DRAFT_SOW.docx

TECHNICAL SPECIFICATIONS-REQUIREMENTS

AIRCRAFT ENGINE (CFM56-3C1) LEASE

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 Lease (with the option to purchase) of one 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. The period of performance will be: October 1, 2014 - September 30, 2015 with four (4) Option Years.

III. TECHNICAL REQUIREMENTS:

The engine must have a maximum takeoff rated thrust of 23,500 pounds with no fixed de-rate. During this period of performance the engine will be operated under the USMS Reduced Power Takeoff Program with takeoff rated thrust set at 22,000 pounds of thrust via the aircraft’s Flight Management System (FMS). All FAA Airworthiness Directives (AD) must be accomplished with no recurring inspections due during the base year of the contract. 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 during the base year of the contract. 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 during this period of performance. 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.

“Stores Program”: The engine is to be in a formal “stores” program at the Contractor’s facility until needed by JPATS. The engine must be able to be shipped to the JPATS Oklahoma City operational site within 24 hours of being notified by JPATS of the requirement. Alternate destinations may also be required in that a need for a replacement engine may occur at an enroute location other than Oklahoma City. The engine Historical Log Book will be shipped to JPATS when the engine is shipped; either together or separately. The Contractor shall be responsible to perform all periodic (calendar) inspections, lubrication, corrosion prevention control program (CPCP) items, maintenance and servicing on this engine while in the “stores” program at their facility. The Contractor is also responsible to accomplish Airworthiness Directives (AD) and manufacturer Service Bulletins (SB) with dates of compliance within the contract period of performance whether the engine is in the stores program at their facility or installed on a JPATS controlled aircraft.

IV. TECHNICAL APPROACH:

When required to be installed and operated on a JPATS controlled aircraft, the estimated utilization of this engine will not exceed 140 flight hours and 100 flight cycles per month. It will be operated exclusively by the USMS and will not be sub-leased to any other entity; government or civil. This engine will be operated to Title 14 CFR Part 91 standards at all times during this lease period. All required line maintenance, line servicing and routine (minor) inspections will be performed by a Title 14 CFR Part 145 Certificated Repair Station (CRS) in accordance with the policies and procedures detailed in their FAA approved Inspection Procedure Manual (IPM) and the applicable Aircraft Maintenance Manual (AMM). Title 14 CFR Parts 91 and 43 will be the standard for all routine maintenance, inspections, repairs and servicing performed on this engine. Routine maintenance, inspection, repairs, and servicing will be based on the aircraft manufacturer’s Maintenance Planning Document (MPD) or on an FAA approved maintenance and inspection program. Any parts replaced by JPATS while the engine is installed on a JPATS controlled aircraft during this period of performance will come from FAA approved vendors and have FAA 8130-3 serviceable tags attached. Airworthiness determination for dispatch will be made in accordance with the Boeing MMEL. Maintenance items having relief specified in the MMEL will be deferred in accordance with policies and procedures outlined in the USMS General Maintenance Manual (GMM).

V. DELIVERY:

Upon JPATS’ request (when the engine is required) the Contractor will deliver the engine with:

· A non-incident statement

· A FAA 8130-3 tag

· Either a test cell or on-wing Max Power Assurance Run Sheet with documented EGT margins at 22,000 pounds of thrust and 23,500 pounds

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

· Its Historical Log Book and all associated documentation

· Trend analysis for at least the previous 90 days of operation

· A parts listing for all Line Replaceable Units that are serially controlled and shows traceability back to birth

VI. ACCEPTANCE:

When the engine is required for installation by JPATS; JPATS will perform the following during the acceptance process:

· An on-wing Max Power Assurance Run Sheet documenting EGT margins at 22,000 pounds of thrust and 23,500 pounds

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

· A review and analysis of the engine Historical Log Book and all associated documentation

· A trend analysis evaluation for at least the previous 90 days of operation

· An inspection of the engine chip detectors

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

VII. REDELIVERY:

When the engine is no longer required by JPATS, and is removed from the JPATS aircraft, it will be returned to the Contractors facility and re-entered into a formal “stores” program. The Contractor will take any and all actions required to ensure the engine is deemed serviceable and acceptable for future shipments and installation on a JPATS aircraft as required by JPATS and the applicable FAA regulatory requirements. During this re-delivery process, JPATS will perform:

· An on-wing Max Power Assurance Run Sheet documenting EGT margins at 22,000 pounds of thrust and 23,500 pounds

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

· A review and analysis of the aircraft flight log books capturing all maintenance and inspections performed on the engine during the period of performance to include all parts installed and FAA 8130-3 tags

· A trend analysis evaluation for the period of engine operation

· An inspection of the engine chip detectors

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

· Delivery of a non-incident statement for the period of engine operation