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Failure to comply with Step a and Step b could result in injury to personnel.

NOTE

Any item noted in Step a and Step b which affects proper use of harness will be cause to reject harness assembly
as unserviceable.

a. Ensure personnel restraint kit inspection tag is within serviceable date. Check harness (5) and safety straps (7) for

evidence of damage, wear, fraying straps, loose or improper stitches; hardware for corrosion and damage; and strap
lock bar (31) for proper operation. Check the safety strap restraint bolts (18) for damage, the bolt handle (34) for
proper operation, and the attachment pin (42) for proper installation and for installation of the washer (39). Ensure
streamer (37) is attached.

b. Check safety pack (17) for evidence of tampering or damage. Check hook assemblies (19) for proper operation of

locks. Ensure seals are intact and tags showing which hook to attach to harness are securely attached.

c. Attach two safety straps (7) to the safety pack (17).

Ensure that safety pack is attached to harness per Figure 1-15. Failure to comply could result in death or serious
injury of personnel.

d. Attach safety pack (17) to back of harness (5) with three attaching straps (16) and connect proper hook (19) (metal

tagged) to harness (5). Attach the two accessory bags (11) to the harness, using the four attaching straps (32). Put on
the harness and adjust as necessary to obtain a snug

¿

t. Tuck in loose ends of harness to prevent interference with

movements of harness wearer.

NOTE

The slotted Delrin (plastic) plug is designed to keep water, debris, and other contaminants out of the threaded

¿

tting insert, and must be kept

À

ush with the airplane surface when the restraint

¿

tting is not in use. The plug

should not be removed for attachment of the harness bolt assembly since the bolt blade, once engaged in the plug
slot, will thread the plug into the

¿

tting and then return the plug to

À

ush when the harness bolt assembly is

disconnected. If the plug is discovered damaged or missing, clean out the

¿

tting and insert a new plug. For

corrosion inspection and removal, and installation of personnel restraint

¿

ttings, refer to TO 1C-5M-23, Chapter 6

through TO 1C-5M-23, Chapter 8 and TO 1C-5M-3, Chapter 3.

e. Before getting on top of the airplane, secure a harness bolt assembly to the nearest airplane

¿

tting. With the slotted

Delrin plug (44)

À

ush with the airplane surface, secure the harness bolt assembly by inserting bolt blade (40) into the

slot of the Delrin plug and rotating both components clockwise into the airplane

¿

tting until the harness bolt assembly

is seated.

TO 1C-5M-2-1

1-10

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Содержание C-5M

Страница 1: ...tribution 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...

Страница 2: ...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...

Страница 3: ...ncerning 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...

Страница 4: ...ste 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...

Страница 5: ...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 w...

Страница 6: ...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 a...

Страница 7: ...r 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...

Страница 8: ...onic 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...

Страница 9: ...e 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...

Страница 10: ...cedure 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...

Страница 11: ...re 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...

Страница 12: ...TO 1C 5M 2 1S 1 Figure 1 21 Circuit Breaker Locations Sheet 6 10...

Страница 13: ...TO 1C 5M 2 1S 1 Figure 1 21 Circuit Breaker Locations Sheet 13 11...

Страница 14: ...TO 1C 5M 2 1S 1 Figure 3 34 Crew Lavatory Waste Servicing AF68 0213 AF68 0216 and AF69 0024 12...

Страница 15: ...TO 1C 5M 2 1S 1 Figure 3 34 1 Tank Cleaning Adapter 13...

Страница 16: ...TO 1C 5M 2 1S 1 Figure 3 34 2 Toilet Maintenance Switch 14...

Страница 17: ...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 ex...

Страница 18: ...4 54 0 5 1 5 24 0 Index 1 Index 13 0 Index 14 Blank 0 FP 1 0 FP 2 Blank 0 FP 3 0 FP 4 Blank 0 FP 5 0 FP 6 Blank 0 FP 7 0 FP 8 Blank 0 FP 9 0 FP 10 Blank 0 TO 1C 5M 2 1 LIST OF EFFECTIVE PAGES INSERT L...

Страница 19: ...ng 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 Powe...

Страница 20: ...es 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...

Страница 21: ...3 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 R...

Страница 22: ...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...

Страница 23: ...vicing Trucks 3 6 3 2 5 Single Point Refueling 3 7 3 2 6 Refueling for Normal Fuel Sequencing 3 14 3 2 7 Over Wing Refueling 3 14 3 2 8 Single Point Defueling 3 17 3 2 9 Fuel Servicing from C 5 Airpla...

Страница 24: ...ing System Safety Precautions 3 69 3 8 2 Dewar Drain Procedure 3 69 3 8 3 Dewar Drain Procedure Using Ground Servicing Unit Part Number CVA 9K 90 TM AF 3 72 3 8 4 Liquid Nitrogen Fuel Tank Inerting an...

Страница 25: ...16 3 17 Escape Slide Servicing 3 118 3 17 1 Precharging the Escape Slide Reservoirs 3 118 3 18 Crew Door Accumulator Servicing 3 119 3 18 1 Precharging the Crew Door Accumulator 3 119 3 19 Relief Crew...

Страница 26: ...n 5 1 5 2 Emergency Removal Procedures 5 1 5 2 1 Emergency Removal Procedures Nose Gear Up Main Gear Normal 5 1 5 2 2 Emergency Removal Procedures All Main Gear Up Nose Gear Normal 5 4 5 2 3 Emergency...

Страница 27: ...Fuel JETTISON and VIA AIU ALT POWER Switch Locations 1 138 1 25 Caution Light and Emergency Exit Light Switch Locations 1 139 1 26 Touchdown Sensor Location 1 140 1 27 Display Defaults 1 141 1 28 INST...

Страница 28: ...r 2 138 2 44 IRCM P TA Handling Fixture 2 139 2 45 IRCM P TA Hydraulic Lift 2 140 2 46 Universal Heavy Duty Cradle 2 141 2 47 MLG Door Cradle 2 142 2 48 Aft Cargo Side Door Cradle 2 143 2 49 APU Groun...

Страница 29: ...21 Lox Servicing 3 165 3 22 Lox Draining 3 167 3 23 FSS Servicing 3 169 3 24 Engine Oil Tank Servicing 3 173 3 25 Engine Starter Magnetic Drain Plug Inspection and Starter Servicing 3 174 3 26 IDG Ser...

Страница 30: ...ication AF68 0213 and AF68 0216 4 42 4 22 Movable Bulkhead Lubrication AF68 0213 and AF68 0216 4 46 4 23 Retractable Rollers Lubrication AF68 0213 and AF68 0216 4 49 4 24 Aft Ramp Lubrication 4 50 4 2...

Страница 31: ...red 3 39 3 3 Normal Tire Servicing Requirements 3 46 3 4 Normal Tire Servicing Requirements 3 57 3 5 Tools and Test Equipment Required 3 60 3 6 Tools and Test Equipment Required 3 68 3 7 Tools and Tes...

Страница 32: ......

Страница 33: ...ns by illustration number a list of tables by table number a detailed table of contents listing chapters and the major items discussed in that chapter and if manual size requires an index locating tex...

Страница 34: ...e ESDS Refer to TO 00 25 234 for ESDS device handling procedures 6 TIME COMPLIANCE TECHNICAL ORDERS Time Compliance Technical Orders TCTO authorize and give instructions for inspection or modi cation...

Страница 35: ...emovable Memory Module SCM Space Cargo Modi cation SPR Single Point Refueling UHF Ultra High Frequency V UHF Very High Frequency VIA Versatile Integrated Avionics WIAGO Wireless Intercom for Aircraft...

Страница 36: ...phatic Naphtha TT N 95 Dry Cleaning Fluid MIL PRF 680 Type II or Type III DS 108 Commercial Isopropyl Alcohol TT I 735 Shopmaster RC Commercial Prior to Adhesive Bonding Acetone ASTM D 329 Aliphatic N...

Страница 37: ...ure practice condition statement etc which if not strictly observed could result in damage to or destruction of equipment or loss of mission effective ness NOTE A NOTE highlights an essential operatin...

Страница 38: ...be used to store all removed hardware All tools equipment and hardware used during a task shall be accounted for at the completion of the task An inspection for foreign objects shall be conducted pri...

Страница 39: ...death of personnel 7 HAZARDOUS MATERIALS Warnings associated with the use of hazardous materials in this manual are listed below Where necessary these warnings are posted before task or step to which...

Страница 40: ......

Страница 41: ...ult in permanent hearing impairment The turbofan engines emit exhaust gases which are capable of reaching very high temperatures and velocities All personnel should study the danger areas shown in Fig...

Страница 42: ...a digital fuel quantity indicator goes blank a possible hot fault exists An undetected additional fault could result in a re or an explosion should an explosive mixture be present in the fuel tank If...

Страница 43: ...e Dzus fastener to forward and aft compartment vertical frames 1 1 12 Closing LH and RH APU and ATM Compartment Access Panels See Figure 1 14 a While holding compartment access panel 1 release single...

Страница 44: ...654 7 177 800 17 780 7 2 135 7 11 263 8 203 200 20 320 8 2 440 8 12 872 9 228 600 22 860 9 2 745 9 14 481 10 254 000 25 400 10 3 050 10 16 090 20 508 000 50 800 20 6 100 20 32 180 30 762 000 76 200 3...

Страница 45: ...800 Table 1 5 Liquid Capacity Ounces Millimeters Liters Pints Liters Quarts Liters Gallons Liters 1 29 574 0 030 1 0 473 1 0 946 1 3 785 2 59 148 0 059 2 0 946 2 1 892 2 7 570 3 88 722 0 089 3 1 419...

Страница 46: ...000 20 9 080 30 850 500 30 13 620 40 1 134 000 40 18 160 50 1 417 500 50 22 700 60 1 701 000 60 27 240 70 1 984 500 70 31 780 80 2 268 000 80 36 320 90 2 551 500 90 40 860 100 2 835 000 100 45 400 Ta...

Страница 47: ...20 97 640 300 21 000 30 146 460 400 28 000 40 195 280 500 35 000 50 244 100 600 42 000 60 292 920 700 49 000 70 341 740 800 56 000 80 390 560 900 63 000 90 439 380 1 000 70 000 100 488 200 Table 1 9 T...

Страница 48: ...Sec ond Miles Per Hour Kilometers Per Hour Knots Kilometers Per Hour 1 0 305 1 1 609 1 1 852 2 0 610 2 3 218 2 3 704 3 0 915 3 4 827 3 5 556 4 1 220 4 6 436 4 7 408 5 1 525 5 8 045 5 9 260 6 1 830 6 9...

Страница 49: ...and screwing both components into the airplane tting When the handle of the bolt is vertical it allows the adapter end of a strap assembly to slide over the handle and down onto the bolt Returning the...

Страница 50: ...proper hook 19 metal tagged to harness 5 Attach the two accessory bags 11 to the harness using the four attaching straps 32 Put on the harness and adjust as necessary to obtain a snug t Tuck in loose...

Страница 51: ...reaching the desired area connect the second strap to a tting nearer the desired area and then disconnect the rst strap connected Disconnecting strap before getting off top of airplane could result i...

Страница 52: ...s to attach the personal fall protection devices The lifeline lanyard used must be no longer than 4 feet long Shock absorbing lanyards and deceleration devices are not authorized Failure to comply may...

Страница 53: ...of avionic components Microminiature connectors are especially susceptible to damage a When disconnecting connectors by pulling connector straight out from receptacle do not pull on wiring b Cover di...

Страница 54: ...panel No 2 ISOLATED DC BUS During normal ground maintenance operations TOUCH DOWN 1 and TOUCH DOWN 2 circuit breakers should always be closed To alert maintenance personnel not to open these circuit...

Страница 55: ...ISON switches Figure 1 24 1 on the ight engineer fuel management panel are in OFF and that the two red guards are down o On the forward overhead panel ensure that the following switches are in OFF Fig...

Страница 56: ...0 or equivalent power cart Place power cart unit switch to OFF t Open external power receptacle door u Ensure that EXT PWR CONTROL circuit breaker in the external power receptacle box is closed Before...

Страница 57: ...OR BUS SWITCH 2 MONITOR BUS SWITCH 3 2 To AUTO AC CROSS TIE SWITCH NOTE Cross tie CLOSED light will be defaulted to NVIS very dim until core processing system power is applied z Verify that cross tie...

Страница 58: ...nics equipment If VIA AIU fan fail message is received remove core power from affected LRU within 30 minutes If a VIA AIU overtemp message is received remove power from affected LRU immediately Failur...

Страница 59: ...SIU 1 PILOT CENTER MFDU 4 Pilot emergency circuit breaker panel lower EMERGENCY DC BUS RIU NO 1 RIU NO 3 RIU NO 5 5 Flight engineer circuit breaker panel No 3 FWD MAIN AC BUS NO 3 PHASE B INST GROUND...

Страница 60: ...C BUS COPILOT MCDU BIP COPILOT LEFT MFDU PLT NAV ELP ANN DIMMER PILOT CNP 12 Navigator circuit breaker panel No 1 AVIONICS BATTERY BUS VIA 1 AIU 1 VIA 2 AIU 2 13 Navigator circuit breaker panel No 1 A...

Страница 61: ...2 is in NORMAL Do not apply force or hang any items on control wheel yoke Failure to comply will result in failures and calibration errors of control wheel hub sensors e Close ground switches on the...

Страница 62: ...ker panel No 1 and navigator circuit breaker panel No 2 Wait 1 minute then return to Step e If VIA 2 is not available on any MCDU MENU page within 2 minutes of display of VIA 1 open ground switches fo...

Страница 63: ...FAIL CCDL FAULT 2 Advisories White BIP FAIL FMS 1 FAIL FMS 2 FAIL COMM MGMT 1 FAIL COMM MGMT 2 FAIL VIA 1 FAN FAIL AIU 1 FAN FAIL VIA 2 FAN FAIL AIU 2 FAN FAIL RIU 1 FAIL RIU 2 FAIL RIU 3 FAIL RIU 4 F...

Страница 64: ...ately 3 minutes NOTE The password for EDS access can be found in the notes section of AFTO Form 781A u On PCIU place cursor on EDS icon then press left mouse button Enter user password then press left...

Страница 65: ...should be accomplished with or without the use of an RMM in the PCIU NOTE It is essential that EDS data is nalized using the PCIU before removing power from the AMC Removing power from the AMC before...

Страница 66: ...nually closed The receptacle is located 20 inches aft of the airplane external electrical power receptacle This receptacle is dedicated to providing power only to the space cargo container The externa...

Страница 67: ...ent AC power provision in the airplane with power source to the AC power provision in the cargo compartment of the airplane receiving the electrical power 1 3 15 Circuit Breaker Locations and Deactiva...

Страница 68: ...rnal hydraulic power to the airplane use the following procedure Prior to connecting external hydraulic power ensure that a warning tag is not attached to the external hydraulic receptacle Failure to...

Страница 69: ...ssurize until the leak is repaired 1 3 19 Disconnecting External Hydraulic Power See Figure 1 31 Disconnect external hydraulic power in the reverse order of connecting external hydraulic power 1 4 ANT...

Страница 70: ...id in and around airplane having silver or silver coated electrical electronic circuitry Rapid oxidation and re can occur when glycol water solutions come in contact with and short across bare or defe...

Страница 71: ...1 Apply uid when LOX carts are in vicinity of airplane 2 Position stabilizers and elevators so that liquid will be drained from surface 2 Apply uid by spray method unless all personnel are clear of s...

Страница 72: ...all be exercised at all times to prevent any damage to the airplane surfaces Sharp instruments such as picks knives or screwdrivers will not be used to loosen the ice formation The use of uid Speci ca...

Страница 73: ...check for and remove accumulations of dust at ight control system equip ment areas d When operating in a dusty environment check for and remove accumulations of dust from hydraulic actuator pistons a...

Страница 74: ...result in injury to personnel Whenever temperatures below 32 F 0 C are anticipated drain potable water tanks and remove all other freezable liquids 1 5 5 2 Hydraulic Systems NOTE At temperatures of 0...

Страница 75: ...warmed above 40 F 40 C b For continuous operation greater than 30 minutes the ight station and avionics bay compartments are warmed above 5 F 15 C c Following exposure of the airplane to ground tempe...

Страница 76: ...oil servicing door for 30 minutes oil tank and into the pressure relief door on the LH thrust reverser in the area of the accessory gearbox b The following are alternate engine start procedures for c...

Страница 77: ...s are in operation 1 5 5 8 EDS EDS should only be operated within the temperature range of 32 F to 122 F 0 C to 50 C Operation of EDS outside of this temperature range can result in damage to EDS comp...

Страница 78: ...unkneeling after exposure to very cold ambient temperatures individual landing gear may stall due to the increased friction The unkneeling operation should be continued as long as adequate airplane t...

Страница 79: ...s should be in the NORM position when using COLD START switch The windshield heat control system will not function automatically if the temperature of the windshield glass is below 40 F 40 C The COLD...

Страница 80: ...r heat is used f If the upper deck compartments must continue to be warmed during cargo compartment warm up select both packs with air ow in NORM or INTMED depending on how much heat can be diverted f...

Страница 81: ...light Engineer No 6 RH TORQUE BOX NO 6 SQUIB Main DC No 1 Flight Engineer No 6 If squib power cannot be removed ares must be removed from airplane Failure to comply could result in injury to personnel...

Страница 82: ...Figure 1 1 Airplane Dimensions TO 1C 5M 2 1 1 42...

Страница 83: ...Figure 1 2 Major Component Weights Sheet 1 of 3 TO 1C 5M 2 1 1 43...

Страница 84: ...Figure 1 2 Major Component Weights Sheet 2 TO 1C 5M 2 1 1 44...

Страница 85: ...Figure 1 2 Major Component Weights Sheet 3 TO 1C 5M 2 1 1 45...

Страница 86: ...Figure 1 3 Airplane Stations Sheet 1 of 8 TO 1C 5M 2 1 1 46...

Страница 87: ...Figure 1 3 Airplane Stations Sheet 2 TO 1C 5M 2 1 1 47...

Страница 88: ...Figure 1 3 Airplane Stations Sheet 3 TO 1C 5M 2 1 1 48...

Страница 89: ...Figure 1 3 Airplane Stations Sheet 4 TO 1C 5M 2 1 1 49...

Страница 90: ...Figure 1 3 Airplane Stations Sheet 5 TO 1C 5M 2 1 1 50...

Страница 91: ...Figure 1 3 Airplane Stations Sheet 6 TO 1C 5M 2 1 1 51...

Страница 92: ...Figure 1 3 Airplane Stations Sheet 7 TO 1C 5M 2 1 1 52...

Страница 93: ...Figure 1 3 Airplane Stations Sheet 8 TO 1C 5M 2 1 1 53...

Страница 94: ...Figure 1 4 Danger Areas Sheet 1 of 17 TO 1C 5M 2 1 1 54...

Страница 95: ...Figure 1 4 Danger Areas Sheet 2 TO 1C 5M 2 1 1 55...

Страница 96: ...Figure 1 4 Danger Areas Sheet 3 TO 1C 5M 2 1 1 56...

Страница 97: ...Figure 1 4 Danger Areas Sheet 4 TO 1C 5M 2 1 1 57...

Страница 98: ...Figure 1 4 Danger Areas Sheet 5 TO 1C 5M 2 1 1 58...

Страница 99: ...Figure 1 4 Danger Areas Sheet 6 TO 1C 5M 2 1 1 59...

Страница 100: ...Figure 1 4 Danger Areas Sheet 7 TO 1C 5M 2 1 1 60...

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