CT-26-00534-A2 - FAA Technical Specifications - 9.14.26.pdf
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- Solicitation number
- RFQCT2600534A2
About this file
This is a Technical Specifications document for Federal Acquisition Regulation (FAR) solicitation PR CT-26-00534-A2 issued by the Federal Aviation Administration (FAA).
The FAA seeks zero-time Lycoming piston aviation engines and specially modified cylinders for the William J Hughes Technical Center for Advanced Aerospace (WJHTCAA) Propulsion and Airpower Engineering Research Laboratory in Atlantic City, New Jersey. Required equipment includes: two Lycoming TIO540-AE2A engines for PIPER PA-46-350P aircraft pre-measured and configured for endurance/durability testing per SAE J-1899/14 CFR Part 33.49; one Lycoming TIO540-AE2A engine configured with drilled cylinder ports to support FAA Kistler pressure transducers for detonation testing; six replacement cylinder kits for TIO-540-AE2A configured with drilled ports for Kistler pressure transducers; and six replacement cylinder kits for TSIO-540-J2B similarly configured. All equipment must be new, traceable directly to Lycoming's Original Equipment Manufacturer (OEM) production and quality control processes, with no prior engine wear or third-party handling. Vendors must provide FAA Form 8130-3 (Authorized Release Certification, Airworthiness Approval Tag) or manufacturer's certification of compliance, along with OEM documentation tracing production back to the OEM production process. The vendor assumes full responsibility for all equipment shipped to FAA William J Hughes Technical Center for Advanced Aerospace, Building 211, Atlantic City International Airport, Atlantic City, NJ 08405.
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FAA Technical Specifications – PR CT-26-00534-A2 The Federal aviation Administration (FAA) requires Avco Corp, doing business as, Lycoming Engines piston aviation engines and specially modified cylinders for use at the FAA’s William J Hughes Technical Center for Advanced Aerospace (WJHTCAA), Propulsion and Airpower (POWER) Engineering Research Laboratory located in Atlantic City New Jersey. The vendor must furnish equipment necessary to provide the types, quantities with configuration of engines and cylinder kits indicated below:
EQUIPMENT PART
NUMBER QTY CONFIGURATION
NOTES
DELIVERY
DESTINATION
Lycoming TIO-
540-AE2A
Engine for
PIPER PA-46-
350P
ENPL-10844 or
RENPL-10844.
Whichever can be delivered faster
Pre-measured and configured for endurance / durability testing (SAE J-1899 / 14 CFR Part 33.49)
WJHTCAA
Lycoming TIO-
540-AE2A
Engine for
PIPER PA-46-
350P
ENPL-10844,
RENPL-10844,
or HENPL- 10844.
Whichever can be delivered faster
Configured with drilled cylinder ports to support FAA Kistler pressure transducers for detonation testing
WJHTCAA
Replacement cylinder kits for
TIO-540-AE2A
OEM created for custom part 6
Configured with drilled ports to support FAA Kistler pressure transducers for detonation testing
WJHTCAA
Replacement cylinder kits for
TSIO-540-J2B
OEM created for custom part 6
Configured with drilled ports to support FAA Kistler pressure transducers for detonation testing
WJHTCAA
Vendor must provide zero-time Lycoming above specified Engines without any prior engine wear (hysteresis). Engines must be traceable back to the Original Equipment Manufacturer (OEM), Lycoming, type design holder production process and OEM quality control (QC) process. Engines must not be handled by third parties or assembled with parts that are not in the QC system of the OEMs (Parts Manufacturer approval).
At a minimum, Vendor must provide the following:
a. FAA form 8130-3- “Authorized Release Certification, Airworthiness Approval Tag”, or manufacturer’s certification of compliance.
b. To ensure compliance with paragraph 3, engines must include documentation from the OEM tracing their production back to the OEM production process.
c. The Vendor will be responsible for all equipment shipped to:
FAA William J Hughes Technical Center for Advanced Aerospace Bldg. 211 Atlantic City International Airport Atlantic City, NJ 08405
File details come from the government source that posted it. Updated .