Automatic Pilot Mechanisms and Airborne Gyro Components: 156738-01, 15704-1B2, 15711-2F
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 156738-01 15673801 | 6615-01-027-9731 | Mounting Base | III End Item Identification: A10AACFT | GE Aviation Systems LLC (35351) | |
| 15703-1A 157031A | 6615-00-223-0750 | Controller, Flight, Automatic Pilo | Frequency in Hertz: 400.0 Phase: Three Power Source: External | Honeywell Intl Inc. (55972) Honeywell Intl Inc. Defense Avionics (19315) | |
| 15703-2A 157032A | 6615-00-717-9042 | Controller, Flight, Automatic Pilo | Frequency in Hertz: 400.0 Phase: Three Power Source: External | Honeywell Intl Inc. (55972) Honeywell Intl Inc. Defense Avionics (19315) | |
| 157034-01-01 1570340101 | 6615-01-003-6464 | Servomotor, Automatic Pilot | III Fsc Application Data: Control, automatic pilot, A-10A Electrical Connection Quantity: 1 Contact Quantity: 23 | GE Aviation Systems LLC (35351) | |
| 15704-1A1 157041A1 | 6615-00-242-5869 | Controller, Flight, Automatic Pilo | Frequency in Hertz: 400.0 Phase: Three Power Source: External | Honeywell Intl Inc. (55972) Honeywell Intl Inc. Defense Avionics (19315) | |
| 15704-1A2 157041A2 | 6615-00-242-5869 | Controller, Flight, Automatic Pilo | Frequency in Hertz: 400.0 Phase: Three Power Source: External | Honeywell Intl Inc. (55972) Honeywell Intl Inc. Defense Avionics (19315) | |
| 15704-1B1 157041B1 | 6615-00-526-4851 | Controller, Flight, Automatic Pilo | Frequency in Hertz: 400.0 Phase: Single Power Source: External | Honeywell Intl Inc. (55972) Honeywell Intl Inc. Defense Avionics (19315) | |
| 15704-1B2 157041B2 | 6615-00-526-4851 | Controller, Flight, Automatic Pilo | Frequency in Hertz: 400.0 Phase: Single Power Source: External | Honeywell Intl Inc. (55972) Honeywell Intl Inc. Defense Avionics (19315) | |
| 157077-01 15707701 | 6615-01-007-4259 | Pickoff, Rotor | General Characteristics Item Description: Rotor housing 1, rotor assembly, 0.812 in.od III Fsc Application Data: Control, automatic pilot, A-10A | GE Aviation Systems LLC (35351) | |
| 157077-02 15707702 | 6615-01-007-4259 | Pickoff, Rotor | General Characteristics Item Description: Rotor housing 1, rotor assembly, 0.812 in.od III Fsc Application Data: Control, automatic pilot, A-10A | GE Aviation Systems LLC (09LX4,35351) | |
| 157080-02-02 1570800202 | 6615-01-134-6358 | Gyroscope, Vertical | III End Item Identification: H-531HELICOPTER | GE Aviation Systems LLC (35351) | |
| 157083-01 15708301 | 6615-01-010-3162 | Stator, Pickoff | III End Item Identification: Control, automatic pilot, A-10A General Characteristics Item Description: 1.49997 to 1.50000 in. od; 0.8200TO 0.8205 in. id; C/O retainer 1; stator assembly, wound 1 | GE Aviation Systems LLC (35351) | |
| 157090-01 15709001 | 6615-01-008-7136 | Torque Ring | III End Item Identification: Control, automatic pilot, A-10A General Characteristics Item Description: Material steel per QQ-S-698 or QQ-T-830; 2.575 in. od; 2.000 in. id; 0.605 in. w; contains ring torque 1; ring 1; copper plate od per MIL-C-14550; 4 holes 0.102 to 0.108 in. dia thru, center to center 0.700 in. | GE Aviation Systems LLC (35351) | |
| 157091-01-01 1570910101 | 6615-01-010-3163 | Gyromotor | General Characteristics Item Description: Rotor 1, stator 1, ball bearing 1 III Fsc Application Data: Control, automatic pilot, A-10A | GE Aviation Systems LLC (35351) | |
| 157092-01-01 1570920101 | 6615-01-080-0137 | Gyromotor | III End Item Identification: 6615010213681; A-10A acft General Characteristics Item Description: Rim assy 1, stator 1, end bell 2, bearing 2; cylindrical in shape | GE Aviation Systems LLC (35351) | |
| 157092-01-04 1570920104 | 6615-01-080-0137 | Gyromotor | III End Item Identification: 6615010213681; A-10A acft General Characteristics Item Description: Rim assy 1, stator 1, end bell 2, bearing 2; cylindrical in shape | GE Aviation Systems LLC (35351) | |
| 157096-01 15709601 | 6615-01-080-0138 | Stator, Gyromotor | III End Item Identification: 6615010213681; A-10 acft General Characteristics Item Description: 1.199 in. O/a dia; 1.506 in. min lg; 1.520 in. max lg; cylindrical in shape with stator shaft centrally located along dia | GE Aviation Systems LLC (35351) | |
| 157098-01 15709801 | 6615-01-011-1025 | Rotor and Stator se | General Characteristics Item Description: Stator 1, rotor 1, 4.590 in.od, 3.001 in.id, 0.560 in.W III Fsc Application Data: Control, automatic pilot, A-10A | GE Aviation Systems LLC (35351) | |
| 15711-1F 157111F | 6615-00-550-6464 | Controller, Flight, Automatic Pilo | Power Source: External Maximum Overall Length: 6.563 inches Maximum Overall Width: 4.469 inches | Honeywell Intl Inc. (55972) | |
| 15711-2F 157112F | 6615-00-562-5522 | Controller, Flight, Automatic Pilo | Honeywell Intl Inc. (55972) Honeywell Intl Inc. Defense Avionics (19315) |