Navigational Instruments: 2ZKH43070-0006, 34201682-002, 34209200-W0S5-001
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2ZKH43070-0006 2ZKH430700006 | 6605-01-649-4274 | Sensor, Inertial System Navigatio | III End Item Identification: F-35 aircraft Criticality Code Justification: FEAT III Part Name Assigned BY Controlling Agency: Device installion internal navagtion system | Northrop Grumman Systems Corporation (76823) | |
| 311875-1N43 3118751N43 | 6605-01-645-4698 | Inertial Reference Unit, Navigati | Overall Height: 3.35 inches nominal III End Item Identification: AN/AAS-53 | ||
| 311875-2002 3118752002 | 6605-01-633-2871 | Inertial Navigation System | III End Item Identification: DB100 imu gyro III Part Name Assigned BY Controlling Agency: Measurement unit, inertial | Goodrich Corporation (05WL4) | |
| 311875-4NB4 3118754NB4 | 6605-01-647-9017 | Inertial Navigation Unit | III End Item Identification: AN/AAS-53 | ||
| 311898-01-2000-0002-1-00000 3118980120000002100000 | 6605-01-640-8893 | Global Positioning System-Inerti | |||
| 311898-11-0800-0121-1-USASD 31189811080001211USASD | 6605-01-631-9064 | Inertial Navigation Unit | |||
| 311898-11-0800-123-1-USASD 3118981108001231USASD | 6605-01-648-4124 | Global Positioning System-Inerti | III End Item Identification: MQ-4C broad area maritime surveillance III Part Name Assigned BY Controlling Agency: LN-251 ins/gps navi | ||
| 311925-100F 311925100F | 6605-01-626-1188 | Inertial Navigation System | End Item Identification: F-22 aircraft (radar system installation) 4TH gen Part Name Assigned BY Controlling Agency: Inertial navigation | ||
| 312ST | 6605-00-952-4497 | Standard Weight too | Special Features: One case, one forceps, 12 weights from 1 gram to 500 grams stainless steel | Henry Troemner LLC (60836) | |
| 318-1182 3181182 | 6605-01-595-4842 | Sensor Gp-Speed | End Item Identification: Truck, dump transmission group | Caterpillar Inc. (11083) | |
| 32011 | 6605-01-628-6187 | Compass, Magnetic, Mounted | Special Features: Magnetic reflector compass binnacle | Lyman Baker & Company Inc. (54121) | |
| 34200303-110 34200303110 | 6605-01-629-3871 | Inertial Navigation Unit | Honeywell International Inc. (0BFA5) | ||
| 34200304-202 34200304202 | 6605-01-629-3870 | Sensor, Inertial System Navigatio | Honeywell International Inc. (0BFA5) | ||
| 34200550-0003 342005500003 | 6605-01-418-3279 | Inertial Navigation System | End Item Identification: V-22 aircraft Criticality Code Justification: FEAT Special Features: Essential to weapon system performance or operation or the preservation of life or safety of operating personnel. | Honeywell International Inc. (0BFA5) | |
| 34200750-M042-025 34200750M042025 | 6605-01-628-9027 | Global Positioning System-Inerti | III End Item Identification: F-15SA III Part Name Assigned BY Controlling Agency: Embedded gps inerti | Honeywell International Inc. (0BFA5) | |
| 34200750-M41-009 34200750M41009 | 6605-01-649-8126 | Inertial Navigation Unit | Honeywell International Inc. (0BFA5) | ||
| 34200750-R041-009 34200750R041009 | 6605-01-648-9988 | Inertial Navigation Unit | Actuation Method: Any acceptable Contact Type: Any acceptable Mechanical Connection Type: Any acceptable | Honeywell International Inc. (0BFA5) | |
| 34200800-3075A 342008003075A | 6605-01-631-0446 | Inertial Navigation Unit | Honeywell International Inc. (0BFA5) | ||
| 34201682-002 34201682002 | 6605-01-633-4824 | Sensor, Inertial System Navigatio | Honeywell International Inc. (0BFA5) | ||
| 34209200-W0S5-001 34209200W0S5001 | 6605-01-641-2935 | Embedded, Gps, Ins | Honeywell International Inc. (0BFA5) |