MODIFICATION
16 -- C-130 Loadmaster Crashworthy Seat (CWS) Stowage Fixture Modification Kits and Stanchion Modification
- Notice Date
- 5/5/2015
- Notice Type
- Modification/Amendment
- NAICS
- 336413
— Other Aircraft Parts and Auxiliary Equipment Manufacturing
- Contracting Office
- Department of the Air Force, Air Force Materiel Command, PK/PZ - Robins AFB, 215 Page Rd, Robins AFB, Georgia, 31098-1611, United States
- ZIP Code
- 31098-1611
- Solicitation Number
- FA8504-15-R-93594
- Point of Contact
- Robert O. Anderson, Phone: 4783274281
- E-Mail Address
-
robert.anderson.31@us.af.mil
(robert.anderson.31@us.af.mil)
- Small Business Set-Aside
- Service-Disabled Veteran-Owned Small Business
- Description
- This is a solicitation notice of intent that AFLCMC/WLNKA anticipates issuing a solicitation/contract for a "build to print" effort to manufacture C-130 Loadmaster Crashworthy Seat (CWS) Stowage Fixture Modification kits. The contractor will manufacture the required fixtures; install the fixtures to Government Furnished seats; modify Government Furnished stanchions, and; return seats and stanchions to Robins AFB Ga. Particulars follow: CWS Kit, NSN: 1560K0104324ALG, 1ea. First Article, 382 ea. production and 29 ea. Optional, Delivery FA 120 DAY ARO, Production 50/Mo. Beginning 90 DAY ARO FA approval. Stanchion Modification, NSN 201112690-10, 18 ea., Delivery 90 DAY ARO Government Provided Stanchions. Modification materials follow: The Upper Stowage Fixture locks the seat into the desired, stowed position. Dimensions: 5.5"L x 4"W x.75"D. Features: two.5" holes for pin placement, and one.2" hole for lanyard attachment. Material: Aluminum Alloy, 6061-T651, Plate IAW SAE AMS-QQ-A-250/11, OR 6061-T6511, Extruded Bar IAW SAE AMS-QQ-A-200/8. Finish: Anodize IAW MIL-A-8625, Type II, Class 2 (Black). Both sides will be engraved to identify Left Hand or Right Hand application. The Lower Stowage Fixture Assembly provides greater range of motion for the seat. Dimensions: 8"L x 2.5"W x 2"D. Features: two.625" threaded holes for attached hardware, and two.2" holes for mounting to the Interface Assembly. Attached Hardware: two Locking Spring Plungers, PN 201112750-01. Material: Aluminum Alloy, 6061-T651, Plate IAW SAE AMS-QQ-A-250/11, OR 6061-T6511, Extruded Bar IAW SAE AMS-QQ-A-200/8. Finish: Anodize IAW MIL-A-8625, Type II, Class 2 (Black). Top side will be engraved to identify LH and RH positioning. The proposed contract action is for supplies and services for which the Government intends to solicit as a FAR 15, competitive, 100% small business set aside for Small Disabled Veteran Owned Small Business (SDVOSB). Please see 22 APR 2015 Updated SOW. Due to the fact that the previous responses were due on a Federal Holiday the response date is extended to 27 MAY 2015, 1600 EST.
- Web Link
-
FBO.gov Permalink
(https://www.fbo.gov/spg/USAF/AFMC/WRALC/FA8504-15-R-93594/listing.html)
- Record
- SN03720875-W 20150507/150505235703-6981c21ba0eba8287191ed5763c05631 (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
(may not be valid after Archive Date)
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