Gulfstream

Gulfstream PRODUCT SUPPORT PROPOSAL Prepared for Presented by G.... G550 Serial Number 5070 J. Aviation Business Jets AG Mr. Martin Eibioht Stephan Forte Regional Sales Manager, Gulfstream Aerospace Gulf.... Proposal It 7019199, ROI 26 June 2015 EFTA01105556 TABLE OF CONTENTS PART I. Workscope Description 3 A. Interior Refurbishment 3 B. Avionics Cabin Electronics 3 C. Mechanical 3 D. Paint 3 PART II. Contingencies and Assumptions of Proposal Offer 4 A. Estimated Leadtime 4 B. Estimated Downtime 4 C. Pricing and Scheduling Terms 4 D. General Contingencies 5 E. Addendum to Proposal and Work Authorization Terms and Conditions 6 PART III. Payment Terms and Remittance Instructions 7 PART IV. Executive Summary and Proposal Acceptance 8 EFTA01105557 warn ( 1 *1 (l) ID # 7018737, R00 15 June 2015 Gulfstream G550 Serial Number 5070 Jet Aviation Business Jets AG PART I. Workscope Description A. INTERIOR REFURBISHMENT Not Requested B. AVIONICS / CABIN ELECTRONICS Not Requested C. MECHANICAL 1. Aircraft Maintenance 1.1 CMP Tasks (Customer Supplied) (Labor Only) $58,204 Accomplish CMP tasks (customer supplied) (Exhibit 1). Note: Correction of discrepancies is not included in the quoted price. 1.2 CB 157 Inspection, Main Landing Gear Door Actuator (Labor Only) $274 This Customer Bulletin (CB 157) is a one-time action to review the installation records of the main landing gear door actuators, Part Number 1159H20264, to determine current life cycle usage and report the findings to Gulfstream. Effectivity: Aircraft Serial Numbers 5001 through 5485, 5487, 5490, 5491 and 5494. Note: Aircraft records must be made available to Gulf stream to comply with this Customer Bulletin. 1.3 BR[SSN REDACTED]50 PDLA Spherical Bearing $1,230 Accomplish Rolls-Royce SB BR[SSN REDACTED]50 - Exhaust - Thrust reverser unit (TRU) - inspection of spherical bearing of the primary door lock actuator (PDLA) and cleaning of the S-Hook Assembly Non-Modification Bulletin. This Non-Modification Service Bulletin includes the procedure for the inspection of the spherical bearing assembly of the PDLA and for the cleaning and inspection of the S-hook assembly. Effectivity: • One (1) BR700-710A1-10 Engines. Thrust Reverser Units (TRU) which have the Primary Door Lock Actuator (PDLA) with the Part Number P466A0001-01 installed. • Two (2) BR700-710A2-20 Engines. Thrust Reverser Units (TRU) which have the Primary Door Lock Actuator (PDLA) with the Part Number P466A0001-01 installed. • Three (3) BR700-710C4-11 Engines. Thrust Reverser Units (TRU) which have the Primary Door Lock Actuator (PDLA) with the Part Number P466A0001-01 installed. Compliance: Rolls-Royce Deutschland recommends that this Non-Modification Service Bulletin be accomplished at the earliest opportunity without undue interruption to the flight schedule on engines which have more than 500 flight hours. For spare engines and modules, Rolls-Royce Deutschland recommends this Non-Modification Service Bulletin be accomplished before installation. Concurrent Requirements: Gulfstream CMP 783337 and 783338. Note: This item only includes the inspection and cleaning of the spherical bearings and S-Hooks. Any parts requiring replacement (Labor and Material) will be accomplished on a time and material basis. 1.4 Aircraft Return to Operation after Non Standard Storage SGER-318 (Budgetary) $33,000 Accomplish aircraft return to operation after Non Standard Storage SGER-318. D. PAINT Not Requested Page 3 of 10 This proposal is confidential between Gulfstream and the Customer. J an Return to Table of Contents GAC Roy. February 5, 2015 EFTA01105558 IC:1111 ( I V . 1 ID # 7018737, ROO 15 June 2015 Gulfstream G550 Serial Number 5070 Jet Aviation Business Jets AG PART II. Contingencies and Assumptions of Proposal Offer Unless expressly stated otherwise in writing, this proposal and the Workscope pricing information included in Part I Workscope, (-Proposer) is based upon the following contingencies and assumptions associated with the activity and work required for the work scope defined in Part I Workscope (-Work-). Additional charges for any Customer-approved Work ultimately performed on Gulfstream G550 aircraft, Serial Number 5070 (-Aircraft"), which is beyond the scope of this Proposal will be billed on a time and materials basis, except as otherwise expressly agreed in writing between the parties. The term Customer shall refer to Jet Aviation Business Jets AG ("Customer") in this Proposal. A. ESTIMATED LEADTIME: This Proposal provides for leadtimes. Leadtime is an estimate expressed in calendar days to allow for planning and scheduling of the Aircraft service visit. Leadtimes commence upon Gulfstream's receipt of Customer's signed Proposal and material callout selections. Leadtimes may be addressed by other relevant contingencies set out in this Proposal. B. ESTIMATED DOWNTIME: This Proposal provides for downtime. Any downtime estimates included in this Proposal are based upon Gulfstream's general understanding of the time required to accomplish the work outlined in this Proposal. Said understanding is in turn based upon Customer satisfying any leadtime requirements. Estimated downtime may be adjusted depending on the final induction schedule and mutually agreed facility selected for completion of the Work. For the avoidance of doubt, any expression of downtime is only provided as an estimate. This estimate is not a contractual commitment by Gulfstream. Estimated downtime is stated in working days, defined as Monday through Friday, excluding applicable recognized local holidays. If additional Work is required beyond that specifically identified in this Proposal, then the estimated downtime may be extended by Gulfstream. Estimated downtime may increase or decrease depending upon the availability of the mutually agreed facility selected for completion of the Work. C. PRICING AND SCHEDULING TERMS: This Proposal is contingent on all Work being accomplished during a single coordinated maintenance visit. The quoted prices contained herein are valid (i) if the Proposal is signed and returned to Gulfstream within ninety (90) days of the date of the Proposal, and (ii) the Work is scheduled to be accomplished at a mutually agreeable facility and time within six (6) months from the date of this Proposal. Unless otherwise indicated on the face of this Proposal, any proposal for Work in a Gulfstream US facility is valid for each Gulfstream US facility. Proposals for work at any non-US Gulfstream facilities are specific and binding only as to the facility identified on the Proposal. Overtime: Gulfstream will not charge overtime for the Work required in this Proposal, unless there are (i) Discovered Discrepancies as addressed below, (ii) Changes documented on Work Change Requests (WCRs) as described below, or (iii) Customer requests to accelerate the estimated downtime for any Work. Customer must approve all overtime activity prior to Gulfstream performing and billing for overtime. Discovered Discrepancies: Except as specifically identified in PART I Workscope, this Proposal does not include repairs to the Aircraft resulting from discrepancies in the Aircraft (including without limitation corrosion) discovered during the performance of the agreed Workscope. All discovered discrepancies will be corrected upon request at additional charge and with additional downtime. This process is further described in the Changes (-WCRs-) paragraph. Page 4 of 10 This proposal is confidential between Gulfstream and the Customer. JCM Return to Table of Contents GAC Rey. February S. 2015 EFTA01105559 ID # 7018737, R00 15 June 2015 Gulfstream G550 Serial Number 5070 Jet Aviation Business Jets AG PART II. Contingencies and Assumptions of Proposal Offer (continued) C. PRICING AND SCHEDULING TERMS (continued) Changes ("WCRs"): This Proposal is subject to further financial and schedule modification, which will be documented on work change requests ("WCRs") presented to the Customer for approval, if any of the following occurs: • Subsequent to the date of this Proposal, a relevant aviation regulatory authority or OEM (including Gulfstream) publishes any change in relevant technical documentation which affects the Workscope. • Additional billable work, which is not specifically delineated in the Workscope, is required to perform the quoted Workscope. This additional work may include by way of example relocation of existing aircraft equipment, beyond that already defined in the Workscope, due to space limitations. Consumables: There will be a 4.0% charge for consumables, to a maximum of $5,000, on all work orders containing labor revenue charges. This charge will be calculated based on the total labor revenue man-hours invoiced on the work order. Only invoices defined as 'Road Trip Invoice- will be exempt from this charge. CFE, Drop Shipments and Handling Fees: Customer furnished parts or equipment (-CFE-) and drop shipments made by the Customer to Gulf stream will be subject to a handling fee of 15% based on current manufacturer list price of the part or item furnished. The handling fee will not apply to parts originally purchased from Gulfstream. Proof of purchase from Gulfstream must be shown to waive the handling fee. Third Party Vendors: Any estimates given for services provided to Gulfstream by outside vendors, whether for repair, calibration, overhaul, exchange or the like, are subject to adjustment based upon the actual charges billed to Gulfstream by such outside entity. Excluded fees, taxes, etc.: All prices stated herein are exclusive of freight, fuel, flight costs, environmental fees, and/or any applicable taxes. Exchange Services — Retention of Removed Equipment: Any parts exchanged as part of the Workscope, and related price adjustments will be governed by Gulfstream's then current parts exchange program. Except as specifically identified in PART I Workscope, equipment removed as part of the Workscope will become the property of Gulfstream. PlaneParts©: Except as specifically identified in a PART I Workscope, this Proposal does not take into account any parts provided at no charge under Gulfstream's PlanePartse program. To enroll or learn more about the PlanePartsO program please visit http://www.quffstream.com/product-supporUsupport-services/planeparts. D. GENERAL CONTINGENCIES: Requirement for Customer Furnished Records: This Proposal is based upon the Aircraft being in the configuration, and containing the equipment. as indicated in Gulfstream CMP records and any records supplied by Customer to support this Proposal. This Proposal is also contingent upon the Customer supplying, upon induction or within leadtimes, all avionic, electrical, system, interior or structural drawings, diagrams, analysis and records, which accurately represent the current condition of the aircraft ("Customer Records"), as approved by the relevant aviation authority, and which are required by Gulfstream to conduct the Work. Any changes which are required to be made by Gulfstream to the Customer Records, or due to the inadequacy of the Customer Records, in connection with the Work, will be subject to additional charges. These additional charges will be documented pursuant to the Changes ("WCRs") clause and subject to Customer approval. Page 5 of 10 This proposal is confidential between Gulfstream and the Customer. JCM ah Return to Table of Contents SAC Rev. February 5.2015 EFTA01105560 LAMM mint ' 1..10 e ,r e. ID # 7018737, R00 15 June 2015 Gulfstream G550 Serial Number 5070 Jet Aviation Business Jets AG PART II. Contingencies and Assumptions of Proposal Offer (continued) D. GENERAL CONTINGENCIES: (continued) General Exceptions: Except as specifically identified in PART I Workscope: • Aircraft Preservation: This Proposal does not include any preservation tasks related to the Aircraft, its engines or systems. Customer is responsible for making certain that all specific preservation tasks related to the Aircraft, its engines or systems, which are required or may become required while the Aircraft is at Gulf stream's facility for the Workscope, are identified on the Work Order. • Certification Basis: All Work to be accomplished by Gulfstream under the Workscope, assumes the Aircraft is operated in compliance with FAR Part 91 or the equivalent not-tor hire operating rules of the relevant aviation authority. • Non-standard Equipment: Gulfstream is not responsible for vendor to vendor incompatibilities which may be discovered during the course of the installation. • Manuals — Modifications: Changes to the Aircraft's Completion Center Maintenance Handbook (CCMH) or Cabin Operating Manual (COM) are not included as part of this Proposal. Should a modified CCMH or COM be requested by the Customer, it may be provided at additional charge. Any changes to the Aircraft's Minimum Equipment List ("MEL") are the Customers responsibility and are not included herein. • Access, Closure, Removal and Replacement: Access and closure, removal and replacement required to perform the Workscope are not included as a part of this Proposal. Touch-Up Paint: For aircraft with standard Gulfstream paint schemes (one (1) base color and two (2) stripes), the sealing and touch-up (by brush) of panels is included in the Workscope. Aircraft with non-standard paint schemes will be subject to an additional charge for the additional time required to complete the paint touch-up. Unused Wiring: Any existing wiring or tubing made obsolete by the Work will be capped and stowed. Wiring or tubing removal, if requested by the Customer, will be at additional charge. Termination after acceptance of Proposal: Unless the Customer has specifically directed otherwise, once the Proposal is signed and returned to Gulfstream, and prior to the Workscope being scheduled in accordance with Section C Pricing and Scheduling Terms, this Proposal shall be binding upon Gulfstream as to the prices set forth herein. All preliminary engineering materials and components ordered to support the Workscope, any labor expended, any restock charges incurred, and any other direct costs supporting the Workscope are chargeable to the Customer if the proposed Workscope is thereafter canceled by the Customer. If materials or components cannot be returned to their respective vendor(s), Customer will be billed in full for these items. In such case, the materials and components become the property of the Customer. If the Work is rescheduled for a later arrival, these charges will be applied to the rescheduled visit, as appropriate. Confidentiality: This Proposal and any related documents are strictly confidential between Gulfstream and Customer and will not, without the prior written consent of the other party, be disclosed by either party, in whole or in part, to any third party except to such party's accountants, lawyers, and bankers, and Gulfstream's suppliers, provided such third parties agree to confidentiality as may be necessary for either party to carry out its obligations or enforce its rights pursuant to this Proposal. E. ADDENDUM TO PROPOSAL AND WORK AUTHORIZATION TERMS AND CONDITIONS Not Applicable Page 6 of 10 This proposal is confidential between Gulfstream and the Customer. JCM a•; Return to Table of Contents GAC Rey. February 5, 2015 EFTA01105561 t itJl:aln:llti X e e.) ID # 7018737, R00 15 June 2015 Gulfstream G550 Serial Number 5070 Jet Aviation Business Jets AG PART III. Payment Terms and Remittance Instructions For Customers with available credit and except as set forth below, payment terms are net 30 days from date of invoice. For Work estimated to exceed $100.000. Customer agrees to make progress payments on the following schedule: 50% of the estimated amount prior to commencement of Work on the Aircraft, and final payment of the remaining 50% 30 days from date of final invoice. Additional deposits may be required for long-lead or special purchased parts, which are not refundable, should the visit be cancelled or work scope changed to eliminate those items. Additional deposits may also be requested if there is a significant amount of growth in the job, including significant material costs. If any portion of an invoice is disputed. then Customer shall nevertheless pay all undisputed amounts per this schedule. Gulfstream shall not be required to release Customers Aircraft to depart if Customer's total outstanding balance owed to the Gulfstream Parties exceeds the lesser of $150,000.00 or Customer's available credit limit. All sums past due bear interest at the lesser of 1.5% per month, or the maximum rate allowable by law, plus reimbursement for attorney fees and other costs of collection. For customers without available credit, including those without open credit terms (Cash in Advance, Cash on Delivery, etc.), progress payments will be required as outlined above with remaining outstanding balance payable at departure. See the Work Authorization terms and conditions for further details on payment terms. If Applicable, Aircraft Records and Condition Survey ("ARCS"). ARCS fees are payable in advance of the inspection being performed. Acceptable methods of payment related to ARCS and supporting aircraft sales transactions include payment via wire transfer/ACH, certified check and Gulfstream accepted credit card. Costs incurred in remediation of discrepancies documented during the ARCS or required in conjunction with the supporting aircraft sales transaction are immediately due upon completion of the ARCS and prior to the departure of the aircraft. This section applies to all customers, including those who have available credit. Remittance can be made to the following: Checks: Gulfstream Aerospace Corporation (Overnight) Gulfstream Aerospace Corporation (Box #730349) P.O. Box 730349 c/o JP Morgan Chase Bank, NA Dallas. TX 75373-0349 Attn: Dallas National Wholesale Lockbox TX1-0029 14800 Frye Road Ft. Worth, TX 76155 Wire Transfer Gulfstream Aerospace Corporation Instructions: JP Morgan Chase Bank, NA 1 Bank One Plaza Chicago. IL 60670 Account No. Reference your ive ( Digit Customer Number (XX-XXX) Bank Fedwire Boutin No. Identifiers: S.W.I.F.T ACH Cre it outing o. Note: Please reference the Quote ID Number and one of the following (as applicable): • Invoice Number • Sales Order Number • Job or Work Order Number • Aircraft Serial or Registration Number • Customer Account Number Page 7 of 10 This proposal is confidential between Gulfstream and the Customer. J CM ah Return to Table of Contents GAC Rey. February 5, 2015 EFTA01105562 ID # 7018737, R00 15 June 2015 Gulfstream G550 Serial Number 5070 Jet Aviation Business Jets AG PART IV. Executive Summary and Proposal Acceptance Please select items in Accept/Decline columns. Once an item is accepted, the amount will auto populate the total. (Please note that quoted dollars and downtime may vary based on concurrent work with accepted/declined items.) A. INTERIOR B. AVIONICS / CABIN ELECTRONICS C. MECHANICAL —AIrcr —Inalntenance 1.1 t CMP Tasks 1 1.2 CB 157 Inspection, Main Landing Gear Door Actuator 1.3 BR[SSN REDACTED]50 PDLA Spherical Bearing 1.4 Aircraft Return to Operation after Non Standard Storage SGER-318 (Budgetary) D. PAINT (USD) Accept Decline $58,204 $274 $1,230 $33,000 $01 QUOTED WORKSCOPE TOTAL BASED ON CUSTOMER ACCEPTED ITEMS 'Default value Is set to SO until Customer selections have been made above. 11 Page Sot 10 This proposal is confidential between Gulfstream and the Customer. JCM/ah Return to Table of Contents GAC Roy. February 5, 2015 EFTA01105563 p- pry, (;Idimmi ni C TOOl) ID # 7018737, R00 15 lune 2015 Gulfstream G550 Serial Number 5070 Jet Aviation Business Jets AG PART IV. Executive Summary and Proposal Acceptance (continued) Estimates based on Quoted Worksc Materials/Outside Services for CMP Inspection Package(s)1 $37,125 The estimated amount includes items marked with an "X" on the attached CMP Exhibit(s). The estimates are for budgeting purposes only and are subject to pricing and availability at the time of aircraft induction. Input Facil Gulfstream Long Beach 4150 East Donald Douglas Drive Long Beach, ff rni 1725 Main Phone: Note: Changes to facility input may affect downtime. Please contact your Regional Sales Manager. dule Planning Estimated Days Leadtime 5 Calendar Days (For definition, see Part II Section A or click here) Downtime 8 Working Days (For definition, see Part II Section B or click here Note: An additional downtime estimate of three (3) working days may be required to clear discrepancies found during the inspection. This estimate is based on aircraft model, age of aircraft, and history of discrepancies found during the inspection(s). These above estimates are for planning purposes only and are not to be used as a completion date for the workscope. Quote Validity Pricing contained in this proposal is valid for 90 days from the date of this proposal. For further details/definition. see Part II Section C or click here) Pricing No This proposal supersedes Proposal ID Number 7018737, R00 dated 15 June 2015. Page 9 of 10 This proposal is confidential between Gulfstream and the Customer. JCWah Return to Table of Contents GAG Rev. February 5. 2015 EFTA01105564 tllkut:un 1 e ,r ' 10 ID a 7018737, R00 15 June 2015 Gulfstream G550 Serial Number 5070 Jet Aviation Business Jets AG PART IV. Executive Summary and Proposal Acceptance (continued) Upon acceptance of this Proposal, the prices and quotes stated herein (subject to all contingencies or other stated assumptions) constitute a formal Fixed Price Quote, which is included in Gulfstream's standard Work Authorization Agreement Terms and Conditions. Your acceptance of all or any portion of this Proposal confirms your acknowledgement that you have read and express agreement to be bound by these terms. This Proposal expressly incorporates by reference and is subject to Gulfstream's standard Work Authorization Agreement Terms and Conditions which are attached hereto as ATTACHMENT A. The Work Authorization, which will include a Work Order which details all items of Work to be accomplished during the service visit, including those items selected and documented by Customer from this Proposal, will constitute the agreement between the parties and will supersede this Proposal when executed by both parties. The Work Authorization will be signed at the Aircraft's induction into the agreed Gulfstream Service Center. IN WITNESS WHEREOF, the parties have caused this Proposal to be executed by their duly authorized representatives. Copies of a fully executed agreement. emailed between the parties will be effective as an original signed agreement. JET AVIATION BUSINESS JETS AG ("Customer") ("Gulfstream") GULFSTREAM AEROSPACE CORPORATION By: Name: Title: Date: By: Name: Stephan Forte Title: Regional Sales Manager, Product Support Sales Date: 26 June 2015 Please complete and return all pages of PART IV via fax or email Page 10 of 10 This proposal is confidential between Gulfstream and the Customer. JCM/ah Return to Table of Contents GAC Rey. February S. 2015 EFTA01105565 ATTACHMENT A WORK AUTHORIZATION AGREEMENT TERMS AND CONDITIONS 1. AGREEMENT. This Work Authorization Agreement, including documents incorporated by reference, (the "Agreement") identifies the services and materials (the "Work") to be provided by Gulfstream, its employees, agents, representatives, and contractors. (collectively "Gulfstream") to the aircraft identified on the first page of this Agreement (the "Aircraft") plus the associated terms and conditions of the Agreement. -Customer" means collectively the customer identified on the first page hereof, and all owners, operators, lessors, lessees and insurers of the Aircraft. "Gulfstream Parties" means Gulfstream, General Dynamics Corporation and each of their affiliates, including without limitation the Jet Aviation companies ("Jet Aviation"), and all such entities' employees, agents, representatives and contractors. This Agreement is the parties' entire agreement concerning the Work and replaces prior verbal or written agreements with respect thereto. This Agreement's terms and conditions (but excluding changes in the scope of the Work and overtime authorizations) may not be altered except by a writing that expressly references this Agreement and is signed by authorized representatives of both parties. 2. WORK CHANGES. Customer authorizes Gulfstream to expend labor and materials reasonably appropriate to the mutually agreed Work. Work changes (including requests for overtime) require mutual agreement of the parties. Customer's oral changes increasing the scope of the Work or approving overtime are binding (unless othenvise provided by law). Customer payment of the invoice for any additional Work item is customer acknowledgement that the additional item was mutually agreed upon as part of the Work. 3. PRICING. Except as otherwise specifically agreed between the parties in writing, all Work (including engineering services) performed under this Agreement is on a TIME AND MATERIALS BASIS unless expressly subject to a formal fixed•price quote signed by both Gulfstream and Customer. ESTIMATES OF EXPECTED HOURS/MATERIAL COSTS ARE NOT QUOTES AND ARE BILLED SOLELY ON A TIME AND MATERIALS BASIS. For time and materials Work: (a) labor (including engineering services) is billed according to the rates set forth in the Gulfstream Aircraft Services Rate Letter in effect as of the date the Work is performed; and (b) materials are billed according to Gulfstream's standard prices in effect on the date the material is used. Any incremental charge under Gulfstream's Component Exchanged Program will be billed by supplementary invoice. 4. PAYMENT TERMS. For customers with available credit, and except as set forth below, payment terms are net 30 days from date of invoice. For Work estimated to exceed $100,000, Customer agrees to make progress payments on the following schedule: 50% of the estimated amount prior to commencement of Work on the Aircraft, and final payment of the remaining 50% 30 days from the date of final invoice. Additional deposits may be required for long-lead or special purchased parts, which are not refundable, should the visit be cancelled or work scope changed to eliminate those items. Additional deposits may also be requested if there is a significant amount of growth in the scope of the Work, including significant material costs. If any portion of an invoice is disputed, then Customer shall nevertheless pay all undisputed amounts per this schedule. Gulfstream shall not be required to release Customer's Aircraft to depart if Customer's total outstanding balance owed to the Gulfstream Parties exceeds the lesser of $150,000.00 or Customer's available credit limit. All sums past due bear interest at the lesser of 1.5% per month, or the maximum rate allowable by law, plus reimbursement for attorney fees and other costs of collection. For customers without available credit, including those without open credit terms (cash in advance, cash on delivery, etc.), progress payments will be required as outlined above with remaining outstanding balance payable at departure. 5. TAXES. Customer is responsible for all Federal, State, local and foreign taxes, fees, levies, penalties, excises, charges, surcharges, import and export charges and other duties and tariffs ("Taxes") applicable to the Work performed hereunder, the materials used or transportation (other than taxes on income of Gulfstream) and Customer shall indemnify and hold Gulfstream s harmless with respect thereto. 5.1 Any and all payments by the Customer under the terms of this Agreement shall be exclusive of any Taxes. Customer shall bear, and shall indemnify Gulfstream for any such Taxes in the event they are or become due at any time in accordance with the applicable laws and regulations. Should customer be required by applicable law to withhold or deduct any Taxes from such payments, then the sum payable shall be increased as necessary so that after making all required deductions, Gulfstream receives an amount equal to the sum it would have received had no such deductions been made. GAC Rev. May 7.2015 1 of 4 EFTA01105566 6. WARRANTY. 6.1 GENERAL. Gulfstream warrants that the Work conforms to the pertinent specifications prescribed by the applicable aircraft/component manufacturer, and that any components or other items supplied hereunder (but excluding Customer-furnished items) are free from defects in material and workmanship. This warranty extends to defects discovered within twelve (12) months, or one thousand (1,000) flight hours, whichever comes first, after completion of the Work; except that the warranty period for any Work performed as warranty work is equal to the pre-existing unexpired warranty period. Parts qualifying for the "Exclusive Gulfstream Parts Warranty Extension" Program, or other extended published Gulfstream warranty programs, if any, are entitled to an extended warranty period pursuant to the terms of such programs as they exist on the date this Agreement is executed. To the extent that any Work is being performed as warranty work under a service center warranty originally extended by a Gulfstream Party to a prior owner or operator of the Aircraft, then this Agreement shall constitute an assignment of such original warranty to Customer except that the terms and conditions thereof shall be those in this Agreement (including Sections 7, 8 and all other disclaimers and limitations in this Agreement). 6.2 REMEDY. Gulfstream's sole obligation for breach of warranty for Work other than inspection activities, and Customer's sole remedy, is limited to the repair, replacement or correction (at Gulfstream's reasonable discretion) of the defective Work. All parts and labor required for disassembly, removal, installation and reassembly of the defective item are Gulfstream's expense, but only if the Work is performed at a Gulfstream or Jet Aviation facility authorized to work on the applicable aircraft model. Gulfstream is not responsible for any costs or expenses associated with transporting the Aircraft or warranted items to any repair facility. Gulfstream's sole obligation for negligent or otherwise defective inspection activities, including any damage to an Aircraft that results from any alleged negligent inspection, and Customer's sole remedy, is limited to refund of any payments made by Customer for that portion of such inspection that was defective. 63 ADDITIONAL REMEDY FOR COLLATERAL AIRCRAFT DAMAGE. 63.1 In addition to the warranty remedy provided in Section 6.2, but subject to Section 6.3.2 below, if any defective Work, negligence or willful misconduct of a Gulfstream Party related to performance of this Agreement causes damage to the Aircraft within the warranty period set out in Section 6.1, then as Customer's sole remedy Gulfstream will repair at no charge (as further described below) any such Aircraft damage that is directly and immediately caused by a Gulfstream Party. Such repairs will be accomplished at a Gulfstream or Jet Aviation facility authorized to work on the aircraft model, and on the same terms and conditions hereof (excluding payment obligations) using methods selected by Gulfstream in its reasonable discretion; provided, however, if Gulfstream reasonably deems the Aircraft to be damaged beyond economical repair, then the sole remedy is for Gulfstream to pay Customer the Aircraft's pre-damage fair market value and for Gulfstream to receive clear title thereto. 63.2 Notwithstanding anything else in this Agreement, Gulfstream's remedy obligations under this Agreement shall not include Aircraft damage that either (a) allegedly is caused by a negligent inspection where the damage occurs after completion of the Work or (b) is caused by a Right Operations Accident (as defined below) even if such accident is allegedly caused by a Gulfstream Party (including negligence of a Gulfstream employed flight crew member on the Aircraft). "Flight Operations Accident" means an accident or incident occurring between ramp movement for flight through takeoff, flight, landing, taxi and parking in which the Aircraft suffers damage from contact with the earth or other objects. 6.4 TERMINATION OF WARRANTY. The warranties and Gulfstream's obligations for the repair of Aircraft Damage set forth above in Section 6 are void if either the Aircraft or warranted item have been subjected to maintenance, overhaul, installation, storage, operation, or use which is improper or not in accordance with the aircraft/component manufacturer's instructions (including failure to comply with approved operating and maintenance manuals, instructions or bulletins, or customary maintenance or airmanship practices), or to any accident or casualty that proximately causes or contributes to the failure or substandard performance of the warranted item or further damage to the Aircraft. 6.5 CUSTOMER'S OBLIGATIONS. Gulfstream's warranty obligations hereunder are expressly conditioned upon compliance with all of the following: Customer must provide Gulfstream with written notice within 60 days after the defect becomes apparent; Customer must return or otherwise dispose of the item at issue as directed by Gulfstream within 30 days after receipt of Gulfstream's instructions; and Customer shall maintain and make available to Gulfstream all records (including FDR, CVR and other aircraft recorded data) reasonably related to the maintenance, use and condition of the item at issue. GAC Rev. May 7.2015 2 of 4 EFTA01105567 7. DISCLAIMERS. THE EXPRESS WARRANTIES IN SECTION 6 OF THIS AGREEMENT ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES (EXCEPT FOR THE WARRANTY OF TITLE) AND REPRESENTATIONS, EXPRESS, IMPLIED, OR STATUTORY, INCLUDING WITHOUT LIMITATION IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS (INCLUDING FITNESS FOR A PARTICULAR PURPOSE) (COLLECTIVELY "EXCLUDED WARRANTIES"). Except as expressly set forth in this Agreement, Customer, on behalf of itself and all owners, operators, lessors, lessees, and insurers of the Aircraft, hereby waives and releases all rights, claims, and remedies (through subrogation or otherwise) with respect to any and all Excluded Warranties, duties, obligations, and liabilities in tort or contract arising by law or othenvise from this Agreement or the Work, including: (1) liability for a Gulfstream Party's own negligence or (2) strict liability or product liability. For the avoidance of doubt, this Section 7 does not modify the rights and obligations of Gulfstream and Customer (or owner of Aircraft if different from Customer), as expressly stated in any Gulfstream Aircraft Warranty Agreement between the parties. 8. EXCLUSION OF ALL OTHER DAMAGES. Notwithstanding anything else in this Agreement, the Gulfstream Parties shall not be liable for punitive, special, incidental or consequential damages that arise from or relate in any way to this Agreement, or the Aircraft's presence at a Gulfstream Party's facility as a result of this Agreement, whether arising out of contract, warranty, tort or by statute or otherwise. Such excluded damages include damages for loss of use, loss of time, inconvenience, diminution in value or commercial loss. Furthermore, Gulfstream Parties shall not be liable for any damages which are covered by any insurance policy maintained by Customer. THE EXCLUSION OF SUCH DAMAGES AS SET FORTH HEREIN SHALL APPLY NOTWITHSTANDING ANY OTHER PROVISION OF THIS AGREEMENT, SHALL BE DEEMED INDEPENDENT OF ALL WARRANTIES, AND OTHER PROVISIONS OF THIS AGREEMENT, AND SHALL SURVIVE ANY FAILURE OF THE ESSENTIAL PURPOSE OF ANY WARRANTY OR LIMITED REMEDY UNDER THE TERMS OF THIS AGREEMENT. 9. LIABILITY TO THIRD PARTIES. The limitations of liability in these terms and conditions will not be interpreted to affect in any way a Gulfstream Party's obligations, if any, for third party personal injury, wrongful death or property damage to other than the Aircraft or its contents. 10. NO BAILMENT. No bailment is created by this Agreement, and Gulfstream shall not act as insurer of the Aircraft while the Aircraft is present at Gulfstream's facility or otherwise in Gulfstream's custody or control. 11. NO DELAY PENALTY. Gulfstream will use reasonable efforts to complete the Work in a timely manner. Reasonable efforts does not include overtime unless the Customer agrees to bear overtime charges. Notwithstanding such obligation, Gulfstream shall not under any circumstances be liable for damages, late delivery penalty, fee or the like should it fail to perform the Work within any period of time specified by the Parties. 12. ACCEPTANCE OF DELIVERY. Gulfstream will tender the Aircraft to Customer for delivery at the facility where the Work was performed, unless othenvise agreed in writing. Customer shall promptly inspect the Work, and, upon correction or Customer approved deferral of any discrepancies in such Work, Customer shall accept the Aircraft. 13. TITLE. Title to all materials installed in the Aircraft under this Agreement does not pass until acceptance and payment of the Work by Customer, through delivery of the Aircraft or as otherwise mutually agreed in writing. 14. EXCESS STORAGE CHARGE. Unless otherwise agreed between the parties in writing, should Customer's Aircraft remain at Gulfstream's facility following completion of the Work for more than five (5) days, for whatever reason (including a failure to pay for the Work performed), Gulfstream is authorized by Customer to charge the prevailing rate for day storage of aircraft as then charged by Fixed Base Operators for aircraft of similar size on the airport where the Aircraft is stored (but not less than $200.00 per day). Unless otherwise expressly agreed in writing as part of this Agreement, Gulfstream is under no obligation to provide any maintenance services whatsoever to the Aircraft while being stored under this provision and any dilapidation of the Aircraft during such storage period shall be Customer's sole responsibility. 15. SAFETY AND SECURITY. Customer's employees, agents, subcontractors and representatives shall abide by all applicable Gulfstream policies, procedures and safety protocols when present on Gulfstream's premises. 16. INDEMNITY BY CUSTOMER ENTERING GULFSTREAM'S PREMISES FOR PERSONAL INJURY AND DAMAGE TO OTHER PROPERTY. Customer assumes the risk of and agrees to indemnify and hold GAC Rev. May 7.2015 3 of 4 EFTA01105568 harmless the Gulfstream Parties from and against any and all liability, damage, loss, cost and expense, including attorney's fees, on account of any claim, suit or action made or brought against a Gulfstream Party (including claims brought against a Gulfstream Party because of a Gulfstream Party's own negligence) for the death of or injury to employees, agents, representatives and subcontractors of Customer, or damage or destruction of property of Customer, its employees, agents, representatives or subcontractors, (other than damage or destruction of the Aircraft upon which Work is performed, which is addressed elsewhere under this Agreement) sustained arising from or related to Customer's presence on the Gulfstream Party's facilities (including its hangars and ramps but excluding a Gulfstream Party's customer lobby and customer briefing rooms) during the course of the Agreement, except for the willful misconduct of a Gulfstream Party or its employees acting within the scope of their employment. 17. ARBITRATION. Any controversy or claim arising out of either this Agreement or Customer's service visit to Gulfstream shall be governed by the laws of the State of Georgia, without regard for rules concerning conflicts of law, and settled by one (I) arbitrator (except if the claim is in excess of $2 Million, then by three (3) neutral arbitrators) under the Commercial Arbitration Rules of the American Arbitration Association ("AAA") in the City where the work hereunder was performed If the arbitration proceedings shall be conducted before a panel of three neutral arbitrators, the panel shall be selected using the following process: Within 15 days after the commencement of arbitration, each party shall select one person meeting the specified qualifications to act as neutral arbitrator, and the two thus selected shall select a third neutral arbitrator meeting the specified qualifications within 15 days of their appointment to act as the chair of the arbitration panel. If the arbitrators selected by the parties are unable to or fail to agree upon the third arbitrator, the third arbitrator shall be selected by the American Arbitration Association. In an arbitration with a single arbitrator, the parties shall use their best efforts to agree upon an arbitrator(s) within thirty (30) days after service of the claim, and if agreement is not reached by such date then either party may request the AAA to appoint an arbitrator(s) in accordance with its rules. The U.N. Convention on Contracts for the International Sale of Goods (frequently referred to as the "UNCISG") shall not apply. 18. MISCELLANEOUS. If any provision of this Agreement is held invalid under applicable law, such provision will be ineffective only to the extent of such invalidity without invalidating the remainder of this Agreement. If there is any conflict between these terms and conditions hereof and any document incorporated herein by reference, then these terms and conditions shall control unless such document expressly states the contrary. The words "include," "including" and variations thereof are not terms of limitation and shall be deemed followed by "without limitation." Exports or re-exports of commodities, technology and software provided as part of the Work are subject to the U.S. Export Administration Regulations and diversion contrary to U.S. law is prohibited. Customer shall comply with all applicable U.S. export laws and regulations. 18.1 Customer shall not assign, sell, transfer or otherwise dispose of neither this Agreement nor any rights hereunder without first obtaining the express written consent of Gulfstream. 18.2 The failure of any of the parties to exercise any right under this Agreement shall not be construed as a waiver or relinquishment for the future enforcement of such right at any time. 19. AUTHORIZATION OF AIRCRAFT OWNER/LESSOR/LESSEE. The person signing this Agreement on behalf of Customer represents, warrants and affirms that he is an AUTHORIZED AGENT OF THE AIRCRAFT OWNER(S), and, if applicable, lessor(s) and/or lessee(s) with full authority to enter into this Agreement and bind such owner(s), lessor(s), or lessee(s), with respect to all Work contemplated herein and on behalf of himself and his employer agrees to indemnify Gulfstream for all losses arising from any breach of this representation and warranty. Customer Acknowledgement: By: Name: Title: GAC Rev. May 7.2015 4 of 4 EFTA01105569 IDa 7019199 RO1 Exhibit 1 Mandatory Code Related Code Code Description Included in Material Estimate 200099' () RH 1A (500 Hrs) Engine 2 Check 200101' 1A(500 Hrs/12 Mos) CHECK 200201' IC (12 MOS) CHECK 200202' 2C (24 MOS) CHECK 200203' 3C (36 MOS) CHECK 200205' 5C (60 MOS) CHECK 200324' 24/24 (MOS) CHECK 121400 LH Air Turbine Starter Oil - Change X 801011 LH Air Turbine Starter Magnetic Chip Collector - Detailed Inspection 121400 (121401) RH Air Turbine Starter Oil - Change X 801011 (801012) RH Ai Turbine Starter Magnetic Chip Collector - Detailed Inspection 237004 Cockpit Voice Recorder -Operational Test 237008' Download And Analysis Of CVR 240106 L Emergency Battery - BITE i Battery Level Test 240107 R Emergency Battery - BITE 1 Battery Level Test 240108 Fwd Emergency Battery- BITE I Battery Level Test 240109 Aft Emergency Battery - BITE! Battery Level Test 240121 Emergency Battery Power System (Left) - Operational Test 240122 Emergency Battery Power System (Right) - Operational Test 240123 Emergency Battery Power System (Forward) - Operational Test 240124 Emergency Battery Power System (Aft) - Operational Test 242005 Standby Electrical Power System - Operational Test 242111 Integrated Drive Generator (Left) - Detailed Inspection 242109 Integrated Drive Generator (Left) - Oil Level Check 242141 Integrated Drive Generator Oi Scavenger Filter Differential Pressure Indicator (Left) - Inspection 242112 Integrated Drive Generator (Right) - Detailed Inspection 242110 Integrated Drive Generator (Right) - Oil Level Check 242142 Integrated Drive Generator Oi Scavenger Filter Differential Pressure Indicator (Right) - Inspection 242115 Integrated Drive Generator (Left) - Servicing 242116 Integrated Drive Generator (Right) - Servicing 243011 L Main Battery - Capacity Check 243001 Main Battery (Lett) - Removal / Installation 243012 R Main Battery. Ct al a ___, 243002 Main Battery (Right) - Removal 1 Instalation 251006 Crew Seats Inertia Reel (Pilot) - Operational Test 251007 Crew Seats Inertia Reel (Copilot) - Operational Test 251008 Crew Seats Inertia Reel (Observer) - Operational Test 251016 Crew Seat Restraints (Pilot). Detailed Inspection 251017 Crew Seat Restraints (Copilot) - Detailed Inspection 251018 Crew Seat Restraints (Observer) - Detailed Inspection 252102 Passenger Seats Restraints - Detailed Inspection 252104 Passenger Seats Inertia Reels - Operational Test 256011 Crew Smoke Goggles (Pilot) - Detailed Inspection 256012 Crew Smoke Goggles (Copilot) - Detailed Inspection 256013 Crew Smoke Goggles (Observer) - Detailed Inspection 256017 Fire / Crash Axe - Inspection 256043 First Aid Kit (No. 1) - Detailed Inspection 256045 First Aid Kit (No. 1) Time Limited Supplies - Discard X 256041 Fest Aid Kit (No. 1) - Removal i Installation 256071 Flashlight (No.1)- Operational Test 256061 Flashlight (No. 13 256072 Flashlight (No. 2j- Operational Test 256062 Flashlight (No. 2) 256073 Flashlight (No. 3) -Operational Test 256063 Flashlight (No. 3) 256074 Flashlight (No. 4)- Operational Test 256064 Flashlight (No. 4) 256201 Life Vest(s) - Detailed Inspection 256202 Life Raft(s) (No. 1) - Detailed Inspection 256260 Life Raft (No. 1) - Removal 1 Installation 256203 Life Rafts) No. 2 - Detailed Inspection 256261 Life Raft (No. 2) - Removal 1 Installation 256205 Life Vest • Restore 256211 Life Vest (No. 1) - Removal / Installation X 256212 Life Vest (No. 2) - Removal! Installation X 256213 Life Vest (No. 3) - Removal! Installation X 256214 Life Vest (No. 4) - Removal! Installation X 256215 Life Vest (No. 5) - Removal I Installation X 256216 Life Vest (No. 6) - Removal; Installation X 256217 Life Vest (No. 7) - Removal! Installation X 256218 Life Vest (No. 8) - Removal! Installation X 256219 Life Vest (No. 9) - Removal! Installation X Page 1 of 5 EFTA01105570 l0rr 7019199 R01 Exhibit 1 Mandatory Code Related Code Code Description Included in Material Estimate 256220 Life Vest (No. 10) - Removal / Installation X 256221 Life Vest (No. 11) - Removal 1 Installation X 256222 Life Vest (No. 12) - Removal / Installation X 256223 Life Vest (No. 13) - Removal / Installation X 256250 Life Vest (Pilot) - Removal! Instalation X 256251 Life Vest (Copilot) - Removal! Installation X 256252 Life Vest (Observer) - Removal! Instalation X 256282 Personal Breathing Equipment (No. 1)- Detailed Inspection 256281 Personal Breathing Equipment (No. 1) - Removal / Installation 256285 Personal Breathing Equipment (No. 2)- Detailed Inspection 256284 Personal Breathing Equipment (No. 2) - Removal / Installation 256286 Personal Breathing Equipment (No. 2)- Discard X 256306 Emergency Locator Transmitter - Operational Test (FAR 91.207) 256301 Emergency Locator Transmitter - Removal / Installation 256311 Emergency Locator Transmitter - Operational Check 256406 Defibrillator Electrode Pads - Discard (Set No. 1) X 256700 Life Vest (No. 1) - Restore 256701 Life Vest (No. 2) - Restore 256702 Life Vest (No. 3) - Restore 256703 Life Vest (No. 4) - Restore 256704 Life Vest (No. 5) - Restore 256705 Life Vest (No. 6) - Restore 256706 Life Vest (No. 7) - Restore 256707 Life Vest (No. 8) - Restore 256708 Life Vest (No. 9) - Restore 256709 Life Vest (No. 10) - Restore 256710 Life Vest (No. 11) - Restore 256711 Life Vest (No. 12) - Restore 256712 Life Vest (No. 13) - Restore 256726 Life Vest (Pilot) - Restore 256727 Life Vest (Copilot) - Restore 256728 Life Vest (Observer). Restore 261302 APU (Fire) Shutdown Circuit - Operational Test 282641 APU Fuel Shut-off Valve . Operational Check 262021 Engine Fire Bottle (Left) - (Hydrostatic) Functional Test X 262020 Engine Fire Bottle (Left) - Removal! Installation 262128 Engine Fire Bottle Cartridge (Left Bottle. Lett Squib) - Removal! Installation 262129 Engine Fire Bottle Cartridge (Left Bottle. Right Squib) - Removal /Instalation 262130 Engine Fire Bottle Cartridge (Left Bottle. APU Squio) - Removal / Installation 262026 Engine Fire Bottle (Right) - (Hydrostatic) Functional Test X 262025 Engine Fire Bottle (Right) - Removal / Installation 262131 Engine Fire Bottle Cartridge (Right Bottle. Leh Squib) - Removal / Instalation 262132 Enre Fire Bottle Cartridge (Right Bottle. Right Squib) - Removal / Installation 262133 Engkie Fire Bottle Cartridge (Right Bottle. Spare Squib) - Removal / Installation 262108 Engine Fire Bottle Cartridge (Right Bottle. Spare Squib. Service Life) - Discard X 262110 Engine Fire Bottle Cartridge (Left Bottle. Left Squib. Service Life) - Discard X 262112 Engine Fire Bottle Cartridge (Left Bottle. Right Squib. Service Life) - Discard X 262114 Engine Fire Bottle Cartridge (Right Bottle. Left Squib. Service Life) - Discard X 262116 Engine Fire Bottle Cartridge (Right Bottle. Right Squib, Service Life) - Discard X 262118 Engine Fire Bottle Cartridge (Left Bottle. APU / Spare Squib. Service Life) - Discard X 262122 Engine and APU Fire Extinguishing Firing Circuitry (Left Engine) - Integrity Test 262123 Engine and APU Fire Extinguishing Firing Circuitry (Right Engine) - Integrity Test 262124 Engine Fire Bottle Pressure Switch (Left) - Operational Test 262125 Engine Fire Bottle Pressure Switch (Right) - Operational Test 262126 Engine and APU Fire Extinguishing Firing Circuitry (APU) - Integrity Test 262512 Portable Water Fire Extinguisher (Forward Cabin. Hydrostatic) - Functional Test 262560 Trash Receptacle Enclosure (Aft Lavatory) - Detailed Inspection 262561 Trash Receptacle Enclosure (Forward Lavatory). Detailed Inspection 262563 Trash Receptacle Enclosure (Forward Galley! Annex) - Detailed Inspection 262570 Trash Receptacle Fire Extinguishing Bottle (Weight Check. Aft Lavatory) - Functional Test 262571 Trash Receptacle Fire Extinguishing Bottle (Weight Check. Forward Lavatory) - Functional Test 262573 Trash Receptacle Fire Extinguishing Bottle (Weight Check. Forward Galley) - Functional Test 262583 Trash Receptacle Fire Extinguisher Nozzles (Aft Lavatory)- Detailed Inspection 262584 Trash Receptacle Fire Extinguisher Nozzles (Forward Lavatory) - Detailed Inspection 262586 Trash Receptacle Fire Extinguisher Nozzles (Forward Galley / Annex) - Detailed Inspection 262601 Portable Halon Fire Extinguisher (Cockpit) - Inspection 262600 Portable Halon Fire Extinguisher (Cockpit) - Removal / Installation 262602 Portable Halon Fire Extinguisher (Cockpit) - Weight Check 262611 Portable Halon Fire Extinguisher (Forward Cabin) - Inspection 262610 Portable Halon Fire Extinguisher (Forward Cabin) - Removal! Installation 262612 Portable Halon Fire Extinguisher (Forward Cabin) - Weight Check 262631 Portable !talon Fire Extinguisher (Aft Lavatory) - Inspection 262630 Portable Halon Fire Extinguisher (Mt Lavatory) - Removal / Installation Page 2 of S EFTA01105571 IDa 7019199 RO1 Exhibit 1 Mandatory Code Related Code Code Description Included in Material Estimate 262632 Portable !talon Fire Extinguisher (Aft Lavatory) - Weight Check 271011 Aileron Control and Trim Cables in Main Wheel Wells / Wing Trailing Edge - Detailed Inspection 272108 Rudder Control and Trim Cables in Main Wheel Well 1 Tail Compartment - Detailed Inspection 273019 Elevator Drive Rod - Lubrication 273005 Elevator Control System - Operational Test 273100 Elevator Control and Trim Cables in Main Wheel Well and Tall Compartment - Detailed Inspection 274202 Horizontal Stabilizer Actuator - Lubrication 275019 Flap Actuator Travel NW (Left) - Lubrication 275020 Flap Actuator Travel NW (Right) - Lubrication 276105 Speed Brake Cable Assemblies in Main Wheel Well / Wing Trailing Edge - Detailed Inspection 281407 Gravity Water/ Fuel Drain Valve (Left) - Operational Test 281408 Gravity Water/ Fuel Drain Valve (Right) - Operational Test 282606 Engine Feed Dual Wall Fuel Line (Left) - Detailed Inspection 282607 Engine Feed Dual Wall Fuel Line (Right) - Detailed Inspection 282608 APU Feed Dual Wall Fuel Line - Details Inspection 282609 Engine Heated Return Feed Dual Wall Fuel Line (Left) - Detailed Inspection 282610 Engine Heated Return Feed Dual Wall Fuel Line (Right) - Detailed Inspection 282629 Engine Fuel Shut-off Valve (Left) - Operational Check 282630 Engine Fuel Shut-off Valve (Right) - Operational Check 291501 Hydraulic System Shut-off Valve (Left). Operational Test 291502 Hydraulic System Shut-off Valve (Right) - Operational Test 292501 Auxiliary Hydraulic Pump Manifold Differential Pressure Indicator - Detailed Inspection 292502 Power Transfer Unit Manifold Differential Pressure Indicator - Detailed Inspection 304105 Windshield Surface Seal (Left) - Detailed Inspection 304106 Windshield Surface Seal (Right) - Detailed Inspection 313002 DFDR - Functional Test X 313003' Download And Analysis Of FDR 315001 Central Warning System (Including Audio) - Operational Test 316205 DFDR Fail Message - Operational Test 316206 Configuration Message - Operational Test 321005 Main Landing Gear (Left) - Lubrication 321006 Main Landing Gear (Right) - Lubrication 321201 Main Landing Gear Shock Absorber (Left) - Servicing X 321202 Main Landing Gear Shock Absorber (Right) - Servicing X 321221 Main Landing Gear Corrosion Inhibiting Compound Reapplication (Left) 321222 Main Landing Gear Corrosion Inhibiting Compound Reapplication (Right) 321801 Main Landing Gear Door Hinges (Left) - Lubrication 321802 Main Landing Gear Door Hinges (Right) - Lubrication 321803 Main Landing Gear and Doors (Left) - Zonal Inspection 321804 Main Landing Gear and Doors (Right) - Zonal Inspection 322004 Nose Landing Gear - Lubrication 322202 Nose Landing Gear Shock Strut - Servicing X 322220 Nose Landing Gear Corrosion Inhibiting Compound Reapplication 322306 Nose Landing Gear Bungee-Lubrication 322305 Nose Gear Bungee - Removal/ Installation 323700 Nose Lancing Gear Sequencing Unkage - Check / Adjustment 323906 Landing Gear Cycling - Operational Test 322801 Nose Landing Gear Door Hinges - Lubrication 322802 Nose Landing Gear and Doors - Zonal Inspection 323023 Main Landing Gear Spindle Pin Freeplay (Left) - Details Inspection 323024 Main Landing Gear Spindle Pin Freeplay (Right) - Detailed Inspection 323037 Main Landing Gear Bungee (Left) - Lubrication 323039 Main Landing Gear Bungee (Left) - Removal / Installation 321025 Main Landing Gear (Left) - Rigging /Adjustment 121500 Hydraulic System Reservoir (Left) - Servicing 121501 Hydraulic System Reservoir (Right) - Servicing 323038 Main Landing Gear Bungee (Right) - Lubrication 323040 Main Landing Gear Bungee (Right) - Removal / Instaation 321026 Main Landing Gear (Right) - Rigging i Adtustment 323901 Landing Gear Emergency Extension - Operational Test 323006 Landing Gear Emergency Extension Nitrogen Blow-dam Bottle - Servicing 290001 Hydraulic System Meeting Procedure 324303 Parking / Emergency Brake - Operational Test 324305 Brake Wear Indicator (Left Outboard) - Detailed Inspection 324306 Brake Wear Indicator (Left Inboard) - Detailed Inspection 324307 Brake Wear Indicator (Right Inboard) - Detailed Inspection 324308 Brake Wear Indicator (Right Outboard) - Detailed Inspection 325201 Nose Wheel Steering Unit - Lubrication 325202 Nose Wheel Steering Collar Assembly / Slave Gear - Lubrication 334050 Navigation (Position) Light Lens - Detailed Inspection 335020 Cabin Emergency Lighting - Operational Test 341304 Air Data System No. 1 - Functional / Leak Test 530205 Birdstrike Plate (Left) - Removal / Installation Page 3 of 5 EFTA01105572 ION 7019199 RO1 Exhibit 1 Mandatory Code Related Code Code Description Included in Material Estimate 530206 Birdstrike Plate (Right) - Removal! Instaation 341305 Air Data System No. 2 - Functional / Leak Test 341306 Air Data System No. 3 - Functional / Leak Test 345305 ATC No. 1 - Functional Test / Inspection (FAR 91.413) 345306 ATC No. 2 - Functional Test / Inspection (FAR 91.413) 351110 Crew Oxygen Mask and Regulator (Pilot) - Detailed Inspection 351111 Crew Oxygen Mask and Regulator (Copilot) - Detailed Inspection 351112 Crew Oxygen Mask and Regulator (Observer) - Detailed Inspection 352004 Passenger Oxygen Drop-down Mask Assemblies - Detailed Inspection 352009 Passenger Oxygen System (Auto! Manual Mode) - Functional Test 352506 Therapeutic Oxygen System (Outlet No. 1) - Functional Test 352516 Therapeutic Oxygen Mask (No. 1) - Detailed Inspection 353002 Portable Oxygen Bottle and Mask Assembly (No. 1) - Detailed Inspection 353001 Portable Oxygen Bottle (No. 1) - Removal / Installation 353003 Portable Oxygen Bottle (No. 1) - (Hydrostatic) Functional Test X 353004 Portable Oxygen System (No. 1 Bottle) - Operational Test 381300 Supply Line Motor Drain Valve - Operational Test 381301 Drain Line Motor Drain Valve - Operational Test 382003 Water Sterilizer Filter - Discard X 381039 Water Sterilizer - Removal / Installation 381029 Water System - Operational Test 382002 Water Sterilizer Filter - Removal / Installation 491005 APU Enclosure FS 767 - FS 797 - Zonal Inspection 491007 APU Enclosure Thermal Blanket/Coating - General Visual Inspection 491300 APU Compartment Drain Collectors - General Visual Inspection 491301 Auxiliary Power Unit Turbine Plenum Drains - Operational Test 521007 Main Entrance Door Bayonet Position Indicator Dots - General Visual Inspection 521015 Main Entrance Door - Operating Procedures 521009 Main Entrance Door Hinge Pins - Detailed Inspection 521008 Main Entrance Door Hinge Pins - Removal / Installation X 521010 Main Entrance Door - Lubrication 521012 Main Entrance Door Internal - Detailed Inspection 523003 Baggage Compartment Door Seal - Detailed Inspection 523004 Baggage Compartment Door Seal Air Supply Moisture Drain Orifice - Detailed Inspection 523005 Baggage Compartment Door - Lubrication 523008 Baggage Door Seal Check Valve - Operational Test 525001 Auxiliary Pressure Bulkhead Door Seal - Detailed Inspection 527001 Main Entrance Door Secondary Handle Lock Switch and Circuitry - Operational Test 530201 Radome to Structure Perimeter Steps - Detailed Inspection 531005 External Lower Fuselage FS -4 thru FS 758 View From Ground - Zonal Inspection 531012 Exterior Radome Fairing Installation - Detailed Inspection 531014 Enhanced Vision System Sapphire Window Installation - Detailed Inspection 531015 Nose Gear Wheel Well FS 44 - FS 119 - Zonal Inspection 531045 Main Gear Wheel Wells FS 576- FS 632 (Lett)- Zonal Inspection 531046 Main Gear Wheel Wells FS 576- FS 632 (Right) - Zonal Inspection 531047 Main Gear Wheel Wells FS 576 - FS 632 (Cove Panel Drain Holes) - (Enhanced) Zonal Inspection 531048 Main Gear Wheel Wells FS 576- FS 632 (Wiring Harness) - (Enhanced) Zonal Inspection 531055 Aft Cabin Below Floor FS 632 - FS 684 - Zonal Inspection 531060 Baggage Compartment Below Floor FS 684 - FS 758 - Zonal Inspection 531065 External Upper Fuselage FS 63 - FS 758 View From Ground - Zonal Inspection 531080 Left Electronic Equipment Rack FS 141 - FS 166 - Zonal Inspection 531081 Right Electronic Equipment Rack FS 147- FS 181 - Zonal Inspection 531082 Electronic Equipment Rack FS 147 - FS 181 - (Enhanced) Zonal Inspection 531085 External Aft Fuselage and Empennage FS 758 - FS 1123 Viewed From Ground - Zonal Inspection 531095 Aft Fuselage Above Floor FS 758 - FS 974 - Zonal Inspection 570009 Wing Lower Surface (Left) - Zonal Inspection 570010 Wing Lower Surface (Right) - Zonal Inspection 570015 Lower Wing Extension BL 542 - BL 545 (View from Ground) (Left) - Zonal Inspection 570016 Lower Wing Extension BL 542 - BL 545 (View from Ground) (Right) - Zonal Inspection 574015 Wing Leading Edge External BL 44.0- BL 529 Inboard of Navigation Light (Left) - Zonal Inspection 574016 Wing Leading Edge External BL 44.0- BL 529 Inboard of Navigation Light (Right) - Zonal Inspection 575001 Wing Trailing Edge (Left) - Zonal Inspection 575002 Wing Trailing Edge (Right) - Zonal Inspection 575003 Wing Rear Beam (Left) - Zonal Inspection 575004 Wing Rear Beam (Right) - Zonal Inspection 575021 Wing Rear Beam (Left Enhanced) - Zonal Inspection 575022 Wing Rear Beam (Right Enhanced) - Zonal Inspection 711301 LH External - Powerplants. Cowl Doors. Inlet Areas. Thrust Reverser and Nose Cowls (as viewed from ground) - Zonal Inspection 711301 (711302) RH External - Powerplants, Cowl Doors. Inlet Areas. Thrust Reverser and Nose Cowls (as viewed from ground) - Zonal Inspection 783013 Thrust Reverser Ground Relay (Left) - Operational Test 783014 Thrust Reverser Ground Relay (Right) - Operational Test Page 4 of 5 EFTA01105573 'Du 7019199 RO1 Exhibit 1 Mandatory Code Related Code Code Description Included in Material Estimate 783337 Primary Lock Actuator and Mechanism (Lett) - Inspection 710021 EngMe Test 3A (Lett) - Thrust Reverser Check 783115 Thrust Reverser Deactivate / Activate (Left) - Procedure 783338 Primary Lock Actuator and Mechanism (Right) - Inspection 710022 Engkie Test 3A (Right) - Thrust Reverser Check 783116 Thrust Reverser Deactivate / Activate (Right) - Procedure 790011 (790012) RH Magnetic Chip Detectors - Details Inspection 710017 (710018) RH Engine Run Leak Check Test 2A - LP Fuel System! Oil System 790015 (790016) RH Engine Fwd Bearing Chamber Magnetic Chip Detector - Removal! installation 790017 (790018) RH Engine Aft Bearing Chamber Magnetic Chip Detector - Removal! Installation 790019 (790020) RH Engine Accessory Gear Box Magnetic Chip Detector - Removal / Installation 793001 (793002) RH Oil Filter Differential Pressure Indicator - Detailed Inspection 887850 BR[SSN REDACTED]50 - Primary Door Lock Actuator - Ins() (Left) 897850 BR[SSN REDACTED]50 - Primary Door Lock Actuator - Insp (Right) 994001 AD 2012-02-08 - Aviation Communication & Surveillance Systems. LLC Page 5 of 5 EFTA01105574