Automatic Pilot Mechanisms and Airborne Gyro Components: 6615PL1014684, 6615PL1619849, 84885
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
6615PL1014684 | 6615-01-329-0949 | Accelerometer, Electrical, Linear | End Item Identification: Used on C5 and C130 aircraft | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
6615PL1037319 | 6615-01-101-1884 | Indicator Light Assembly | General Characteristics Item Description: Lights 9; lamps 9; black opaque letters; cres body; 4.250 in. lg max; 3.270 in. w; 1.140 in. H | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
6615PL1073783 | 6615-01-060-6839 | Cable Assembly, Grip, Force Transd | End Item Identification: F-16 acft General Characteristics Item Description: 22.00 in. lg | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
6615PL1619849 | 6615-01-042-7834 | Gyroscope, Rate | End Item Identification: F-16 acft Special Features: Manufacturers name: rate gyroscope assembly, flight control | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
6615PL1619872 | 6615-01-129-7445 | Panel, Manual Trim | End Item Identification: F-16 a/b acft Special Features: Manufacturers name: manual trim panel assembly Functional Description: A line replaceable unit of the flight control system which provides 4 identical trim commands for pitch, roll and yaw to the flight control computer | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
6615PL1630760 | 6615-00-137-6038 | Gyroscope, Rate | Overall Length: 5.195 inches nominal Overall Height: 2.872 inches nominal Overall Width: 2.890 inches nominal | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
6615PL1630763 | 6615-01-073-9442 | Panel Assembly, Indicating, Light | End Item Identification: F-16 acft General Characteristics Item Description: Contains panel 2, glass 1; panel matl plastic, MIL-P-5425; glass matl per DD-G-451 | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
7000260-503 7000260503 | 6615-01-689-7410 | Servocylinder | End Item Identification: G550 aircraft Part Name Assigned BY Controlling Agency: Servo drive assembly aw-ps critical | ||
70410-22760-056 7041022760056 | 6615-01-650-8979 | Nrp, Pitch Trim Serv | End Item Identification: Mark III helicopters (SH-60B) | Sikorsky Aircraft Corporation (78286) | |
71550-25003-042 7155025003042 | 6615-01-621-4312 | Nrp, Accl Pgtl Assy | Part Name Assigned BY Controlling Agency: Pigtail assembly accelerometer | Sikorsky Aircraft Corporation (78286) | |
71550-25003-043 7155025003043 | 6615-01-621-4313 | Nrp, Accl Pgtl Assy | End Item Identification: MH-60R helicopter Part Name Assigned BY Controlling Agency: Pigtail assembly accelerometer | Sikorsky Aircraft Corporation (78286) | |
724E2301-1 724E23011 | 6615-01-687-3238 | Overhead Panel | End Item Identification: CH-47F(SG) helicopter Part Name Assigned BY Controlling Agency: Copilot/overhead panel lighting control panel assembly | The Boeing Company (77272) | |
724ES028-3 724ES0283 | 6615-01-687-2243 | Controller, Flight, Automatic Pilo | End Item Identification: CH-47F(SG) helicopter Part Name Assigned BY Controlling Agency: Cyclic control grip | The Boeing Company (77272) | |
724VS100-17 724VS10017 | 6615-01-687-2565 | Computer, Flight Control | End Item Identification: CH-47F(SG) helicopter Part Name Assigned BY Controlling Agency: Digital afcs computer | The Boeing Company (77272) | |
79728 | 6615-01-647-6888 | Computer, Flight Control | Special Features: Computer, flight control: aecv puma ii waterproof ddl M1 avionics with saasm gps module. the M1 avionics module provides aircraft and payload control and aircraft and payload data responses to and from the ground control station by means of digital data links on oconus operating frequencies. the internal saasm gps module serial number must be reported to the lcsm if lost or destroyed. | Aerovironment Inc. (3SQS9) | |
799-7714 7997714 | 6615-01-690-1284 | Controller, Flight, Automatic Pilo | Part Name Assigned BY Controlling Agency: Controller, flight, automatic pilot | Mason Electric Company (81579) | |
81384 | 6615-01-647-6888 | Computer, Flight Control | Special Features: Computer, flight control: aecv puma ii waterproof ddl M1 avionics with saasm gps module. the M1 avionics module provides aircraft and payload control and aircraft and payload data responses to and from the ground control station by means of digital data links on oconus operating frequencies. the internal saasm gps module serial number must be reported to the lcsm if lost or destroyed. | Aerovironment Inc. (3SQS9,60107) | |
84233 | 6615-01-677-0501 | Computer, Flight Control | Part Name Assigned BY Controlling Agency: Assy, waterproof avionics, dk saasm type ii, M3/M4 nato, | Aerovironment Inc. (3SQS9) | |
844E2303-1 844E23031 | 6615-01-687-3239 | Center Panel | End Item Identification: CH-47F(SG) helicopter Part Name Assigned BY Controlling Agency: Assembly - pilot/center instrument lighting control panel | The Boeing Company (77272) | |
84885 | 6615-01-676-8449 | Computer, Flight Control | Part Name Assigned BY Controlling Agency: Clutch, shaft assembly | Aerovironment Inc. (3SQS9) |