Automatic Pilot Mechanisms and Airborne Gyro Components: 677000, 67862-302-1, 679686-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 677000 | 6615-00-078-1099 | Gyroscope Assembly | Northrop Grumman Guidance And (06481) | ||
| 677014 | 6615-00-479-9483 | Insert, Gyroscope | Northrop Grumman Guidance And (06481) | ||
| 67719-302 67719302 | 6615-01-087-1551 | Gyroscope, Integrating | Overall Length: 2.500 inches maximum Wheel Power Method: Electric Overall Diameter: 1.295 inches maximum | Atlantic Inertial Systems Inc. (63395) Northrop Grumman Corp. (88932) | |
| 67719-309 67719309 | 6615-01-415-0896 | Gyroscope, Displacement | III End Item Identification: Tank, abrams M-1 Overall Length: 2.500 inches nominal Wheel Power Method: Electric | Northrop Grumman Corp. (88932) | |
| 677230 | 6615-00-885-1012 | Accelerometer, Electrical, Linear | Northrop Grumman Guidance And (06481) | ||
| 677486 | 6615-00-890-9122 | Ring, cap Connecting | General Characteristics Item Description: Material aluminum alloy 6061 QQ-A-225/8 cond T6, 2.141 in. od, 2.030 in. id, anodize per MIL-A-8625 type I class I | Northrop Grumman Guidance And (06481) | |
| 677544 | 6615-00-758-2474 | Switch Assembly, Bel | Keaster Products Incorporated (52316) Northrop Grumman Guidance And (06481) | ||
| 677558 | 6615-00-992-9013 | Bellows, Compensating | General Characteristics Item Description: 1.060 to 1.062 in. O/a dia; 0.145TO 0.190 id; inside threads, 4-40 UNC-2B 3 full threads, threads shall withstand a 15 pound steady axial pull without damage to bellows assembly | Northrop Grumman Guidance And (06481) | |
| 677B538P1 | 6615-00-511-2864 | Cover, Control | BAE Systems Controls Inc. (89954) | ||
| 67835-302-1 678353021 | 6615-00-466-2441 | Rotor, Gyro | General Characteristics Item Description: Major components, rotors 1, sleeves 2, sleeve dimensions, length 0.949 inch, diameter 1.233 inches III Fsc Application Data: Missile LGM-30 | Boeing Company, The (94756) | |
| 67854-302-1 678543021 | 6615-00-096-1689 | Insert, Valve | III End Item Identification: Gyroscope, displacement, airborne General Characteristics Item Description: Beryllium, 4.124 in. outside dia, 3.733 in. inside dia, 0.739 in. W III Fsc Application Data: Missile guidance set, LGM&30 | Boeing Company, The (94756) | |
| 67856-302-1 678563021 | 6615-00-096-1695 | Ring, Pickoff, Dummy | III End Item Identification: Gyroscope, displacement, airborne General Characteristics Item Description: Beryllium, 3.665 in. od 2.968 in id, 0.315 in W III Fsc Application Data: Missile guidance set, LGM&30 | Boeing Company, The (94756) | |
| 67862-302-1 678623021 | 6615-00-096-1714 | Gyromotor | III End Item Identification: Gyroscope, displacement, airborne General Characteristics Item Description: Rotor 1, stator 1 III Fsc Application Data: Missile guidance set, LGM&30 | Boeing Company, The (94756) | |
| 678919-161 678919161 | 6615-00-342-9611 | Motor and Drive Ass | Lockheed Martin Corporation (56232) | ||
| 679337-0002 6793370002 | 6615-01-009-2322 | Strut Assembly, Gyroscope | III End Item Identification: Carrier inertiel navigation system, AN/ASN-92 V | Northrop Grumman Guidance And (06481) | |
| 679337-2 6793372 | 6615-01-009-2322 | Strut Assembly, Gyroscope | III End Item Identification: Carrier inertiel navigation system, AN/ASN-92 V | Northrop Grumman Guidance And (06481) | |
| 679429 | 6615-00-349-0488 | Accelerometer Assembly, Electrica | III End Item Identification: Cains | Northrop Grumman Guidance And (06481) | |
| 679567 | 6615-00-526-8364 | Controller, Engaging, Automatic Pi | Frequency in Hertz: 400.0 Phase: Single Power Source: External | Lockheed Martin Corporation (56232) | |
| 679686-0001 6796860001 | 6615-01-009-2320 | Float Assembly | General Characteristics Item Description: Motor and shell assembly P/N 679685-1, 2 jewel bearing assembly P/N 676955 | Northrop Grumman Guidance And (06481) | |
| 679686-1 6796861 | 6615-01-009-2320 | Float Assembly | General Characteristics Item Description: Motor and shell assembly P/N 679685-1, 2 jewel bearing assembly P/N 676955 | Northrop Grumman Guidance And (06481) |