Flight Instruments: 819560-1, 822-0179-013, 822-1000-021
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 819560-1 8195601 | 6610-00-872-2567 | Regulator Module | Teledyne Technologies Inc. (98571) | ||
| 819727-1 8197271 | 6610-00-872-2545 | Plate, Port End Assy | Teledyne Technologies Inc. (98571) | ||
| 819760-1 8197601 | 6610-00-938-2002 | Gear Assy, Spur | Teledyne Technologies Inc. (98571) | ||
| 819778 | 6610-00-872-0452 | Strip, Bi-Metal set | Teledyne Technologies Inc. (98571) | ||
| 81B17-1 81B171 | 6610-01-071-7958 | Inclinometer, Aircraft | Sigma TEK Inc. (86887) | ||
| 82-01031-001 8201031001 | 6610-01-199-0493 | Panel Assembly | III End Item Identification: 6610011712590 General Characteristics Item Description: Cover plate 2;CHASSIS 1;NAMEEPLATE 1;CONNECTOR 2;SWITCH 2 | Raytheon E-Systems Inc. (33875) | |
| 82-01819-001 8201819001 | 6610-01-199-0499 | Panel Assembly, Edge Lit | III End Item Identification: 6610011712590 General Characteristics Item Description: Retainer 2;CONNECTOR 1;LIGHT assembly 3;LAMP 3 | L-3 Communications Integrated (0GCL4) Raytheon E-Systems Inc. (33875) | |
| 820-275-9 8202759 | 6610-00-866-1723 | Movement, Indicator | Hickok Incorporated (28569) | ||
| 82192-6 821926 | 6610-00-409-8019 | Reel, Tape | General Characteristics Item Description: 6.130 in. flange dia, 2.120 in. hub dia | Transico Inc. (97525) | |
| 822-0179-002 8220179002 | 6610-01-459-0598 | Concentrator unit | III End Item Identification: Challenger 604 | Rockwell Collins Inc. (13499) | |
| 822-0179-003 8220179003 | 6610-01-493-9923 | Computer, Air Data | III Part Name Assigned By Controlling Agency: Data concentrator unit, DCU-4002 | Rockwell Collins Inc. (13499) | |
| 822-0179-013 8220179013 | 6610-01-517-8628 | Computer, Air Data | III Part Name Assigned By Controlling Agency: Data concentrator unit Intelligence Input Method: Electrical | Rockwell Collins Inc. (13499) | |
| 822-0371-159 8220371159 | 6610-01-531-0787 | Computer, Air Data | III End Item Identification: CN-235, aircraft Power Source: External Intelligence Input Method: AIR | Rockwell Collins Inc. (4V792) | |
| 822-0390-001 8220390001 | 6610-01-414-7481 | Processor, Flight Information | Special Features: Uses a green P44 phosphor cathode ray tube for display.anvis gen III compatable keyboard Input Intelligence Type: Flight command information III Unpackaged unit Length: 6.50 inches nominal | Rockwell Collins Inc. (13499) | |
| 822-0842-142 8220842142 | 6610-01-459-0599 | Computer, Air Data | III End Item Identification: Challenger 604 | Rockwell Collins Inc. (13499) | |
| 822-0842-421 8220842421 | 6610-01-504-1276 | Computer, Air Data | III End Item Identification: ADS-850 III Fsc Application Data: Equipment type ADC-850E III Part Name Assigned By Controlling Agency: Air data computer, rvsm | Rockwell Collins Inc. (13499) | |
| 822-0845-001 8220845001 | 6610-01-526-0555 | Computer, Air Data | Special Features: Engine indication and crew alerting systems (eicas) routing unit; temperature minus 55 to plus 70 deg. ; 55, 000 ft. altitude; passive power Intelligence Input Method: Electrical Mounting Type: RACK | Rockwell Collins Inc. (13499) | |
| 822-0867-008 8220867008 | 6610-01-459-0601 | Control-Display unit | III End Item Identification: Challenger 604 | Rockwell Collins Inc. (13499) | |
| 822-0943-021 8220943021 | 6610-01-498-4063 | Control-Display unit | Rockwell Collins Inc. (13499) | ||
| 822-1000-021 8221000021 | 6610-01-460-1385 | Display unit, Flight Information | III End Item Identification: CC130 hercules aircraft General Characteristics Item Description: Electronic flight crt panel mounted display used as a electronic attitude director indicator or electronic horizontal situation indicator; case is 4.98 in W by 4.60 in. H by 9.80 in. lg; 41 pin circular bayoned locking typeconnector on rear of case | Rockwell Collins Inc. (4V792) |