1C-5M-2-1_601-690.pdf

Figure 4-3. MLG Lubrication (Sheet 5)

TO 1C-5M-2-1

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Figure 4-3. MLG Lubrication (Sheet 6)

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Figure 4-3. MLG Lubrication (Sheet 7)

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Figure 4-4. Visor Door Lubrication

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Figure 4-5. Crew Entry Door Lubrication (Sheet 1 of 2)

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Figure 4-5. Crew Entry Door Lubrication (Sheet 2)

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Figure 4-6. Flight Deck Stair Ladder Lubrication

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Figure 4-7. Wing Leading Edge Slat Drive System Lubrication (Sheet 1 of 4)

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Figure 4-7. Wing Leading Edge Slat Drive System Lubrication (Sheet 2)

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Figure 4-7. Wing Leading Edge Slat Drive System Lubrication (Sheet 3)

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Figure 4-7. Wing Leading Edge Slat Drive System Lubrication (Sheet 4)

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Figure 4-8. Wing Leading Edge Structure Lubrication

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Figure 4-9. Ground Spoiler Actuator Lubrication

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Figure 4-10. Flight Spoiler Servo Lubrication

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Figure 4-11. Wing Trailing Edge Flap Actuator Lubrication

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Figure 4-12. Aileron Servo Lubrication

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Figure 4-13. Wing Trailing Edge Structure Lubrication (Sheet 1 of 2)

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Figure 4-13. Wing Trailing Edge Structure Lubrication (Sheet 2)

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Figure 4-14. Rudder Servo Lubrication

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Figure 4-15. Elevator Servo Lubrication (Sheet 1 of 2)

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Figure 4-15. Elevator Servo Lubrication (Sheet 2)

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Figure 4-16. Pitch Trim Actuator Lubrication (Sheet 1 of 3)

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Figure 4-16. Pitch Trim Actuator Lubrication (Sheet 2)

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Figure 4-16. Pitch Trim Actuator Lubrication (Sheet 3)

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Figure 4-17. Elevator Structure Lubrication

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Figure 4-18. Rudder Structure Lubrication

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Figure 4-19. Aft Cargo Side Door Lubrication (AF69-0024 and AF83-1285 and Up)

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Figure 4-20. Aft Cargo Center Door Lubrication (AF69-0024 and AF83-1285 and Up) (Sheet 1 of 2)

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Figure 4-20. Aft Cargo Center Door Lubrication (AF69-0024 and AF83-1285 and Up) (Sheet 2)

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Figure 4-21. Aft Cargo Center Doors Lubrication (AF68-0213 and AF68-0216) (Sheet 1 of 4)

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Figure 4-21. Aft Cargo Center Doors Lubrication (AF68-0213 and AF68-0216) (Sheet 2)

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Figure 4-21. Aft Cargo Center Doors Lubrication (AF68-0213 and AF68-0216) (Sheet 3)

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Figure 4-21. Aft Cargo Center Doors Lubrication (AF68-0213 and AF68-0216) (Sheet 4)

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Figure 4-22. Movable Bulkhead Lubrication (AF68-0213 and AF68-0216) (Sheet 1 of 3)

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Figure 4-22. Movable Bulkhead Lubrication (AF68-0213 and AF68-0216) (Sheet 2)

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Figure 4-22. Movable Bulkhead Lubrication (AF68-0213 and AF68-0216) (Sheet 3)

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Figure 4-23. Retractable Rollers Lubrication (AF68-0213 and AF68-0216)

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Figure 4-24. Aft Ramp Lubrication

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Figure 4-25. Troop Compartment Stair Ladder Lubrication (AF69-0024 and AF83-1285 and Up)

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Figure 4-26. No. 5 Service Door Lubrication

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Figure 4-27. No. 6 Service Door Lubrication (AF69-0024 and AF83-1285 and Up)

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Figure 4-28. No. 7 Service Door Lubrication

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CHAPTER 5

CRASH HANDLING

5.1 PREPARATION.

5.1.1 General. When a crash damaged or disabled C-5 is blocking a runway, clearing the runway is of primary impor-tance. It is also important that the airplane be removed from the runway with as little additional damage as possible.

Preparation for removal should include the writing of a detailed plan that takes into consideration factors such as safety, extent of damage, repair allowances, availability of support equipment, attitude of the airplane, condition of supporting terrain, and distance to the repair site.

5.1.2 Safety Precautions. Crash handling will involve many operations which are hazardous. Safety precautions must be consistent with the removal procedure and be an integral part of the removal plan. These precautions must be followed to avoid injury to personnel or loss of life. Certain general precautions will be applicable to each crash damage situation and certain precautions will be applicable to each speci c operation. Typical general precautions are: static grounding, defueling and purging, removing batteries, removing oxygen containers, and washing away spilled fuel or hydraulic uid.

5.1.3 Removal of Cargo Equipment. The crash handling procedures that follow are based on an airplane gross weight of 350,000 pounds or less. Each incident will have to be analyzed to determine the necessity of being at this gross weight for removal. Generally it is very desirable to be at a low gross weight so as to minimize the likelihood of further airplane damage and to have larger safety margins for support equipment.

5.1.4 Removal from Crash Site.

Removal of major airplane components can cause dangerous shifts in airplane center of gravity. Compensate by adding ballast as required. Failure to comply could result in damage to the airplane, injury to personnel, or loss of life.

Any crash incident will require damage assessment and planning dictated by the circumstances. The airplane should be inspected for damage to primary structure and determinations made as to whether or not the structural integrity has been affected. If the landing gear is capable of supporting the airplane, the normal towing procedures should be followed. If the landing gear cannot be extended or is damaged so as to be incapable of functioning, emergency procedures must be employed. Refer to Paragraph 5.2. If it is necessary to remove certain airplane components to reduce weight, decrease dimensions, or prevent damage, consideration must be given to their weight and effect on airplane center of gravity. Refer to Chapter 1 for weights of major components and for center of gravity limitations.

5.1.5 Protecting Crash Damaged Airplanes from Corrosion. Coat exposed bearing surfaces with Speci cation MIL- PRF-23872 grease. Cover all tears, punctures, and openings left by component removal to prevent entry of water and foreign material. Tape loose ends of electrical connectors. Plug and wrap open ends of all ducts and tubing. Install covers on engines, ram air turbine inlets, and APU exhaust openings.

5.2 EMERGENCY REMOVAL PROCEDURES.

5.2.1 Emergency Removal Procedures, Nose Gear Up, Main Gear Normal.

a. Inspect for damage.

b. Establish airplane gross weight and center of gravity to be in safe limits for jacking as shown in Chapter 2.

c. Raise the nose of the airplane using one of the following methods:

5-1

(1) Raise the nose for positioning on B-4A jacks by kneeling the aft main bogies. Refer to Chapter 2 for jacking procedure with nose gear failed in kneeled or collapsed position.

(2) If the aft main bogies cannot be kneeled or if it is not safe or feasible to do so, then the nose of the airplane may be raised by using a special jacking procedure. (See Figure 5-1.)

Do not manifold jacks together that are different sizes or types. Failure to comply will result in unequal loading and unequal ram travel, possibly damaging airplane structure.

NOTE

If portable jacks of the size and type speci ed are not available, 70-ton portable jacks, Federal Stock No. 4910- 640-4113, may be used as substitutes provided they are manifolded in pairs similar to the method shown in Figure 5-1. For jack operation and service instructions, refer to TO 35A2-2-33-1.

(a) Manifold two F-1 or two F-2 type or equivalent axle jacks together by interconnecting the pressure lines.

(See Figure 5-1.) The interconnecting hose and tee tting should be rated for 5,000 PSI operating pressure to ensure safe operation at the jack rated operating pressure.

(b) Position the jacks on a rm, level bearing surface of sufficient area to prevent sinking or settling of the jack lift. It will be necessary to use cribbing to obtain the desired vertical position.

(c) Attach the 4F33138 jacking adapter to the airplane in accordance with procedures in Chapter 2.

(d) Establish communications between all jacking personnel and maintain communications at all times during jacking procedures.

These axle jacks do not have safety locks. Personnel must not be under the raised portion of the airplane when axle jacks are the only means of support. Failure to comply could result in injury to personnel or loss of life.

NOTE

With axle jacks manifolded as shown in Figure 5-1, both jack pumps should be operated simultaneously to maintain an approximate equal uid level in the reservoirs.

(e) Jack the nose of the airplane using as much of the jack ram travel as possible.

(f) Working from each side of the airplane, slide shoring under nose wheels.

NOTE

Both jack release valves should be operated simultaneously or in small alternate increments to avoid over owing a reservoir.

(g) Lower jacks slowly until nose of airplane is supported by the retracted nose wheels.

(h) With jack ramps collapsed, add cribbing to build up jack base until collapsed ram is repositioned under the jacking adapter. Repeat Step c(2)(e) through Step c(2)(h) until nose is high enough to position B-4A jacks under the forward fuselage jack points.

(i) Position B-4A forward fuselage jacks under jacking adapter and using procedures speci ed in Chapter 2, jack the airplane nose high enough for nose gear extension. (Minimum height from ground to centerline of NLG trunnion is 86 inches.)

5-2

(j) Lower the nose gear and install ground safety downlocks.

(k) Inspect for damage and if nose gear is capable of supporting nose of airplane, tow airplane according to procedures in Chapter 2.

Do not manifold jacks together that are different sizes or types. Failure to comply will result in unequal loading and unequal ram travel, possibly damaging airplane structure.

NOTE

If portable jacks of the size and type speci ed are not available, 70-ton portable jacks, Federal Stock No. 4910- 640-4113, may be used as substitutes provided they are manifolded in pairs similar to the method shown in Figure 5-1. For jack operation and service instructions, refer to TO 35A2-2-33-1.

d. Support the nose of the airplane as follows if the nose gear cannot be lowered or is damaged.

(1) Open or remove NLG doors to clear retracted nose gear.

NOTE

The nose of the airplane can be supported by the retracted gear through the unlock truss.

(2) Remove kneeling door to get added clearance. Refer to TO 1C-5M-2-10, Chapter 6, for kneeling door removal procedures.

NOTE

Nose gear reaction will be approximately 40,000 pounds for an airplane gross weight of 350,000 pounds.

(3) Use a low bed trailer with converter dolly as shown in Figure 5-2. Trailer and converted dolly must be used in proper combination to obtain the support capacity required. Equipment shown in Figure 5-2 is a 40-ton minimum capacity low bed, 6-wheel semitrailer using a 9-ton minimum capacity converter dolly.

(4) Position the converter dolly to the trailer in a straight ahead position so that there will be no turning required at the fth wheel. Converter dollies rated at 9 tons minimum capacity will carry the weight provided the longitudi-nal center of the load is between 55 and 75 inches forward of the center of the trailer axles.

(5) Build up support at the aft edge of trailer bed space for the center two wheels of the NLG. This support must offer a stable platform, therefore, individual timbers must be attached together to prevent slippage. In building up this support, allow clearance between the NLG fairing and the trailer gooseneck to compensate for de ections.

NOTE

The wheel spacer between the outer wheels on each side is a thin walled tube and is not capable of withstanding the high radial loads encountered in tiedown. There probably will be damage to the wheel spacers as they collapse onto the axle. They must be inspected and replaced as required.

(6) Lower the jacks until the nose of the airplane is supported by the trailer. Fasten the trailer and airplane securely together. (See Figure 5-2.) Chains and tiedown devices normally used for cargo tiedown may be used. Pad the chains sufficiently to prevent damage to airplane structure and components. The tying together of the airplane and trailer must be such that there is no relative motion during towing.

e. Tow airplane forward or aft using the main gear towing arrangement shown in Figure 5-3. Follow the procedure and observe the safety precautions in Chapter 2. Some steering is possible by forcing the trailer tires to slide laterally as the airplane is towed forward. If the airplane must be moved to a repair site requiring sharper turning, then each signi cant change in direction will necessitate repositioning the trailer relative to the airplane to effect a turn.

5-3

f. An alternate method of moving the airplane is as follows:

(1) Raise the nose of the airplane using one of the previously described methods.

(2) Remove NLG doors and kneeling door and strip away xed fairing to expose the retracted NLG wheels.

(3) Lower the nose of the airplane to rest on the retracted wheels.

(4) Tow the airplane straight forward or aft using main gear towing procedures in accordance with Chapter 2.

5.2.2 Emergency Removal Procedures, All Main Gear Up, Nose Gear Normal.

a. Inspect for damage.

b. Establish that airplane gross weight is at minimum obtainable and that center of gravity is within safe limits for jacking. Refer to Chapter 2.

c. In winds exceeding the limits for fuselage jacking it may be necessary to stabilize the airplane laterally prior to jacking. As an example, a side wind of 40 knots will produce a side load of roughly 9,000 pounds on the airplane.

Stabilize the airplane as shown in Figure 5-4 using steel cable, cable adjuster, or winch, and ground anchors or pilings on both sides of the airplane. (A 1/2-inch diameter MIL-W-1511 cable is capable of 22,800 pounds.) Attach cables at the FS 1523 frame and the NLG trunnion frame using padding to prevent damage. Tension cables to prevent lateral movement of the airplane and monitor cable tension during jacking.

d. Raise airplane using one of the following methods.

(1) The preferred method of jacking the airplane is using the aft four fuselage jack pads as follows:

(a) Fabricate support blocks as shown in Figure 5-4.

Do not manifold jacks together that are different sizes or types. Failure to comply will result in unequal loading and unequal ram travel, possibly damaging airplane structure.

NOTE

If portable jacks of the size and type speci ed are not available, 70-ton portable jacks, National Stock No.

4910-00-640-4113, may be used as substitutes provided they are manifolded in pairs similar to the method shown in Figure 5-5. For jack operation and service instructions, refer to TO 35A2-2-33-1.

(b) Manifold two type MD-1 75-ton capacity axle jacks together by interconnecting the pressure lines. (See Figure 5-5.) The interconnecting hose and tee ttings should be rated for 5,075 PSI operating pressure to insure safe operation at the jack rated operating pressure.

(c) Position the jacks on a rm, level bearing surface of sufficient area to prevent sinking or settling of the jack lift. The left side jacks are manifolded together and the right side jacks are manifolded together. (See Figure 5-5.)

(d) Attach the jacking adapters at FS 1964 and remove the jack pad access door at FS 1106. Refer to Chapter 2.

(e) Establish communications between all jacking personnel and maintain communications at all times during the jacking procedure.

5-4

NOTE

With all jacks manifolded as shown in Figure 5-5, both jack pumps should be operated simultaneously to maintain an approximately equal level in the reservoirs.

(f) Position the manifolded jacks under the jack pads using cribbing to obtain the required vertical position. (See Figure 5-4.)

(g) Jack the airplane using as much of the jack ram travel as possible. (Maximum ram travel is 12-3/4 inches.)

Turn the ram lock rings as the ram moves up to maintain a 1/4-inch maximum space between the rings and cylinders.

(h) If the MLG doors are closed, gain access to the aft bogie area on each side by cutting through the MLG door at the aft outboard corner.

(i) Remove the attachments retaining the aft MLG door (TO 1C-5M-2-10, Chapter 6), and slide the door outward and away from the airplane.

The landing gear yoke must be in place to provide stability to the FS 1603 trunnion frame while the frame is being used to support the airplane. Failure to comply could result in collapse of the frame causing additional damage to the airplane, injury to personnel, or loss of life.

(j) Position the shoring and support block under the trunnion frame at FS 1603 (Figure 5-4) and lower the jacks.

If the FS 1603 is damaged, the trunnion frame at FS 1523 may be used.

(k) Repeat Step d(1)(f), Step d(1)(g), and Step d(1)(j) until airplane is high enough to be supported by the 60-ton Hydraulic Tripod Jacks (4S90014). Refer to Chapter 2 for use of fuselage tripod jacks.

(2) Raise the airplane using air lifting bags under the wings. Figure 5-6 shows the general arrangement of the bags.

Use air lifting bags rated for at least 3.5 pounds per square inch in ation pressure with a cross section no greater than 90 inches by 80 inches.

Determine the safe center of gravity limits using the geometric pattern of the air lifting bags under the wing rather than the fuselage jack points. Failure to comply could result in damage to the airplane, injury to personnel, or loss of life due to an unstable lifting condition.

(a) Establish the center of gravity within safe limits.

Air lifting bags must be arranged between the front beam (15 percent chord) and the rear beam (63 percent chord) in such a way to minimize overlap of the front and rear beams. Failure to comply could result in damage to the wing.

(b) Position shoring under the wings and build up shoring to within approximately 1 foot of the lower surface.

(c) Position air lifting bags between shoring and wing using rubber sheeting on each side of the air lifting bag for protection and to prevent slippage.

(d) Manifold airbags such that they can be in ated and de ated in pairs.

5-5

NOTE

Any 14 of the 16 airlifting bags per side will lift the airplane at the pressures indicated in Figure 5-6. The two additional air lifting bags permit de ation -reshoring - rein ation cycling to attain greater height.

e. Raise the fuselage until the distance from the centerline of the MLG trunnion to the ground is 112 inches. This is the clearance required for gear extension.

f. Extend gear and inspect for damage. If the gear is capable of supporting the airplane, lower airplane onto gear and tow airplane in accordance with procedures in Chapter 2.

g. Support the airplane as follows if the gear cannot be lowered or is damaged. (See Figure 5-7.)

(1) Remove MLG doors. Refer to TTO 1C-5M-2-10, Chapter 6, for door removal procedures.

(2) Remove MLG fairing section from FS 1428 through FS 1478. Refer to TO 1C-5M-3, Chapter 5, for removal instructions.

The landing gear yoke must be in place to provide stability to the FS 1603 trunnion frame while the frame is being used to support the airplane. Failure to comply could result in additional damage to the airplane, injury to personnel, or loss of life.

(3) To provide a minimum support capability of 150,000 pounds per side, position 2 semitrailers/converter dolly combination side by side under each trunnion frame as shown in Figure 5-7. Trailer and converter dolly must be used in combination to obtain the support required. Trailer shown is a 40-ton minimum capacity low bed, 6-wheel semitrailer. Converter dolly is a 9-ton minimum capacity model.

(4) Position the converter dolly to trailer in a straight ahead position so that there will be no turning required at the fth wheel. Converter dollies rated at 9 tons minimum capacity will carry the weight provided the longitudinal center of the load is between 55 and 75 inches forward of the center of the trailer axles.

(5) Position trailers under airplane as shown in Figure 5-7. The trailers must be xed relative to each other so that a stable platform is provided.

(6) Build up the support at the aft edge of the load space using the fabricated support block as shown in Figure 5-7.

Individual timbers must be attached together to prevent slippage. Fabrication of I-beam grid(s) should be as shown in Figure 5-7, view C and view D. The beams should be 8 inches minimum standard structural steel. All gear up recovery will require 3 each 42-foot beams and 16 each 3-foot beams. Support under 1 main gear will require 3 each 16-foot beams and 8 each 3-foot beams.

(7) Lower jacks until the airplane is supported by the trailers. Fasten the trailer and airplane securely together. Chains and tiedown devices normally used for cargo tiedown may be used. Provide a drag strap as a primary load path between the trailer and the airplane for towing loads. (See Figure 5-7.) Pad chains sufficiently to prevent damage to the airplane structure and components. The tying together of the airplane and trailers must be such that there is no relative motion during towing.

Constantly monitor the condition of the tiedown chains to ensure that trailer and airplane remain securely tied.

Failure to comply could result in damage to the airplane.

h. Tow airplane forward or aft using nose gear towing or the arrangement shown in Figure 5-8. Turning will cause the trailer tires to slide laterally, therefore, turns should be at as large a turning radius as practical.

5.2.3 Emergency Removal Procedures, Main Gear Up on One Side, Nose Gear Normal.

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a. Inspect for damage.

b. Establish that airplane gross weight is at minimum obtainable and that center of gravity is within safe limits for jacking. Refer to Chapter 2.

c. If possible, kneel the normal gear per instructions in TO 1C-5M-2-10, Chapter 6.

d. Obtain an 8,000-pound fuel unbalance in the outboard main or auxiliary tanks with the heavy wing on side opposite the failed gear.

e. Raise the airplane using one of the following methods.

(1) Lift the low side of the airplane using special jacking procedure as follows:

(a) Use the two fuselage jack points on the failed gear side. Refer to Paragraph 5.2.2 for instructions on manifolding of jacks, positioning of cribbing, and preparation for jacking.

(b) Jack the airplane so that the aft MLG door clears the ground.

(c) Remove aft MLG door according to Paragraph 5.2.2.

(d) Position shoring and support block under the FS 1603 trunnion frame (Figure 5-5) and lower jacks. If the FS 1603 frame is damaged, the trunnion frame at FS 1523 may be used.

(e) Using increments of 4 to 6 inches, alternately jack and shore according to instructions in Paragraph 5.2.2 until the airplane is level.

(f) Using the four fuselage jack points and manifolded axle jacks (Figure 5-4 and Figure 5-5) raise the fuselage high enough to be supported by the 60-ton hydraulic tripod jacks (4S90014). Refer to Chapter 2 for use of fuselage tripod jacks.

(2) Lift the low side of the airplane using air lifting bags under the low wing. (See Figure 5-6.) Refer to Paragraph

5.2.2 for procedures on use of air lifting bags.

(a) Level the airplane using air lifting bags under the low wing.

(b) If airplane is high enough, transfer support to the 60-ton hydraulic tripod jacks (4S90014). Refer to Chapter 2 for use of fuselage tripod jacks.

(c) If airplane is not high enough to accommodate the tripod jacks, raise airplane using air lifting bags under both wings until the fuselage jacks can be used.

f. Open or remove all MLG doors and inspect for damage. Raise the fuselage until the distance from the center line of MLG trunnion to the ground is at least 112 inches. This will provide clearance for gear extension.

g. Extend gear and inspect for damage. If the gear is capable of supporting the airplane, lower airplane onto gear and tow according to procedures in Chapter 2.

NOTE

The airplane may be towed without special support if one forward and one opposite aft bogie is normal or if both forward bogies are normal and the nose is ballasted to move the center of gravity forward of the forward bogies.

h. Support the airplane as follows if the gear cannot be lowered or if the gear is not capable of supporting the airplane.

(1) Unkneel the normal gear if it was previously kneeled.

(2) Remove forward MLG door. Refer to TO 1C-5M-2-10, Chapter 6.

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(3) Remove MLG fairing section between FS 1428 and FS 1478. Refer to TO 1C-5M-3, Chapter 5.

(4) Position two trailers under the airplane as shown in Figure 5-7. Refer to Paragraph 5.2.2 for information on support.

Constantly monitor the condition of the tiedown chains to ensure that trailer and airplane remain securely tied.

Failure to comply could result in damage to the airplane.

NOTE

• It is permissible for the center line of trunnion frame on the damaged side to be as much as 10 inches higher than the undamaged side when the airplane is supported for towing.

• When towing with a combination of normal bogies and semitrailers, a difference in support stiffness will be noted which could cause erratic towing response and handling characteristics.

i. Tow airplane forward or aft using nose gear towing or the appropriate arrangement shown in Figure 5-8. Turning will cause the trailer tires to slide laterally, therefore, turns should be as large a radius as practical.

5.2.4 Emergency Removal Procedures, All Gear Up. Raise, support, and tow the airplane using the appropriate combination of procedures given in Paragraph 5.2.1 and Paragraph 5.2.2.

5.3 EXTENT OF DAMAGE DUE TO LANDING GEAR FAILURE.

Damage to the airplane can result if the landing gear is collapsed when the airplane is at rest or is being towed, or if the landing gear is overloaded when the airplane is landed.

5.3.1 Tire Blowout. Inspect the airframe skin, landing gear doors, and exposed wheel well structure in the immediate vicinity of the blown tire for damage caused by strips and pieces of the tire hitting the airframe.

5.3.2 Nose Gear Up Landing. (See Figure 5-9.) A landing with the nose landing gear in the retracted position will result in damage to the forward portion of the underside of the fuselage.

5.3.3 Main Gear Up on One Side Landing. (See FO-2.) A landing with the main gear in the retracted position on one side will result in damage to the fuselage, outboard nacelle, and wing tip on the side with the retracted gear.

5.3.4 All Main Gear Up Landing. (See FO-3.) A landing with all the main gear in the retracted position will result in damage to the underside of the fuselage, the outboard nacelle, and wing tips.

5.3.5 All Gear Up Landing. (See FO-4.) A landing with all of the landing gear in the retracted position will result in damage to the underside of the fuselage, the outboard nacelles, and the wing tips.

5.4 INSPECTION.

Examine the entire airplane thoroughly and inspect the damaged area in detail. Look for hidden damage and distortion to primary structure and functional systems. Since the landing impact may have caused excessive loads in certain structural members and deformations which might not be apparent to visual inspection, alignment should be checked. Examine all landing gear and support structure for damage, alignment, and functional operation. Use the inspection methods in Chapter 1 as necessary to check structure.

5-8

Figure 5-1. Jacking with Nose Landing Gear Failed (Sheet 1 of 3)

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Figure 5-1. Jacking with Nose Landing Gear Failed (Sheet 2)

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Figure 5-1. Jacking with Nose Landing Gear Failed (Sheet 3)

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Figure 5-2. Forward Fuselage Support with Nose Landing Gear Failed (Sheet 1 of 2)

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Figure 5-2. Forward Fuselage Support with Nose Landing Gear Failed (Sheet 2)

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Figure 5-3. Towing with Nose Landing Gear Failed (Sheet 1 of 2)

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Figure 5-3. Towing with Nose Landing Gear Failed (Sheet 2)

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Figure 5-4. Jacking with Main Landing Gear Failed (Sheet 1 of 2)

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Figure 5-4. Jacking with Main Landing Gear Failed (Sheet 2)

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Figure 5-5. Manifolding 75-Ton Axle Jacks

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Figure 5-6. Lifting with Air Bags, Main Landing Gear Failed

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Figure 5-7. Center Fuselage Support with Main Landing Gear Failed (Sheet 1 of 2)

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Figure 5-7. Center Fuselage Support with Main Landing Gear Failed (Sheet 2)

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Figure 5-8. Towing with Main Landing Gear Failed (Sheet 1 of 2)

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Figure 5-8. Towing with Main Landing Gear Failed (Sheet 2)

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Figure 5-9. Nose Gear Up Landing

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INDEX

Paragraph, Figure, Subject Table Number

A AN/ALE-47 Safety . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.6 APU Access Panel Opening and Closing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-14 APU Control and System Control Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-23 APU Exhaust Duct Cover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-75 APU Fire Extinguishing System Control Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-6 APU Ground Handling Cart. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-49 APU Inlet Duct Protective Plug . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-74 APU Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 3-28 ATM Accumulator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 3-44 ATM Accumulator Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.20

Precharging the ATM Accumulators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.20.1 ATM Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 3-27 Aft Cargo Center Door Hoisting Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-30 Aft Cargo Center Door Lubrication (AF69-0024 and AF83-1285 and Up). . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 4-20 Aft Cargo Center Doors Lubrication (AF68-0213 and AF68-0216) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 4-21 Aft Cargo Side Door Cradle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-48 Aft Cargo Side Door Lubrication (AF69-0024 and AF83-1285 and Up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 4-19 Aft Ramp Lubrication. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 4-24 Aileron Counterweight Sling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-32 Aileron Ground Safety Lock Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-78 Aileron Servo Lubrication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 4-12 Air Conditioning Air ow Selector Chart . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-34 Airplane Chock Locations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-16 Airplane Dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-1 Airplane Exterior Walkways and No-Step Areas . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-5 Airplane Grounding Provisions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-18 Airplane Lubrication Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 4-1 Airplane Maintenance and Ground Handling Markings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-6 Airplane Recovery and Launch Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.12

Airplane Launch Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.12.2 Airplane Recovery Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.12.1

Airplane Stations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-3 Airplane Tiedown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-17 Airplane Towing Capability. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . T 2-1 All Gear Up Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FO-4 All Main Gear Up Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FO-3 Allowable CG Limits for Fuselage Jacking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-21 Anti-Icing System Panels (for Switch Locations) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-22 Anti-Icing, Deicing, and Snow and Frost Removal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4

Anti-Icing, Deicing, and Snow and Frost Removal Procedures. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4.3 General Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4.2 Removal of Deposits. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4.4 Removing Frost . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4.5 Removing Ice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4.6 Safety Precautions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.4.1

Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . T 1-3 Auxiliary Power Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.11

APU Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.11.3 ATM Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.11.1 Draining the APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.11.4 Draining the ATM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.11.2

Index 1

B Battery Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.23

Servicing of Airplane Battery and APU Battery . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.23.1 Buffet-Lavatory Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 3-40

C Cargo Winch (Part No. 4F90000-103B) (AF68-0213, AF68-0216, and AF69-0024) . . . . . . . . . . . . . . . . . . . . . . F 3-46 Cargo Winch (Part No. 4F90000-105A) (AF68-0213, AF68-0216, and AF69-0024) . . . . . . . . . . . . . . . . . . . . . . F 3-47 Cargo Winch (Part No. 4PF90020-101A) (AF83-1285 and Up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 3-48 Cargo Winch Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.22

Alternate Cargo Winch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.22.1 Cargo Winch Lubrication (PN 4F90000-103B) (AF68-0213, AF68-0216, and AF69-0024) . . . . . . . . . . . . . . . . 3.22.2 Cargo Winch Lubrication (Part No. 4F90000-105A) (AF68-0213, AF68-0216, and AF69-0024) . . . . . . . . . . . . 3.22.3 Cargo Winch Lubrication (Part No. 4F90020-101A) (AF83-1285 and Up) . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.22.4

Caution Light and Emergency Exit Light Switch Locations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-25 Center Fuselage Support with Main Landing Gear Failed. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 5-7 Center Wing Root Area Maintenance Platform . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-67 Circuit Breaker Locations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-21 Concurrent Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3

CSS Duties Prior to Airplane Arrival . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3.5 CSS Duties upon Airplane Arrival. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3.6 Concurrent Servicing Procedures. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3.7 Concurrent Servicing Terms and Abbreviations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3.1 Fuel Servicing Safety Zone . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3.3 Location of Personnel During Concurrent Servicing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3.2 Refueling Team . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.3.4

Condensate Drain Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 3-8 Connecting SCM External Electrical Power (AF68-0213 and AF68-0216). . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-29 Core Cowl Dolly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-63 Cradle Sling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-38 Crew Compartment Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.14

Cleaning and Disinfecting the Crew Galley Potable Water System (AF68-0213, AF68-0216, and AF69-0024). . . 3.14.5 Crew Galley Servicing (AF68-0213, AF68-0216, and AF69-0024) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.14.1 Crew Galley Servicing (AF83-1285 and Up). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.14.4 Crew Lavatory Cold Weather Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.14.9 Crew Lavatory Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.14.6 Crew Lavatory Waste Servicing (AF68-0213, AF68-0216, and AF69-0024) . . . . . . . . . . . . . . . . . . . . . . . . . . 3.14.7 Crew Lavatory Waste Servicing (AF83-1285 and Up). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.14.8 Crew Lavatory Water Drain Servicing (AF68-0213, AF68-0216, and AF69-0024) . . . . . . . . . . . . . . . . . . . . . 3.14.12 Crew Lavatory Water Fill Servicing (AF68-0213, AF68-0216, and AF69-0024) . . . . . . . . . . . . . . . . . . . . . . 3.14.10 Crew Lavatory Water Fill Servicing (AF83-1285 and Up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.14.11 Draining the Galley Potable Water Tanks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.14.3 Filling the Galley Potable Water Tanks. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.14.2

Crew Door Accumulator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 3-42 Crew Door Accumulator Servicing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.18

Precharging the Crew Door Accumulator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.18.1 Crew Entry Door Lubrication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 4-5 Crew Galley and Lavatory Water Fill Servicing (AF68-0213, AF68-0216, and AF69-0024) . . . . . . . . . . . . . . . . . F 3-32 Crew Galley and Lavatory Water Tank Valves (AF68-0213, AF68-0216, and AF69-0024) . . . . . . . . . . . . . . . . . . F 3-33 Crew Lavatory Waste Servicing (AF68-0213, AF68-0216, and AF69-0024). . . . . . . . . . . . . . . . . . . . . . . . . . . . F 3-34 Crew Lavatory Waste Servicing (AF83-1285 and Up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 3-35

TO 1C-5M-2-1

INDEX - CONTINUED

Paragraph, Figure, Subject Table Number

Index 2

D Danger Areas . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-4 Display Defaults . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-27

E Elevator Servo Lubrication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 4-15 Elevator Structure Lubrication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 4-17 Emergency Entrances and Exits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FO-1 Emergency Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-2 Emergency Removal Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.2

Emergency Removal Procedures, All Gear Up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.2.4 Emergency Removal Procedures, All Main Gear Up, Nose Gear Normal. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.2.2 Emergency Removal Procedures, Main Gear Up on One Side, Nose Gear Normal . . . . . . . . . . . . . . . . . . . . . . 5.2.3 Emergency Removal Procedures, Nose Gear Up, Main Gear Normal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.2.1

Empennage External Access Provisions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-9 Empennage Internal Access Provisions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-13 Engine Air-Truck Transport Base . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-66 Engine Cradle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-64 Engine Emergency Shutoff Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-5 Engine Maintenance Platform . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-56 Engine Maintenance Tie Off Point at Pylon Quadrapod Truss . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-17 Engine Oil Tank Servicing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 3-24 Engine Protective Covers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-70 Engine Servicing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.9

Engine Oil Tank Quantity Check . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.9.1 Engine Starter Magnetic Drain Plug Inspection and Starter Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.9.3 Gravity Fill Engine Oil Tank Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.9.2

Engine Starter Magnetic Drain Plug Inspection and Starter Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 3-25 Escape Slide Reservoir . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 3-41 Escape Slide Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.17

Precharging the Escape Slide Reservoirs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.17.1 Extent of Damage Due to Landing Gear Failure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.3

All Gear Up Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.3.5 All Main Gear Up Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.3.4 Main Gear Up on One Side Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.3.3 Nose Gear Up Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.3.2 Tire Blowout . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.3.1

External Pneumatic Receptacle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-30 External Power Receptacles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 1-20 Extinguishers and Local Fire Access Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F 2-4 Extinguishing Ground Fires . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1

Access to Local Fires . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.5 Emergency Entrances and Exits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.6 Emergency Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.3 Engine and APU Fire Extinguishing System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.7 FE1301 Fire Suppression (AF68-0213, AF68-0216, and AF69-0024) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.12 Fire Extinguishing Agents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.8 Fire Suppression System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.11 Fire Suppression System (FSS). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.2 General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.1 Highly Flammable Areas . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.4 Portable Fire Extinguishers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.9 Portable Fire ghter Assemblies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1.10

Extreme Climatic and Environmental Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.5 ATM, Power Transfer Units, Engine Pumps, and APU. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .