TM 1-1510-218-10
8A-25
f. Takeoff.
NOTE
Following takeoff from runways covered
with snow or slush, consideration should
be given to operating the landing gear
through several complete cycles, within
limits, to dislodge ice accumulated from
the spray of slush and water and to prevent
gear freezing in the retracted position.
Takeoff procedures for cold weather operations
are the same as for normal takeoff. Taking off with
temperature at or below freezing, with water, slush, or
snow on the runway, can cause ice to accumulate on
the landing gear and can throw ice into the wheel well
areas. Such takeoffs shall be made with brake deice
on and with the ice vanes extended to preclude the
possibility of ice build-up on engine air inlets. Monitor
oil temperature to ensure operation within limits.
Before flight into icing conditions, the pilot's and
copilot's
WSHLD
ANTI-ICE
switches should be set at
NORMAL
position.
g. During
Flight.
(1)
After takeoff from a runway covered with
snow or slush, it may be advisable to leave brake
deice on to dislodge ice accumulated from the spray of
slush or water. Monitor
BRAKE DEICE ON
annunciator for automatic termination of system
operation and then turn the switch off. During flight,
trim tabs and controls should also be exercised
periodically to prevent freezing. Ensure that anti-icing
systems are activated before entering icing conditions.
Do not activate the surface deice system until ice has
accumulated 1/2 inch. The propeller deice system
operates effectively as an anti-ice system and it may
be operated continuously in flight. If propeller
imbalance due to ice does occur, it may be relieved by
increasing RPM briefly, then returning to desired
setting.
(2)
Ice vanes must be extended when
operating in visible moisture or when freedom from
visible moisture cannot be assured, at +5 °C OAT or
less. Ice vanes are designed as an anti-ice system,
not a deice system. After the engine air inlet screens
are blocked, extending the ice vanes will not rectify the
condition. Ice vanes should be retracted at +15 °C
OAT and above to assure adequate engine oil cooling.
(3)
Stalling airspeeds should be expected to
increase when ice has accumulated on the aircraft
causing distortion of the wing airfoil. For the same
reason, stall warning devices are not accurate and
should not be relied upon. Keep a comfortable margin
of airspeed above the normal stall airspeed. Maintain
a minimum of 140 knots during sustained icing
conditions to prevent ice accumulation on unprotected
surfaces of the wing. In the event of windshield icing,
reduce airspeed to 226 knots or below.
h. Descent.
Use normal procedures in Section
II. Brake deicing should be considered if moisture was
encountered during previous ground operations or in
flight, in icing conditions with gear extended.
i. Landing.
Landing on an icy runway should
be attempted only when absolutely necessary and
should not be attempted unless the wind is within 10
q
of runway heading. Application of brakes without
skidding the tires on ice is difficult. In order not to
impair pilot visibility, reverse thrust should be used
with caution when landing on a runway covered with
snow or standing water. Use normal procedures in
Section II.
j. Engine
Shutdown.
Use normal procedures
in Section II.
k. Before Leaving Aircraft.
When the aircraft
is parked outside on ice or in a fluctuating freeze/thaw
temperature condition, the following procedures should
be followed. After wheel chocks are in place, release
the brakes to prevent freezing. Fill fuel tanks to
minimize condensation, remove any accumulation of
dirt and ice from the landing gear shock struts, and
install protective covers to guard against possible
collection of snow and ice.
8A-57. DESERT OPERATION AND HOT WEATHER
OPERATION.
Dust, sand, and high temperatures encountered
during desert operation can sharply reduce the
operational life of the aircraft and its equipment. The
abrasive qualities of dust and sand on turbine blades
and other moving parts of the aircraft and the
destructive effect of heat upon the aircraft instruments
will necessitate hours of maintenance if basic
preventive measures are not followed. In flight, the
hazards of dust and sand will be difficult to escape,
since dust clouds over a desert may be found at
altitudes up to 10,000 feet. During hot weather
operations, the principal difficulties encountered are
high turbine gas temperatures (TGT/ITT) during
engine starting, overheating of brakes, and longer
takeoff and landing rolls due to the higher density
altitudes. In areas where high humidity is
encountered, electrical equipment, such as
communication equipment and instruments, will be
subject to malfunction by corrosion, fungi, and
moisture absorption by nonmetallic materials.
Summary of Contents for C-12C
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Page 21: ...TM 1 1510 218 10 Figure 2 2 Typical General Interior Arrangement 2 5 ...
Page 22: ...TM 1 1510 218 10 Figure 2 3 Principal Dimensions C Sheet 1 of 2 2 6 ...
Page 23: ...TM 1 1510 218 10 2 7 Figure 2 3 Principal Dimensions D T Sheet 2 of 2 ...
Page 37: ...TM 1 1510 218 10 2 21 Figure 2 9 Control Pedestal D2 Sheet 1 of 3 ...
Page 38: ...TM 1 1510 218 10 Figure 2 9 Control Pedestal T1 Sheet 2 of 3 2 22 ...
Page 39: ...TM 1 1510 218 10 2 23 Figure 2 9 Control Pedestal T2 Sheet 3 of 3 ...
Page 43: ...TM 1 1510 218 10 Figure 2 12 Cabin Door and Cabin Emergency Hatch D T 2 27 ...
Page 51: ...TM 1 1510 218 10 Figure 2 15 Overhead Control Panel C D T1 Sheet 1 of 2 2 35 ...
Page 52: ...TM 1 1510 218 10 Figure 2 15 Overhead Control Panel T2 Sheet 2 of 2 2 36 ...
Page 54: ...TM 1 1510 218 10 Figure 2 16 Overhead Circuit Breaker Panel C Sheet 1 of 4 2 38 ...
Page 55: ...TM 1 1510 218 10 Figure 2 16 Overhead Circuit Breaker Panel D1 Sheet 2 of 4 2 39 ...
Page 56: ...TM 1 1510 218 10 2 40 Figure 2 16 Overhead Circuit Breaker Panel D2 Sheet 3 of 4 ...
Page 57: ...TM 1 1510 218 10 Figure 2 16 Overhead Circuit Breaker Panel T1 Sheet 4 of 4 2 41 ...
Page 59: ...TM 1 1510 218 10 2 43 Figure 2 17 Instrument Panel C D1 Sheet 1 of 4 ...
Page 60: ...TM 1 1510 218 10 2 44 Figure 2 17 Instrument Panel D2 Sheet 2 of 4 ...
Page 61: ...TM 1 1510 218 10 2 45 Figure 2 17 Instrument Panel T1 Sheet 3 of 4 ...
Page 62: ...TM 1 1510 218 10 Figure 2 17 Instrument Panel T2 Sheet 4 of 4 2 46 ...
Page 69: ...TM 1 1510 218 10 2 53 Figure 2 18 Fuel System ...
Page 75: ...TM 1 1510 218 10 2 59 Figure 2 20 Gravity Feed Fuel Flow ...
Page 76: ...TM 1 1510 218 10 2 60 Figure 2 21 Crossfeed Fuel Flow ...
Page 97: ...TM 1 1510 218 10 Figure 2 24 Oxygen System Servicing Pressure Chart 2 81 ...
Page 102: ...TM 1 1510 218 10 Figure 2 25 Oxygen System C Sheet 1 of 2 2 86 ...
Page 103: ...TM 1 1510 218 10 Figure 2 25 Oxygen System D T Sheet 2 of 2 2 87 ...
Page 106: ...TM 1 1510 218 10 2 90 Figure 2 26 Environmental System ...
Page 110: ...TM 1 1510 218 10 Figure 2 27 DC Electrical System Schematic C D1 2 94 ...
Page 114: ...TM 1 1510 218 10 Figure 2 28 DC Electrical System Schematic D2 T1 Sheet 1 of 2 2 98 ...
Page 115: ...TM 1 1510 218 10 Figure 2 28 DC Electrical System Schematic T2 Sheet 2 of 2 2 99 ...
Page 126: ...TM 1 1510 218 10 Figure 2 29 AC Electrical System Schematic Diagram D2 Sheet 2 of 3 2 110 ...
Page 127: ...TM 1 1510 218 10 Figure 2 29 AC Electrical System Schematic Diagram T Sheet 3 of 3 2 111 ...
Page 133: ...TM 1 1510 218 10 Figure 2 31 Pitot and Static System 2 117 ...
Page 153: ...TM 1 1510 218 10 Figure 2 34 Mooring 2 137 2 138 blank ...
Page 154: ... ...
Page 290: ......
Page 376: ...TM 1 1510 218 10 Figure 3C 7 ADI Pitch Scale 3C 22 ...
Page 387: ...TM 1 1510 218 10 Figure 3C 12 Map ARC Format Figure 3C 13 Map Symbols 3C 33 ...
Page 449: ...TM 1 1510 218 10 3C 95 Figure 3C 39 Lateral Course Edit ...
Page 465: ...TM 1 1510 218 10 Figure 3C 56 Entry and Display of VNAV Parameters 3C 111 ...
Page 473: ...TM 1 1510 218 10 Figure 3C 64 Alternate Flight Plan Schedule 3C 119 ...
Page 484: ...TM 1 1510 218 10 Figure 3C 75 Parallel Entry Into a Holding Pattern 3C 130 ...
Page 506: ...TM 1 1510 218 10 Figure 3C 99 MFP Geometry Definitions 3C 152 ...
Page 515: ...TM 1 1520 218 10 10 Figure 3C 108 FROM TO Options for the Data Page Examples Only 3C 161 ...
Page 517: ...TM 1 1520 218 10 3C 163 Figure 3C 110 Data For Option 1 Figure 3C 111 Data For Option 2 ...
Page 518: ...TM 1 1520 218 10 3C 164 Figure 3C 112 Data For Option 3 Figure 3C 113 Data For Option 4 ...
Page 574: ... ...
Page 576: ... ...
Page 578: ...TM 1 1510 218 10 Figure 5 1 Instrument Markings and Operating Limits C D Sheet 1 of 7 5 2 ...
Page 579: ...TM 1 1510 218 10 5 3 Figure 5 1 Instrument Markings and Operating Limits C D Sheet 2 of 7 ...
Page 582: ...TM 1 1510 218 10 Figure 5 1 Instrument Markings and Operating Limits Sheet 5 of 7 5 6 ...
Page 583: ...TM 1 1510 218 10 Figure 5 1 Instrument Markings and Operating Limits Sheet 6 of 7 5 7 ...
Page 599: ...TM 1 1520 218 10 Figure 6 2 Fuel Moment Chart 6 5 ...
Page 601: ...TM 1 1520 218 10 Figure 6 3 Baggage Moment 6 7 ...
Page 602: ...TM 1 1520 218 10 Figure 6 4 Personnel Moments 6 8 ...
Page 603: ...TM 1 1520 218 10 Figure 6 5 Cargo Moment C D1 T1 1 of 2 6 9 ...
Page 604: ...TM 1 1520 218 10 Figure 6 5 Cargo Moment T2 2 of 2 6 10 ...
Page 606: ...TM 1 1520 218 10 Figure 6 6 Cargo Loading C D T1 1 of 2 6 12 ...
Page 607: ...TM 1 1520 218 10 6 13 Figure 6 6 Cargo Loading T2 2 of 2 ...
Page 608: ...TM 1 1520 218 10 6 14 Figure 6 7 Center of Gravity Limitations ...
Page 609: ...TM 1 1520 218 10 6 15 Figure 6 8 Center of Gravity Limitations Above 12 500 ...
Page 610: ...TM 1 1520 218 10 6 16 Figure 6 9 Cargo Restraint and Tiedown Method ...
Page 612: ... ...
Page 621: ...TM 1 1510 218 10 Figure 7 5 Takeoff Performance Planning Tabulations Flaps 0 7 9 ...
Page 622: ...TM 1 1510 218 10 Figure 7 6 Takeoff Performance Planning Tabulations Flaps 0 7 10 ...
Page 623: ...TM 1 1510 218 10 Figure 7 7 Takeoff Performance Planning Tabulations Flaps 40 7 11 ...
Page 624: ...TM 1 1510 218 10 Figure 7 8 Takeoff Performance Planning Tabulations Flaps 40 7 12 ...
Page 625: ...TM 1 1510 218 10 Figure 7 9 Stall Speeds Power Idle 7 13 ...
Page 626: ...TM 1 1510 218 10 Figure 7 10 Temperature Conversion Correction for Compressibility 7 14 ...
Page 627: ...TM 1 1510 218 10 Figure 7 11 ISA Conversion 7 15 ...
Page 628: ...TM 1 1510 218 10 Figure 7 12 Altimeter Position Error Correction Normal System 7 16 ...
Page 629: ...TM 1 1510 218 10 Figure 7 13 Airspeed Calibration Normal System Ground Roll 7 17 ...
Page 634: ...TM 1 1510 218 10 Figure 7 18 Takeoff Distance Flaps 0 7 22 ...
Page 635: ...TM 1 1510 218 10 Figure 7 19 Accelerate Stop Distance Flaps 0 7 23 ...
Page 636: ...TM 1 1510 218 10 Figure 7 20 Accelerate Go Distance Flaps 0 7 24 ...
Page 637: ...TM 1 1510 218 10 Figure 7 21 Takeoff Distance Flaps 40 7 25 ...
Page 638: ...TM 1 1510 218 10 Figure 7 22 Accelerate Stop Distance Flaps 40 7 26 ...
Page 639: ...TM 1 1510 218 10 Figure 7 23 Accelerate Go Distance Flaps 40 7 27 ...
Page 640: ...TM 1 1510 218 10 Figure 7 24 Line Speed Check During Takeoff Ground Run 7 28 ...
Page 641: ...TM 1 1510 218 10 Figure 7 25 Climb Two Engines Flaps 0 7 29 ...
Page 642: ...TM 1 1510 218 10 Figure 7 26 Climb Two Engines Flaps 40 7 30 ...
Page 643: ...TM 1 1510 218 10 Figure 7 27 Climb One Engine Inoperative 7 31 ...
Page 644: ...TM 1 1510 218 10 Figure 7 28 Time Fuel Distance to Cruise Climb 7 32 ...
Page 645: ...TM 1 1510 218 10 Figure 7 29 Service Ceiling One Engine Inoperative 7 33 ...
Page 646: ...TM 1 1510 218 10 Figure 7 30 Landing Distance Without Propeller Reversing Flaps 100 7 34 ...
Page 647: ...TM 1 1510 218 10 Figure 7 31 Landing Distance Without Propeller Reversing Flaps 40 7 35 ...
Page 648: ...TM 1 1510 218 10 Figure 7 32 Landing Distance Without Propeller Reversing Flaps 0 7 36 ...
Page 649: ...TM 1 1510 218 10 Figure 7 33 Landing Distance With Propeller Reversing Flaps 100 7 37 ...
Page 650: ...TM 1 1510 218 10 Figure 7 34 Landing Distance With Propeller Reversing Flaps 40 7 38 ...
Page 651: ...TM 1 1510 218 10 Figure 7 35 Landing Distance With Propeller Reversing Flaps 0 7 39 ...
Page 652: ...TM 1 1510 218 10 Figure 7 36 Stopping Distance Factors 7 40 ...
Page 653: ...TM 1 1510 218 10 Figure 7 37 Cabin Altitude for Various Airplane Altitudes 7 41 ...
Page 662: ...TM 1 1510 218 10 Figure 7 46 Recommended Cruise Speeds 1700 RPM 7 50 ...
Page 663: ...TM 1 1510 218 10 Figure 7 47 Recommended Cruise Power 1700 RPM 7 51 ...
Page 664: ...TM 1 1510 218 10 Figure 7 48 Fuel Flow at Recommended Cruise Power 1700 RPM 7 52 ...
Page 673: ...TM 1 1510 218 10 Figure 7 57 Recommended Cruise Speeds 1800 RPM 7 61 ...
Page 674: ...TM 1 1510 218 10 Figure 7 58 Recommended Cruise Power 1800 RPM 7 62 ...
Page 675: ...TM 1 1510 218 10 Figure 7 59 Fuel Flow at Recommended Cruise Power 1800 RPM 7 63 ...
Page 684: ...TM 1 1510 218 10 Figure 7 68 Maximum Cruise Speeds 1900 RPM 7 72 ...
Page 685: ...TM 1 1510 218 10 Figure 7 69 Maximum Cruise Power 1900 PRM 7 73 ...
Page 686: ...TM 1 1510 218 10 Figure 7 70 Fuel Flow at Maximum Cruise Power 1900 RPM 7 74 ...
Page 687: ...TM 1 1510 218 10 Figure 7 71 Maximum Range Power 1700 RPM ISA 30 C 7 75 ...
Page 688: ...TM 1 1510 218 10 Figure 7 72 Maximum Range Power 1700 RPM ISA 20 C 7 76 ...
Page 689: ...TM 1 1510 218 10 Figure 7 73 Maximum Range Power 1700 RPM ISA 10 C 7 77 ...
Page 690: ...TM 1 1510 218 10 Figure 7 74 Maximum Range Power 1700 RPM ISA 7 78 ...
Page 691: ...TM 1 1510 218 10 Figure 7 75 Maximum Range Power 1700 RPM ISA 10 C 7 79 ...
Page 692: ...TM 1 1510 218 10 Figure 7 76 Maximum Range Power 1700 RPM ISA 20 C 7 80 ...
Page 693: ...TM 1 1510 218 10 Figure 7 77 Maximum Range Power 1700 RPM ISA 30 C 7 81 ...
Page 694: ...TM 1 1510 218 10 Figure 7 78 Maximum Range Power 1700 RPM ISA 37 C 7 82 ...
Page 711: ...TM 1 1510 218 10 7A 9 Figure 7A 5 Airspeed Calibration Normal System Takeoff Ground Roll ...
Page 712: ...TM 1 1510 218 10 7A 10 Figure 7A 6 Airspeed Calibration Normal System ...
Page 713: ...TM 1 1510 218 10 7A 11 Figure 7A 7 Altimeter Correction Normal System ...
Page 714: ...TM 1 1510 218 10 7A 12 Figure 7A 8 Airspeed Calibration Alternate System ...
Page 715: ...TM 1 1510 218 10 7A 13 Figure 7A 9 Altimeter Correction Alternate System ...
Page 716: ...TM 1 1510 218 10 7A 14 Figure 7A 10 Indicated Outside Air Temperature Correction ISA ...
Page 717: ...TM 1 1510 218 10 7A 15 Figure 7A 11 ISA Conversion ...
Page 718: ...TM 1 1510 218 10 7A 16 Figure 7A 12 Fahrenheit to Celsius Temperature Conversion ...
Page 719: ...TM 1 1510 218 10 7A 17 Figure 7A 13 Stall Speeds Power Idle ...
Page 720: ...TM 1 1510 218 10 7A 18 Figure 7A 14 Cabin Altitude for Various Airplane Altitudes ...
Page 724: ...TM 1 1510 218 10 7A 22 Figure 7A 18 Minimum Takeoff Power With Ice Vanes Extended 65 Knots ...
Page 725: ...TM 1 1510 218 10 7A 23 Figure 7A 19 Takeoff Flight Path ...
Page 726: ...TM 1 1510 218 10 7A 24 Figure 7A 20 Wind Component ...
Page 727: ...TM 1 1510 218 10 7A 25 Figure 7A 21 Take Off Distance Flaps UP ...
Page 728: ...TM 1 1510 218 10 7A 26 Figure 7A 22 Accelerate Stop Flaps UP ...
Page 729: ...TM 1 1510 218 10 7A 27 Figure 7A 23 Accelerate Go Flaps UP ...
Page 730: ...TM 1 1510 218 10 7A 28 Figure 7A 24 Net Gradient of Climb Flaps UP ...
Page 731: ...TM 1 1510 218 10 7A 29 Figure 7A 25 Take off Distance Flaps APPROACH ...
Page 732: ...TM 1 1510 218 10 7A 30 Figure 7A 26 Accelerate Stop Flaps APPROACH ...
Page 733: ...TM 1 1510 218 10 7A 31 Figure 7A 27 Accelerate Go Flaps APPROACH ...
Page 734: ...TM 1 1510 218 10 7A 32 Figure 7A 28 Net Gradient of Climb Flaps APPROACH ...
Page 735: ...TM 1 1510 218 10 7A 33 Figure 7A 29 Climb Two Engines Flaps UP ...
Page 736: ...TM 1 1510 218 10 7A 34 Figure 7A 30 Climb Two Engines Flaps APPROACH ...
Page 737: ...TM 1 1510 218 10 7A 35 Figure 7A 31 Climb One Engine Inoperative ...
Page 738: ...TM 1 1510 218 10 7A 36 Figure 7A 32 Service Ceiling One Engine Inoperative ...
Page 739: ...TM 1 1510 218 10 7A 37 Figure 7A 33 Time Fuel and Distance to Climb ...
Page 748: ...TM 1 1510 218 10 7A 46 Figure 7A 42 Normal Cruise Speeds 1700 RPM ...
Page 749: ...TM 1 1510 218 10 7A 47 Figure 7A 43 Normal Cruise Power 1700 RPM ...
Page 750: ...TM 1 1510 218 10 7A 48 Figure 7A 44 Fuel Flow At Normal Cruise Power 1700 RPM ...
Page 751: ...TM 1 1510 218 10 7A 49 Figure 7A 45 Range Profile Normal Cruise Power 1700 RPM ...
Page 760: ...TM 1 1510 218 10 Figure 7A 54 Maximum Cruise Speeds 1700 RPM 7A 58 ...
Page 761: ...TM 1 1510 218 10 Figure 7A 55 Maximum Cruise Power 1700 RPM 7A 59 ...
Page 762: ...TM 1 1510 218 10 Figure 7A 56 Fuel Flow At Maximum Cruise Power 1700 RPM 7A 60 ...
Page 763: ...TM 1 1510 218 10 Figure 7A 57 Range Profile Maximum Cruise Power 1700 RPM 7A 61 ...
Page 772: ...TM 1 1510 218 10 Figure 7A 66 Normal Cruise Speeds 1800 RPM 7A 70 ...
Page 773: ...TM 1 1510 218 10 Figure 7A 67 Normal Cruise Power 1800 RPM 7A 71 ...
Page 774: ...TM 1 1510 218 10 Figure 7A 68 Fuel Flow at Normal Cruise Power 1800 RPM 7A 72 ...
Page 775: ...TM 1 1510 218 10 Figure 7A 69 Range Profile Normal Cruise Power 1800 RPM 7A 73 ...
Page 784: ...TM 1 1510 218 10 Figure 7A 78 Maximum Cruise Speeds 1800 RPM 7A 82 ...
Page 785: ...TM 1 1510 218 10 Figure 7A 79 Maximum Cruise Power 1800 RPM 7A 83 ...
Page 786: ...TM 1 1510 218 10 7A 84 Figure 7A 80 Fuel Flow At Maximum Cruise Power 1800 RPM ...
Page 787: ...TM 1 1510 218 10 Figure 7A 81 Range Profile Maximum Cruise Power 1800 RPM 7A 85 ...
Page 804: ...TM 1 1510 218 10 Figure 7A 90 Range Profile Maximum Range Power 1700 RPM 7A 102 ...
Page 805: ...TM 1 1510 218 10 Figure 7A 91 Range Profile Full Main and Auxiliary Tanks 7A 103 ...
Page 806: ...TM 1 1510 218 10 Figure 7A 92 Endurance Profile Full Main and Auxiliary Tanks 7A 104 ...
Page 807: ...TM 1 1510 218 10 Figure 7A 93 Range Profile Full Main Tanks 7A 105 ...
Page 808: ...TM 1 1510 218 10 Figure 7A 94 Endurance Profile Full Main Tanks 7A 106 ...
Page 817: ...TM 1 1510 218 10 Figure 7A 103 Pressurization Controller Setting for Landing 7A 115 ...
Page 818: ...TM 1 1510 218 10 Figure 7A 104 Holding Time 7A 116 ...
Page 819: ...TM 1 1510 218 10 Figure 7A 105 Time Fuel and Distance to Descend 7A 117 ...
Page 820: ...TM 1 1510 218 10 Figure 7A 106 Climb Balked Landing 7A 118 ...
Page 822: ...TM 1 1510 218 10 7A 120 Figure 7A 108 Landing Distance Without Propeller Reversing Flaps UP ...
Page 823: ...TM 1 1510 218 10 7A 121 Figure 7A 109 Landing Distance With Propeller Reversing Flaps DOWN ...
Page 824: ...TM 1 1510 218 10 7A 122 Figure 7A 110 Landing Distance With Propeller Reversing Flaps UP ...
Page 825: ...TM 1 1510 218 10 7A 123 7A 124 blank Figure 7A 111 Stopping Distance Factors ...
Page 826: ... ...
Page 853: ...TM 1 1510 218 10 8 27 Figure 8 2 Stall Speed ...
Page 883: ...TM 1 1510 218 10 8A 23 Figure 8A 3 Figure Stall Speeds Power Idle ...
Page 892: ...TM 1 1510 218 10 9 2 Figure 9 1 Emergency Exits and Equipment ...
Page 896: ...TM 1 1510 218 10 9 6 Figure 9 2 Maximum Glide Distance ...
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Page 948: ... PIN 0 000 ...