Navigational Instruments: 600556, 600559, 6010821
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 600556 | 6605-00-871-9234 | Gimbal, Outer Roll | Northrop Grumman Guidance And (06481) | ||
| 600559 | 6605-00-345-3512 | Retainer, Index and | TRW Inc. (13799) | ||
| 600563 | 6605-00-321-3371 | Lens, Driftmeter | TRW Inc. (13799) | ||
| 600570 | 6605-00-673-6396 | Gear Assy | Northrop Grumman Guidance And (06481) | ||
| 600585 | 6605-00-070-0326 | Lamp Assy | TRW Inc. (13799) | ||
| 600619 | 6605-00-031-8472 | Handle | TRW Inc. (13799) | ||
| 600646 | 6605-00-673-6371 | Lead Assy | Northrop Grumman Guidance And (06481) | ||
| 600659-01 60065901 | 6605-00-694-0053 | Shield Assy | GE Aviation Systems LLC (35351) | ||
| 600667 | 6605-00-673-6364 | Adapter, Plate | Northrop Grumman Guidance And (06481) | ||
| 600723 | 6605-00-815-7797 | Gimbal, Pitch | Northrop Grumman Guidance And (06481) | ||
| 600731 | 6605-00-076-2469 | Clip, Spring | Northrop Grumman Guidance And (06481) | ||
| 600732-01 60073201 | 6605-00-694-0070 | Panel, Front Control | GE Aviation Systems LLC (35351) | ||
| 600748 | 6605-00-509-7964 | Cover, Pedestal Case | TRW Inc. (13799) | ||
| 600752-01 60075201 | 6605-00-694-0071 | Dust Cover Assy | GE Aviation Systems LLC (35351) | ||
| 600768-01 60076801 | 6605-00-694-0077 | Base, Amplifier Moun | GE Aviation Systems LLC (35351) | ||
| 600776 | 6605-00-328-8771 | Housing, Upper Lens | TRW Inc. (13799) | ||
| 600780 | 6605-00-031-8479 | Brush and Block Ass | TRW Inc. (13799) | ||
| 600786-1 6007861 | 6605-00-987-7688 | Brake | Tally Printer Corporation (12344) | ||
| 600930 | 6605-00-031-8488 | Pulley-Gear Asy | TRW Inc. (13799) | ||
| 6010821 | 6605-01-025-1271 | Transmitter, Induction Compass | III End Item Identification: Beech 300 acft & CC144 challengertransport acft III Functional Description: The "flux valve" is a magnetic azimuth detector that senses the direction of the horizontal component of the earth's magnetic field relative to thelongitudinal axis of the acft and converts info to an electrical signal which when applied to the gyro, maintains continuous alignment to the actual mag heading, resulting in drift-free heading reference, self-maintained to an accuracy of porm 2 degrees Criticality Code Justification: SUPP | Embraer - Empresa Brasileira DE (001JK) Embraer Empresa Brasileira DE (S4956) |