Automatic Pilot Mechanisms and Airborne Gyro Components: 4Y91578-105A, 501-1160-01, 501-1494-01
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4Y91578-105A 4Y91578105A | 6615-00-072-6591 | Tube Assembly | Lockheed Martin Corporation (98897) | ||
| 4Y91578-109A 4Y91578109A | 6615-00-226-4622 | Tube Assembly, Eleva | Lockheed Martin Corporation (98897) | ||
| 4Y91578-111A 4Y91578111A | 6615-00-110-3062 | Tube Assembly, Eleva | Lockheed Martin Corporation (98897) | ||
| 5000 | 6615-00-187-1222 | Control, Directional, Automatic Pi | Power Source: External Maximum Overall Length: 12.000 inches Maximum Overall Width: 7.062 inches | Sigma TEK Inc. (86887) | |
| 50003 | 6615-01-266-7641 | Gyroscope, Displacement | Special Features: The gypo provides accurate pitch and roll displacement outputs to either an attitude indicator, an autopilot or both Overall Length: 6.600 inches nominal Overall Width: 4.000 inches nominal | Flightline Electronics Inc. (50027) | |
| 50003-1 500031 | 6615-01-266-7641 | Gyroscope, Displacement | Special Features: The gypo provides accurate pitch and roll displacement outputs to either an attitude indicator, an autopilot or both Overall Length: 6.600 inches nominal Overall Width: 4.000 inches nominal | Flightline Electronics Inc. (50027) | |
| 50003-1 500031 | 6615-01-484-1609 | Gyroscope, Displacement | III End Item Identification: CH-47-D chinook helicopter | The Boeing Company (77272) | |
| 5000B-14 5000B14 | 6615-01-149-0770 | Control, Directional, Automatic Pi | Power Source: External Inclosure Type: Encased Mounting Method: Bezel ring | Sigma TEK Inc. (86887) | |
| 500118 | 6615-00-332-8327 | Housing, Sensor Asse | III End Item Identification: 66152709344, F-15 General Characteristics Item Description: Aluminum alloy, finish, lusterless gray III Fsc Application Data: Controls, automatic pilot | Axsys Technologies Inc. (10112) Donel Systems LLC (98659) | |
| 501057 | 6615-00-199-8836 | Contact, Gyro | Technical Wire Products LLC (07700) | ||
| 501-1027-01 501102701 | 6615-00-877-9343 | Gyroscope, Rate | Special Features: Four pin electrical receptable bendix scintilla pt series, or equal; connector mates with scintilla type PT06P-8-4S, or equal Overall Length: 4.745 inches nominal Overall Width: 2.880 inches nominal | L-3 Communications Avionics Systems (25583) | |
| 501-1027-02 501102702 | 6615-01-371-7565 | Gyroscope, Rate | L-3 Communications Avionics Systems (25583) | ||
| 501-1105-03 501110503 | 6615-01-114-9281 | Gyroscope, Displacement | III End Item Identification: Sabre 80 aircraft | L-3 Communications Avionics Systems (25583) | |
| 501-1121-01 501112101 | 6615-01-554-3648 | Gyroscope, Displacement | L-3 Communications Avionics Systems (25583) | ||
| 501-113-01 50111301 | 6615-01-390-3206 | Gyroscope, Displacement | L-3 Communications Avionics Systems (25583) | ||
| 501-1135-01 501113501 | 6615-00-313-1579 | Gyroscope, Displacement | L-3 Communications Avionics Systems (25583) | ||
| 501-1160-01 501116001 | 6615-01-441-8337 | Gyro, Verticle | L-3 Communications Avionics Systems (25583) | ||
| 501-1210-01 501121001 | 6615-01-516-1072 | Gyroscope, Displacement | III Part Name Assigned By Controlling Agency: Vertical gyroscope | L-3 Communications Avionics Systems (25583) | |
| 501-1332-01 501133201 | 6615-01-125-6581 | Gyroscope, Displacement | Special Features: Mounting data - per SCS-413: design activity data: jet electronics and technology, inc. fscm 25583, P/N 501-1332-01; aircraft installed. funct desc: gyroscope develops electrical signals representative of aircraft attitude thru 360 deg roll and +/-82 deg pitch Overall Length: 6.600 inches nominal Overall Width: 4.000 inches nominal | L-3 Communications Avionics Systems (25583) | |
| 501-1453-01 501145301 | 6615-01-492-5112 | Gyroscope, Rate | L-3 Communications Avionics Systems (25583) | ||
| 501-1494-01 501149401 | 6615-01-258-6213 | Gyroscope, Displacement | L-3 Communications Avionics Systems (25583) |