Mfg Part Number: CPU-187-A | Alternate P/N: CPU187A | Manufacturer: Joint Electronics Type Designation |
NSN : 6610-01-372-8170 | NIIN : 013728170 | Item Name : Computer Air Data |
CAGE Code : 80058 | FSC : 6610 Flight Instruments |
Thank you for taking an interest in the various military NSN parts and aerospace parts we offer on our website. You have currently taken interest in part number CPU-187-A, a Joint Electronics Type Designation item produced under CAGE Code 80058. For further identification purposes, part number CPU-187-A is also listed with the NSN 6610013728170, and it is organized under Federal Supply Class (FSC) 6610 Flight Instruments for ease of procural. By filling out and submitting the form provided below, you will be able to receive purchasing options on this item directly from our staff. For us to best tailor our presented solution to your unique needs and restrictions alike, we ask that you please offer our team details like your desired quantity, target pricing, and expected fulfillment timeframe. We can even accommodate many time constraints and limitations that customers may face, so be sure to let us know of any requests when you submit an RFQ form for part number CPU-187-A.
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MRC | Criteria | Characteristic |
---|---|---|
AJAF | Unpackaged Unit Length | 12.560 INCHES NOMINAL |
FREQ | Frequency In Hertz | 400 |
AJAG | Unpackaged Unit Width | 6.200 INCHES NOMINAL |
AJAH | Unpackaged Unit Height | 6.940 INCHES NOMINAL |
ACUQ | Alternating Current Voltage Rating In Volts | 115 |
FAAZ | Phase | SINGLE |
AAXX | Mounting Type | RACK |
AXQJ | Intelligence Input Method | AIR OR ELECTRICAL |
AXQH | Input Intelligence Type | AIR DENSITY AND AIR PRESSURE AND ALTITUDE, GENERAL DATA AND AIR TEMPERATURE AND PRESSURE ALTITUDE AND ANGLE OF ATTACK AND SPEED AND TRUE AIR SPEED AND TRUE ANGLE OF ATTACK |
MRC | Decoded Requirement | Clear Text Reply |
AGAV | End Item Identification | F-16 AIRCRAFT |
RTSE | Relationship To Similar Equipment | DIFFERENCES FROM CPU-136/A: A; OUTPUTS NOT USED IN CPU-136/A HAVE BEEN DELETED. ONE TEST CONNECTOR HAS BEEN DELETED. MEMORY AND HARDWARE GROWTH ARE INCREASED. B; NEW DATA WORD IS TRANSMITTED ON THE MUX BUS FOR AIRCRAFT MAINTENANCE FAULT CODE REPORTING/FAULT ISOLATION ENHANCEMENTS. C; RELIABILITY HAS BEEN INCREASED. D; AIR DATA COMPUTER WILL BE MAINTAINED AT 2 LEVELS IN LIEU OF 3. E; NEW AIR DATA COMPUTER CAN BE SUBSTITUTED FOR CPU-136/A BUT NOT VICE VERSA. THIS IS REQUIRED TO PREVENT DEMODIFICATION OF UPDATED AIRCRAFT THAT WILL NOT HAVE I-LEVEL AIR DATA SUPPORT REQUIRED FOR CPU-136/A. |
TMDN | Type/Model Designation | CPU-187/A |
AWZJ | Power Source | EXTERNAL |
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CPU-191-A | CPU-80-A | CPU4A | CPU-1506-1 |
CPU41P | CPU76A | CPU-209-A | CPU30 |
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