 Inspector Training System and should befamiliar with CASR.
b) Should be familiar with the problems of operating or maintainingaircraft;
3. Aircraft CertiHcation Training
The training for aircraft inspection refer to SI 8900-1.3 InspectorTraining System
a. FCN 6003 Aircraft Certification.
b. FCN 6203 Major Repair and Alteration
c. FCN 61001 Airworthiness Directives
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APPENDIX 2
DGCA REFERENCES FOR AIRCRAFT INSPECTIONS GUIDANCE
Civil Aviation Safety Regulations Requirements
CASRPart91.
CASRPart 121.
CASR Part 135.
CASR Part 43.
CASR Part 45.
CASR Part 36
CASR Part 25.
PART I GENERAL DATA
I.A. AIRCRAFT MAKE MODEL
• Nationality 6b Registration Marks, Registration Number, Serial Number,Aircraft Category, Mfg. Year, Operator, TC/TCDS, Validation Number( Rev/Date), MTOW and Number OF SEATReference; TC, TCDS and Certificate of Registration
• TOTAL TIME, CURRENT INSPECTION, LAST INSPECTION (TSN/CSN),AIRCRAFT UTILIZATION DURING ONE YEAR (YEAR/ HOURS/CYCLES)
Reference: Aircraft Logbook
I.B. ENGINE MAKE & MODEL
• (S/N, TSN, CSN, TBO, Remaining)Reference: Engine Logbook
I.e. PROPELLER /ROTOR MAKE & MODEL
• (S/N, TSN, CSN, TBO, Remaining)
Reference: Propeller Logbook
I.D. APU MAKE & MODEL
• (S/N, TSN, CSN, TBO, Remaining)
Reference: APU Logbook
I.E. LANDING GEAR
• Nose L/G, Left Main L/G, Right Main L/G (P/N, S/N, TBO, Remaining)
Reference: Component Status
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PART II AIRCRAFT STATUS
II.A. Aircraft document and manual
• II.A.l. Certificate of Registration,Reference:
CASR 47
CASR 91.25
ILA.2. Certificate of Airworthiness
Reference:
CASR 21
CASR 91.25
II.A.3. Insurance
Reference:
CASR 47
CASR 91.25
II.A.4. Maintenance manual
Reference:
CASR 43
II.A.5. Weight and balance manualReference:
CASR 121.135(d)(7)CASR 121.153
CASR 121.165
CASR 135.135(d)(4)CASR 135.153
CASR 135.360
CASR 135.601
II.A.6. Wiring diagram manualReference:
CASR 43
II.A.7. Structure repair manualReference:
CASR 43
II.A.8. Illustrated part catalogReference:
CASR 43
II.A.9. Aircraft flight manual/ pilot operating handbookII.A. 10. Flight crew operating manualII.A. 11. Quick reference handbookReference:
CASR 91,25
CASR 91. 529(c)CASR 121.135(d)CASR 121.141
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CASR 121.143
CASR 121.173
CASR 135.135
CASR 135.143
CASR 135.173
CASR 135.175
CASR 135.183
CASR 135.303
CASR 135.307
II.A.12. Master MEL and/or MELReference:
CASR 91.509
CASR 121.135(c)(19)CASR 121 Appendix PCASR 135.303
CASR 135.321
CASR 135.443
CASR 135.445
CASR 135.611
CASR 135.637
II.A.13. Noise certificate
Reference:
CASR 21.183
CASR 36
CASR 91.25
CASR 91.525
CASR 91.529
II.A.14. Aircraft aeronautical station license
Reference:
CASR 91.25
Il.B. Logbook and test report
II.B.l. Aircraft flight/ maintenance logIl.B.2. Deferred item list (ie, HIL, CDL, DMI, DDR)Reference:
CASR 91.25
CASR 91.145
CASR 121.563
CASR 121.701
CASR 121.709
CASR 135.563
CASR 135.701
CASR 135.709
Il.B.3. Airframe, engine, propellerReference:
CASR 43.2
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II.B.4. Compass swing and data reportReference:
CASR 121.305
CASR 135.305
ILB,5. Weight and balance reportReference:
CASR 121.135
CASR 121.153
CASR 121.165
CASR 135.135
CASR 135.153
CASR 135.360
II.B.6. Altimeter and static system test reportReference:
CASR 43 Appendix ECASR 91.411
II.B.7. ATC transponder test report and mode S transponder encodingReference:
CASR 91.413
CASR 43 Appendix F
n.B.8. VOR inspection for IFRReference:
CASR 91.171
II.B.9. ELT test reportReference:
CASR 91.207
II.C. Aircraft inspection and maintenance reports
II.C. 1. Statement of build standard (new aircraft) from manufacturerReference:
CASR 21 Subpart H
II.C.2. Statement of accident/incident from the last operator (if any)Reference:
CASR 21.3
II.C.3. Approved maintenance program (Doc. No, revision, date)Reference:
CASR 91.409
CASR 135.367
CASR 121.367
II.C.4. Inspection work package for compliance, annual/100 Hrsinspection, structural inspection program, corrosionprotection control program, non routine inspection
Reference:
CASR 43 Appendix D
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CASR 121.367
CASR 135.367
CASR 135xGe
II.C.5. Component status (OC, CM, HT), life limited part (for bridging refAC 121-1)
Reference:
CASR 43.1
CASR 43.2
CASR 43.11
CASR 91.409
CASR 121.367
CASR 135.367
II.C.6. Airworthiness directives, alert service bulleting statusReference:
CASR 39
CASR 91.213
CASR 91.403
CASR 91.409
CASR 91.417
CASR 91.421
CASR 91.551
CASR 121.369
CASR 121.380
CASR 121.628
CASR 135.157
CASR 135.380
CASR 135.628
CASR 135.xGe
II.C.7. Damage and repair status and work package reportReference:
CASR 43.9
CASR 121.707
CASR 135.707
II.C.8. Alteration/modification status and work package andReference:
CASR 43 Appendix ACASR 121.707
CASR 135.707
II.C.9. Service difficulty reportReference:
CASR 121.703
CASR 135.703
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PART III AIRCRAFT INSPECTION
III.A. External Visual Inspection
III.A.l. Landing gear/ skid and wheel well areaIII.A. 1.1. Data plate, placards and markingReference:
CASR 45.11
CASR 45.13
III.A. 1.2. Sign of corrosion, wear, chafing lines or wiresReference: NIL
III.A. 1.3. Structural integrity of gears and doors for cracks, dents,other obvious damage
Reference: NIL
III.A. 1.4. Sign of leaks (struts, actuators valves, tube and hose)Reference: NIL
III.A. 1.5. Wheel installation and safety locking deviceReference:
CASR 43 Appendix D
III.A. 1.6. Tire condition
Reference:
CASR 43 Appendix D
III.A. 1.7. Brake installation for security, wear, condition and leaksReference:
CASR 43 Appendix D
III.A. 1.8. Skids and floats for security and conditionReference:
CASR 91.205
III.A. 1.9. Steering mechanism for security, wear, and conditionReference:
CASR91xA.2
III.A. 1.10. Brake pin indicator for minimum lengthReference: NIL
III.A. 1.11. Torque links for security and excessive playReference: NIL
III.A. 1.12. Fairing for security and missing fastenersReference: NIL
III.A. 1.13. Lighting for conditionReference: NIL
III.A. 1.14. Main gear static dischargeReference: NIL
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11I.A.2. Fuselage and EmpenageIII.A.2.1. Identification Plate
Reference:
CASR 45.11
CASR 45.30
a. Aircraft
It must be secured to the aircraft fuselage exterior so that it islegible to a person on the ground, and must be either
adjacent to and aft of the rearmost entrance door or on the
fuselage surface near the tail surfaces
Reference:
CASR 45.11
b. Manned Free Balloons
It must be secured to the balloon envelope and must be
located, if practicable, where it is legible to the operator whenthe balloon is inflated. In addition, the basket and heater
assembly must be permanently and legibly marked with the
manufacturer's name, part number (or equivalent), and serialnumber (or equivalent)
Reference:
CASR 45.11
c. Power Parachute and Weight Shift Control
It must be secured to the aircraft fuselage exterior so that it islegible to a person on the groundReference:
CASR 45.11
d. Additional Identification Plate (Nationality & RegistrationMarks)
It must be secured to the aircraft in a prominent positionnear pilot's entrance
Reference:
CASR 45.30
III.A.2.2. Nationality 85 registration marks and national flag forlegibility, location and size, and other marking requirements
Reference:
CASR 45.21
CASR 45.22
CASR 45.23
CASR 45.24
CASR 45.25
CASR 45.27
CASR 45.29
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III.A.2.3. Structure for cracks, corrosion, dents, rubbing and otherobvious damages
Reference: NIL
III.A.2.4. Exterior exit markings and exterior emergency lighting and
escape route
Reference:
CASR 121.310
CASR 135.349
III.A.2.5. Drain holes for obstruction stain or other sign of leaksReference: NIL
III.A.2.6. Radome, pitot tubes, static ports, stall warning, windshield,wiper, sensors, antennas, for condition, security 8e corrosion
Reference:
CASR91xA.2
CASR 25.1323
III.A.2.7. Loose/missing improper fasteners
III.A.2.8. Elevators, rudder and tabs for obvious damage, cracks,corrosions, rubbing and excessive play
Reference: NIL
III.A.2.9. Fire discharge dishes for indicationReference:
CASR 91.533
CASR 121.221
CASR 121.309
CASR 135.349
IILA.2,10. Lavatory (evidence of fresh blue water streaks)Reference:
CASR 121.308
CASR 135.347
CASR 25.820
CASR 25.854
IILA.3. Auxiliary Power Unit
IILA.3.1. Identification plate
Reference:
CASR 45.11
CASR 45.13
CASR 45.30
IILA.3.2. Door for security and missing/loose fastenerIII.A.3.3. Any indication of wear, leak, chaffing line, wire
Reference: NIL
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III.A.3.4. Fire extinguisher and sensor
Reference:
CASR 91.533
CASR 121.221
CASR 121.309
CASR 135.349
1II.A.4. Wings and Pylon
III.A.4.1. AH lights for general condition and broken lensesReference:
CASR 121.310
CASR 135.349
III.A.4.2. Structure for cracks, corrosion, dents and other damageIII.A.4.3. Fuel caps for security
IILA.4.4. Wing tip for general condition and damageIII.A.4.5. Anti/de-icing devices for condition and damageIII.A.4.6. Leading edge for dents, abrasion, obvious damage, and stall
warning for function condition
III.A,4.7. Leading edge devices, rubber boots, wiring, hoses, forcondition and leak
III.A.4.8. Evidence of fuel leaks;
III.A.4.9. Flaps, flaps track and flaps well for cracks, corrosion, leaks,abrasion, dents, delamination, and condition of connectors,
wiring, lines and hoses
III.A.4.10. Aileron and tabs for obvious cracks, corrosion, dents,
delimination, excessive play
III.A.4.11. Static discharge for condition;
III.A.4.12. Access panels/hatch/inspection door for security
Reference: Aircraft Maintenance Manual
III.A.5. Power Plants
ni.A.5.1. Engine identification plate
Reference:
CASR 45.11
CASR 45.13
CASR 45.30
III.A.5.2. Fan blade, turbine blade, and sensors for damage
III.A.5.3. Engine mount, cowling and pylons
III.A.5.4. Cowling 86 doors for security and missing/loose fasteners
III.A.5.5. Inlet cowl for dents, corrosion and abrasion
III.A.5.6. Acoustic, access panel for security, dents, corrosion,delimination and crack
III.A.5.7. Reverse doors for stowage security and leaks,
III.A.5.8. Exhaust for turbine/tail pipe damage and leaks
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III.A.5.9, Fire extinguisher bottle gauge for security and correctpressure
Reference: Engine and Aircraft Maintenance Manual
1II.A.6. Propeller/ Rotor
III.A.6.1. Propeller/rotor identification plateReference:
CASR 45.11
CASR 45.13
CASR 45.30
ni.A.6.2. Propeller blade and deicer boots, for dent, crack,deterioration, delamination and general condition
III.A.6.3. Drive shaft, yoke, swash plate, rotor head for wear, dent,crack, deterioration, delamination and general condition
III.A.6.4. Spinner for cracks and dent
III.A.6.5. Main rotor blades, for secured, wear, obvious damage, and
general condition (including color codes)
III.A.6.6. Tail rotor for secured, wear, obvious damage, and general
condition;
III.A.6.7. Tail rotor gearbox, drive shaft and oil level for security,
cracks, damage, leaks and general condition
Reference: Propeller, Rotor and Aircraft Maintenance Manual
III.B Interior Inspection
III.B. 1. Lavatory fire protection;
III.B. 1.1. Each lavatory in the airplane must be equipped with a smoke
detector system or equivalent provides a warning light in the
cockpit or provides a warning light or audio warning in the
passenger cabin readily detected by a flight attendant
III.B. 1.2. Each lavatory in the airplane must be equipped with a built-
in fire extinguisher and capable of automatic discharge, for
each disposal receptacle for towels, paper, or waste located in
the lavatory
III.B.2. Emergency Equipment and Additional Emergency Equipment
note: Each item of emergency and flotation equipment:
(1) Must be inspected regularly, and so indicated date of lastinspection;
(2) Must he readily accessible to the crew;
(3) Must be clearly identified and clearly marked to indicate itsmethod of operation; and
When carried in a compartment or container, must be marked
on the compartment or container, the date of last inspection
III.B.2.1. Hand Fire Extinguisher
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Note:
a. At least two of the required hand fire extinguisher installedin passenger cariying airplanes must contain Halon 1211(CASR 121.309) or equivalent extinguisher agent.
b. At least one of the required hand fire extinguisher installedin passenger canying airplanes must contain Halon 1211(CASR 135.349)
c. For individual Certificate of Airworthiness is first issued on
or after 31 December 2016 shall not be of a type listed inthe 1987 Montreal Protocol (Annex A, Group II.)
1. Halon 1211
2. Halon 1301
3. Halon 2402
A. At least one hand fire extinguisher must be conveniently
located for use:
i. in each galley compartment
ii. in each class E cargo compartment
iii. on the flight deck
B. In passenger compartment, at least one Halon 1211
(CASR 121.309)
7 - 30 at least one
31 - 60 at least two
61-200 Minimum 3 ea
201-300 Minimum 4 ea
301-400 Minimum 5 ea
401-500 Minimum 6 ea
501-600 Minimum 7 ea
> 600 Minimum 8 ea
In passenger compartment (CASR
135.349)
> 9 at least one
In passenger compartment (CASR
91.533)
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—r^^-30
0-50
at least oneMinimum 1 ea
> oU
51 - 150 Minimum 2 ea
151-250 Minimum 3 ea
> 250 Minimum 4 ea
> 9 pax seat (CASR 135. 349)
III.B.2.2. First Aid Kit, must be readily acessible to the crew, storedsecurely, free form dust, moisture and temperature (CASR
121 App. A)
First Aid Kit, must be readily acessible to the crew, stored
securely, free form dust, moisture and temperature (CASR
91.533)
0 - 100 Minimum 1 ea
101 - 200 Minimum 2 ea
201 -300 Minimum 3 ea
301 -400 Minimum 4 ea
401 - 500 Minimum 5 ea
>500 Minimum 6 ea
IILB.2.3. Emergency Medical Kit (check contain in accordance with
appendix A)
At least one (CASR 121 Appendix A)
In airplanes for which a flight attendant is reqxiired ( CASR
135.349)
III.B.2.4. Crash Axe
a. Each airplane accommodating more than 19
passengers (CASR 91.533)
b. Each airplane operated under CASR 135 that
has a lockable non frangible door separating the flight deck
from the passenger cabin (CASR 135,349)
c. Each airplane operated under CASR 121 (CASR
121.309)
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III.B.2.5. Megaphone (CASR 91.533, 121.309)61 -99 1 ea (rearward)
> 99 2 ea (forward &rearward
)
III.B.2.6. Emergency Exit (CASR 91.607, CASR 135.349, CASR121.310)
a. Interior Emergency Exit marking, placement and legibility
b. Lighting for interior emergency exit marking
c. Emergency exit operating handles and instruction
d. Emergency exit access, must be unobstructed
III.B.2.7. Portable lights, ensure available for each flight attendant seat
and accesible from each fight attendant seat (CASR 91.205,CASR 121.310, CASR 135.357)
III.B.2.8 Protective Breathing Equipment (CASR 121.337)a. One in flight deck
b. One PBE is required for each hand fire extinguisher
located for use in a galley
c. One PBE is required for each hand fire extinguisher in pax
compartment (located within 3 feet from hand firex)d. One for use in each Class A, B, and E cargo compartment
III.B.2.9 Portable O^^gen (CASR 121.333)
III.B.2.10 Emergency Locator Transmitter, type 406 (CASR 91.207).
Note: If the aircraft installed with fixed and deployableautomatic type transmitters, it must be attached to the
airplane as far aift as practicable
a. Type of ELT
Automatic Fixed (AF)
Automatic Portable (AP)
Automatic Deployable (AD)
Survival (S)
b. < 20 passenger seat at least one (automatic)
Record ELT Battery due:
c. > 19 passengers for which the individual certificate of
airworthiness is first issued after 1 July 2008 at least two(one of which shall be automatic)
Record ELT Battery due:
and
d. ELT annual inspection (after the last inspection) for:
(iv) Proper installation
(v) Battery corrosion
(vi) Operation of the controls and crash sensor
44
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OCTOBER 2017
The presence of a sufficient signal radiated from its antenna
e. ELT encoding
III.B.3. Emergency Equipment for Overwater Operation (CASR 91,207, 91.223, CASR 121.309, 121.339, CASR 135.349,135.351, 135.355)
III.B.4. Miscellaneous Equipment (CASR 121.313, 135.321)
III.B.4.1. Spare of protective fuse or bulb (if installed)
HI.B.4.2. A windshield wiper or equivalent for each pilot stationIII.B.4.3. Two independent static pressure systems
III.B.4.4. A means to monitor from the flight deck side of the door the
area outside the flight deck door (except for cargo)
III.B.4.5. Door between the passenger and pilot or crew rest
compartments, for transport category and/or cargo operation
with a mtow in excess of 45.500 kg or with a passenger
seating greater than 60
III.B.4.6. A placard on each door of access to a an emergency exit, toindicate that it must be open during takeoff and landing
III.B.5. Passenger Information (CASR 121.317)III.B.5.1. Passenger information marking and placard in Bahasa or
Bilingual (Bahasa - English) (CASR 21.29 a.3)
a. Fasten seat belt sign or placard is visible from each
passenger seat
b. No smoking sign or placard, in cabin and lavatory
III.B.6. Public Address System
III,B.6,1. Public Address System (more than 19 pax) (CASR 121.318,CASR 135.331)
(note: Transport category manufactured after December 1996)III.B.7. Crewmember Interphone System
III.B.7.1. Crewmember Interphone System (more than 19 pax) (CASR
121.319, CASR 135.333)
III.B.8. Passenger Briefing Card
III.B.8.1. Passenger Briefing Card (CASR 91.537(b), CASR 121.503(b),
CASR 135.107(b)
III,B.9. Seats, Safety Belts, Shoulder Harnesses, and Child Restraint
Systems (CASR 121.311, CASR 135.119, CASR 91.521)III.B.9.1. Passenger seats, seat belts, cushion/upholstery materials,
armrest for condition, reclining mechanism for properoperations
III.B.9.2. Exit seat, check table, reclining mechanism to make sure notblocking emergency exit ( CASR 121.585, 135.121)
III.B.9.3. Child Restraint System, check for security
III.B.9.4. At each flight deck station equipped with a combined safety
belt and shoulder harness, check for security
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III.B.IO. Cargo and Bagggage Compartment (CASR 121.221)
III.B.lO.l. Fire precaution
a. Class "A" (All parts of the compartment are easily accesible
and fire therein would be ready discernible to a crewmember)
There must be a hand fire extinguisher available for each
Class A compartment.
b. Class "B" (Enough access for crew member to reach all
the compartment and no smoke, flame or extingushingagent enter the compartment occupied by crew or
passanger)
(1) It must have a separate approved smoke or fire detectorsystem to give warning at the pilot or flight engineerstation
(2) There must be a hand fire extinguisher available for thecompartment
(3) It must be lined with fire resistant material
c. Class "C" (Not conform with requirement Class A, B, D orE)
1. It must have a separate smoke or fire detector system togive warning at the pilot or flight engineer station
2. It must have an approved built-in fire extinguishingsystem controlled from the pilot or flight engineer station
3. It must be designed to exclude hazardous quantities ofsmoke, flames, or extinguishing agents from enteringinto any compartment occupied by the crew or passenger
4. It must have ventilation and draft controlled so that the
extinguishing agent provided can control any fire thatmay start in the compartment
5. It must be lined with fire resistant material
d. Class "D" (Designed and constructed that a fire occuringtherein will be completely confined without endargingthesafety of the airplane or occupants)
1. It must have a means to exclude hazardous quantities ofsmoke, flames, or noxious gases from entering anycompartment occupied by the crew or passengers
2. Ventilation and drafts must be controlled within each
compartment
3. It must be completely lined with fire resistant material
e. Class "E" for Cargo only
1. It must be completely lined with fire resistant material
2. It must have a separate system of an approved typesmoke or fire detector to give warning at the pilot or flightengineer station
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3. It must have a means to shut off the ventilating air flowto or within the compartment and the controls for thatmeans must be accessible to the flight crew in the crewcompartment
4. It must have a means to exclude hazardous quantities ofsmoke, flames, or noxious gases from entering the flightcrew compartment
III.B. 10.2. Check cargo door for leaks, damage and general condition
III.B.10.3. Smoke detectors for damage
III.B. 10.4. Lighting is operable and protective cover is installed
lll.B.10.5. Flooring and pallet system for general condition
III.B. 10.6. Placard of weight limitation for availability and legibility
lll.B.10.7. A 9G cargo net for condition (if applicable)
III.C. COCKPIT INSPECTION
INSTRUMENT, EQUIPMENT MARKING, PLACARD ARE CORRECTLYINSTALLED AND LEGIBLE.
III.C. 1. Instrument for VFR (day) (CASR 91.205)III. C. 1.1. Airspeed indicator
III. C. 1.2. Altimeter
III. C. 1.3 Magnetic Direction IndicatorIII.C. 1.4. A tachometer for each engine
III.C. 1.5 A cylinder head temperature indicator for each air cooled eng.III.C. 1.6. Oil in temperature indicator for each engineIII.C. 1.7. A fuel quantity indicator for each fuel tankIII.C. 1.8. An oil pressure indicator for each engineIII.C. 1.9. A manifold pressure indicator for each engineIII.C.1.10. Landing gear position indicator, if the aircraft has a
retractable landing gear
III.C.2. Instrument for IFR (CASR 91.205), specified requirement VFR(day)
III.C.2.1. GjTTOScopic rate of turn indicatorIII. C. 2.2. Slip / Skid indicator
III.C.2.3. Sensitive altimeter adjustable for barometric pressureIILC.2.4. Clock
IILC.2.5. Gyroscopic pitch and bank indicator (AH)III.C.2.6. Gyroscopic direction indicator (directional gyro or equivalent)
III.C.3. Flight and Navigation Instrument (CASR 121.305)III.C.3.1. An airspeed indicating system with heated pitot tubeIII.C.3.2. Two sensitive pressure altimeterIII.C.3.3. Clock
III.C.3.4. A free air temperture indicatorIII.C.3.5. Gyroscopic pitch and bank indicator (AH)
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III.C.3.6. Gjn-oscopic rate and turn indicator combined with an integralskip/skid indicator (turn and bank indicator)
III.C.3.7. Gjnroscopic direction indicator (dyrectional gyro or equivalent)III.C.3.8. A magnetic compass
III.C.3.9. A vertical speed indicator (rate of climb indicator)
III.C.3.10. Two Gyroscopic pitch and bank indicator (AH) or :
Third Gyroscopic pitch and bank indicator (AH) for :
(i). turbojet ,or
(ii). turbo prop having pax seat >30 or payload > 7500 lbs
III.C.4, Engine Instrument (CASR 121.307)
III.C.4.1. Oil in temperature indicator for each engine
III.C.4.2. A fuel pressure indicator for each engineIII.C.4.3, A means for indicating fuel quantity for each fuel tank
III.C.4.4. An oil pressure indicator for each engineIII.C.4.5. An oil quantity indicator for each oil tank
111,0.4.6. An independent fuel pressure warning device for each engineor a master warning device for all engines
III.0.5. Flight and navigation Instrument (OASR 135.305)III.0.5.1. Two independent airspeed indicating systemIII.0.5.2. Two independent sensitive altimeter system
III.0.5.3. Clock
III.0.5.4. A free air temperature indicator
III.0.5.5. GjToscopic direction indicator (directional gyro or equivalent)III.0.5.6. A magnetic compass
III.0.5.7. GjToscopic pitch and bank indicator (AH)III.0.5.8. Vertical speed indicator (rate of climb indicator)
III.0.5.9. Two Gyroscopic pitch and bank indicator (AH) for turbojetand turbo prop.
III.0.5.10. Third Gyroscopic pitch and bank indicator (AH) for turbojet
III.0.6. Engine Instrument (OASR 135.317)III.0.6.1. A tachometer for each engine
III.0.6.2. A carburetor air temperature indicator for each engineIII.0.6.3. A cylinder head temperature indicator for each air cooled eng.III.0.6.4. Oil in temperature indicator for each engine
III.0.6.5. A fuel pressure indicator for each engineIII.0.6.6. A fuel flowmeter or fuel mixture indicator for each engine not
equipped with an automatic altitude mixture control
III.0.6.7. A means for indicating fuel quantity for each fuel tank
III.0.6.8. An oil pressure indicator for each engineIII.0.6.9. An oil quantity indicator for each oil tank
III.0.6.10. An independent fuel pressure warning device for each engineor a master warning device for all engines
III.0.6.11. A device for each reversible propeller
48
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III.C.6.12. A manifold pressure indicator for each engine
IILC.7. Navigation and Radio Communication (CASR 91.205, CASR91.175CASR, 91.215, CASR 121.99, CASR 121.349, CASR
135.309, CASR 135.311, CASR 121,345,)
III.C.7.1. HF
III.C.7.2. VHF
III,C.7.3. ATC Transponder
III.C.7.4. VOR
III.C.7.5. DME
III.C.7.6. ILS
IILC.8. EQUIPMENTS
III.C.8.1. Weather Radar (CASR 121.357, 135.315)
III.C.8.2. 1. TCAS (CASR 91.227)
Turbine, MTOW>33.000 lbs (15.000 Kg) for whichthe individual Airworthiness Certificate is first issued after 31
December 2015, shall be equipped with TCAS II2. TCAS (CASR 121.356)
a. Turbine, MTOW>33.000 lbs (15.000 Kg), TSO 119a,
version 6,04A Enhance or equivalent installed before
May 1, 2003
TSO 119b, version 7.1 or a later or equivalent
b. Combi airplane PaxlO - 30 seat TCAS I TSO 118
c. Piston, MTOW>33.000 lbs TCAS I TSO 118
III.C.8.3. TAWS (CASR 121.354, CASR 135.319)
TSO C-151Class A or equivalent for >9 pax
TSO C-151Class B or equivalent for 6-9 pax
CASR 91.229
MTOW > 5700 kg or Pax seat >9
TSO C-151 or equivadent
III.C.8.4. GPS/INS/Doppler Radar/ONS/IRS or FMS
(CASR 121.355, CASR 121.358)
III.C.8.5. Low altitude windshear system (CASR121.352)
Aeroplanes (except turboprop) manufactured after 2 January1991, must be equipped with either an approved airborne
windshear warning & flight guidance system, an approvedairborne detection & avoidance system, or combination ofthese systems
ni.C.8.6. Pitot Heat Indicating System (CASR 121.342, CASR 135.325)
All transport category aicraft (CASR 121.342)>20 pax (CASR 135.325)
III.C.8.7. Flight Data Recorder, check for applicability and type of FDR
CASR 91.233 and Appendix E (Airplane), F (Helicopter)
49
SI 8900-6.1
OCTOBER 2017
AIRPLANE
i Ail airplane first issue of C of A on or after IJanuaiy 1989with maximum certificated take-off mass more than
27.000 kg (Type I FDR)
ii All airplane first issue C of A on or after 1 Jan. 1989 with
maximum certificated take-off mass more than 5.700 kg,up to and including 27.000 kg Ciype II FDR)
iii All airplane first issue of C of A after 1 January 2005 withmaximum certificated take-off mass more than 5.700 kg(Type lA)
iv All turbine engine airplane first issue of C of A on or after1 January 2016 with a seating configuration of more than5 passenger seat and maximum certificated take-off mass
of 5700 kg or less (Type II)HELICOPTER
i All helicopters first issued of C of A on or after 1 January2016 with maximum certificated take-off mass more than
3180 kg (Type IVA)ii All helicopters first issued of C of A on or after 1 January
1989 with maximum certificated take-off mass more than
7000 kg or having a passanger seating configuration ofmore than 19 (Type IV)Record ULB Battery due:Annual read out for required number of parameter to berecorded and quality (measurement range, recordinginterval, accuracy, resolution)
Calibration for 5 year or at least 2 year in accordance with
manufacturer recommendation
III.C.8.8. CVR/CARS (CASR 91.235)AIRPLANE
1 All turbine-engine airplanes, for which the individualcertificate of airworthiness was first issued on or after 1
Januaiy 2016, with a seating configurations of more thanfive passenger seats and a maximum certificated take-off
mass of 5 700 kg or less shall be equipped with either aCVR or a CARS
ii All turbine-engine airplanes for a maximum certificatedtake-off mass of over 5 700 kg for which the individualcertificate of airworthiness was first issued on or after 1
January 2016 and required to be operated by more thanone pilot shall be equipped with a CVR
ill All airplanes of a maximum certificated take-off mass ofover 27 000 kg for which the individual certificate of
airworthiness is first issued on or after 1 Januaiy 1987shall be equipped with a CVR
50
SI 8900-6.1
OCTOBER 2017
HELICOPTER
i All helicopters of a maximum certificated take-off mass of
over 7 000 kg for which the individual certificate ofairworthiness is first issued on or after 1 January 1987
shall be equipped with a CVR. For helicopters not
equipped with an FDR, at least main rotor speed shall be
recorded on the CVR
ii All helicopters of a maximum certificated take-off mass of
over 7 000 kg for which the individual certificate of
airworthiness was first issued before 1 January 1987 shall
be equipped with a CVR. For helicopters not equipped with
an FDR, at least main rotor speed shall be recorded on the
CVR
From 1 January 2016, a magnetic tape 85 wire shall be
discontinued, and capable of two hours recording
From 1 Januaiy 2016, all CVR shall be capable of
retaining the information recorded during at least the last
two hours of their operation
Record ULB Battery, due:
Annual Examination
III.C.9. Lighting (CASR 91.209, CASR 121.323, CASR 135.307)
111. C. 9.1. Instrument light
III.C.9.2. Anti Collision lightIII. C.9.3. Position/Navigation light
III. C. 9.4. Two Landing light
III.C.9.5. Taxi light
III.C.9.6. Logo light
III.C.9.7. Cabin light (ceiling, windows, service, entry, exit, etc.)
PART IV FUNCTIONAL CHECK
IV.A Aircraft System
rV.A. 1. Flight control system
IV.A.2. Recording system (FDR, CVR)
IV.A.3. Fire precaution (engine, APU, cargo)
IV.A. 4. Smoke detector system (lavatory, cargo)
IV.A.5. Public address system and interphone system
Reference: Aircraft Maintenance Manual
IV.A. 6. Pitot heat indicating system
Reference:
CASR 121.342
CASR 135.325
IV.A.7. Lighting (nav. Light, anti-collision light, instrument light,
landing light, emergency light, passenger information light)
IV.A. 8. ELTtest
Reference: Aircraft Maintenance Manual
51
SI 8900-6.1
OCTOBER 2017
IV.A.9. Other applicable systems.
Reference: Aircraft Maintenance Manual
IV.B. Communication
IV.B.l. HF, VHF, ATC transponder
Reference: Aircraft Maintenance Manual
IV.C. Navigation
IV.C.l. ADF, VCR, DME, ILS
IV.C.2. Weather radar
Reference: Aircraft Maintenance Manual
IV.C.3. TAWS TSO 0151 class A and windshear
Reference:
CASR 121.352
IV.C,4. TCAS
IV.C.5. GPS/INS/IRS/FMSReference: Aircraft Maintenance Manual
PART V GROUND RUN AND TEST FLIGHT
V, 1. Ground run and test flight conducted according to test planeV.2. Ground run and test result
V.3. Test flight result
Reference: Aircraft Maintenance Manual
52
SI 8900-6.1
OCTOBER 2017
APPENDIX 3
AIRCRAFT INSPECTION CHECKLIST
Instruction to complete Aircraft Inspection Checklist (DGCA Form 21-40)
1) Inspection Place and Date (e.g. CGK, 2 October 2017, SUB, 2 October2017)
2) Aircraft Make Model (e.g. B737-800, ATR 72-600, BELL 429, A320-200)
3) Nationality and Registration Mark (E.G. PK-GIA, PK-DON, PK-LMA)
4) Registration Number : refer to Certificate of Registration (e.g. 1234, 3456,789)
5) Serial Number: Manufacture Serial Number (MSN) (e.g. 549, 2124, 3107)
6) Aircraft Category: refer to TO or TODS (e.g. Transport, Normal, Utility)
7) Manufacture Year: (e.g. 1990, 2000, 2017)
8) Operator : name of aircraft operator (e.g. Garuda, Lion, Sriwijaya)
9) TC/TC Validation Number: number of TO or TO Validation (e.g. A008HOOl, B002)
10) TC/TC Validation Revision: Revision index of TC or TC validation
11) TC/TC Validation Date : Date of TC or TC validation
12) MTOW: Maximum Take of Weight refer to TCDS
. 13) Total Time (TSN fis CSN): Time Since New (TSN) and Cycle Since New referto Aircraft Log Book
a. Total Time Current DGCA Inspection (TSN 86 CSN) : Time Since New (TSN)and Cycle Since New (CSN) when DGCA conduct aircraft Inspection referto Aircraft Log Book
b. Total Time Last DGCA Inspection (TSN 86 CSN): Time Since New (TSN) andCycle Since New (CSN) previous year DGCA conduct aircraft Inspectionrefer to Aircraft Log Book)
14) Aircraft Utilization During One Year (Per 31 December): Check to TSN andCSN per 31 December (e.g. TSN 31 December 2016 minus TSN 31December 2015)
15) Engine Make Model: (e.g. CFM 56-7, JT8D, RR250, PT6A, Trent 700 )16) Engine Serial Number: Manufacture Serial Number (MSN) (e.g. 549, 2124
3107)
17) Engine TSN: Time Since New (TSN) refer to Engine Log Book
18) Engine CSN: Cycle Since New (CSN) refer to Engine Log Book
19) Engine TBO: Time Between Overhaul (TBO) engine refer to CAMP, AMM orMPD
20) Engine Remaining; remaining TSN or CSN of engine compare with TBO '
21) Propeller/Rotor Make and Model: (e.g. Hartzel HC-B3TN-3DY)
22) Propeller/Rotor Serial Number Manufacture Serial Number (MSN) (e.g.549, 2124, 3107)
53
23) Propeller/Rotor TSN: Time Since New (TSN) refer to Propeller/Rotor LogBook
24) Propeller/Rotor CSN: Cycle Since New (CSN) refer to Propeller/Rotor LogBook
25) Propeller/Rotor TBO: Time Between Overhaul (TBO) propeller/rotor referto CAMP, AMM or MPD
26) Propeller/Rotor Remaining: remaining TSN or CSN of propeller/rotorcompare with TBO
27) APU Make and Model: (e.g. GTCP331-350)
28) APU Serial Number: Serial Number Manufacture Serial Number (MSN)(e.g. 549, 2124, 3107)
29) APU TSN: Time Since New (TSN) refer to APU Log Book
30) APU CSN: Cycle Since New (CSN) refer to APU Log Book
31) APU TBO: Time Between Overhaul (TBO) APU refer to CAMP, AMM orMPD
32) APU Remaining: remaining TSN or CSN of APU compare with TBO
33) Nose Landing Gear (part Number, Serial Number, TBO and Remaining)
34) Left Main Landing Gear (part Number, Serial Number, TBO andRemaining)
35) Right Main Landing Gear (part Number, Serial Number, TBO andRemaining)
36) Satisfactory Boxes: Tick for each inspection item performed "YES" or "NO"
37) Remark Boxes: Tick if fmding(s) are noted for each inspection item
38) Action Taken Select the action taken. Information to the representative ofoperator is defaulted action to be taken
a) [0) No remarks
b) (1) Corrective action before issued C ofA
c) (2) Aircraft grounded by DGCA Inspector
39) Item: Inspection item, e.g (ILA.12. Master MEL and/or MEL, II.B.3.Airframe, engine, propeller. III.A. 1.1. Data plate, pacards and marking)
40) Cat: Enter finding category based:G: General remarks or observations1: Category 1 finding is considered to have a minor influence on safety2: Categoiy 2 finding may have a significant influence3: Category 3 finding may have a major influence on safety
41) Remark and Finding : Indicate the detail(s) of the remark or observationor finding
42) Senior Inspector Signature: Inspector(s) name and signature
43) Assign inspector Signature: Inspector(s) name and signature
54
iifemA
MINISTRY OF TRANSPORTATION
DIRECTORATE GENERAL OF CIVIL AVIATION
Gedung Perkantoran Bandara Soekamo-Hatta
Jl. 03, Cengkareng - Tangerang
website: www.dephub.go.id; e-mail: [email protected]
INSPECTION RECORDS ISSUANCE OF ORIGINAL / RECURRENTCERTIFICATE OF AIRWORTHINESS
1). Inspection place and date
iPAimi^MERaLlD^T^M
2). A. AIRCRAFT MAKE MODEL:
3). Nationality &
Registration
Marks
4).
Registration
Number
5). Serial
Number
6). Aircraft
Category7). Mfg
Year
8). Operator
9). TO/TO VaUdation
Number.
10). TC/TC
Validation Revision
11 . TC/TC
Validation Date
12). MTOW
13). Total Time
a). Current DGCA Inspection b). Last DGCA Inspection
TSN (FH)
CSN (PC)
14). Aircra !t utilization duringone year (per 31 December)
Year: Hours Cycles:
15.) B. ENGINE MAKE £s MODEL:
No. 16). Serial Number 17). TSN 18). CSN 19). TBO 20). Remaining
21.) C. PROPELLER/ROTOR MAKE & MODEL:
No. 22). Serial
Number
23). TSN 24). CSN 25). TBO 26). Remaining
1
2
3
4
5
6
27.) D. APU MAKE & MODEL:
No. 28). Serial
Number
29). TSN 30). CSN 31). TBO 32). Remaining
1
E. LANDING GEAR
Nomenclature Part Number Serial Number TBO Remaining
33). Nose L/G
34). Left Main L/G
35). Right Main L/G
A. Aircraft Document & Manual (as applicable)
(check for currency and condition)
Item Description 36).
Satisfactory37). Remarks
Yes No
n.A.i Certificate of Registration
II.A.2 Certificate of Airworthiness
II.A.3 Insurance
II.A.4 Maintenance Manual
II.A.5 Weight & Balance Manual
II.A.6 Wiring Diagram Manual
II.A.7 Structure Repair Manual
II.A.8 Illustrated Part Catalog
II.A.9 Aircraft Flight Manual / Pilot
Operating Handbook
II.A.10 Flight Crew Operating Manual
II.A.11 Quick Reference Handbook
II.A.12 Master M.E.L and M.E.L
II.A.13 Noise Certificate
II.A.14 Aircraft Aeronautical Station License
B. Log Book and Test Report
Item Description 36).
Satisfactory
37). Remarks
Yes No
II.B.l Aircraft Flight/Maintenance Log
n.B.2Deferred item list (ie. HIL, CDL, DMI,
DDR)
II.B.3 Aiframe, Engine, Propeller
II.B.4 Compass Swing Data Report
II.B.5Weight 8b Balance Report
(CASR 121.153, CASR 135.153)
II.B.6Altimeter 8b Static System Test
Report
(CASR 91.411, CASR 43 App. E)
II.B.7ATC Transponder Test Report
(CASR 91.413, CASR 43 App. F)
Mode S Transponder encoding
II.B.8VOR inspection for IFR (CASR
91.171)
II,B.9ELT Test Report (CASR 91.207)
C. Aircraft Inspection and Maintenance Records
Item Description 36).
Satisfactory
37). Remarks
Yes No
II.C.l Statement of Build Standard (new
aircraft) from manufacturer
II.C.2 Statement of accident/incident fromthe last operator (if any)
^7
II.C.3 Approved Maintenance Program
(Doc. No, Revision, Date)
II.C.4 Inspection work package for
compIiance:(CASR91.409,135.367,121.367)
Latest inspection type:
date:
at:
/ TSN/CSN
Annual / 100 Hrs Inspection
Structural Inspection Program
Corrosion Protection Control
Program
Non routine inspection
II.C.5 Component status (OC, CM, HT) SsLife Limited Part
(for bridging refAC 121-1)
II.C.6 Airworthiness Directives 85 Allert
Service Bulletin Status
II.C.7 Damage and Repair status and work
package report
II.C.8 Alteration/Modification status andwork package
II.C.9 Service Difficulty Report
tg^|^l^^RC^EgUNSP£C7IONfl|||HA. External Visual Inspection
1. Landing gear / skid and wheel well area
Item Description 36).
Satisfactory
37). Remarks
Yes No
Data plate, placards and marking
III.A.1.2 Sign of corrosion, wear, chafing lines
or wires
iir.A.1.3 Structural integrity of gears and
-58
doors for cracks, dents, otherobvious damage
III.A.1.4 Sign of leaks (struts, actuatorsvalves, tube and hose)
III.A.1.5 Wheel installation and safety lockingdevice
III.A.1.6 Tire condition
III. A. 1.7 Brake installation for security, wear,condition and leaks
III.A.1.8 Skids and floats for security andcondition
III.A.1.9 Steering mechanism for security,wear, and condition
III.A.1.10 Brake pin indicator for minimum
length
iii.A.i.n Torque links for security andexcessive play
III.A.1.12 Fairing for security and missingfasteners
III.A.1.13 . Lighting for condition
III.A.1.14 Main Gear Static Discharge
2. Fuselage and Empenage
Item Description 36).
Satisfactory37). Remarks
Yes No
III.A.2.1 Identification Plate (CASR 45.11)
a. Aircraft
It must be secured to the aircraft
fuselage exterior so that it is legibleto a person on the ground, and mustbe either adjacent to and aft of therearmost entrance door or on the
fuselage siorface near the tail
surfaces
b. Manned Free Balloons
It must be secured to the balloon
envelope and must be located, ifpracticable, where it is legible to the
operator when the balloon is
inflated. In addition, the basket and
heater assembly must be
permanently and legibly markedwith the manufacturer's name, part
number (or equivalent), and serial
number (or equivalent).
c. Power Parachute and Weight Shift
Control
It must be secured to the aircraft
fuselage exterior so that it is legibleto a person on the ground.
d. Additional Identification Plate
(Nationality & Registration Marks)
CASR 45.30).
It must be secured to the aircraft in
a prominent position near pilot's
entrance
III.A.2.2 Nationality & Registration Marks
and National Flag for legibility,location and size, and other marking
requirements (CASR 45.21, 45.22,
45.23, 45.24, 45.25. 45.27, 45.29)
III:a.2.3 Structure for cracks, corrosion,
dents, rubbing and other obvious
damages
III.A.2.4 Exterior Exit markings and exterior
emergency lighting and escape route(CASR 121.310, 135.349)
III.A.2.5 Drain holes for obstruction stain or
other sign of leaks
III.A.2.6 Radome, pitot tubes, static ports,stall warning, windshield, wiper,sensors, antennas, for condition,security 8b corrosion
Iir.A.2.7 Loose/missing improper fasteners
in.A.2.8 Elevators, rudder and tabs for
obvious damage, cracks, corrosions,
rubbing and excessive play
III.A.2.9 Fire discharge dishes for indication
m.A.2.10 Lavatory Servicing Areas (evidence of
fresh blue water streaks)
3. APU
Item Description 36).
Satisfactory
37). Remarks
Yes No
III.A.3.1 Identification Plate
m.A.3.2 Door for security and missing/loosefastener
III.A.3.3 Any indication of wear, leak, chaffingline, wire
III.A.3.4 Fire extinguisher and sensor
4. Wings and Pylon
Item Description 36).
Satisfactory37). Remarks
Yes No
m.A.4.1 AH lights for general condition and
broken lenses
III.A.4.2 Structure for cracks, corrosion,
dents and other damage
III.A.4.3 Fuel caps for security
III.A.4.4 Wing tip for general condition and
damage
III.A.4.5 Anti/de-icing devices for conditionand damage
ni.A.4.6 Leading edge for dents, abrasion,
obvious damage, and stall warningfor function condition
III.A.4.7 Leading edge devices, rubber boots,
wiring, hoses, for condition and leak
III.A.4.8 Evidence of fuel leaks
III.A.4,9 Flaps and flaps track for cracks,
corrosion, leaks, abrasion, dents,delamination, and condition of
wiring, lines and hoses
III.A.4.10 Aileron and tabs for obvious cracks,
corrosion, dents, delimination,
excessive play
m.A.4.11 Static discharge for condition
III.A.4.12 Access panels/hatch/inspection
door for security
5. Power plants
Item Description 36).
Satisfactory
37). Remarks
Yes No
III.A.5.1 Engine Identification Plate (CASR
45.11)
It must be affixed to the engine at an
accessible location
III.A.5.2 Fan blade, turbine blade, and
sensors for damage
in.A.5.3 Engine mount, cowling and pylons
III.A.5.4 Cowling & doors for security and
missing/loose fasteners
III.A.5.5 Inlet cowl for dents, corrosion and
abrasion
III.A.5.6 Acoustic, access panel for security,
dents, corrosion, delimination and
crack
III.A.5.7 Reverse doors for stowage security
and leaks
III.A.5.8 Exhaust for turbine/tail pipe
damage and leaks
IILA.5.9 Fire extinguisher bottle gauge for
security and correct pressure
6. Propeller / Rotor
Item Description 36).
Satisfactory37). Remarks
Yes No
nLA.6.1 Propeller/rotor Identification Plate
(CASR 45.11)
It must be affixed to the propeller atan accessible location
III.A.6.2 Propeller blade and deicer boots, fordent, crack, deterioration, '
fn
delamination and general condition
IILA.6.3 Drive shaft, yoke, swash plate, rotor
head for wear, dent, crack,
deterioration, delamination and
general condition
in.A.6.4 Spinner for cracks and dent
ni.A.6.5 Main rotor blades, for secured, wear,
obvious damage, and general
condition (including color codes)
III.A.6.6 Tail rotor for secured, wear, obvious
damage, and general condition
m.A.6.7 Tail rotor gearbox, drive shaft and oil
level for security, cracks, damage,
leaks and general condition
B. Interior Inspection
1. Lavatory Fire Protection (CASR 121.308, CASR 135.347)
Item Description 36).
Satisfactory
37). Remarks
Yes No
Each lavatory in the airplane must
be equipped with a smoke detector
system or equivalent provides a
warning light in the cockpit or
provides a warning light or audio
warning in the passenger cabin
readily detected by a flight attendant
III.B.1.2 Each lavatory in the airplane must
be equipped with a built-in fire
extinguisher and capable ofautomatic discharge, for eachdisposal receptacle for towels, paper,
or waste located in the lavatory
2. Emergency Equipment and Additional Emergency Equipment (CASR 91.207, 91.533, CASR 121.309, CASR 121.310, CASR 121 App. A, CASR 135.349)
note: Each item of emergency and flotation equipment:
(4) Must be inspected regularly, and so indicated date of last inspection;
(5) Must be readily accessible to the crew;
(6) Must be clearly identified and clearly marked to indicate its method of operation;and
(7) When carried in a compartment or container, must be marked on the compartment
f.1
or container, the date of last inspection
Hand Fire Extinguisher
Note:
a. At least two of the required handfire extinguisher installed in
passenger carrying airplanes mustcontain Halon 1211 (CASR 121.309)or equivalent extinguisher agent.
b. At least one of the required handfire extinguisher installed in
passenger carrying airplanes must
contain Halon 1211 (CASR 135.349)
c. For individual Certificate of
Airworthiness is first issued on or
after 31 December 2016 shall not
be of a type listed in the 1987
Montreal Protocol (Annex A, GroupII.)
1. Halon 1211
2. Halon 1301
3. Halon 2402
A. At least one hand fire
extinguisher must be convenientlylocated for use:
i. in each galley compartment
ii. in each class E cargo
compartment
iii. on the flight deck
B. In passenger compartment, at
least one Halon 1211 (CASR121.309)
7-30
31 - 60
at least one
at least two
AA
61-200 Minimum 3 ea
201-300 Minimum 4 ea
301-400 Minimum 5 ea
401-500 Minimum 6 ea
501-600 Minimum 7 ea
> 600 Minimum 8 ea
In passenger compartment (CASR
135.349)
>9 at least one
In passenger compartment (CASR
91.533)
7-30 at least one
> 30 at least two
m.B.2.2 First Aid Kit, must be readily
acessible to the crew, stored
securely,
free form dust, moisture and
temperature (CASR 121 App. A)
0-50 Minimum 1 ea
51-150 Minimum 2 ea
151-250 Minimum 3 ea
>250 Minimum 4 ea
> '9 pax seat (CASR 135. 349)
First Aid Kit, must be readily
acessible to the crew, stored
securely, free form dust, moisture
and temperature (CASR 91.533)
0- 100 Minimum 1 ea
101 -200 Minimum 2 ea
201 -300 Minimum 3 ea
301-400 Minimum 4 ea
401 - 500 Minimum 5 ea
>500 Minimum 6 ea
III.B.2.3 Emergency Medical Kit (check
contain in accordance with appendixA)
At least one (CASR 121 Appendix A)
In airplanes for which a flightattendant is required ( CASR135.349)
III.B.2.4Crash Axe
a. Each airplane accommodatingmore than 19 passengers (CASR91.533)
b. Each airplane operated underCASR 135 that has a lockable non
frangible door separating the flightdeck from the passenger cabin(CASR 135.349)
c. Each airplane operated underCASR 121 (CASR 121.309)
III.B.2.5 Megaphone (CASR 91.533, 121.309)
61 -991 ea (rearward)
>992 ea (forward &
rearward)
III.B.2.6Emergency Exit (CASR 91.607,CASR 135.349, CASR 121.310)
a. Interior Emergency Exit
marking, placement and legibility
b. Lighting for interior emergencyexit marking
c. Emergency exit operating
handles and instruction
d. Emergency exit access, must
be unobstructed
III.B.2.7 Portable lights, ensure available for
each flight attendant seat and
accesible from each fight attendantseat (CASR 91.205, CASR 121.310,
CASR 135.357)
III.B.2.8 Protective Breathing Equipment(CASR 121.337)
fxf.
a. One in flight deck
b. One PBE is required for eachhand fire extinguisher located foruse in a galley
c. One PBE is required for eachhand fire extinguisher in paxcompartment (located within 3 feetfrom hand firex)
d. One for use in each Class A,B, and E cargo compartment
III.B.2.9 Portable Ojgrgen (CASR 121.333)
m.B.2.10 Emergency Locator Transmitter, type406 (CASR 91.207).
Note: If the aircraft installed with
fixed and deployable automatic type
transmitters, it must be attached to
the airplane as far aft as practicable
a. Type of ELT
Automatic Fixed (AF)
Automatic Portable (AP)
Automatic Deployable (AD)
Survival (S)
b. < 20 passenger seat at least one
(automatic)
Record ELT Battery due:
c. > 19 passengers for which theindividual certificate of airworthiness
is first issued after 1 July 2008 at
least two (one of which shall be
automatic)
Record ELT Battery due:
and
d. ELT annual inspection (after
the last inspection) for:
(vii) Proper installation
(viii) Battery corrosion
(ix) Operation of the controls andcrash sensor
(x) The presence of a sufficientsignal radiated from its antenna
e. ELT encoding
3. Emergency Equipment for Overwater
Operation (CASR 91, 207, 91.223, CASR
121.309, 121.339, CASR 135.349, 135.351,135.355)
4. MisceUaneous Equipment (CASR 121.313, 135.321)
Spare of protective fuse or bulb (ifinstalled)
III.B.4.2 A windshield wiper or equivalent for
each pilot station
III.B.4.3 Two independent static pressuresystems
III.B.4.4 A means to monitor from the flightdeck side of the door the area
outside the flight deck door (exceptfor cargo)
III.B.4.5 Door between the passenger andpilot or crew rest compartments, fortransport category and/or cargooperation with a mtow in excess of
45.500 kg or with a passengerseating greater than 60.
III.B.4.6 A placard on each door of access to a
an emergency exit, to indicate that it
must be open during takeoff and
landing
5. Passenger Information (CASR 121.317)
III.B.5.1 Passenger information marking and placard in Bahasa or Bilingual (Bahasa -English) (CASR 21.29 a.3)
a. Fasten seat belt sign or placard is
visible from each passenger seat
b. No smoking sign or placard, incabin and lavatory
A9
6. Public Address System
Public Address System (more than
19 pax) (CASR 121.318, CASR
135.331)
(note: Transport category
manufactured after December 1996)
7. Crewmember Interphone System
Crewmember Interphone System(more than 19 pax) (CASR 121.319,
CASR 135.333)
8. Passenger Briefing Card
ni.B.8.1 Passenger Briefing Card (CASR
91.537(b), CASR 121.503(b), CASR
135.107(b).
9. Seats, Safety Belts, Shoulder Harnesses, and Child Restraint Systems (CASH
121.311, CASH 135.119, CASH 91.521)
UI.B.9.1 Passenger seats, seat belts,
cushion/upholstery materials,armrest for condition, recliningmechanism for proper operations
III.B.9.2 Exit seat, check table, reclining
mechanism to make sure not
blocking emergency exit ( CASR
121.585, 135.121)
III.B.9.3 Child Restraint System, check for
security
III.B.9.4 At each flight deck station equipped
with a combined safety belt and
shoulder harness, check for security.
10. Cargo and Bagggage Compartment (CASH 121.221)
III.B.lO.l Fire precaution
A. Class "A" (All parts of thecompartment are easily accesible
and fire therein would be ready
discernible to a crew member)
There must be a hand fire
extinguisher available for each Class
A compartment.
B. Class "B" (Enough access for
crew member to reach all the
compartment and no smoke, flame
or extingushing agent enter the
compartment occupied by crew or
passanger)
(4) It must have a separateapproved smoke or fire detectorsystem to give warning at the pilot orflight engineer station
(5) There must be a hand fireextinguisher available for thecompartment
(6) It must be lined with fireresistant material
C. Class "C" (Not conform with
requirement Class A, B, D or E)
(1) It must have a separate smokeor fire detector system to givewarning at the pilot or flightengineer station
(2) It must have an approvedbuilt-in fire extinguishing systemcontrolled from the pilot or flightengineer station
(3) It must be designed to excludehazardous quantities of smoke,flames, or extinguishing agents fromentering into any compartmentoccupied by the crew or passenger
(4) It must have ventilation anddraft controlled so that the
extinguishing agent provided cancontrol any fire that may start in thecompartment
(5) It must be lined with fireresistant material
D. Class "D" (Designed and
constructed that a fire occuringtherein will be completely confined
without endargingthe safety of the
airplane or occupants)
(1) It must have a means toexclude hazardous quantities ofsmoke, flames, or noxious gasesfrom entering any compartmentoccupied by the crew or passengers
(2) Ventilation and drafts must becontrolled within each compartment
(3) It must be completely linedwith fire resistant material
70
E. Class "E" for Cargo only
(1) It must be completely linedwith fire resistant material
(2) It must have a separatesystem of an approved type smoke orfire detector to give warning at thepilot or flight engineer station
(3) It must have a means to shutoff the ventilating air flow to orwithin the compartment and thecontrols for that means must beaccessible to the flight crew in thecrew compartment
(4) It must have a means toexclude hazardous quantities ofsmoke, flames, or noxious gasesfrom entering the flight crewcompartment
Iir.B.10.2 Check cargo door for leaks, damageand general condition
III.B.10.3 Smoke detectors for damage
III.B.10.4 Lighting is operable and protectivecover is installed
m.B.10.5 Flooring and pallet system forgeneral condition
III.B.10.6 Placard of weight limitation foravailability and legibility
III.B.10.7 A 9G cargo net for condition (ifapplicable)
C. COCKPIT INSPECTION
INSTRUMENT, EQUIPMENT MARKING, PLACARD ARE CORRECTLY INSTALLED ANDLEGIBLE.
1. Instrument for VFR (day) (CASR 91.205]
Item Description 36).
Satisfactory37). Remarks
Yes No
71
nr.c.i.i Airspeed indicator
III.C.1.2 Altimeter
III.C.1.3 Magnetic Direction Indicator
m.c.1.4 A tachometer for each engine
III.C.1.5 A cylinder head temperature
indicator for each air cooled eng.
III.C.1.6 Oil in temperature indicator for eachengine
III.C.1.7 A fuel quantity indicator for each
fuel tank
III.C.1.8 An oil pressure indicator for each
engine
m.c.1.9 A manifold pressure indicator for
each engine
III.C.l.lO Landing gear position indicator, if
the aircraft has a retractable landinggear
2. Instrument for IFR (CASR 91.205), specified requirement VFR (day)
Item Description 36).
Satisfactory37). Remarks
Yes No
III.C.2.1 Gyroscopic rate of turn indicator
III.C.2.2 Slip/Skid indicator
m.C.2.3 Sensitive altimeter adjustable forbarometric pressure
III.C.2.4 Clock
m.c.2.5 Gyroscopic pitch and bank indicator
(AH)
m.C.2.6 G3n-oscopic direction indicator
(directional gyro or equivalent)
3. Flight and Navigation Instrument (CASR 121.305)
Item Description 36).
Satisfactory37). Remarks
Yes No
70
III.C.3.1 An airspeed indicating system with
heated pitot tube
III.C.3.2 Two sensitive pressure altimeter
III.C.3.3 Clock
III.C.3.4 A free air temperture indicator
III.C.3.5 Gjroscopic pitch and bank indicator
(AH)
III.C.3.6 Gyroscopic rate and turn indicator
combined with an integral skip/skid
indicator (turn and bank indicator)
III.C.3.7 Gyroscopic direction indicator(d5rrectional g3rro or equivalent)
IILC.3.8 A magnetic compass
III.C.3.9 A vertical speed indicator (rate of
climb indicator)
III.C.3.10 Two Gyroscopic pitch and bank
indicator (AH) or :
Third Gyroscopic pitch and bank
indicator (AH) for:
(i). turbojet ,or
(ii). turbo prop having pax seat >30
or payload > 7500 lbs
4. Engine Instrument (CASK 121.307)
Item Description 36).
Satisfactory37). Remarks
Yes No
III.C.4.1 Oil in temperature indicator for each
engine
in:c.4.2 A fuel pressure indicator for each
engine
m.C.4.3 A means for indicating fuel quantityfor each fuel tank
m.C.4.4 An oil pressure indicator for each
engine
III.C.4.5 An oil quantity indicator for each oiltank
7-?
III.C.4.6 An independent fuel pressure
warning device for each engine or amaster warning device for all engines
5. Flight and navigation Instrument (CASR 135.305)
Item Description 36).
Satisfactory37). Remarks
Yes No
III.C.5.1 Two independent airspeed indicatingsystem
III.C.5.2 Two independent sensitive altimeter
system
III.C.5.3 Clock
III.C.5.4 A free air temperature indicator
III.C.5.5 G3Toscopic direction indicator
(directional gyro or equivalent)
ni.C.5.6 A magnetic compass
III.C.5.7 Gyroscopic pitch and bank indicator(AH)
III.C.5.8 Vertical speed indicator (rate ofclimb indicator)
III.C.5.9 Two G5rroscopic pitch and bank
indicator (AH) for turbojet and turboprop.
III.C.5.10 Third G3Toscopic pitch and bank
indicator (AH) for turbojet
6. Engine Instrument (CASR 135.317)
Item Description 36).
Satisfactory37). Remarks
Yes No
III.C.6.1 A tachometer for each engine
ni.C.6.2 A carburetor air temperature
indicator for each engine.
III.C.6.3 A cylinder head temperatureindicator for each air cooled eng.
IILC.6.4 Oil in temperature indicator for each
engine
74
III.C.6.5
IILC.6.6
III.C.6.7
A fuel pressure indicator for each
engine
A fuel flowmeter or fuel mixture
indicator for each engine notequipped with an automatic altitudemixture control
A means for indicating fuel quantityfor each fuel tank
III.C.6.8 An oil pressure indicator for each
engine
III.C.6.9 An oil quantity indicator for each oil
tank
III.C.6.10 An independent fuel pressurewarning device for each engine or amaster warning device for all engines
III.C.6.11 A device for each reversible propeller
III.C.6.12 A manifold pressure indicator for
each engine
7. Navigation and Radio Communication (CASH 91.205, CASR 91.175CASR, 91.215,CASK 121.99, CASR 121.349, CASR 135.309, CASR 135.311, CASR 121.345,)
Item
IILC.7.1
Description
HF .ea
36).
Satisfactory
Yes No
37). Remarks
III.C.7.2 VHF .ea
Ill.C.7.3 ATC Transponder .ea
III.C.7.4 VOR .ea
IIl.C.7.5 DME .ea
III.C.7.6 ILS .ea
8. EQUIPMENTS
Item Description 36).
Satisfactory
Yes No
37). Remarks
III.C.8.1 Weather Radar
(CASR 121.357,
135.315)a
7^
III.C.8.2 1. TCAS (CASR 91.227)
Turbine,
MTOW>33.000 lbs
(15.000 Kg) for
which the
individual
Airworthiness
Certificate is first
issued after 31
December 2015,
shall be equippedwith TCAS II
ea
2. TCAS (CASR 121.356)
(i) Turbine,
MTOW>33.000 lbs
(15.000 Kg),TSO
119a, version 6,04A
Enhance or
equivalent installed
before May 1, 2003
TSO 119b,
version 7.1 or a
later or equivalent
(ii) Combi
airplane PaxlO - 30
seat TCAS I
TSO 118
(iii) Piston,
MTOW>33.000 lbs
TCAS I TSO 118
.ea
.ea
.ea
m.C.8.3 TAWS (CASR
121.354, CASR
135.319)
TSO C-151Class A
or equivalent for >9
pax
TSO C-151ClassB
or equivalent for 6 -
9 pax
a
CASR 91.229
MTOW > 5700 kg orPax seat >9
TSO C-151 or
equivalent
a.
III.C.8.4 GPS/INS/Doppler
Radar/ONS/IRS or
FMS
(CASR 121.355,
CASR 121.358)
a
III.C.8.5 Low altitude windshear system
(CASR121.352)
Aeroplanes (except turboprop)manufactured after 2 January 1991,
must be equipped with either an
approved airborne windshear warningSs flight guidance system, an approved
airborne detection & avoidance
system, or combination of these
systems
III.C.8.6 Pitot Heat Indicating System (CASR
121.342, CASR 135.325)
(1) All transport category aicraft(CASR 121.342)
(11) >20 pax (CASR 135.325)
III.C.8.7 Flight Data Recorder, check for
applicability and type of FDR CASR
91.233 and Appendix E (Airplane), F
(Helicopter)
AIRPLANE
(i) All airplane first issue of C of Aon or after IJanuary 1989 withmaximum certificated take-off mass
more than 27.000 kg (Type I FDR)
(ii) All airplane first issue C of A onor after 1 Jan. 1989 with maximum
certificated take-off mass more than
5.700 kg, up to and including 27.000
ni
kg (Type II FDR)
(iii) All airplane first issue of C of Aafter 1 Januaiy 2005 with maximumcertificated take-off mass more than
5.700 kg [Type lA)
(iv) All turbine engine airplane firstissue of C of A on or after 1 Januaiy2016 with a seating configuration ofmore than 5 passenger seat andmaximum certificated take-off mass of
5700 kg or less (Type 11)
HELICOPTER
(i) All helicopters first issued of C
of A on or after 1 Januaiy 2016 with
maximum certificated take-off mass
more than 3180 kg (Type IVA)
(ii) All helicopters first issued of C
of A on or after 1 Januaiy 1989 with
maximum certificated take-off mass
more than 7000 kg or having a
passanger seating configuration of
more than 19 (Type IV)
Record ULB Batteiy due:
Annual read out for required number
of parameter to be recorded and
quality (measurement range,recording interval, accuracy,resolution)
Calibration for 5 year or at least 2
year in accordance with
manufacturer recommendation
III.C.8.8 CVR/CARS (CASR 91.235)
AIRPLANE
(i) All turbine-engine airplanes, forwhich the individual certificate of
airworthiness was first issued on or
after 1 January 2016, with a seatingconfigurations of more than fivepassenger seats and a maximumcertificated take-off mass of 5 700 kgor less shall be equipped with either aCVR or a CARS.
(ii) All turbine-engine airplanes fora maximum certificated take-off mass
78
of over 5 700 kg for which theindividual certificate of airworthiness
was first issued on or after 1 January2016 and required to be operated bymore than one pilot shall be equippedwith a CVR.
(iii) All airplanes of a maximumcertificated take-off mass of over 27
000 kg for which the individualcertificate of airworthiness is first
issued on or after 1 January 1987shall be equipped with a CVR.
HELICOPTER
(i) All helicopters of a maximum
certificated take-off mass of over 7
000 kg for which the individual
certificate of airworthiness is first
issued on or after 1 January 1987
shall be equipped with a CVR. For
helicopters not equipped with anFDR, at least main rotor speed shall
be recorded on the CVR.
(ii) All helicopters of a maximum
certificated take-off mass of over 7
000 kg for which the individual
certificate of airworthiness was first
issued before 1 January 1987 shall beequipped with a CVR. For helicopters
not equipped with an FDR, at leastmain rotor speed shall be recorded on
the CVR.
From 1 January 2016, a magnetic
tape & wire shall be discontinued,
and capable of two hours recording
From 1 January 2016, all CVR shall
be capable of retaining the
information recorded during at leastthe last two hours of their operation
Record ULB Batteiy, due:
Annual Examination
9. Lighting (CASR 91.209, CASR 121.323, CASR 135.307)
Item Description 36).
Satisfactory
37). Remarks
Yes No
70
III.C.9.1 Instrument light
III.C.9.2 Anti Collision light
III.C.9.3 Position/Navigation light
ni.C.9.4 Two Landing light
m.C.9.5 Taxi light
III.C.9.6 Logo light
III.C.9.7 Cabin light (ceiling, windows, service,entiy, exit, etc.)
A« Aircraft System
Item Description 36).
Satisfactory
37). Remarks
Yes No
IV.A. 1 Flight control system
IV.A.2 Recording system (FDR, CVR)
IV.A.3 Fire precaution (Engine, APU, Cargo)
IV.A.4 Smoke detector system (Lavatory,Cargo)
IV.A.5 Public address system 85 InterphoneSystem
IV.A.6 Pitot heat indicating system CASR121.342, CASR 135.325
IV.A.7 Lighting (nav. light, anti-collision
light, instrument light, landing light,emergency light, passenger
information light)
IV.A.8 ELT test
IV.A.9 Other Applicable System
B. Communication
Item Description
1
36).
Satisfactory37). Remarks
Yes No
IV.B.l HF, VHF, ATC Transponder |1
sn
C. Navigation
Item Description 36).
Satisfactory
37). Remarks
Yes No
IV.C.l ADF, VOR, DME, ILS
IV.C.2 Weather Radar
IV.C.3 TAWS TSO C151 Class A 85
Windshear (CASR 121.352)
IV.C.4 TCAS
IV.C.5 GPS/INS/IRS/FMS
Nav. data base due period:
Item Description 36).
Satisfactory
37). Remarks
Yes No
V.l Ground run and test flight conductedaccording to test plan
V.2 Ground Run Test result
V.3 Test Flight result
Aircraft grounded by DGCA inspector
Corrective actions before issued the Airworthiness Certificate (C of A)
No remarks
lREKli\^RK(©R4BINiyuN,uifiuseaiset)arateisneeHas
61
SENIOR INSPECTOR
Name/ Signature / Date
ASSIGNED INSPECTOR
Name/ Signature / Date
Note:
This form can also be used to record airworthiness inspection for issuance of Export Certificate ofAirworthinessfor Aircraft. Special requirements of importing country must be considered to include in the inspection record.Finding must be clearly addressed prior to get an acceptance from importing country, when it intended to be putas an exemption to Export Certificate of Airworthiness.
DIRECTOR GENERAL OF CIVIL AVIATION
signed
Dr. Ir. AGUS SANTOSO,M.Sc
s6^uai aslinyaD4GIAN HUKUM
/O
lAltP&feNAMA SARI^cnilSina / (IV/a)
NIP. 19680704 199503 2 001
87