Rate Per Engine Flight Hour ENGINE SERVICES AGREEMENT BETWEEN GE ENGINE SERVICES, INC. AND AVIANCA CFM56-5B Agreement Number: 1-271756304 Dated: January 18, 2008
Exhibit 10.15
Note: Certain portions have been omitted from this Agreement in accordance with a request for confidential treatment submitted to the Securities and Exchange Commission. Omitted information has been replaced with an asterisk. Omitted information has been filed separately with the Securities and Exchange Commission.
OnPointsm Solutions
Rate Per Engine Flight Hour
BETWEEN
GE ENGINE SERVICES, INC.
AND
AVIANCA
CFM56-5B
Agreement Number: 1-271756304
Dated: January 18, 2008
This proposed Agreement will remain open until January 18, 2008 and will expire if not signed by all Parties on or before that date.
PROPRIETARY INFORMATION NOTICE
The information contained in this document is GE Engine Services, Inc. (“GE”) and AVIANCA Proprietary Information and is disclosed in confidence. It is the property of GE and AVIANCA and will not be used, disclosed to others or reproduced without their express written consent. If consent is given for reproduction in whole or in part, this notice and the notice set forth on each page of this document will appear in any such reproduction. U.S. export control laws may also control the information contained in this document. Unauthorized export or re-export is prohibited.
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
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TABLE OF CONTENTS
Article No. |
Topic |
Page No. |
||||
1. |
Recitals | 3 | ||||
2. |
Definitions | 3 | ||||
3. |
Term | 3 | ||||
4. |
Scope | 3 | ||||
5. |
Equipment Covered | 3 | ||||
6. |
Rate Per EFH Services | 3 | ||||
7. |
Supplemental Work | 7 | ||||
8. |
General Provisions | 8 | ||||
9. |
Customer Responsibilities | 9 | ||||
10. |
[*] | 10 | ||||
11. |
[*] | 10 | ||||
12. |
[*] | 11 | ||||
13. |
Termination | 11 | ||||
14. |
General Terms and Conditions | 12 | ||||
Exhibit No. |
Topic |
Page No. |
||||
A. |
Definitions | 14 | ||||
B. |
Equipment Covered | 17 | ||||
C. |
Addition of Engines | 20 | ||||
D. |
Removal of Engines | 21 | ||||
E. |
Pricing | 22 | ||||
F. |
On-Wing Support – Supplemental Work | 28 | ||||
G. |
Line Replaceable Units | 29 | ||||
H. |
Warranty | 31 | ||||
I. |
General Terms & Conditions | 32 | ||||
J. |
Warranty Assignment Letter | 35 |
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OnPointsm Solutions Engine Services Agreement
Article 1 – Recitals | ||||
1.1 | Parties and Effective Date | THIS ENGINE SERVICES AGREEMENT is made as of this 10th day of January, 2008 by and between Aerovias del Continente Americano S.A. (AVIANCA), having its principal place of business at Centro Administrativo, Xxxxxxx Xx Xxxxxx, Xxxxxx, Xxxxxxxx (“Customer”) and GE Engine Services, Inc., having its principal place of business at 0 Xxxxxxx Xxx, Xxxxxxxxxx, Xxxx 00000 (“GE”) (either a “Party” or collectively, the “Parties”). | ||
Article 2 – Defined Terms | ||||
2.1 | Definitions | See Exhibit A for terms not otherwise defined in this Agreement | ||
Article 3 – Term | ||||
3.1 | [*] | [*] | ||
3.2 | Exclusive Agreement | This Agreement, insofar as it relates to Services, including Supplemental Work, will be exclusive. Except as otherwise expressly provided in this Agreement, Customer will not enter into any other arrangement with a third party, including Customer’s or Customer’s affiliates’ shops, for such Services with respect to Customer’s Engines during the term hereof. If the Customer regains operational control and/or maintenance responsibility for a previously removed Engine, Customer will add such Engine to this Agreement. | ||
Article 4 – Scope | ||||
4.1 | Scope | The OnPoint Solutions program is a comprehensive engine maintenance program under which Services are performed by GE on Engines and priced on a rate per engine flight hour (hereinafter “Rate Per EFH” ) basis or, for Supplemental Work as described in Article 7, priced on a time and material or other pricing basis as set forth in Exhibit E. GE agrees to provide parts, materials and Service(s) to restore Equipment to Serviceable condition in accordance with the established Repair Specification, the Workscope and the terms of this Agreement. | ||
Article 5 – Equipment Covered | ||||
5.1 | Equipment Covered | Customer’s fleet of Engines covered under this Agreement as of the Effective Date are identified in Exhibit B, which may be amended from time to time to incorporate addition or removal of Engines from the Agreement. GE will provide rates (based on the methodology used for the Firm Aircraft) for any of the Purchase Right Aircraft, and Rolling Purchase Right Aircraft, if so requested by Customer. Customer then has the option to include these into this Agreement under such revised rates. | ||
Article 6 – Rate Per EFH Services | ||||
6.1 | [*] | [*] | ||
6.2 | [*] | [*] | ||
6.3 | Addition or Removal of Engines | [*] delivered new to Customer will be covered without the requirement for any Qualifying Shop Visit; only the impact on pricing must be agreed on by the parties. Customer may remove Engines from the Agreement in accordance with Exhibit D. GE has the right to adjust the Rate Per EFH for additions or removals of Engines as further described therein. [*] | ||
6.4 | [*] | [*] |
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6.5 | [*] | [*] | ||
1. Correct a deficiency known or suspected at that time or performance deterioration which has created an Unserviceable condition or to comply with an AD if such AD mandates compliance prior to the next scheduled shop visit per the Removal Schedule. | ||||
2. If applicable, to install new LLP due to life expiration (unless the LLP installed at the last shop visit prior to the Effective Date did not conform to the minimum build requirement in the Repair Specification). | ||||
3. A Minimum Build Standard of 12,000 cycles will be used for all shop visits. | ||||
6.6 | Workscope and Repair Specification | Upon Induction of Engines, GE will prepare a preliminary Workscope and provide a copy of such Workscope to Customer. Such Workscope may include reliability and performance enhancements and Approved Aviation Authority approved repairs. GE may recommend amendment to the Repair Specification to include reliability and performance enhancements during the term hereof to improve Engine operating characteristics and incorporate OEM-approved repairs, subject to Customer’s comments and approval that will not be unreasonably withheld, conditioned or delayed, provided there is no cost or operational impact. The final Workscope must be approved in writing by Customer before restorative Services commence. Any changes or amendments to the Repair Specification will be mutually agreed by the Parties and may result in an adjustment in the pricing set forth in Exhibit E. | ||
6.7 | [*] | [*]
3. Recommend, as appropriate, the replacement of a Delivered Engine with a Serviceable replacement Engine of like configuration and condition. In such case, title to the removed Engine will vest with GE and title to the replacement Engine will vest with Customer or the owner of the Delivered Engine, provided the terms of such replacement comply with any aircraft lease or mortgage applicable to such replaced Engine. Customer will make reasonable commercial efforts to facilitate such title passage.
4. Repair or replace LLP with LLP having at least as much remaining life, on a part by part basis, as the removed LLP.
5. Repair LRU’s received with an Engine for a Rate Per EFH Shop Visit and which were installed on the Engine when it was removed from the aircraft for Services, as evidenced by records provided in accordance with Article 9.9.
6. Comply with Airworthiness Directives (“ADs”), that are published as of the Effective Date and AD’s and Category 1 through 6 Service Bulletins that are required to be incorporated during the term of this Agreement regardless of the permitted compliance date. If an AD has an option of inspecting or making repairs, GE and Airline will mutually agree as to the proper course of action.
7. Provide all labor, materials and parts necessary to return Engine to a Serviceable condition where an Engine or module requires Services for, or as a result of, Major FOD, to a maximum amount for each Engine of the greater of any insurance deductible covering such Major FOD event or $500,000.00. The rate for this coverage is based upon the historical fleet average for this Engine line and is subject to adjustment for the actual FOD rate experienced by Customer during this Agreement.
8. Administer the support and repair services subcontract with Xxxxxxxx Aerostructures for the nacelles and thrust reversers for the fee plus any other fees charged by the vendor under the subcontract, which will be passed through from the vendor, listed in Exhibit E-1. Customer has until September 30, 2008 to elect this coverage. Customer may elect to have this coverage cover only its owned Engines and not the Engines leased from C.I.T. as identified on Exhibit B. Should Customer elect this coverage it must also elect the Optional Line Replaceable Units coverage set forth on Exhibit G. |
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9. Repair LRU’s identified in Exhibit G that are removed from an Engine at the flight line in accordance with the terms set forth in the Exhibit. Customer has until September 30, 2008 to elect coverage for the Optional Line Replaceable Units set forth on the Exhibit. Customer may elect to have this coverage cover only its owned Engines and not the Engines leased from C.I.T. as identified on Exhibit B. | ||||
6.8 | [*] | [*] | ||
6.9 | Transportation | GE will be obligated for arranging and paying for the costs of roundtrip transportation from the location of Engine removal to the location of Engine installation specified by Customer, provided such costs do not exceed the costs of roundtrip transportation from Customer’s primary hub in BOG to the Designated Repair Station and from the Designated Repair Station to Customer’s primary hub in BOG for each Rate Per EFH Shop Visit and will provide all required maintenance services for such Engine’s transportation stands and containers while at GE’s facility. If such costs do exceed the costs of roundtrip transportation from Customer’s primary hub in BOG to the DRS, and return, Customer will be responsible for such excess cost. | ||
6.10 | Program Manager | Assign a Customer Program Manager who will: | ||
1. Be the point of contact for Customer with respect to Services. | ||||
2. Draft a Procedures Manual to the extent required for the Customer’s Rate Per EFH Program, and submit such Procedures Manual for comments and joint approval. | ||||
3. Develop with Customer, on a monthly basis, a Removal Schedule (“RS”) to forecast Delivery for Engines for Services. The RS will identify by serial number the Engine(s) to be removed during the following six (6) month period, the anticipated reason for removal of each and the schedule for Delivery. The forecast will be provided in a mutually agreeable format quarterly on a rolling annual basis. | ||||
6.11 | Engineering Support | GE will provide the following engineering support services: | ||
1. Notify Customer of any deviations from the configuration specification of Engines Delivered for Service, and request resolution of same. | ||||
2. Provide an Engine findings report (which may include photographs), identifying damage detected and repair(s) accomplished. | ||||
3. Consultation on trend reports. | ||||
4. Advice covering engine enhancements. | ||||
5. GE will work with Customer in Inspection of records for used engines being considered by Customer for acquisition and shop visit development for return of leased engines, but Customer shall be solely responsible for making the final determination as to the quality of the used engines. |
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6.12 | [*] | [*] | ||
6.12.1 | [*] | [*] | ||
6.12.2 | Return of Lease Engines | Customer will ship the lease engine DDP (Incoterms 2000) to a GE housekeeping facility as soon as practicable, but in no case later than ten (10) Days following Redelivery of an Engine. Daily engine rental fees and hourly restoration charges will be waived during such ten (10) day period. Customer will commence paying such applicable daily rental fees and hourly restoration charge on the eleventh (11th) day following correction of the AOG condition. The foregoing will constitute the sole remedy of Customer and the sole liability of GE for lease engine availability and resolution of AOG conditions under this Agreement. | ||
6.13 | Diagnostics | Implement Comprehensive Diagnostics services (“Diagnostics”) to identify and diagnose trend shifts as follows:
• [*]
Any information provided to Customer by GE for use in troubleshooting and managing operations is advisory only. GE is not responsible for line maintenance or other actions resulting from such advice. Customer is responsible for identifying and resolving any aircraft or Engine faults or adverse trends. |
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6.14 | OnWing Support | Customer will have access to GE On-Wing Support Worldwide Network for scheduled, unscheduled, line or hospital shop maintenance Services not otherwise considered to be Rate Per EFH Services, up to a maximum of seven hundred and fifty (750) hours per year of the Agreement. Customer may carry over a maximum of fifty percent (50%) of unused hours from any one Agreement year the carry-over amount is not cumulative. Non-labor related expenses (travel time, shipping, materials, etc.) will be liquidated at $80/hr to calculate an equivalent OWS hour. Any excess OWS Services above the hours described above will be invoiced as Supplemental Work. | ||
6.15 | BER Engine | If an Engine is determined by GE to be BER, GE will offer either to repair such engine under applicable Rate Per EFH Rates or replace such Engine by substituting an engine of at least equivalent value, utility and marketability, in either case at no additional charge to Customer beyond the applicable Rate Per EFH Rates. If the latter option is selected by Customer, there will be no penalty charged under Exhibit C for the engine which is BER. | ||
6.16 | [*] | [*] | ||
Article 7 – Supplemental Work | ||||
7.1 | Supplemental Work | [*] | ||
7.1.1 | Supplemental Services | 1. Any shop visit not described in the Rate Per EFH Program, including Services provided on Engines not eligible for Rate Per EFH Services;
2. Services described in Article 6 of this Agreement will be Supplemental Work if GE and Customer have reasonably determined that Equipment requires Services for, or as a result of:
a. An Aircraft Accident or Aircraft Incident;
b. Major FOD above and beyond what is covered in Article 6.7;
c. The incorporation of SBs not covered in Article 6.7
d. An act of God, military action or terrorist activity;
e. Improper or negligent installation, operation, removal or maintenance of Customer’s Equipment not in conformance with OEM manuals and experimental test applied to the Equipment, unless performed by GE;
f. Failure of a non-OEM-approved LRU, part or repair;
g. Engine upgrade programs or conversion to another thrust rating;
h. Lease return conditions or sale of the Engine;
i. Repair or replacement of BFE/QEC components;
j. Damage caused by transport of Equipment by unapproved method, unless at GE’s direction or under GE’s control.
k. Replacement of scrapped LRU’s, except as provided in Exhibit G.
3. Cost of LLP material replaced for life expiration will be priced in accordance with the Supplemental Work pricing terms set forth in Exhibit E-5 through E-6.
4. GE will provide, at Customer’s request, Supplemental Work on-wing Services at the rates set forth in Exhibit F. |
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5. In the event that Customer decides to Deliver an Engine for Services not eligible for Rate per EFH Services against the advice and consent of GE’s Customer Program Manager or delegate, GE will treat such shop visit as Supplemental Work.
6. Maintenance services for Engine transportation stands and containers during Supplemental Work shop visits are charged as Supplemental Work.
7. For Engines undergoing a shop visit initiated by a requirement for Supplemental Work to be performed, restoration and parts replacement which would have been performed as Rate per EFH Services had the event or condition which initiated the requirement for Supplemental Work not occurred, will nevertheless be performed as Rate per EFH Services. | ||||
Article 8 – General Provisions | ||||
8.1 | [*] | [*] | ||
8.2 | Documentation | GE will prepare and provide to Customer a Services records package that complies with AAA regulations. | ||
8.3 | [*] | [*] | ||
8.4 | Preparation for Redelivery | GE will prepare and package Equipment in shipping containers which Customer has provided for Redelivery in accordance with standard commercial practice. | ||
8.5 | Redelivery | After completion of Services, GE will Redeliver the Engine to Customer. In the event Redelivery of an Engine cannot occur due to any act or failure to act of Customer, GE may place such Engine into storage. In such event, GE will notify Customer of such storage, GE’s Redelivery obligations will be deemed fulfilled, all risk of loss or damage to the Equipment will thereupon pass to Customer, and any amounts payable to GE upon Redelivery will be payable upon presentation of GE’s invoice. Engines in storage will be considered available spare Engines for purposes of Article 6.12 above. Customer will reimburse GE for all expenses incurred by GE, such as, but not limited to, preparation for and placement into storage, handling, inspections, preservation and insurance of the Equipment. Upon payment of all amounts due hereunder, GE will assist and cooperate with Customer in the removal of Equipment placed in storage. | ||
8.6 | Parts Replacement Procedures | |||
8.6.1 |
[*] | [*] | ||
8.6.2 |
[*] | [*] | ||
8.6.3 |
[*] | [*] | ||
8.6.4 |
[*] | [*] | ||
8.6.5 |
Customer Furnished Equipment (“CFE”) | For Supplemental Work only, Customer may supply parts to GE as CFE, if such parts are: (A) consistent with the approved Workscope; (B) provided with an AAA serviceability tag; and (C) ready for immediate use. Such CFE is subject to a material handling fee in accordance with Supplemental Work pricing in Exhibit E. If such CFE includes non-OEM parts, Customer will release GE from, and will indemnify and hold GE harmless from and against, any and all claims, liabilities, damages and losses of any nature whatsoever resulting from use of such CFE. | ||
8.6.6 |
[*] | [*] | ||
8.6.7 |
Scrapped Parts | GE will dispose of all Scrapped Parts at its sole expense and without any further adjustment to Customer. If the Services are being provided as Supplemental Work, Scrapped Parts will instead be retained for at least thirty (30) days pending Customer instruction for possible warranty claims. |
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8.7 | Subcontracting | Except as provided in Section 6.8 regarding repair of Engines at GE’s facility in Brazil, GE has the right to subcontract any Services to any GE Repair Station or affiliate or any subcontractor selected by GE or GE’s affiliates, as long as such facility, affiliate or subcontractor is properly certified and rated by the AAA to perform the required Services. If GE does subcontract, the Customer obligations under this Agreement, including transportation expense, will be no greater than if such Services were performed at the DRS, Customer will, at its sole expense, have the right to review GE’s quality system audit report(s) for such subcontractor(s). Subcontracting of any Services will not relieve GE of its performance obligations set forth in this Agreement. | ||
Article 9 – Customer Responsibilities | ||||
9.0 | Customer Obligations | Customer will: | ||
9.1 | Qualifying Shop Visit | For Engines added under Exhibit C, Section 2, have a Qualifying Shop Visit performed on all used Engines added to this Agreement, unless waived by GE. All non-OEM approved parts or repairs will be removed at Customer’s expense prior to eligibility for Rate Per EFH Services. | ||
9.2 | Notice of Delivery | Provide three (3) Days advance written notice of Delivery of Equipment for scheduled removals prior to dispatch. Customer will not Deliver piece parts or components for repair separate from Customer’s Engine without GE’s written consent. | ||
9.3 | Customer Representative | Designate in writing one (1) or more Customer representative. | ||
9.4 | Removal Schedule | Prepare with GE’s Customer Program Manager, a forecast of operational and maintenance program schedules, fleet operational status, Engine/aircraft flight hours and cycles, scheduled Engine or Engine module removals, Engine sale or return, and any other relevant information to allow the Parties to formulate an RS. | ||
9.5 | Line Maintenance | Provide all line maintenance and repair and line station support, consistent with applicable maintenance manuals. | ||
9.6 | Troubleshooting | Troubleshoot Equipment in accordance with applicable maintenance manuals. | ||
9.7 | Pre-existing Warranties | Assure that any requested repair of an Engine, accessory or component that is covered under a third-party warranty that is not assigned to GE will be performed directly by that person at no expense to GE. Notwithstanding the above, GE may accept a purchase order for the time and material repair of a warranted item from Customer or the person giving the warranty. | ||
9.8 | Assignment of Warranties | Assign to GE all applicable Engine warranties and guarantees using the Warranty Assignment Letter attached hereto as Exhibit J. GE will arrange with CFM and Customer for assignment of warranties. | ||
9.9 | Engine Documentation | Provide to GE the information and records, set forth in the Procedures Manual, to establish the Engine condition. Customer’s failure to timely furnish the required information may cause delay of and records may delay Induction of the Engine for Service, may cause an Excusable Delay and may result in premature LLP replacement. | ||
9.10 | External Equipment Configuration | Provide to GE, or arrange for Airbus to provide to GE, an external Engine configuration specification. | ||
9.11 | Office Facilities | Ensure that adequate office space, parking, telephone, facsimile and computer connection is available for the GE representative(s), if assigned to the Customer’s facility. | ||
9.12 | [*] | [*] |
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9.13 | Monitoring Equipment |
Provide an automated method to transfer operational and maintenance data to GE for the monitoring and diagnosis of Engine condition. If the aircraft is equipped with air-to-ground equipment such as ACARS, the Customer will forward the data directly to the GE SITA/ARINC address. If air-ground equipment is not available, GE will work with Customer to establish an alternative electronic means of providing this data. | ||
9.14 | Packaging Equipment | Be obligated for all packaging, labeling and associated documentation of the Equipment at Delivery, in accordance with the International Civil Aviation Organizations (ICAO) Technical Instructions for the Safe Transport of Dangerous Goods by Air, and if the Equipment is to be transported over the United States of America, the US Department of Transportation Regulations 49 CFR 171-180. If required by applicable law or regulations, Customer will further provide a material safety data sheet to GE at Delivery of the Equipment indicating any substances contained within the Equipment to be consigned. Customer will indemnify, defend and hold harmless GE from all or any claims, liabilities, damages, judgments, costs, penalties, fines or any punitive damages imposed, alleged, or assessed by any third party against GE and caused by and to the extent of Customer’s non-compliance with this Article 9.14. | ||
9.15 | Shipping Stands | Provide all shipping stands, shipping containers, mounting adapters, inlet plugs and covers, required to package Equipment for Redelivery. | ||
Article 10 – [*] | ||||
10.1 | [*] | [*] | ||
Article 11 – [*] | ||||
11.1 | [*]
Time of Shop Visit (“TSV”) |
[*]
Customer will remit to GE, prior to Redelivery of each Engine, an amount equal to the actual EFH incurred by that Engine since delivery from manufacturer of the aircraft in which such Engine was originally installed (for a new installed Engine), or since delivery from manufacturer (for a new spare Engine), or since the last Rate Per EFH Shop Visit for that Engine, whichever occurred last, but no less than the monthly minimum set forth in Article 11.2 below, multiplied by the Current adjusted and escalated TSV Rate Per EFH. Such amount will be set forth in an invoice issued by GE to Customer at least ten (10) days prior to the expected Redelivery date. In the event that Customer causes such payment to be made on its behalf by a third party, and such third party fails to pay some or all of the payment due to GE, then Customer will make the payment, in whole or in part, to make up the amount not paid. In the event that such payment is not paid in full, GE is entitled to suspend its performance under this Agreement with respect to such Engine until such amount is paid in full. | ||
11.2 | [*] | [*] | ||
11.3 | Added Engines | For Engines added subsequent to the Effective Date, Customer will make Rate Per EFH payments in accordance with Article 11.1 for all EFH from the date such added Engines enter the Program. | ||
11.4 | Supplemental Work Payments | |||
11.4.1 | Initial Invoice | [not used] | ||
11.4.2 | Final Invoice | [*] | ||
11.5 | Alternate Payment Terms | In the event Customer’s account becomes delinquent, GE reserves the right to require different terms of payment or other commercially acceptable assurances of payment. | ||
11.6 | [*] | [*]. |
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11.7 | [*] | [*] | ||
11.8 | [not used] | |||
11.9 | Other Liens | Customer: (i) acknowledges that GE has the legal right to assert mechanic’s liens or other statutory or common law liens under applicable law (foreign or domestic) against Engines following performance of Services under this Agreement, for which payment has not been made by Customer and (ii) agrees to supply such information, including name and address of the owner of each Engine, as reasonably requested by GE to facilitate filing of such liens in New York or any other jurisdiction where Services may be performed. With respect to Engines leased by Customer, GE understands that Customer has been authorized and required by the owners to cause Services to be performed. GE may, at its option, notify the owners of the existence of this Agreement and GE’s lien rights arising from performance of Services. | ||
11.10 | Enforcement | If Customer fails to tender any payment owing under this Agreement and GE initiates foreclosure with respect to any Engine, for which payment has not been made, whether pursuant to a security interest granted under this Agreement or a mechanic’s lien, then Customer agrees to supply to GE all records, log books and other documentation pertaining to the maintenance condition of the Engine, and a certificate either (i) certifying that the Engine has not been involved in any Aircraft Accident or Incident or (ii) specifying the date and facts surrounding any accident or incident in which the Engine has been involved and the nature and extent of the damage sustained (such records, log books, certificate and other documentation referred to hereinafter as the “Engine Documents”). The Parties recognize that the failure by Customer to deliver the Engine Documents may have a material, adverse effect on the value of any Engine with respect to which foreclosure has been initiated by GE and the ability of GE to sell or lease the Engine, and that the damages GE may sustain as a result are not readily calculable. | ||
Article 12 – [*] | ||||
12.1 | [*] | [*] | ||
12.2 | [*] | [*] | ||
Article 13 – Termination | ||||
13.1 | Failure to Pay/Insolvency | GE may terminate or suspend performance of all or any portion of this Agreement if Customer: (A) fails to make any payments when due, unless cured within thirty (30) Days of such due date; (B) makes any agreement with creditors due to its inability to make timely payments of its debts; (C) enters into bankruptcy or liquidation, whether compulsory or voluntary; (D) becomes insolvent; or (E) becomes subject to the appointment of a receiver of the whole or material part of its assets. If such termination should occur, Customer will not be relieved of its payment obligation for Services rendered hereunder. | ||
13.2 | [*] | [*] |
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13.3 | Effect of Termination | Upon termination or upon expiration of the Agreement: | ||
(A) All Customer Engine documentation, manuals and records shall be transferred to Customer at no cost to Customer, and
(B) The parties will cooperate reasonably and in good faith to accomplish the transition described above with no disruption to the operations of Customer or the maintenance of the Engines. | ||||
13.4 | [*] | [*] | ||
13.5 | [*] | [*] | ||
13.6 | Work in Process, Redelivery of Customer Equipment |
Upon the termination or expiration of this Agreement, GE will complete all work in process in a diligent manner and Redeliver all Engines, parts and related documentation, provided that Customer (a) has paid in full all charges for all such Services and material, plus all costs and fees, incurred by GE in providing support, including any lease engines, and (b) has returned all lease engines provided under this Agreement. | ||
Article 14 – General Terms and Conditions | ||||
General Terms & Conditions | See Exhibit I for General Terms and Conditions. | |||
Article 15 | Insurance and Indemnity | |||
15.1 | Liability Insurance | Throughout the Term and for a period of two (2) years thereafter, GE will maintain for the benefit of Customer commercial aviation liability insurance in an amount of not less than One Hundred Million Dollars ($100,000,000.00) combined single limit on an occurrence basis for bodily injury and property damage including contract liability and products liability on an aggregate basis coverage. GE will also maintain for the benefit of Customer throughout the Term aircraft all risk hull and spares insurance, including transit coverage. All insurance policies shall be primary without contribution from any insurance carried by Customer and shall name Customer as an Additional Insured with respect to GE’s indemnity obligations hereunder. All insurance policies will continue in full force and effect for at least thirty (30) days after Customer receives written notice of cancellation, termination or material alteration thereof. GE will obtain the insurance required by this Section from a financially sound insurance company of recognized responsibility and will furnish Customer with a certificate of insurance evidencing such coverage in compliance with this Agreement prior to the commencement of any Services and at least annually thereafter, as well as on request from Customer not more than twice per year. | ||
15.2 | [*] | [*] Agreement has caused damage to tangible personal property or bodily injury (including death), if and to the extent that such damage or injury is proximately caused by the negligent or other legally culpable act or omission of GE. Customer shall furnish to GE prompt written notice and requisite authority, information and assistance to defend.
Customer agrees to indemnify, defend and hold GE harmless from claims by third parties asserted against GE that Customer’s possession, use, or maintenance of the aircraft or Engine (not attributable to GE) has caused damage to tangible personal property or bodily injury (including death), if and to the extent that such damage or injury is proximately caused by the negligent or other legally culpable act or omission of Customer and is determined by a court of competent jurisdiction to be the legal liability of Customer, provided that GE furnishes to Customer prompt written notice and requisite authority, information and assistance to defend. | ||
15.3 | Claims | Customer will promptly notify GE of any claim made or suit brought within the scope of Section 15.2 and GE may assume and conduct the defense of such claim and may effect any settlement which it deems proper, provided that no such settlement may result in any cost or penalty to Customer or require Customer to change or restrict its operations or maintenance functions or waive any rights hereunder. |
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The Parties have caused this Agreement to be executed by their duly authorized officer or representatives who represent to each other and both Parties that each is employed in the capacity indicated below and has the unequivocal authority to execute and deliver this Agreement, which shall be effective as of the date first above written.
This Agreement is executed by each of the Parties as of the day and year written below:
GE ENGINE SERVICES, INC. | Aerovias del Continente Americano S.A. (AVIANCA) | |||||||
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EXHIBIT A – DEFINITIONS
Capitalized terms used but not otherwise defined in this Agreement will have the following meanings:
Agreement | This Rate Per EFH Engine Services Agreement, as the same may be amended or supplemented from time to time, including all its Exhibits and Schedules. | |
Aircraft Accident | An occurrence caused by the operation of an aircraft, and in which any person suffers a fatal injury or serious injury as a result of being in or upon the aircraft or by direct contact with the aircraft or anything attached to the aircraft, or in which the aircraft receives substantial damage or a third party’s property is damaged in any way. | |
Aircraft Incident | An occurrence, other than an Aircraft Accident, caused by the operation of an aircraft that affects or could affect the safety of operations and that is investigated and reported. | |
Airworthiness Directive or “AD” | A document issued by the Approved Aviation Authority having jurisdiction over the Engines, identifying an unsafe condition relating to such Engines and, as appropriate, prescribing inspections and the conditions and limitations, if any, under which the Engines may continue to operate. | |
Approved Aviation Authority or “AAA” | As applicable, the Federal Aviation Administration of the United States (“FAA”), or the Unidad Administrativo Especial de Aeronautica Civil (UAEAC) or such other equivalent aviation authority having jurisdiction over the Engines or the performance of Services provided hereunder. | |
Base Year | 2006 is the calendar year in which the Base Price is applicable and which is the baseline year used for economic adjustments. | |
Beyond Economic Repair or “BER” | Where the cost to restore Equipment to the requirements of the Repair Specification, when calculated on a Supplemental Work basis, exceeds sixty-five percent (65%) of the fair market value of a comparable item of Serviceable Equipment. | |
CLP | The manufacturer’s Current catalog or manufacturer’s Current list price pertaining to a new item of Equipment. | |
Current | As of the time of the applicable Service or determination. | |
Day | Calendar day unless expressly stated otherwise. If performance is due on a recognized public holiday, performance will be postponed until the next business day without penalty. | |
Delivery | The arrival of Equipment together with all applicable records and required data Delivery Duty Paid (“DDP”) International Chamber of Commerce, Incoterms 2000, at the DRS, whereby Customer fulfills the obligations of seller and GE fulfills the obligations of buyer. “Deliver” means the act by which Customer accomplishes Delivery. | |
Designated Repair Station or “DRS” | The primary Repair Station designated by GE, where GE performs or is obligated to perform Services on Engines. | |
Dollars or “$” | The lawful currency of the United States of America. | |
Engine | Each bare engine assembly, which is the subject of this Agreement and identified in Exhibit B, including its essential LRU’s, controls, accessories and parts as described in the engine manufacturer’s specification manuals. | |
Engine Flight Cycle or EFC | A flight cycle of an Aircraft on which an Engine is installed from wheels up to wheels down | |
Engine Flight Hour or “EFH” | Engine flight hour expressed in hourly increments of aircraft flight from wheels up to wheels down. | |
Equipment | An individual or collective reference, in the proper context, to Engines, Engine modules, Engine assemblies and sub-assemblies, Engine mounted controls and accessories, LRU’s, and components and parts of any of the foregoing. | |
Foreign Object Damage or “FOD” | Damage to any portion of the Engine caused by impact with or ingestion of a non-Engine object such as birds, stones, hail, ice, vehicles, tools or debris. FOD may be further classified as a “Major FOD,” which means FOD that causes an out of limit condition per the Aircraft Maintenance Manual, and which, either immediately or over time, requires the Engine to be removed from service or prevents the reinstallation of the Engine. | |
Induction | The date work commences on the Equipment at the DRS when all of the following have taken place: (i) GE’s receipt of the Equipment and required data (ii) Parties’ approval of the Workscope (iii) Parties’ agreement on use of the Customer Furnished Equipment; and (iv) receiving inspection (including pre-testing if needed). | |
Life Limited Part or “LLP” | A part with a limitation on use established by the OEM or the AAA, stated in cumulative EFH or cycles. |
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
14
Line Replaceable Unit or “LRU” | A major control or accessory that is mounted on the external portion of an Engine, which can be replaced while the Engine is on-wing. | |
OEM | The original manufacturer of an item of Equipment. | |
Overtime | All labor hours charged on a basis other than Straight Time. | |
Performance Restoration | The Services performed during an Engine shop visit in which, at a minimum, the compressor, combustor and high-pressure turbine are exposed and subsequently refurbished, consistent with the Repair Specification. | |
Procedures Manual | A separate document, not part of this Agreement, which provides detailed procedures and guidance for the administration of the Rate Per EFH Program. In case of conflict between the Procedures Manual and the Agreement, the Agreement will prevail. | |
Qualifying Shop Visit | A Repair Station visit during which the initial Performance Restoration is performed on an Engine on a Supplemental Work basis. The purpose of the Qualifying Shop Visit is to qualify such Engine for the Rate Per EFH fixed rate pricing for subsequent shop visits. | |
QEC or Quick Engine Change | An assembly of parts mounted on an Engine to enable the Engine to be installed on an aircraft. | |
Rate Per EFH | The Monthly Rate Per EFH and the TSV Rate Per EFH as set forth on Exhibit E-1. | |
Redelivery | The arrival at Customer’s facility of Serviceable Equipment with legally required certifications, Delivery Duty Paid (“DDP”), International Chamber of Commerce, Incoterms 2000, whereby Customer fulfills the obligations of buyer and GE fulfills the obligations of seller. “Redeliver” will also mean the act by which GE completes Redelivery. | |
Removal Schedule or “RS” | The schedule jointly developed by GE and Customer for scheduled or anticipated Engine removals for Services or scheduled or anticipated Engine removal from operation. | |
Repair Specification | The mutually agreed repair specification which establishes the baseline to which an Engine or item of Equipment will be inspected, disassembled, repaired, modified, reassembled and tested to make such Engine or item of Equipment Serviceable. Such Repair Specification will meet or exceed the recommendations of the OEM’s operational specifications, applicable OEM maintenance or overhaul manuals and Customer’s maintenance plan that has been approved by the AAA. | |
Repair Station | One or more of the repair facilities owned by GE or its affiliates, now or in the future, which are certified by the appropriate AAA to perform the applicable Service hereunder. A list of such repair facilities will be provided to Customer from time to time. | |
Repairable | Capable of being made Serviceable. | |
Rotable Part | A new or used Serviceable part drawn from a common pool of parts used to support one or more customers. A Rotable Part replaces a like part removed from an Engine when such removed part requires repair. | |
Scrapped Parts | Those parts determined by GE to be Unserviceable and BER. | |
Service(s) | With respect to any item of Equipment, all or any part of those maintenance, repair and overhaul services under this Agreement and the furnishing of parts, materials, labor, facilities, tooling, painting, plating and testing in connection therewith. “Serviced” will be construed accordingly. | |
Service Bulletin or “SB” | The document issued and identified as a Service Bulletin by an OEM to notify the operator of modifications, substitution of parts, special inspections, special checks, amendment of existing life limits or establishment of first time life limits, or conversion of an Engine from one model to another. | |
Serviceable | Meeting all OEM and AAA specified standards for airworthiness. | |
Straight Time | The labor hours charged during an employee’s regular workday that are not subject to overtime compensation in accordance with the applicable law, a collective bargaining agreement or the recognized practice at the relevant GE Repair Station. | |
Supplemental Work | Any Service provided hereunder that is not covered under the Rate Per EFH Program. Supplemental Work will be performed by GE and invoiced to Customer in accordance with the pricing set forth in Exhibit E | |
Termination | The ending of this Agreement before the expiration of the Initial Term or extension thereof. |
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
15
Turn Around Time | The number of Days between Induction and when an Engine is ready to ship as evidenced by placement of the Serviceable Tag, exclusive of Excusable Delay as defined in Exhibit I. | |
Unserviceable | Not meeting all OEM and AAA specified standards for airworthiness. | |
Workscope | The document written by GE and approved by Customer describing the prescribed repair or approach to repair of Equipment to meet the requirements of the Repair Specification. | |
Workscope Planning Guide | The base document which provides an approach for incorporating an “on-condition” maintenance concept for the Engine with the goal of improving the Engine time between shop visits and reducing maintenance costs, while maintaining the reliability of the Engine in service. |
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
16
EXHIBIT B: EQUIPMENT COVERED
Customer will maintain a spare Engine(s) to installed Engines ratio of not less than eight percent (8%), rounded up to the next whole Engine, during the term of this Agreement. However, GE will work with Customer if the rounding falls slightly less than 8%.
Count |
ESN |
Date of |
Time Since |
Cycles Since |
Time Since |
Cycles Since |
Date of last |
[*] |
[*] | |||||||||
1 |
xxx-xxx | 02/01/2008 | 0 | 0 | 0 | 0 | N/A | |||||||||||
2 |
xxx-xxx | 02/21/2008 | 0 | 0 | 0 | 0 | N/A | CIT | [*] | |||||||||
3 |
xxx-xxx | 02/21/2008 | 0 | 0 | 0 | 0 | N/A | CIT | [*] | |||||||||
4 |
xxx-xxx | 04/01/2008 | 0 | 0 | 0 | 0 | N/A | CIT | [*] | |||||||||
5 |
xxx-xxx | 04/01/2008 | 0 | 0 | 0 | 0 | N/A | CIT | [*] | |||||||||
6 |
xxx-xxx | 05/01/2008 | 0 | 0 | 0 | 0 | N/A | CIT | [*] | |||||||||
7 |
xxx-xxx | 05/01/2008 | 0 | 0 | 0 | 0 | N/A | CIT | [*] | |||||||||
8 |
xxx-xxx | 09/01/2008 | 0 | 0 | 0 | 0 | N/A | |||||||||||
9 |
xxx-xxx | 09/01/2008 | 0 | 0 | 0 | 0 | N/A | |||||||||||
10 |
xxx-xxx | 11/01/2008 | 0 | 0 | 0 | 0 | N/A | |||||||||||
11 |
xxx-xxx | 11/01/2008 | 0 | 0 | 0 | 0 | N/A | |||||||||||
12 |
xxx-xxx | 10/01/2008 | 0 | 0 | 0 | 0 | N/A | |||||||||||
13 |
xxx-xxx | 10/01/2008 | 0 | 0 | 0 | 0 | N/A | |||||||||||
14 |
xxx-xxx | 01/01/2009 | 0 | 0 | 0 | 0 | N/A | |||||||||||
15 |
xxx-xxx | 08/01/2009 | 0 | 0 | 0 | 0 | N/A | |||||||||||
16 |
xxx-xxx | 08/01/2009 | 0 | 0 | 0 | 0 | N/A | |||||||||||
17 |
xxx-xxx | 09/01/2009 | 0 | 0 | 0 | 0 | N/A | |||||||||||
18 |
xxx-xxx | 09/01/2009 | 0 | 0 | 0 | 0 | N/A | |||||||||||
19 |
xxx-xxx | 10/01/2009 | 0 | 0 | 0 | 0 | N/A | |||||||||||
20 |
xxx-xxx | 10/01/2009 | 0 | 0 | 0 | 0 | N/A | |||||||||||
21 |
xxx-xxx | 01/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
22 |
xxx-xxx | 01/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
23 |
xxx-xxx | 01/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
24 |
xxx-xxx | 01/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
25 |
xxx-xxx | 02/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
26 |
xxx-xxx | 02/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
27 |
xxx-xxx | 02/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
28 |
xxx-xxx | 02/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
29 |
xxx-xxx | 04/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
30 |
xxx-xxx | 04/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
31 |
xxx-xxx | 04/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
32 |
xxx-xxx | 04/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
33 |
xxx-xxx | 05/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
34 |
xxx-xxx | 05/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
35 |
xxx-xxx | 05/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
36 |
xxx-xxx | 05/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
37 |
xxx-xxx | 05/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
38 |
xxx-xxx | 06/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
39 |
xxx-xxx | 06/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
40 |
xxx-xxx | 07/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
41 |
xxx-xxx | 07/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
42 |
xxx-xxx | 08/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
43 |
xxx-xxx | 08/01/2010 | 0 | 0 | 0 | 0 | N/A |
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
17
44 | xxx-xxx | 10/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
45 |
xxx-xxx | 10/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
46 |
xxx-xxx | 11/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
47 |
xxx-xxx | 11/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
48 |
xxx-xxx | 11/01/2010 | 0 | 0 | 0 | 0 | N/A | |||||||||||
49 |
xxx-xxx | 01/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
50 |
xxx-xxx | 01/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
51 |
xxx-xxx | 01/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
52 |
xxx-xxx | 01/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
53 |
xxx-xxx | 02/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
54 |
xxx-xxx | 02/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
55 |
xxx-xxx | 02/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
56 |
xxx-xxx | 02/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
57 |
xxx-xxx | 03/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
58 |
xxx-xxx | 03/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
59 |
xxx-xxx | 04/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
60 |
xxx-xxx | 04/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
61 |
xxx-xxx | 04/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
62 |
xxx-xxx | 04/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
63 |
xxx-xxx | 04/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
64 |
xxx-xxx | 05/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
65 |
xxx-xxx | 05/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
66 |
xxx-xxx | 07/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
67 |
xxx-xxx | 07/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
68 |
xxx-xxx | 08/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
69 |
xxx-xxx | 08/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
70 |
xxx-xxx | 09/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
71 |
xxx-xxx | 09/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
72 |
xxx-xxx | 09/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
73 |
xxx-xxx | 09/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
74 |
xxx-xxx | 10/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
75 |
xxx-xxx | 10/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
76 |
xxx-xxx | 10/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
77 |
xxx-xxx | 11/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
78 |
xxx-xxx | 11/01/2011 | 0 | 0 | 0 | 0 | N/A | |||||||||||
79 |
xxx-xxx | 01/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
80 |
xxx-xxx | 01/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
81 |
xxx-xxx | 01/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
82 |
xxx-xxx | 02/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
83 |
xxx-xxx | 02/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
84 |
xxx-xxx | 03/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
85 |
xxx-xxx | 03/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
86 |
xxx-xxx | 04/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
87 |
xxx-xxx | 04/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
88 |
xxx-xxx | 05/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
89 |
xxx-xxx | 05/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
90 |
xxx-xxx | 06/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
91 |
xxx-xxx | 06/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
92 |
xxx-xxx | 06/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
93 |
xxx-xxx | 06/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
94 |
xxx-xxx | 07/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
95 |
xxx-xxx | 07/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
96 |
xxx-xxx | 07/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
97 |
xxx-xxx | 08/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
98 |
xxx-xxx | 08/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
99 |
xxx-xxx | 09/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
100 |
xxx-xxx | 09/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
101 |
xxx-xxx | 10/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
102 |
xxx-xxx | 10/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
103 |
xxx-xxx | 11/01/2012 | 0 | 0 | 0 | 0 | N/A |
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
18
104 | xxx-xxx | 11/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
105 |
xxx-xxx | 12/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
106 |
xxx-xxx | 12/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
107 |
xxx-xxx | 12/01/2012 | 0 | 0 | 0 | 0 | N/A | |||||||||||
108 |
xxx-xxx | 12/01/2012 | 0 | 0 | 0 | 0 | N/A |
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
19
EXHIBIT C: ADDITION OF ENGINES
Section 1: For Engines that have not undergone an Engine shop visit (including New Engines)
New Engines are Engines that (a) have not undergone a shop visit, (b) have less than 100 EFH TSN and (c) which contain only OEM approved parts and OEM approved repairs. Such New Engines will enter the Rate Per EFH Program without requiring a Qualifying Shop Visit.
Process for Adding Engines
1. | Customer will provide Engine serial number, aircraft tail number, previous operator, current owner, TSN, TSLV, CSN, CSLV, historic derate information together with such other reasonable data as GE may request (to the extent available) and thrust rating to be used for the added Engine(s). |
2. | GE will review all of the Engine data set forth above and will calculate the TSN to CSN ratio and take-off derate (assumed to be zero % if not provided) for such Engine. |
3. | The resulting TSN to CSN ratio (expressed as an EFH to cycle ratio) and take-off derate information will be compared to the Base point (in effect immediately prior to the date such Engine is added to the Rate Per EFH program) of the TSV Rate Per EFH Severity Matrix to determine the adjusted Rate Per EFH for such Engine. Such adjusted Rate Per EFH will be multiplied by the EFH incurred prior to the addition of the Engine into the Rate Per EFH program and paid by Customer to GE at the next Shop Visit. |
4. | The Parties will amend Exhibit B accordingly as mutually agreed. |
Section 2: For Engines that have undergone a shop visit
Process for Adding Engines
1. | Customer will provide Engine serial number, aircraft tail number, previous operator, current owner, TSN, TSLV, CSN, CSLV, historic derate information together with such other reasonable data as GE may request (to the extent available) and thrust rating to be used for the added Engine(s). Customer will provide additional reasonable information as requested. |
2. | Unless waived by GE based on an evaluation of operating parameters of the Engine being added and other business considerations, GE will perform or Customer will have performed at a GE approved repair facility a Qualifying Shop Visit. |
3. | The Parties will amend Exhibit B accordingly. |
4. | If an engine proposed to be added hereunder has had a heavy maintenance shop visit performed by a GE repair facility within one hundred hours prior to the proposed inclusion, it will be added without the requirement for any further Qualifying Shop Visit provided proper documentation and inspection (by GE) has occurred verifying that a Qualifying Shop Visit is not required. |
Section 3 – [*]
[*]
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
20
EXHIBIT D: REMOVAL OF ENGINES
Section 1: All Engines – Conditions For Removal
Customer may remove Engines from this Agreement upon advance written notice, if Customer is no longer operating the Equipment and is no longer responsible for maintenance of the Equipment for the following reasons only:
1. | Bona fide sale or other bona fide transfer to an unaffiliated third party |
2. | Return to Lessor; |
3. | If GE has reasonably determined the Engine to be BER. |
[*]
Section 2: [*]
[*]
Section 3: [*]
[*]
Section 4: Rate Per EFH Adjustment – Remainder of the Fleet
GE will evaluate the effect of any Engine’s removal on the Rate Per EFH and the parties will agree on appropriate adjustments to such Rate Per EFH (and the Monthly Rate Per EFH payment) accordingly. Such adjusted Rate Per EFH and any adjusted Monthly Rate Per EFH will be mutually agreed between GE and Customer and thereafter will be incorporated into the Agreement by way of amendment. Such adjusted Rate Per EFH will take into consideration the effect of such removal on the fleet size, age and condition of the remaining Engines (for example, the nature and extent of the Services to be provided, Engine hardware configuration and number of repairs performed). Customer will pay the Rate Per EFH, as adjusted for such removal, for all EFH incurred by all Engines from the date of the Engine removal.
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
21
Exhibit E – PRICING (Unless otherwise stated herein, all rates and prices set forth in this Exhibit E are stated in 2006 U.S. Dollars)
E-1A. A320 RATE PER EFH
[*] | Rate Per EFH | |
[*] | ||
[*] |
E-2A. A320 Rate Per EFH Operating Parameters & Rate Adjustment (The Rate Per EFH is predicated on the parameters set forth below).
[*] | [*] | [*] | [*] | [*] | ||||
[*] |
E-1B. [*]
[*] | Rate Per EFH | |
[*] | ||
[*] |
E-2B. A319 Rate Per EFH Operating Parameters & Rate Adjustment (The Rate Per EFH is predicated on the parameters set forth below).
Engines Delivered in accordance with the Delivery Schedule set forth in Exhibit B |
Utilization: 2843 Average EFH Per Year per Aircraft |
[*] | Take-Off Derate: 17 % at a
thrust |
LLP Minimum Build: 12000 Cycles | ||||
[*] |
The rate for Engines which incur flight hours while installed on both an A320 and an A319 will be apportioned according to the hours incurred at each thrust level.
[*]
E-3 [*]
[*]
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
22
Exhibit E-4 – Rate Per EFH Sensitivity Matrix – to be Provided by GE.
* | [Two pages have been omitted in accordance with a request for confidential treatment.] |
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
23
X- 0 [*]
[*]
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
24
Exhibit X- 0 – [*]
[*]
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
25
Exhibit X- 0 – [*]:
[*]
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
26
Exhibit E-8 – Service Credits
[*]
The above issued credits may only be applied by Customer towards the purchase of CFM56-5 initial provisioning equipment.
Such credit amounts are not subject to escalation and are subject to adjustment for any change in the operating parameters (including number and delivery dates of Engines) set forth above. However, if after purchasing the required amount of initial provisioning equipment, Avianca has not used all of the credits, the remaining credits may be used as a credit for any invoices issued by GE under this Agreement. Customer may carry over any unused credits issued in any year, however, all credits must be applied by the end of the term of this Agreement. For the avoidance of doubt, unused credit amounts outstanding at the end of the term of the Agreement will be canceled.
In addition, GE shall issue to Customer spare Engine Service credits, in the amounts set forth below:
[*].
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
27
EXHIBIT F – Supplemental Work ON-WING SUPPORTSM – FIELD SERVICE TECHNICAL AND REPAIR SUPPORT RATES)
GE On Wing Support, Inc., will provide on wing support technicians, along with special tooling, to perform flight-line services, on wing and off wing inspection, maintenance, and repair of Engines as specified in a mutually executed workorder by Customer. Such Engine support services may be provided, as designated by Customer and agreed by service provider at Customer’s facilities or at repair facilities owned by GE On Wing Support, Inc. or its affiliates. All Services provided shall be in accordance with its standard commercial quality control policies, procedures, and practices. A turn-time estimate for each workscope for acceptance by Customer prior to beginning of work will be provided.
FIXED WORKSCOPE PRICING
[*]
Other pricing applicable for Engine maintenance provided by GE On Wing Support, Inc
A. | Workscope Pricing and Deployment |
1) | If additional workscopes not listed in the fixed price workscope schedule are required, they will be priced and quoted prior to beginning of work. The fixed rate workscope schedule pricing covers all technician repair activity, preparation and deprep requiring normal manpower and tooling in normal work conditions. Reasonable additional charges may apply for unusual engine or work conditions. |
[*]
B. | Material and Subcontractor |
GE On Wing Support, Inc. furnished material or subcontracted services required for repair of Customer’s equipment at the direction of Customer shall be charged at acquisition cost plus a ten percent (10%) fee.
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
28
EXHIBIT G – LINE REPLACEABLE UNITS
[*]
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
29
CFM56-5 LRU Components | ATA Chapter | |
Electronic Control Unit | 73-2 | |
Hydromechanical Fuel Control | 73-2 | |
Fuel Pump | 73-1 | |
Fuel Return Valve | 73-1 | |
HPTCC Valve | 75-2 | |
Air Valve LPTACC Module | 75-2 | |
N2 Speed Sensor | 77-1 | |
IDG Oil Cooler | 73-1 | |
Transfer Gearbox | 72-6 | |
VSV Actuator | 75-3 | |
Bleed Valve Fuel (Hyd) Gear Motor | 75-3 | |
Fuel Flow Transmitter | 73-3 | |
Ignition Exciter | 74-1 | |
Master Ballscrew Actuator Assembly | 75-3 | |
Transient Bleed Air Xxxxx | 00-0 | |
Xx. 0 Bearing Vibration Sensor | 77-3 | |
T12 Temperature Sensor | 73-2 | |
Lubrication Unit | 79-2 | |
Alternator stator | 73-2 | |
T25 Temperature Sensor (CIT) | 73-2 | |
Burner Modulating Valve | 73-1 | |
Ballscrew Actuator Assembly | 75-3 | |
Ignition Lead Assembly | 74-2 | |
Oil/Fuel Heat Exchanger | 79-2 | |
T5 Temperature Sensor | 77-2 | |
Oil Tank | 79-1 | |
Servo Fuel Heater | 73-1 | |
T3 Sensor Compressor Outlet Temperature | 77-2 | |
T495 Thermocouple Wiring Harness | 77-2 | |
Clogging Indicator Transmitter | 79-2 | |
HPTCC Thermocouple | 73-2 | |
Bleed Valve Stop Mechanism | 75-3 | |
Alternating Current Generator (Rotor) | 73-2 | |
Electrical Harness (Jx) | 73-2 | |
N1 Speed Sensor | 77-1 | |
Fuel Nozzles | 73-1 | |
Oil Temperature Sensor | 79-3 | |
P25 Sensor Assembly | 72-0 | |
Air Turbine Engine Starter | 80-1 | |
4.0 Inch Diameter Starter Valve Assembly | 80-1 |
Optional Line Replaceable Units* | ATA Chapter | |
Integrated Drive Generator & Adapter | 24-1 | |
Hydraulic Pump | 29-1 | |
Valve-Bleed Press, Reg | 36-1 | |
HP Regulator Valve | 36-1 | |
Valve – I.P, Check | 36-1 |
* | Customer has until September 30, 2008 to elect coverage of these parts. |
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
30
EXHIBIT H – Warranty
H-1 – Rate Per EFH Services Warranty
[*]
H- 2 – Supplemental Work Warranty
[*]
H -3 – [*]
[*]
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
31
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
32
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
33
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
34
Exhibit J – Warranty and Guarantee Assignment Letter
(Customer Letterhead)
(Date)
(Name and Address of Original Engine Manufacturer)
Attn:
Re: | Assignment of Third Party Warranty and Guarantees |
Dear (Sir/Madam):
(Customer) and the (Original Engine Manufacturer) entered into Agreement Number dated , 20 , wherein (Customer) agreed to purchase a specified number of aircraft engines and (Original Engine Manufacturer) agreed to provide certain warranties and guarantees with regard to said engines to (Customer).
(Customer) and GE Engine Services, Inc. have entered into a separate engine maintenance agreement Number dated 20 , (“Maintenance Agreement”) for the maintenance, repair and overhaul of said engines. The Maintenance Agreement specifies that (Customer) shall, during the term of the Agreement, assign to GE Engine Services, Inc. the benefit of all warranties and certain guarantees applicable during the Term of the Agreement to the engines covered by the Maintenance Agreement only to the extent that they relate to the repair of the Engines. The guarantees to be assigned are: shop visit rate guarantee, exhaust gas temperature guarantee, extended new module and engine guarantee, extended ultimate life guarantee, extended campaign change guarantee, extended new parts guarantee, and vendor interface warranty.
This letter serves as official notification: 1) to (Original Engine Manufacturer) of Customer’s assignment of the applicable warranties and guarantees under the engine purchase agreement; and 2) to GE Engine Services, Inc. of (Customer)’s fulfillment of this obligation under the Maintenance Agreement.
(Original Engine Manufacturer), please indicate your concurrence with said assignment by signing in the space provided below and returning a copy of this letter to the undersigned.
(Signature Block)
RATE PER EFH | GE and AVIANCA PROPRIETARY INFORMATION |
Subject to restrictions on the cover or first page
35