Thank you for taking interest in Boeing Company The part number 42C93900-001, which is listed with the NSN 4920-01-358-0940 and a product description of “Test Program Set.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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| MRC | Criteria | Characteristic |
|---|---|---|
| MRC | Decoded Requirement | Clear Text Reply |
| FEAT | Special Features | INTERFACE BETWEEN THE ADIT II PCA ADAPTER SET AND THE PCA; SIGNAL TRACING AND CONTINUITY ASSURANCE CAPABILITIES TO THE UUT; A UNIQUE ADAPTER WHICH INTERFACE BETWEEN THE UUT AND THE TEST STATION; PROVIDES A SUPPORT FRAME ASSEMBLEY TO SECURE THE UUT; A VIGINIA PANEL WITH BALL AND DETENTS FOR INTERFACING WITH THE APAS AND A HOUSING WHICH HOUSES THE WIRING; THE COOLING AIR WHICH IS REQUIRED FOR THE UUT IS PROVIDE FROM THE APAS THROUGH THE FORGED LOOP AIR HOSE IN THE ITA AND CHANNELED THROUGH THE FLEXIBLE AIR DUCT TO THE UUT;THE ITA WILL WORK IN CONJUNCTION WITH THE ADIT II TEST STATION AND THE APAS |
| AGAV | End Item Identification | B-1B ACFT ITA PCA BOX 7 CENTRAL AVIONICS BAY |
| FTLD | Functional Description | TO FALUT ISOLATE THE FAILED LRU, SRU OR COMPONENT AND TO VERIFY THE PERFORMANCE OF THE MODIFIED POWER CONTROL ASSEMBLY(PCA) |
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