Navigational Instruments: 34200750-R041-205, 34200750-R401-960, 34201300-3C88
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 34200750-R041-205 34200750R041205 | 6605-01-568-9244 | Inertial Navigation System | Honeywell International Inc. (0BFA5) | ||
| 34200750-R041-960 34200750R041960 | 6605-01-511-3424 | Inertial Navigation unit | III End Item Identification: F-15 aircraft Special Features: Contains 3 ring laser gyros; 3 accelerometers in a strap down configuration, embedded global postion reciever, 1553/B mutiplex bus, built in test, F-15 avionics interface card Overall Length: 7.000 inches nominal | Honeywell International Inc. (0BFA5) | |
| 34200750-R401-960 34200750R401960 | 6605-01-511-3424 | Inertial Navigation unit | III End Item Identification: F-15 aircraft Special Features: Contains 3 ring laser gyros; 3 accelerometers in a strap down configuration, embedded global postion reciever, 1553/B mutiplex bus, built in test, F-15 avionics interface card Overall Length: 7.000 inches nominal | Honeywell International Inc. (0BFA5) | |
| 34200800-3035-SM 342008003035SM | 6605-01-534-0467 | Inertial Navigation unit | III End Item Identification: C-130J Overall Width: 7.000 inches nominal Overall Height: 7.000 inches nominal | Honeywell International Inc. (0BFA5) | |
| 34200800-3035-SM-UK 342008003035SMUK | 6605-01-521-4430 | Inertial Navigation System | Honeywell International Inc. (0BFA5) | ||
| 34200800-3098SM 342008003098SM | 6605-01-524-9311 | Inertial Navigation unit | III End Item Identification: Hawk 127 aircraft Special Features: Technical maintenance plan 7069.018-7, reference 72-40-01/001 | Honeywell International Inc. (09128) | |
| 34200850 | 6605-01-455-0302 | Navigation set | Special Features: Embedded gps/ins (9.8 egi); platform breguet 1150 | Thales Avionics LTD (K0385) | |
| 34200850-300G 34200850300G | 6605-01-496-6507 | Inertial Navigation System | III End Item Identification: Aermacchi fighter trainer aircraft, model MB-339 | Honeywell International Inc. (0BFA5) | |
| 34200850-30J8 3420085030J8 | 6605-01-473-0551 | Inertial Navigation System | III Part Name Assigned By Controlling Agency: Embeded gps/ins (9.8 egi) Mounting Method: Lock pin Mounting point Quantity: 2 | Honeywell International Inc. (0BFA5) | |
| 34200850-3PK8 342008503PK8 | 6605-01-455-0302 | Navigation set | Special Features: Embedded gps/ins (9.8 egi); platform breguet 1150 | Honeywell International Inc. (0BFA5) Thales Avionics LTD (K0385) | |
| 34200850-800G 34200850800G | 6605-01-457-4652 | Inertial Navigation System | Special Features: Consists of: chassis, wired assy; top cover W/tether; cca; dcps module; isa; battery, lithium; assorted screw, washer, gasket, adhesive, tape, cement, label; gps antenna | Honeywell International Inc. (0BFA5) | |
| 34201300-2C83 342013002C83 | 6605-01-436-2790 | Inertial Navigation unit | Honeywell International Inc. (0BFA5) | ||
| 34201300-3C83 342013003C83 | 6605-01-436-2790 | Inertial Navigation unit | Honeywell International Inc. (0BFA5) | ||
| 34201300-3C84 342013003C84 | 6605-01-436-2790 | Inertial Navigation unit | Honeywell International Inc. (0BFA5) | ||
| 34201300-3C84 SM 342013003C84SM | 6605-01-436-2790 | Inertial Navigation unit | Honeywell International Inc. (0BFA5) | ||
| 34201300-3C85 342013003C85 | 6605-01-471-7257 | Inertial Navigation unit | Honeywell International Inc. (0BFA5) | ||
| 34201300-3C86 342013003C86 | 6605-01-478-2373 | Inertial Navigation unit | Honeywell International Inc. (0BFA5) | ||
| 34201300-3C86SM 342013003C86SM | 6605-01-478-2373 | Inertial Navigation unit | Honeywell International Inc. (0BFA5) | ||
| 34201300-3C87 342013003C87 | 6605-01-477-6564 | Inertial Navigation unit | Honeywell International Inc. (0BFA5) | ||
| 34201300-3C88 342013003C88 | 6605-01-479-1237 | Inertial Navigation unit | Honeywell International Inc. (0BFA5) |