Draft_Technical_Specifications.docx

TECHNICAL SPECIFICATIONS-REQUIREMENTS

AIRCRAFT ENGINE (CFM56-3C1) PURCHASE

JUSTICE PRISONER AND ALIEN TRANSPORTATION SYSTEM (JPATS)

OKLAHOMA CITY, OKLAHOMA

I. BACKGROUND

The primary mission of U.S. Marshals Service, Justice Prisoner and Alien Transportation System (JPATS) is the safe, secure and efficient transportation of federal and non-federal prisoners and the provision of aircraft and flight crew for the support of other operational missions. Additional mission assignments include, but are not limited to, international flights in support of foreign extraditions, witness security and enforcement operations, strategic deployment of USMS and Special Operations Group personnel and equipment and other special operations assigned by the USMS or U.S. Attorney General.

II. GENERAL

JPATS has a requirement for the Purchase of one (1) Aircraft Engine, Model: CFM56-3C1. The engine will be identified as the “Backup” engine to be installed on one (1) of JPATS’ Boeing 737-400 Aircraft, as needed. Delivery of engine will be to the USMS hangar in Oklahoma City OK within ten (10) days after award.

III. TECHNICAL REQUIREMENTS:

The engine must have a maximum takeoff rated thrust of 23,500 pounds with no fixed de-rate. All applicable FAA Airworthiness Directives (AD) must be accomplished with no recurring inspections due at time of delivery to JPATS. Proof of AD accomplishment is required to be provided to JPATS. All manufacturers’ Mandatory / Alert Service Bulletins (SB) must be accomplished with no recurring inspections due at time of delivery to JPATS. Proof of SB accomplishment is required to be provided to JPATS. The replacement threshold for all engine Life Limited Parts (LLP) must not come due within 1200 cycles. Proof of serviceability (life) remaining must be provided to JPATS. The candidate JPATS aircraft that this engine would possibly be utilized on all have United States (N number) registration and Standard Certificates of Airworthiness. The engine must have been operational on an aircraft possessing a Standard Certificate of Airworthiness for a time-frame of not less than 60 days within the previous 180 days from date of quote submission.

IV. DELIVERY:

The Contractor will deliver the engine (to Oklahoma City OK) with:

· A non-incident statement from previous operator

· A FAA 8130-3 tag

· Either a test cell or on-wing Max Power Assurance Run Sheet with documented EGT margins at 80% N1, 85% N1 and 90% N1.

· A video boroscope of the entire engine to include fan, compressor, combustion and turbine sections; to include a boroscope report

· Its Historical Log Book and all associated documentation

· Trend analysis data (ECM) for at least 60 days of operation

· NOTE: Must cover a 60 day time-frame within the 180 days prior to proposal submission

· A parts listing for all Line Replaceable Units that are serially controlled

· Proof of AD compliance

· Proof of SB compliance

· Proof of life remaining (cycles) on Life Limited Parts

V. ACCEPTANCE:

JPATS will perform the following during the acceptance process:

· Review non-incident statement

· Review FAA 8130-3 tag

· Review and evaluate the Max Power Assurance Run Sheet

· Review and evaluate the video boroscope report

· Review the engine Historical Log Book and all associated documentation

· Review trend analysis data

· Perform a configuration audit of all installed Line Replaceable Units that are serially controlled

· Review AD compliance

· Review SB compliance

· Review life remaining on Life Limited Parts