EFTA01083127

Gulfstream PRODUCT SUPPORT PROPOSAL Prepared for Presented by Gulfstream GV Serial Number 572 Torn Baliya South Aviation, Inc. Regional Sales Manager, Gulfstream Aerospace Mr. Fred Machado EFTA01083127 TABLE OF CONTENTS PART I. Workscope Description 3 A. Interior Refurbishment 3 B. Avionics / Cabin Electronics 3 C. Mechanical 3 D. Paint 7 PART II. Contingencies and Assumptions of Proposal Offer 8 A. Estimated Leadtime 8 B. Estimated Downtime 8 C. Pricing And Scheduling Terms 8 D. General Contingencies 9 E. Addendum To Proposal And Work Authorization Terms And Conditions.. 10 PART III. Payment Terms and Remittance Instructions 11 PART IV. Executive Summary and Proposal Acceptance 12 EFTA01083128 ID # 7018884, R00 12 lune 2015 Gulfstream GV Serial Number 572 South Aviation, Inc. PART I. Workscope Description A. INTERIOR REFURBISHMENT Not Requested B. AVIONICS / CABIN ELECTRONICS Not Requested C. MECHANICAL 1. Aircraft Records and Condition Survey 1.1 Lite Package - Aircraft Records and Condition Survey (ARCS) - Exhibit 1 $27,000 Included in Lite Package: • Aircraft Records Survey (see section below) • Aircraft Condition Survey (see section below) 1.2 Basic Package - Aircraft Records and Condition Survey (ARCS) - Exhibit 2 $47,500 Included in Basic Package: • Aircraft Records Survey (see section below) • Aircraft Condition Survey (see section below) • ARCS Test Flight (see section below) • APU Borescope Inspection (see exhibit) • Left and Right Engine Borescopes and Engine Runs (see exhibit) 1.3 Standard Package - Aircraft Records and Condition Survey (ARCS) - Exhibit 3 $75,000 Included in Standard Package: • Aircraft Records Survey (see section below) • Aircraft Condition Survey (see section below) • ARCS Test Flight (see section below) • APU Borescope (see exhibit) • Left and Right Engine Borescopes and Engine Runs (see exhibit) • Nose and Main Landing Gear and Components - Detailed Inspection (see exhibit) • Aircraft Brake Inspection (see section below) 1.4 Premium Package - Aircraft Records and Condition Survey (ARCS) - Exhibit 4 $98,000 Included in Premium Package: • Aircraft Records Survey (see section below) • Aircraft Condition Survey (see section below) • ARCS Test Flight (see section below) • APU Borescope (see exhibit) • Left and Right Engine Borescopes and Engine Runs (see exhibit) • Nose and Main Landing Gear and Components - Detailed Inspection (see exhibit) • Aircraft Brake Inspection (see section below) • 500 Hour / 1A Inspection Codes (see exhibit) • 12 Month / 1C Inspection Codes (see exhibit) • 1000 Hour / 2A Inspection (see exhibit) Page 3 of 14 This proposal is confidential between Gulfstream and the Customer. soh Return to Table of Contents GAC Rev. February 5.2015 EFTA01083129 ID * 7018884, R00 12 lune 2015 Gulfstream GV Serial Number 572 South Aviation, Inc. PART I. Workscope Description (Continued) C. MECHANICAL (CONTINUED) 1. Aircraft Records and Condition Survey (Continued) Workscope Description Note: Please refer to the above items when determining which sections apply to the Package selected. Special Requirements: • Review workscope and identify points of contact with both buyer and seller present and have both parties sign the Hold Harmless Agreement. • The party requesting and financially obligated for the Aircraft Records and Condition Survey (usually the Buyer) must have an authorized representative sign the work order and the Hold Harmless. • There will be a representative from all parties involved that will make decisions on all minor corrective actions to be accomplished during Aircraft Records and Condition Survey. If there is no representative present, no corrective action can be accomplished until authorized. • Upon completion of the Aircraft Records and Condition Survey, the discrepancy list will be provided to the party(s) responsible for disposition. If a second or third party is involved with rectification of any discrepancies found, the parties will identify who will be responsible for the corrective actions. At this time, separate work orders will be opened and responsibilities assigned to each party for the work requested. • All parties involved, based on the Service Center workload, at that time will mutually agree to the downtime schedule for the authorized work. Aircraft Records Survey includes the following: • Review of Maintenance History and Records: A review of all available maintenance records will be accomplished. The review will include a search for recorded damage history, special inspections accomplished, missing records, compliance with required inspections, maintenance, and mandatory directives. Any problems with incomplete or improper maintenance entries, missing certificate numbers or signatures, or disorganized maintenance logs will be documented in the report. If a complete reconstruction of maintenance records or logbooks is desired, it will be considered an effort over and above the basic Survey price and schedule and will be performed at time and material upon approval. • Documentation of Non-Applicable Maintenance Bulletins: Gulfstream will update the aircraft records for non- applicable or previously accomplished directives (ACB, CB & AD) that are not documented in the maintenance records. A budgetary estimate to research and document non-applicable or previously accomplished bulletins is $75 per occurrence. Incomplete records may substantially increase this cost. • Review of Required Aircraft Documentation: A review of weight and balance, equipment list, and electrical load analysis will be performed to determine that the known current aircraft configuration is reflected. All data will be cross-referenced against Major Repair and Alteration FAA Form 377 found and the avionics inventory. Subject matter and date of Form 337 and any related Supplemental Type Certificates (STC's) numbers will be listed. The certificate of airworthiness and current registration will be checked to ensure a match to the aircraft. • Review of Required Flight Manuals & Supplements: Gulfstream approved flight manuals will be reviewed to determine revision status and presence of all required approved flight manual supplements. Flight manual supplements will be cross-checked against STCs. • Update of Required Flight Manuals and Supplements: If required, Gulfstream will update any missing or outdated items in the flight manual supplements section of the flight manual or supplement binder with current data. A budgetary estimate to research and retrieve missing flight manual supplements is $75 per occurrence. Incomplete records may substantially increase this cost. Page 4 of 14 This proposal is confidential between Gulfstream and the Customer. sd' Return to Table of Contents DAC Roy. February 5, 2015 EFTA01083130 ID # 7018884. ROO 12 lune 2015 (;u:silvan,GV Gulfstream GV Serial Number 572 South Aviation, Inc. PART I. Workscope Description (Continued) C. MECHANICAL (CONTINUED) 1. Aircraft Records and Condition Survey (Continued) Aircraft Condition Survey includes the following: • Cockpit and Cabin Avionics Equipment - Operational Test: A cockpit avionics ramp check is performed and involves powering up all major avionics equipment and operationally testing systems, such as navigation, communication and flight management systems for proper operation. A cabin ramp check is performed and involves powering up of cabin outfitting components and systems. This test does not include the use of test equipment or troubleshooting of avionic systems. Results will be fully documented on the work order and findings will be highlighted in the Survey. As the Survey progresses, discrepancies may be identified. At this point, discrepancies will be listed on summary sheets and provided to customer. Any Engineering dispositions will be an additional expense and will be billed, as required. • Inventory of Avionics and Emergency Equipment: A physical inventory of major avionics equipment will be accomplished and the results recorded in the report. The avionics inventory is limited to accessible areas only, additional access will be billed at time and material. This inventory will be cross- referenced against the equipment list during the documentation review. All cabin and cockpit installed emergency equipment will be inventoried and recorded in the report. • Physical Survey: Is in accordance with attached Gulfstream CMP (Computerized Maintenance Program) tasks, which provide a detailed view of specified areas of aircraft. The suggested survey workscope is intended to provide you with a general visual evaluation of selected areas of the aircraft. • Cockpit and Cabin Compartment Above Floor Inspection: A general visual Inspection will be performed of cockpit, cabin, and baggage compartments for mechanical and cosmetic discrepant conditions which are deemed as unsatisfactory. Interior access will not be required or included for this general visual inspection. Note: This general visual Inspection does not include NDT of cabin windows. • Optional FAA 135 Regulation Log Research: A budgetary estimate to perform a FAA 135 Regulation Log Research is approximately $3,500. This FAA Part 135 Regulation Log Research is limited to the collection of pertinent parts tracking documents associated with Life-Limited or otherwise tracked serialized components, which are currently, installed on the aircraft from the aircraft historical records files supplied by the operator at time of aircraft input. Note: This research does not imply to include any requirements as to pertain to the physical condition of the aircraft in regards to FAA Part 135 Compliance. Aircraft Records and Condition Survey Report: • The report is a bound document and is divided into indexed sections. The format facilitates rapid access to desired information and highlights the major elements of the Survey. All findings and information yielded by this Survey will be provided in the report and on the related work order upon completion of the Survey. Two (2) copies of the report will be provided to the purchaser of the Survey and one (1) copy of the discrepancies noted to the owner (additional report copies are available at $150/each). Copies will not be provided to any other party including the owner of the aircraft unless expressly authorized in writing by the purchaser of the Survey. Page 5 of 14 This proposal is confidential between Gulfstream and the Customer. seh Return to Table of Contents GAG Rev. February 5. 2015 EFTA01083131 ID # 7018884, R00 12 lune 2015 Gulfstream GV Serial Number 572 South Aviation, Inc. PART I. Workscope Description (Continued) C. MECHANICAL (CONTINUED) 1. Aircraft Records and Condition Survey (Continued) ARCS Test Flight: • This is an extensive flight test regimen flown by Gulfstream test pilots. The flight test card will be identical to the one used by Gulfstream's Flight Department to evaluate pre-owned aircraft being considered for purchase by Gulfstream. • ARCS Flight results are fully documented and reported in the work order and the ARCS Survey Report. • Gulfstream Test Pilots are not located at all Gulfstream facilities. All pilot travel expenses (if required) and fees will be the responsibility of the customer per the Gulfstream Labor Rate letter. • Included in the item price: -A- Pilot Labor (for test flight only) Preflight Traveler (required prior to Flight Test). • Not included in the price and (if required) are estimated at $7,500": Pilot Labor (for travel only) Per Diem — Two (2) Pilots for Two (2) Days Lodging — Two (2) Rooms for One (1) Night Rental car — One (1) Day) 4 Airfare — Two (2) Round Trip "Based on U.S. Domestic travel. • Fuel for the Flight Test will be billed separately. For budgetary purposes, an estimated 1,800 to 2,300 gallons of fuel will be required to accomplish the test flight. Actual charges will vary depending on the amount of fuel on the aircraft at arrival, and fuel prices at the time of service. Standard Package Brake Inspection (accomplished on the Aircraft): • A detailed visual inspection of the brakes will be accomplished (without disassembly) prior to removal from the aircraft. This will include inspection of the drive clips and leak checks. • The Brake wear indicators will be measured and the remaining wear will be documented in the work order. • Following the landing gear corrosion inspection (see CMP exhibit), the brakes will be reinstalled and a complete functional test performed. Premium Package Brake Inspection (accomplished at a Gulfstream repair and overhaul facility): • The brakes will be removed and sent to a Gulfstream repair and overhaul facility for the following: Detailed Visual Inspection Heat Pack Removal and Inspection (Note: Any remaining wear will be documented in the work order.) Key Slot/Tenon Slot Inspection •• Torque Tube Inspection Cylinder Block Teardown and Inspection Leak Checks • Discrepancies will be documented on a work order with determination of the financially responsible party (buyer or seller), prior to commencement of the work. • Upon completion of the inspection, the brakes will be reinstalled and a complete functional test performed. Page 6 of 14 This proposal is confidential between Gulfstream and the Customer. sch Return to Table of Contents GAC Rey. February 5, 2015 EFTA01083132 ID # 7018884, ROO 12 lune 2015 Gulfstream GV Serial Number 572 rerun GN, South Aviation, Inc. PART I. Workscope Description (Continued) C. MECHANICAL (CONTINUED) 1. Aircraft Records and Condition Survey (Continued) Optional Services: • Gulfstream also offers a complete in-house detailing service for your Gulfstream aircraft. Our experienced team of professionals can perform any detailing service; from a dry wash of the aircraft exterior to shampooing and stain-treating carpets and furnishings. • Exterior services include washing of the aircraft (to include landing gear), waxing the aircraft with Aeroglaze, buff and polish of leading edge "brite work', and sanding to remove surface corrosion. An application of Teflon coating is also available to enhance the life of your paint as well as to reduce aircraft exterior cleaning time and costs. • Interior services include sanitizing galley and lavatories, re-corking of drawers, shampooing of carpets, re- oiling of leather, and an application of soil and stain repellent for the carpet and upholstery. D. PAINT Not Requested Page 7 of 14 This proposal is confidential between Gulfstream and the Customer. set Return to Table of Contents GAC Rey. February 5, 2015 EFTA01083133 ID # 7018884, ROO 12 lune 2015 Gulfstream GV Serial Number 572 I South Aviation, Inc. 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 GV aircraft, Serial Number 572 (-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 South Aviation, Inc. ("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 (VCRs") paragraph. Page 8 of 14 This proposal is confidential between Gulfstream and the Customer. sob Return to Table of Contents GAC Rey. February 5, 2015 EFTA01083134 ID It 7018884, ROO 12 lune 2015 Gulfstream GV Serial Number 572 South Aviation, Inc. 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 Gulfstream 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 PlaneParts© program. To enroll or learn more about the PlaneParts© program please visit htto://www.gulfstream.com/oroduct-suoport/suoport-services/planeoarts. 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 9 of 14 This proposal is confidential between Gulfstream and the Customer. sd' Return to Table of Contents GAC Rey. February 5, 2015 EFTA01083135 ID # 7018884, ROO 12 lune 2015 Gulfstream GV Serial Number 572 I r South Aviation, Inc. 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 Gulfstream'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-for 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 Customer's 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 Page 10 of 14 This proposal is confidential between Gulfstream and the Customer. SOP, Return to Table of Contents GAC Rey. February 5, 2015 EFTA01083136 ID # 7018884, R00 12 lune 2015 Gulfstream GV Serial Number 572 South Aviation, Inc. 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 non- refundable should the visit be cancelled or work scope change to eliminate those items. If any portion of an invoice is disputed, the Customer shall nevertheless pay all undisputed amounts per this schedule. Gulfstream shall not be required to release Customers aircraft to depart if Customers total outstanding balance owed to the Gulfstream parties exceeds the lesser of $150,000 or Customers available credit limit. All sums past due bear interest at the lessor of 1.5% per month, or the maximum rate allowable by law, plus reimbursement of 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. 10-15825 Reference your Five (5) Digit Customer Number (XX-XXX) Bank Fedwire Routing No. (ABA) Identifiers: S.W.I.F.T CHASUS33 ACH Credit Routing No. (ABA 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 11 of 14 This proposal is confidential between Gulfstream and the Customer. Return to Table of Contents GAC Rey. February 5, 2015 EFTA01083137 ID ft 7018884, R00 12 lune 2015 Gulfstream GV Serial Number 572 South Aviation, Inc. 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 REFURBISHMENT (USD) Accept (select one) B. AVIONICS CABIN ELECTRONICS C. MECHANICAL 1. Aircraft Records and Condition Survey II Lite Package - Aircraft Records and Condition Survey (ARCS) $27.000 i 1.2 Basic Package - Aircraft Records and Condition Survey (ARCS) $47,500 Standard Package - Aircraft Records and Condition Survey (ARCS) $75,500 Premium Package - Aircraft Records and Condition Survey (ARCS) $98,000 D. PAINT QUOTED WORKSCOPE TOTAL BASED ON CUSTOMER ACCEPTED ITEMS 'Default value is set to SO until Customer selections have been made above. Page 12 of 14 This proposal is confidential between Gulfstream and the Customer. seh Return to Table of Contents GAC Rev. February 5.2015 EFTA01083138 ID * 7018884, ROO 12 lune 2015 Gulfstream GV Serial Number 572 I ;411sliraii i ( IA South Aviation, Inc. PART IV. Executive Summary and Proposal Acceptance (continued) Schedule Planning Estimated Days Leadtime 5 Calendar Days (For definition, see Part II Section A or click here Downtime 10-12 Working Days (For definition, see Part II Section B or r kh-r- Ritote 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) The Aircraft Records and Condition Survey is limited in scope, and Gulfstream cannot guarantee that this Survey will uncover all problems that exist with the inspected aircraft. Ultimately, the buyer must rely on their own judgment as to the aircraft value and the sellers warranty, if any, as to the aircraft's condition. For budgetary planning purposes, estimated material for the Aircraft Records and Condition Survey CMP packages (Items 1.2 through 1.4) is approximately $7,000, and it does not include material required for clearing of any discrepancies. Page 13 of 14 This proposal is confidential between Gulfstream and the Customer. soh Return to Table of Contents CAC Rev. February 5. 2015 EFTA01083139 ID # 7018884, R00 12 lune 2015 Gulfstream GV Serial Number 572 t i 'Al 1 1 ( - i\ South Aviation, Inc. 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. SOUTH AVIATION, INC. GULFSTREAM AEROSPACE CORPORATION ("Customer- ) ("Gulfstream") By: By: Name: Name: Tom Baliya Title: Title: Regional Sales Manager, Product Support Sales Date: Date: 12 June 2015 Please complete and return all pages of PART IV via fax (+1 or email (psintemalsales@gulfstream.com). Page 14 of 14 This proposal is confidential between Gulfstream and the Customer. seh Return to Table of Contents GAC Rey. February 5, 2015 EFTA01083140 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 tenns 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 their affiliates, including 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 otherwise 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 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. 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, levies, penalties and tariffs 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 harmless with respect thereto. 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).. GAC Rev. Jan. 1.2014 1 of 4 EFTA01083141 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. 6.3.1 In addition to the warranty remedy provided in Section 6.2, but subject to Section 6.3.2 below, if any defective Work, or 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 6A, 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 pm•damage fair market value and for Gulfstream to receive clear title thereto. 6.3.2 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 Flight 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. 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 otherwise 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 Gulfstrcam 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 GAC Rev. Jan. 1.2014 2 of 4 EFTA01083142 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. 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 otherwise 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 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 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 (1) 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 GAC Rev. Jan. 1.2014 3 of 4 EFTA01083143 the two thus selected shall select a third neutral arbitrator meeting the specified qualifications within IS 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. 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: GAC Rev. Jan. I. 2014 4of4 EFTA01083144 IDs 7018884.800 Tiered Package • Aircraft Records and Condition Survey Included in MIMagrarglift Related Code Code Description Material Estimate Lite Package • Aircraft Records and Condition Survey (Exhibit 1) Check Airworthiness Directives Check Customer Bulletins Perform Avionics Inventory Review Aircraft Status and Records Cockpit ;Cabin .' Baggage Comport. Above Floor General visual inspection Avionics • Functional Ramp Test (Inspection 291401 Main Hydraulic System Manifold Differential Pressure Indicator (Left) • Detailed Inspection 291402 Right System Manifold Differential Pressure Indicator • Detailed Inspection 292501 Auxiliary Hydraulic Pump Manifold Differential Pressure Indicator - Detailed Inspection 292502 Power Transfer Unit Manifold Differential Pressure Indicator • Detailed Inspeclion 316206 Configuration Warning Message: Han - Operational Test 321803 Main Landing Gear and Doors (Left) • Zonal Inspection 321804 Main Landing Gear and Doors (Right) • Zonal Inspection 322802 Nose Landing Gear and Doers • Zonal Inspection 324305 Brake Weer Indicator (Left Outboard) • Detailed Inspection 324308 Brake Weer Indicator (Left Inboard) • Detailed Inspection 324307 Brake Weer Indicator (RigN Inboard) • Detailed Inspection 324308 Brake Wear indicator (RigN Outboard) • Detailed Inspection 490001 Auxiliary Power Unit • Functional Test 491005 APO Enclosure FS 767- FS 797 • Zonal Inspection 496001 APU Exhaust Wet -General Visual Inspection 531010 Redone FS .4 thru FS 63 • Zonal Inspection 530205 Birdthike Plate (Leh) • Removal i InsIallation 530206 Birdstrike Plate (Right) • Removal i Installation 531015 Nose Gear Wheel Well FS 40 • FS 119 • Zonal Inspection 531045 Main Gear Wheel Wells FS 576 • FS 632 (Celt) • 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 531068 External Fuselage • General Visual inspection 531080 Left Electronic Equipment Rack FS 165 • FS 189 • Zonal Inspection 531081 Right Electronic Equipment Rack FS 147 • FS 181 • Zonal Inspection 531095 Alt Fuselage Move Floor FS 758 • FS 974 • Zonal Inspection 541005 Pylons External (Left) • Zonal Inspection 541008 Pylons External (Right) - Zonal Inspection 551003 Horizontal Stabilizer General Skins • General Visual Inspection 553040 Vertical Stabilizer • General Visual Inspection 570005 Wing Upper Surface View from on Wing (Left) • Zonal Inspection 570006 Wing Upper Surface View from on Wing (Right) • Zonal Inspection 570009 Wing Lower Surface (Left) - Zonal Inspection 570010 Wing Lower Surface (Rant)• Zonal Inspection 570013 Upper Wing Extension BL 642 • BL 545 (View from en Wing) (left) • Zonal inspection 570014 Upper Wing Extension BL 542 • BI- 545 (View from on Wing) (Right) • Zonal inspection 570015 Lower Wing Extension BL 542 • BL 545 (View from Ground) (Left) • Zonal inspection 570016 Lower Wino Extension BL 542 • BL 545 (View from Ground) (Right)• Zonal Inspeclion 574015 Wing Leading Edge External BL 44.0 • BL 529 Inboard of Navigation Light (Celt) • 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 711316 Poweeplant and Needle Doors Internal (Left) - Zonal Inspection 711316 Powerplant and Needle Doors Internal (Right) • Zonal Inspection 717007 LH Engine Drains System • Detailed Inspection 717008 RH Engine Drains System • Detailed Inspection Basle Pack • Aircraft Records and Condition Surve Exhibit Basic Package is Exhibit 1 Codes plus the following codes: GV Preflight inspection Checklist IRSOCT • 113 Rev. 23) 492301 Mil Compressor and Turbine Section • Boresco e Inspection 492102 APU Branched Wring Herne::: - Inspection 494206 Igniter Aug Mfg • Removal: Installation X 494207 Igniter Plug (Right) - Removal /Installation X 494208 APU Igniter Plug (Leg) - Inspection f Check 494209 APU Igniter Plug (Right) - Inspection/ Check 496102 EGT Sensor No. I (58 FtE220-49.75591 - Removal , Iretallalon 497005 APU Exhaust Gas and Tervoeralwe Sensor - Removal .' Installation 710025 LH Engine Test 0 • Engine Power Assurance Check 710011 LH Engine Rim • PreOperational Checks 710013 LH Engine Riot • Checklist 710028 RH Engine Test 4 • Engine Power Assurance Check 710012 RH Engine Run - Pre-Op:rational Checks 710014 RH Engine Run - Cheddisl 710029 LH Engine Test 6 • Vibration Survey 710030 RH Engine Test 6 • Vibration Survey 723101 LII Lowdresswe Compressor (Fan) Blades • Detailed Inspection 723102 RH Low-pressure Compressor (Fan) Blades • Detailed Inspection 724005 LII HP Turbine Stage 1 Rotor Blades • Baroscope 726006 RH HP Turbine Stage 1Rotor Blades • Borescepe 724007 L/1 High-pressure Turbine Neale Guide Vanes • Special Detailed inspection 742001 LH Engine banter Plug (No. 1) • Removal ! Installation 742036 LH Engine enter Plug (No. I) • Inspection i Check 742023 LH Ignition Syslern - Operational Check Page 1 or 6 EFTA01083145 Es 7018884.800 Tiered Package - Aircraft Records and Condition Survey Included in higggillikritalliga Related Ciltht Pncln Dtmorioll001 Material Estimate 742003 LH Engine Igniter Plug (No. 2) . Removal / Installation 742007 LH Engine Igniter Plug (No. 2) . InsFection :Check 724006 RH High-pressure Turbine Houle Guide Vanes • Special Detailed Inspection 742002 RH Engine Igniter Plug (No. I1- Removal .' IrMallaben 742006 RH Engine Igniter Plug No. II - Inspection / Check 742024 RH Ignitkin Syslem • Operational Check 742004 RH Engine Igniter Plug (No. 2) - Removal! Installation 742008 RH Engine Igniter Plug INo. 21- Inspection! Check 724009 LH Combustion Liner • Special Detailed Inspection 724010 RH Combustion Liner • Special Detailed Inspection 731023 LH Low-pressure Fuel Finer • Detailed Inspection 731027 LH Low.presstre Fuel Filler • Removal / Installation X 710015 LH Engine Tesl I - Wet Moll Operation Leak Chedt 731024 RH Low-pressure Fuel Filter • Detailed Inspeclion 731028 RH Lew ressure Fuel Filler • Removal! Installation X 710016 RH Engine Tesl 1 • Wel MotOr Operation Leak Check 790011 LH Me and Accessory Gearbox node C Detectors • Detailed In lion X 710017 LH Engine Rim Leak Check Test 2A • LP Fuel Syslem! Oil System 790015 LH Engine Fwd Bearing Chamber Magnetic Chip Detector . Removal / Installation 790017 LH Engine All Bearing Chamber Magnetic Chp Deteclor • Removal! Installation 790019 LH Engine Accessory Gear Box Magnelic Chip Detector • Removal lInsIallation 790012 RH Engine and Accessory Gearbox Magnetk Chip Detectors • Detailed Inspection X 710018 RH Engine Run Leak Check Test 2A - LP Fuel System/ Oil System 790016 RH Engine Fwd Bearing Chanter Magneto Chip DCICAOr . Removal i Installation 790018 RH Engine AR Bearing Chamber Magnetic Chip Detector - Removal / Installation 790020 RH Engine Accessory Gear Box Magnetic Cap DeCdor - Removal / Inslalalion 792101 LH Oil Pressure Filter • Detailed Insoettlen / Discard 792105 LH Oil System Pressure Filler Element • Removal; Inslallation X 792102 RH Oil Pressure Alter • Detailed Inspection! Discard 792106 RH Oil System Pressure Plot Element . Removal: Ireallaion X Standard Package • Aircraft Records and Gandhian Survey (Exhibil 3) Standard package is Exhibit 1 and Exhibit 2 Codes plus the following cedes: 321003 Main Landing Gear ComponeMs (Leg) • Detailed Corrosion Inspection X 121500 Hydraulic System Reservoir ILO) • Servicing 121501 Hydraulic Syslem Reservoir (Righti • Servicing 290001 Hydraulic System Reeding Procedure 290002 Hydraulic System Reed Procedure • Alletmle 321005 Men Landing Gear (Lehi - Lubricalion 321027 Men Gear Trunnion Pin (Len Fernald) • Removal/ Inslalalion 321029 Men Gear Trunnion Pin (Len AM - Removal! Installation 321201 Men Landing Gear Shock Absorber (Left) • Servicing 321217 Men Landing Gear Shock Absorber (Lefil • Removal / Installation 321228 Men Landing Gear Axie Filling Airmen Pin (Left) Corrosion Inhibiting Corncound Application 321235 Men Landing Gear Me Filling and Me Filling Nut (Lek) Corrosion Inhibiting Convourrd Application 321239 Man Landing Gear Shock Absorber Upper and Lower Mach Fins (Left) Corrosion Inhbiling Compered Application 321243 Man Landing Gear Sidebrace Actuator Mach Pins/ Trunnion Area (Led Corrosion Inhibiting Compound Application 321247 Man Landing Gear Uplock Roller Refll Corrosion Inhibiting Cron-pound Application 321251 Man Landing Gear Striker Ann (Lef) Corrosion Irbil:ding Compound Applicaton 321301 Man Landing Gear Me Filling (Leg - Removal! Installation 323006 Lancing Gear Emergency Extension Nitrogen Slowdown Bottle - Servicing 323015 Man Landing Gear Spindle Pin (Lein - Removal! Installation 323021 Men Landing Gear Sidebrace Reg) - Removal / Installation 323900 Landng Gear • Functional Tesl 323901 Landng Gear Emergency Eden ion Operational Tesl 323906 Landng Gear Cycling - Operational Tesl 324003 Men Wheel Assembly (Left Outeoard) - Removal/Installation 324004 Men Wheel Assembly (Left Inboard) - Removal! Inslaltalion 324009 Man Landing Gem Wheel Bearing (LSI Oulboardl • Inspecion / Check 324010 Man Landing Gem Wheel Bearing (Leg Intoardi - Inspection / Check 324017 Wheel and Brakes - Functional Teal 324101 Man Wheel Brake (Leh) - Blaming Procedures 324105 Brake Assembly (Left Outboard): Removal / Installation 324106 Brake Assembly (Left Inboard) . Removal/ Inslalalion 324110 Brake Syslem Temperature Sensor (Lell Outboard) - Removal / Inalallalion 324111 Brake Syslem Ternperakee Sensor (Lell Inboard( • Removal / InstallMien 324124 Parking ;Emergency Brake AC0.111"413,01. Servicing 324144 Man Landing Gear Brake Assembly (Len Outboard) . Detailed Inspection 324145 Men Landing Gear Brake Assembly (Len Inboard) - Deleted Inspection 324153 Brake Rotor Drive Clip (Lell Outboard) - Inspection 324154 Brake Rotor Drive Clip (Lell Inboard! • Inspection 324202 Anbskid - Asclional Teal 324221 Wheel Speed Transact, (Left Outmatch - Removal / Installation 324222 Wheel Speed Transact, (Left Inboard) - Removal/ Inslalatial 321004 Main Landing Gear Componerris (Right) • Defined Corrosion Inspection X 321006 Man Landing Gear (Right) • Lubricabon 321028 Man Gear Trunnion Pin (Right Forward) - Removal! Installation 32103D Man Gear Trunnion Pin (Right Afl) - Removal! Installation _321202 Man LandingGear Shock. Absorber ggighl) • Servicing 321218 Man Landing Gear Shock Absorber (Right) • RemovalI InsIaltalion 321232 Man Landing Gear Me Fitting Airmen Pin (Right) Corrosion Inhibring Confound Application 321236 Man Larding Gear Me Filling and Me Filling Nut (Flight) Corrosion Inhibiting Compound Application 321240 Men Landing Gear Shock Absorber Upper and Lower Alla,' Fins (RigMl Corrosion Inhibiting Compound Application 321244 Man Landing Gear Sidebrace Actuator Mach Pins/ Trunnion Area (Righl) Corrosion Inhibiting Confound AppIcation 321249 Man Landing Gear Uplock Roller (Right) Corrosion Inhibiling Cm/pound Appicalice Page 2 of EFTA01083146 CM 7018884.R00 Tiered Package - Aircraft Records and Condition Survey Included in MIggialifidatt Related Cede r'4 newidllei Material Estimate 321252 Man Landing Gear Striker Mn (Right) Corrosion Inhibiting Conpourd Application 321302 Man Landing Gear Axle Filling (Right) - Removal / Inslallation 323016 Man Landing Gear Spindle Pin (Right) - Removal / installation 323022 Man Landing Gear Sidebrace (Right) - Removal I Installation 324005 Man Wheel Assembly (Righl inboard] - Removal! Installation 324006 Man Wheel Assembly (Rionl Outboard). Removal! Installation 324011 Man Landing Gear Wheel Bearing (Right Inboard)- inspection /Check 324012 Man Larding Gear Wheel Bearing (Right Outboard) • Inspection /Check 324102 Man Wheel Brake (Rohn . Bleeding Proceolues 324107 Brake Assembly (Right Inboard] - Removal 1Installation 324108 Brake Assembly (Right Outboard] • Removal I Installation 324112 Brake System Temperature Sensor (Right Inboard) • RemovalI insIaltalion 324113 Brake System Temperature Sensor (Right Cu:board) - Removal / Installation 324146 Man Landing Gear Brake Assembly (Right Inboard) • Detailed Inspection 324147 Man Landing Gear Brake Assembly (Right Outboard] - Detailed Inspection 324155 Brake Baler Drive pip (Right Inboard) - Inspection 324156 Brake Rotor Drive Clip (Right OulboarM - Inspection 324223 Wheel Speed Transdocer (Right Inboard! - Removal! Installation 324224 Wheel Speed Transdocer (Rids Outboard) • Removal !Installation 122003 Nose landing Gear Components • Detailed Corrosion Inspection X 321255 Nose Landng Gear Shock SDul and Axle Assembly Corrosion Initialing Compound Application 321256 Nose Landng Gear Trunnian Assembly Corrosion Inhibiting Compound Application 321259 Nose Landng Gear Truss Brace Assembly Corrosion InNbiling Compound Application 321260 Nose Landng Gear Upper Tnomion Attach Pins Corrosion Inhibiting Compound Application 321263 Nose Landng Gear Upper Crag Brace Attach Pin Corrosion Inhibiting Compound Application 321264 Nose LandngGear Striker Arms Corrosion inhibting Compound Application 322004 Nose Lancing Gear - Lubrication 322202 Nose Landng Gear Shock SUM - Servicing 324001 Nose Wheel Assembly (Leh) - Removal / installation 324002 Nose Wheel Assembly (Right) • Removal/Installation 324007 Nose Wheel Bearings (Lell) • inspection / Pack 324008 Nose Wheel Bearingsiliht . insoecbon I Pack 325003 Steering - Functional Test Premium Package - Aircraft Records and Condition Survey (Exhibit 4) Premium Package is Exhibit 1. Exhibit 2 and Exhibit 3 Codes plus the following codes: 1A! 500 Hour Inspection Codes 121400 LH Air Tate* Starter Oil • Change X 121401 RH Air Turbine Starter Oil • Change X 212511 Display Unit Fan Filbert • Inspection 316021 DU No. 1 • Removal: IrMallVion 316022 DU Ne. 2 - Removal! Installation 316023 DU No. 3 - Removal I Installation 316024 DU Ne. 4 • Removal I Instant/ion 316025 DU Ne. 5 • Removal I Instant/ion 316026 DU No. 8. Removal: Installation 215227 Primary I Secondary Heal Exchanger (Left)- Detailed Inspeclian 215228 Primary / Secondary Heal Exchanger (Right) • Detailed Inspection 242111 Integrated Drive Generator (Left) - Detailed Inspection 242109 Integrated Drive Generator (Leff] . Oil Level Check 242141 Integrated Drive Generator Oil Scavenger Filter Dillerenbal Pressure Imitator (Left) • Inspection 242112 Integrated Drive Generator (Right) • Detailed Inspection 242110 Integrated Drive Generator !Right) • Oil Level Check 242142 Integrated Drive Generator Oil Scavenger Filter Dillerenbal Pressure InciCaler (Right) • Inspection 242115 Integrated Drive Generator (Left) • Servicing 242118 Integrated Drive Generator (Right) • Servicing 258282 Personal Breathing Equipment (No. 1) - Debited Inspection 256281 Personal Breathing tot:went No. II • Removal i Installation 258285 Personal Breathing Equipment (No. 2) • Detailed Inspection 256284 Personal Breathing Eq.:rent No. 21- Removal ,Iratallaton 271107 Aileron Actuator Load Relief Bungee Assembly (Left) - Inspection 271108 Micron Actuator Load Relief Bungee Assembly (Right) • Inspection 271307 Aileron Hydraulic Boost Actuator (Leg) • Inspection 271308 Aileron Hydraulic Boost Actuator (Right) • Inspection 273008 Elevator Actuator Load Relief &epee (Left) • Inspection 273009 Elevator Actuator Load Relief Bmgee (Right) • Inspection 273407 Elevator Hydraulic Dual Tandem Actuator (Lift). Inspection 273408 Elevator Hydraulic Dual Tandem Actuator (Right) - Inspection 276019 Flap Actuator Travel Nut Mehl • Lubrication 275020 Flap Actuator Travel Nut (Right) • Lubrication 281407 Gravity Water / Fuel Drain Valve (Left)- Operational Test 281408 Gravity Water! Fuel Drain Valve (Right) - Operational Test 304105 Windshield Sine. Seal (Left) • Detailed Inspection 304108 Windshield Surface Seal (Right) - Detailed Inspection 318001 Caning Wanting System (Including Audio) • Operational Test 318201 Symbol Generator Switching • Operational Check 318203 MENU Capability to Display Standby Engine InsamneMs • Operational Test 318207 Enhanced Ground Proximity Warning System • Operational Check 318208 Elevator Mistrim / Aileron Roblin Messages • Operational Test 321045 Main Landing Gear and Attachments (Left) • General Visual Inspection 321048 Main Landing Gear and Attachments (Right) • General Visual Inspection 321801 Main Landing Gear Door tinges (Leh) • Lubrication Page 3 of 6 EFTA01083147 we 7018884.800 Tiered Package - Aircraft Records and Condition Survey Included in MiliglIBNISI201 EithlkiiCracig Code Description Material felinele 321802 Main Landing Gear Door 16119/15 (Right) • Lutz...kat:Ion 322006 Nose Landing Gear and Attachments • General Visual Inspection 322901 Nose Landing Gear Door Hinges • Lubrication 328201 Nose Wheel Steering Unit • Lubrication 328202 Nose Wheel Steering Collar Assembly I Slave Gear • Lubrication 334050 Navigation (Position) Light Lens- Detailed Inspection 831012 Exterior Radome Faking Installation • Detailed Inspection 831014 Enhanced Vision System Sapphire Window Installation • Detailed Inspeciion 723103 LH Low-pressure Compressor (Fan) Annulus Fillers • Detailed Inspection 723109 LH Lowpresswe Compressor Inlet Cone - Detailed Inspection 723161 LH LP Compressor Front Blade Retaining Ring - Detailed Inspection 723165 LH Fiord Blade Retaining Ring • Removal / Installation 723801 LH Lowpressure Can-presser Nose Cone- Removal! Inslallalion 723805 LH Lorepressure Compressor (Fan) Mnulus Filler No. 1 - Removal !Installation 723806 LH Lov&presswe Compressor (Fan) Mnulus Filler No. 2 - Removal ., Inslallalion 723807 LH Lovepressure Compressor (Fan) Annulus Filler No. 3 - Removal ., Installation 723808 LH Lorepresswe Compress:, (Fan) Annulus Filler No. 4 - Removal ., Inslallalion 723809 LH Low pressure Con-presser (Fan) Annulus Filler No. 5 - Removal) Installation 723810 LH Lowpressure Compressor (Fan) Annulus Filler No. 6 - Removal / Installation 723811 LH Lowpressure Compressor (Fan) Annulus Filler No. 7 - Removal / Installation 723812 LH Lowpressure Con-presser (Fan) Annulus Filler No. 8 - Removal / Installation 723813 LH Lowpressure Can-presser (Fan) Annulus Filler No. 9 - Removal / Installation 723814 LH Lowpressure Can-presser (Fan) Annulus Filler No. 10 - Removal / Installation 723815 LH Lowpressure Can-presser (Fan) Annulus Filler No. II - Removal / Installation 723816 LH Lowprassure Can-pressor (Fan) Annulus Filler No. 12 - Removal / Installation 723817 LH Lowpressure Can-pressor (Fan) Annulus Filler No. 13 - Removal / Installation 723818 LH Lorepressure Compressor (Fan) Annulus Filler No. 14 - Removal / Installation 723819 LH Lorepressure Compressor (Fan) Annulus Filler No. 15 - Removal / Installation 723820 LH Lovepressure Compressor (Fan) Annulus Filler No. 16 - Removal / Installation 723121 LH_Lorepressure Compressor (Fan) Annulus Filler No. 17 - Removal/Installation 723(122 LH Lowprassure Con-presser (Fan) Annulus Filler No. 18 - Removal/Installation 723823 LH Lowpressure Compressor (Fan) Annulus Filler No. 19 - Removal/Installation 723824 LH Lowpressure Compressor (Fan) Annulus Filler No. 20 - Removal/Installation 723825 LH Lowpressure Can-presser (Fan) Annulus Filler No. 21 - Removal t Installation 723826 LH Lowpressure Can-presser (Fan) Annulus Filler No. 22 - Removal i Installation 723827 LH Lowpressure Can-presser (Fan) Annulus Filler No. 23 - Removal i Installation 723828 LH Lowpresswe Compressor (Fan) Annulus Filler No. 24 - Removal! Installation 723853 LI1Nose Cone Rotating Fairi • Removal: Inslallalion 723104 RH Low-pessue Compressor (Fan) Mnulus Fillers • Detailed Inspection 723109 (7231101 . RH Lowpressura Compressor Mel Cone . Detailed Irepeolon 723161 (7231621 RH LP Compass°. From Blade Retaining Ring . Detailed in ion 723165 (7231661 RH Freed Blade Retaining Ring - Removal / Imullaton 723801 (7238021 RH LtI1WPICSSUM Compressor Nose Cone . Removal/ Inslallalion 723805 (7238291 RH Low.oressure Cancressor Pan) Annulus. File, No. 1 • Removal; Inslallalion 723806 (7238301 RH Low.oressure Compressor IFan) Annulus File, No. 2 • Removal; Inslallalion 723807 (7238311 RH Low.pressure Compressor (Fan) Annulus File, No. 3 • Removal; Inslallalion 723808 (7238321 RH Low.pressure Compressor Pan) Annulus Filer No. 4 - Removal i Inslallalion 723809 (7238331 RH Low.pressure Compressor Wan) Annulus Filer No. 5 - Removal; Inslallalion 723810 (7238341 RH Low.pressure Compressor (Fan) Annulus Filer No. 6 • Removal t Inslallalion 723811 (7238351 RH Low.pressure Compressor (Fan) Annulus Filer No. 7 • Removal / Installation 723812 (723836) RH Lowpressure Compressor (Fan) Annulus Filer No. 8 • Removal / Installation 723813 (7238371 RH Low.pressure Compressor (Fan) Annulus Filer No. 9 • Removal; Inslallalion 723814 (7238381 RH Lowpressura Compressor (Fan) Annulus File, No. 10 • Renal : Installation 723815 (7238391 RH Lowpressura Compressor Wan) Annulus File, No. 11 . Removal: Installation 723816 (7238401 RH Lowpressura Compressor Pan) Annulus Filer No. 12 - Removal .' Installation 723817 (7238411 RH Lowpressura Compressor Pan) Annulus File, No. 13. Removal: Installation 723818 (7238421 IN Low.oressura Compressor Pan) Annulus File, No. 14 - Removal / Installation 723819 (7328431 RH Low.oressura Compressor (Fan) Annulus File, No. 1S. Removal / Installation 723820 (7238441 RH Low.pressure Compressor Pan) Annulus Filer No. 16. Removal / Installation 723821 (7238451 RH Low.pressure Compressor (Fan) Annulus Filer No. 17 - Removal / Irotallation 723822 (7238461 RH Low.pressure Canpressor (Fan) Annulus Filer No. 18. Removal / Iretallatton 723823 (7238471 RH Low.pressure Canpressor (Fan) Annulus Filer No. 19 - Removal / Iretallatton 723824 (7238481 RH Low.pressure Canpressor (Fan) Annulus Filer No. 20 - Removal / Iretallatton 723825 (723849) RH Lowpressura Canpressor (Fan) Annulus Filer No. 21 - Removal / Irotallatton 723826 (7238501 R/I Lowpressura Ccapressor (Fan) Annulus Filer No. 22 - Removal / Ireallaton 723827 (7238511 RH Lowpressura Ccapressor (Fan) Annulus File, No. 23 • Removal / Installation 723828 (7238521 RH Lowpressura Ccapressor Wan) Annulus File, No. 24 - Removal I Installation 723853 (7238541 RH Nose Cone Relating Fairing - Removal/ Inslalalien 726101 LH Accessory Gearbox Engine Oil Tank Flre Blanket • Detailed Inspection 726102 RH Accessory Gearbox Engine Oil Tank Fire Blanket • Detailed Inspection 783337 Primary Lock Actuator and Mechanism (Left) - Inspection 710021 Engine Test 3A 'Leh) - Thrust Reverser Cheek 783338 Primary Lock Actuator and Mechanism (Right) • Inspection 710022 Engine Test 3A tRighl) • Thrust Reverser Check 793001 LH Oil Aber Differential Pressure Indicator • Detailed Inspection 793002 RH Oil Filter Differential Pressure Indicator • Detailed Inspection 688010 BR700-80.900340 • Air Turbine Starter Oil Level 898010 BR70080-900340 • Air Turbine Starter Oil Level lcuLL2 Month InspecticutCodel 237004 Cockpit Voice Recorder • °corollary,' Test 240121 Emergency Battery Power System (Lett) • Operational Tesl 240122 Emergency Battery Power System (RigM1• Condone' Test 240123 Emergency Battery Power System (Forward) • Operational Test 240124 Emergency Battery Power System (Aft) - Operational Test 243011 L Main Battery- Capacity Check Page 4 of 6 EFTA01083148 log 7018884.800 Tiered Package • Aircraft Records and Condition Survey Included in Mandokautags Petaled Cade Pncln Reariotigg Material Estimate 243001 Man Battery (Cell)' Removal I Installation 213012 A Main Battery • Capacity Check 243002 Man Battery (Right) • Removal / Installation 256017 Fire / Crash Axe • Inspection 256028 Smoke Hood (Pilot) • Detailed Inspection 256027 Smoke Hoed (Copilot). Detailed Inspection 256028 Smoke Hoed (Observer) • Detailed Inspection 256043 First Aid Kit (No. 1) • Detailed Inspection 256041 First Aid 101 (No. 1) - Removal .• Installation 256044 First Aid Kit (No. 2) • Detailed Inspection 256042 First Aid 101 (No. 2) 256071 Flashlight (lb. 1) • Operational Test 256061 FlasHight (No. I) 256072 Flashlight (No. 2) • Operational Test 256062 FlasNight (No. 2) 256073 Flashlight (No. 3) • Operational Test 256063 Flashr hi No. 3) 256074 Flashlight lib 4) • Operational Test 256064 Flashlight (No. 4) 256075 Flashlight (No. 5) • Operational Test 256065 FlasHight (No. 51 256161 Medical Kit • Detailed Inspection 256160 Medical kit 256201 Life Vesl(s) • Detailed Inspection 256211 Life Vest (No. 1) • Percival ., Installation 256212 Lila Vest (No. 2). Removal .• Installation 256213 Life Vest (b. 3)' Remaval / Installation 256214 Life Vest (be. 4) - Removal / Installation 256215 Life Vest (No. 5) - Removal1Installation 256216 Life Vest (No.. 8) - gemomai'Installation 256217 Lib Vest (No. 7) - Removal / Installation 256218 Life Vest (No. 8) - Removal / Installation 256219 Life Vest (No. 9) - Removal / Installation 256220 Life Vesl (No. 101 . Removal/Installation 256221 Life Vesl (No. 111 - Removal/Installation 256222 Life Vesl (No. 121 . Removal/Installation 256223 Life Vesl (No. 13) . Removal/Installation 256224 Life Vesl (No. 14) . Removal ! Installation 256225 Life Vest (No. 15) . Removal/Installation 256226 Lib Vest (No. 16) . Removal/ Installation 256227 Life Vest (No. 171. Removal I Installation 256228 Life Vest (No. 181 - Removal r Installation 256229 Life Vest (No. 19) - Removal r Installation 256230 Lila Vest (No. 201 - Removal r Installation 256231 Life Vest (No. 211 - Removal; Installation 256232 Life Vest (No. 221 . Removal; Installation 256233 Life Vest (No. 23) . Removal/ Installation 256234 Life Vest (No. 24) . Removal/Installation 256235 Life Vest (No. 25) . Removal/Installation 256236 Life Veal (No. 26) . Removal / Installation 256250 Life Veal (Pilot). Removal! Installation 256251 Life Vest (Copilot) - Removal / keIrJlalion 256252 Life Vest (Observer) - Removal I Installation 256253 Life Vest (Crew Member) • Removal! Installation 256202 Life BM(s) (No. 1) • Detailed Inspection 256260 Lib Raft (No. II • Removal! Installation 256203 the Rata) (NO. 2) • Detailed Inspection 256261 Life Raft (No. 21 • Removal ,' Installation 256308 Emergency Locator Transmitter • Operational Test (FAR 91.207) 256301 Emergency Locator Transmitter • Removal! Installation 256311 Emergency Locator Transmitter . Operational Check 282559 Trash Receptacle Enclosure (Credenza)• Detailed Inspection 282560 Trash Receptacle Enclosure (Alt Lavatory) • Detailed Inspection 282561 Trash Receptacle Enclosure (Forward Lavatory) • Detailed Inspection 282562 Trash Receptacle Enclosure (Alt Galley! Annex) • Detailed Inspectica 282563 Trash Receptacle Endows, (Forward Galley I Annex) • Detailed Inspection 282564 Trash Receptacle Enclosure (Crew Refreshment Area) • Detailed Inspection 282585 Trash Receptacle Enelene (VP Cabinet) • Detailed Inspection 262568 Trash Receptacle Emden, (Midcabin Galley) • petaled Inspection 282562 Trash Receptacle Fke Extinguisher Wales (Credenta) • Detailed Inspection 282583 Trash Receptacle Fire Extinguisher Hordes (Alt Lavatory) • Detailed Inspection 262564 Trash Receptacle Fke Extinguisher Regales (Forward Lavatory)• Detailed Inspection 282585 Trash Receptacle Fke Extinguisher Noules (Aft Galley !Annex) • Detailed Inspection 282589 Trash Receptacle Fke Extinguisher Hordes (Forward Galley I Annex) • Detailed Inspection 262587 Trash Receptacle Fke Extinguisher Noules (Crew Refresh/nerd Area) • Detailed Inspection 262588 Trash Receptacle Fke Extinguisher Howes (VIP Cabinet) • Detailed Inspection nzses Trash Receptacle Fke Extinguisher Hordes (IMelcabin Gassy) • Detailed Inspection 262801 Portable Helen Fire Extingtisher (Cockpit) • Inspection 262600 Portable Raton Fire Eein iS1101 Cock . Removal! Installation 282802 Portable Halal Pm fad Sher (Cockpit) • Weight Check 262811 Portable Kahan Fire Ertl Sher (Forward Cabin • Inspection 262610 Portable 'talon Fire EeineLli51101 (Forward Cabin) • Removal; Installation 282812 Portable Raton Foe Extinguisher (Forward Cabin) • Weight Check 282821 Portable Raton Fire Extlnaulther (Alt Cabin) • Inspection 262620 Portable listen Fire CeinelliShel (Alt Cabin( . Removal! Imeallation 282822 Portable Raton Fire Extinguisher (Aft Cabin) • Weight Check 282831 Portable Raton Fire Extinguisher (Alt Lavatory) • Inspection P5905 e EFTA01083149 Oa 7018664,800 Tiered Package - Aircraft Records and Condition Survey Included in MillIdiggIlLcatt Related Ciatig reido Gerwrichtigg Material Estimate 262630 Portable 'talon Fire Extinguisher (Alt Lawmen.) • Removal / Installation 262632 Portable Malan Fire Extinguisher (Mt Lavatory) • Weight Check 262642 Portable Kahan Fire Extinguisher (Baggage Compartment} Weight Check 262640 Portable 'talon Fire Extinguisher (Baggage Compartment). Removal: Installation 262641 Portable !talon Fire Extinguisher (Baggage Cornoartmenl) • Inspection 335020 Cabin Emergency Llghtino • Operational Test 144008 IRU No. 1 Fan Filter • Inspection 344011 IRU No. 1 Fan Filler • Removal I Installation 316013 Symbol Generator No. 3 • Removal / Installation 316010 Symbol Generator • Operagenal Check 344009 IRU No. 2 Fan Filter • Inspection 344012 IRU No. 2 Fan Filler - Removal I Installation 242604 R IDG GCU - Removal / Installation 246002 R BPCU • Removal I Installation 242100 Engine AC Gereralion • Cperational Check 344010 IRU No. 3 Fan Filter • Inspection 344013 IRU No. 3 Fan Filler - Removal I Installation 344004 Inertial Reference System • Operational Check 316011 Symbol Generator No. 1 • Removal / Installation 353002 Portable Oxygen Bottle and Mask Assembly (No. I) • Detailed Inspection 353001 Portable Oxygen Bottle (No. I) • Removal / Installation 353007 Portable 0 Bottle and Mask As No. • Detailed Ins lien 353006 Portable Oxygen Bottle (No. 2) . Removal / Installation 182003 Water Sterilizer Finer • Discard X 361039 Water &entity - Removal I Installation 381029 Water System • Cperational Test 382002 Water Stonlizer Filial - Removal / Installation 621010 Main Entrance Deer • Lubrication 521015 Man Enhance Dear • Cperating Procedures 623005 Baggage Compartment Door • Lubrication 625001 Auxiliary Pressure Bulkhead Door Seal • Detailed Inspection 2A! 1000 New Inspection Codes 271110 Aileron Inter-Column Linkage Disconnect Assemblies • Operational Test 271303 Aileron Harclover Prevention System (Left) • Operational Check 271103 Aileron /' Flight Spoiler Control System - Finctional Test 271141 Aileron Actuator Load itch& Bungee (Loll)' Load Inspection 271304 Aileron Herdover Prevention System (Right) • Operational Check 271142 Aileron Actuator Load Reid Bungee (Right) • Load Inspection 272004 Rudder Torque Tube Bearing • Lubrication 272301 Rudder Ilardever Prevention System • Operational Test 272113 Rudder and Trim Control System - Operational Check 273032 LonaitudinM Control System Friction Check • inspection /Check 273113 Elevator Inter•Column Linkage Disconnect Assembly • Operational Test 273405 Elevator Hardener Prevention System • Operational Test 271143 Elevator Actuator Load Rebel Bungee Meg' - Load Inspection 271144 Elevator Actuator Load Rebel Bungee (Right) - Load Inspection 273005 Elevator Control System • Cperational Test 274106 Emergency Horizontal Stabilizer (Backup Mode) • Operational Test 276201 Ground Spoiler Auto Deploy Rejected Takeoff Mode • Operational Test 278202 Ground Spoiler Manual Retract Mode • Operational Test 493404 APIJ Fuel System Components, Lines and Connections • General Visual Inspection 711003 Intel Cowl Aerodynamic Surfaces (Lett) • Detailed Inspection 711004 Intel Cowl Aerodynamic Surfaces (Right) • Detailed Inspection 711005 Cowl Fasteners and Attachment Features (Lett) • Detailed Inspection 711006 Cowl Fasteners and Attachment Features (Right) • Detailed Inspection 711007 Inlet Cowl Rear Bulkhead External Surfaces (Left) • Detailed Inspection 711008 Inlet Cowl Rear Bulkhead External Surfaces (Right) • Detailed Inspection 711015 Fixed Cowls (Len) • Detailed Inspection 711016 Fixed Cowls (Right) • Detailed Inspection 723311 LH Variable Staler Vane Drive Bracket Belts • Torque Reapplication 711019 Engine Loser Cowl Door (Lefts • Removal I Installation 710019 LH Engine Rio Leak Check Test 28 • Ira Fuel System 723312 RH Variable Stator Vane Drive Bracket Bolts • Torque Reapplication 711020 Engine Lower Cowl Door (Right) - Removal / Installation 710020 RH Engine Run Leak Check Test 28 - HP Fuel System 723401 LH Fan Track! Cold Stream Duct • Detailed Inspection 723402 RH Fan Track: Cold Stream Duct • Detailed Inspection 753025 LH Variable Staler Vane Mechanism • Lubrication 763115 Thrust Reverser Deactivate! Activate (Call) • Procedure 753026 RH Variable Stater Vane Mechanism • Lubrication 703116 Thrust Reverser Deactivate! Activate Oliglal - Procedure T80005 Thrust Reverser and Exhaust (Leg) • Zonal Inspection 780006 Thrust Reverser and Exhaust (Right) • Zonal Inspection 783009 Thrust Reverser Front Face Torsion Box Front Frame (Left) • Detailed Inspection 783010 Thrust Reverser Front Face Torsion Box Front Frame (Right) • Detailed Inspection 801011 LII Air Turbine Starter Magnetic Chip Collector • Detailed Inspection 801012 RH Air Turbine Starter Magnetic Chip Collector • Detailed Inspection Page 6 o!6 EFTA01083150