NDI X-ray Testing Rotor Blade Pins, Rear Rotor Blades, and Aircraft Slings for Apache AH-64D

Agency: Department of the Army
State: Federal
Level of Government: Federal
Category:
  • H - Quality Control, Testing, and Inspection Services
Opps ID: NBD00159908441156824
Posted Date: Oct 5, 2017
Due Date: Oct 27, 2017
Solicitation No: W912L2-18-T-0002
Source: Members Only
Solicitation Number :
W912L2-18-T-0002
Notice Type :
Combined Synopsis/Solicitation
Synopsis :
Added: Oct 05, 2017 1:00 pm
Peace Vanguard requires a Non-Destructive Inspections NDI) to be performed on aircraft slings on an annual basis. The inspection of slings ensures that structural discrepancies in slings are found before sling failure during use. Peace Vanguard also requires an X-ray inspection to be performed on aircraft blade retention pins and tail rotor blades.

NDI is a wide group of analysis techniques used in science and technology industry to evaluate the properties of a material, component or systems without causing damage. NDI will be done on aircraft slings using PT & MT methods. X-Rays inspections will be done for blade pins using the RT method and on a schedule of 250 flight hours, or on the first 125 flight hour inspection after the replacement of a blade pin. Vendor must also be able to perform radiographic X-ray on the tail rotor blade pin using equipment SMART 300HP or equivalent. Results of the testing will be sent via email to the Government representative, who will be identified at time of agreement execution. Vendor must be able to perform rotor blade pin x-ray inspections based on the attached requirements (Appendix 1) and tail rotor blade inspection based on attached(Appendix 2).


See attached RFQ, SOW, and Appendices 1 & 2 for full details.

POC is SGT Justin Geisendaffer, (602) 267-2875, justin.m.geisendaffer.mil@mail.mil

Please consult the list of document viewers if you cannot open a file.
Package #1
Posted Date:
October 5, 2017
Description: Request for Quote and Statement of Work
Description: Testing specifications for blade pins
Description: Testing specifications for rear rotor blades
Contracting Office Address :
5645 East McDowell Road
Phoenix, Arizona 85008-3442
Place of Performance :
Contractor laboratory

United States
Primary Point of Contact. :
Justin Geisendaffer,
Contract Specialist
Phone: 6022672875
Secondary Point of Contact :
Thomas W. McKendry,
Contracting Officer
Phone: 60227672704

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