EFTA01105727.pdf

A OCNIMAL OVNAMNCC COMPANY 1 February 2013 Mr. Larry Visoski JEGE, LLC 3800 Southern Blvd suite 204 West Palm beach, FL 33406 Office: 561-328-7963 Dear Mr. Visoski, In response to your request, Gulfstream is pleased to provide the following Service Center proposal for maintenance to be accomplished on Gulfstream GIV-SP aircraft. After review of this proposal and its attachments (if applicable), should you have any questions, concerns, or scheduling requests, please feel free to contact me, so we can coordinate a mutually agreeable input date for your aircraft. Furthermore, if this proposal with its attachments and Terms and Conditions is acceptable to you, please sign and return the Summary page to or Thank you for considering Gulfstream for the proposed workscope on your aircraft. Please do not hesitate to call me with any questions or for additional information. Sincerely, 6' Tom Baliya National Sales Mana er Office: Mobile: Fax: WPUdlh EFTA01105727 Gulfstream® A GUN DYNAMICS COMPANY GAC02 I3-047-CIV-SP.OCS-R00 I February 2013 Gulfstream GIV-SP MGR. LIC WORKSCGPE 1. Aircraft/Records and Condition Survey (Exhibit 1) Labor and Materials $23,000.00 Description: The Aircraft Records and Condition Survey includes Records / Logbook Research and Pre-buy Inspection Schedule of Events I. Review workscope and identify points of contact with both buyer and seller present and have both parties sign the Hold Harmless Agreement. 2. 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. 3. 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. 4. 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. 5. All parties involved, based on the Service Center workload, at that time will mutually agree to the downtime schedule for the authorized work. The Aircraft/Records Survey includes the followine: 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 crass-checked against STC's. 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 2 of 8 This proposal is confidential between Gulfstream and the customer. EFTA01105728 Gulfstream® A clatuenAt DYNAMICS COMPANY GAC02I3-047-CIV-SP.OCS-R00 I February 2013 Gulfsbeam GIV-SP MGR. LLC The Condition Survey includes the following: Functional Test of Avionics Equipment: An avionics ramp check is performed and involves powering up all major avionics equipment and functionally testing navigation, communication and flight management systems for proper operation. 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. They will be identified as information items or items required for return to service and will be performed at Time and Material. 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 thorough physical 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. This above floor inspection does not include operational testing of components or equipment. Corrections and repairs to discrepant conditions found will be accomplished as time and materials. Interior access will not be required or included for this general visual inspection. Aircraft Records and Condition Survey Report: The report is a bound document and is divided into fourteen (14) 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 (I) copy of the discrepancies noted to the owner (additional report copies are available at SI 50.00/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. Ootional 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. 2. Option: Auxiliary Power Unit Borescope (Exhibit 2) Labor $900.00 Task: Perform APU Borescopes. Page 3 of 8 This proposal is confidential between Gulfstream and the customer. EFTA01105729 Gulfstream® A OlINERAL DYNAMICS COMPANY GAC02 I3-047-GIV-SP.OCS-R00 I February 2013 Gulfslream GIV-SP MGR. LIC 3. Option: Engine Runs and Borescopes (Exhibit 3) Labor $13,000.00 Task: Perform Engine Runs and Borescopes. 4. Option: Landing Gear Corrosion Inspection (Exhibit 4 Dunlop /Exhibit 5 ABS) Labor $25,500.00 Task Landing Gear Corrosion Inspection (Exhibit 4 Dunlop /Exhibit 5 ABS) Note: For budretary planning purposes, estimated material and outside services for the above quoted CMP package is approximately $500.00 and it does not include material required for clearing of any discrepancies. 5. Option: Two Pilots' for Condition Survey Flight (Must be performed with Engine Runs and Borescopes) Labor $5,500.00 Condition Survey Flight • Two (2) Pilots' for Condition Survey Flight (Based on an 8 hour day). • Engine runs and borescopes will be required prior to performing a Gulfstream Condition Survey Flight and is not included with this option. • The Engine runs and borescope Option must be selected / performed prior to the Condition Survey Flight: • The flight test card will be identical to the one used by our own Gulfstream Flight Department to evaluate pre-owned aircraft that are being considered for purchase by Gulfstream. • This is an extensive flight test regimen flown by Gulfstream test pilots (at an additional expense). • Test flight results are fully documented and reported in work order and Survey Report. The optional Flight Test may affect downtime. • All pilot's fees and travel expenses will be the responsibility of the customer per the Gulfstream labor rate letter and is not included in this proposal. Note: Fuel will be billed on actuals. AIRFRAME CONTINGENCIES This proposal does not include correction/clearing of any discrepancies and/or corrosion that may be found, outside services. additional due items (i.e. customer requirements. completion/outfitter requirements. Pan 135 "for hire" requirements. etc.). and/or consumables. These issues will be addressed separately from this proposal with the customer and may impact scheduled downtime. Any revision(s) to Chapter 5/Maintenance Schedule issued prior to aircraft arrival may affect the inspection price. Should additional work be required. it will be accomplished on a time and material basis, unless otherwise noted. For aircraft with standard paint schemes (one (I) base color and two (2) stripes), the sealing and touch-up (by brush) of panels will be considered part of the inspection hours for that task. Aircraft with non-standard paint schemes will be charged for the additional time required to complete the paint touch-up. Time required to seal and touch-up sealant for discrepancies on items not open for inspection being performed during this visit will be billed at time and material. Page 4 of 8 This proposal is confidential between Gulfstream and the customer. EFTA01105730 Gulfstream® A GENERAL DYNAMICS COMPANY GAC02 I3-047-GIV-SP.OCS-R00 I February 2013 Gulfstream GIV-SP MGR. LLC REMITTANCE INSTRUCTIONS Checks: Gulfstream Aerospace Corporation (Overnight) Gulfstream Aerospace Corporation (Box #730349) P.O. Box 730349 do JP Morgan Chase Bank. NA Dallas, TX 75373-0349 Ann: Dallas National Wholesale Lockbox TX1-0029 14800 Frye Road Ft. Worth, TX 76155 Wire Transfer Gulfstream Aerospace Corporation Instructions: JP Morgan Chase Bank. NA I Bank One Plaza Chicago. IL 60670 Account No- Reference your Five (5) Digit Customer Number (XX-XXX) Bank Fedwire Routin No. Identifiers: S.W.I.F.T ACH Credit Routing No. Note: Please reference one of the following (as applicable): • Invoice No. • Sales Order No. • Job or Work Order No. • Aircraft Serial or Tail No. • Contact Name • Customer Account No. (XX-XXXX) TERMS AND CONDITIONS Gulfstream Aerospace Corporation requires the estimated amount be paid in full for AircrafURecords and Condition Survey prior to aircraft induction to Service Center. All Aircraft/Records and Condition Survey related discrepancies must be paid in full prior to aircraft departure. All prices stated herein are exclusive of freight. fuel, flight costs. and / or environmental fees. Additionally, 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. This proposal is not valid at Gulfstream's Luton United Kingdom facility. Work items not quoted in this proposal will be billed on a time and material basis per our published labor rates at the time of aircraft induction for Maintenance. Electrical. Avionics. Refurbishment. and Engine/APU Maintenance. For time and materials work: (a) labor (including engineering services) is billed according to the rates set forth in the Gulfstream Labor Rate Letter in effect as of the date the work is performed: and (b) materials are billed according to Gulfstreant'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. This proposal is contingent on all work being accomplished during the same timeframe. unless otherwise noted. The quoted prices are valid for a period of thirty (30) days of receipt of proposal. unless otherwise noted. Gulfstream recommends a firm schedule be established and work be completed within the next three (3) to six (6) months from the date of this proposal. Any change in workscope and/or schedule may require review by Gulfstream and requires revision of this proposal. Gulfstream reserves the right to pass on price increases to the customer. The Customer is responsible for making certain that all specific preservation tasks related to the Aircraft, its engines or systems. that are required or may become required while the Aircraft is at Gulfstream's facility for the Workscope be indentified on the Work Authorization squawk list. Page 5 of 8 This proposal is confidential between Gulfstream and the customer. EFTA01105731 Gulfstream' A casomanAL DYNAMICS COMPANY GACO2 I3-047-CIV-SP.00S-R00 I February 2013 Gulfstream GIV-SP MGR. LLC TERMS AND CONDITIONS (continued) Gulfstream warrants that the work conforms to the pertinent specifications prescribed by the applicable aircraft I 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 exists on the date this agreement is executed. Proposal pricing and schedules are contingent upon the customer supplying the existing avionics, electrical, and aircraft system prints, drawings and diagrams. which accurately represent the current condition of the aircraft. Any changes from the existing drawings will be performed on a time and material basis with customer approval. Any relocations of existing equipment required due to space limitations will be performed at time and materials until a firm proposal can be prepared. Detailed parameters of this proposal may require modifications following an in-depth physical inspection. Materials used during the clearing/correction of discrepancies and/or items based on time and material will be quoted and/or invoiced on an "As Required" basis. There will be a 3.5% charge for consumables. to a maximum of 54.000.00. 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 a "Road Trip Invoice" will be exempt from this charge. Customer furnished parts and drop shipments will be subject to a handling fee of 15% based on current manufacturer list price. 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. If enrolled in Gulfstreant's PlanePartsni program. certain components supplied in regard to this proposal will be at no charge to the Customer. To enroll or learn more about the program. please visit http://www.gulfstream.com/product support/planeparts/. Any estimates given for outside services are not intended to be exact figures. Repair. calibration, overhaul. and/or exchange pricing will be billed as accrued. be it either less than or more than quoted. Changes to the 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. it will be quoted separately or performed on a time and materials basis. Any changes to the Minimum Equipment List (MEL) are the Customer's responsibility and are not included herein. All exchange parts prices are subject to our vendor acceptance of exchange core. Should exchange core be rejected or subjected to an extra charge by Vendor at any time for reasons of abnormal wear and tear, damage. unauthorized modifications. or other discrepancies. the customer agrees to reimburse Gulfstream for resultant extra costs. Any existing unused wiring will be capped and stowed. Wiring removal (if requested/required) will be handled on a time and material basis and billed additional to the proposed amount. All removed equipment will be retained by Gulfstream. unless otherwise noted. Interior access will be performed on a time and material basis. unless otherwise noted within this proposal. When aircraft is firmly scheduled into a Gulfstream facility, preliminary engineering and planning commences. and materials / components are ordered for the workscope. If the workscope is canceled. the customer will be charged for any labor expended and/or any restock charges incurred on materials I components ordered. If materials / components cannot be returned to vendor(s), customer will be billed in full for these items. In such case, the materials I components would become the property of the customer. If the workscope is rescheduled for a later arrival. these charges will be applied to the rescheduled visit. Page 6 of 8 This proposal is confidential between Gulfstream and the customer. EFTA01105732 Gulfstream® A caloganAL DYNAMICS COMPANY GAC02I3-047-31V-SP.OCS-R00 I February 2013 GulfsIream GIV-SP JEGE. LLC TERMS AND CONDITIONS (continued) Working days are defined as Monday through Friday. Should additional work be required. other than that quoted herein. the estimated downtime may require extension. This proposal does not include overtime. Any overtime required will be approved by the customer prior to work commencing. All non-scheduled NDT will be on an overtime basis due to NDT planned scheduling. Customer's oral changes increasing the scope of the Work or approving overtime are binding (unless otherwise provided by law). International Contingencies Of Applicable; Foreign Registered Aircraft Only with Domestic Input): Foreign Operators Civil Air Authority (FOCAA). FAA. or concurrence of both agencies must first approve this STC Project prior to start of aircraft modification. Any cost involved in this approval process will be charged as time and materials. Upon customer's acceptance of this proposal. Gulfstream will submit an "Undue Burden" Project Request or FOCA certification fees to the FAA ACO or FOCAA as applicable. Once the FAA and/or FOCA approves the "Undue Burden" Project Request or FOCA certification fees. the ACO will notify the Foreign Civil Air Authority (FCAA). Once the FAA ACO receives concurrence from the FCAA. the ACO will notify Gulfstream. Gulfstream will submit Application (8110-12). Cert. Plan and an LOI to the FAA ACO and/or FOCA. Please note (if applicable), the time estimated to accomplish these steps is approximately three (3) to six (6) months depending on resource availability of the FAA and/or FOCA. 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. Quoting Contact: Dan Hyde, Mechanical Quotin Mana er Tele: email: Page 7 of 8 This proposal is confidential between Gulfstream and the customer. EFTA01105733 Gulfstreams A ousenAL DYNAMICS COMPANY GAC0213-047-CIV-SP.OCS-R00 I February 2013 Gulfsiream GIV-SP JEGE. LLC PROPOSAL SUMMARY • Please initial items in Accept/Decline columns. (Please note that quoted dollars and downtime may vary based on concurrent work with accepted/declined items.) Item Workscope Amount Accept Decline 1. Aircraft Records and Condition Survey $23,000.00 2. Option: Auxiliary Power Unit Borescope $900.00 3. Option: Engine Runs and Borescopes $13,000.00 4. Option: Landing Gear Corrosion Inspection $25,500.00 5. Option: Two (2) Pilot's for Condition Survey Flight (Must be $5,500.00 Performed with Engine Runs and Borescopes) TOTAL WITH OPTIONS $67,900.00 ♦ 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 seller's warranty, if any, as to the aircraft's condition. ♦ Downtime required for this workscope will be eleven (11) working days. This downtime estimate is subject to any discrepancies that may be found. ♦ Leadtime required for this workscope will be five (5) calendar days after proposal acceptance and is subject to equipment availability. ♦ This proposal (or estimate) expressly incorporates and is subject to Gulfstream Aerospace Corporation's standard work authorization Terms and Conditions. Your acceptance of all or any portion of this proposal (or estimate) confirms our agreement to accept those standard Terms and Conditions. (Please sign and return this page to .) Proposal Acceptance Signature Date This proposal summary does not include items based on lime and material, discrepancies or corrosion found or other materials required. handling fees, or other additional expenses outside the specified workscope of the enclosed proposal. Page 8 of 8 This proposal is confidential between Gulfstream and the customer. EFTA01105734  GIV Aircraft / Records and Condition Survey (Exhibit 1) NON-MSG3 Aircraft RFQ # GAC0213-047-GIV-SP.OCS-R00 CMP Primary Code Description 100310 CK AIRWORTHINESS DIRECTIVES 100320 CK SERVICE BULLETINS 134401 CM AVIONICS INVENTORY 191108 REVIEW A/C STATUS AND RECORDS 231001 AVIONICS--FUNC RAMP TEST 291030 Combined Hyd Sys DPI (Eng-driven Pump Bypass) - Inspection 291031 Flight Hyd Sys DPI (Eng-driven Pump Bypass) - Inspection 291032 Combined Hyd Sys DPI (Main Pressure) - Inspection 291033 Flight Hyd Sys DPI (Main Pressure) • Inspection 291034 Combined Hyd Sys DPI (Main Return) - Inspection 291035 Flight Hyd Sys DPI (Main Return) - Inspection 292020 Auxiliary System DPI (Pressure) • Inspection 292021 Auxiliary System DPI (Return) - Inspection 292024 Utility System DPI (Pressure) - Inspection 292025 Utility System DPI (Pump Bypass) - Inspection 330007 Emergency Exit Lights - Operational Test 330010 Exterior Lights - Operational Test 324108 Wheel Brake Lining - Wear Check (Brake-By-Wire) 324268 Brake Linings - Wear Check (HMAB / Dunlop) 351005 Crew Oxygen System (Pilot) • Operational Test 311006 Crew Oxygen System (Copilot) - Operational Test 521009 Baggage Door Inflatable Seal Sys - Ops Test 532005 Cabin Compartment Above Floor - Inspection 532017 Cockpit Compartment Above Floor - Inspection 532027 Entrance Compartment Behind Panel - Inspection 532041 Baggage Compartment Above Floor • Inspection 532067 Tail Compartment Above Floor - Inspection 533005 Exterior Fuselage - Inspection 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 535008 Nose Compartment / Radome Interior - Inspection 541017 Pylon External / Internal (Left) - Inspection 541018 Pylon External / Internal (Right) - Inspection 551019 Horizontal Stabilizer / Elevator (Exterior) (Left) • Inspection 551020 Horiz Stabilizer / Elevator (Exterior) (Right) • Inspection 553005 Vertical Stabilizer / Rudder (Exterior) - Inspection 554007 Rudder External - Inspection 571005 Wing Exterior (Left) - Inspection 571006 Wing Exterior (Right) - Inspection 490002 AUX POWER UNIT--OPS TEST GICP36-100 APU ONLY 490005 APU Enclosure - Inspection GICP36-100 APU ONLY 490052 APU - Operational Test GTCP36-150(G) ONLY 490053 APU Enclosure GTCP36.150(G) - Inspection GTCP36-150(G) ONLY Page 1 of 5 EFTA01105735  Auxiliary Power Unit Borescope (Exhibit 2) RFQ0 GAC0213.047-GIVSP.OCS-R00 CMP Primary Code Description 490000* APU GTCP 36-100 - Borescope 490000* APU GTCP 36-150 - Borescope Page 2 of 5 EFTA01105736  Option: Engine Runs and Boreseopes (Exhibit 3) RFQ* GAC0213-047-GIV-SP.OCS-R00 CMP Primary Code Description 710019 Powerplant Internal -Inspection 711009 Cowl Latch. Engine (Left) - Rigging (Related Code) 710025 Engine Borescope • Inspection 710031 Engine - Ops Test 732001 Engine Acceleration- Test Adjustment (Related Code) 732005 Engine Deceleration- Test! Adjustment (Related Code) 732079 Engine Handling (ACU) Solenoid - Ops Check (Related Code) 732057 Engine Approach Idle Solenoid - Ops Check (Related Code) 732011 Ground Idle. Engine - Test! Adjustment (Related Code) 732013 Approach Idle - Adjustment /Test (Related Code) 783013 T/Rev Interlock Feedback Sys (LH) - Ops Test (Related Code) 783014 T/Rev Interlock Feedback Sys (RH) - Ops Test (Related Code) 783017 Maximum Rev Thrust (LH) - Ops Test / Adjust (Related Code) 783018 Maximum Rev Thrust (RH) - Ops Test Adjustment 723001 Intermediate Compressor Case. Engine - Inspection 723002 Intermediate Compressor Case. Engine - Inspection 730001 Fuel Contamination Check. Engine • Inspection 742001 Engine Ignition System - Ops Check 742006 No. 2 Igniter Plug - Removal / Installation 742016 No. 2 Igniter Plug - Inspection 774955 Engine Chip Detector - Visual Check 792007 Filler. Engine Pressure Oil- Cleaning Inspection 791033 Eng Oil Level - Check (Service. Using Onbd Sys (Related Code) 792013 Engine Scavenge Strainers - Inspection 710020 Powerplant Internal - Inspection 711010 Cowl Latch. Engine (Right) - Rigging (Related Code) 710026 Engine Borescope • Inspection 710032 Engine - Ops Test 732(XX2 Engine Acceleration - Test! Adjustment (Related Code) 732006 Engine Deceleration- Test Adjustment (Related Code) 732050 Engine Handling (ACU) Solenoid - Ops Check (Related Code) 732058 Engine Approach Idle Solenoid - Ops Check (Related Code) 750006 Airflow Control System- Test (Related Code) 732012 Ground Idle. Engine - Test Adjustment 732014 Approach Idle - Adjustment (Test 730002 Fuel Contamination Check. Engine • Inspection 742002 Engine Ignition System - Ops Check 742008 No. 2 Igniter Plug - Removal / Installation 742018 No. 2 Igniter Plug - Inspection 774956 Engine Chip Detector - Visual Check 792009 Filter. Engine Pressure Oil - Cleaning!Inspection 791034 Eng Oil Level - Check / Service. Using Onbd Sys (Related Code) 792014 Engine Scavenge Strainers - Inspection Page 3 of 5 EFTA01105737  Landing Gear Corrosion Inspection (Exhibit 4) Dunlop WhetLs and Brakes RPQ # GACO213-047-GIV-SP.00S-R00 CMP Primary Code Description 320011 Nose Landing Gear and Components - Detailed Inspection 320006 Nose Landing Gear and Systems - Lubrication 320027 Nose Landing Gear Axle Assy - Corr Inhib Comp App 320028 Nose Landing Gear Shock Strut Assy - Corr Inhib Comp App 320030 Nose Landing Gear Truss Brace Assy - Corr Inhib Comp App 320031 Nose Landing Gear Upper Upper Tnum Attach Points - Corr Inhib Comp App 320032 Nose Landing Gear Upper Drag Brace Attach Pin - Corr Inhib Comp App 320033 Nose Landing Gear Striker Arms - Cow Inhib Comp App 322028 Nose Gear Shock Strut - Service 322036 Nose Gear Axle Fitting - Removal! Installation 323001 Landing Gear Normal - Functional Test 323004 Landing Gear Emergency Extension - Functional Test 324009 Nose Gear Wheel Assy (Left) - Removal / Installation 324010 Nose Gear Wheel Assy (Right) - Removal / Installation 325001 Nose Wheel Steering - Functional Test 325010 Nose Wheel Steering Unit - Removal l Installation 320013 Main Landing Gear and Components (Left) - Detailed Inspection 320004 NILG and Systems (Left) - Lubrication 320015 NILG Axle Fitting Attach Pin (Left) - Con Inhib Comp App 320017 MLG (Left) Axle Fitting - Corr Inhib Comp App 320019 MLG (Left) Shock Absorber - Corr Inhib Comp App 320021 MLG (Lt) Side Brace Act Attach Pins & Trunn Area - Cow Inhib Comp App 320023 MLG (Left) Uplock Roller - Corr Inhib Comp App 320025 MW (Left) Striker Ann - Corr Inhib Comp App 321015 NILG Spindle Pin (Leto- Removal / Installation 321031 NILG Shock Absorber (Left) - Removal / Installation 321075 Main Landing Gear Trunnion Pin (Left Aft) - Removal / Installation 323002 Landing Gear Cycling - Operational Check 323015 Actuator. Main Landing Gear Side Brace (Left) 324250 MLG Wheel Assy (L. Outboard No. I) - Rem / last (Dunlop) 324251 MLG Wheel Assy (L. Inboard No.2) - Rem /hist (Dunlop) 324220 MLG Wheel Bearing (L. Outboard No. I) - Inspection / Pack 324221 NILG Wheel Bearing (L. Inboard No.2) - Inspection / Pack 324260 Main Gear Brake (Leh. Outboard No.1) - Removal / Install 324261 Main Gear Brake (Left. Inboard No.1) - Removal / Install 324206 HydroMechanical Analog Brake Wear- Detailed Inspection 324207 Parking / Emergency Brake - Operational Test 320014 Main Landing Gear and Components (Right) - Detailed Inspection 320005 MLG and Systems (Right) - Lubrication 320016 MLG Axle Fitting Attach Pin (Right) - Corr Inhib Comp App 320018 MLG (Right) Axle Fitting -Corr Inhib Comp App 320020 MLG (Right) Shock Absorber - Corr Inhib Comp App 32w22 MLG (R) Side Brace Act Attach Pins & Trunn Area - Corr Inhib Comp App 320024 MLG (Right) Uplock Roller -Corr Inhib Comp App 320026 MLG (Right) Striker Ann - Corr Inhib Comp App 321016 MLG Spindle Pin (Right) - Removal / Installation 321032 MLG Shock Absorber (Right) - Removal / Installation 321076 Main Landing Gear Trunnion Pin (Right Aft) - Rem / Inst 323016 Actuator. Main Landing Gear Side Brace (Right) 324252 MLG Wheel Assy (R. Inboard No.3)- Rem / Inst (Dunlop) 324253 MLG Wheel Assy (R. Outboard No. 4)- Rem / Inst (Dunlop) 324222 MLG Wheel Bearing (R. Inboard No.3) - Inspection / Pack 324223 MLG Wheel Bearing (R. Outboard No. 4) - Inspection / Pack 324263 Main Gear Brake (R. Inboard No. 3) - Rem Inst (Dunlop) 324264 Main Gear Brake IR. Outboard No. 4)- Rem! Inst (Dunlop) Page 4 of 5 EFTA01105738  GIV Loading Gear Corrosion Inspection (Exhibit St ABS Wheels and Brakes CSIP Primary Code Description 321003 Main Landing Gear Components IL) • Detailed Corrosion Inspection 321005 nun Landing Gear (Left) Lubmation 321221 Main Landing Gear CIC Reapplication (Left) 321228 MI.G Axle Pitting Attach Pin (Left) CIC Application 321235 MW Axle Fitting and Axle Fining Not (Left) CIC Application 321239 MI.G Shock Absorber Upper de Loner Attach Pins Il.)CIC Application 321243 Sidebeace Actuator Attach Pim /Trannkin Area tLefOCIC Application 321247 Maui Landing Gnu Uplock Roller Men) CM Application 321251 Maui Landing Gear Striker Ann (Left) CIC Application 321029 Man Gym Trunnion Pm deft Mu . Removal Installation 321217 Man Landing (kit Shock Absorber (Left) . Removal/ Innallation 321201 Main landing Gat Shock Absorber (Left) . Servicing 324105 Brake Assembly (Left Outboard) - Removal/Installation 324106 Brake Assembly (Left Inboard) . Removal/Installation 324144 Maui Landing Gear Brake Assembly(left Outboard) - D. Inspection 324145 Maui Landing Gear Brake Assembly(left Inboard) . D. Inspection 323202 Aneiskid • Functional Test 323221 Wheel Speed Transducer (Left Outboan1) Removal/Installation 3242r Wheel Speed Transducer (Left Inboard) . Removal/Installation 323021 Mnn Landing (kit Sidebeace iLeft) Removal/Installation 323900 Landing 4r Functional Test 323901 landing ( -Ka linICKSCOCy EXICatiC0 Operational Test 324003 Main Wheel Assembly (Len Ouilmard) - Removal / Installation 324009 Main Landing Gear Wheel Bearing (Left Outboard)-Inspection/Check 324004 Maui Wheel Assembly (Left Inboard) • Removal / Installation 324010 Man Landing Gear Wheel Bearing (Left Inboard) - Inspection /Check 324010 Man landing Gear Wheel Bearing (Left Inboard) - Inspection /Check 321004 Main Landing Gear Components Oil. Detailed Corrosion Inspection 321006 nun Landing Gear (Right). Lubrication 321222 Man Landing Gear CIC Reapplication (Right 321232 MW Axle Fitting Attach Pin(Right CIC Application 321236 MW Axle Fitting and Axle Fatting Not (Rigid)CIC Application 321240 MW Shock Absorber Upper de Lower Attach Pins OR) CIC Application 321244 Sidebeace Actuate« Attach Pins I Tranitkm Area Might) CIC Application 321248 Main Landing Gear Uplock Roller (Righta CIC Application 321252 Man landing (kit Sinker Arm (Righ)CIC Application 321030 Main Gear Trunnion Pmt Right Aft) Removal / Installation 321218 Mani Landing Gear Shock Absorber (Right) - Removal / Installation 321202 Main landing Gem Shock Absorber (Right) Servicing 324107 Brake AssemblyMight Inboard) - Removal I Installation 324108 Brake Assembly (Rigid Outboard) • Removal /Installation 324011 nun Landing Gear Wheel Bearing (Right Inboard)- Inspection! Check 324146 Main Landing Gear Brake Assembly(Right Inboard) - D. Inspection 324223 Wheel Speed Transducer (Rigid Inboard). Removal /Installation 324224 Wheel Speed Transducer (Rigid Outboard) • Removal/Installation 323022 Main Landing Gear Sidebrace Might) • Removal / Installation 324005 Maui Wheel Assembly (Right Inboard). Removal / Installation 324012 Maui landing Gear Wheel Bearing (Right Outboard) • Inspection/Check 324006 Maui Wheel Assembly (Right Outboardi • Removal/Installation 324147 Maui Landing Gem Brake Assembly (ItigM Outboard). D Inspection 322003 Nose Landing Gear Components • Detailed Corrosion Inspection 321255 Nose Landing Gear Stock Strut and Axle Assembly CIC Application 321256 Nose Landing Gear Trunnion Assembly CM Application 321259 Nose Landing Gear Truss Brace Assembly CIC Application 321260 Nose Landing Gear Upper Trunnion Attach Pins CIC Application 321263 Nine Landing Gear Upper Drag Brace Attach Pin CIC Application 321264 Nose Landing Gear Striker Arms CIC Application 322220 Nose Landing Gear CIC Reapplication 322004 Nose Landing Gear. Lubrication 322202 Nose Landing Gear Shock Strut Servicing 323900 landing Gear. Functional Test 324001 Nose Wheel Assembly (Left) . Removal / Installation 324007 Nose Wheel Bearings (Left) Inspection / Pack 324002 Nose Wheel Assembly (Right) - Removal/Installation 324000 Nose Wheel Bearings (Right) - Inspection / Pack 325003 Steering - Functional Test Page 5 of 5 EFTA01105739