Navigational Instruments: 670056-1, 670918-9, 6-714AM042S
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 670056-1 6700561 | 6605-00-070-5955 | Computer | Lockheed Martin Corporation (98897) | ||
| 670275 | 6605-00-099-4075 | Case and Insert Ass | Lockheed Martin Corporation (56232) | ||
| 670434 | 6605-00-134-1801 | Detector Module, Pit | Northrop Grumman Guidance And (06481) | ||
| 670560 | 6605-00-809-5227 | Tower Stage Assembl | Northrop Grumman Guidance And (06481) | ||
| 67056-502-21 6705650221 | 6605-00-110-3574 | Amplifier, Control Group | Boeing Company, The (94756) | ||
| 670574 | 6605-00-110-2620 | Amplifier, Electronic Control | Basic Shape Style: Rectangular or square Circuit Construction Type: Solid state Inclosure Type: OPEN | Northrop Grumman Guidance And (06481) | |
| 67084-301 67084301 | 6605-00-991-2009 | Alignment Group, Optical | Boeing Company, The (94756) | ||
| 670918-0009 6709180009 | 6605-00-314-2596 | Insert and Weight Assembly | III End Item Identification: P/N 683420-8, fscm 06481 General Characteristics Item Description: Basic shape cylindrical, components insert 1, weight 1 III Fsc Application Data: Airborne inertial navigation system | Northrop Grumman Guidance And (06481) | |
| 670918-9 6709189 | 6605-00-314-2596 | Insert and Weight Assembly | III End Item Identification: P/N 683420-8, fscm 06481 General Characteristics Item Description: Basic shape cylindrical, components insert 1, weight 1 III Fsc Application Data: Airborne inertial navigation system | Northrop Grumman Guidance And (06481) | |
| 670938-4 6709384 | 6605-00-311-0600 | Heater, Gyro, External | Northrop Grumman Guidance And (06481) | ||
| 671006-2 6710062 | 6605-00-498-1572 | Panel, Front, Compute | Northrop Grumman Guidance And (06481) | ||
| 671337-105 671337105 | 6605-00-159-2362 | Control, Navigation | General Characteristics Item Description: Kearfott division singergeneral precision inc, part no. C709026055 Reference Number Differentiating Characteristics: As differentiated by in accordance W-lockheed dwg 671337-105 | Lockheed Martin Corporation (98897) | |
| 671363 | 6605-00-110-9499 | Mode Selector unit | III End Item Identification: EC135J aircraft III Fsc Application Data: Inertial navigation system, aircraft III Reference Data and Literature: To 5N1-4-8-42 | L-3 Communications Corporation (1PQF4) Raytheon Technical Services Company (36378) | |
| 671366 | 6605-00-346-1630 | Wiring Harness, Dire | Lockheed Martin Corporation (56232) | ||
| 671390-1 6713901 | 6605-00-809-5924 | Network, Front, Panel | Northrop Grumman Guidance And (06481) | ||
| 671475-1 6714751 | 6605-00-809-5864 | Module, Air Speed | Northrop Grumman Guidance And (06481) | ||
| 671480-2 6714802 | 6605-00-208-3423 | Computer, Navigational | III End Item Identification: F111 aircraft III Fsc Application Data: Airborne inertial navigation system Power Source: Self-contained | Northrop Grumman Guidance And (06481) | |
| 671485-1 6714851 | 6605-00-179-8985 | Module, Front Panel | Northrop Grumman Guidance And (06481) | ||
| 671494-2 6714942 | 6605-00-208-3431 | Module, Slant Range | III End Item Identification: P/N 671480-2, fscm 06481 General Characteristics Item Description: Chassis mounted III Fsc Application Data: Computer, air navigation | Northrop Grumman Guidance And (06481) | |
| 6-714AM042S 6714AM042S | 6605-01-138-0817 | Antenna Coupler unit | III End Item Identification: Aircraft model KA-6D General Characteristics Item Description: 6 250 in. lg, 6.250 in. W, 2.500 in. H | Litton Systems Inc. (30782) |