Automatic Pilot Mechanisms and Airborne Gyro Components: 8503422-901, 8519-02, 852D158G2
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 8503422-901 8503422901 | 6615-01-225-8140 | Drum and Housing Assembly | Honeywell International Inc. (07187) | ||
| 8503423-901 8503423901 | 6615-01-226-1012 | Trim Actuator | Honeywell International Inc. (07187) | ||
| 8511364 | 6615-00-621-3018 | Gyroscope, Rate | U S Army Aviation and Missile (18876) | ||
| 8519-02 851902 | 6615-00-943-7866 | Frame Assy, Gyro | Parker-Hannifin Corporation (93835) | ||
| 8519535-901 8519535901 | 6615-01-408-9403 | Controller, Flight, Automatic Pilo | III End Item Identification: C130H acft | Honeywell International Inc. (07187) | |
| 8519540-901 8519540901 | 6615-01-408-9405 | Controller, Flight, Automatic Pilo | III End Item Identification: C130H acft | Honeywell International Inc. (07187) | |
| 8519600-903 8519600903 | 6615-01-588-0704 | Processor, Flight Control | III End Item Identification: C130 hercules Special Features: Used on the rnzaf C-130LEP III Part Name Assigned By Controlling Agency: System processor | Honeywell International Inc. (07187) | |
| 8519930-901 8519930901 | 6615-01-423-7489 | Controller, Flight, Automatic Pilo | III End Item Identification: Aircraft, lockheed corp, model C130H | Honeywell International Inc. (07187) | |
| 851D675G3 | 6615-00-978-2115 | Stator, Pickoff | General Characteristics Item Description: Contains 1 housing, stator; 1 shield, coil; 1 insulator, disk; 1 winding, pickoff; 1 insulation sleeve | BAE Systems Controls Inc. (89954) | |
| 851D850G1 | 6615-00-836-5359 | Network, Single Shot | BAE Systems Controls Inc. (89954) | ||
| 851D868G1 | 6615-00-980-8537 | Network, Attenuator | General Characteristics Item Description: 1.175 in. lg; 0.765 in. h; 0.575 in. w; C/O resistor 13; wiring board comp 2; shell, electrical | BAE Systems Controls Inc. (89954) | |
| 8520113-901 8520113901 | 6615-01-394-1818 | Processor, Signal, Sp | III End Item Identification: CH-47D; chinook helicopter Special Features: Service bulletin 145-46-1005; to correct potential power up problem III Part Name Assigned By Controlling Agency: Torque cruise and rpm display; tcrd | Honeywell International Inc. (07187) | |
| 8520113-904 8520113904 | 6615-01-394-1818 | Processor, Signal, Sp | III End Item Identification: CH-47D; chinook helicopter Special Features: Service bulletin 145-46-1005; to correct potential power up problem III Part Name Assigned By Controlling Agency: Torque cruise and rpm display; tcrd | Honeywell International Inc. (07187) | |
| 852106 | 6615-00-604-3158 | Magnet Assy | Honeywell International Inc. (07187) Lockheed Martin Corporation (56232) | ||
| 8523791 | 6615-01-490-3637 | Drum Housing | III End Item Identification: Aircraft, stratolifter C-135 Special Features: Item is subassembly of nsn 6615-01-225-8140 (drum and housing assembly); material: aluminum alloy plate, 6061-T651, QQ-A-250/11 Overall Length: 3.450 inches nominal | Honeywell International Inc. (07187) | |
| 85254320080 | 6615-00-612-6743 | Cover Assy | Kollsman Inc. (89944) | ||
| 8527198-901 8527198901 | 6615-01-483-3217 | Processor, Flight Control | III End Item Identification: C-130J aircraft III Reference Data and Literature: 1C-130J-4-22-1 fig 3 index 10 III Relationship to Similar Equipment: Replaces 6615-01-483-3220 after tcto 1C-130J-660 | Honeywell International Inc. (07187) | |
| 8527198-902 8527198902 | 6615-01-483-3217 | Processor, Flight Control | III End Item Identification: C-130J aircraft III Reference Data and Literature: 1C-130J-4-22-1 fig 3 index 10 III Relationship to Similar Equipment: Replaces 6615-01-483-3220 after tcto 1C-130J-660 | Honeywell International Inc. (07187) | |
| 852754 | 6615-01-376-4012 | Gyroscope, Rate | Northrop Grumman Guidance And (06481) | ||
| 852D158G2 | 6615-00-972-0900 | Pendulum, Accelerome | BAE Systems Controls Inc. (89954) |