NAVIGATIONAL INSTRUMENTS AVIONICS Parts 6605-01-128-5258 through 6605-01-131-0447 |
|
|
| Leading Edge Sourcing Services |
 |
|
We solve sourcing challenges for parts like 6605-01-128-5258, 6605-01-128-5259, 6605-01-128-5260, 6605-01-128-5279, 6605-01-128-5407, 6605-01-128-7226, 6605-01-128-9225, 6605-01-128-9226, 6605-01-128-9227, 6605-01-128-9228 -- hard to find, long lead time, and obsolete part requirements.
|
 |
|
|
<<< 401 402 403 404 405 406 407 408 409 410 411 412 413 414 415 416 417 418 419 420 421 422 423 424 425 426 427 428 429 430 431 432 433 434 435 436 437 438 439 440 441 442 443 444 445 446 447 448 449 450 451 452 453 454 455 456 457 458 459 460 461 462 463 464 465 466 467 468 469 470 471 472 473 474 475 476 477 478 479 480 481 482 483 484 485 486 487 488 489 490 491 492 493 494 495 496 497 498 499 500 >>>
|
| Part number | Description | Category | Details |
6605-01-128-5258 | DISPLAY MODULE | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | QUALITY ASSURANCE PER MIL-Q-21549B-SP-1 |
6605-01-128-5259 | AMPLIFIER | | |
6605-01-128-5260 | SWITCH, T R | | |
6605-01-128-5279 | KEYER | | |
6605-01-128-5407 | TRACER, DEAD RECKONING | | |
6605-01-128-7226 | SUPPORT, WEDGE | GENERAL CHARACTERISTICS ITEM DESCRIPTION | USED IN THE GAP BETWEEN THE HEAD-UP DISPLAY INSTALLATION & THE F-16 AIRCRAFT STRUCTURE; GUIDE PINS IN HEAD-UP DISPLAY SHALL CLEAR INSTRUMENT PANEL BY 0.070 IN. MIN |
6605-01-128-9225 | PLATE, DRIVE | SPECIAL TEST FEATURES | MIL-Q-21549B-SP24-1 |
6605-01-128-9226 | HARNESS ASSEMBLY | SPECIAL TEST FEATURES | MIL-Q-21549B-SP24-1 |
6605-01-128-9227 | CHANNEL, SUPPORT | SPECIAL TEST FEATURES | MIL-Q-21549B-SP24-1 |
6605-01-128-9228 | CHANNEL, SUPPORT | SPECIAL TEST FEATURES | MIL-Q-21549B-SP24-1 |
6605-01-128-9923 | HANDLE ASSEMBLY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | MIL-Q-21549B-SP24-1 |
6605-01-128-9924 | CLEAT | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | MIL-Q-21549B-SP24-1 |
6605-01-129-2887 | PROTECTOR, ELECTROMAGNETIC | GENERAL CHARACTERISTICS ITEM DESCRIPTION | INCLUDES NUCLEAR CRITICAL HARDNESS ITEMS:ENCLOSURE R/N 7563452-011(1) CIRCUIT CARD ASSY R/N 80-26021-001(1) CONDUIT ASSY,SHIELDED R/N 7563779-001(1); W/ CONNECTOR,ELEC,PLUG R/N MS3476L18-32S(1) CONNECTOR,RECEPT R/N MS3122E18-32PY(1) |
6605-01-129-9565 | COMPASS HOLDER ASSE | | |
6605-01-129-9566 | SIGHT HOLDER | | |
6605-01-129-9567 | HOLDER, COMPASS | | |
6605-01-129-9573 | SIGHT ASSEMBLY, REAR | | |
6605-01-130-0018 | MOUNTING FOOT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CONSISTS OF STEEL BAR ROUND,0.562 IN. DIA,6.375 IN. LONG,ONE END THREADED 0.438 IN.-14 UNC,THREAD 0.375 IN. LONG |
6605-01-130-0021 | ADAPTER, RESOLVER | SPECIAL TEST FEATURES | MIL-Q-21549B-SP24-1 |
6605-01-130-0022 | ADAPTER, MOTOR | SPECIAL TEST FEATURES | MIL-Q-21549B-SP24-1 |
6605-01-130-4414 | BOX, CONNECTOR | | |
6605-01-130-4415 | GIMBAL, OUTER | | |
6605-01-130-6884 | WIRING HARNESS, BRANCHED | SPECIAL FEATURES | C/O WIRE,AWG 20,R/N 7553937-004,1; WIRE,AWG 26,R/N 7553937-001,1; WIRE,20 AWG,R/N 7553937-004,1; WIRING HARNESS,R/N 7888400-031 OR 7886581-11,1; PIN CONTACT,R/N 8597807-001,1; MARKER SLEEVE,R/N 8595296-172,1; LACING TAPE,R/N 7553937-002 |
6605-01-131-0446 | LENS, INDEX | III END ITEM IDENTIFICATION | AIRCRAFT MODEL F-18 |
6605-01-131-0447 | PACKER | III END ITEM IDENTIFICATION | AIRCRAFT MODEL F-18 |