US-FED-00000386259 - Shroud, Inflight Refueling - Deadline July 29,2026

SynopsisPR: FD[ phno? redacted ]1. Estimated issue date and estimated closing/response date:Issue: July 29, 2026Closes: August 28, 20262. RFP# SPRTA1–26–R–0374Request for Proposal3. Service/Spare/Repair/OH: Spares4. AMC: 3/D5. Nomenclature/Noun: Shroud, Inflight Refueling6. NSN: [ phno? redacted ]9217. PN: 400671–48. History: 23 Dec 2020, 3 each, Mission Systems Davenport Inc. (72429)03 Aug 2020, 10 each, Mission Systems Davenport Inc. (72429)9. Description/Function: Shroud, Inflight Refueling. DIMENSIONS, 16.0 INCH (L) BY 12.0 INCH (W) BY 12.0 INCH (H). 5.0 POUNDS (WEIGHT). MATERIAL CONTENT, The shroud assembly is a double skinned, glass–fibre structure. This is part of the Multi Point Refueling System (MPRS). The shroud assembly fits over the reception coupling to streamline the coupling and protect its latch mechanism. It also protects and directs air flow over the two air driven generators.. APPL. TO KC–135.10. Total Line Item Quantity: L/I 0001 8 eachL/I 0002 1 Lot (Production Surge Plan)11. Application (Engine or Aircraft): KC–13512. Destination: Ship to SW3211, Tinker AFB, OK13. Required Delivery: L/I 0001 2 each On or Before 01 JAN 2027