tm 1-1520-240-10 technical manual operator's manual for army ch ...

Recommendations

Info

Figure 9-1-3. 712 Single - Engine Service Ceiling TM 1-1520-240-10 9-1-7
TM 1-1520-240-10 Figure 9-1-4. 712 Height Velocity Diagram for Safe Landing After Single-Engine Failure (Sheet 1 of 3) 9-1-8
Page 1:
TECHNICAL MANUAL OPERATOR’S MANUA
Page 4 and 5:
TM 1-1520-240-10 b Change 1 WARNING
Page 7:
URGENT TM 1-1520-240-10 CHANGE HEAD
Page 11 and 12:
*Zero in this column indicates an o
Page 13 and 14:
TM 1-1520-240-10 TECHNICAL MANUAL H
Page 15:
TM 1-1520-240-10 Chapter/Section Pa
Page 18 and 19:
TM 1-1520-240-10 1-1-13. Aircraft D
Page 20 and 21:
TM 1-1520-240-10 2-1-2 Figure 2-1-1
Page 22 and 23:
TM 1-1520-240-10 2-1-4 Figure 2-1-3
Page 24 and 25:
TM 1-1520-240-10 2-1-10. Brakes and
Page 26 and 27:
TM 1-1520-240-10 2-1-8 Figure 2-1-5
Page 28 and 29:
TM 1-1520-240-10 2-1-10 Figure 2-1-
Page 30 and 31:
TM 1-1520-240-10 2-1-12 Figure 2-1-
Page 32 and 33:
TM 1-1520-240-10 2-1-14 Figure 2-1-
Page 34 and 35:
TM 1-1520-240-10 2-1-16 Figure 2-1-
Page 36 and 37:
TM 1-1520-240-10 2-1-18 Figure 2-1-
Page 38 and 39:
TM 1-1520-240-10 2-2-2 Fwd Valve Fw
Page 40 and 41:
TM 1-1520-240-10 2-2-8. TROOP WARN
Page 42 and 43:
TM 1-1520-240-10 The power turbine
Page 44 and 45:
TM 1-1520-240-10 Figure 2-3-2. Emer
Page 46 and 47:
TM 1-1520-240-10 and NO. 2 OIL TEMP
Page 48 and 49:
TM 1-1520-240-10 d. RRPM droop comp
Page 50 and 51:
TM 1-1520-240-10 2-3-10 Figure 2-3-
Page 52 and 53:
TM 1-1520-240-10 Table 2-3-1. T55-G
Page 54 and 55:
TM 1-1520-240-10 2-3-14 Table 2-3-1
Page 56 and 57:
TM 1-1520-240-10 Table 2-3-1. T55-G
Page 58 and 59:
TM 1-1520-240-10 2-3-18 Figure 2-3-
Page 61 and 62:
2-4-1. Fuel Supply System. The fuel
Page 63 and 64:
2-4-6. Manual Defueling Valve. A ma
Page 65 and 66:
2-4-6). The switches are used to te
Page 67 and 68:
2-5-1. Flight Control System. The h
Page 69 and 70:
Figure 2-5-2. Cyclic Stick Grip 2-5
Page 71 and 72:
(1) HDG Switch. The HDG (heading) s
Page 73 and 74:
2-6-1. Hydraulic Power Supply Syste
Page 75 and 76:
us through the RAMP PWR switch and
Page 77 and 78:
TM 1-1520-240-10 No. 2 engine trans
Page 79 and 80:
TM 1-1520-240-10 2-7-12. Transmissi
Page 82 and 83:
2-9-1. Anti Icing Systems. Anti ici
Page 84 and 85:
through the HYDRAULICS MAINT PNL LT
Page 86 and 87:
TM 1-1520-240-10 SECTION X. HEATING
Page 88 and 89:
TM 1-1520-240-10 SECTION XI. ELECTR
Page 90:
2-11-7. BATT Switch. NOTE The follo
Page 93 and 94:
TM 1-1520-240-10 2-12-2 Figure 2-12
Page 95 and 96:
TM 1-1520-240-10 a. Electroluminesc
Page 97 and 98:
TM 1-1520-240-10 2-13-4 Figure 2-13
Page 99 and 100:
TM 1-1520-240-10 bulkhead. The six
Page 101 and 102:
TM 1-1520-240-10 2-13-8 Figure 2-13
Page 104 and 105:
2-14-1. General. The following para
Page 106 and 107:
When the helicopter descends below
Page 108 and 109:
2-14-13. Controls and Function, Rad
Page 110 and 111:
2-14-21. CHRONOMETER. Two digital c
Page 112 and 113:
Table 2-14-1. Master Caution Panel
Page 114 and 115:
2-14-30. CAUTION LT Panel. The CAUT
Page 116 and 117:
SECTION XV. SERVICING, PARKING, AND
Page 118 and 119:
k. Remove ground cables from the he
Page 120 and 121:
Figure 2-15-2. Servicing Diagram (S
Page 122 and 123:
Figure 2-15-2. Servicing Diagram (S
Page 124 and 125:
TM 1-1520-240-10 Table 2-15-1. Serv
Page 126 and 127:
Table 2-15-3. JP-4 Equivalent Fuel
Page 128 and 129:
2-15-7. Gravity Refueling. Perform
Page 130 and 131:
2-15-15. Transmission Oil System. S
Page 132 and 133:
FLIGHT CONTROL, UTILITY, POWER STEE
Page 134 and 135:
Figure 2-15-4. Protective Covers TM
Page 136:
Figure 2-15-6. Installation of Heli
Page 139 and 140:
TM 1-1520-240-10 3-1-2 Table 3-1-1.
Page 141 and 142:
TM 1-1520-240-10 3-2-2 Figure 3-2-1
Page 143 and 144:
TM 1-1520-240-10 3-2-6. Word-of-Day
Page 145 and 146:
TM 1-1520-240-10 3-2-9. Conferencin
Page 147 and 148:
TM 1-1520-240-10 SET. 3-2-8 (2) Cha
Page 149 and 150:
TM 1-1520-240-10 3-2-10 NOTE The an
Page 151 and 152:
TM 1-1520-240-10 c. Frequency Range
Page 153 and 154:
TM 1-1520-240-10 3-2-19. Controls a
Page 155 and 156:
TM 1-1520-240-10 3-2-21. HF Radio S
Page 157 and 158:
TM 1-1520-240-10 3-2-24. Operating
Page 159 and 160:
TM 1-1520-240-10 CONTROLS/ FUNCTION
Page 161 and 162:
TM 1-1520-240-10 CONTROLS/ INDICATO
Page 163 and 164:
Page 165 and 166:
TM 1-1520-240-10 (6) Push the INIT
Page 167 and 168:
TM 1-1520-240-10 NOTE To exit and s
Page 169 and 170:
Page 171 and 172:
TM 1-1520-240-10 3-3-8. Gyromagneti
Page 173 and 174:
TM 1-1520-240-10 3-3-6 Figure 3-3-5
Page 175 and 176:
Page 177 and 178:
TM 1-1520-240-10 LEFT DISPLAY RIGHT
Page 179 and 180:
TM 1-1520-240-10 e. FLY-TO DEST thu
Page 181 and 182:
TM 1-1520-240-10 from the No. 2 (No
Page 183 and 184:
TM 1-1520-240-10 3-3-35. Horizontal
Page 185 and 186:
Page 187 and 188:
TM 1-1520-240-10 tered in any of th
Page 189 and 190:
TM 1-1520-240-10 (7) Observe the CD
Page 191 and 192:
TM 1-1520-240-10 LEFT DISPLAY RIGHT
Page 193 and 194:
TM 1-1520-240-10 3-3-26 NOTE To acc
Page 195 and 196:
TM 1-1520-240-10 (3) Position updat
Page 197 and 198:
TM 1-1520-240-10 (4) To select the
Page 199 and 200:
TM 1-1520-240-10 NOTE In this mode,
Page 201 and 202:
TM 1-1520-240-10 Table 3-3-4. Map D
Page 204 and 205:
3-4-1. Transponder System (AN/APX-1
Page 206 and 207:
3-4-3. Normal Operation — Transpo
Page 208 and 209:
4-1-1. Radar Signal Detecting, AN/A
Page 210 and 211:
4-1-2. CONTROLS AND FUNCTION, RADAR
Page 212 and 213:
4-1-3). Check OFP and EID numbers a
Page 214 and 215:
4-1-6. Controls and Indicators, Mis
Page 216 and 217:
CONTROLS/ FUNCTION INDICATOR ARM In
Page 218 and 219:
Figure 4-1-6. Flare Dispenser Syste
Page 220 and 221:
4-1-18. Controls and Function, Coun
Page 222 and 223:
4-1-24. Normal Operation. WARNING K
Page 224 and 225:
4-1-26. CMDS Messages. Below is a l
Page 226 and 227:
Figure 4-1-8. Heads Up Display AN/A
Page 228 and 229:
No. Symbol Source Range/Description
Page 230 and 231:
CAUTION Keep the protective caps on
Page 232 and 233:
8. MODE 1-4/DCLT switch — DCLT (1
Page 234 and 235:
4-2-1. Armament Subsystems The arma
Page 236 and 237:
Figure 4-2-1. Armament Subsystem TM
Page 238 and 239:
single cartridges or short bursts c
Page 240 and 241:
Figure 4-2-5. Right Machine Gun Mou
Page 242 and 243:
Figure 4-2-8. Ammunition Can — In
Page 244:
Figure 4-2-10. M41 Mount — Instal
Page 247 and 248:
TM 1-1520-240-10 (3) Cable cutter s
Page 249 and 250:
TM 1-1520-240-10 4-3-4 Figure 4-3-2
Page 251 and 252:
TM 1-1520-240-10 4-3-6 Figure 4-3-3
Page 253 and 254:
TM 1-1520-240-10 (3) Hoist master s
Page 255 and 256:
TM 1-1520-240-10 (2) Break the shea
Page 257 and 258:
TM 1-1520-240-10 Figure 4-3-10. Hoi
Page 259 and 260:
TM 1-1520-240-10 The hook assembly
Page 261 and 262:
TM 1-1520-240-10 Figure 4-3-12. Cen
Page 263 and 264:
TM 1-1520-240-10 4-3-18 CAUTION The
Page 265 and 266:
TM 1-1520-240-10 HOOK OPEN caution
Page 267 and 268:
TM 1-1520-240-10 4-3-22 Figure 4-3-
Page 269 and 270:
TM 1-1520-240-10 4-3-24 Figure 4-3-
Page 272 and 273:
TM 1-1520-240-10 SECTION IV. EXTEND
Page 274 and 275:
Figure 4-4-1. ERFS II Fuel Tank TM
Page 276 and 277:
Figure 4-4-2. ERFS II Fuel Control
Page 278:
4-4-9. FARE Transfer. CAUTION Some
Page 282 and 283:
5-2-1. Instrument Markings. 5-2-2.
Page 284 and 285:
400 810 890 781 940 890 O C C C C C
Page 286 and 287:
Figure 5-2-1 Instrument Markings (S
Page 288:
5-3-1. Engine Rating and Power Leve
Page 292 and 293:
5-5-1. Airspeed Operating Limits. A
Page 294:
Figure 5-5-2. Airspeed Limitations
Page 298 and 299:
5-7-1. Engine Inlet Screen Limitati
Page 300 and 301:
Figure 5-7-1. Rotor Blade Start-Up
Page 302:
TM 1-1520-240-10 5-7-5/(5-7-6 blank
Page 305 and 306:
TM 1-1520-240-10 SEA STATE 5-8-2 Ta
Page 308 and 309:
6-1-1. Purpose. This chapter contai
Page 310:
6-2-1. DD Form 365-3 Chart C — Ba
Page 313 and 314:
TM 1-1520-240-10 6-3-2 Figure 6-3-1
Page 315 and 316:
TM 1-1520-240-10 6-4-11. Litter Sup
Page 317 and 318:
TM 1-1520-240-10 6-4-4 Figure 6-4-2
Page 319 and 320:
TM 1-1520-240-10 6-4-6 Figure 6-4-4
Page 321 and 322:
TM 1-1520-240-10 6-4-8 Figure 6-4-5
Page 323 and 324:
TM 1-1520-240-10 6-4-10 Figure 6-4-
Page 326 and 327:
6-5-1. Mission Equipment. CH-47D mi
Page 328:
Figure 6-5-1. Mission Equipment Wei
Page 331 and 332:
TM 1-1520-240-10 6-6-8. Uniformly D
Page 333 and 334:
TM 1-1520-240-10 6-6-10. Concentrat
Page 335 and 336:
TM 1-1520-240-10 face of the floor.
Page 337 and 338:
TM 1-1520-240-10 6-6-8 Figure 6-6-3
Page 339 and 340:
TM 1-1520-240-10 6-6-10 Figure 6-6-
Page 341 and 342:
TM 1-1520-240-10 6-6-12 Figure 6-6-
Page 343 and 344:
TM 1-1520-240-10 6-6-21. Winch. Ref
Page 345 and 346:
TM 1-1520-240-10 6-6-16 CAUTION Do
Page 347 and 348:
TM 1-1520-240-10 6-6-35. Cargo Weig
Page 349 and 350:
TM 1-1520-240-10 Figure 6-6-11. Car
Page 351 and 352:
TM 1-1520-240-10 6-6-22 Figure 6-6-
Page 353 and 354:
TM 1-1520-240-10 6-6-24 CAUTION Exc
Page 355 and 356:
TM 1-1520-240-10 6-6-26 Table 6-6-2
Page 357 and 358:
TM 1-1520-240-10 6-6-28 Table 6-6-3
Page 359 and 360:
TM 1-1520-240-10 6-6-30 Figure 6-6-
Page 361 and 362:
TM 1-1520-240-10 6-6-32 Figure 6-6-
Page 363 and 364:
TM 1-1520-240-10 6-7-2 Figure 6-7-1
Page 365 and 366:
TM 1-1520-240-10 b. Calculated Data
Page 368 and 369:
7-2-1. Emergency Torque Available.
Page 370 and 371:
SECTION III. MAXIMUM TORQUE AVAILAB
Page 372:
Figure 7-3-2. Maximum Torque Availa
Page 375 and 376:
TM 1-1520-240-10 7-4-2 Figure 7-4-1
Page 377 and 378:
TM 1-1520-240-10 7-5-2 Figure 7-5-1
Page 380 and 381:
7-6-1. Description. The takeoff cha
Page 382 and 383:
7-7-1. Description. The cruise char
Page 384 and 385:
Pressure OAT Altitude (ft) (C) Tabl
Page 386 and 387:
Page 388 and 389:
Figure 7-7-1 Example Cruise Chart (
Page 390 and 391:
Figure 7-7-3. 98 and 100% Rotor RPM
Page 392 and 393:
Figure 7-7-5. 98 and 100% Rotor RPM
Page 394 and 395:
Figure 7-7-7. 100% Rotor RPM, 10 an
Page 396 and 397:
Figure 7-7-9. 100% Rotor RPM, 50C,
Page 398 and 399:
Figure 7-7-11. 98 and 100% Rotor RP
Page 400 and 401:
Page 402 and 403:
Figure 7-7-15. 100% Rotor RPM, 10 a
Page 404 and 405:
Page 406 and 407:
Page 408 and 409:
Page 410 and 411:
Page 412 and 413:
Page 414 and 415:
Page 416 and 417:
Page 418 and 419:
Page 420 and 421:
Page 422 and 423:
Page 424 and 425:
Page 426 and 427:
Page 428 and 429:
Page 430 and 431:
Page 432 and 433:
Page 434 and 435:
Page 436 and 437:
Page 438 and 439:
Page 440 and 441:
Page 442 and 443:
Page 444 and 445:
Page 446 and 447:
Page 448 and 449:
Page 450 and 451:
Page 452 and 453:
Page 454 and 455:
Page 456 and 457:
Page 458 and 459:
Page 460 and 461:
Page 462 and 463:
Page 464 and 465:
Page 466 and 467:
Page 468 and 469:
Page 470 and 471:
Figure 7-7-83. 100% Rotor RPM, -10
Page 472 and 473:
7-8-1. Description. The drag chart
Page 474 and 475:
7-9-1. Description. a. Climb and de
Page 476 and 477:
Figure 7-9-2. Climb Performance (Sh
Page 478 and 479:
7-10-1. Description. The idle fuel
Page 480:
Figure 7-10-2. Idle Fuel Flow Chart
Page 483 and 484:
TM 1-1520-240-10 7-11-2 Figure 7-11
Page 485 and 486:
TM 1-1520-240-10 c. Estimated Data.
Page 488 and 489:
SECTION II. CONTINGENCY TORQUE AVAI
Page 490 and 491:
SECTION III. MAXIMUM TORQUE AVAILAB
Page 492:
Figure 7A-3-2. Intermediate Torque
Page 495 and 496:
TM 1-1520-240-10 7A-4-2 Figure 7A-4
Page 497 and 498:
TM 1-1520-240-10 7A-5-2 Figure 7A-5
Page 500 and 501:
7A-6-1. Description. The takeoff ch
Page 502 and 503:
7A-7-1. Description. The cruise cha
Page 504 and 505:
Page 506 and 507:
Page 508 and 509:
Figure 7A-7-1. Example Cruise Chart
Page 510 and 511:
Figure 7A-7-3. 98 and 100% Rotor RP
Page 512 and 513:
Figure 7A-7-5. 98 and 100% Rotor RP
Page 514 and 515:
Figure 7A-7-7. 100% Rotor RPM, 10 a
Page 516 and 517:
Figure 7A-7-9. 100% Rotor RPM, 50C,
Page 518 and 519:
Figure 7A-7-11. 98 and 100% Rotor R
Page 520 and 521:
Page 522 and 523:
Figure 7A-7-15. 100% Rotor RPM, 10
Page 524 and 525:
Figure 7A-25. Figure 7A-7-17. 100%
Page 526 and 527:
Page 528 and 529:
Page 530 and 531:
Page 532 and 533:
Figure 7A-7-25. 100% Rotor RPM, 50C
Page 534 and 535:
Figure 7A-36. Figure 7A-7-27. 98 an
Page 536 and 537:
Page 538 and 539:
Page 540 and 541:
Page 542 and 543:
Page 544 and 545:
Figure 7A-46. Figure 7A-7-37. 98 an
Page 546 and 547:
Page 548 and 549:
Page 550 and 551:
Page 552 and 553:
Page 554 and 555:
Page 556 and 557:
Page 558 and 559:
Page 560 and 561:
Page 562 and 563:
Page 564 and 565:
Page 566 and 567:
Page 568 and 569:
Page 570 and 571:
Page 572 and 573:
Page 574 and 575:
Page 576 and 577:
Page 578 and 579:
Page 580 and 581:
Page 582 and 583:
Page 584 and 585:
Figure 7A-7-77. 100% Rotor RPM, -10
Page 586 and 587:
Page 588 and 589: Figure 7A-7-81. 98 and 100% Rotor R
Page 590 and 591: Figure 7A-7-83. 100% Rotor RPM, -10
Page 592 and 593: 7A-8-1. Description. The drag chart
Page 594 and 595: 7A-9-1. Description. a. Climb and d
Page 596 and 597: Figure 7A-9-2. Climb Performance (S
Page 598 and 599: 7A-10-1. Description. The idle fuel
Page 600: Figure 7A-10-2. Single Engine Fuel
Page 603 and 604: TM 1-1520-240-10 7A-11-2 Figure 7A-
Page 605 and 606: TM 1-1520-240-10 d. Normal Procedur
Page 607 and 608: TM 1-1520-240-10 8-2-2 * 6. Forward
Page 609 and 610: TM 1-1520-240-10 8-2-4 18. 714A P3
Page 611 and 612: TM 1-1520-240-10 8-2-6 15. Upper bo
Page 613 and 614: TM 1-1520-240-10 8-2-8 * 20. Cyclic
Page 615 and 616: TM 1-1520-240-10 8-2-10 * 38. GEN 1
Page 617 and 618: TM 1-1520-240-10 8-2-12 Figure 8-2-
Page 619 and 620: TM 1-1520-240-10 Takeoff over water
Page 621 and 622: TM 1-1520-240-10 8-2-16 14. PWR XFE
Page 624 and 625: 8-3-1. General. The flight characte
Page 626 and 627: SECTION IV. ADVERSE ENVIRONMENTAL C
Page 628 and 629: 8-4-17. Before Leaving Helicopter.
Page 630: operating in these conditions, shou
Page 633 and 634: TM 1-1520-240-10 nals will be used
Page 635 and 636: TM 1-1520-240-10 9-1-4 EMERGENCY EX
Page 637: TM 1-1520-240-10 9-1-10. Dual Engin
Page 641 and 642: TM 1-1520-240-10 Figure 9-1-4. 712
Page 643 and 644: TM 1-1520-240-10 Figure 9-1-6. 714A
Page 645 and 646: TM 1-1520-240-10 Figure 9-1-6. 714A
Page 647 and 648: TM 1-1520-240-10 9-1-16 Figure 9-1-
Page 649 and 650: TM 1-1520-240-10 2. ENG COND lever
Page 651 and 652: TM 1-1520-240-10 9-1-28. Engine Shu
Page 653 and 654: TM 1-1520-240-10 9-1-40. 714A Torqu
Page 655 and 656: TM 1-1520-240-10 9-1-54. FUEL LOW a
Page 657 and 658: TM 1-1520-240-10 9-1-65. Emergency
Page 659 and 660: TM 1-1520-240-10 9-1-73. Flight Con
Page 662 and 663: 9-2-1. ARMAMENT 9-2-2. Armament Sub
Page 664 and 665: Figure FO-1. General Arrangement (S
Page 666 and 667: DC ALE 47 DCDU 5 10 NO.1 SEQ NO.2 S
Page 668 and 669: Figure FO-4. DC Power Supply (Typic
Page 670 and 671: EAPS 1 FAN EAPS 2 FAN Figure FO-6.
Page 672: APPENDIX A REFERENCES TM 1-1520-240
Page 675 and 676: TM 1-1520-240-10 ABBREVIATION TERM
Page 677 and 678: TM 1-1520-240-10 ABBREVIATION TERM
Page 679 and 680: TM 1-1520-240-10 APPENDIX C CONDITI
Page 681: CONDITION 2408-13-1 ENTRY REQUIRED
Page 684 and 685: TM 1-1520-240-10 Subject Paragraph,
Page 686 and 687: TM 1-1520-240-10 Subject Paragraph,
Page 688 and 689:
TM 1-1520-240-10 Subject Paragraph,
Page 690 and 691:
Page 692 and 693:
Page 694 and 695:
Page 696 and 697:
Page 698 and 699:
Page 700 and 701:
Page 703:
By Order of the Secretary of the Ar
Page 707 and 708:
RECOMMENDED CHANGES TO PUBLICATIONS
Page 709 and 710:
Page 711 and 712:
Page 713 and 714:
The Metric System and Equivalents L
show all

tm 1-1520-240-10 technical manual operator's manual for army ch ...

Create successful ePaper yourself

Delete template?

Save as template?