Document:

exhibit1037_09wje-pax051

 Page 1  BOEING PROPRIETARY        SERVICE LIFE POLICY COMPONENTS     between    THE BOEING COMPANY    and    ALLEGIANT AIR, LLC    SUPPLEMENTAL EXHIBIT SLP1    TO PURCHASE AGREEMENT NUMBER PA-05130  

 

WJE-PA-05130-SLP1 Page 2  BOEING PROPRIETARY    SERVICE LIFE POLICY COMPONENTS    relating to    BOEING MODELS 737-8-200 AND 737-7 AIRCRAFT    This is the listing of SLP Components for the Aircraft which relate to Part 3,  Boeing Service Life Policy of Exhibit C, Product Assurance Document to the AGTA and  is a part of Purchase Agreement No. PA-05130.  1. Wing.  (i) Upper and lower wing skins and stiffeners between the  forward and rear wing spars.  (ii) Wing spar webs, chords and stiffeners.  (iii) Inspar wing ribs.  (iv) Inspar splice plates and fittings.  (v) Main landing gear support structure.  (vi) Wing center section lower beams, spanwise beams and floor  beams, but not the seat tracks attached to floor beams.  (vii) Wing-to-body structural attachments.  (viii) Engine strut support fittings attached directly to wing primary  structure.  (ix) Support structure in the wing for spoilers and spoiler  actuators; for aileron hinges and reaction links; and for  leading edge devices and trailing edge flaps.  (x) Trailing edge flap tracks and carriages.  (xi) Aileron leading edge device and trailing edge flap internal,  fixed attachment and actuator support structure.  2. Body.  (i) External surface skins and doublers, longitudinal stiffeners,  longerons and circumferential rings and frames between the  forward pressure bulkhead and the vertical stabilizer rear  spar bulkhead and structural support and enclosure for the  APU but excluding all system components and related  installation and connecting devices, insulation, lining, and  decorative panels and related installation and connecting  devices.  (ii) Window and windshield structure but excluding the windows  and windshields.  

 

WJE-PA-05130-SLP1 Page 3  BOEING PROPRIETARY  (iii) Fixed attachment structure of the passenger doors, cargo  doors and emergency exits, excluding door mechanisms and  movable hinge components. Sills and frames around the  body openings for the passenger doors, cargo doors and  emergency exits, excluding scuff plates and pressure seals.  (iv) Nose wheel well structure, including the wheel well walls,  pressure deck, bulkheads, and gear support structure.  (v) Main gear wheel well structure including pressure deck and  landing gear beam support structure.  (vi) Floor beams and support posts in the control cab and  passenger cabin area, but excluding seat tracks.  (vii) Forward and aft pressure bulkheads.  (viii) Keel structure between the wing front spar bulkhead and the  main gear wheel well aft bulkhead including splices.  (ix) Wing front and rear spar support bulkheads, and vertical and  horizontal stabilizer front and rear spar support bulkheads  including terminal fittings but excluding all system  components and related installation and connecting devices,  insulation, lining, and decorative panels and related  installation and connecting devices.  (x) Support structure in the body for the stabilizer pivot and  stabilizer screw.  3. Vertical Stabilizer.  (i) External skins between front and rear spars.  (ii) Front, rear and auxiliary spar chords, webs and stiffeners  and attachment fittings.  (iii) Inspar ribs.  (iv) Rudder hinges and supporting ribs, excluding bearings.  (v) Support structure in the vertical stabilizer for rudder hinges,  reaction links and actuators.  (vi) Rudder internal, fixed attachment and actuator support  structure.  4. Horizontal Stabilizer.  (i) External skins between front and rear spars.  (ii) Front and rear spar chords, webs and stiffeners.  (iii) Inspar ribs.  (iv) Stabilizer center section including hinge and screw support  structure.  

 

WJE-PA-05130-SLP1 Page 4  BOEING PROPRIETARY  (v) Support structure in the horizontal stabilizer for the elevator  hinges, reaction links and actuators.  (vi) Elevator internal, fixed attachment and actuator support  structure.  5. Engine Strut.  (i) Strut external surface skin and doublers and stiffeners.  (ii) Internal strut chords, frames and bulkheads.  (iii) Strut to wing fittings and diagonal brace.  (iv) Engine mount support fittings attached directly to strut  structure and including the engine-mounted support fittings.  6. Main Landing Gear.  (i) Outer cylinder.  (ii) Inner cylinder, including axles.  (iii) Upper and lower side struts, including spindles, universals  and reaction links.  (iv) Drag strut.  (v) Orifice support tube.  (vi) Downlock links including spindles and universals.  (vii) Torsion links.  (viii) Bell crank.  (ix) Trunnion link.  (x) Actuator beam, support link and beam arm.  7. Nose Landing Gear.  (i) Outer cylinder.  (ii) Inner cylinder, including axles.  (iii) Orifice support tube.  (iv) Upper and lower drag strut, including lock links.  (v) Steering plates and steering collars.  (vi) Torsion links.  NOTE: The Service Life Policy does not cover any bearings, bolts, bushings, clamps,  brackets, actuating mechanisms or latching mechanisms used in or on the SLP  Components.exhibit1038_10wje-pax051

    This copy of the document filed as an Exhibit excludes certain identified information because  such information is both (i) not material and (ii) would likely cause competitive harm if publicly  disclosed. Omissions are designated by the symbol [...***...].       The Boeing Company   P.O. Box 3707   Seattle, WA 98124 2207     Page 1  BOEING PROPRIETARY    WJE-PA-05130-LA-2101477      Allegiant Air, LLC  1201 N. Town Center Drive  Las Vegas, NV 89144      Subject: [...***...]    Reference: Purchase Agreement No. PA-05130 (Purchase Agreement) between The  Boeing Company (Boeing) and Allegiant Air, LLC (Customer) relating to  Model 737-8-200 aircraft and Model 737-7 aircraft (each or collectively,  Aircraft)    This letter agreement (Letter Agreement) amends and supplements the  Purchase Agreement. All terms used but not defined in this Letter Agreement will have  the same meaning as in the Purchase Agreement.  The Purchase Agreement incorporates the terms and conditions of WJE-AGTA  between Boeing and Customer. This Letter Agreement modifies certain terms and  conditions of the AGTA with respect to the Aircraft.    1. [...***...].  1.1 [...***...].   1.2 [...***...].  

 

  WJE-PA-05130-LA-2101477 Page 2  BOEING PROPRIETARY  1.3 [...***...].  Months Prior to Delivery Amount Due  [...***...] [...***...]  [...***...] [...***...]  [...***...] [...***...]  [...***...] [...***...]  [...***...] [...***...]    2. [...***...].  2.1 [...***...] the Purchase Agreement [...***...] Customer [...***...]. Other  terms and conditions [...***...] Agreement for the Aircraft.  2.2 [...***...]the Purchase Agreement.  [...***...] Boeing [...***...] Customer  [...***...] prior to delivery of the Delivering Aircraft.  3. [...***...] described in Article 1 above, [...***...].  3.1 [...***...] Customer [...***...].  3.2 [...***...] Customer [...***...] Customer and Boeing [...***...].   4. [...***...].  4.1 Customer [...***...], on:  (i) [...***...] under the Purchase Agreement,   (ii) [...***...] between Boeing and Customer, or   (iii) [...***...] with Boeing,  [...***...], then Boeing may, [...***...] Customer, [...***...] Non-Payment [...***...].    4.2 If Boeing [...***...] to Boeing, [...***...] instruction from Boeing to the  contrary, [...***...] designated by Boeing.  4.3 For all purposes of this Article 4, including without limitation, notice,  [...***...]. Nothing herein will constitute [...***...] of Boeing; all [...***...] will be [...***...].  Boeing expressly reserves all of its rights and remedies under any agreement and  applicable law.    5. [...***...].  

 

  WJE-PA-05130-LA-2101477 Page 3  BOEING PROPRIETARY  5.1 Customer [...***...].  5.2 Notwithstanding any [...***...] of this Letter Agreement or the Purchase  Agreement, [...***...] Letter Agreement are provided to Customer in consideration of  Customer becoming the operator of the Aircraft and cannot be assigned, in whole or in  part, without the prior written consent of Boeing. . Nothing in this statement is intended  to support recovery from Allegiant of any benefits supplied hereunder for delivered  Aircraft.  6. Confidentiality.  The information contained herein represents confidential business information  and has value precisely because it is not available generally or to other parties.  Customer will limit the disclosure of its contents to (i) Customer and Customer affiliates’  employees, officers and directors and (ii) Customer and Customer affiliates’ legal  counsel, professional advisors and auditors subject to a duty of confidence or a non- disclosure undertaking, in each case with a need to know the contents for purposes of  helping Customer perform its obligations under the Purchase Agreement and who  understand they are not to disclose its contents to any other person or entity without the  prior written consent of Boeing unless disclosure is required by applicable law or court  order, in which case, Customer shall (i) notify Boeing in writing of such disclosure  requirement or request prior to making such disclosure, and will take steps to protect  the information contained herein, and (ii) use reasonable efforts to obtain redaction and  confidential treatment for the disclosed information or parts thereof.  In addition, with  respect to disclosure of the contents hereof to third parties who may be or are involved  with financing (in any form, including sale and lease-back) of Aircraft (and/or Advance  Payments) under the Purchase Agreement, Customer shall be entitled to disclose such  information to such third party financiers, after consultation with Boeing, as the parties  shall mutually agree (each acting reasonably and within industry and financing norms).   In addition to any equitable relief that may be available to the damaged party in  the event of a breach of this paragraph, the damaged party will have remedies available  to it under the Purchase Agreement and at law. If the foregoing correctly sets forth your  understanding of our agreement with respect to the matters contained herein, please  indicate your acceptance and approval below.  

 

  WJE-PA-05130-LA-2101477 Page 4  BOEING PROPRIETARY    ACCEPTED AND AGREED TO this          Date:           ALLEGIANT AIR, LLC   THE BOEING COMPANY       By:   By:        Name:   Name: [...***...]       Title:   Title: Attorney-In-Fact

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