Flight Instruments: CAI-LNAV, CF00030-1-20, CF00034-1
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
CAI-LNAV CAILNAV | 6610-01-527-1643 | Computer, Flight Director | Special Features: V5.8A system; compatable with standard gps and gps-nav III Part Name Assigned By Controlling Agency: Cambridge l-nav system | SOC Commercial Aeronautique DU (FA3F6) | |
CAI-LNAV-VARIO-R/O CAILNAVVARIORO | 6610-01-519-0421 | Indicator, Vertical Velocity | End Item Identification: Caf 007S and caf 008S l-nav system Diameter: 57.0 millimeters nominal | SOC Commercial Aeronautique DU (FA3F6) | |
CB21-925 CB21925 | 6610-00-019-5415 | Cover Plate Assembl | G T A A LLC (70214) | ||
CC00004-2-5 CC0000425 | 6610-00-401-2601 | Tray Assy | Lockheed Martin Corporation (81755) | ||
CCL/R63/2 REVISION/42C CCLR632REVISION42C | 6610-01-102-0194 | Accelerometer, Mechanical | Ministry of Defence Navy Ships (K2516) | ||
CCL/R63/2 REVISION ITEM 42C CCLR632REVISIONITEM42C | 6610-01-102-0194 | Accelerometer, Mechanical | Ministry of Defence Navy Ships (K2516) | ||
CCM-7010 CCM7010 | 6610-01-501-3600 | Computer Subassembly | Special Features: Itr processor cntr End Item Identification: Global air traffic management system, C-135 aircraft III Part Name Assigned By Controlling Agency: Common computing module | Rockwell Collins Inc. (4V792) | |
CD-207/URC CD207URC | 6610-01-519-3080 | Control-Display unit | III End Item Identification: Used on joint tactical radio system (jtrs) ground vehicle and tacp configuration | Joint Electronics Type Designation (80058) | |
CD-244/URC CD244URC | 6610-01-576-8955 | Control-Display unit | III End Item Identification: JTRS Special Features: Operating system: microsoft windows ce; data processing: 100 mips; memory processing ram: 128 mb ram; channel operation: up to 4 jtr channels, hamux red interface to jtr or docking station; video graphics array, lcd with soft keys for hmi, red switch policy (rsp) acknowledgement, cik interface; zeroization supports multiple single levels of security; input power: 20 to 28 vdc conditioned, 8.25 W max; depth: 2.80 in; weight: 4.00 lbs Maximum Overall Width: 3.600 inches | Joint Electronics Type Designation (80058) | |
CD532766 | 6610-01-027-1641 | Indicator, Position | Mounting Facility Type and Quantity: 1 threaded case Electrical Connection Quantity: 1 End Item Identification: Awacs E3A aircraft | Solartron Electronics Inc. (65092) | |
CE582M101 | 6610-01-424-0283 | Accelerometer, Mechanical | Endevco Corporation (95411) | ||
CF00005-6 CF000056 | 6610-00-491-4092 | Coupler Assy, Instru | III End Item Identification: F111 acft III Part Name Assigned By Controlling Agency: Instrument set coupler assembly III Reference Data and Literature: T.O. 5FA1-4-3, 5FA1-8-1 | Lockheed Martin Corporation (81755) | |
CF00010-1-20 CF00010120 | 6610-00-617-3066 | Indicator, Position | Lockheed Martin Corporation (81755) | ||
CF00023-3 CF000233 | 6610-00-061-2225 | Indicator, Air Speed | Mounting Facility Type and Quantity: 1 bezel Electrical Connection Quantity: 1 End Item Identification: F111A aircraft | Lockheed Martin Corporation (81755) | |
CF00030-1-2 CF0003012 | 6610-00-179-1708 | Indicator, Position | Lockheed Martin Corporation (81755) | ||
CF00030-1-20 CF00030120 | 6610-00-437-5680 | Indicator, Position | Width: 3.250 inches nominal Mounting Facility Type and Quantity: 1 panel Electrical Connection Quantity: 1 | Catty H D Corp. (01726) | |
CF00030-2-1 CF0003021 | 6610-00-199-8895 | Transmitter, Position | Lockheed Martin Corporation (81755) | ||
CF00033-1-1 CF0003311 | 6610-00-809-4305 | Indicator, Position | End Item Identification: F111 Supplementary Features: T.O. 5A12-3-10-4 | Lockheed Martin Corporation (81755) | |
CF00033-1-21 CF00033121 | 6610-00-445-5646 | Indicator, Position | End Item Identification: F111 Supplementary Features: T.O. 5A12-3-10-4 | Lockheed Martin Corporation (81755) | |
CF00034-1 CF000341 | 6610-00-803-4374 | Indexer, Angle of at | Lockheed Martin Corporation (81755) |