Navigational Instruments: 662-404C, 663570-03, 66413-507-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 662-404C 662404C | 6605-00-474-4954 | Housing, Control cab | Elgin National Industries Inc. (20209) | ||
| 662433 | 6605-00-994-0194 | Computer, Navigational | Phase: Three Frequency in Hertz: 400.0 Power Source: External | Northrop Grumman Guidance And (06481) | |
| 662437 | 6605-00-994-0195 | Computer Subassembly | Special Features: Major components: card guide 1; circuit card assembly 4; fan, axial 1; filter assembly 1; generator, reference signal 1; meter, time totalizing 5 End Item Identification: Computer, navigation; R/N 662433 and CP-733/ASN; 6605-00-994-0194 Component Type and Quantity: 3 capacitor and 1 chassis and 1 cover and 9 diode and 1 filter and 1 housing and 1 panel and 25 relay and 1 solenoid | Northrop Grumman Guidance And (06481) | |
| 66252-502-11 6625250211 | 6605-00-140-0879 | Amplifier, Electronic Control | Boeing Company, The (94756) | ||
| 662896 | 6605-00-032-0413 | Stator Asy | Lockheed Martin Corporation (56232) | ||
| 662910-2 6629102 | 6605-01-096-8659 | Gyro, Upper, Fine | Northrop Grumman Guidance And (06481) | ||
| 663126 | 6605-01-467-0345 | Compass, Magnetic, Unmounted | III End Item Identification: 5895014350571 Design Type: Top reading Instrument Type: DRY | Vectronix Inc. (7Z946) | |
| 663450-08 66345008 | 6605-00-124-9419 | Inertial Navigation | General Characteristics Item Description: Operating power requirements 115V ac, 400 hz, single phase, outputs 28V dc, initial 1704 W, long term 615 W | Litton Systems Inc. (30782) | |
| 663450-100-01 66345010001 | 6605-00-124-9419 | Inertial Navigation | General Characteristics Item Description: Operating power requirements 115V ac, 400 hz, single phase, outputs 28V dc, initial 1704 W, long term 615 W | Litton Systems Inc. (30782) | |
| 663454-0001-700 6634540001700 | 6605-01-550-7729 | Computer Subassembly | End Item Identification: LTN-58 inu, subassembly, gimbal | Litton Systems Inc. (30782) Northrop Grumman Guidance And (06481) | |
| 66-346 66346 | 6605-00-659-8775 | Counter Assembly, Electronic, Digi | Lockheed Martin Corporation (56232) | ||
| 663550-04-01 6635500401 | 6605-00-124-9447 | Display unit, Contro | General Characteristics Item Description: Operating power requirement 28V dc, output 5V dc | Litton Systems Inc. (30782) | |
| 66355-507-1 663555071 | 6605-00-926-4381 | Network, Voltage Sustaining | Boeing Company, The (94756) | ||
| 663570-03 66357003 | 6605-00-165-5888 | Mode Selector unit | Litton Systems Inc. (30782) | ||
| 663599 | 6605-01-117-1744 | Mounting Block, Gyro | General Characteristics Item Description: Material aluminum alloy A356 casting; 1.670 in. H | Northrop Grumman Guidance And (06481) | |
| 663814 | 6605-01-116-1664 | Stop, Gyro | Northrop Grumman Guidance And (06481) | ||
| 663819-01-01 6638190101 | 6605-01-034-8738 | Display unit, Remote | III End Item Identification: Aircraft model EP-3E | Litton Systems Inc. (30782) | |
| 66402-308-41 6640230841 | 6605-01-141-1013 | Integrator, Accelerometer | General Characteristics Item Description: C/O disk, R/N 66393-308-1, 1; magnet, R/N 475-0213-001, 1; support, R/N 66542-308-1, 1; encoder, R/N 66610-308-1, 1; shaft, R/N 66389-308-3, 1; motor, R/N 467-0110-002, 1 III Fsc Application Data: D220 mark ii inertial reference unit | Boeing Company, The (94756) | |
| 66412-308-1 664123081 | 6605-00-476-9376 | Septum, Fluid Separation | General Characteristics Item Description: Used on stable platform assy, TO5N24&6&4 III Fsc Application Data: Airborne inertial navigation system | Boeing Company, The (94756) | |
| 66413-507-1 664135071 | 6605-00-926-6917 | Converter, Temperature Data | Boeing Company, The (94756) |