(A03) :00001 :0 :2 A1 Mach meter ( A ) (true airspeed) ( B ) (indicated airspeed) ( C )(equivalent airspeed) (installation error) :00002 :0 :1 B2pressure altitude true altitude( A ) 29.92 ( B ) ( C )indicated airspeed pressure altitude :00003 :0 :2 C3 constant power outside air temperature ( A )true altitude ( B )true altitude ( C )true altitude :00004 :0 :2 B4local altimeter setting( A ) ( B ) ( C ) (terrain clearance) :00005 :0 :1 C5(IFR flight)(preflight check) ( A ) (calibrated altitude) ( B ) 29.92" Hg ( C ) (actual elevation) 75 :00007 :0 :1 B6(taxiing) (VSI) 100fpm ( A )1

( B ) 100fpm ( C )(mechanic) :00009 :0 :2 C7 180 (skidding turn)(rolling out) (straight and level)(coordinated flight) (attitude indication)( A ) (coordinated flight) ( B ) (nose high) ( C )(miniature aircraft) (skid) :00010 :0 :2 A8(precess) ( A ) ( B ) ( C ) :00011 :0 :1 C9( A ) ( B ) ( C ) :00012 :0 :2 A10( A ) (angle of bank)/(angle of attack) ( B ) (angle of bank)/(angle of attack) ( C )(angle of attack) :00013 :0 :2 B11 (standard rate turn)(bank) "" ("primary")( A )(Heading indicator). ( B ) (Turn and slip indicator) (turn coordinator) ( C ) (attitude indicator) :00014 :0 :1 A12 180 ( A )1 ( B )2 ( C )3 :00015 :0 :1 A13 (IFR flight) (HI) pretakeoff check( A )5 2

(magnetic heading) (taxi turn) (alignment) ( B )5 aligns itself ( C ) 5 ground operationprecess 2 :00016 :0 :1 C14 taxi check( A ) ( B )dip ( C ) ()(heading) :00017 :0 :1 A15(standard rate turn) ( A ) ( B ) ( C ) (magnetic heading) :00018 :0 :2 A16(ram air input) (drain hole) ( A ) (airspeed indicator) ( B ) (airspeed indicator) ( C ) (airspeed indicator) :00019 :0 :1 C17 500FPM (static ports) VSI ( A )(500 FPM ) ( B ) 500 FPM ( C )VSI :00020 :0 :1 A18 (pitot tube) ( A ) ( B ) ( C ) (Vertical Speed Indicator) :00021 :0 :1 B19(alternate source of static pressure)( A ) ( B ) ( C ) 3

:00022 :0 :2 C20( A ) (cross-check) (instrument interpretation). ( B ) (instrument interpretation)(cross-check). ( C ) (cross-check) (instrument interpretation) . :00023 :0 :2 B21 3 (glide slope) ( A )(ground speed) ( B ) (ground speed) ( C ) (glide slope) :00024 :0 :1 C22GS( A ) (true airspeed) ( B )(calibrated airspeed). ( C ) (ground speed) :00025 :0 :2 B23(standard rate turn) ( A )(attitude indicator) ( B ) (turn coordinator) ( C ) () (Heading indicator). :00026 :0 :2 C24 (pitch instrument)( A )(attitude indicator) ( B ) (VSI) ( C ) (airspeed indicator) :00027 :0 :1 A25(standard rate turn) (pitch instrument) ( A )(Altimeter). ( B ) (VSI) ( C ) (airspeed indicator) :00028 :0 :2 C26(level cruising flight) :( A )(attitude indicator) (pitch attitude)(power) ( B )(power)(attitude indicator)4

(pitch)(VSI) ( C ) (power)(attitude indicator) (pitch) :00029 :0 :2 A27 (unusual flight attitude) (recovering) (level pitch attitude) ( A ) (airspeed indicator)(Altimeter) (VSI) (trend). ( B ) ( C ) :00030 :0 :2 B28(spiraling) (nose-low) (unusual flight attitude)( A ) (pitch attitude)(power) ( B )(power) (bank attitude) ( C )(power) (bank attitude) :00031 :0 :1 A29(DME)( A )(Slant range) NM. ( B )(Slant range) SM. ( C ) (Line-of-sight direct distance) VORTAC SM. :00032 :0 :1 B30(VORTAC)(AGL) 6000 DME ( A )0 ( B )1 ( C )1.3 :00033 :0 :2 B31(DME)(Slant range) DME ( A ) DME 1,000 ( B ) DME 1,000 ( C )(Line-of-sight) :00034 :0 :1 B32(VOR/DME) VOR (inoperative)DME (identifier)5

( A )1020 Hz. 30 ( C )1350 Hz. 60

20 ( B )1350 Hz.

:00035 :0 :2 A33DME (ILS) ( A )(OM). ( B ) (visibility) ( C ) (TDZ) :00036 :0 :2 A34VOR VOR ( A ) VOR (radial) 4 ( B ) VOR (radial) 4 ( C ) VOR (radial) 6 :00037 :0 :2 B35 VOR ( A )OBS 180 4 CDI needleFROM ( B ) OBS radial;CDI needle 4 FROM ( C ) VOR OBS 000 CDI needle 4 TO :00038 :0 :2 C36 (publication) VOR (ground checkpoint)( A )(Aeronautical Information Manual) ( B )(En Route Low Altitude Chart) ( C ) /(Airport/Facility Directory) :00039 :0 :1 A37 CDI (airborne checkpoint) VOR ( A )(radial) 6 ( B )(radial) 6 4 ( C )(radial) 4 :00040 :0 :1 A38VOTVOR ( A ) 4 . ( B ) 6 . ( C ) 8 .6

:00041 :0 :1 A39 VOR ( A ) (coded identification)(navigation indications) ( B ) (coded identification) ( C ) VOR VOR :00048 :0 :1 A40 IFR (way point)( A ) (RNAV) (RNAV) ( B ) VOR (radial) ( C ) VOR DME :00050 :0 :2 A41(SDF)(LDA) ( A )SDF (LDA) ( B )SDF (GS) (LDA) ( C )SDF (MB) (LDA)(OM) :00051 :0 :1 A42(LDA)(ILS Localizer) ( A )LDA . ( B )LDA 6 12 (ILS) 5. ( C )LDA VOR . :00052 :0 :2 C43(ILS) ( A )(MM) ( B )(OM) ( C ) (Compass locator) :00053 :0 :2 B44(ILS) IM ( A )(dot) ( B ) (dots) ( C )(dashes) :00054 :0 :1 B45(ILS) (MM)7

(GS)( A )100 . ( B )200 ( C )300 :00056 :0 :1 B46 GPS VFR GPS IFR ( A ) ( B ) ( C ) :00057 :0 :2 C47 IFR GPS ( A ) ( B )( C ) :00301 :0 :1 B48 ?( A ) ( B ) , ( C ) 30 :00302 :0 :2 A49, , , ( A ) ( B ) ( C ) :00303 :0 :1 B50 , ?( A ) , ( B ) , , ( C ) , :00304 :0 :2 C51 , , , :( A ) 500 ( B ) 1000 ( C ) 2000 :00305 :0 :1 B52 1000 , , ?( A ) 500 1000 ( B ) 500 1500 ( C ) 1000 2000

8

:00306 :0 :2 A53 VOR , VOR / / , VOR / , , VOR , ?( A ) ( B ) , ( C ) VOR NDB :00308 :0 :1 A54 , , ?( A ) ( B ), 7700 ( C ) 48 , , :00309 :0 :1 B55"....CLEARED AS FILED" ATC , : ( A )(STAR) ( B ) ( C ) , :00310 :0 :2 C56 , , ATC , ( A )(DPS) , (STARS) , . ( B ) . ( C )(DPS) , (STARS) , . :00313 :0 :2 C57 210 8000 , 140 , ?( A )210 ( B )450 ( C )490 :00315 :0 :1 B58 "Radar contact" , :( A ) , , . ( B ) , , . ( C ) , . :00316 :0 :19

C59 , , "RESUME OWN NAVIGATION" , :( A ) , . ( B ) , . ( C ). :00319 :0 :2 A60(MEA) ?( A ) , , . ( B ) , , , , . ( C ) , , , , DME . :00320 :0 :2 A61 , "(MEA)" , , , , ? ( A ) ( B ) ( C ) :00321 :0 :2 C62 , , : , , , , ?( A ). ( B ). ( C ) 1000 . :00332 :0 :1 A63 VOR (holding pattern) , ?( A ) VOR VOR , , . ( B ) , ( C ) , :00333 :0 :2 C64(holding pattern) , , ?( A ) , , . ( B ) 180 , . ( C ) , .

10

:00334 :0 :2 C65 NDB (holding pattern) , ?( A ) , , , . ( B ) , , , , . ( C ). :00335 :0 :1 B66 , ( ) , , 69 , 70 , 71 , 70 , JUDDS TWO ARRIVAL AFD 72 , FT 3000, 6000, 9000 , BDL 3320 , 3425+05 , 3430+00( A )1 14 . ( B )58 . ( C )50 :00336 :0 :1 A67( , ) , GJT ( Walker Field Airport ) DRO ( Durango-La Plata Co Airport ) , 21 , . 22 , 24 , FT 12,000 18,000 , F( A )1 08 . ( B )1 03 . ( C )58 . :00342 :0 :1 A68 , ILS , , , . ( A ) ( B ) ( C ) , , :00343 :0 :1 C69, ILS , , ?( A ) , , ATC ( B ) , , , . ( C ) , :00360 :0 :2 B70( A ) ( B ) 1.3 ( C ) 1.3 11

:00361 :0 :2 C71(contact approach) ?( A ) , , ( B ) , , ( C ) , , :00362 :0 :2 A72, ? ( A )compass locator ILS ( B ) , ADF VOR , ( C ) DME , :00363 :0 :2 A73 RVR , , RVR , , ?( A ) RVR ( B ) HIRL , RVR ( C ) ILS , RVR :00364 :0 :2 B74 7 , ?( A ) ( B ) ( C ) :00365 :0 :1 C75 VASI , , :( A ) ( B ) VASI ( C ) VASI :10001 :0 :1 C76( true altitude)?( A ). ( B ). ( C ). :10002 :0 :112

B77 29.92 (true altitude)(indicated altitude)?( A ) . ( B ). ( C )(density altitude) . :10003 :0 :1 A78()() (scale of the pressure altimeter)( A ) (true altitude). ( B )(pressure altitude). ( C ) (pressure altitude). :10004 :0 :1 B79 6,500 30.42" Hg (pressure altitude)( A )7,500 ( B )6,000 ( C ) 6,500 :10005 :0 :1 B80(pressure altitude) _______( A ). ( B )(standard datum plane). ( C ). :10006 :0 :1 C81 290 (FL290)() () 30.57" Hg 650 ( A ) 715 . ( B )1,300 ( C ). :10007 :0 :1 B82 250(FL250) () 28.92" Hg(pressure altitude)( A )24,000 ( B )25,000 ( C )26,000 :10008 :0 :1 C83() ()( A ) 29.92" Hg. ( B ). ( C )(airport elevation). :10009 :0 :113

B84(gyro) ( A )(precession) 90 . ( B ) . ( C ) . :10010 :0 :1 C85 180 (steep turn) (rolling out)(straight and level) (attitude indication)( A ). ( B ) (skid). ( C ). :10011 :0 :1 A86 ( A )(horizon bar ) 5 . ( B ) (horizon bar ). ( C )(horizon bar ) . :10012 :0 :1 C87 160 (/) 130 (/) (full panel) ( A ),. ( B ) . ( C ) 130 (/) . :10013 :0 :1 B88(taxiing) (turn coordinator)( A )(miniature aircraft) ( B )(miniature aircraft) ( C )(angle of bank) :10014 :0 :1 A89 (turn coordinator)(miniature aircraft ( A ). ( B ). ( C ) . :10015 :0 :1 C90(bank)14

( A ). ( B ) ( C ) :10016 :0 :1 C91( A )(Coriolis force) ( B ) ( C ) :10017 :0 :1 A92()(power) 500 (pitch)(bank)()(power) ( A )(attitude indicator),() (Heading indicator), (manifold pressure gauge)(tachometer) . ( B ) (VSI),(attitude indicator), (airspeed indicator). ( C ) (airspeed indicator),(attitude indicator), (manifold pressure gauge)(tachometer). :10018 :0 :1 C93 100 ( A )(attitude indicator) 2 bar (two bar widths). ( B )(attitude indicator) 1 bar (two bar widths). ( C )(attitude indication) bar (two bar widths). :10019 :0 :1 C94()(power) (pitch)(bank)()(power)( A ) (attitude indicator),() (Heading indicator), (manifold pressure gauge)(tachometer). ( B ) (Altimeter),(attitude indicator), (airspeed indicator). ( C ) (Altimeter),() (Heading indicator), (manifold pressure gauge)(tachometer) . :10020 :0 :1 C95(attitude indicator)(pitch instruments)( A )(Altimeter) (airspeed indicator) ( B )(Altimeter)(VSI) ( C ) (Altimeter), (airspeed indicator)(VSI) :10021 :0 :115

A96()(power) ( A ) (airspeed indicator). ( B )(attitude indicator). ( C )(Altimeter). :10022 :0 :1 C97(pitch correction)( A )(altimeter)(VSI) ( B ) (manifold pressure gauge)(VSI) ( C )(attitude indicator),(altimeter),(VSI) :10023 :0 :1 A98(pitch attitude) ( A ),,,. ( B ),(wind velocity), . ( C )(relative wind),,. :10024 :0 :1 A99 ( A ) 10. ( B ) 20. ( C ) 25. :10025 :0 :1 C100(VOR)(full-scale deflection)( A )4 . ( B )5 . ( C )10 . :10026 :0 :1 C101(VOR) ( A )(zone of confusion)(CDI) . ( B )(TO-FROM indicator). ( C )TOFROM indicator :10027 :0 :1 B102 30 VOR ( A )2 ( B )3 ( C )5 :10028 :0 :1 B103(VOR)30 (CDI) ( A )1.5 . ( B )2.5 . ( C )3.5 .16

:10029 :0 :1 C104(VORTAC)(CDI) ( A )(radial). ( B )(OBS) . ( C )(radial). :10030 :0 :1 C105 14 CFR part 91 ( A )(owner). ( B ) (operator). ( C )(pilot-in-command). :10031 :0 :1 C106 FAA ( A ). ( B ). ( C ) . :10032 :0 :1 C107(half-standard rate turn) 360 ( A )1 . ( B )2 . ( C )4 . :10033 :0 :1 A108(standard rate turn) 180 ( A )1 . ( B )2 . ( C )3 . :10034 :0 :1 A109( A )() (Heading indicator) (turn coordinator). ( B )() (Heading indicator) (attitude indicator) . ( C )(attitude indicator) (turn coordinator). :10035 :0 :1 B110( A ) (instrument interpretation),(trim),. ( B ) (cross-check), (instrument interpretation),. ( C ) (cross-check),, .17

:10036 :0 :1 C111(supporting instruments)( A ) (airspeed indicator) (Vertical Speed Indicator). ( B )(Altimeter)(attitude indicator) . ( C )(attitude indicator) (VSI). :10037 :0 :1 C112(unusual attitudes) (level)( A )(attitude indicator) . ( B ) (VSI). ( C ) . :10038 :0 :1 A113(VOR) ( A ),, ,. ( B ),(VOR) (VOT),,. ( C ) ,,,,. :10039 :0 :1 C114(VOT)(VOR) (CDI) ( A )090 (radial) . ( B )180 (radial). ( C )360 (radial). :10040 :0 :1 B115(VOR)(CDI) (OBS)( A ) (radial)4 . ( B )(radial)6 . ( C )0 ""(FR) (VOR). :10041 :0 :1 C116(VORTAC) 30 ( A ) (VOR)(DME). ( B )(VOR) (DME).18

( C )(DME)(VOR). :10042 :0 :1 A117 B ( A ) 4096 (transponder). ( B ) (VOR)(DME). ( C )4096 (transponder). :10043 :0 :1 C118(VOR) (CDI) ( A )5 6 . ( B )8 10 . ( C )10 12 . :10044 :0 :1 B119 350 270(MH350,RB270) ( A )060 . ( B )260 . ( C )260 . :10047 :0 :1 A120 18000 (IFR flight) (VOR) ( A ) 80 . ( B ) 40 . ( C ) 70 . :10048 :0 :1 B121(CDI)(full-scale deflection) ( A ). ( B ) . ( C ). :10049 :0 :1 C122(DME) (inoperative)( A ). ( B ) . ( C ) . :10052 :0 :1 A123 (turn coordinator)(miniature aircraft) ( A ). ( B )(angle of bank) . ( C )(miniature aircraft).19

:10064 :0 :1 A124 ?( A ) ( B ) ( C ) :10065 :0 :1 C125, ?( A ) ( B ) ( C ) :10066 :0 :1 A126( A ) ( B ) ( C ) :10067 :0 :1 B127?( A ) ( B ) ( C ) :10068 :0 :1 B128?( A ) ( B ) ( C ) :10069 :0 :1 C129 :( A ) ( B ) ( C ) :10070 :0 :1 C130? ( A ) ( B ) ( C ) :10072 :0 :120

C131( A ) ( B ) ( C ) :10073 :0 :1 C132( A ) ( B ) ( C ) :10074 :0 :1 B133hyperventilation,? ( A ) ( B ), ( C ) :10075 :0 :1 C134, ,?( A ) , ( B ) ( C ) , :10076 :0 :1 B135( turn coordinator) ( A ) ( B ) ( C ) :10077 :0 :1 C136( A ) ( B ), ( C ), :10078 :0 :1 A137( A )(horizontal bar) ( B ) (warmup)(horizontal bar) ( C ) :10079 :0 :1 A138( turn coordinator)21

( A )(rate of roll)(rate of turn) ( B ) ( C ) :10080 :0 :1 C139?( A ) ( B ) ( C ) :10081 :0 :1 B140( skipping) ( load factor )( A ) ( B ) ( C ) :10082 :0 :1 A141(Turn Coordinator)? ( A ) ( B ) ( C ) :10083 :0 :1 A142 ?( A ) ( B ) ( C ) :10084 :0 :1 A143?( A ) ( B ) ( C ) :10085 :0 :1 C144 180 ( skipping) , , ? ( A ) ( B ), ( C ) :10086 :0 :1 B145, 180 ,?( A ).22

( B ) ( C ) :10087 :0 :1 A146?( A ) ( B ) ( C )( ) :10088 :0 :1 B147, ? ( A ) ( B ) ( C ) :10089 :0 :1 C148?( A ) ( B ) ( C ) :10090 :0 :1 C149roll in ( A ) ( B ) ( C ) :10091 :0 :1 C150 500 ( A ) ( 500 ) ( B ) 500 ( C ) :10092 :0 :1 C151IFR ( A ) ( B ) 29.92Hg-in ( C ) 75 :10093 :0 :1 C15223

( A ) ( B ) ( C ) :10094 :0 :1 B153( turn and slip indicator) ( A ) ( B ), ( C ) :10095 :0 :1 A154( turn and slip indicator) ( A ), ( B ) ( C ) :10096 :0 :1 A155? ( A )5 , , . ( B )5 . ( C ), ,. :10097 :0 :1 C156,, ?( A ). ( B ) ,. ( C ), . :10098 :0 :1 A157,, ?( A )A. ( B )B. ( C )C. , . :10099 :0 :1 B158 15 360 ?( A )A. 135 225 ( B )B. 090 270 ( C )C. 180 000 :10100 :0 :124

C159( A ) ( B ) ( C ) ( D )C :10101 :0 :1 A160,? ( A ), ( B ) ( C ), ( D ) A :10102 :0 :1 C161 ( A )A. ( B )B. ( C )C. :10103 :0 :1 B162 ( A )A. ( B )B. ( C )C. :10104 :0 :1 C163 ( A ) ( B ) ( C ) :10105 :0 :1 B164 ( A ) ( B ) ( C ) :10106 :0 :1 C165, 360 ?( A ) ( B ) ( C ) :10107 :0 :1 A166, 180 ?( A )25

( B ) ( C ) :10108 :0 :1 B167, ?( A ) ( B ) ( C ) :10109 :0 :1 A168,? ( A )180 ( B )270 ( C )360 :10110 :0 :1 C169 180,, ?( A ) ( B ) ( C ) :10111 :0 :1 C170, 135( A )1 ( B )1 20 ( C )1 30 :10112 :0 :1 C171, 090 300, ?( A )30 ( B )40 ( C )50 :10113 :0 :1 B172,( A ), 90 ( B ) ( C ) :10114 :0 :1 A173, 090 270? ( A )1 ( B )2 ( C )3 :10115 :0 :1 C174 ?( A ) ( B ) ( C ) :10116 :0 :126

A175? ( A ) ( B ) ( C ) :10117 :0 :1 B176 ( A ) ( B ) ( C ) :10118 :0 :1 B177 6500 MSL 30.42 In-Hg ( A )7500 ( B )6000 ( C )6500 :10119 :0 :1 B178 ( A ) ( B ) ( C ) :10120 :0 :1 A179 ( A ) ( B ) ( C ) :10121 :0 :1 C180 ( A ) ( B ) ( C ) :10122 :0 :1 C181( A ) ( B ) ( C ) :10123 :0 :1 B182(QNH),?( A ) ( B ) ( C ) :10124 :0 :1 B183( Pressure Altitude) ( A ) ( B ) ( C )

27

:10125 :0 :1 B184 ?( A ) ( B ) ( C ) :10131 :0 :1 A185 DME ILS DME ( A ) ( B ) ( C ) :10132 :0 :1 A186 DME ILS/LOC ( A ) LOC DME/TACAN ( B ) "LOC/DME" ( C )( Aeronautical Information Manual) :10133 :0 :1 B187 ( Parallel ILS approach ) ( A ) ( Parallel ILS approach ) 4,300 ; ( B ) ( Parallel ILS approach ) 1 1/2 ( C )( minimums) :10134 :0 :1 A188 ILS , ( A ) ( B ) ( C ) :10135 :0 :1 C189 ILS ( A ) ( B ) ( C ) :10136 :0 :128

C190ILS :( A ), ( B ), ( C ), :10137 :0 :1 B191 ILS ( front course )( inner marker) , ?( A ) ( B )"" ( C ) DASH :10138 :0 :1 C192( A ) ( B ) ( C ) :10139 :0 :1 B193(Middle Marker)? ( A )100 ( B )200 ( C )300 :10140 :0 :1 A194SDF LDA ( A )SDF 6 12 LDA 5 ( B )SDF LDA ( C )SDF LDA :00006 :1 :1 C195( Fig1) 12,000 ( A )2 ( B )3 ( C )4 :00042 :1 :1 A196( Fig2) VORTAC ? ( A ) . ( B ) . ( C ) . :00043 :1 :2 A197( Fig3)(HSI) "A"( A )9 6. ( B ) 9 . ( C ) 6 . :00043 :2 :2 B198( Fig3) HSI "B" ( A )11 ( B )5 13. ( C )7 11.

29

:00043 :3 :2 C199( Fig3) HSI "C" ( A )9 ( B )4 ( C )12 :00043 :4 :2 C200( Fig3) HSI "D" ( A )1 ( B )10 ( C )2 :00043 :5 :2 C201( Fig3) HSI "E" ( A ) 8 . ( B ) 3 . ( C )8 3. :00043 :6 :1 A202( Fig3) HSI "F" ( A )4 ( B )11 ( C )5 :00044 :1 :1 B203( Fig4) 4 (TO) (magnetic bearing) ( A )285. ( B )055. ( C )235. :00044 :2 :1 B204( Fig4) RMI 055 (radial)( A )1 ( B )2 ( C )3 :00044 :3 :1 A205( Fig4) RMI (TO)( A )1 ( B )2 ( C )3 :00045 :1 :1 B206( Fig5) 16DME (right-hand arc) ( A ) VOR-2 ( B ) VOR-2 ( C ) VOR-1 :00045 :2 :1 C207( Fig6) ILS (MAP) (marker beacon)( A )30

-(dashes)(dots); - ( B )- ; - ( C )-; - :00046 :1 :2 C208( Fig6 60AJ 61J) CARCO (GS) (localizer)(course)( A ) CARCO (glide slope) (course) ( B ) CARCO (glide slope) (course) ( C ) CARCO (glide slope)(course) :00046 :2 :2 B209( Fig6) LDA Roanoke Regional (ILS)( A )LOC ( B )LOC ( C ) (MM) (GS) :00058 :1 :2 B210( Fig7) No. 1 NAV OBS CDI (ambiguity indication) (TO) ( A )175. ( B )165. ( C )345. :00059 :1 :2 A211( Fig8 65J 66) GRICE (intersection)( A ) V552 GRICE ( B ) V552 GRICE ( C ) V552 GRICE :00311 :1 :1 C212( Fig9) STAKK , ?( A ) 6,500 . ( B )1,400 . ( C )10,200 . :00311 :2 :1 C213( Fig9) 140 , () ?( A )350 ( B )475 ( C )700

31

:00318 :1 :2 B214( Fig10) ( A ) ( B ) ( C ) :00322 :1 :1 C215( Fig11) V112, BTG VORTAC LTJ VORTAC , Gymme :( A )6,400 . ( B )6,500 . ( C )7,000 . :00322 :2 :1 C216( Fig11) V468 BTG VORTAC YKM VORTAC , TROTS ( A )7,100 . ( B )10,000 . ( C ) 11,500 . :00324 :1 :1 A217( Fig12) V27 , GVO MQO VORTACS , VOR COP ?( A ) GVO VORTAC 20 DME ( B ) MQO VORTAC 20 DME ( C ) SBA VORTAC 30 DME :00325 :1 :1 B218( Fig13) V86 , BOZEMAN VORTAC , ?( A )8,500 ( ) ( B )9,300 ( ) ( C )9,700 ( ) :00326 :1 :2 A219( Fig14) : "HOLD EAST OF THE ABC VORTAC ON THE ZERO NINER ZERO RADIAL, LEFT TURNS" ?( A ) ( B ) ( C ) :00326 :2 :2 B220( Fig14) : "CLEARED TO THE ABC VORTAC. HOLD SOUTH ON THE ONE EIGHT ZERO RADIAL" ?( A ) ( B ) ( C ) :00326 :3 :2 C221( Fig14) : "CLEARED TO THE32

XYZ VORTAC. HOLD NORTH ON THE THREE SIX ZERO RADIAL, LEFT TURNS" ? ( A ) ( B ) ( C ) :00326 :4 :2 B222( Fig14) : "CLEARED TO THE ABC VORTAC. HOLD WEST ON THE TWO SEVEN ZERO RADIAL" ?( A ) ( B ) ( C ) :00326 :5 :2 B223( Fig14) : "CLEARED TO THE XYZ NDB. HOLD NORTHEAST ON THE ZERO FOUR ZERO DEGREE BEARING FROM THE NDB. LEFT TURNS" 117, ? ( A ) ( B ) ( C ) :00326 :6 :2 A224( Fig14) : "CLEARED TO THE ABC NDB. HOLD SOUTHWEST ON THE TWO THREE ZERO DEGREE BEARING FROM THE NDB" , 117 , , ?( A ) ( B ) ( C ) :00338 :1 :2 C225( Fig15) BZN VOR DBS VORTAC , 260 24 , 185 ? ( 17 E )( A ) 33 . ( B )37 . ( C )39 . :00339 :1 :2 B226( Fig16) JUMBO.JUMBO2 ? ( A )SAT VOR ( B )JUMBO . ( C )CWK VOR :00339 :2 :2 C227( Fig16) DELMO , ? ( A )010 ( B )040 ( C )350 :00341 :1 :233

B228( Fig17) DPK.DPK2 ? ( A )CMK VORTAC. ( B )DPK VORTAC. ( C )BRISS . :00344 :1 :1 A229( Fig18) Eugene Mahlon Sweet Field , 16 ( TDZ ) ?( A )363 ( ). ( B ) 365 ( ) ( C )396 ( ) :00344 :2 :1 B230( Fig18) 90 , ILS , ILS ?( A )415 ( B )484 . ( C )555 . :00346 :1 :1 B231( Fig19) RNAV ( GPS ) RWY 33 , ?( A ) (FAF) 5.0 DME , . ( B )GPS (MAP) " RW33" . ( C ) MDA , (MAP) 1.8 DME . :00346 :2 :1 A232( Fig19) 33 , , LNAV , ?( A )1,240 ( ) ; 1 ( B )1,280 ( ) ; 1-1/4 ( C )1,100 ( ) ; 1 :00348 :1 :1 A233( Fig20) 36 ? ( A )19 ( B )18 ( C )22 :00348 :2 :1 C234( Fig20) (localizer) , ?( A ) , ( DME ) , ( B ) , ( ATIS ) , ( DME ) ( C ) , ( DME ) , :00348 :3 :134

C235( Fig20) ILS RWY 36L , (glideslope) , ? ( 120 ) ( A )425 ( B )530 ( C )646 :00352 :1 :2 B236( Fig21) Portland International , LOC/DME RWY 21 , ( MDA) ? ( A )1,100 () ; 1 . ( B )680 () ; 1 ( C )680 () ; 1 :00353 :1 :1 A237( Fig22) 90 , 6 DME , 2400 () , ( FAF ) 2000 ( ) , ?( A )200 ( B )400 ( C )600 :00354 :1 :1 B238( Fig23) ILS RWY 06 , (glideslope) ?( A )3,000 () ( B )1,800 ( ) ( C )1,690 () :00354 :2 :1 C239( Fig23) Bradley International 6 , ( A )HIRL, REIL VASI. ( B )HIRL VASI. ( C )ALSF2 HIRL. :00356 :1 :1 B240( Fig24) 28R , ? ( A )3,649 () ( B )3,517 () ( C )3,450 ( ) :00357 :1 :1 C241( Fig25) OALDY "straight-in LOC" , :( A ) 32 ( B ) ( C ) , :00358 :1 :1 C242( Fig26) RNAV ( GPS ) RWY 36 , 35

( A ) BAQXI ( B ) , FEHXE ( C ), FEHXE :00359 :1 :2 B243( Fig27) Roanoke Regional LDA RWY / GS 6 , (circle to land) ?( A )24 ( B )6 - 24 ( C ), 1/2 :10045 :1 :1 B244( Fig28) 360 (TO-FROM indicator) FROM (CDI)( A )1 ( B )2 ( C )3 :10046 :1 :1 C245( Fig29) VORTAC VORTAC ( A ) . ( B ) . ( C ) . :10050 :1 :1 A246( Fig30)(free gyro mode) ( A ) . ( B ). ( C ) . :10050 :2 :1 C247( Fig30)(remote indicating compass) 5 ( A ) (slaved gyro mode). ( B ) (free gyro mode). ( C ) (free gyro mode). :10053 :2 :2 C248( Fig31 ) WAGGE TWO DEPARTURE, MUSTANG TRANSITION, V165 , FMG VOR ?( A )12000 MSL ( B )10500 MSL ( C )10000 MSL

36

:10053 :3 :2 B249( Fig31 ) 160 , 10 , 16 , 9200 MSL ?( A )925 / ( B )1850 / ( C )1233 / :10053 :4 :2 B250( Fig31 ) WAGGE TWO LOVELOCK ?( A )WAGGE2.WAGGE ( B )WAGGE2.LLC ( C ) WAGGE2.WAGGE+ WAGGE2.LLC :10053 :5 :2 C251( Fig31 ) WAGGE LOVELOCK VOR ? ( A )14 ( B )63 ( C )77 :10053 :6 :2 C252( Fig31 ) WAGGE JERGA ? ( A )SWR VOR ( B )LLC VOR ( C )HZN VOR :10059 :1 :1 C253( Fig32 ) 1 , MCA V264 12000W, ? :( A ) V264 , 12000 MSL ( B ) V264 , 12000 MSL ( C ) V264 , 12000 MSL :10059 :2 :1 B254( Fig32 ) 2 , ? :( A ) 6300 3000 ( B ) VOR ( C ) V137 MORON 63 PSP VOR :10059 :3 :1 C255( Fig32 ) 3 Big Bear City Airport ? : ( A )3500 ( B )5800 ( C )6748 :10059 :4 :1 A256( Fig32 ) 4 , ? :( A ) V264 7700 MSL , 22 VOR ( B ) V264 8500 MSL 37

, 22 VOR ( C ) V264 7700 MSL , 25 VOR :10059 :5 :1 B257( Fig32 ) 5 :( A )V388 ( B ) VOR ( C )DEWAY ACINS 55 :10201 :1 :1 B258( Fig33)A-1 VOR VOR ( A )79 ( B )89 ( C )50 ( D )99 :10201 :2 :1 A259( Fig33) TNN VORTAC VHF ( A )124.7MHZ ( B )121.1MHZ ( C )363.8MHZ ( D )328.7MHZ :10201 :3 :1 C260( Fig33)B-591 TINHO ( A )199/100 ( B )222/85 ( C )199/105 ( D )200/120 :10201 :4 :1 B261( Fig33) ( A )135.9MHZ ( B )130.1MHZ ( C )114.9MHZ ( D ) 128.1MHZ :10201 :5 :1 A262( Fig33)W-4 HLG VORTAC TNN VORTAC ( A )4000 ( B )5000 ( C )8000 ( D )7000 :10201 :6 :1 C263( Fig33)W-2 ( A ) NDB ( B ) NDB/DME ( C ) APU VOR NDB/DME ( D ) GENIE NDB/DME :10201 :7 :1 A264( Fig33)W-6 ( A ) 5000 ( B )6000 ( C )8000 ( D )10000 38

:10201 :8 :1 A265( Fig33)W-8 APU ( A ) ( B ) ( C ) :10202 :1 :1 B266( Fig34)(ZONLI)( A )TIA R196 /10DME ( B )HLG R-052/30DME ( C )ITSG R-260/25DME :10202 :10 :1 A267( Fig34) ILS RWY10 ( A ) ( B ) :10202 :11 :1 B268( Fig34)-ILS RWY10 ( A ) ( B )LK ( C )APU :10202 :12 :1 D269( Fig34) ILS RWY10 LU ( A ) ( B ) ( C ) ( D ) :10202 :13 :1 B270( Fig34)(YILAN)( A )LK R-138/30DME ( B )APU R-154/80DME ( C )AP R-154/30DME :10202 :14 :1 B271( Fig34)(ZONLI)( A ) ( B ) ( C ) :10202 :15 :1 D272( Fig34)(YILAN) LK 6000 ( A ) ( B ) ( C ) ( D ) :10202 :16 :1 B273( Fig34) LK ( A )5000 ( B ) 5000 ( C )4000 :10202 :17 :139

C274( Fig34) ILAN LK-138 BRG LK

( A ) ( B ) ( C ) :10202 :2 :1 C275( Fig34) ILS RWY10 ( A )MDA263/VIS1600 ( B )MDA760/VIS3200 ( C ) MDA1120/VIS4800 :10202 :3 :1 B276( Fig34) ILS RWY10 ( A )2 ( B )3 ( C ) 5 :10202 :4 :1 C277( Fig34)( A )13 ( B )18 ( C )5 :10202 :5 :1 A278( Fig34) R16 4000 ( A ) ( B ) ( C ) :10202 :6 :1 B279( Fig34)(ZONLI)( A ) ( B ) :10202 :7 :1 A280( Fig34)-ILS RWY10

( A ) 4 ( B ) 4 ( C ) :10202 :8 :1 B281( Fig34) LK (095) ( A ) ( B ) ( C ) :10202 :9 :140

B282( Fig34) ILS RWY10 ( A )1600 ( B )1200 ( C )800 :10203 :1 :2 B283( Fig35)( A )112.5MHZ ( B )108.1MHZ ( C )335KHZ ( D )250KHZ :10203 :2 :2 D284( Fig35)( A ) 10 ( B ) 10 ( C ) 7 ( D ) 7 :10203 :3 :2 C285( Fig35) ( A )319 ( B )846 ( C )518 :10203 :4 :2 A286( Fig35)(MDA)( A )800 ( B )787 ( C )1200

====================English Version====================

Question:00001 Group:0 Difficult:2 A1What information does a Mach meter present?( A )The ratio of aircraft true airspeed to the speed of sound. ( B )The ratio of aircraft indicated airspeed to the speed of sound. ( C )The ratio of aircraft equivalent airspeed, corrected for installation error, to the speed of sound. Question:00002 Group:0 Difficult:1 B2Under which condition will pressure altitude be equal to true altitude? ( A )When the atmospheric pressure is 29.92" Hg. ( B )When standard atmospheric conditions exist. ( C )When indicated altitude is equal to the pressure altitude. Question:00003 Group:0 Difficult:2 C3If the outside air temperature increases during a flight at constant power and at a constant indicated altitude, the true airspeed will( A )decrease41

and true altitude will increase. ( B )increase and true altitude will decrease. ( C )increase and true altitude will increase. Question:00004 Group:0 Difficult:2 B4The local altimeter setting should be used by all pilots in a particular area, primarily to provide for( A )the cancellation of altimeter error due to nonstandard temperatures aloft. ( B )better vertical separation of aircraft. ( C )more accurate terrain clearance in mountainous areas Question:00005 Group:0 Difficult:1 C5How should you preflight check the altimeter prior to an IFR flight? ( A )Set the altimeter to the current temperature. With current temperature and the altimeter indication, determine the calibrated altitude to compare with the field elevation. ( B )Set the altimeter first with 29.92" Hg and then the current altimeter setting. The change in altitude should correspond to the change in setting. ( C )Set the altimeter to the current altimeter setting. The indication should be within 75 feet of the actual elevation for acceptable accuracy. Question:00007 Group:0 Difficult:1 B6You check the flight instruments while taxiing and find that the vertical speed indicator (VSI) indicates a descent of 100 feet per minute. In this case, you ( A )must return to the parking area and have the instrument corrected by an authorized instrument repairman. ( B )may take off and use 1 00 feet descent as the zero indication. ( C )may not take off until the instrument is corrected by either the pilot or a mechanic. Question:00009 Group:0 Difficult:2 C7During normal operation of a vacuum-driven attitude indicator, what attitude indication should you see when rolling out from a 180* skidding turn to straight-and-level coordinated flight?( A )A straight-and-level coordinated flight indication. ( B )A nose-high indication relative to level flight. ( C )The miniature aircraft shows a turn in the direction opposite the skid. Question:00010 Group:0 Difficult:2 A8When an aircraft is accelerated, some attitude indicators will precess and42

incorrectly indicate a( A )climb. ( B )descent. ( C )right turn. Question:00011 Group:0 Difficult:1 C9What force causes an airplane to turn?( A )Rudder pressure or force around the vertical axis. ( B )Vertical lift component. ( C )Horizontal lift component. Question:00012 Group:0 Difficult:2 A10When airspeed is decreased in a turn, what must be done to maintain level flight?( A )Decrease the angle of bank and/or increase the angle of attack. ( B )increase the angle of bank and/or decrease the angle of attack. ( C )increase the angle of attack. Question:00013 Group:0 Difficult:2 B11During standard-rate turns, which instrument is considered "primary" for bank?( A )Heading indicator. ( B )Turn and slip indicator or turn coordinator. ( C )Attitude indicator. Question:00014 Group:0 Difficult:1 A12If a standard rate turn is maintained, how long would it take to turn 180*? ( A )1 minute. ( B )2 minutes. ( C )3 minutes. Question:00015 Group:0 Difficult:1 A13What pretakeoff check should be made of a vacuum-driven heading indicator in preparation for an IFR flight?( A )After 5 minutes, set the indicator to the magnetic heading of the aircraft and check for proper alignment after taxi turns. ( B )After 5 minutes, check that the heading indicator card aligns itself with the magnetic heading of the aircraft. ( C ) Determine that the heading indicator does not precess more than 2* in 5 minutes of ground operation. Question:00016 Group:0 Difficult:1 C14On the taxi check, the magnetic compass should( A )swing opposite to the direction of turn when turning from north. ( B )exhibit the same number of degrees of dip as the latitude. ( C )swing freely and indicate known headings. Question:00017 Group:0 Difficult:143

A15What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a south heading in the Northern Hemisphere?( A )The compass will indicate a turn to the right, but at a faster rate than is actually occurring. ( B )The compass will initially indicate a turn to the left. ( C )The compass will remain on south for a short time, then gradually catch up to the magnetic heading of the aircraft. Question:00018 Group:0 Difficult:2 A16What indication should a pilot observe if an airspeed indicator ram air input and drain hole are blocked?( A )The airspeed indicator will react as an altimeter. ( B )The airspeed indicator will show a decrease with an increase in altitude. ( C )No airspeed indicator change will occur during climbs or descents. Question:00019 Group:0 Difficult:1 C17What would be the indication on the VSI during entry into a 500 FPM actual descent from level flight if the static ports were iced over?( A )The indication would be in reverse of the actual rate of descent (500 FPM climb). ( B )The initial indication would be a climb, then descent at a rate in excess of 500 FPM. ( C )The VSI pointer would remain at zero regardless of the actual rate of descent. Question:00020 Group:0 Difficult:1 A18During flight, if the pitot tube becomes clogged with ice, which of the following instruments would be affected?( A )The airspeed indicator only. ( B )The airspeed indicator and the altimeter. ( C )The airspeed indicator, altimeter, and Vertical Speed Indicator. Question:00021 Group:0 Difficult:1 B19If while in level flight, it becomes necessary to use an alternate source of static pressure vented inside the airplane, which of the following variations in instrument indications should the pilot expect?( A )The vertical speed to momentarily show a descent. ( B )The altimeter to read higher than normal. ( C )The vertical speed to show a climb. Question:00022 Group:0 Difficult:2 C20What is the correct sequence in which to use the three skills used in instrument flying?( A )Aircraft control, cross-check, and instrument44

interpretation. ( B )Instrument interpretation, cross-check, and aircraft control. ( C )Cross-check, instrument interpretation, and aircraft control. Question:00023 Group:0 Difficult:2 B21What effect will a change in wind direction have upon maintaining a 3* glide slope at a constant true airspeed?( A )When ground speed decreases, rate of descent must increase. ( B )When ground speed increases, rate of descent must increase. ( C )Rate of descent must be constant to remain on the glide slope. Question:00024 Group:0 Difficult:1 C22The rate of descent on the glide slope is dependent upon( A )true airspeed. ( B )calibrated airspeed. ( C )ground speed. Question:00025 Group:0 Difficult:2 B23What is the primary bank instrument once a standard rate turn is established?( A )Attitude indicator. ( B )Turn coordinator. ( C ) Heading indicator. Question:00026 Group:0 Difficult:2 C24What is the primary pitch instrument during a stabilized climbing left turn at cruise climb airspeed?( A )Attitude indicator. ( B )VSI. ( C ) Airspeed indicator. Question:00027 Group:0 Difficult:1 A25What is the primary pitch instrument when establishing a constant altitude standard rate turn?( A )Altimeter. ( B )VSI. ( C )Airspeed indicator. Question:00028 Group:0 Difficult:2 C26To enter a constant-airspeed descent from level cruising flight, and maintain cruising airspeed, the pilot should( A )first adjust the pitch attitude to a descent using the attitude indicator as a reference, then adjust the power to maintain the cruising airspeed. ( B )first reduce power, then adjust the pitch using the attitude indicator as a reference to establish a specific rate on the VSI. ( C )simultaneously reduce power and adjust the pitch using the attitude indicator as a reference to maintain the cruising airspeed. Question:00029 Group:0 Difficult:245

A27While recovering from an unusual flight attitude without the aid of the attitude indicator, approximate level pitch attitude is reached when the ( A )airspeed and altimeter stop their movement and the VSI reverses its trend. ( B )airspeed arrives at cruising speed, the altimeter reverses its trend, and the vertical speed stops its movement. ( C )altimeter and vertical speed reverse their trend and the airspeed stops its movement. Question:00030 Group:0 Difficult:2 B28Which is the correct sequence for recovery from a spiraling, nose-low, increasing airspeed, unusual flight attitude?( A )Increase pitch attitude, reduce power, and level wings. ( B )Reduce power, correct the bank attitude, and raise the nose to a level attitude. ( C )Reduce power, raise the nose to level attitude, and correct the bank attitude. Question:00031 Group:0 Difficult:1 A29Which distance is displayed by the DME indicator?( A )Slant range distance in NM. ( B )Slant range distance in SM. ( C )Line-of-sight direct distance from aircraft to VORTAC in SM. Question:00032 Group:0 Difficult:1 B30Which DME indication should you receive when you are directly over a VORTAC site at approximately 6,000 feet AGL?( A )0 ( B )1 ( C ) 1.3 Question:00033 Group:0 Difficult:2 B31As a rule of thumb, to minimize DME slant range error, how far from the facility should you be to consider the reading as accurate?( A )Two miles or more for each 1,000 feet of altitude above the facility. ( B )One or more miles for each 1,000 feet of altitude above the facility. ( C )No specific distance is specified since the reception is line-of-sight. Question:00034 Group:0 Difficult:1 B32When a VOR/DME is collocated under frequency pairings and the VOR portion is inoperative, the DME identifier will repeat at an interval of ( A )20 second intervals at 1020 Hz. ( B )30 second intervals at 1350 Hz. ( C ) 60 second intervals at 1350 Hz. Question:00035 Group:0 Difficult:246

A33When installed with the ILS and specified in the approach procedures, DME may be used( A )in lieu of the OM. ( B )in lieu of visibility requirements. ( C )to determine distance from TDZ. Question:00036 Group:0 Difficult:2 A34When making an airborne VOR check, what is the maximum allowable tolerance between the two indicators of a dual VOR system (units independent of each other except the antenna)?( A )4* between the two indicated radials of a VOR. ( B )Plus or minus 4* when set to identical radials of a VOR. ( C )6* between the two indicated radials of a VOR. Question:00037 Group:0 Difficult:2 B35How should the pilot make a VOR receiver check when the aircraft is located on the designated checkpoint on the airport surface?( A )Set the OBS on 180* plus or minus 4*; the CDI should center with a FROM indication. ( B )Set the OBS on the designated radial. The CDI must center within plus or minus 4* of that radial with a FROM indication. ( C )With the aircraft headed directly toward the VOR and the OBS set to 000*, the CDI should center within plus or minus 4* of that radial with a TO indication. Question:00038 Group:0 Difficult:2 C36In which publication can the VOR receiver ground checkpoint(s) for a particular airport be found?( A )Aeronautical Information Manual. ( B )En Route Low Altitude Chart. ( C )Airport/Facility Directory. Question:00039 Group:0 Difficult:1 A37Which is the maximum tolerance for the VOR indication when the CDI is centered and the aircraft is directly over the airborne checkpoint? ( A )Plus or minus 6* of the designated radial. ( B )Plus 6" or minus 4* of the designated radial. ( C )Plus or minus 4* of the designated radial. Question:00040 Group:0 Difficult:1 A38What is the maximum tolerance allowed for an operational VOR equipment check when using a VOT?( A )Plus or minus 4*. ( B )Plus or minus 6*. ( C )Plus or minus 8*. Question:00041 Group:0 Difficult:147

A39What indication should a pilot receive when a VOR station is undergoing maintenance and may be considered unreliable?( A )No coded identification, but possible navigation indications. ( B )Coded identification, but no navigation indications. ( C )A voice recording on the VOR frequency announcing that the VOR is out of service for maintenance. Question:00048 Group:0 Difficult:1 A404069. What is a way point when used for an IFR flight?( A )A predetermined geographical position used for an RNAV route or an RNAV instrument approach. ( B )A reporting point defined by the intersection of two VOR radials. ( C )A location on a victor airway which can only be identified by VOR and DME signals. Question:00050 Group:0 Difficult:2 A41What is a difference between an SDF and an LDA facility?( A ) The SDF course width is either 6* or 12" while the LDA course width is approximately 5*. ( B )The SDF course has no glide slope guidance while the LDA does. ( C )The SDF has no marker beacons while the LDA has at least an OM. Question:00051 Group:0 Difficult:1 A42What is the difference between a Localizer-Type Directional Aid (LDA) and the ILS localizer?( A )The LDA is not aligned with the runway. ( B )The LDA uses a course width of 6* or 12*, while an ILS uses only 5*. ( C )The LDA signal is generated from a VOR-type facility and has no glide slope. Question:00052 Group:0 Difficult:2 C43Which range facility associated with the ILS can be identified by a twoletter coded signal?( A )Middle marker. ( B )Outer marker. ( C ) Compass locator. Question:00053 Group:0 Difficult:2 B44Which indications will a pilot receive where an IM is installed on a front course ILS approach?( A )One dot per second and a steady amber light. ( B )Six dots per second and a flashing white light. ( C )Alternate dashes and a blue light.

48

Question:00054 Group:0 Difficult:1 B45Approximately what height is the glide slope centerline at the MM of a typical ILS?( A )100 feet. ( B )200 feet. ( C )300 feet. Question:00056 Group:0 Difficult:1 B46Hand-held GPS systems, and GPS systems certified for VFR operation, may be used during IFR operations as( A )the principal reference to determine enroute waypoints. ( B )an aid to situational awareness. ( C )the primary source of navigation. Question:00057 Group:0 Difficult:2 C47During IFR operation using an approved GPS system for navigation, ( A )no other navigation system is required. ( B )active monitoring of an alternate navigation system is always required. ( C )the aircraft must have an approved and operational alternate navigation system appropriate for the route. Question:00301 Group:0 Difficult:1 B48How can an instrument pilot best overcome spatial disorientation? ( A )Use a very rapid cross-check. ( B )Properly interpret the flight instruments and act accordingly. ( C )Avoid banking in excess of 30 degree. Question:00302 Group:0 Difficult:2 A49A sloping cloud formation, an obscured horizon, and a dark scene spread with ground lights and stars can create an illusion known as( A ) elevator illusions. ( B )autokinesis. ( C )false horizons. Question:00303 Group:0 Difficult:1 B50Which statement is correct regarding the use of cockpit lighting for night flight?( A )Reducing the lighting intensity to a minimum level will eliminate blind spots. ( B )The use of regular white light, such as a flashlight, will impair night adaptation. ( C )Coloration shown on maps is least affected by the use of direct red lighting. Question:00304 Group:0 Difficult:2 C51In the case of operations over an area designated as a mountainous area where no other minimum altitude is prescribed, no person may operate an aircraft under IFR below an altitude of( A )500 feet above the49

highest obstacle. ( B )1,000 feet above the highest obstacle. ( C )2,000 feet above the highest obstacle. Question:00305 Group:0 Difficult:1 B52When ATC has not imposed any climb or descent restrictions and aircraft are within 1,000 feet of assigned altitude, pilots should attempt to both climb and descend at a rate of between( A )500 feet per minute and 1,000 feet per minute. ( B )500 feet per minute and 1,500 feet per minute. ( C ) 1,000 feet per minute and 2,000 feet per minute. Question:00306 Group:0 Difficult:2 A53What action should you take if your No. 1 VOR receiver malfunctions while operating in controlled airspace under IFR? Your aircraft is equipped with two VOR receivers. The No. 1 receiver has VOR / Localizer / Glide Slope capability, and the No. 2 has on( A )Report the malfunction immediately to ATC. ( B )Continue the flight as cleared; no report is required. ( C )Continue the approach and request a VOR or NDB approach. Question:00308 Group:0 Difficult:1 A54While on an IFR flight, a pilot has an emergency which causes a deviation from an ATC clearance. What action must be taken?( A )Notify ATC of the deviation as soon as possible. ( B )Squawk 7700 for the duration of the emergency. ( C )Submit a detailed report to the chief of the ATC facility within 48 hours. Question:00309 Group:0 Difficult:1 B55An abbreviated departure clearance "...CLEARED AS FILED..." will always contain the name( A )and number of the STAR to be flown when filed in the flight plan. ( B )of the destination airport filed in the flight plan. ( C )of the first compulsory reporting point if not in a radar environment. Question:00310 Group:0 Difficult:2 C56Which clearance procedures may be issued by ATC without prior pilot request?( A )DPS, STARS, and contact approaches. ( B )Contact and visual approaches. ( C )DPS, STARS, and visual approaches. Question:00313 Group:0 Difficult:250

C57A particular instrument departure procedure requires a minimum climb rate of 210 feet per NM to 8,000 feet. If you climb with a ground speed of 140 knots, what is the rate of climb required in feet per minute?( A )210 ( B )450 ( C )490 Question:00315 Group:0 Difficult:1 B58What does the ATC term "Radar Contact" signify?( A )Your aircraft has been identified and you will receive separation from all aircraft while in contact with this radar facility. ( B )Your aircraft has been identified on the radar display and radar flight-following will be provided until radar identification is terminated. ( C )You will be given traffic advisories until advised the service has been terminated or that radar contact has been lost. Question:00316 Group:0 Difficult:1 C59Upon intercepting the assigned radial, the controller advises you that you are on the airway and to "RESUME OWN NAVIGATION." this phrase means that( A )you are still in radar contact, but must make position reports. ( B )radar services are terminated and you will be responsible for position reports. ( C )you are to assume responsibility for your own navigation. Question:00319 Group:0 Difficult:2 A60What is the definition of MEA?( A )The lowest published altitude which meets obstacle clearance requirements and assures acceptable navigational signal coverage. ( B )The lowest published altitude which meets obstacle requirements, assures acceptable navigational signal coverage, twoway radio communications, and provides adequate radar coverage. ( C )An altitude which meets obstacle clearance requirements, assures acceptable navigation signal coverage, two-way radiocommunications, adequate radar coverage, and accurate DME mileage. Question:00320 Group:0 Difficult:2 A61Reception of signals from an off-airway radio facility may be inadequate to identify the fix at the designated MEA. In this case, which altitude is designated for the fix?( A )MRA. ( B )MCA. ( C )MOCA. Question:00321 Group:0 Difficult:2 C62Which condition is guaranteed for all of the following altitude limits: MAA,51

MCA, MRA, MOCA, and MEA? (Non-mountainous area.)( A ) Adequate navigation signals. ( B )Adequate communications. ( C )1,000-foot obstacle clearance. Question:00332 Group:0 Difficult:1 A63What timing procedure should be used when performing a holding pattern at a VOR?( A )Timing for the outbound leg begins over or abeam the VOR, whichever occurs later. ( B )Timing for the inbound leg begins when initiating the turn inbound. ( C )Adjustments in timing of each pattern should be made on the inbound leg. Question:00333 Group:0 Difficult:2 C64At what point should the timing begin for the first leg outbound in a nonstandard holding pattern?( A ). Abeam the holding fix, or wings level, whichever occurs last. ( B ). When the wings are level at the completion of the 180 turn outbound. ( C ). When over or abeam the holding fix, whichever occurs later. Question:00334 Group:0 Difficult:2 C65When holding at an NDB, at what point should the timing begin for the second leg outbound?( A )When the wings are level and the wind drift correction angle is established after completing the turn to the outbound heading. ( B )When the wings are level after completing the turn to the outbound heading, or abeam the fix, whichever occurs first. ( C )When abeam the holding fix. Question:00335 Group:0 Difficult:1 B66Determine the time to be entered in block 10 of the flight plan. (Refer to the FD excerpt below, and use the wind entry closest to the flight planned altitude.) . route of flight Figures 69, 70, and 71 , Flight log and MAG VAR , Figure 70 , JUDDS T( A )1 hour 14 minutes. ( B )58 minutes. ( C )50 minutes. Question:00336 Group:0 Difficult:1 A67(Refer to FD excerpt below, and use the wind entry closest to the flight planned altitude.) Determine the time to be entered in block 10 of the flight from GJT to DRO. Route of flight Figure 21 , Flight log & MAG VAR Figure 22 , En route chart Figure( A )1 hour 08 minutes. ( B )152

hour 03 minutes. ( C )58 minutes. Question:00342 Group:0 Difficult:1 A68When being radar vectored for an ILS approach, at what point may you start a descent from your last assigned altitude to a lower minimum altitude if cleared for the approach?( A )When established on a segment of a published route or IAP. ( B )You may descend immediately to published glide slope interception altitude. ( C )Only after you are established on the final approach unless informed otherwise by ATC. Question:00343 Group:0 Difficult:1 C69While being vectored, if crossing the ILS final approach course becomes imminent and an approach clearance has not been issued, what action should be taken by the pilot?( A )Turn outbound on the final approach course, execute a procedure turn, and inform ATC. ( B )Turn inbound and execute the missed approach procedure at the outer marker if approach clearance has not been received. ( C )Maintain the last assigned heading and query ATC. Question:00360 Group:0 Difficult:2 B70Aircraft approach categories are based on( A )certificated approach speed at maximum gross weight. ( B )1.3 times the stall speed in landing configuration at maximum gross landing weight. ( C )1.3 times the stall speed at maximum gross weight.

Question:00361 Group:0 Difficult:2 C71When may you obtain a contact approach?( A )ATC may assign a contact approach if VFR conditions exist or you report the runway in sight and are clear of clouds. ( B )ATC may assign a contact approach if you are below the clouds and the visibility is at least 1 mile. ( C )ATC will assign a contact approach only upon request if the reported visibility is at least 1 mile. Question:00362 Group:0 Difficult:2 A72Which substitution is permitted when an ILS component is inoperative? ( A )A compass locator or precision radar may be substituted for the ILS outer or middle marker. ( B )ADF or VOR bearings which cross either the outer or middle marker sites may be substituted for these markers. ( C )DME, when53

located at the localizer antenna site, should be substituted for the outer or middle marker. Question:00363 Group:0 Difficult:2 A73RVR minimums for landing are prescribed in an IAP, but RVR is inoperative and cannot be reported for the intended runway at the time. Which of the following would be an operational consideration?( A ) RVR minimums which are specified in the procedures should be converted and applied as ground visibility. ( B )RVR minimums may be disregarded, providing the runway has an operative HIRL system. ( C )RVR minimums may be disregarded, providing all other components of the ILS system are operative Question:00364 Group:0 Difficult:2 B74What effect would a light crosswind of approximately 7 knots have on vortex behavior?( A )The light crosswind would rapidly dissipate vortex strength. ( B )The upwind vortex would tend to remain over the runway. ( C )The downwind vortex would tend to remain over the runway. Question:00365 Group:0 Difficult:1 C75The middle and far bars of 3-bar VASI will( A )both appear white to the pilot when on the upper glidepath ( B )constitute a 2-bar VASI for using the lower glidepath ( C )constitue a 2-bar VASI for using the upper glidepath Question:10001 Group:0 Difficult:1 C76Which condition would cause the altimeter to indicate a lower altitude than actually flown (true altitude)?( A )Air temperature lower than standard. ( B )Atmospheric pressure lower than standard. ( C )Air temperature warmer than standard. Question:10002 Group:0 Difficult:1 B77Under what condition will true altitude be lower than indicated altitude with an altimeter setting of 29.92" Hg?( A )In warmer than standard air temperature. ( B )In colder than standard air temperature. ( C )When density altitude is higher than indicated altitude. Question:10003 Group:0 Difficult:154

A78Altimeter setting is the value to which the scale of the pressure altimeter is set so the altimeter indicates( A )true altitude at field elevation. ( B )pressure altitude at field elevation. ( C )pressure altitude at sea level. Question:10004 Group:0 Difficult:1 B79At an altitude of 6,500 feet MSL, the current altimeter setting is 30.42" Hg. The pressure altitude would be approximately( A )7,500 feet. ( B ) 6,000 feet. ( C )6,500 feet. Question:10005 Group:0 Difficult:1 B80Pressure altitude is the altitude read on your altimeter when the instrument is adjusted to indicate height above( A )sea level. ( B )the standard datum plane. ( C )ground level. Question:10006 Group:0 Difficult:1 C81En route at FL290, the altimeter is set correctly, but not reset to the local altimeter setting of 30.57" Hg during descent. If the field elevation is 650 feet and the altimeter is functioning properly, what is the approximate indication upon landing?( A )715 feet. ( B )1,300 feet. ( C )Sea level. Question:10007 Group:0 Difficult:1 B82While you are flying at FL250, you hear ATC give an altimeter setting of 28.92" Hg in your area. At what pressure altitude are you flying? ( A )24,000 feet. ( B )25,000 feet. ( C )26,000 feet. Question:10008 Group:0 Difficult:1 C83If you are departing from an airport where you cannot obtain an altimeter setting, you should set your altimeter( A )on 29.92" Hg. ( B )on the current airport barometric pressure, if known. ( C )to the airport elevation. Question:10009 Group:0 Difficult:1 B84One characteristic that a properly functioning gyro depends upon for operation is the( A )ability to resist precession 90* to any applied force. ( B )resistance to deflection of the spinning wheel or disc. ( C ) deflecting force developed from the angular velocity of the spinning wheel. Question:10010 Group:0 Difficult:155

C85If a 180* steep turn is made to the right and the aircraft is rolled out to straight-and-level flight by visual references, the attitude indicator ( A )should immediately show straight-and-level flight. ( B )will show a slight skid and climb to the right. ( C )may show a slight climb and turn. Question:10011 Group:0 Difficult:1 A86Which condition during taxi is an indication that an attitude indicator is unreliable?( A )The horizon bar tilts more than 5* while making taxi turns. ( B )The horizon bar vibrates during warmup. ( C )The horizon bar does not align itself with the miniature airplane after warmup. Question:10012 Group:0 Difficult:1 C87While cruising at 160 knots, you wish to establish a climb at 130 knots. When entering the climb (full panel), it is proper to make the initial pitch change by increasing back elevator pressure until the( A )attitude indicator, airspeed, and vertical speed indicate a climb. ( B )vertical speed indication reaches the predetermined rate of climb. ( C )attitude indicator shows the approximate pitch attitude appropriate for the 130-knot climb. Question:10013 Group:0 Difficult:1 B88What indication should be observed on a turn coordinator during a left turn while taxiing?( A )The miniature aircraft will show a turn to the left and the ball remains centered. ( B )The miniature aircraft will show a turn to the left and the ball moves to the right. ( C )Angle of bank. Question:10014 Group:0 Difficult:1 A89What indications are displayed by the miniature aircraft of a turn coordinator?( A )Rate of roll and rate of turn. ( B )Direct indication of bank angle and pitch attitude. ( C )Indirect indication of bank angle and pitch attitude. Question:10015 Group:0 Difficult:1 C90During a constant-bank level turn, what effect would an increase in airspeed have on the rate and radius of turn?( A )Rate of turn would increase, and radius of turn would increase. ( B )Rate of turn would decrease, and radius of turn would decrease. ( C )Rate of turn would decrease, and radius of turn would increase.

56

Question:10016 Group:0 Difficult:1 C91What causes the northerly turning error in a magnetic compass? ( A )Coriolis force at the mid-latitudes. ( B )Centrifugal force acting on the compass card. ( C )The magnetic dip characteristic. Question:10017 Group:0 Difficult:1 A92As power is increased to enter a 500 feet per minute rate of climb in straight flight, which instruments are primary for pitch, bank, and power respectively? ( A )Attitude indicator, heading indicator, and manifold pressure gauge or tachometer. ( B )VSI, attitude indicator, and airspeed indicator. ( C )Airspeed indicator, attitude indicator, and manifold pressure gauge or tachometer. Question:10018 Group:0 Difficult:1 C93As a rule of thumb, altitude corrections of less than 100 feet should be corrected by using( A )two bar widths on the attitude indicator. ( B ) less than a full bar width on the attitude indicator. ( C )less than half bar width on the attitude indicator. Question:10019 Group:0 Difficult:1 C94As power is reduced to change airspeed from high to low cruise in level flight, which instruments are primary for pitch, bank, and power, respectively?( A )Attitude indicator, heading indicator, and manifold pressure gauge or tachometer. ( B )Altimeter, attitude indicator, and airspeed indicator. ( C )Altimeter, heading indicator, and manifold pressure gauge or tachometer. Question:10020 Group:0 Difficult:1 C95Which instruments, in addition to the attitude indicator, are pitch instruments?( A )Altimeter and airspeed only. ( B )Altimeter and VSI only. ( C )Altimeter, airspeed indicator, and vertical speed indicator. Question:10021 Group:0 Difficult:1 A96Which instrument is considered primary for power as the airspeed reaches the desired value during change of airspeed in a level turn?( A ) Airspeed indicator. ( B )Attitude indicator. ( C )Altimeter. Question:10022 Group:0 Difficult:1 C97Which instruments should be used to make a pitch correction when you57

have deviated from your assigned altitude?( A )Altimeter and VSI. ( B )Manifold pressure gauge and VSI. ( C )Attitude indicator, altimeter, and VSI. Question:10023 Group:0 Difficult:1 A98Conditions that determine the pitch attitude required to maintain level flight are( A )airspeed, air density, wing design, and angle of attack. ( B ) flight path, wind velocity, and angle of attack. ( C )relative wind, pressure altitude, and vertical lift component. Question:10024 Group:0 Difficult:1 A99Approximately what percent of the indicated vertical speed should be used to determine the number of feet to lead the level-off from a climb to a specific altitude?( A )10 percent. ( B )20 percent. ( C )25 percent. Question:10025 Group:0 Difficult:1 C100What angular deviation from a VOR course centerline is represented by a full-scale deflection of the CDI?( A )4*. ( B )5* . ( C )10*. Question:10026 Group:0 Difficult:1 C101When using VOR for navigation, which of the following should be considered as station passage?( A )The first movement of the CDI as the airplane enters the zone of confusion. ( B )The moment the TO-FROM indicator becomes blank. ( C )The first positive, complete reversal of the TOFROM indicator. Question:10027 Group:0 Difficult:1 B102A VOR receiver with normal five-dot course sensitivity shows a three-dot deflection at 30 NM from the station. The aircraft would be displaced approximately how far from the course centerline?( A )2 NM. ( B ) 3 NM. ( C )5 NM. Question:10028 Group:0 Difficult:1 B103An aircraft which is located 30 miles from a VOR station and shows a 1/2 scale deflection on the CDI would be how far from the selected course centerline?( A )1 1/2 miles. ( B )2 1/2 miles. ( C )3 1/2 miles. Question:10029 Group:0 Difficult:158

C104After passing a VORTAC, the CDI shows 1/2 scale deflection to the right. What is indicated if the deflection remains constant for a period of time? ( A )The airplane is getting closer to the radial. ( B )The OBS is erroneously set on the reciprocal heading. ( C )The airplane is flying away from the radial. Question:10030 Group:0 Difficult:1 C105Who is responsible for determining that the altimeter system has been checked and found to meet 14 CFR part 91 requirements for a particular instrument flight?( A )Owner. ( B )Operator. ( C )Pilot-incommand. Question:10031 Group:0 Difficult:1 C106Your aircraft had the static pressure system and altimeter tested and inspected on January 5, of this year, and was found to comply with FAA standards. These systems must be reinspected and approved for use in controlled airspace under IFR by( A )January 5, next year. ( B ) January 5, 2 years hence. ( C )January 31, 2 years hence. Question:10032 Group:0 Difficult:1 C107If a half-standard rate turn is maintained, how long would it take to turn 360?( A )1 minutes. ( B )2 minute. ( C )4 minutes. Question:10033 Group:0 Difficult:1 A108If a standard rate turn is maintained, how long would it take to turn 180? ( A )1 minutes. ( B )2 minute. ( C )3 minutes. Question:10034 Group:0 Difficult:1 A109What instruments are considered supporting bank instruments during a straight, stabilized climb at a constant rate?( A )Attitude indicator and turn coordinator. ( B )Heading indicator and attitude indicator. ( C ) Heading indicator and turn coordinator. Question:10035 Group:0 Difficult:1 B110What are the three fundamental skills involved in attitude instrument flying?( A )Instrument interpretation, trim application, and aircraft control. ( B )Cross check, instrument interpretation, and aircraft control. ( C ) Cross check, emphasis, and aircraft control.

59

Question:10036 Group:0 Difficult:1 C111Which instruments are considered to be supporting instruments for pitch during change of airspeed in a level turn?( A )Airspeed indicator and VSI. ( B )Altimeter and attitude indicator. ( C )Attitude indicator and VSI. Question:10037 Group:0 Difficult:1 C112During recoveries from unusual attitudes, level flight is attained the instant ( A )the horizon bar on the attitude indicator is exactly overlapped with the miniature airplane. ( B )a zero rate of climb is indicated on the VSI. ( C )the altimeter and airspeed needles stop prior to reversing their direction of movement. Question:10038 Group:0 Difficult:1 A113What record shall be made in the aircraft log or other permanent record by the pilot making the VOR operational check?( A )The date, place, bearing error, and signature. ( B )The date, frequency of VOR or VOT, number of flight hours since last check, and signature. ( C )The date, place, bearing error, aircraft total time, and signature. Question:10039 Group:0 Difficult:1 C114When using VOT to make a VOR receiver check, the CDI should be centered and the OBS should indicate that the aircraft is on the( A ) 090 radial. ( B )180 radial. ( C )360 radial. Question:10040 Group:0 Difficult:1 B115When the CDI needle is centered during an airborne VOR check, the omnibearing selector and the OBS indicator should read( A )within 4 of the selected radial. ( B )within 6 of the selected radial. ( C )0 TO, only if you are due south of the VOR. Question:10041 Group:0 Difficult:1 C116What is the meaning of a single coded identification received only once approximately every 30 seconds from a VORTAC?( A )The VOR and DME components are operative. ( B )VOR and DME components are both operative, but voice identification is out of service. ( C )The DME component is operative and the VOR component is inoperative.

60

Question:10042 Group:0 Difficult:1 A117Which of the following is required equipment for operating an aircraft within Class B airspace?( A )A 4096 code transponder with automatic pressure altitude reporting equipment. ( B )A VOR receiver with DME. ( C )A 4096 code transponder. Question:10043 Group:0 Difficult:1 C118When checking the sensitivity of a VOR receiver, the number of degrees in course change as the OBS is rotated to move the CDI from center to the last dot on either side should be between( A )5 and 6. ( B )8 and 10. ( C )10 and 12. Question:10044 Group:0 Difficult:1 B119What is the magnetic bearing TO the station for an aircraft with MH350 RB270?( A )060. ( B )260. ( C )270. Question:10047 Group:0 Difficult:1 A120For IFR operations off of established airways below 18,000 feet, VOR navigational aids used to describe the "route of flight" should be no more than ( A )80 NM apart. ( B )40 NM apart. ( C )70 NM apart. Question:10048 Group:0 Difficult:1 B121Full scale deflection of a CDI occurs when the course deviation bar or needle( A )deflects from left side of the scale to right side of the scale. ( B )deflects from the center of the scale to either far side of the scale. ( C )deflects from half scale left to half scale right. Question:10049 Group:0 Difficult:1 C122How should a pilot determine when the DME at municipal County Airport is inoperative?( A )The airborne DME will always indicate ``0'' mileage. ( B )The airborne DME will ``search,'' but will not ``lock on.'' ( C ) The airborne DME may appear normal, but there will be no code tone. Question:10052 Group:0 Difficult:1 A123What does the miniature aircraft of the turn coordinator directly display? ( A )Rate of roll and rate of turn. ( B )Angle of bank and rate of turn. ( C ) Both the miniature aircraft and the ball will remain centered.

61

Question:10064 Group:0 Difficult:1 A124Abrupt head movement during a prolonged constant rate turn in IMC or simulated instrument conditions can cause?( A )Pilot disorientation ( B )False horizon ( C )Elevator illusion Question:10065 Group:0 Difficult:1 C125A sloping cloud formation, an obscured horizon, and a dark scene spread with ground lights and starts can creat an illusion known as?( A ) Elevator illusions ( B )Autokinesis ( C )False horizons Question:10066 Group:0 Difficult:1 A126An abrupt change from climb to straight and level flight can create the illusion of?( A )tumbling backwards ( B )a nose up attitude ( C )a descent with the wings level Question:10067 Group:0 Difficult:1 B127a rapid acceleration during takeoff can create the illusion of? ( A )spinning in the oppsite direction ( B )being in a nose up attitude ( C ) diving into the ground Question:10068 Group:0 Difficult:1 B128Why is the hypoxia particular dangerous during flights with one pilot? ( A )Night vision may be so impaired that the pilot connot see other aircraft. ( B )Symptoms of hypoxia may be difficult to recognize before the pilot's reactions are affected. ( C )The pilot may not be able to control the aircraft even if using oxygen. Question:10069 Group:0 Difficult:1 C129The sensations which lead to spatial disorientation during instrument flight conditions( A )are frequently encountered by beginning instrument pilots,but never by pilots with moderate instrument experience. ( B )occur, in most instances,during the initial period of transition from visual to instrument flight ( C )must be supressed and complete reliance placed on the indications of the flight instrument. Question:10070 Group:0 Difficult:1 C130How can an instrument pilot best overcome spatial disorientation? ( A )Rely on kinesthetic sense. ( B )Use a very rapid cross-check. ( C )Read62

and interpret the flight instruments, and act accordingly. Question:10072 Group:0 Difficult:1 C131A pilot is more subject to spatial disorientation if( A )kinesthetic senses are ignored ( B )eyes are moved often in the process of cross-checking the flight instruments ( C )body signals are used to interpret flight attitude Question:10073 Group:0 Difficult:1 C132Which procedure is recommended to prevent or overcome spatial disorientation( A )Reduce head and eye movements to the extent possible ( B )Rely on kinsthetic sense ( C )Rely on the indications of the flight instruments Question:10074 Group:0 Difficult:1 B133What action should be taken if hyperventilation is suspected? ( A )Breathe at a slower rate by taking very deep breaths. ( B )Consciously breathe at a slower rate than normal ( C )Conciously force yourself to take deep breaths and breathe at a faster rate than normal Question:10075 Group:0 Difficult:1 C134If both the ram air input and the drain hole of the pitot systems are blocked, what reactions should you observe on the airspeed indicator when power is applied and a climb is initiated out of severe icing conditions? ( A )The indicated airspeed would show a continuous deceleragtion while climbing ( B )The airspeed would drop to, and remain at, zero ( C )No change until an actual climb rate is established then indicated airspeed will increase Question:10076 Group:0 Difficult:1 B135What indication should be observed on a turn coordinator during a left turn while taxiing?( A )The miniature aircraft will show a turn to the left and the ball remains centered. ( B )The miniature aircraft will show a turn to the left and the ball moves to the right. ( C )Both the miniature aircraft and the ball will remain centered. Question:10077 Group:0 Difficult:1 C136On the taxi check, the magnetic compass should( A )Swing opposite to the direction of turn when turning from north. ( B )Exhibit the same number of degrees of dip as the latitude. ( C )Swing freely and indicate63

known headings. Question:10078 Group:0 Difficult:1 A137Which condition during taxi is an indication that an attitude indicator is unreliable?( A )The horizon bar tilts more then 5 degree while making taxi turns. ( B )The horizon bar vibrates during warmup. ( C )The horizon bar does not align itself with the miniature airplane after warmup. Question:10079 Group:0 Difficult:1 A138What does the miniature aircraft of the turn coordinator directly display? ( A )Rate of roll and rate of turn ( B )Angle of bank and rate of turn. ( C ) Angle of bank. Question:10080 Group:0 Difficult:1 C139What pre-takeoff check should be made of the attitude indicator in preparation for IFR flight?( A )The horizon bar does not vibrate during warmup. ( B )The miniature aircraft should erect and become stable within 5 minutes ( C )The horizon bar should erect and become stable within 5 minutes Question:10081 Group:0 Difficult:1 B140During a skidding turn to right,what is the relationship between the component of lift, centrifugal force, and load factor?( A ) Centrifugal force is less than horizonal lift and the load factor is increase ( B ) Centrifugal force is greater than horizonal lift and the load factor is increase ( C )Centrifugal force and horizonal lift are equal and the load factor is decrease Question:10082 Group:0 Difficult:1 A141What indications are displayed by the miniature aircraft of a turn coordinator?( A )Rate of roll and rate of turn ( B )Direct indication of back angle and pitch attitude ( C )Indirect indication of back angle and pitch attitude Question:10083 Group:0 Difficult:1 A142What indication should a pilot observe if an airspeed indicator ram air input and drain hole are blocked?( A )The airspeed indicator will react as an altimeter ( B )The airspeed indicator will show a decrease with an64

increase in altitude ( C )No airspeed indicator change will occur dduring climbs or descents Question:10084 Group:0 Difficult:1 A143What indication is presented by the miniature aircraft of the turn coordinator?( A )Indirect Indication of the bank attitude ( B )Direct indication of the bank attitude and the quality of the turn ( C )Quality of the turn Question:10085 Group:0 Difficult:1 C144During normal operation of a vacuum-driven attitude indicator, what attitude indication should you see when rolling out from a 180 degree skidding turn to straight-and-level coordinated flight?( A )A straight-and-level coordinated flight indication ( B )A nose-high indication relative to level flight ( C )The miniature aircraft shows a turn in the direction opposite the skid. Question:10086 Group:0 Difficult:1 B145During normal coordinated turns, what error due to precession should you observe when rolling out to straight-and -level flight from a 180o steep turn to the right ?( A )A straight-and-level coordinated flight indication. ( B )The miniature aircraft would show a slight turn indication to the left. ( C )The miniature aircraft would show a slight descent and wings-level attitude. Question:10087 Group:0 Difficult:1 A146What information does a Mach meter present ?( A )The ratio of aircraft true airspeed to the speed of sound. ( B )The ratio of aircraft indicated airspeed to the speed of sound. ( C )The ratio of aircraft equivalent airspeed, corrected for installation error, to the speed of sound. Question:10088 Group:0 Difficult:1 B147What is the relationship between centrifugal force and the horizontal lift component in a coordinated turn?( A )Horizontal lift exceeds centrifugal force. ( B )Horizontal lift and centrifugal force are equal. ( C ) Centrifugal force exceeds horizontal lift . Question:10089 Group:0 Difficult:165

C148What force causes an airplane to turn?( A )Rudder pressure or force around the vertical axis. ( B )Vertical lift component. ( C )Horizontal lift component. Question:10090 Group:0 Difficult:1 C149What should be the indication on the magnetic compass as you roll into a standard rate turn to the left from an east heading in the Northern Hemisphere?( A )The compass will initially indicate a turn to the right. ( B )The compass will remain on east for a short time, then gradually catch up to the magnetic heading of the aircraft. ( C )The compass will indicate the aproximate correct magnetic heading if the roll into the turn is smooth. Question:10091 Group:0 Difficult:1 C150What would be the indication on the VSI during entry into a 500 FPM actual descent from level flight if the static ports were iced over?( A )The indication would be in reverse of the actual rate of descent (500 FPM climb) ( B )The initial indication would be a climb, then descent at a rate in excess of 500 FPM. ( C )The VSI pointer would remain at zero regardless of the actual rate of dcescent Question:10092 Group:0 Difficult:1 C151How should you preflight check the altimeter prior to an IFR flight? ( A )Set the altimeter to the current temperature. With current temperature and the altimeter indecation determine the calibrated altitude to compare with the field elevation. ( B )Set the altimeter first with 29.92" Hg and then the current altimeter setting. The change in altitude should correspond to the change in setting. ( C )Set the altimeter to the cuurent altimeter setting. The indication should be within 75 feet of the actual elevation for acceptable accuracy. Question:10093 Group:0 Difficult:1 C152Which practical test should be made on the electric gyro instruments prior to starting an engine?( A )Check that the electrical connections are secure on the back of the instruments. ( B )Check that the attitude of the miniature airctaft is wings level before turning on electrical power. ( C )Turn on the electrical poewer and listen for any unusual or irregular mechanical noise.

66

Question:10094 Group:0 Difficult:1 B153Prior to starting an engine, you should check the turn-and-slip indicator to determine if the( A )needle indication properly corresponds to the angle of the wings or rotors with the horizon ( B )needle is approximately centered and the tube is full of fluid ( C )ball will move freely from one end of the tube to the other when the aircraft is rocked Question:10095 Group:0 Difficult:1 A154What indications should you observe on the turn-and -slip indicator during taxi?( A )The ball moves freely opposite the turn, and the needle deflects in the direction of the turn ( B )The needle deflects in the direction of the turn, but the ball remains centered. ( C )The ball deflects opposite the turn, but the needle remains centered Question:10096 Group:0 Difficult:1 A155what pretakeoff check should be made of a vacuum driven heading indicator in preparation for an IFR flight?( A )After 5 minutes,set the indicator to the magnetic heading of the aircraft and check for proper alignment after taxi turns ( B )after 5minutes, check that the heading indicator card aligns itself with the magnetic heading of the aircraft. ( C )Determine that the heading indicator does not precess more than 2o in 5 minutes of ground operation. Question:10097 Group:0 Difficult:1 C156What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from an easterly heading in the Northern Hemisphere?( A )The compass will initially indicate a turn to the left. ( B )The compass will remain on east for a short time,them gradually catch up to the magnetic heading of the aircraft. ( C )The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth. Question:10098 Group:0 Difficult:1 A157What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a south heading in the Northern Hemisphere ?( A )The compass will indicate a turn to the right,but at a faster rate than is actually occurring. ( B )The compass will initially indicate a turn to the left. ( C )The compass will remain on south for a short67

time, then gradually catch up to the magnetic heading of the aircraft. Question:10099 Group:0 Difficult:1 B158On what headings will the magnetic compass read most accurately during a level 360o turn, with a bank of approximately 15o( A )135o through 225 o ( B )90o and 270 o ( C )180o and 0 o Question:10100 Group:0 Difficult:1 C159What causes the northerly turning error in a magnetic compass?( A )Coriolis force at the mid-latitudes. ( B )Centrifugal force acting on the compass card. ( C )The magnetic dip characteristic. Question:10101 Group:0 Difficult:1 A160What should be the indication on the magnetic compass when you roll into a standard rate turn to the left from a south heading in the Northern Hemisphere( A )The compass will indicate a turn to the left, but at a faster rate than is actually occurring. ( B )The compass will initially indicate a turn to the right. ( C )The compass will remain on south for a short time, then gradually catch up to the magnetic heading of the aircraft. Question:10102 Group:0 Difficult:1 C161what should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a westerly heading in the northern hemisphere?( A )The compass will initially show a turn in the opposite direction,then turn to a northerly indication but lagging behind the actual heading of the aircraft. ( B )The compass will renain om a westerly heading for a short time,then gradually catch up to the actual heading of the aircraft. ( C )The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth. Question:10103 Group:0 Difficult:1 B162what should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a northerly heading in the northern hemisphere?( A )The compass will indicate a turn to the right,but at a faster rate than is actually occurring. ( B )The compass will initially indicate a turn to the left. ( C )The compass will remain on north for a short time,then gradually catch up to the magnetic heading of the aircraft.

68

Question:10104 Group:0 Difficult:1 C163what should be the indication on the magnetic compass as you roll into a standard rate turn to the left from a west heading in the Northern Hemisphere ( A )the compass will initially indicate a turn to the right ( B )the compass will remain in west for a short time, then gradually catch up to the magnetic heading of the aircraft ( C )the compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth Question:10105 Group:0 Difficult:1 B164what should be the indication on the magnetic compass as you roll into a standard rate turn to the left from a north heading in the Northern Hemisphere ( A )the compass will indicate a turn to the left, but ar a faster rate than is actually occuring ( B )the compass will initially indicate a turn to the right ( C )the compass will remain on north for a short time, then gradually catch up to the magnetic heading of the aircraft Question:10106 Group:0 Difficult:1 C165If a half-standard rate turn is maintained, how long would it take to turn 360( A )1 minute ( B )2 minutes ( C )4 minutes Question:10107 Group:0 Difficult:1 A166If a standard rate turn is maintained, how long would it take to turn 180 ( A )1 minute ( B )2 minutes ( C )3 minutes Question:10108 Group:0 Difficult:1 B167If a half-standard rate is maintained, how much time would be required to turn clockwise from a heading of 90 to a heading of 180( A )30 seconds ( B )1 minute ( C )1 minute 30 second Question:10109 Group:0 Difficult:1 A168Errors in both pitch and bank indication on an attitude indicator are usually at maximum as the aircraft rolls out of a( A )180turn ( B )270 turn ( C )360 turn Question:10110 Group:0 Difficult:1 C169If a 180 steep turn is made to the right and the aircraft is rolled out to straight-and-level flight by visual references,the attitude indicator ( A )should immediately show straight-and-level flight ( B )will show a slight69

skid and climb to the right ( C )may show a slight climb and turn Question:10111 Group:0 Difficult:1 C170If a half-standard rate turn is maintained,how long would it take to turn 135( A )I minute ( B )1 minute 20 seconds ( C )1 minute 30 seconds Question:10112 Group:0 Difficult:1 C171If a standard rate turn is maintained ,how much time would be required to turn to the left from a heading of 090 to a heading of 300( A )30 seconds ( B )40seconds ( C )50 seconds Question:10113 Group:0 Difficult:1 B172One characteristic that a properly functioning gyro depends upon for operation is the( A )ability to resist precession 90 to any applied force ( B )resistance to deflection of the spinning wheel or disc ( C ) deflecting force developed from the angular velocity of the spinning wheel Question:10114 Group:0 Difficult:1 A173If a standard rate is maintained ,how much time would be required to turn to the right from a heading of 090 to a heading of 270( A )1 minute ( B )2 minutes ( C )3 minutes Question:10115 Group:0 Difficult:1 C174If,while in level flight,it becomes necessary to use an alternate source of ststic pressure vented inside the airplane,which of the following should the pilot expect?( A )The gyroscospic instruments to become inoperative. ( B )The altimeter and airspeed indicator to become inoperative. ( C )The vertical speed to momentarily show a climb. Question:10116 Group:0 Difficult:1 A175During flight,if the pitot-tube becomes clogged with ice,which of the following instruments would be affected?( A )The airspeed indicator only. ( B )The airspeed indicator and the altimeter. ( C )The airspeed indicator ,altimeter,and Vertical Speed Indicator. Question:10117 Group:0 Difficult:1 B176The local altimeter setting should be used by all pilots in a paticular area,70

primarily to provide for( A )the cancellation of altimeter error due to nonstander temperature aloft ( B )better vertical seperation of aircraft ( C ) more accurate terran clearance in mountainous areas Question:10118 Group:0 Difficult:1 B177At an altitude of 6,500 feet MSL, the current altimeter setting is 30.42 inches Hg. The pressure altitude would be approximately( A )7,500 feet ( B )6,000 feet ( C )6,500 feet Question:10119 Group:0 Difficult:1 B178If severe turbulence is encountered during your IFR flight , the airplane should be slowed to the design maneuvering speed because the( A ) manueuverablility of the airplane will be increased. ( B )amount of excess load that can be imposed on the wing will be decreased. ( C )airplane will stall at a lower angle of attack, giving an increased margin of safety. Question:10120 Group:0 Difficult:1 A179When an aircraft is accelerated, some attitude indicators will precess and incorrectly indicate a( A )climb ( B )descent ( C )right turn Question:10121 Group:0 Difficult:1 C180 ( A )left turn ( B )climb ( C )descent Question:10122 Group:0 Difficult:1 C181The displacment of a turn coodinator during a coordinated turn will ( A )indicate the angle of bank ( B )remain constant for a given bank regardless of airspeed ( C )increase as angle of bank increases Question:10123 Group:0 Difficult:1 B182Altimeter setting is the value to which the scale of the pressure altimeter is set so the altimeter indicates( A )Pressure altitude at sea level ( B ) true altitude at field elevation ( C )pressure altitude at field elevation Question:10124 Group:0 Difficult:1 B183pressure altitude is the altitude read on your altimeter when the altimeter is adjusted to indicate height above( A )sea level ( B )the standard datum plane ( C )ground level

71

Question:10125 Group:0 Difficult:1 B184If while in level flight, it becomes necessary to use an alternate source fo static pressure vented inside the airplane, which of the following variations in instrument in dications should the pilto expect?( A )The altimeter will read lower than normal, airspeed lower than normal, and the VSI will momentarily show a descent. ( B )The altimeter will read higher than normal, airspeed greater than normal, and the VSI will momentarily show a clmb. ( C )The altimeter will read lower than normal, airspeed greater than normal, and the VSI will momentarily show a climb and then a descent. Question:10131 Group:0 Difficult:1 A185when installed with the ILS and specified in the approach procedures, DME may be used( A )in lieu of the OM. ( B )in lieu of visibility requirements. ( C )to determine distance from TDZ. Question:10132 Group:0 Difficult:1 A186How does a pilot determine if DME is available on an ILS/LOC? ( A )IAP indicate DME/TACAN channel in LOC frequency box ( B ) LOC/DME are indicated on en route low altitude frequency box ( C ) Loc/DME frquencies available in the Aeronautical Information Manual. Question:10133 Group:0 Difficult:1 B187which of following statements is true regarding Parallel ILS approaches? ( A )Parallel ILS approach runway centerlines are separated by at least 4300 feet and standard IFR seperation is provided on the adjacent runway. ( B ) Parallel ILS approaches provide aircraft a minimum of 1 1/2 miles radar separation between successive aircraft on the adjacent localizer course. ( C ) Landing minimums to the adjacent runway will be higher than the minimums to the primary runway, but will normally be lower than the published circling minimums. Question:10134 Group:0 Difficult:1 A188When being radar vectored for an ILS approach, at what point may you start a descent from your last assigned altitude to a lower minimum altitude if cleared for the approach?( A )When established on a segment of a published route or IAP. ( B )You may descend immediately to published glide slope interception altitude. ( C )Only after you are established on the final approach unless informed otherwise by ATC.72

Question:10135 Group:0 Difficult:1 C189To remain on the ILS glidepath, the rate of descent must be( A ) decreased if the airspeed is increased. ( B )decreased if the ground speed is increased. ( C )increased if the ground speed is increased. Question:10136 Group:0 Difficult:1 C190The rate of descent required to stay on the ILS glide slope?( A ) must be increased if the groundspeed is decreased. ( B )will remain constant if the indicated airspeed remains constant. ( C )must be decresed if the groundspeed is decreased. Question:10137 Group:0 Difficult:1 B191Which indications will a pilot receive where an IM is Installed on a front course ILS approach? ( A )One dot per second and a steady amber light. ( B )Six dots per second and a flashing white light. ( C )Alternate dashes and a blue light. Question:10138 Group:0 Difficult:1 C192The rate of descend on the glide slope is dependent upon?( A ) true airspeed ( B )calibrated airspeed ( C )groundspeed Question:10139 Group:0 Difficult:1 B193Approximately what height is the glide slope center line at the MM of a typical ILS?( A )100 feet ( B )200 feet ( C )300 feet Question:10140 Group:0 Difficult:1 A194What is a difference between an SDF and LDA facility?( A )The SDF course width is either 6o or 12o while the LDA course width is approximately 5o ( B )The SDF course has no glide slope guidance while the LDA does. ( C )The SDF has no marker beacons while the LDA has at least an OM. Question:00006 Group:1 Difficult:1 C195(Refer to Figure 1.) Which altimeter depicts 12,000 feet?( A )2 ( B )3 ( C )4 Question:00042 Group:1 Difficult:173

A196(Refer to Figure 2.) In which general direction from the VORTAC is the aircraft located?( A )Northeast. ( B )Southeast. ( C )Southwest. Question:00043 Group:1 Difficult:2 A197(Refer to table 96 and 97 of Figures 3.) To which aircraft position(s) does HSI presentation "A" correspond?( A )9 and 6. ( B )9 only. ( C )6 only. Question:00043 Group:2 Difficult:2 B198(Refer to table 96 and 97 of Figures 3.) To which aircraft position(s) does HSI presentation "B" correspond?( A )11 ( B )5 and 13. ( C )7 and 11. Question:00043 Group:3 Difficult:2 C199(Refer to table 96 and 97 of Figures 3.) To which aircraft position does HSI presentation "C" correspond?( A )9 ( B )4 ( C )12 Question:00043 Group:4 Difficult:2 C200(Refer to table 96 and 97 of Figures 3.) To which aircraft position does HSI presentation "D" correspond?( A )1 ( B )10 ( C )2 Question:00043 Group:5 Difficult:2 C201(Refer to table 96 and 97 of Figures 3.) To which aircraft position(s) does HSI presentation "E" correspond?( A )8 only. ( B )3 only. ( C )8 and 3. Question:00043 Group:6 Difficult:1 A202(Refer to table 96 and 97 of Figures 3.) To which aircraft position does HSI presentation "F" correspond?( A )4 ( B )11 ( C )5 Question:00044 Group:1 Difficult:1 B203(Refer to Figure 4.) What is the magnetic bearing TO the station as indicated by illustration 4?( A )285*. ( B )055*. ( C )235*. Question:00044 Group:2 Difficult:1 B204(Refer to Figure 4) Which RMI illustration indicates the aircraft is located on the 055* radial of the station and heading away from the station? ( A )1 ( B )2 ( C )374

Question:00044 Group:3 Difficult:1 A205(Refer to Figure 4.) Which RMI illustration indicates the aircraft is southwest of the station and moving closer TO the station?( A )1 ( B )2 ( C )3 Question:00045 Group:1 Difficult:1 B206(Refer to Figure 5.) Where should the bearing pointer be located relative to the wing-tip reference to maintain the 16 DME range in a right-hand arc with a right crosswind component?( A )Behind the right wing-tip reference for VOR-2. ( B )Ahead of the right wing-tip reference for VOR-2. ( C )Behind the right wing-tip reference for VOR-1 . Question:00045 Group:2 Difficult:1 C207(Refer to Figure6) Which sequence of marker beacon indicator lights, and their respective codes, will you receive on the ILS RWY 6 approach procedure to the MAP?( A )Blue-alternate dots and dashes; amberdashes. ( B )Amber-alternate dots and dashes; blue-dashes. ( C )Blue-dashes; amber-alternate dots and dashes. Question:00046 Group:1 Difficult:2 C208(Refer to table 60AJ and 61J of Figures 6.) What is your position relative to the CARCO intersection, glide slope, and the localizer course? ( A )Past CARCO, below the glide slope, and right of the localizer course. ( B )Approaching CARCO, above the glide slope, and left of the localizer course. ( C )Past CARCO, above the glide slope, and right of the localizer course. Question:00046 Group:2 Difficult:2 B209(Refer to Figure 6) How does an LDA facility, such as the one at Roanoke Regional, differ from a standard ILS approach facility?( A )The LOC is wider. ( B )The LOC is offset from the runway. ( C )The GS is unusable beyond the MM. Question:00058 Group:1 Difficult:2 B210(Refer to Figure 7.) Which OBS selection on the No. 1 NAV would center the CDI and change the ambiguity indication to a TO?( A )175. ( B )165. ( C )345.

75

Question:00059 Group:1 Difficult:2 A211(Refer to table 65J and 66 of Figures 8.) What is your position relative to GRICE intersection?( A )Right of V552 and approaching GRICE intersection. ( B )Right of V552 and past GRICE intersection. ( C )Left of V552 and approaching GRICE intersection. Question:00311 Group:1 Difficult:1 C212(Refer to Figure 9.) At which minimum altitude should you cross the STAKK intersection?( A )6,500 feet MSL. ( B )1,400 feet MSL. ( C )10,200 feet MSL. Question:00311 Group:2 Difficul