MODIFICATION
59 -- F-22 Cable Assemblies
- Notice Date
- 4/20/2018
- Notice Type
- Modification/Amendment
- NAICS
- 335931
— Current-Carrying Wiring Device Manufacturing
- Contracting Office
- Department of the Air Force, Air Force Materiel Command, AFLCMC / AFSC / AFNWC - HILL AFB, ., Hill AFB, Utah, 84056, United States
- ZIP Code
- 84056
- Solicitation Number
- FA8224-18-R-8058
- Archive Date
- 6/9/2018
- Point of Contact
- Shelly Bachison, Phone: 941115865091
- E-Mail Address
-
shelly.bachison@us.af.mil
(shelly.bachison@us.af.mil)
- Small Business Set-Aside
- Total Small Business
- Description
- Clarification: It is the Government's intent that the sample cables requested for technical evaluation be a preexisting cable(s) demonstrating the salient characteristics. If you have a cable that demonstrates all characteristics in one, that is permissible. However, if you need to send in more than one cable to cover all characteristics, that is also allowable. For instance, one cable may demonstrate only flexibility. A second cable may demonstrate the cable jacket requirements. If utizing more than one sample cable, please label each cable with which characteristic(s) it demonstrates. The US Government will not reimburse any costs associated with manufacturing samples as it is our intent that previously manufactured cables be utilized to demonstrate technical capability. Understanding that this requirement may have been unclear, please send in a sample cable(s) that meet the following standards in addition to flexibility: •c. Each c a b le s h a ll inc lud e internal st r a in r elief which is f r ee f r o m e xt e r n a l h a r d w a r e. •e. Self-Test Plug enclosed back shell (Shorting Cap Back shell) will be no less than 1.0 inch and no more than 1.5 inches. •f. A ll c onn ec to rs and c ompon e n ts s h a ll be v o id o f a n y s h a r p p r o t r u s i o n s t h a t w ill s n a g o n o t h e r ob je c t s. •g. C a b le j a c k et s h a ll be no n-e l a st om e r. •h. C a b le j a c k et s h a ll n o t s n a g or f r a y. •j. Th r e a d primer/sealer compound s h a ll b e a pp lied u po n fi n a l c l o cking ( t i gh t en in g o f all t h r e a d ed a ss e mb lies) o f c a b l e a ss e mb ly. •k. S h ield t e r m i n a t i o n s s h a ll be in a cc o r d a n ce w i t h p r od u c t i o n le v el d r a win g schematics. •l. S p a r e wi r es s h a ll be popu la t ed in a cc o r d a n ce w i t h t h e i nd ivid u a l p r odu c t i o n le v el d r a win g s. •m. A ll S elf-Test P l ug s sh a ll be laser etched and c a b l es m a r k e d w i t h n o n - s h r i n k, non-adhesive, s elf - p o s i t i o n i n g ( i. e. n o t fi x ed p os i t i on ) I D M a r k e r s with crush resistance of 250lbs. •n. All cable legs will be marked with non-shrink, non-adhesive, engraved and filled or laser etched. •o. Cable labels must have an UID, Cable Name, Part Number and Cage Code. •p. C a b le, A d a p t er a n d pl u g m a r ki ng s sh a ll be o f p e r m a n ent m e a n s e ng r a v ed or laser etched o n non-fixed l a b e l and/or each leg. S ee p r odu c t i o n le v el d r a win g s f o r s p ecific s. •q. A ll Self-Test P l u g s and (ST 1 ) s h a ll be e ng r a v ed and filled or laser etched o n enclosed back-shell. •r. A ll c onn ec to r ends which do not have attached Self-Test Plugs s h a ll h a v e a rubber Dust Cap which is pe r m a n en t ly attached t o the c a b l e. •s. The Self-Test Plug/D u s t C ap a tt a ch m ent s h a ll p r o v i d e 36 0 de g r ee r o t a t i o n ( s ee d r a win g s f o r image d e t a il s ). •t. The Self-Test Plug/D u s t C ap c onn ec t i o n t o c a b le s h a ll p r o v i d e n o less t h a n 6 inches b u t no m o re t h a n 9 inc h es d is t a n ce b e t w e en t h e c onn ec t i o n p o i n t a n d t h e Dust Cap. Technical Testing documentation shall include: Lanyard Strength, Capability testing, and the following: •b. A ll c a b l es s h a ll have an internal strain relief and p r o v i d e a m i n i mu m o f 80 l b s o f st r a in r elief f o r 10 m i n u t e s without stretching or elongating more than 5%. d. A ll a tt a ched Self- Test Plugs /Dust Caps of t h e c a b l e s h a ll p r o v i d e a m i n i mu m of 5 0 l b s. o f t en s ile s t r en g t h w i t h ou t breaking. •u. C a b le j a c k et (convoluted tubing) s h a ll be a b r a s i o n, che m ic a l a n d h e a t r e s i s t a n t. Must meet or exceed (Temperature MIL-STD 28800E Test method 7.3 a, b and 1 through 5). •v. Storage Temperature: -51C to 71C Operating Temperature: -40C to 71C Storage Altitude: 40,000 feet Operating Altitude: 15,000 feet
- Web Link
-
FBO.gov Permalink
(https://www.fbo.gov/spg/USAF/AFMC/OOALC/FA8224-18-R-8058/listing.html)
- Place of Performance
- Address: F2DCCF -309 SMXG/OBA, Attn: Thomas King, 7278 4th St BLDG 100 Rm 108, HIll Air Force Base, Utah, 84056, United States
- Zip Code: 84056
- Zip Code: 84056
- Record
- SN04896609-W 20180422/180420230734-668a21d49150f9ce41b0dab3f06113da (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
(may not be valid after Archive Date)
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