Automatic Pilot Mechanisms and Airborne Gyro Components: 207438-2, 20868, 209-074-084-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 207438-2 2074382 | 6615-00-390-5965 | Pivot | Kearfott Corporation (88818) | ||
| 207438-5 2074385 | 6615-00-511-3369 | Pivot, Bearing, Steel | General Characteristics Item Description: Used on control, directional autopilot, P/N 423040-2 III Fsc Application Data: Control, directional autopilot, P/N 423040-2 | Kearfott Corporation (88818) | |
| 207515-1 2075151 | 6615-01-494-3989 | Gyroscope, Displacement | III End Item Identification: Used on sapphire aircraft thermal imaging camera | Flir Systems Inc. (64869) | |
| 207695-00 20769500 | 6615-01-381-1515 | Gyroscope, Rate | Wheel Power Method: Electric Elastic Restraint Application Method: Electric | Atlantic Inertial Systems Inc. (63395) | |
| 207780-01 20778001 | 6615-01-354-1340 | Gyroscope, Rate | III End Item Identification: C130;AWADS radar b kit Special Features: Rotor speed 24, 000 rpm;single axis;weight 6 oz. max Overall Length: 2.025 inches nominal | Atlantic Inertial Systems Inc. (63395) DRS Sustainment Systems Inc. (20418) | |
| 20807 | 6615-00-967-3680 | Parts kit, Actuator, | Woodward HRT (0HMS1) | ||
| 20808 | 6615-00-967-3677 | Parts kit, Actuator, | Cadillac Gage Textron Inc. (10237) | ||
| 20868 | 6615-00-996-1354 | Gate, Damper, Gyroscope | General Characteristics Item Description: Brass per QQ&B&626, 0.592 in. lg, 0.249 to 0.250 in. W, 0.136 to 0.138 in. H III Fsc Application Data: Automatic flight control system | Atlantic Inertial Systems Inc. (24321,63395) Whittaker Controls Inc. (79318) | |
| 2088412-1 20884121 | 6615-00-682-5121 | Servo Motor Damping | Honeywell International Inc. (27914) Raytheon Company (06845) | ||
| 2090 | 6615-00-795-0928 | Rack Assembly, Equip | Federal Shock Mount Corp. (97970) | ||
| 209-001-726-1 2090017261 | 6615-00-927-7354 | Stop, Stabilization | Bell Helicopter Textron Inc. (97499) | ||
| 20905G1 | 6615-00-163-9549 | Accelerometer, Electrical, Linear | III Fsc Application Data: Automatic flight control system, aircraft Overall Length: 2.660 inches nominal Overall Width: 1.570 inches maximum | BAE Systems Information And (94117) | |
| 209-074-080-103 209074080103 | 6615-01-079-3529 | Amplifier unit | Bell Helicopter Textron Inc. (97499) | ||
| 209-074-081-115 209074081115 | 6615-01-079-3530 | Module Assembly, Pit | Bell Helicopter Textron Inc. (97499) | ||
| 209-074-081-117 209074081117 | 6615-01-078-1980 | Module Assembly, Rol | Bell Helicopter Textron Inc. (97499) | ||
| 209-074-081-119 209074081119 | 6615-01-078-1981 | Module Assembly, Yaw | Bell Helicopter Textron Inc. (97499) | ||
| 209-074-081-121 209074081121 | 6615-01-300-4522 | Sensor, Amplifier, Pitch | III End Item Identification: Helicopter model H-1 | Bell Helicopter Textron Inc. (97499) | |
| 209-074-081-123 209074081123 | 6615-01-256-8171 | Sensor, Amplifier, Roll | III End Item Identification: Helicopter model H-1 | Bell Helicopter Textron Inc. (97499) | |
| 209-074-081-125 209074081125 | 6615-01-256-8172 | Sensor, Amplifier, Yaw | III End Item Identification: Helicopter model H-1 | Bell Helicopter Textron Inc. (97499) | |
| 209-074-084-1 2090740841 | 6615-01-119-9261 | Control, Rate | Bell Helicopter Textron Inc. (97499) |