U -- PROCURE AIRCRAFT DAMAGE REPAIR TRAINING BEYOND THE LIMITS OF PUBLISHED REPAIR INSTRUCTIONS.

Notice Date

December 22, 2000

Contracting Office

WR-ALC/PKOS, 215 Byron St, Robins Air Force Base, GA 31098-1611

ZIP Code

31098-1611

Solicitation Number

F09650-01-Q-0235

Response Due

January 4, 2001

Point of Contact

John Glenn (912)926-5215

E-Mail Address

F09650-01-Q-0235 (john.glenn@robins.af.mil)

Description

This is a combined synopsis/solicitation for commercial items prepared in accordance with the format in Subpart 12.6, as supplemented with additional information included in this notice. This announcement constitutes the ONLY solicitation; quotes are being requested and a written solicitation will not be issued. This solicitation F09650-01-Q-0235 is a Request for Quote. This solicitation incorporates provisions and clauses that are in effect through Federal Acquisition Circular (FAC) 97-20. NAICS Code: 541330 size $20 million. Place of Performance/FOB: Robins AFB, GA. Period of Performance: 8-19 January 01 CLIN 0001 -- Procure, one time, instructional training for 15 aircraft engineers which provides instructions to assess, analyze, design, and repair aircraft metallic damage beyond the limits identified in published repair instructions. This solicitation is sole source to Boeing Flight Safety or their certified authorized dealers. The following clauses apply: 52.252-2 -- Clauses Incorporated by Reference. The full text of a clause may be accessed electronically at this/these address(es): Regulations URLS: (Click on the appropriate regulation.) http://farsite.hill.af.mil/reghtml/far/farltoc/htm http://farsite.hill.af.mil/reghtml/dfars/dfarltoc.htm http://farsite.hill.af.mil/reghtml/affars/affarltoc.htm http://farsite.hill.af.mil/reghtml/afmcfars/afmcltoc.htm 52.212-1 -- Instructions to Offerors -- Commercial; 52.212-2 -- Evaluation -- Commercial Items -- Price and only price related factors; all or none; 52.212-4 -- Offeror Representations and Certifications -- Commercial Items; 52.212-4 -- Contract Terms and Conditions -- Commercial Items; 52.212-5 -- Contract Terms and Conditions Required to Implement Statutes or Executive Orders -- Commercial Items. 52.222-26 -- Equal Opportunity 52.222-41 -- Service Contract Act of 1965, As Amended 52.222-42 -- Statement of Equivalent Rates for Federal Hires 5352.237-9001 -- Contractor Identification Wage Determination 94-2139 Rev. 20 dated 09/14/2000 applies to this solicitation. DPAS Rating -- 0 CBD Note 22 apply to this solicitation. RFQ's may be faxed to (478) 926-3590 Attn: John Glenn. RESPONSE TIME: 4 January 2001. BUYER: John Glenn, 478-926-5215. STATEMENT OF WORK: 1. Scope. The purpose of this training is to provide students with the tools needed to assess, analyze, and design metallic repair for aircraft damage beyond the limits of published repair manuals. Topics of the course should include design and airworthiness requirements; typical structures and loads, material behavior and properties, fastener selection, joint design, and durability concepts. The course should include a combination lecture, discussion, practical exercises and a factory field trip. 2. Objectives. The students should be able to identify basic design requirements for structural repairs; describe typical aircraft structure and loads; identify fasteners and joints used in repair; design a metallic structural repair for damage beyond structural repair manual limits with reasonable assurance of approval from flight safety agencies. 3. Requirements. The contractor shall furnish all labor, travel, and training material necessary to satisfy the service requirements for the following specific areas pertaining to aircraft structural repair. Design Considerations. Basic design tools, testing and FAA certification process. Loads. General external loads; static strength checks; internal load distribution; wing, fuselage and empennage loads. Materials. Aluminum, titanium, and steel alloy usage; stress corrosion, hydrogen embrittlement; and untempered martensite. Fasteners. Fastener callouts; rivets; hi-loks; lock bolts; bolts; nuts, and washers. Joints. Joint allowable; joint analysis; in-line row joint repair; staggered row joint repair; eccentrically loaded joints; and shims. Durability. Corrosion resistance; fatigue concepts; damage tolerance concepts; cold working holes; and shot peening. Structural Repair Design. Steel, chord, and web/skin repairs. Credentials. Instructor must have real world experience and access to Boeing proprietary design data. Training Facility. The government will provide a suitable training facility at Robins AFB, Georgia.

Record

Loren Data Corp. 20001227/USOL001.HTM (W-357 SN509604)