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FORM ING-002

CIELOS DEL PERU S.A.WORK CARD

COVER SHEETCompany W/C N° Orig W/C N° Rev. N° Rev. Date RII Involved

1-WC-MP-10LM-007 10LM-007 1

August 7,

2006 YES NO

Model A/C Reg N° Related Card Zone Access Area

DC10 NONE100, 200, 300, 400,500, 600, 700, 800

NONEWHOLE AND COMPLETE

AIRCRAFT

TITLE

PRE-FLIGHT

EFFECTIVITY

Aircrafts

Engines

Appliances

Reg. Nº / Serial Numbers: N831LA / 46936 N833LA / 46937 N305FE / 47870 N609GC / 46932

N614GC / 46931 N68044 / 46903

OB-1749 / 46891 Initial/Interval E/MH E/ET Crew Skill ATA

N°

DUE DATE

Version 1 2.0 2.0

Threshold C/MH Task Req. COMPLIANCE

Repeat DAILY GVI

1

A&P

Mechanic,

Avionic

Mechanic

12

Tools

NONE

Consumable material

NitrogenSkydrol 500 B4

Exxon 2380

Oxygen

Parts

NONE

Engineering Approval Feed Back Instructions

Prepared by: Wilfredo Rodríguez

Date: August 7, 2006

Eng Chief: Eng. Ladislav Petric

Date: August 7, 2006

After performing this W/C, communicate to Engineering andPlanning Department to keep an accomplishment record on

the fleet.

Compliance RecordA/C – ESN – Appliance S/N: Mechanic: Inspector (RII If required):

Station Date: Date:

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FORM ING-002

CIELOS DEL PERU S.A. WORK CARD

W/C N° Rev N° Date A/C N° or ESN Pages

1-W/C-MP-10LM-007 1August 7,

2006 1 of 11

General NotesThis Work Card was issued to perform a General Visual Inspection of the aircraft for proper configuration and

acceptable conditions. Perform every 24 hrs. or each crew change, whichever comes first.

General Visual Inspection (GVI) - A visual examination that will detect obvious unsatisfactory

conditions/discrepancies. This type of inspection may require removal of fillets, fairings, access panels/doors, etc.

Work stands ladders, etc. may be required to gain proximity.

Step by Step Work InstructionsSTEPS Mechanic Inspector

STEP 1 : COCKPIT PREPARATION

NOTE: Enter your initials after performing each operation.

-

Pressurize hydraulic system (Ref. DC10-AMM 29-00-00).____- Extend flaps and slats. Tag appropriate controls and circuit

breakers.____

STEP 2: EXTERIOR INSPECTION


Perform General Visual Inspection of the following areas for proper

configuration and acceptable conditions (Refer to Figure 1) with the following

items:

1.

LEFT FORWARD FUSELAGEA. Check fluid leaks, security of access panels and skin

condition.____

B. Verify that outflow valves are in full open position.____

C. Verify potable water door and system for condition.____

D. Check left static ports for damage, condition, alignment and noapparent restrictions.____

E. Check that air conditioning packs 1 and 2 doors are closed and

secured.____

F. Check that air conditioning pack 1 and 2 exhaust area is

clear.____

G. Inspect left fuselage landing light for correct alignment and

general condition.____

H. Check that air conditioning pack 1 and 2 inlet area is clear.____

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Step by Step Work InstructionsSteps Mechanic Inspector

I. Check left angle of attack sensor for security.____

J. Verify that oxygen blowout disc is intact.____

K. Verify that all access doors are closed and secured (Lavatory

Service Panel, Avionics Compartment Lower Door).____

L. Check pitot probes for damage, condition, alignment and no

apparent restrictions.____

M. Check the radome skin for external condition and security.____

N. Check that windshield wipers are out of view.____

2. NOSE LANDING GEAR AND NOSE WHEELWELL

A. Inspect nose landing and taxi lights for correct alignment and

general condition.____

B. Inspect nose wheelwell light for general condition.____

C. Check nose gear safety pin and steering bypass valve pin are

removed.____

D. General condition of the gear and tires. Inspect for cuts, FODand correct inflation (Table 1).____

E. Observe strut extension is per chart placard.____

F. Scissors links connected quick-disconnect pins engaged fullyand ground shift mechanism rod for correct alignment.____

G. Verify that bulkhead access door is closed.____

H. Inspect sound proofing blankets do not obscure viewing tubes(for N registration) or viewing window (for OB

registration).____

I. Check for fluid leaks.____

J. Verify that nose landing gear doors are closed and secured.____

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3. RIGHT FORWARD FUSELAGE

A. Check the TAT probe for security and general condition.____

B. Check right angle of attack sensor for security.____

C. Check that air conditioning pack 3 inlet area is clear.____

D. Inspect right fuselage landing light for correct alignment and

general condition.____E. Check that air conditioning pack 3 door is closed and

secured.____

F. Check that air conditioning pack 3 exhaust area is clear.____

G. Check ADG door for security.____

H. Check right static ports for damage, condition, alignment and no

apparent restrictions.____

I. Inspect forward cargo compartment. Look at the items that

follow:- Cargo door lock viewing windows clean.____- Cargo door seals and mechanism for condition and correctly

installed.____- Cargo moving equipment for condition and correctly

installed.___

- Cargo compartment lining for condition.____

J. When forward cargo door is closed, inspect handle latched andvent door is in the correct position. Inspect external latch viewer

for door pin engagement as per placard.____

K. Check cabin pressure relief vents and valves for general

condition.____

L. Verify that all access doors are closed and secured (Center

Accessory Compartment Door).____

M. Inspect right wing and engine scan light, and taxi and runaway

turnoff light for correct alignment and general condition.____

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4. PYLON AND ENGINE 3

A. Check 1st

stage fan blades, nose cowl interior and N1 sensingheads for foreign object damage.____

B. Check for fluid leaks, loose cowling latches, access doors

properly closed (Engine Oil Tank Access Door; CSD, Pneumatic

Starter and AC Generator Access Door).____

C. Check reverser for damage/properly stowed.____

D. Check the low pressure turbine for damaged blades, metal in

tailpipe.____

5. RIGHT WING

A. Check access doors, wing tip and lights for security and generalcondition.____

B. Check access panels for missing fasteners and generalcondition.____

C. Check ailerons, flaps, spoilers and slats for damage and general

condition.____

D. Check for damaged or missing static discharges.____

E. Check gear down indicator for the correct position.____

F. Fuel level sticks and fuel panels are flush and fastened.____

G. Check fuel vent and fuel dump pipe for no fuel leakage.____

6. RIGHT, LEFT AND CENTER MAIN LANDING GEARS

A. Check general condition of gear and tires. Inspect for cuts, FODand correct inflation (Table 1).____

B. Inspect brake lines and wear indicator pins.____

C. Observe strut extension is per chart placard. CLG piston press

1000psi.____

D. Verify that gear safety pins are removed.____

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E. Check for fluid leaks.____

F. Verify that gear doors are properly closed and secured.____

G. Inspect wheelwell lights for general condition.____

7. RIGHT CENTER AND AFT FUSELAGE

A. Inspect center shroud drains and cavity drain valves for presence

of fuel.____

B. Inspect center cargo compartment. Look at the items that follow:

- Cargo door lock viewing windows clean.____

- Cargo door seals and mechanism for condition and correctlyinstalled.____

- Cargo moving equipment for condition and correctly

installed.___

- Cargo compartment lining for condition.____

C. When center cargo door is closed, inspect handle latched and vent

doors are in the correct position. Inspect external latch viewer fordoor lock pin engagement as per placard.____

APU

NOTE: Perform the following items with APU turned off. Use

the necessary equipment to get access to the APU

Compartment.

A. Oil supply; check and replenish as necessary with lubricatingoil.____

B. Fuel supply; check and drain as necessary.____

C. APU compartment door is closed and latched.____

D. APU inlet and exhaust area is clear.____

E. Access doors and panels are closed and fastened.____

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8. TAIL PYLON AND ENGINE 2

A. From ground level, check for indications of damage, fluid leaks

access doors, cowling latches and work platform fairings properlyclosed, reverser stowed.____

9. EMPENNAGE

A. From ground level check for indications of damage, fluid leaksand general condition.____

B. Access doors and panels are closed and fastened.____

C. Check horizontal and vertical stabilizers, rudder and elevators fordamage and general condition.____

D. Check for damaged or missing static dischargers.____

E. Check the tail cone for security and general condition.____

10. LEFT AFT FUSELAGE

A. Inspect aft cargo compartment. Look at the items that follow:

- Cargo door lock viewing windows clean.____

- Cargo door seals and mechanism for condition and correctly

installed.____- Cargo compartment lining for condition.____

- Cargo net for condition and installation.____

B. When aft cargo door is closed, inspect handle latched and vent

doors are in the correct position. Inspect external latch viewer for

door lock pin engagement as per placard.____

11. LEFT WING

A. Check access doors, wing tip and lights for security and generalcondition.____

B. Check access panels for missing fasteners and general

condition.____

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STEP 2: INTERIOR PRE-FLIGHT


A. Crew seats, seat belts and harnesses for condition.____

B. Cockpit windows for condition.____

C. Perform a General Visual Inspection of flight deck emergency

equipment and systems per condition: service crew oxygen

cylinders as required in Table 2.____

D. Perform the following electrical tests:

- Voice Recorder test (Refer to AMM 23-71-01).____

- Cargo door test.____

- Windshield heat test.____

- Fuel system test.____- Emergency Lights.____

- External and Wheel well lights.____

- Cockpit and Instrument lights.____

NOTE: Assure that Oxygen Masks are in correct location perLOPA.

E. Cockpit door for condition and operation.____

F. Make sure the following documents are displayed on the cockpitdoor.____

- Certificate of Airworthiness.____

- Aircraft Registration.____

- Radio License.____

- Certificate of Liability Insurance.____

- ELT C-406-2 Maintenance Certificate.____

- “Constancia de Conformidad” (only for N registered).____

NOTE: Radio license only to N register aircraft.

G. Verify L1 and R1 lights and emergency accumulator pressure.___

H. Verify that appropriate manuals are onboard.____

I. Perform a General Visual Inspection of the Main CargoCompartment and system as required.____

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J. After all items are completed; ensure that equipment and

personnel are clear of control surface area. Remove tags from

controls and circuit breakers, close circuit breakers and positionflaps and slats to retract position.____

K. Verify that gear pins are removed prior to departure and stored inupper closet at L1 door. Make log page entry for Pre-Flight

completed.____

NOTE: (Before push back) Check that access doors L1 & R1,

fwd, center & aft lower cargo compartment doors

and main cargo door are closed and secured (view

pin on sight).

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FORM ING-002




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Tables

TABLE 1

POSITION NORMAL PRESSURE

REPLACE ON TIRE IF

FOUND WITH

FOLLOWING PRESS

REPLACE BOTH TIRES

SAME AXLE IF FOUND

WITH FOLLOWING

PRESS

MLG 205 PSI 150 PSI BELOW 130 PSI

CLG 175 PSI 130 PSI BELOW 112 PSI

NLG 190 PSI 150PSI BELOW 126 PSI

CAUTION: DRY NITROGEN SHOULD BE USED FOR TIRE INFLATION (REF. AD

87-08-09). FAILURE TO OBEY COULD CAUSE DAMAGE TO THE

AIRCRAFT.

TABLE 2

NOTE: Crew oxygen pressure: minimum dispatch pressure 1450 PSI at 21.2°C (70°F).

Service oxygen to 1850 PSI if pressure is below 1650 PSI. Make ITV entry as

required.

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Step by Step Work InstructionsFigures

Figure 1

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