EFTA00589859.pdf

Gulfstream PRODUCT SUPPORT PROPOSAL Prepared for Presented by Gulfstream GIV Serial Number 1085 JEGE, LLC Mr. Larry Visoslri Rusty Cramer Regional Sales Manager, Gulfstream Aerospace Gulfstream Proposal # RO1 03 February 2016 EFTA00589859 TABLE OF CONTENTS PART I. Workscope Description 3 A. Interior Refurbishment 3 B. Avionics Cabin Electronics 3 C. Mechanical 5 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 EFTA00589860 ID # RO1 03 February 2016 Gulfstream GN Serial Number 1085 JEGE. LLC PART I. Workscope Description A. INTERIOR REFURBISHMENT AIM Not Requested B. AVIONICS / CABIN ELECTRONICS 1. Avionics 1.1 ASC 477 NZ 2010 V6.1 - TRIPLE $168,250 This Aircraft Service Change upgrades the existing NZ-2000 Flight Management Systems (FMS), via installation of version 6.1 software, to an NZ-2010 system with SBAS/LPV GPS upgrade. New Components: Two (2) Honeywell WAAS Capable GPS Receivers (Part Number (PN) HG2021KB01) Two (2) WAAS Capable GPS Antennas (PN S67-1575-137) One (1) ASC 477 Kit, NZ-2000 Flight Management System (FMS) 6.1 Upgrade. Modified Components: Three (3) each Honeywell NZ-2000 Navigation Computers (PN 7018879-030xx to 7018879-03036) Two (2) each Honeywell PZ-800 Performance Computers (PN 7004609-xxx to 7004609-940) Performance computers not at a minimum level of PN 7004609-925 will require additional upgrades not covered by this installation. Additional charges will apply. Prerequisites: • NZ-2000 Computers: Hardware Mod "E". For units without this modification, Honeywell Service Bulletin 7018879- 34-0051 (Pub. No. A21- 6111-004) will be required. Estimated additional cost is $2,600/unit. • PZ-800 Computers: Part Number 7004609-925. For units not at the -925 level or higher, additional modifications are required and will be addressed on a time and material basis. • The aircraft must currently be equipped with dual Global Positioning System (GPS) receivers. • Aircraft Serial Numbers 1000 through 1389: GPS #1 and #2 installations not installed by Gulfstream STC ST01716AT-D will require engineering review prior to incorporation of this ASC. • Existing FMS #1 and #2 installations must match Gulfstream STC ST01715AT-D or equivalent prior to incorporation. Concurrent Requirements: None Training: Pilot familiarization and training for Honeywell's FMS 6.1 software is offered through the Honeywell PC-FMS Training tool. Operators may order the tool at I or send an email to Effectivity: This Service Change is applicable to Gulfstream IV aircraft Serial Numbers 1000 through 1252 having ASC 349 or equivalent, and 1253 and subsequent. Certification: Per Gulfstream ASC 477 Navigation (ATA 34) NZ-2000 6.1 Software Upgrade with SBAS/LPV GPS Upgrade. Notes: • Price includes interior access, installation labor, the ASC Kit and associated materials. • The design of an Aircraft Service Change (ASC) is configured to a standard ("greenie") production aircraft. If spare wires, pin connections or locations called out in the ASC have been used for other modification, additional charges may apply. • This ASC may only be installed at Gulfstream Aerospace or Gulfstream- approved facilities. • All resources for this Service Change are managed by Gulfstream Product Support. Please contact your Regional Sales Manager to coordinate the availability of components and installation. • This ASC does NOT include Approval Guidance for RNP Procedures with SAAAR (Special Aircraft and Aircrew Approval Required). Page 3 of 14 This proposal is confidential between Gulfstream and the Customer. Micah Return to Table of Contents GAC Rev. October 15. 2015 EFTA00589861 ;i 11kt ID # R01 03 February 2016 Gulfstream GN Serial Number 1085 AGE. LLC PART I. Workscope Description (continued) B. AVIONICS CABIN ELECTRONICS 1. Avionics (continued) 1.2 Synthetic Vision (PDSV) - Provisions $35,000 • Provision for Synthetic Vision (PDSV) will be installed. • New SVS SEL switches will be installed on the Pilot and Co-pilots Glareshield and placarded INOP. • A new wiring interface will be installed between the existing Honeywell Symbol Generators (SG's), Traffic Alert and Collision Avoidance System (TCAS), Global Positioning System (GPS) and the Cockpit Display Units (DU's). Prerequisites: • ASC 476 - DU-885 Indicating / Recording Systems (ATA 31) Electronic Display System DU-885 Liquid Crystal Display (LCD) Installation (PlaneDeck). • ASC 477 - NZ 2010 6.1 Software with SBAS/LPV GPS Installation. Certification: This installation will be accomplished under a Gulfstream STC. Deviations from the STC (if required) would be completed on a Time and Material basis or quoted separately on a Work Change Request (WCR). Notes: • These are provisions only. The Symbol Generators (SG's) and Cockpit Display Units (DU's) will require software upgrades and modifications to activate the Synthetic Vision (PDSV) capability. Additional charges will apply. • Synthetic Vision activation is predicated on completion of the Gulfstream STC. Please contact your Gulfstream Regional Sales Manager (RSM) for current STC status. • The cost of this item will be deducted from the final PDSV installation price when the Customers elect to complete the installation. 1.3 ASC 476B V1.10 Software Enhancements Warranty Comply with the Revision B of ASC 476, installation of Barco Service Bulletin SBAv606167B. Warranty: The Display Unit retrofit upgrade to Software Version, V1.10 will be provided at No Charge (NC) if performed at a Gulfstream GIV Authorized Warranty Facility or Factory Authorized Service Center within twenty-four (24) months of the release date (08 August 2014) of this revision. Prerequisites: ASC 476 or ASC 476A Indicating / Recording Systems (ATA 31), Electronic Display System — DU-885 Liquid Crystal Display (LCD) Installation (PlaneDeck) and having Display Units, PN K9321061A02 (Black) or Part Number 9321061A11 (Grey). Notes: • This ASC is managed by Product Support Program Management (PSPM) and may only be installed at Gulf stream erosoace or GuItstr am- Thies. Incorporation must be coordinated through Gulfstream Scheduling at or . If not scheduled, aircraft downtime could increase significantly. • Only qualified personnel specifically trained and equipped may accomplish the Barco Service Bulletin, SBAv606167B REV 00 (or later revision). 1.4 ASC 415B Indicating and Recording - Upgrade SPZ-8000/8400 $28,744 This Service Change Revision upgrades the Fault Warning Computers (FWC) and, in some cases, the Symbol Generators (SG). For a detailed description of the improvements offered with this upgrade, please log in to your portal and review the "SPZ-8000 Modification Summary" listed on page 8 of ASC 415B. Prerequisites: None Effectivity: This Service Change is effective for GIV Aircraft 1000-1472. This or a similar change will be installed in production on Aircraft 1473 and subsequent. Note: This proposal does not include any squawks, pre-existing discrepancies or vendor Service Bulletins that may be required, except as specified. If required, this additional work will be handled on the basis of time and materials. Page 4 of 14 This proposal is confidential between Gulfstream and the Customer. Micah Return to Table of Contents GAC Rev. October 15. 2015 EFTA00589862 t I I ID rr S 801 03 February 2016 Gulfstream GN Serial Number 1085 JEGE, LLC PART I. Workscope Description (continued) C. MECHANICAL 2. Aircraft Maintenance Z1 12 Month CMP Tasks (Labor Only) $6,386 Accomplish 12 Month CMP Tasks. (Exhibit 1) Notes: • Correction of discrepancies is not included in the quoted price. • Due List projected through 31 December 2016. 2.2 24 Month CMP Tasks (Labor Only) $37,063 Accomplish 24 Month CMP Tasks. (Exhibit 2) Notes: • Correction of discrepancies is not included in the quoted price. • Due List projected through 31 December 2016. 2.3 36 Month CMP Tasks (Labor Only) $32,621 Accomplish 36 Month CMP Tasks. (Exhibit 3) Notes: • Correction of discrepancies is not included in the quoted price. • Due List projected through 31 December 2016. • If Cadmium Plating Degradation is found during the Wing Tank Internal Inspection, estimated repairs cost can be $35.000 in labor and materials depending on the condition of the aircraft. 2.4 150 Hour CMP Tasks (Labor Only) $1,527 Accomplish 150 Hour CMP Tasks. (Exhibit 4) Notes: • Correction of discrepancies is not included in the quoted price. • Due List projected through 31 December 2016. 2.5 150 Cycle CMP Tasks (Labor Only) $833 Accomplish 150 Cycle CMP Tasks. (Exhibit 5) Notes: • Correction of discrepancies is not included in the quoted price. • Due List projected through 31 December 2016. 2.6 Miscellaneous CMP Tasks (Labor Only) $15,686 Accomplish Miscellaneous CMP Tasks. (Exhibit 6) Notes: • Correction of discrepancies is not included in the quoted price. • Due List projected through 31 December 2016. Page 5 of 14 This proposal is confidential between Gulfstream and the Customer. Dlirseb Return to Table of Contents GAC Rev. October 15. 2015 EFTA00589863 ;1 lilS11)%it i ( ID a s R01 03 February 2016 Gulfstream GN Serial Number 1085 JEGE. LLC PART I. Workscope Description (continued) 2. Aircraft Maintenance (continued) 2.7 CB 227 Replacement, Oxygen System Flexible Hoses (Labor Not to Exceed) $11,425 This Customer Bulletin (CB 227) is a one-time action to replace all existing Part Number O202071 oxygen system flexible hoses with Part Number 37009 oxygen system flexible hoses. Effectivity: Aircraft Serial Numbers 1000 through 1499. Notes: • Estimated labor includes access to the affected oxygen system dropdown box flexible hoses. This includes access to oxygen drop-down boxes located in Personal Services Units (PSUs), as well as removal and reinstallation of headliners in the vestibule, forward galley, forward lavatory, crew rest, aft galley, or aft lavatory as necessary, and includes access to the therapeutic oxygen system. • The quoted price does not include removal of any cabinetry, cabin furniture or cabin compartment dividers. 2.8 CB 232A Modification, Aircraft Main Battery Chargers See Below Not Applicable to this aircraft per equipment installed This Customer Bulletin (CB 232A) is a one-time action to incorporate ELDEC Service Bulletin 8-842-24-02. Effectivity: All GIV Aircraft having part number 1159SCAV520 Series battery chargers Notes: • This Customer Bulletin is a managed program and must be accomplished at a Gulfstream Aerospace authorized facility. This Customer Bulletin must be coordinated through he Gulfstream Pro ram ffi vi mail at or by calling Gulfstream Scheduling at 1. or . If not scheduled, down times could increase significantly. • 1159SCAV520-5 Battery Chargers within (spares warranty) will be modified free of charge to 1159SB57520-11 or may be replaced with 1159SCAV520-7. Operators choosing to replace the 1159SCAV520-5 with 1159SCAV520-7 will incur additional costs. • Materials will be billed, as required. 2.9 CB 235 - Main Landing Gear Door Actuator End Cap Replacement - Life Limit (Labor Only) $3,936 Materials as Required (See Notes) This Customer Bulletin is a one-time action to replace all main landing gear door actuators that have been identified per CB 234 as having 9,500 Cycles Since New (CSN) or greater and all main landing gear door actuators for which CSN cannot be determined. Effectivity: All GIV aircraft Compliance: Compliance with this Customer Bulletin is required within twelve (12) months from the original issue date of 01 July 2015. Notes: • Contact Gulfstream Repair Control at or 800-810-4853 Option 1, then Option 3 for actuator rental / exchange availability and repair schedule prior to removing actuator(s) from the aircraft. • This Customer Bulletin is a managed program and must be scheduled through Gulfstream Repair Control. Gulfstream will manage a limited component rental / exchange pool. Operators performing this Customer Bulletin may elect to utilize the rental / exchange pool while the end caps on their original components are replaced. Due to a limited availability of assets, failure to schedule could result in significantly increased downtime. Page 6 of 14 This proposal is confidential between Gulfstream and the Customer. Dlirseh Return to Table of Contents GAC Rev. October 15. 2015 EFTA00589864 Giv ID R01 03 February 2016 Gulfstream GN Serial Number 1085 JEGE, LLC PART I. Workscope Description (continued) D. PAI Not Requested Page 7 of 14 This proposal is confidential between Gulfstream and the Customer. Dfitseh Return to Table of Contents GAC Rev. October 15. 2015 EFTA00589865 1 i II 1.`,11) i ( n ri ID or R01 03 February 2016 Gulfstream GN Serial Number 1085 JEGE. LLC 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 GIV aircraft, Serial Number 1085 ("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 JEGE, LLC ("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, and within the same calendar year as the date of this Proposal. Gulfstream reserves the right to adjust the pricing in this Proposal it the foregoing conditions are not satisfied. 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. Dlirseh Return to Table of Contents GAC Rev. Ocioter 15. 2015 EFTA00589866 ID # S RO1 03 February 2016 Gulfstream GIV Serial Number 1085 JEGE. LLC 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 vendor parts, materials, or 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© oroaram. To enroll or learn more about the PlaneParts© program please visit 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. Dlifseh Return to Table of Contents GAC Rev. October 15. 2015 EFTA00589867 fv: ID v R01 03 February 2016 Gulfstream GN Serial Number 1085 JEGE. LLC 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-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 Gulf stream, 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 10 of 14 This proposal is confidential between Gulfstream and the Customer. Dlitseh Return to Table of Contents GAC Rev. October 15. 2015 EFTA00589868 G ID a R01 03 February 2016 Gulfstream GN Serial Number 1085 JEGE, LLC 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. Unless otherwise agreed in writing, 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 Customers Aircraft to depart if Customers 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.), as additional items are added to the Work, additional progress payments may be required to continue Work on the Aircraft and all remaining outstanding balances must be paid prior to Aircraft 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) 021 000 021 Identifiers: S.W.I.F.T CHASUS33 ACH Credit Routing No. (ABA) 071 000 013 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. Dlitseh Return to Table of Contents GAC Rev. October 15. 2015 EFTA00589869 in, ID ir 801 03 February 2016 Gulfstream GN Serial Number 1085 AGE. LLC 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 ASC 477 NZ 2010 V6.1 - TRIPLE Synthetic Vision (PDSV) - Provisions ASC 476B V1.10 Software Enhancements ASC 415B Indicating and Recording - Upgrade SPZ-800018400 1.1 1.2 1.3 1.4 C. MECHANICAL Aircraft Maintenance 2.1 12 Month CMP Tasks 2.2 24 Month CMP Tasks 2.3 36 Month CMP Tasks 2.4 150 Hour CMP Tasks 2.5 150 Cycle CMP Tasks 2.6 Miscellaneous CMP Tasks 2.7 CB 227 Replacement, Oxygen System Flexible Hoses 2.8 CB 232A Modification, Aircraft Main Battery Chargers 2.9 CB 235 - Main Landing Gear Door Actuator End Cap Replacement - Life Limit (USD) Accept Decline $168.250 $35,000 See Item $28.744 D. PAINT QUOTED WORKSCOPE TOTAL BASED ON CUSTOMER ACCEPTED ITEMS 'Default value Is set to SO until Customer selections have been made above. $6.386 $37,063 $32.621 $1,527 $833 $15,686 $11.425 I See Item $3.936 Estimates based on Quoted Workscope , Materials/Outside Services for CMP Inspection Package(s)' $13,150 The estimated amount includes items marked with an *X" on the attached CMP Exhibit(s). The estimates are for planning purposes only and are subject to pricing and availability at the time of aircraft induction. Page 12 of 14 This proposal is confidential between Gulfstream and the Customer. Dlitseh Return to Table of Contents GAC Rev. October 15. 2015 EFTA00589870 ID # S R01 03 February 2016 Gulfstream GN Serial Number 1085 JEGE, LLC PART IV. Executive Summary and Proposal Acceptance (continued) Schedule Planning Estimated Days Estimated Leadtime' See Note 'The above leadtime is an estimate expressed in calendar days to allow for planning and scheduling of the Aircraft service visit and will 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. Note: This proposal contains items that are managed programs. Please contact your Regional Sales Manager for leadtime. Typical leadtimes for this item/workscope are 30 calendar days. Estimated Downtime' 20 Working Days 2The above downtime estimate is 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. Input Facility Gulfstream West Palm Beach 1500C Perimeter Road West Palm Beach. Florida 33406 Main Phone: Note: Changes to facility input may affect downtime. Please contact your Regional Sales Manager. 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 li h r Pricing • This proposal supersedes proposal ROO dated 05 January 2016. • If Cadmium Plating Degradation is found during the Wing Tank Internal Inspection, estimated repairs cost can be $35,000 in labor and materials depending on the condition of the aircraft. Page 13 of 14 This proposal is confidential between Gulfstream and the Customer. DIfseh GAC Rev. October 15. 2015 Return to Table of Contents EFTA00589871 ID a R01 03 February 2016 Gulfstream GN Serial Number 1085 JEGE. LLC 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. JEGE, LLC ("Customer") GULFSTREAM AEROSPACE CORPORATION ("Gulfstream") By: By: Name: Name: Rusty Cramer Title: Title: Regional Sales Manager, Product Support Sales Date: Date: 03 February 2016 Please complete and return all pages of PART IV via fax ( or email Page 14 of 14 This proposal is confidential between Gulfstream and the Customer. Dlitseh Return to Table of Contents GAC Rev. Ocioter 15. 2015 EFTA00589872 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 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 Gulfsueam's standard prices in effect on the date the material is used. Any incremental charge under Gulfsueam'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. Unless otherwise agreed in writing, for Work estimated to exceed One Hundred Thousand Dollars ($100,000.00), 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 One Hundred Fifty Thousand ($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.). as additional items are added to the Work, additional progress payments may be required to continue Work on the Aircraft and all remaining outstanding balances must be paid prior to Aircraft 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 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. Jan. 21.2016 1 of 4 EFTA00589873 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. Pans 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. 6.3 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 TERNIINATION 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. Jan. 21.2016 2 of 4 EFTA00589874 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: (I) 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 Patty'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. 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. INCIDENTAL CUSTOMER PROPERTY. Gulfstream assumes no responsibility or liability for any Incidental Customer Property brought or delivered to Gulfstream's premises by Customer, whether on the Aircraft or otherwise. "Incidental Customer Property" is any item associated with the Aircraft, its crew, representatives of the Customer, or its passengers, that is not a part of the certified Aircraft or directly related to its operation. such as loose aircraft or cabin equipment. typical catering supplies, or the like. Gulfstream reserves the right to decline to store any Incidental Customer Property on its premises which it deems, in its sole discretion, inappropriate or dangerous. The Customer is responsible for importing or exporting of Incidental Customer Property into or out of the boundaries of any nation and must adhere to all applicable import or export control laws and regulations. including without limitation Export Administration Regulations ("EAR") and International Traffic in Arms Regulations ("ITAR") for entries into and out of the United States. The Customer hereby agrees to defend, indemnify, and hold Gulfstream harmless from any and all claims made against Gulfstream arising out of Incidental Customer Property brought or delivered to Gulfstream's facilities, including losses incurred because of damage or theft, improper shipping or receiving, together with any criminal or civil penalties or other duties, imposts, taxes, liens or other obligation imposed by any governmental entity resulting from the presence of Incidental Customer Property on Gulfstream's facilities. 10. 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 other than the Aircraft or its contents. U. NO BAILMENT. No bailment is created by this Agreement, and Gulfstream shall not act as insurer of the Aircraft or any Incidental Customer Property while the Aircraft or Incidental Customer Property is present at Gulfstream's facility or otherwise in Gulfstream's custody or control. 12. 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. 13. 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. 14. 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. GAC Rev. Jan. 21.2016 3 of 4 EFTA00589875 15. 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. 16. 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. 17. INDEMNITY BY CUSTOMER ENTERING GULFSTREANI'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. 18. 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 Two Million Dollars ($2.000,000.00), 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 AAA. 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 UnitedNations. Convention on Contracts for the International Sale of Goods (frequently referred to as the "UNCISG") shall not apply. 19. 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. 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 20. 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. Jan. 21.2016 4 of 4 EFTA00589876 [DI R01 Mandatory Code Related Code Code Description Included In Material Estimate 12 Month CMP Tasks (Exhibit 1) 237004 Cockpit Voice Recorder System - Operational Test 240250 Emergency Securaplane Battery No. 1 - BITE / Battery Level Test 240251 Emergency Securaplane Battery No. 2 - BITE / Battery Level Test 240252 Emergency Securaplane Battery No. 3 - BITE / Battery Level Test 240253 Emergency Securaplane Battery No. 4 - BITE / Battery Level Test 250001• ICA for LCD Monitor 250002• ICA for 406MHZ ELT 256110 Emergency Locator Transmitter - Operational Test (FAR 91.207) 256105 Emergency Locator Transmitter - Removal / Installation 256269 LIFE VESTS-INTEG. CHECK 262582 EXT. H2O AFT CABIN-INSPECT 262621 Portable Halon Fire Extinguisher (Right Cockpit) - Weight Cheek 262601 Portable Halon Fire Extinguisher (Right Cockpit) - Removal / Installation 262622 Portable Halon Fire Extinguisher (Forward Cabin) - Weight Cheek 262612 Portable Halon Fire Extinguisher (Forward Cabin) - Removal / Installation 262623 Portable Halon Fire Extinguisher (Aft Cabin) - Weight Check 262603 Portable Halon Fire Extinguisher (Alt Cabin) - Removal / Installation 262633 Portable Halon Fire Extinguisher (Alt Cabin) - Inspection 270011 Control Surface Hinge Joints - Lubrication 271029 Aileron Actuator Load Relief Bungee (Left) - Inspection 271039 Aileron Actuator Load Relief Bungee (Right) - Inspection 273056 Elevator Actuator Load Relief Bungee - Inspection 312015 Pilot Clock Battery - Replacement 312016 Copilot Clock Battery - Replacement 322042 Nose Gear Axle Assembly - Corrosion Prevention 320027 Nose Landing Gear Axle Assembly - Corrosion Inhibiting Compound Application 322035 Nose Gear Axle Fitting - Removal / Installation 324009 Nose Gear Wheel Assembly (Lett) - Removal / Installation 324049 Nose Gear Wheel Bearings (Left) - Inspection / Pack 324010 Nose Gear Wheel Assembly (Right) - Removal / Installation 324050 Nose Gear Wheel Bearings (Right) - Inspection / Pack 330007 Emergency Exit Lights - Operational Test 330010 Exterior Lights - Operational Test 344095 IRU No. 1 Securaplane Battery - BITE / Battery Level Test 344096 IRU No. 2 Securaplane Battery - BITE / Battery Level Test 344097 IRU No. 3 Securaplane Battery - BITE / Battery Level Test 351005 Crew Oxygen System (Pilot) - Operational Test 351006 Crew Oxygen System (Copilot) - Operational Test 351007 Crew Oxygen System (Observer) - Operational Test 521003 Main Entrance Door - Lubrication 521008 Main Entrance Door Inflatable Seal System - Operational Test 521009 Baggage Door Inflatable Seal System - Operational Test 521080 Inflatable Door Seal - Purging Procedure 523004 Baggage Door - Lubrication 534015 Main Landing Gear Installation (Left) - Inspection 534016 Main Landing Gear Installation (Right) - Inspection 534018 Main Landing Gear Wheel Well Compartment - Inspection 534020 Nose Wheel Well and Gear - Inspection 571030 Wing Vertical Breather Angle - Inspection 710019 LH Powerplant Internal - Inspection 711009 Cowl Latch. Engine (Lett) - Rigging 710019 (710020) RH Powerplant Internal - Inspection 711010 Cowl Latch. Engine (Right) - Rigging 24 Month CMP Tasks (Exhibit 2) 212077 Air Conditioning Shutoff Valve Filter (Left) - Inspection 212061 Air Conditioning Shut-ott Valve Filter (Left) - Removal / Installation 212078 Air Conditioning Shutoff Valve Filter (Right) - Inspection 212062 Air Conditioning Shut-ott Valve Filter (Right) - Removal / Installation 212115 Nose Compartment Cooling System - Operational Test 213053 Cabin Pressure Warning Indication System - Functional Test 213081 Pressurization Safety Valve - Inspection 213080 Cabin Pressurization Safety Valve - Removal / Installation 213083 Pressurization Safety Valve - Ground Test 213052 Cabin Pressure Waming Snitch - Removal / Installation 213085 Pressurization System - Operational Test Page 1 ol 6 EFTA00589877 IDN R01 Mandatory Code Related Code Code Description Included in Material Estimate 213090 Cabin Pressure Controller (Manual Mode) - Operational Test 216097 Air Cycle Machine Compressor Outlet Overheat Switch (Left) - Trip Point Check 216095 Air Cycle Machine Compressor Outlet Overheat Switch (Left) - Removal / Installation 216098 Air Cycle Machine Compressor Outlet Overheat Switch (Right) - Trip Point Check 216096 Air Cycle Machine Compressor Outlet Overheat Switch (Right) - Removal / Installation 236010 Static Discharger Wick (Left Wing) - Resistance Check 236011 Static Discharger Wick (Right Wing) - Resistance Check 236014 Static Discharger Wick (Left Horizontal Stabilizer) - Resistance Cheek 236015 Static Discharger Wick (Right Horizontal Stabilizer) - Resistance Check 236016 Static Discharger Wick (Vertical Stabilizer) - Resistance Check 236020 Static Discharger Wick (Tail Cone) - Resistance Check 237041 CVR Underwater Locator Beacon (DK100 / DK120) - Operational Test 237047 CVR Underwater Locator Beacon - Battery Voltage Check (DK100 / DK120) 237005 CVR Unit - Removal / installation 237025 CVR Underwater Locator Beacon - Replacement (0K100) 237048 CVR Underwater Locator Beacon - Switch Cleaning (DK100 / DK120) 243030 Auxiliary TRU - Inspection / Cleaning 243189 Battery Circulating Fan - Operational Test 251125 Crew Seat Inertia Reels - Operational Test 256112 WELT Registration (NO.2 RAFT) 261035 Engine Alternator Overheat Switch (Left) - Trip Point Cheek 261025 Engine Alternator Overheat Switch (Left) - Removal / Installation 261036 Engine Alternator Overheat Switch (Right) -Trip Point Check 261030 Engine Alternator Overheat Switch (Right) - Removal / Installation 261065 Combined Hydraulic System Overheat Switch - Trip Point Check 261055 Combined Hydraulic System Overheat Switch - Removal / Installation 261066 Flight Hydraulic System Overheat Switch - Trip Point Cheek 261060 Flight Hydraulic System Overheat Switch - Removal / Installation 261235 Bleed Air Manifold Overheat Switch (Left) - Trip Point Check 261225 Bleed Air Manilold Overheat Switch (Left) - Removal / Installation 261236 Bleed Air Manifold Overheat Switch (Right) - Trip Point Check 261230 Bleed Air Manifold Overheat Switch (Right) - Removal / Installation 261440 APU Overheat Switch - Trip Point Check 261415 APU Fire Detection Switch (Top) - Removal / Installation 261420 APU Fire Detection Switch (Bottom) - Removal / Installation 261425 APU Fire Detection Switch (Above Alternator) - Removal / Installation 261430 APU Fire Detection Switcli AN Inlet) - Removal / Installation 262075 Fire Bottle (APU) - Weight Cheek 262035 APU Fire Bottle - Removal / Installation 262155 Fire Pull Handle - Operational Test 262165 Fire Extinguisher System (Left) - Functional Test 262166 Fire Extinguisher System (Right) - Functional Test 262170 Fire Extinguisher System (APU) - Functional Test 270006 Shutoff Valve. Flight Control Manual - Operational Test 276001 Ground Spoiler System - Operational Test 276004 Ground Spoiler Fault Detection System - Functional Test 282073 APU Wing Fuel Shut-off Valve - Functional Test 301005 Wing Anti-Ice (Left) - Operational Test 301006 Wing Anti-Ice (Right) - Operational Test 302005 Cowl Anti-Ice (Left Engine) - Operational Test 302006 Cowl Anti-Ice (Right Engine) - Operational Test 303009 Total Temperature Probe Heat System - Operational Test 303012 Angle of Attack Heat - Operational Test 320009 Landing Gear (Left Main) Corrosion Inhibiting Compound Reapplication 320010 Landing Gear (Right Main) Corrosion Inhibiting Compound Reapplication 320034 Nose Landing Gear Corrosion Inhibiting Compound Reapplication 321041 Main Gear Shock Absorber (Left) - Service 321042 Main Gear Shock Absorber (Right) - Service 322006 Nose Gear Shock Strut - Friction Check 322028 Nose Gear Shock Strut - Service 322433 Nose Landing Gear Spring Rod Assembly - Lubrication 322430 Nose Landing Gear Spring Rod Assembly - Removal / Installation 323003 Nose Landing Gear Sequencing Linkage - Check / Adjustment 323002 Landing Gear Cycling - Operational Check 322434 Main Landing Gear Bungee (Left) - Lubrication 322431 Main Landing Gear Bungee (Loll) - Removal / Installation 322435 Main Landing Gear Bungee (Right) - Lubrication 322432 Main Landing Gear Bungee (Right) - Removal / Installation Page 2 of 6 EFTA00589878 ID# R01 Mandatory Code Related Code Code Description Included in Material Estimate 323001 Landing Gear - Normal - Functional Test 291057 Combined / Flight Hydraulic System Reservoir - Filling Procedures 323004 Landing Gear - Emergency - Functional Test 323115 Bottle. Landing Gear Air - Service 323025 Main Gear Side Brace Fitting Pin (Left) - Inspection 323015 Side Brace Actuator (Left) - Removal / Installation 323026 Main Gear Side Brace Fitting Pin (Right) - Inspection 323016 Side Brace Actuator (Right) - Removal! Installation 324101 Wheel Brake - Functional Test (Brake-by-wire) 341052 Total Air Temperature Probe Aspirator - Operational Test 342037 Compass Swing No. 1 342038 Compass Swing No. 2 346031 FMS Navigation Computer No. 1 - Battery Pack Replacement X 346015 FMS Navigation Computer No. 1 - Removal! Installation 349800 Flight Management System No. t - Operational Check 346032 FMS Navigation Computer No. 2 - Battery Pack Replacement X 346016 FMS Navigation Computer No. 2 - Removal! Installation 346033 FMS Navigation Computer No. 3 - Battery Pack Replacement X 346017 FMS Navigation Computer No. 3 - Removal! Installation 352005 Passenger Oxygen System - Operational Test 362005 Bleed Air Manifold Pressure Indication - Functional Test 510070 24 Month Honeycomb (Aluminum Panels Only) - Inspection / Bond Test 521007 Main Entrance Door Internal - Detailed Inspection 521002 Main Entrance Door Cable Tension - Check 521024 Main Entrance Door Hinge Pins - Detailed Inspection 521022 Main Entrance Door Hinge Pins - Removal / Installation 521051 Door Seal Pressure Regulator - Functional Test 527005 Main Entrance Door Warning System - Operational Test 527008 Baggage Door Warning System - Operational Test 527012 Tail Compartment Door Warning System Operational Test - 532005 Cabin Compartment Above floor - Inspection 532017 Cockpit Compartment Above floor - Inspection 532019 Cockpit Compartment Below Floor - Inspection 251109 Pilot Seat - Removal / Installation 251110 CoPilot Seat - Removal! Installation 532021 Cockpit Compartment Below Pedestal - Inspection 532027 Entrance Compartment Behind Panel - Inspection 532029 Entrance Compartment Above Floor - Inspection 532031 Entrance Compartment Below Floor - Inspection 532033 Entrance Compartment Shelf - Inspection 532041 Baggage Compartment Above Floor - Inspection 523001 Baggage Door - Removal! Installalion 532045 Baggage Compartment Behind Panel - Inspection 532050 Engine / APU Fuel Feed Line - Inspection 532052 Torque Box - Inspection 532055 Fuselage Interior I Wing Attach - Inspection 532067 Tail Compartment Above Floor - Inspection 532069 Tail Compartment Below Floor - Inspection 272001 Rudder Control System - Operational Test 272019 Rudder Cable Assembly FS 470 - FS 760 (Right) - Removal /Installation 272020 Rudder Cable Assembly FS 470 - FS 760 (Left) - Removal / Installation 273001 Elevator Control System - Operational Test 273033 Elevator Cable Assembly FS 470 - FS 740 (Left) - Removal / Installation 273034 Elevator Cable Assembly FS 470 - FS 740 (Right) - Removal /Installation 532070 Shear Clips Aft Fuselage - Inspection 533005 Exterior Fuselage - Inspection 535008 Nose Compartment / Radome Interior - Inspection 535012 Tail Cone interior - Inspection 535004 Tailcone - Removal / Installation 562005 Emergency Window Release Mechanism (Internal and External) - Functional Test 562007 Emergency Exil and Cabin Windows - Leak Check 571064 Wing to Fuselage Attachments (Left) - Ultrasonic and Visual Corrosion Damage Tolerance 571065 Wing to Fuselage Attachments (Right) - Ultrasonic and Visual Corrosion Damage Tolerance 783005 Engine Thrust Reverser (Left) - Inspection 783006 Engine Thrust Reverser (Right) - Inspection 783009 Engine Thrust Reverser (Left) - Operational Test 783010 Engine Thrust Reverser (Right) - Operational Test Page 3 of 6 EFTA00589879 IDN R01 Mandatory Code Related Code Code Description Included In Material Estimate 36 Month CMP Tasks (Exhibit 3) 245051 AC / DC Power Distribution System - Functional Test 270101 Stall Barrier / Angle of Attack System - Operational Test 270221 Stall Barrier Dump Valve - Operational Test 272038 Rudder Pedals - Lubrication 275009 Flap Actuator Yoke (Left Inboard) - Inspection 275003 Flap (Loll) - Removal! Installation 275010 Flap Actuator Yoke (Right Inboard) - Inspection 275004 Flap (Right) - Removal! Installation 275011 Flap Actuator Yoke (Left Outboard) - inspection 275012 Flap Actuator Yoke (Right Outboard) - Inspection 275027 Flap Actuator Bushing (Left) - Service! Lubrication 275005 Inboard Flap Actuator (Lelt) - Removal / Installation 275007 Outboard Flap Actuator (Lelt) - Removal / Installation 275028 Flap Actuator Bushing (Right)- Service / Lubrication 275006 Inboard Flap Actuator (Right) - Removal / Installation 275008 Outboard Flap Actuator (Right) - Removal / Installation 280005 Fuel Control System - Functional Test 532007 Forward Cabin Compartment Below Floor - Inspection 532009 Midcabin Compartment Below Floor - Inspection 551019 Elevator Skins (Left) - General Visual inspection 551020 Elevator Skins (Right) - General Visual Inspection 551023 Horizontal Stabilizer / Elevator (Interior! Exterior) (Left) - Inspection 551024 Horizontal Stabilizer / Elevator (Interior! Exterior) (Right) - Inspection 553005 Vertical Stabilizer! Rudder (External) - Inspection 553007 Vertical Stabilizer! Rudder (Internal) - Inspection 571011 Wing Front Beam HI-Lite Collars (Left)- Inspection 261169 Wing Anti-ice Overlemp Switch (Left) - Trip Point Check 574005 Wing Leading Edge (Leif inboard) - Removal / Installation 574011 Wing Leading Edge (Leif Center) - Removal / Installation 574017 Wing Leading Edge (Leif Outboard) - Removal / installation 571012 Wing Front Beam MI-Lite Collars (Right) - Inspection 261170 Wing Anti-ice Overleap Switch (Right) - Trip Point Check 574006 Wing Leading Edge (Right Inboard) - Removal / Installation 574012 Wing Leading Edge (Right Center) - Removal / Installation 574018 Wing Leading Edge (Right Outboard) - Removal / Installation 571025 Wing Tank Interior (Left) - Inspection 280010 Delueling Procedures 280018 Fuel Tank (Left) - Leak Check 282025 Fuel Pickup Screen (Main Leif Wing) - Inspection 282026 Fuel Pickup Screen (Alternate Left Wing) - Inspection 571003 Wing Fasteners - Cadmium Plating Degradation - Check (Left) 571026 Wing Tank Interior (Right) - Inspection 280019 Fuel Tank (Right) - Leak Check 282027 Fuel Pickup Screen (Main Right Wing) - Inspection 282028 Fuel Pickup Screen (Alternate Right Wing) - inspection 571004 Wing Fasteners . Cadmium Plating Degradation - Check (Right) 150 Hour CMP Tasks (Exhibit 4) 200001' Operation One 276065 Takeoff Alarm System - Functional Test 999005 AD 90.02-05 Takeoll Alarm ISM 1000 - 1092) 554007 Rudder External - Inspection 710021 Engine External (Left) - Inspection 710022 Engine External (Right) - Inspection 730001 Fuel Contamination Check, Engine - Inspection 730001 (730002) Fuel Contamination Check, Engine - Inspection 742001 Engine Ignition System - Operational Check 742001 (742002) Engine Ignition System - Operational Check 792007 Filter, Engine Pressure Oil - Cleaning / Inspection 791033 LH Engine Oil Level - Check / Service (Using Onboard Replenishment System) 792007 (792009) Filter, Engine Pressure Oil - Cleaning / Inspection 791033 (791034) RH Engine Oil Level - Check / Service (Using Onboard Replenishment System) Page 4 of 6 EFTA00589880 IDS R0t Mandatory Code Related Code Code Description Included in Material Estimate 150 Cycle CMP Tasks (Exhibit 5) 200002' Operations Two ( 150 Cycle ) 270206 Stall Barrier Actuator - Service! Lubrication 271035 Spoiler Load Relief Bungee, Left - Lubrication 271036 Spoiler Load Relief Bungee, Right - Lubrication 271037 Bungee, Left Aileron Load Relief - Lubrication 271038 Bungee, Right Aileron Load Relief - Lubrication 272027 Rudder Bungee - Lubrication 272036 Rudder Torque Tube Bearing - Lubrication 273002 Elevator Load Relief Bungee - Lubrication 275019 Wing Flap (Left) - Lubrication 275020 Wing Flap (Right) - Lubrication 275023 Wing Flap Traveling Nut (Left) - Lubrication 275024 Wing Flap Traveling Nut (Right) - Lubrication Misc CMP Tasks (Exhibit 6) 213051 Pressure Relay Switch - Screen Inspection 215006 Air Conditioning System (Temperature Control Valves) - Functional Check 215005 Air Conditioning System - Operational Test 217027 Ozone Converter (Left) - Functional Test X 217025 Ozone Convener (Left) - Removal r Installation 217028 Ozone Converter (Right) - Functional Test X 217026 Ozone Converter (Right) - Removal! Installation 217075 Water Separator Bag (Left) - Inspection X 217070 Water Separator (Leh) - Removal / Installation 217076 Water Separator Bag (Right) - inspection X 217071 Water Separator (Right) - Removal / Installation 240108 Standby Power System - Operational Test 243105 Battery, S1—Capacity Check 243106 Battery. #2—Capacity Check 262631 Portable Haien Fire Extinguisher (Right Cockpit) - Inspection 262632 Portable Haien Fire Extinguisher (Forward Cabin) - inspection 262691 EXT,AFT GALLEY HALON TRASH-WT 273019 Elevator Trim Tab Actuator (Left) - Lubrication 273020 Elevator Trim Tab Actuator (Right) - Lubrication 304003 Windshield Wiper Lock Pin - Lubrication / Adjustment 314007 FWC No. 1 Trend and Limit Monitoring - Data Download 314008 FWC No. 2 Trend and Limit Monitoring - Data Download 320004 Main Landing Gear (Left) - Lubrication 320005 Main Landing Gear (Right) - Lubrication 320006 Nose Gear - Lubrication 344051 IRU No. 1 Blower Filter - Inspection 344005 Inertial Reference Unit No. 1 - Removal / Installation 344086 AHRS / IRU - Operational Check 344052 IRU No. 2 Blower Filter - Inspection 344006 Inertial Reference Unil No. 2 - Removal / Installation 344055 IRU No. 3 Blower Filter - Inspection 344010 Inertial Relevance Unil No. 3 - Removal / Installation 344088 IRU No. 1 Securaplane Battery! Heater Assembly - Replacement X 344068 IRU No. 1 Securaplane Battery - Removal / Installation 344061 IRU No. 1 URDC Battery - Removal / Installation 344089 IRU No. 2 Securaplane Battery! Heater Assembly - Replacement X 344069 IRU No. 2 Securaplane Battery - Removal / Installation 344062 IRU No. 2 URDC Battery - Removal / Installation 350122 Oxygen Bottle (No. 2) - Hydrostatic Test X 350102 Oxygen Cylinder (No. 2) - Removal / Installation 351001 Crew Oxygen Low-Pressure Switch - Operational Test 350123 Oxygen Bottle (No. 3) - Hydrostatic Test X 350103 Oxygen Cylinder (No. 3) - Removal / Installation 350124 Oxygen Bottle (No. 4) - Hydrostatic Test X 350104 Oxygen Cylinder (No. 4) - Removal / Installation 381010 Filter Element, No. 1 Potable Water System - Removal / Installation 381025 Potable Water System - Flush! Sanitize 539472 Aft Pressure Bulkhead - Inspection 541017 Pylon External/Internal (Left) - Inspection 541018 Pylon External/ Internal (Right) - Inspection Page 5 of 6 EFTA00589881 IDA RO1 Mandatory Code Related Code Code Description Included In Material Estimate 541019 Pylon Internal (Left) - Inspection 541020 Pylon Internal (Right) - Inspection 571033 Rib. Wing Sponson (Left) - Inspection 571034 Rib, Wing Sponson (Right) - Inspection 576005 Aileron Interior (Left) - Inspection 576006 Aileron Interior (Right) - Inspection 723001 LH Intermediate Compressor Case. Engine - Inspection 723001 (723002) RH Intermediate Compressor Case, Engine - Inspection 761001 LH Controls. Engine - Operational Test 761001 (761002) RH Controls, Engine - Operational Test 761005 LH Controls. Engine - Service! Lubrication 761005 (761006) RH Controls, Engine - Service / Lubrication 783007 Engine Thrust Reverser Hot Short To Ground (Left) - Inspection 346025 FMS COU No. 1 - Removal/ Installation 783008 Engine Thrust Reverser Hot Short To Ground (Right) - Inspection 801011 Engine Starter Oil Level (Left) - Check 801012 Engine Starter Oil Level (Right) - Check 994019 AD 2015-16-04 Kidde Graviner Page 6 ol 6 EFTA00589882