(3) Set temperature controls to AUTO and COOL.
(4) For AF69-0024 and AF83-1285 and up, close troop compartment valve.
(5) Open all gasper nozzles.
(6) Close all compartment doors, hatches, and windows.
b. For AF69-0024 and AF83-1285 and up, after 20 to 30 minutes of operation, the forward upper deck should be cooled
sufficiently to open up the troop compartment valve.
c. No signi
¿
cant cargo compartment cooling can be obtained by operating both air conditioning packs from the APU.
Some cooling can be obtained by operating one pack with both APU, and the other pack with engine bleed air. Operate
one pack to maintain cooling in the upper deck compartments while the other pack is used to cool the cargo compart-
ments. Use of overhead recirculation fan increases air
À
ow from the lower cargo ducts.
1.5.4.3
Desert and Tropical Refueling.
In preparing the airplane for parking or operation during extremely hot weather,
observe the following precautions:
a. Take extreme care with all engine fuel at temperatures of 120 °F (49 °C) or more.
b. Particularly avoid the danger of sparks.
c. Open fuel drums with bronze or other non-sparking tools only.
1.5.5
Condition: Cold Temperatures.
When outside ambient temperatures are from 32 °F to -45 °F (0 °C to -43 °C) and
below, the following items shall be considered for proper operation and maintenance of the airplane.
1.5.5.1
Potable Water Tanks.
Do not add antifreeze to potable water storage tanks, Failure to comply could result in injury to personnel.
Whenever temperatures below 32 °F (0 °C) are anticipated, drain potable water tanks and remove all other
freezable liquids.
1.5.5.2
Hydraulic Systems.
NOTE
At temperatures of 0 °F (-18 °C) and below, hydraulic
À
uid foams readily. Do not over
¿
ll reservoirs or foam may
clog vents.
a. At temperatures of -25 °F (-32 °C) and below, leaks may occur at hydraulic components and lines throughout the
airplane. A check for leaks should be accomplished after the hydraulic systems are pressurized. Major leaks will
require system shutdown; minor leaks may stop as the system is warmed by operations or if heat is applied to the
component.
b. After cold soaks of 16 hours or longer at temperatures below -25 °F (-32 °C), leaks may occur at landing gear
components in the wheel wells, at hydraulic components in the cargo compartment, as well as at other random points
in the utility and
À
ight control subsystems throughout the airplane when the hydraulic systems are pressurized. An
inspection for leaks should be immediately accomplished throughout the airplane upon pressurization of the hydraulic
systems. Ground crew assistance should be provided to the scanner for this purpose while the
À
ight engineer monitors
À
uid quantity indicators for signi
¿
cant losses. Major leaks will require shutdown of the affected system for corrective
action. Self-warming of the hydraulic subsystem during initial operation will not be sufficient to cause the leaks to
stop. Preheating of the various manifold assemblies will be necessary, or the cargo compartment temperatures main-
tained near 0 °F (-18 °C) following shutdown on the previous
À
ight.
TO 1C-5M-2-1
1-34
Содержание C-5M
Страница 12: ...TO 1C 5M 2 1S 1 Figure 1 21 Circuit Breaker Locations Sheet 6 10...
Страница 13: ...TO 1C 5M 2 1S 1 Figure 1 21 Circuit Breaker Locations Sheet 13 11...
Страница 14: ...TO 1C 5M 2 1S 1 Figure 3 34 Crew Lavatory Waste Servicing AF68 0213 AF68 0216 and AF69 0024 12...
Страница 15: ...TO 1C 5M 2 1S 1 Figure 3 34 1 Tank Cleaning Adapter 13...
Страница 16: ...TO 1C 5M 2 1S 1 Figure 3 34 2 Toilet Maintenance Switch 14...
Страница 32: ......
Страница 40: ......
Страница 82: ...Figure 1 1 Airplane Dimensions TO 1C 5M 2 1 1 42...
Страница 83: ...Figure 1 2 Major Component Weights Sheet 1 of 3 TO 1C 5M 2 1 1 43...
Страница 84: ...Figure 1 2 Major Component Weights Sheet 2 TO 1C 5M 2 1 1 44...
Страница 85: ...Figure 1 2 Major Component Weights Sheet 3 TO 1C 5M 2 1 1 45...
Страница 86: ...Figure 1 3 Airplane Stations Sheet 1 of 8 TO 1C 5M 2 1 1 46...
Страница 87: ...Figure 1 3 Airplane Stations Sheet 2 TO 1C 5M 2 1 1 47...
Страница 88: ...Figure 1 3 Airplane Stations Sheet 3 TO 1C 5M 2 1 1 48...
Страница 89: ...Figure 1 3 Airplane Stations Sheet 4 TO 1C 5M 2 1 1 49...
Страница 90: ...Figure 1 3 Airplane Stations Sheet 5 TO 1C 5M 2 1 1 50...
Страница 91: ...Figure 1 3 Airplane Stations Sheet 6 TO 1C 5M 2 1 1 51...
Страница 92: ...Figure 1 3 Airplane Stations Sheet 7 TO 1C 5M 2 1 1 52...
Страница 93: ...Figure 1 3 Airplane Stations Sheet 8 TO 1C 5M 2 1 1 53...
Страница 94: ...Figure 1 4 Danger Areas Sheet 1 of 17 TO 1C 5M 2 1 1 54...
Страница 95: ...Figure 1 4 Danger Areas Sheet 2 TO 1C 5M 2 1 1 55...
Страница 96: ...Figure 1 4 Danger Areas Sheet 3 TO 1C 5M 2 1 1 56...
Страница 97: ...Figure 1 4 Danger Areas Sheet 4 TO 1C 5M 2 1 1 57...
Страница 98: ...Figure 1 4 Danger Areas Sheet 5 TO 1C 5M 2 1 1 58...
Страница 99: ...Figure 1 4 Danger Areas Sheet 6 TO 1C 5M 2 1 1 59...
Страница 100: ...Figure 1 4 Danger Areas Sheet 7 TO 1C 5M 2 1 1 60...