1C-5M-2-1_1-100.pdf

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OPERATIONAL SUPPLEMENT

TO 1C-5M-2-1S-2

OPERATIONAL SUPPLEMENT

TECHNICAL MANUAL

MAINTENANCE

ORGANIZATIONAL LEVEL

GROUND HANDLING AND SERVICING

USAF SERIES

C-5M AIRCRAFT

(ATOS)

This publication supplements TO 1C-5M-2-1, dated 20 April 2017. Reference to this supplement will be made on the title page of the basic manual by personnel responsible for maintaining the publication in current status.

COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS SUPPLEMENT TO THE ATTENTION OF ALL AFFECTED AF PERSONNEL

DISTRIBUTION STATEMENT D - Distribution authorized to the Department of Defense and U.S. DoD contractors only (Administrative or Operational Use) (10 September 2009). Other requests for this document shall be referred to AFLCMC/WLSA, 235 Byron St., Suite 19A, Robins AFB, GA 31098-1670. Questions concerning technical content shall be referred to AFLCMC/WLSE, 235 Byron St., Suite 19A, Robins

AFB, GA 31098-1670.

WARNING - This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751, et seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401 et seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

HANDLING AND DESTRUCTION NOTICE - Comply with distribution statement and destroy by any method that will prevent disclosure of contents or reconstruction of the document.

Published Under Authority of the Secretary of the Air Force

19 MAY 2017

TO 1C-5M-2-1S-2

1. Page xvi, LIST OF TIME COMPLIANCE TECHNICAL ORDERS of the basic manual is amended, as a result of TO 35D3-3-84-503, to add the following:

TO No. Date Title

35D3-3-84-503 29 July 2016 Modification of C-5M Engine Handling System from Part Number A5441-20FRK to Final Configuration MA9441-20FJR

2. Page 2-55, paragraph 2.7.13 of the basic manual is amended to change the bootstrap beam and saddle adapter set from Part Number AGSE-B015-G02 to Part Number AGSE-B015-G03.

3. Page 2-55, paragraph 2.7.13 of the basic manual is amended, as a result of TO 35D3-3-84-503, to delete the phrase ‘‘(manual or pneumatic)’’ from the fourth and sixth sentences.

4. Page 2-55, paragraph 2.7.13 of the basic manual is amended, as a result of TO 35D3-3-84-503, to add a new paragraph 2.7.13A to read as follows:

2.7.13A Engine Handling System. The engine handling system (P/N MA9441-20FJR) is designed to pro-vide lifting and lowering of an F138 Engine during engine removal and installation. The engine handling system consists of two 6-ton manual lever hoists, two 3-ton manual lever hoists, four dynamometers, and a reusable storage/shipping container. The engine handling system is used in combination with the bootstrap beam and saddle adapter set which attaches to the engine pylon. Two dynamometers attach to the forward bootstrap beam. The remaining two dynamometers attach to eyelets on the aft bootstrap beam cable. The two 6-ton hoists are atached to the dynamometers on the forward bootstrap beam. The two 3-ton hoists are attached to the dynamometers on the aft bootstrap beam. See TO 1C-5M-2-4JG-1-3, Chapter 2.

THE END

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OPERATIONAL SUPPLEMENT

TO 1C-5M-2-1S-1

OPERATIONAL SUPPLEMENT

TECHNICAL MANUAL

MAINTENANCE

ORGANIZATIONAL LEVEL

GROUND HANDLING AND SERVICING

USAF SERIES

C-5M AIRCRAFT

(ATOS)

This supplement supersedes Operational Supplement TO 1C-5M-2-1S-14, dated 20 November 2015.

This publication supplements TO 1C-5M-2-1, dated 20 April 2017. Reference to this supplement will be made on the title page of the basic manual by personnel responsible for maintaining the publication in current status.

COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS SUPPLEMENT TO THE ATTENTION OF ALL AFFECTED AF PERSONNEL

DISTRIBUTION STATEMENT D - Distribution authorized to the Department of Defense and U.S. DoD contractors only (Administrative or Operational Use) (10 September 2009). Other requests for this document shall be referred to AFLCMC/WLSA, 235 Byron St., Suite 19A, Robins AFB, GA 31098-1670. Questions concerning technical content shall be referred to AFLCMC/WLSE, 235 Byron St., Suite 19A, Robins

AFB, GA 31098-1670.

WARNING - This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751, et seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401 et seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

HANDLING AND DESTRUCTION NOTICE - Comply with distribution statement and destroy by any method that will prevent disclosure of contents or reconstruction of the document.

Published Under Authority of the Secretary of the Air Force

3 MAY 2017

1. Page 1-125, Figure 1-21, Circuit Breaker Locations (Sheet 6) of the basic manual is amended, as a result of TO 1C-5M-544, to be replaced with page 10 of this supplement.

2. Page 1-132, Figure 1-21, Circuit Breaker Locations (Sheet 13) of the basic manual is amended, as a result of TO 1C-5M-544, to be replaced with page 11 of this supplement.

3. Page 3-104, Paragraph 3.14.4 and Paragraph 3.14.5 of the basic manual are amended, as a result of TO 1C-5M-544, to be deleted in their entirety.

4. Page 3-105, Paragraph 3.14.6, Crew Lavatory Servicing of the basic manual is amended, as a result of TO 1C-5M-544, to read as follows:

TO 1C-5M-2-1S-1

3.14.6 Lavatory Servicing. (See Figure 3-34.) Crew lavatory is installed on the right side of the airplane aft of relief crew seats and forward of the galley. Troop compartment lavatory, consisting of two separate toilet units, is installed on forward right end of troop compartment (except on AF68-0213 and AF68-0216).

A service truck capable of supplying fresh water is required to fill the water storage tank behind the crew galley between FS 844 and FS 864. Both relief crew compartment and troop compartment lavatories are serviced from a service panel located at FS 815.

5. Page 3-105, Paragraph 3.14.7, Crew Lavatory Waste Servicing (AF68-0213, AF68-0216, and AF69- 0024) of the basic manual is amended, as a result of TO 1C-5M-544, to read as follows:

3.14.7 Waste Tank Drain Procedure. (See Figure 3-34.) Service the lavatory waste tank as follows:

a. Open the service panel door on bottom of aircraft at FS 815.

b. Open the lever lock cap of the rinse nipple (4).

c. Connect rinse water hose of a Type A/S 32A-8 truck or equivalent to the rinse nipple (4).

d. Open the waste valve (5) cover.

e. Connect the service truck waste service hose to the waste valve (5).

f. Open the internal flapper valve of the waste valve (5) using the PUSH TO OPEN lever (2) on the waste valve (5).

CAUTION

The waste tank drain valve must be open before starting the waste service truck suction pump. Failure to comply could result in damage to airplane.

NOTE

Initial pull force for drain cable handle may be up to 70 pounds during break-in period.

g. Open the waste tank drain valve by the pulling the drain cable handle (6) out from the service panel.

h. Start the waste service truck suction pump.

i. After waste tank and servicing truck waste drain line has been completely drained, stop the waste truck suction pump.

j. Rinse the waste tank by pumping water from the service truck into the rinse line for a minimum of 2 minutes.

k. Stop the flow of rinse water.

l. Start waste service truck suction pump and completely drain the service truck waste line.

CAUTION

The service truck waste suction pump must be off prior to closing ACFT waste tank drain valve. Failure to comply could result in damage to the airplane.

m. Stop the waste truck suction pump after all water has been drained from waste line.

n. Push the drain cable handle (6) fully in to close the waste tank drain valve.

CAUTION

If the airplane is inactive and is to be exposed to freezing temperatures, drain the waste tank as soon as possible after flight termination. Pre-charge waste tank immediately prior to next scheduled flight. Failure to comply could cause serious damage to tank.

o. Pre-charge the waste tank by adding 3 to 5 gallons of rinse water from the service truck.

p. Remove the rinse hose and allow all water to drain from the rinse nipple (4) and close the lever lock cap of the rinse nipple (4).

q. Disconnect the drain line from the waste valve (5).

r. Close the waste valve (5) cover.

s. Rinse the service area with a solution of nine parts water to one part MIL-PRF-87937, Type IV heavy duty cleaner solution, followed by thorough rinsing and drying.

t. Close the service panel door.

6. Page 3-105, following Paragraph 3.14.7, Crew Lavatory Waste Servicing (AF68-0213, AF68-0216, and AF69-0024) of the basic manual is amended, as a result of TO 1C-5M-544, to add new Paragraph 3.14.7A to read as follows:

3.14.7A Waste Tank Drain and Flush Procedure. (See Figure 3-34.) Drain the lavatory waste tank as follows:

a. Open the service panel door on bottom of aircraft at FS 815.

b. Open the lever lock cap of the rinse nipple (4).

c. Connect rinse water hose of a Type A/S 32A-8 truck or equivalent to the rinse nipple (4).

d. Open the waste valve (5) cover.

e. Connect the service truck waste service hose to the waste valve (5).

f. Open the internal flapper valve of the waste valve (5) using the PUSH TO OPEN lever (2) on the waste valve (5).

CAUTION

The waste tank drain valve must be open before starting the waste service truck suction pump. Failure to comply could result in damage to airplane.

NOTE

Initial pull force for drain cable handle may be up to 70 pounds during break-in period.

g. Open the waste tank drain valve by pulling the drain cable handle (6) out from the service panel.

h. Start the waste service truck suction pump.

i. After waste tank and servicing truck waste drain line has been completely drained, stop the waste truck suction pump.

j. Rinse the waste tank by pumping water from the service truck into the rinse line for a minimum of 2 minutes.

k. Stop the flow of rinse water.

l. Start waste service truck suction pump and completely drain the service truck waste line.

CAUTION

The service truck waste suction pump must be off prior to closing ACFT waste tank drain valve. Failure to comply could result in damage to the airplane.

m. Stop the waste truck suction pump after all water has been drained from waste line.

n. Push the drain cable handle (6) fully in to close the waste tank drain valve.

o. Remove the rinse hose and allow all water to drain from the rinse nipple (4) and close the lever lock cap of the rinse nipple (4).

p. Disconnect the drain line from the waste valve (5).

q. Close the waste valve (5) cover.

r. Rinse the service area with a solution of nine parts water to one part MIL-PRF-87937, Type IV heavy duty cleaner solution, followed by thorough rinsing and drying.

s. Close the service panel door.

7. Page 3-105 and page 3-106, Paragraph 3.14.8, Crew Lavatory Waste Servicing (AF83-1285 and Up) of the basic manual is amended, as a result of TO 1C-5M-544, to read as follows:

3.14.8 Lavatory Water Tank Servicing. (See Figure 3-34.) Service the lavatory water tank as follows:

CAUTION

. Use only fresh water to service the lavatory water tank. Do not use water/MiraBowl Q mixture (blue water). Failure to comply could result in damage to equipment.

. If airplane is inactive and and is to be exposed to freezing temperatures, drain the water tank as soon as possible after flight termination. Fill water tank immediately prior to next scheduled flight. Failure to comply could cause serious damage to tank and lines.

NOTE

. The lavatory water tank should be serviced before each flight to ensure a sufficient quantity of water is available for flushing.

. Lavatory water tank capacity is approximately 29 gallons.

a. Ensure electrical power is connected in accordance with paragraph titled Connecting External Electrical Power.

b. Ensure COMP RLY circuit breaker on Flight Engineer Circuit Breaker Panel No. 5 is closed.

c. Open service panel door on bottom of aircraft at FS 815.

d. Open the lever lock cap of the fill/drain nipple (7).

e. Connect rinse water hose line of a Type A/S 32A-8 truck or equivalent to the fill/drain nipple (7).

f. Set the fill/drain switch (3) to the open position and hold until the VALVE OPEN light illuminates.

Release switch.

WARNING

Ensure over flow vent area is clear. Failure to comply may cause injury to personnel and/or damage to equipment.

g. Pump water from the service truck until water begins to flow out of the overflow vent (1) on the lower fuselage of the aircraft, then stop the flow of water from the service truck.

h. Once the water has stopped flowing from the overflow vent (1), set the fill/drain switch (3) to the closed position and hold until the VALVE CLOSED light illuminates. Release switch.

i. Remove the service truck rinse line, allow all residual water to drain, and close the lever lock cap of the fill/drain nipple (7).

j. Ensure VALVE CLOSED light is illuminated. Close service panel door.

k. If electrical power is no longer required, disconnect the electrical power source from the airplane in accordance with paragraph titled Disconnecting External Electrical Power.

8. Page 3-106, Paragraph 3.14.9, Crew Lavatory Cold Weather Servicing of the basic manual is amended, as a result of TO 1C-5M-544, to read as follows:

3.14.9 Water Tank Draining Procedure. (See Figure 3-34.) Drain the water tank as follows:

a. Ensure electrical power is connected in accordance with paragraph titled Connecting External Electrical Power.

b. Ensure COMP RLY circuit breaker on Flight Engineer Circuit Breaker Panel No. 5 is closed.

c. Open the service panel door on bottom of aircraft at FS 815.

NOTE

If draining lavatory water tank onto ramp is undesirable due to poor runoff, freezing weather, etc., use a suitable container, approximately 29 gallons capacity, to catch water.

d. Open the lever lock cap of the fill/drain nipple (7).

e. Set the fill/drain switch (3) to the open position and hold until the VALVE OPEN light illuminates and release switch. Allow water tank to drain.

f. When water stops draining from the fill/drain nipple (7), set the fill/drain switch (3) to the closed position and hold until the VALVE CLOSED light illuminates. Release switch.

g. Close the lever lock cap of the fill/drain nipple (7).

h. Ensure VALVE CLOSED light is illuminated. Close service panel door.

i. If electrical power is no longer required, disconnect the electrical power source from the airplane in accordance with paragraph titled Disconnecting External Electrical Power.

9. Page 3-106, Paragraph 3.14.10, Crew Lavatory Water Fill Servicing (AF68-0213, AF68-0216, and AF69-0024) of the basic manual is amended, as a result of TO 1C-5M-544, to read as follows:

3.14.10 Lavatory Toilet and Waste Tube Cleaning. (See Figure 3-34.1.) Clean the waste tank and waste lines in accordance with the following instructions. Refer to Table 3-9 for materials and equipment required for lavatory cleaning.

NOTE . Soaking allows for efficient vinegar saturation in the waste lines while also allowing the toilet bowl and flush valve disk to be soaked.

. It is very important that crushed ice is used because it will scrape away waste and mineral build-up. The ice should be crushed into approximately 1 inch pieces.

. The last three normal flushes help to clean any leftover residue.

a. Fill each toilet with approximately 1 gallon of vinegar and allow to soak for 5 minutes.

b. Momentarily press the maintenance switch (Figure 3-34.2, 1) and release on each toilet to allow the flush valve to open and release vinegar into waste tubes. Allow to soak for 15 minutes.

c. After allowing 15 minutes for the vinegar to soak in the waste tubes, fill each toilet assembly with approximately 1/2 gallon of crushed ice and 1/2 gallon of vinegar and flush each toilet assembly 3 times.

CAUTION

If freezing temperatures are expected, drain the lavatory water and waste tanks. Failure to comply could result in damage to equipment.

NOTE

Leaving the vinegar solution in the waste tank overnight will help keep the ultrasonic sensors and waste tank surfaces clean.

d. Leave the vinegar solution in the waste tank until next service. If possible, wait 12 hours before servicing the lavatory.

10. Page 3-107, following Paragraph 3.14.10, Crew Lavatory Water Fill Servicing (AF68-0213, AF68-0216, and AF69-0024) of the basic manual is amended, as a result of TO 1C-5M-544, to add new Paragraph

3.14.10.1 to read as follows:

3.14.10.1 Materials and Equipment Required for Lavatory Cleaning. Table 3-9 shows the materials and equipment required for cleaning the waste tank and drain tubes.

Table 3-9. Materials and Equipment Required for Lavatory Cleaning

Part Number Description Quantity Purpose

849695 or equiva- Vinegar 4.5 gallons Cleaning of waste tank and drain lent tubes.

Crushed ice (1 inch 1.5 gallons Waste tank and drain tube cleaning.

pieces)

5% Liquid Sodium 20 fluid ounces Disinfection of water tank.

Hypochlorite (household bleach)

Joy liquid or equiv- Soap, mild 20 fluid ounces Cleaning of waste tank.

alent

201427848-01 Tank cleaning 1 Adding cleaning fluids to waste tank.

adapter

Type A/S 32A-8 Fleet waste truck 1 Servicing of lavatory system.

truck or equivalent

11. Page 3-107, Paragraph 3.14.11, Crew Lavatory Water Fill Servicing (AF83-1285 and Up) of the basic manual is amended, as a result of TO 1C-5M-544, to read as follows:

3.14.11 Lavatory Water Tank Disinfection. (See Figure 3-34.) Disinfect the water tank in accordance with the following instructions. Refer to Table 3-9 for materials and equipment required for lavatory water tank disinfection.

CAUTION

Use only fresh water to service the lavatory water tank. Do not use water/ MiraBowl Q mixture (blue water). Failure to comply could result in damage to equipment.

a. Ensure electrical power is connected in accordance with paragraph titled Connecting External Electrical Power.

b. Ensure COMP RLY circuit breaker on flight engineer circuit breaker panel No. 5 is closed. (See Figure 1-21.)

c. Open service panel door on bottom of aircraft at FS 815.

d. Open the lever lock cap of the fill/drain nipple (Figure 3-34, 7).

e. Drain water tank in accordance with paragraph titled Water Tank Draining Procedure.

f. On tank cleaning adapter (Figure 3-34.1, 1) close Valve 1 (3), fill to top of tube (6) up to Valve 2 (4) with disinfection solution (Sodium Hypochlorite) and close Valve 2 (4).

g. Connect the tank cleaning adapter fill coupler (Figure 3-34.1, 5) to the fill/drain nipple (Figure 3- 34, 7).

h. Connect rinse water hose line of a Type A/S 32A-8 truck or equivalent to the tank cleaning adapter (Figure 3-34.1, 1) at the lav fill nipple (2).

i. Set the fill/drain switch (Figure 3-34, 3) to the OPEN position and hold until the VALVE OPEN light illuminates and release switch.

j. Start pumping water from truck.

WARNING

Ensure over flow vent area is clear. Failure to comply may cause injury to personnel and/or damage to equipment.

k. Open valves (Figure 3-34.1, 3 and 4) on tank cleaning adapter (Figure 3-34.1, 1) and fill water tank until water begins to flow out of overflow vent (Figure 3-34, 1) on the lower fuselage of aircraft.

l. Close Valve 1 (Figure 3-34.1, 3) on tank cleaning adapter (1).

m. Stop the flow of water from the service truck.

n. Hold the fill/drain switch (Figure 3-34, 3) to the close position until the VALVE CLOSED light illuminates and release switch.

o. Open Valve 1 (Figure 3-34.1, 3) on tank cleaning adapter (1) and allow residual water to drain into the servicing truck through rinse line.

p. Remove the service truck rinse line from the tank cleaning adapter; allow any residual water to drain.

q. Disconnect the tank cleaning adapter from the fill/drain nipple (7), and close the lever lock cap of the fill/drain nipple.

r. Close service panel door.

s. Allow solution to remain in the tank for 30 minutes and then flush all toilets 5 times to disinfect system plumbing.

t. Drain water tank in accordance with paragraph titled Water Tank Draining Procedure.

u. Service water tank in accordance with paragraph titled Lavatory Water Tank Servicing.

v. If electrical power is no longer required, disconnect the electrical power source from the airplane in accordance with paragraph titled Disconnecting External Electrical Power.

12. Page 3-107, Paragraph 3.14.12, Crew Lavatory Water Drain Servicing (AF68-0213, AF68-0216, and AF69-0024) of the basic manual is amended, as a result of TO 1C-5M-544, to read as follows:

3.14.12 Lavatory Waste Tank Cleaning. (See Figure 3-34 and Figure 3-34.1.) Clean the waste tank in accordance with the following instructions. Refer to Table 3-9 for materials and equipment required for lavatory waste tank cleaning.

CAUTION

. Use only fresh water to service the lavatory waste tank. Do not use water/MiraBowl Q mixture (blue water). Failure to comply could result in damage to equipment.

. Drain the waste tank if freezing temperatures are expected. Failure to comply could result in damage to equipment.

. Ensure waste tank is drained before performing Lavatory Waste Tank Cleaning. Failure to comply could result in damage to equipment.

a. Open service panel door on bottom of aircraft at FS 815.

b. Drain the lavatory waste tank in accordance with paragraph titled Waste Tank Drain Procedure.

c. Open the lever lock cap of the rinse nipple (Figure 3-34, 4).

d. Connect the rinse water hose line of a Type A/S 32A-8 truck or equivalent to the truck and fill lavatory waste tank with 20 gallons of water and disconnect servicing truck.

e. On tank cleaning adapter (Figure 3-34.1, 1) close Valve 1 (3), fill tube (6) with mild soap and close Valve 2 (4).

f. Connect the tank cleaning adapter fill coupler (Figure 3-34.1, 5) to the rinse nipple (Figure 3-34, 4).

g. Connect rinse water hose line of a Type A/S 32A-8 truck or equivalent to the tank cleaning adapter (Figure 3-34.1, 1) at lav fill nipple (2).

h. Start pumping water from service truck.

i. Open valves (Figure 3-34.1, 3 and 4) on tank cleaning adapter (Figure 3-34.1, 1) and add 10 gallons of water.

j. Close Valve 1 (3) on tank cleaning adapter (1).

k. Stop the flow of water from the service truck and remove service truck rinse hose line.

l. Open Valve 1 (Figure 3-34.1, 3) on tank cleaning adapter (1) and allow residual water to drain.

m. Disconnect the tank cleaning adapter (Figure 3-34.1, 1) from the rinse nipple (Figure 3-34, 4), and close the lever lock cap of the rinse nipple (4).

n. Close service panel door.

o. Allow solution to remain in the waste tank for 24 hours.

p. Drain waste tank in accordance with paragraph titled Waste Tank Drain Procedure.

13. Page 3-107, Paragraph 3.15, TROOP COMPARTMENT SERVICING of the basic manual is amended, as a result of TO 1C-5M-544, to be deleted in its entirety.

14. Page 3-113, Paragraph 3.16, title of the basic manual is amended, as a result of TO 1C-5M-544, to read as follows:

3.16 PRESSURIZED WATER SYSTEM SERVICING (AF83-1285 AND UP).

15. Page 3-113 through page 3-115, Paragraph 3.16.1 through Paragraph 3.16.3 of the basic manual are amended, as a result of TO 1C-5M-544, to be deleted in their entirety.

16. Page 3-187, Figure 3-34, Crew Lavatory Waste Servicing (AF68-0213, AF68-0216, and AF69-0024) (Sheet 1 of 2) of the basic manual is amended, as a result of TO 1C-5M-544, to be replaced with page 12 of this supplement.

17. Page 3-188, Figure 3-34, Crew Lavatory Waste Servicing (AF68-0213, AF68-0216, and AF69-0024) (Sheet 2) of the basic manual is amended, as a result of TO 1C-5M-544, to be deleted in its entirety.

18. Following Figure 3-34 of the basic manual is amended, as a result of TO 1C-5M-544, to add new Figure 3-34.1 and Figure 3-34.2, on page 13 and page 14 of this supplement.

19. Page 3-189, Figure 3-35, Crew Lavatory Waste Servicing (AF83-1285 and Up) of the basic manual is amended, as a result of TO 1C-5M-544, to be deleted in its entirety.

20. Page 3-193 through page 3-200, Figure 3-37 through Figure 3-39 of the basic manual are amended, as a result of TO 1C-5M-544, to be deleted in their entirety.

THE END

Figure 1-21. Circuit Breaker Locations (Sheet 6)

Figure 1-21. Circuit Breaker Locations (Sheet 13)

Figure 3-34. Crew Lavatory Waste Servicing (AF68-0213, AF68-0216, and AF69-0024)

Figure 3-34.1. Tank Cleaning Adapter

Figure 3-34.2. Toilet Maintenance Switch

TO 1C-5M-2-1

TECHNICAL MANUAL

MAINTENANCE

ORGANIZATIONAL LEVEL

GROUND HANDLING AND SERVICING

USAF SERIES

C-5M AIRCRAFT

This revision supersedes TO 1C-5M-2-1, dated 17 February 2012.

This publication incorporates Operational Supplements TO 1C-5M-2-1S-17, dated 15 March 2016, TO 1C-5M-2-1S-19, dated 21 April 2016, TO 1C-5M-2-1S-20, dated 5 May 2016, and TO 1C-5M-2-1S-24, dated 16 September 2016.

DISTRIBUTION STATEMENT D - Distribution authorized to the Department of Defense and U.S. DoD contractors only (Administrative or Operational Use) (10 September 2009). Other requests shall be referred to AFLCMC/WLSA, 235 Byron St., Suite 19A, Robins AFB, GA 31098-1670. Questions concerning technical content shall be referred to AFLCMC/WLSE, 235 Byron St., Suite 19A, Robins AFB, GA 31098- 1670.

WARNING - This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C. Sec 2751, et seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401 et seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

HANDLING AND DESTRUCTION NOTICE - Comply with distribution statement and destroy by any method that will prevent disclosure of contents or reconstruction of the document.

Published Under Authority of the Secretary of the Air Force

20 APRIL 2017

CURRENT

SUPPLEMENTS

Dates of issue for original and changed pages are:

Original. . . . . . . .0. . . . . . .20 April 2017

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 674, CONSISTING OF THE FOLLOWING:

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Title A i - xiii xiv Blank xv - xxi xxii Blank 1-1 - 1-154 2-1 - 2-178 3-1 - 3-215 3-216 Blank 4-1 - 4-54 5-1 - 5-24 Index 1 - Index 13 Index 14 Blank

FP-1

FP-2 Blank

FP-3

FP-4 Blank

FP-5

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FP-7

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FP-9

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TO 1C-5M-2-1

LIST OF EFFECTIVE PAGES INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.

NOTE The portion of the text affected by the changes is indicated by a vertical line in the outer margins of the page. Changes to illustrations are indicated by shaded or screened areas, or by miniature pointing hands.

* Zero in this column indicates an original page.

A USAF

TABLE OF CONTENTS

Chapter Page

LIST OF ILLUSTRATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ix

LIST OF TABLES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xii

INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xv

SAFETY SUMMARY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xix

1 GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

1.1 General Airplane Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

1.1.1 Airplane Description. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

1.1.2 Airplane Dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

1.1.3 Major Component Weights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

1.1.4 Airplane Stations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

1.1.5 Danger Areas. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

1.1.6 Airplane Exterior Walkways and No-Step Areas . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1

1.1.7 Airplane Maintenance and Ground Handling Markings. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-2

1.1.8 Fuel Quantity Indicator Failure (AF83-1285 and Up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-2

1.1.9 Con ned Spaces and Entry Permit Classi cation Listing . . . . . . . . . . . . . . . . . . . . . . . . . . 1-2

1.1.10 Access Provisions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-3

1.1.11 Opening LH and RH APU and ATM Compartment Access Panels . . . . . . . . . . . . . . . . . . . . 1-3

1.1.12 Closing LH and RH APU and ATM Compartment Access Panels . . . . . . . . . . . . . . . . . . . . 1-3

1.2 Metric Equivalents of U.S. Units of Measure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-3

1.3 General Maintenance Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-9

1.3.1 Personnel Restraint Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-9

1.3.2 Attachment of Personnel Restraint Equipment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-9

1.3.3 Safety Harness Attach Clevis . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-11

1.3.4 Engine Maintenance Tie Off Point at Pylon Quadrapod Truss . . . . . . . . . . . . . . . . . . . . . . . 1-12

1.3.5 Performing Maintenance Using a Workstand. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-13

1.3.6 Grounding the Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-13

1.3.7 Electrical Connectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-13

1.3.8 Connecting External Electrical Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-13

1.3.9 Apply Control and Display Electrical Power and Core Processing Electrical Power . . . . . . . . 1-18

1.3.10 Remove Control and Display Electrical Power and Core Processing Electrical Power . . . . . . . 1-25

1.3.11 Disconnecting External Electrical Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-25

1.3.12 Connecting SCM External Electrical Power (AF68-0213 and AF68-0216). . . . . . . . . . . . . . . 1-26

1.3.13 Disconnecting SCM External Electrical Power (AF68-0213 and AF68-0216) . . . . . . . . . . . . . 1-27

1.3.14 Cargo Compartment AC Power Provision. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-27

1.3.15 Circuit Breaker Locations and Deactivation Requirements . . . . . . . . . . . . . . . . . . . . . . . . . 1-27

1.3.16 Connecting External Pneumatic Power. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-27

1.3.17 Disconnecting External Pneumatic Power. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-28

1.3.18 Connecting External Hydraulic Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-28

1.3.19 Disconnecting External Hydraulic Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-29

1.4 Anti-Icing, Deicing, and Snow and Frost Removal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-29

1.4.1 Safety Precautions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-30

1.4.2 General Procedures. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-31

1.4.3 Anti-Icing, Deicing, and Snow and Frost Removal Procedures . . . . . . . . . . . . . . . . . . . . . . 1-32

1.4.4 Removal of Deposits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-32

1.4.5 Removing Frost . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-32

1.4.6 Removing Ice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-32

1.5 Extreme Climatic and Environmental Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-32

1.5.1 Condition: High Winds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-32 i

1.5.2 Condition: Blowing Sand or Dust . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-33

1.5.3 Condition: Heavy Rain . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-33

1.5.4 Condition: Extreme Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-33

1.5.5 Condition: Cold Temperatures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-34

1.5.6 Servicing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-40

1.5.7 Lubrication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-40

1.6 AN/ALE-47 Safety . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-40

2 GROUND HANDLING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

2.1 Extinguishing Ground Fires . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

2.1.1 General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

2.1.2 Fire Suppression System (FSS). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

2.1.3 Emergency Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

2.1.4 Highly Flammable Areas . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

2.1.5 Access to Local Fires . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

2.1.6 Emergency Entrances and Exits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

2.1.7 Engine and APU Fire Extinguishing System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1

2.1.8 Fire Extinguishing Agents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-2

2.1.9 Portable Fire Extinguishers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-2

2.1.10 Portable Fire ghter Assemblies. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-3

2.1.11 Fire Suppression System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-3

2.1.12 FE1301 Fire Suppression (AF68-0213, AF68-0216, and AF69-0024) . . . . . . . . . . . . . . . . . . 2-4

2.2 Towing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-4

2.2.1 General Towing Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-4

2.2.2 NLG Towing Provisions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-4

2.2.3 NLG Towing Modes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-4

2.2.4 MLG Towing Provisions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-4

2.2.5 MLG Towing Modes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-4

2.2.6 Combined NLG and MLG Towing Provisions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5

2.2.7 Combined NLG and MLG Towing Modes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5

2.2.8 Towing Safety Precautions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-6

2.2.9 NLG Towing Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-7

2.2.10 MLG Towing Procedures. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-10

2.2.11 Combined NLG and MLG Towing Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-13

2.2.12 Push-Back Procedures. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-15

2.2.13 Special ALC Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-17

2.2.14 Disconnecting the NLG Steering Torque Arm . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-20

2.2.15 NLG Steering Manifold Input Arm Disconnection for Towing. . . . . . . . . . . . . . . . . . . . . . . 2-21

2.2.16 NLG Steering Manifold Input Arm Reconnection After Towing. . . . . . . . . . . . . . . . . . . . . . 2-21

2.2.17 Connecting the NLG Steering Torque Arm . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-22

2.3 Parking. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-22

2.3.1 Positioning the Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-22

2.3.2 Parking Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-24

2.4 Mooring . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-24

2.4.1 General Mooring Information. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-24

2.4.2 Mooring in Excessive Winds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-25

2.4.3 Tiedown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-26

2.5 Jacking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-27

2.5.1 Jacking Modes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-27

2.5.2 Fuselage Jacking Points. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-28

2.5.3 Wing Jacking Points . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-28

2.5.4 NLG Jacking Point . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-28

2.5.5 MLG Jacking Point . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-28

2.5.6 Jacking Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-28

TO 1C-5M-2-1

TABLE OF CONTENTS - CONTINUED

ii

2.5.7 FS 524 and 1964 Jacking Adapter Removal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-28

2.5.8 FS 524 and FS 1964 Jacking Adapter Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-31

2.5.9 Jacking Safety Precautions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-32

2.5.10 Removal and Installation of Major Components with Airplane on Jacks . . . . . . . . . . . . . . . . 2-33

2.5.11 Allowable Center of Gravity Limits for Fuselage Jacking . . . . . . . . . . . . . . . . . . . . . . . . . . 2-34

2.5.12 Fuselage Jacking Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-34

2.5.13 Forward Fuselage Jacking Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-40

2.5.14 NLG Jacking Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-42

2.5.15 MLG Bogie Jacking Procedure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-42

2.5.16 Stabilization of the Airplane with Jacks at the Two Aft Fuselage Jack Points . . . . . . . . . . . . . 2-43

2.5.17 Removal of Jacks from the Two Aft Fuselage Jack Points . . . . . . . . . . . . . . . . . . . . . . . . . 2-44

2.5.18 MLG Shock Strut Jacking Procedure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-44

2.5.19 Stabilization of the Airplane with Six Fuselage Jacks. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-45

2.5.20 Removal of Six Fuselage Jacks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-46

2.5.21 Raising the Forward Fuselage by Kneeling the Aft MLG . . . . . . . . . . . . . . . . . . . . . . . . . . 2-46

2.5.22 Wing Jacking Procedure Using Four Jacks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-47

2.5.23 Wing Jacking Procedure Using Two Jacks (Depot Only) . . . . . . . . . . . . . . . . . . . . . . . . . . 2-49

2.5.24 Removal of an Inoperative Fuselage Jack from Under the Airplane . . . . . . . . . . . . . . . . . . . 2-50

2.6 Leveling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-53

2.6.1 Airplane Internal Leveling Provisions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-53

2.6.2 Leveling Procedure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-53

2.7 Hoisting Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-53

2.7.1 Universal Beam-Type Sling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-53

2.7.2 Aft Cargo Center Door Hoisting Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-53

2.7.3 Universal Sling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-53

2.7.4 Aileron Counterweight Sling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-54

2.7.5 Universal Wire Rope Sling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-54

2.7.6 Rudder Hoisting Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-54

2.7.7 MLG Removal and Installation Hoisting Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-54

2.7.8 MLG Sidebrace Hoisting Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-54

2.7.9 MLG Drag Strut Hoisting Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-54

2.7.10 Cradle Sling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-54

2.7.11 APU Generator Sling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-54

2.7.12 Engine Inlet Cowling Sling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-55

2.7.13 Bootstrap Beam and Saddle Adapter Set . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-55

2.7.14 Radome Handling and Hoisting Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-55

2.7.15 APU Hoisting Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-55

2.7.16 IDG Install/Remove Fixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-55

2.7.17 Portable Equipment Handling Hoisting Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-55

2.7.18 Visor Door Hoisting Adapter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-55

2.7.19 MLG Outboard Door Actuator Hoisting Beam . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-56

2.7.20 P/TA Portaloader . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-56

2.7.21 Eye to Eye Sling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-56

2.7.22 IRCM P/TA Handling Fixture. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-56

2.7.23 IRCM P/TA Hydraulic Lift . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-56

2.8 Hoisting Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-56

2.8.1 Forward Cargo Ramp Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-56

2.8.2 Forward Ramp Extension Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-56

2.8.3 Aft Cargo Ramp Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-57

2.8.4 Aft Pressure Door Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-57

2.8.5 Aft Cargo Center Door Hoisting Procedure Using the Universal Beam Type Sling (AF69-0024 and AF83-1285 and Up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-58

2.8.6 Aft Cargo Center Door Half Hoisting Procedure Using the Universal Beam Type Sling (AF68-

0213 and AF68-0216) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-59

TO 1C-5M-2-1

iii

2.8.7 Aft Cargo Center Door Hoisting Procedure for Installation or Removal on the Airplane (AF69- 0024 and AF83-1285 and Up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-59

2.8.8 Aft Cargo Center Door Half Hoisting Procedure for Installation or Removal on the Airplane (AF68-0213 and AF68-0216) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-60

2.8.9 Aft Cargo Side Door Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-60

2.8.10 MLG Outboard Door Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-61

2.8.11 Center Windshield Hoisting Procedure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-61

2.8.12 Aileron Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-61

2.8.13 Flap Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-63

2.8.14 Spoiler Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-63

2.8.15 Wing Tip Leading Edge Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-64

2.8.16 Slat Hoisting Procedure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-64

2.8.17 Wing Leading Edge Panel Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-65

2.8.18 Elevator Hoisting Procedure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-65

2.8.19 Rudder Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-66

2.8.20 Vertical Stabilizer Leading Edge Section Hoisting Procedure. . . . . . . . . . . . . . . . . . . . . . . . 2-67

2.8.21 NLG and Components Hoisting Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-67

2.8.22 MLG Shock Strut and Bogie Hoisting Procedure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-67

2.8.23 MLG Drag Strut Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-67

2.8.24 MLG Sidebrace Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-67

2.8.25 Universal Heavy Duty Cradle Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-67

2.8.26 MLG Door Cradle Hoisting Procedure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-68

2.8.27 AFT Cargo Side Door Cradle Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-68

2.8.28 Nose Radome Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-68

2.8.29 P/TA No. 1 and No. 2 Hoisting Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-68

2.9 Ground Handling Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-68

2.9.1 Universal Heavy Duty Cradle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-68

2.9.2 Aft Cargo Side Door Cradle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-68

2.9.3 MLG Door Cradle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-68

2.9.4 APU Ground Handling Cart . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-69

2.9.5 Vertical Stabilizer Internal Access Personnel Platform . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-69

2.9.6 Truck-Mounted Servicing Platform . . . .