737-400_DRY_LEASE_WITH_OPTION_TO_PURCHASE_STATEMENT_OF_WORK-SPECIFICATIONS.doc

March 16, 2015

STATEMENT OF WORK/ TECHNICAL SPECIFICATIONS

Aircraft Lease With Option to Purchase: Boeing 737-400 Aircraft Justice Prisoner and Alien Transportation System (JPATS)

Oklahoma City, Oklahoma I.

GENERAL

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.

JPATS has a requirement for the Lease with Option to Purchase of one (1) Boeing 737-400 aircraft to be operated from the JPATS Oklahoma City operational site. The aircraft will be operated by JPATS as Public Use aircraft meeting the mandatory requirements of Title 14 CFR Part 91 for operations in National Airspace. The period of performance will be: October 1, 2015 - September 30, 2016 with four (4) Option Years. JPATS will have the option to purchase the aircraft at any time during the base year or the option years.

II.

AIRCRAFT UTILIZATION

Based on current mission flying schedules, JPATS’ estimated utilization rate for the proposed aircraft will not exceed 750 flight hours or 500 takeoffs and landings (cycles) per year. “Flight Hour” by definition is “wheels off” during takeoff to “wheels on” during landing. The actual hours and cycles will vary due to scheduling demands.

III.

AIRCRAFT REQUIREMENTS / CONFIGURATION

A. Aircraft / General : The Contractor shall provide one (1) aircraft that, at time of Lease delivery:

1. Is a Boeing 737-400 jet aircraft with a United States of America registration (“N” number) as well as a current and valid FAA issued Standard Certificate of Airworthiness. (NOTE: Brand Name Requirement is based on pilot type certification, passenger seating, maintenance, repair parts and logistics support).

2. Has a printed copy of the Boeing Airplane Flight Manual (AFM) with Performance Specifications and Systems Description and Operation in English print and United States measurement units specific to the aircraft serial number.

3. Has a printed copy of the Boeing Flight Crew Operating Manual (Vol 1 and Vol 2) in English print and United States measurement units’ specific to the aircraft serial number.

4. Has two printed Boeing Quick Reference Handbook (QRH) in English print and United States measurement units specific to the aircraft serial number.

5. Has the Boeing current Weight and Balance Manual (if separate from the Airplane Flight Manual) in English print and United States measurement units.

6. Is accompanied with a current (within 12 calendar months) and valid (meeting FAA standards) weighing report in English print and US measurement units accomplished in accordance with the applicable Boeing weight and balance manual. At a minimum, the report will provide the aircraft’s configuration at weighing, empty weight, weight and moment for each gear, basic empty weight and basic empty weight present of MAC.

7. Is accompanied with the aircraft Layout of Passenger Accommodations (LOPA) in English print and United States measurement units.

8. Is accompanied with current aircraft Equipment List in English.

9. Is accompanied with documentation and manuals for the operation of the aircraft flight systems (e.g. FMS, TCAS, etc.) Aircraft specific serial number and current FCOM Vol. 1 and Vol. 2 will suffice in English print and United States measurement units.

10. Is accompanied by an up-to-date status report in respect to the aircraft, including the AD and SB status of the airframe, appliances, engines, and APU; status of hard time components, alterations, major repairs (337s / STCs), and flight hour / flight cycle summary.

11. Meets all specifications of its original Type Certificate in accordance with Title 14 CFR Part 25.

12. Has not accumulated, and will not accumulate, more than 40,000 total cycles since new (TCSN) during the contract period of performance (base year and option years).

13. Is certified for day, night, Visual Flight Rules (VFR), Instrument Flight Rules (IFR) operations and flight into known icing conditions.

14. Is accompanied with appropriate documentation testifying that the aircraft has not sustained any substantial damage as defined by National Transportation Safety Board 49 CFR Subpart A, General 830.2.

15. Has all cockpit and cabin instrumentation, avionics, placards, gauges readable in the English language and in the United States measuring system.

16. Is “Stage 3” noise level compliant with maximum takeoff noise levels not exceeding those levels as prescribed in Title 14 CFR Part 36, Section B36.5 (d) of appendix B and International Civil Aviation Organization (ICAO) Annex 16, Environmental Protection, Volume 1, Aircraft Noise, Third Edition, July 1993, Amendment 7, effective March 21, 2002, or later edition.

17. Is equipped with an Auxiliary Power Unit (APU) suitable for providing ground electrical power and self-contained engine starts. The APU must be capable of running two environmental systems, simultaneously, for ground heating or cooling the aircraft while maintaining 20 to 25 PSI duct pressure with output EGT within the Boeing maintenance manual limitations. The unit must be capable of supplying electrical power to the aircraft’s electrical system while airborne.

18. Is equipped with an APU that has passed a full gas path video borescope (as applicable).

19. Has a minimum of 156 passenger seats installed with a minimum pitch, between any two rows of seats, of 31 inches. Seats shall be “Tourist Class” configuration and meet Title 14 CFR Part 121 standards for the carriage of passengers. Seat cushions, seat covers and seat backs will conform to Title 14 CFR Part 121 burn criteria.

20. Has the first row of cabin seats on the Left side of the aircraft equipped with a rear-facing triple seat configuration meeting the requirements of Title 14 CFR Part 25.562. (See Attachment #1)

21. Has the first row of Right hand seats immediately forward of the forward most emergency exit equipped with a rear facing triple seat row installed meeting the requirements of Title 14 CFR Part 25.562. (See Attachment #1 – LOPA Example)

22. Is equipped with three (3) flushable lavatories, one located in the forward cabin and two located in the aft cabin, configured for external servicing.

23. Equipped with self-contained, powered, forward air stairs at the L-1 door.

24. Has all Life Limited Parts (LLP) that are associated with the airframe, engines, APU, appliances and landing gear at “mid-life” or greater meaning that they have 50% or greater life remaining based on the interval specified by the Boeing in terms of flight hours, flight cycles or calendar months and the projected aircraft utilization identified in paragraph II.

25. Is powered by the CFM56-3C1 engine with no fixed derate.

26. Has engines with a minimum of 5,000 cycles remaining prior to any scheduled shop visit (scheduled off-wing maintenance) with any recurring inspections identified.

27. Is accompanied by an on-wing Max Power Assurance Run sheet showing clear documentation of 3C1 (23,500 LBS of thrust) EGT Margins of not less than 20 degrees for each installed engine. This requirement must be current and valid and have been performed after the last flight of the previous operator and prior to the first flight by JPATS

28. Has engines eligible for enrollment in an “industry standard” Power by the Hour engine maintenance program.

29. Is accompanied by a video boroscope record of each installed engine with a written boroscope report detailing the internal health of the engines to include the fan, compressor, combustion and turbine sections of the engine. This requirement must be current and valid and have been performed after the last flight of the previous operator (or acceptance flight) and prior to the first flight by JPATS

30. Is accompanied by a Magnetic Chip Detector Inspection of each installed engine in accordance with the Boeing Aircraft Maintenance Manual (AMM) and as witnessed by JPATS personnel.

31. Is in compliance with all applicable published FAA Airworthiness Directives (AD) and Boeing Mandatory Service Bulletins (SB). Any repetitive (recurring) inspections that are associated with these ADs and SBs must not come due within the base year of the contract.

32. Is in compliance with all calendar, flight hour, flight cycle maintenance inspections and events from either a Boeing or FAA approved maintenance program.

33. Has no “Scheduled” Heavy Maintenance or Major Inspection (C Check or higher) due in the base year of the contract.

34. Is equipped with emergency equipment and over water passenger operations equipment in accordance with Title 14 CFR Parts: 121.309, 121.310, 121.337, and 121.339.

35. Has the highest Boeing Gross (Maximum) Take Off weight of 150,000 pounds, highest Gross (Maximum) Landing Weight of 124,000 pounds, and highest Maximum Zero Fuel Weight of 117,000 pounds.

36. Has an operational Class C fire detection and suppression system conforming to Title 14 CFR Parts 25 and 121.

37. Has the minimum number of flight attendant seats required by Title 14 CFR Part 121.

38. Has standard “airline” type and style galleys with service carts, coffee makers, and ovens installed.

39. Has a reinforced Flight Deck Door meeting the standards for a Title 14 CFR Part 121.313 commercial air carrier.

40. Has non-descript paint scheme with no logos from any previous operator visible.

41. Has it’s appropriately assigned U.S. registration (“N”) number applied to the aircraft in accordance with Title 14 CFR Part 45.25 requirements.

42. Is equipped with main landing gear tire assemblies, size H42x16-19/24.

43. Is equipped with brake assemblies, Part Number: 2606672-4.

44. Has each hard time controlled component, and life limited component serviceable and supported by appropriate installation certification documentation with either the EASA Form 1 or FAA Form 8130-3.

45. Has all impact structural damages (regardless of cause) permanently repaired in accordance the Boeing Structural Repair Manual (SRM) or other EASA / FAA-approved data. There shall be no temporary repairs, time-limited repairs or repairs requiring repetitive inspections.

46. Is free of fuel, oil, hydraulic and pneumatic leaks that are beyond the permitted limits set forth in the maintenance manual. Any repair of leaks will have been permanent repairs.

47. Has a fuselage free of dents and abrasions.

48. Has windows free from delamination, blemishes, crazing and properly sealed with all window shades operating smoothly.

49. Has doors that are free moving, correctly rigged and with serviceable seals.

50. Has the wing’s and stabilizer’s leading edges serviceable in accordance with AMM limits (e.g. no significant hail or other foreign object damage).

51. Has wings free of fuel leaks as demonstrated by the Boeing’s relevant testing guidelines.

52. Has horizontal stabilizer and empennage leading edges serviceable in accordance with AMM limits (e.g. no significant hail or other foreign object damage.)

B. Avionic/Navigation/Auto Flight System: In addition to the requirements of Paragraph A the aircraft shall have, as a minimum, the following at the time of delivery to JPATS:

1. Flight Management Systems (FMS) with software version U10.8a and navigation database subscription for the duration of the lease from the date of delivery for worldwide database navigation data conforming to WGS-84 coordinate system, such as the Jeppessen JEP 5, or equal. Additionally, the airport database will incorporate all airports with an instrument approach procedure (IAP) and a runway greater than 5,000 feet in length within the geographical area as defined by the Continental United States (CONUS), Alaska, Hawaii, Canada, Caribbean, Latin America and South America regions.

2. Global Navigation Satellite System (GNSS) specifically, have installed and operating per Boeing’s Flight Operations Manuals, a single required, dual preferred, GPS position updating system, capable of gaining operational approval to conduct Title 14 CFR part 97 instrument procedures within the U.S. National Airspace System (NAS) where domestic air traffic control (ATC) procedures are applied.

3. Capable of navigating RNAV 1 & 2 Airway Routes, Q-Routes and T-Routes, Standard Instrument Departure (SID), and Standard Terminal Arrival Routes (STAR) requiring GPS.

4. At a minimum be certified to execute RNAV/GPS IAPs requiring GPS to LNAV minimums with an appropriate approval certification statement in the Aircraft Flight Manual (AFM), Pilots Operating Manual (POM), or aircraft approved avionics operating manual.

5. The FMS must be fully interfaced with and receive navigational data/inputs from a minimum of two Inertial Reference Systems (IRS), or a minimum of one, preferably two, Global Navigation Satellite Systems (GPS position updating systems), and a minimum of two (2) radio navigation systems.

6. A Flight Guidance/Autopilot System capable of meeting the required lateral and vertical RNAV/VNAV capabilities while coupled to the LNAV system.

7. An Electronic Flight Instrument System (EFIS) consisting of both pilot and copilot:

(a) Electronic Attitude Director Indicator (EADI) with integrated airspeed format display with single and or dual cue capability flight directors.

(b) Electronic Horizontal Situation Indicator (EHSI) utilizing a heading up and not track up display format with TCAS system integrated into display.

(c) Engine gauge EFIS display in United States measurement units.

8. Three (3) digital VHF transceivers communication systems with a minimum of 760 channels with 8.33 KHZ spacing. *All three (3) of these systems will be for voice communication.

9. One (1) HF transceiver communication system with SELCAL.

10. One (1) Honeywell RDR-4B Radar system meeting the requirement of Title 14 CFR Part 121.357 fully interfaced with TAWS mapping for auto tilt functions.

11. One (1) Enhanced Ground Proximity Warning System (EGPWS) with low level wind shear detection meeting the requirement of Title 14 CFR Part 121.358.

12. All aircraft equipment and components necessary for certification for flight operations in Reduced Vertical Separation Minimum (RVSM) airspace.

13. Two (2) Air Data Computers.

14. Class A TAWS conforming to TSO-C151b dated Dec. 17, 2002.

15. Two (2) digital VHF, VOR/LOC navigation receivers.

16. Two (2) glide slope receivers with a minimum of 40 receive channels.

17. One (1) marker beacon receiver systems.

18. Two (2) digital ADF navigation systems.

19. Two (2) Mode S Transponder systems.

20. Traffic Collision Avoidance System (TCAS) II system that meets TSO C–119b (version 7.0), or a later version integrated into the EHSI display.

21. Two (2) Radio Altimeter systems.

22. One (1) Solid State Digital Flight Data Recorder, such as the L3 Flight Data Recorder P/N FA2100-4043-00 or equivalent, which complies with Title 14 CFR Part 121.343 and 131.344 including Part 121 Appendix B and M as applicable.

23. Quick-Access Recorder (QAR) conforming to the USMS Flight Operations Quality Assurance (FOQA) program. The current program hardware accepted QAR is the L3 Micro QAR combined with the Honeywell Digital Flight Data Acquisition Unit (DFDAU) P/N 967-0212-002 utilizing 737-5 data frame for QAR readouts.

24. One (1) Digital Cockpit Voice Recorder.

25. Two (2) Distance Measuring Equipment (DME) Systems, with Nav-1 and Nav-2 channeling.

26. One (1) Altitude Pre-select/Alerter system.

27. Wiring for one (1) Air Cell ST 3100 Iridium Telecommunication Systems (satellite communication system). Supplied system to include coax and antenna capable of supporting a cockpit mounted handset and a cabin mounted handset provided by the U.S. Marshals Service.

28. Digital auto throttle system.

IV

Maintenance / Logistics Support

NOTE:

Applicable during the lease period only. JPATS will assume all maintenance responsibility should the option to purchase be exercised.

JPATS Responsibilities:

1. JPATS will be responsible to perform all Line Maintenance and Line Servicing maintenance inspection and repairs to include the associated logistics requirements. This will be performed by a Title 14 CFR Part 145 Certificated Repair Station (CRS) under a separate contract. All maintenance will be performed on this lease aircraft without discrimination when compared to the Boeing 737-400 aircraft owned and operated by JPATS. Maintenance, inspection and repairs will be to a Title 14 CFR Part 91 standard. JPATS will utilize the polcies and procedures detailed in the USMS General Maintenance Manual (GMM) (See Attachment #2) in the performance of these Line Maintenance and Line Servicing responsibilities.

2. JPATS will be responsible to utilize the JPATS Daily Flight Log Books, FAA Form 337, and United States Marshal Service (USMS) Routine and Non-Routine Work Order Forms for documenting maintenance, inspections and repairs of this aircraft made during the period of this lease.

3. JPATS will be responsible to make all appropriate entries into the Aircraft, Engine, and APU Historical Log Books for all applicable maintenance, inspections and repairs of this aircraft made during the period of this lease.

4. JPATS will be responsible to develop and utilize an automated maintenance tracking program for this aircraft in accordance with the Boeing’s Maintenance Planning Document (MPD) and will be used to identify, track and document all maintenance events performed or coming due during the duration of this lease. This program will be a program common to the aviation industry and will meet a Title 14 CFR Part 91 standard such as CAMPS / Daniels.

5. JPATS will be responsible for attaining, maintaining and utilizing “approved data” to include all required Aircraft Maintenance Manuals (AMM), Illustrated Parts Catalogs (IPC), Structural Repair Manual (SRM) and Wiring Diagram Manual (WDM).

6. JPATS will be responsible for the acquisition of all parts, materials, consumables, free stock, and lubricants required to maintain the aircraft in a safe airworthy condition as detailed in the maintenance and inspection program as well as to correct pilot reported discrepancies (PIREPS). All parts purchased will be done so utilizing acquisition policies and procedures of the aforementioned Title 14 CFR Part 145 CRS using their Approved Vendor List of certified FAA vendors. All parts installed will have FAA Forms 8130-3 attached and will have a since “birth” traceability.

7. JPATS will be responsible for all costs in connection with or related to the use, movement and operation of the Aircraft. Such costs include, but are not exclusive of the costs of flight crews, cabin personnel, fuel, oil, storage, landing and navigation fees, airport charges, passenger services and any and all other mission related expenses.

8. JPATS will be responsible for the accomplishment of FAA issued Airworthiness Directives (AD) with a compliance date falling within the period of this lease, base year and option years, that can be performed at a Line Maintenance level and does not exceed $25,000 in total cost.

9. JPATS will be responsible for the accomplishment of Boeing issued Mandatory Service Bulletins (SB) with a compliance date falling within the period of this lease, base year and option years, that can be performed at a Line Maintenance level and does not exceed $25,000 in total cost.

Contractor Responsibilities:

1. The Contractor will be responsible to perform all “Scheduled” Heavy Maintenance to include scheduled Major Inspections; C Checks or higher, to include “Non-Routine” Discrepancies identified during the heavy maintenance or major inspections. These Heavy Maintenance events and Major Inspections will be performed by a Title 14 CFR Part 145 Certificated Repair Station (CRS) to a Title 14 CFR Part 91 standard, as a minimum.

NOTE:

JPATS defines Heavy Maintenance as any maintenance event to include maintenance, inspection, repair, alteration or overhaul, whether this event is scheduled or unscheduled, that exceeds the technical capabilities of the assigned line maintenance provider; for reasons such as; but not limited to, lack of technical training / expertise, lack of proper facilities (hangar), lack of available manpower, lack of available man-hours, lack of ground support equipment, special tools, test sets, procedures, or fixtures. Scheduled Heavy Maintenance is normally associated with a Major Inspection such as an aircraft C Check or above.

JPATS further defines “Heavy Maintenance” as all scheduled checks at the C-check level or higher; all major repairs, alterations and inspections as defined by Title 14 CFR Part 1.1; engine, APU, and landing gear changes or engine, APU, and landing gear repairs requiring approved data at the Component Maintenance Manual (CMM) level, vice Aircraft Maintenance Manual (AMM) level; or when structural repairs are estimated to require 500 man-hours or more to accomplish.

2. The Contractor will be responsible for the accomplishment of “Unscheduled” Heavy Maintenance on the aircraft or engines. When such heavy maintenance was a direct result of the actions, or inactions, on the part of JPATS employees, or the employees of JPATS Line Maintenance Contractor, reimbursement for this maintenance will be made to the Contractor as an Over and Above effort under a separate Contract Line Item Number (CLIN).

NOTE:

JPATS defines Heavy Maintenance as any maintenance event to include maintenance, inspection, repair, alteration or overhaul, whether this event is scheduled or unscheduled, that exceeds the technical capabilities of the assigned line maintenance provider; for reasons such as; but not limited to, lack of technical training / expertise, lack of proper facilities (hangar), lack of available manpower, lack of available man-hours, lack of ground support equipment, special tools, test sets, procedures, or fixtures. Scheduled Heavy Maintenance is normally associated with a Major Inspection such as an aircraft C Check or above.

JPATS further defines “Heavy Maintenance” as all scheduled checks at the C-check level or higher; all major repairs, alterations and inspections as defined by Title 14 CFR Part 1.1; engine, APU, and landing gear changes or engine, APU, and landing gear repairs requiring approved data at the Component Maintenance Manual (CMM) level, vice Aircraft Maintenance Manual (AMM) level; or when structural repairs are estimated to require 500 man-hours or more to accomplish.

JPATS will reposition the aircraft for heavy maintenance under the following conditions: 1) JPATS has pilots available; 2) The aircraft is signed off as “airworthy” in the JPATS flight log the day of the reposition flight; 3) The reposition is within the 48 contiguous U.S.; 4) All fuel costs will be the responsibility of the Lessor; 5) JPATS pilots will not perform any Functional Check Flights (FCF) required after heavy maintenance; and 6) JPATS pilots will not perform any required test flights after heavy maintenance.

3. The Contractor will be responsible for “off-wing” engine maintenance such as an engine shop visit. When the “off-wing” maintenance or engine shop visit was the direct result of actions, or inactions, on the part of JPATS employees, or the employees of JPATS Line Maintenance Contractor, reimbursement will be made to the Contractor as an Over and Above effort under a separate Contract Line Item Number (CLIN).

4. The Contractor will be responsible to secure a “spare” CFM56-3C1 engine to be utilized by JPATS in keeping the aircraft in revenue service in the event an installed engine must be removed for performance deterioration restoration or an unscheduled failure such as FOD damage.

5. When the Aircraft undergoes any scheduled or unscheduled Heavy maintenance exceeding five (5) days during any month during the Lease Term, the monthly lease rate will abate on a daily basis commencing on the sixth (6th) day after induction of the Aircraft into a maintenance, repair and overhaul facility for the purpose of such Heavy Maintenance and ending on such date as the Aircraft is returned to JPATS. No abatement shall apply in the event that the Heavy Maintenance event is required solely as a result of JPATS’ operation of the Aircraft and unrelated to ordinary wear and tear or latent defects.

6. The Contractor shall ensure that all Heavy Maintenance to the Aircraft is accomplished at an FAA Certificated Repair Station (CRS) utilizing the Repair Station Manual (RSM) and approved data. The CRS shall provide a complete record of all work performed and execute an appropriate return to service.

7. The Contractor shall provide a certificate of insurance or documentation evidencing the insurance of the Aircraft.

V.

DELIVERABLES

Table No. 1 - Deliverables

Delivered with aircraft

VI.

DELIVERY, INSPECTION AND ACCEPTANCE OF THE AIRCRAFT

A. Aircraft -- The Government will inspect the Contractor’s proposed aircraft utilizing a Delivery Inspection Checklist to verify that the aircraft complies with all of the requirements of the Contract.

B. Deliverables --In addition to the aircraft, during the final delivery, inspection, and acceptance process, the Contractor must provide all contract deliverables as identified in this Statement of Work, Table 1, Deliverables (Items 2-10). All flight deck presentations, placards, cockpit indications and gages and associated navigational equipment/instruments and manuals and supporting documentation all in the English language and U.S. standard measurement system.

C. Delivery -- The Contractor shall configure the aircraft for delivery, inspection and acceptance to Oklahoma City, Oklahoma, not later than six (6) weeks from Date of Award. The aircraft shall be delivered in good working order, condition and appearance, with all pilot discrepancies and deferred maintenance items cleared, clean by commercial airline standards and ready for flight with all of the aircraft equipment, components and systems operating within limits specified in the Maintenance Manual and functioning in accordance with their intended use. There shall be no “on-watch” conditions, special callouts, special repetitive inspections, special waivers or exemptions in effect on the Airframe, any Engine, the APU or any part. The aircraft shall be in full compliance with the rules and regulations of the FAA and with applicable Type Certificate Data Sheets. Each AD issued by the FAA and with a compliance date on or prior to Delivery shall be complied with.

D. Delivery/Inspection and Acceptance Flight –

1. The Government will inspect the delivered aircraft to verify that it complies with the contract's requirements. The Government will have seven (7) calendar days to conduct its inspection of the configured aircraft and associated deliverables. During the inspection, the Government will document any findings where the aircraft /deliverables do not meet the contract's requirements. The delivery and inspection process will also include a Maximum Power Assurance Run Check on each Engine in accordance with the Maintenance Manual, a Chip Detector Inspection, and an evaluation of the cruise and take-off trend analysis followed by an Acceptance Flight. This will be done at the Contractor’s expense and shall be overseen by JPATS representatives.

2. The acceptance flight is meant to demonstrate the takeoff and landing capabilities and the en route characteristics of the proposed aircraft. It shall be performed by pilots provided by the Contractor; however, a JPATS pilot shall sit in the center cockpit "jump" seat on the flight deck during this acceptance flight as the official Government observer. This acceptance flight shall be based on a mutually agreed flight profile for duration not to exceed two hours and shall take place at the Delivery Location. All costs and expenses associated with this flight shall be the sole responsibility of the Contractor. The operating parameters of each Engine noted during the take-off power check shall be recorded. An acceptance flight will be deemed successful if all aircraft systems are fully operational and function properly during the reposition flight, and the aircraft exhibits an acceptable level of trim, stability, manoeuvrability, and controllability as determined by the JPATS pilot. Any inoperative or improperly functioning component or system discovered during the acceptance flight shall be documented by the JPATS pilot in the applicable flight log book.

3. After the Delivery/Inspection and the Acceptance Flight, the Contractor shall correct all deficiencies within five (5) calendar days from the date it receives the Government's notice to correct deficiencies, or in a time frame agreed to by the Contracting Officer, prior to a final determination of acceptance by the Government. After the acceptance flight, the Contractor shall perform an inspection of each magnetic chip detector and a full video borescope inspection of each Engine (including, but not limited to, the hot, cold and combustor sections) and the APU. These inspections will be accomplished at the Contractor’s expense. Any deficiencies shall be corrected at the Contractor’s expense.

E. Termination for Cause -- If, after this inspection process, it is determined by the Government that any proposed aircraft is not acceptable or is unavailable for delivery on the required delivery date, the Government may terminate for cause this contract in whole or in part at no cost to the Government.

SOW ATTACHMENTS:

Attachment #1 – Layout of Passenger Accommodations (LOPA) Example (1 page) Attachment #2 – USMS General Maintenance Manual (GMM) (298 pages)