Closed
NONE
Tank, Fuel, Aircraft
- Agency
- DEPT OF DEFENSE
- NAICS
- 336413
- Closed
- Jul 29, 2026
- Posted
- Jun 29, 2026
Description
PR: FD20302600453 1. Estimated issue date and estimated closing/response date: Issue: 15 July 2026 Closes: 17 August 2026 2. RFP# SPRTA1-26-R-0315 Request for Proposal 3. Service/Spare/Repair/OH: AF Spares 4. AMC: 3/B 5. Nomenclature/Noun: TANK,FUEL,AIRCRAFT 6. NSN: CLIN 0001: 1560-01-521-2563FG CLIN 0002: 1560-01-522-0552FG CLIN 0003: 1560-01-522-0554FG CLIN 0004: 1560-01-522-1172FG CLIN 0005: 1560-01-522-1614FG CLIN 0006: 1560-01-522-1615FG CLIN 0007: 1560-01-522-2637FG 7. PN: CLIN 0001: 320-52138-101 CLIN 0002: 320-52132-101 CLIN 0003: 320-52134-101 CLIN 0004: 320-52136-101 CLIN 0005: 320-52130-101 CLIN 0006: 320-52126-101 CLIN 0007: 320-52128-101 8. History: CLIN 0001, FA810305D00810005, 18 Dec 2006, 27 each, THE BOEING COMPANY (81205) CLIN 0002, SPRTA125C0107, 26 Sep 2025, 23 each, AXILLON AEROSPACE (ROCKMART), LLC (56221) CLIN 0003, SPRTA125C0107, 26 Sep 2025, 23 each, AXILLON AEROSPACE (ROCKMART), LLC (56221) CLIN 0004, SPRTA125C0107, 26 Sep 2025, 23 each, AXILLON AEROSPACE (ROCKMART), LLC (56221) CLIN 0005, SPRTA125C0107, 26 Sep 2025, 23 each, AXILLON AEROSPACE (ROCKMART), LLC (56221) CLIN 0006, SPRTA125C0107, 26 Sep 2025, 23 each, AXILLON AEROSPACE (ROCKMART), LLC (56221) CLIN 0007, FA810305D00810005, 18 Dec 2006, 24 each, THE BOEING COMPANY (81205) 9. Description/Function: CLIN 0001 Function: serves as a bladder/container for fuel. When installed this bladders shape is supported by a rigged metal structure. Material: Rubber End Item: B-52 aircraft Length 10.0000’, Width 7.0000’, Height 7.0000’, Weight 200.0000lbs. CLIN 0002 Function: fuel cell. Material: layered nylon and urethane End Item: B-52 aircraft Length 112.3000”, Width 42.3000”, Height 29.3000”’, Weight 150.0000lbs. CLIN 0003: Function: serves as a bladder/container for fuel. When installed this bladders shape is supported by a rigged metal structure. Material: Rubber End Item: B-52 aircraft Length 10.0000’, Width 7.0000’, Height 7.0000’, Weight 200.0000lbs. CLIN 0004: Function: fuel cell. Material: layered nylon and urethane End Item: B-52 aircraft Length 112.3000”, Width 42.3000”, Height 29.3000”, Weight 150.0000lbs. CLIN 0005: Function: fuel cell. Material: BTC-101 layered nylon and urethane End Item: B-52 aircraft Length 112.3000”, Width 42.3000”, Height 29.3000”, Weight 125.0000lbs. CLIN 0006: Function: fuel cell. Material: BTC-101 layered nylon and urethane End Item: B-52 aircraft Length 68.5600”, Width 111.5200”, Height 68.5600”, Weight 125.0000lbs. CLIN 0007: Function: serves as a bladder/container for fuel. Material: Rubber End Item: B-52 aircraft Length 10.0000’, Width 7.0000’, Height 7.0000’, Weight 200.0000lbs. 10. Total Line Item Quantity: CLIN 0001: 80 each CLIN 0002: 57 each CLIN 0003: 57 each CLIN 0004: 57 each CLIN 0005: 57 each CLIN 0006: 57 each CLIN 0007: 80 each 11. Application (Engine or Aircraft): B-52 aircraft 12. Destination: L/I ALL - Ship to SW3211 13. Required Delivery: L/I ALL - Ship To SW3211, 1 Each every month until complete starting September 2026 14. Qualification Requirements: Do not exist. 15. Export Control Requirements: Yes 16. UID: Note to Contractor: UID requirements will apply. 17. Qualified Sources: Axillon Aerospace (Rockmart), LLC (CAGE 56221) 18. Set-aside: This acquisition will not be set aside. 19. Surplus: Surplus is not authorized. 20. Surge Requirement: Surge option clause 252.217-7001 will be included in this solicitation. The successful offeror who is awarded this contract will be required to submit a Capabilities Analysis Plan (CAP) as stated and in accordance with clause 252.217-7001 (b)(2) and Data Item Description attachment DI-MGMT-80969 Production Surge Plan within 30 days after award. 21. Mandatory Language: The Government does not own the data or the rights to the data needed to manufacture this item. Firms interested in participating in this procurement are encouraged to contact the OEM to inquire about the data or rights to the data. In accordance with FAR 5.207(c)(16)(i), all responsible sources...
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