APU Clause Samples

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APU. If the APU undergoes "off the fuselage" maintenance (as hereinafter defined) pursuant to Lessee's Maintenance Program performed by an Approved Maintenance Performer approved by Lessor, subject to the last sentence of this clause (D), Lessor will reimburse Lessee, from the APU Payments paid to Lessor by Lessee as of the date such maintenance is completed, for the actual cost incurred by Lessee for such off the fuselage maintenance. "Off the fuselage" maintenance of the APU means any heavy maintenance of the APU performed by an Approved Maintenance Performer during a shop visit that requires teardown/disassembly, to the extent the same results in performance restoration; provided, however, such maintenance will not include the cost of removal, shipment or re-installation of the APU or any maintenance of components associated with an installed auxiliary power unit. Lessor will make such APU Payments available to Lessee for the cost of off the fuselage maintenance of the removed APU: (x) when Lessee reinstalls such APU in the Airframe following such maintenance or (y) when Lessee replaces such APU with an auxiliary power unit that meets all requirements of this Lease, including Article 6 hereof (determined immediately after such off the fuselage maintenance of the removed APU and on the assumption that the removed APU had been reinstalled in the Airframe).
APU a) Certified Statement on Status of APU; b) In house modifications (if applicable); c) Approved Release to Service Certification for installed units; d) APU Log Book/ Master Record of Installation/ Removals; e) APU Shop Visit Reports & reason for removal, for all APU shop visits; f) Dirty finger print shop work cards and material data sheets for all APU shop visits; g) Statement of APU hours to Aircraft Flying hours (if applicable); h) APU Borescope Report; i) Last Test Run Report; j) All Life Limited Parts (LLPs) will have complete life traceability of time consumed (Cycles and/or Flight Hours as applicable) since new. Such traceability shall include historical removal and installation documentation of each LLP in respect of each APU where such LLP had been installed and where time has been consumed. Each removal and installation document will evidence LLP total Flight Hours and LLP total Cycles accumulated in each Engine or module; k) Each LLP will have a signed and certified cover page including engine or module total hours, total Cycles, part total Flight Hours, total Cycles and date for each removal and installation depicting the life of the part since new. Notwithstanding, any LLPs replaced during the term of the lease will have the most recent FAA 8130-3 tag or JAA Form 1, as applicable, used to install such LLP into the applicable APU; l) APU manufacturer’s or FAA or EASA approved data shall be provided for any discrepancies outside of the APU manufacturer’s APU shop manual limits that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: i) Approval form; ii) Complete description of the discrepancy; iii) Supporting analysis and documentation; m) APU manufacturer’s or FAA or EASA approved data shall be provided for any repairs not in accordance with the APU manufacturer’s APU shop manual that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: i) Approval form; ii) Complete description of repair; iii) Supporting analysis and documentation; and n) Current disk sheet (LLP) signed and certified, if applicable.
APU. (a) The APU shall be serviceable in accordance with the Approved Maintenance Program parameters; (b) The APU will have not less than half-time remaining to the next shop visit based upon the AMR reliability program and the APU manufacturer's MTBR statistics; and (c) If the APU: (i) has fewer Flight Hours remaining until the next scheduled removal for overhaul under the Agreed Maintenance Program than it had on the Delivery Date, then the Lessee shall pay to the Lessor an amount equal to the product of (i) such difference, multiplied by (ii) US$9.00 per Flight Hour; and (ii) has a greater number of Flight Hours remaining until the next scheduled removal for overhaul under the Agreed Maintenance Program than it had on the Delivery Date, then the Lessor shall pay to the Lessee an amount equal to the product of (i) such difference, multiplied by (ii) US$9.00 per Flight Hour.
APU. (a) The APU shall be serviceable in accordance with the Agreed Maintenance Program parameters. (b) The historical and technical records, condition trend monitoring data, power assurance runs and borescope inspection shall not indicate an abnormal acceleration in the rate of performance deterioration or oil consumption in the APU.
APU. (a) The APU shall be serviceable in accordance with the Agreed Maintenance Program.
APU. G001 Certified Statement on Status of APU (if applicable) G002 Certified SB Compliance Report/AD Status Report G003 Approved Release to Service Certification for installed units G004 APU Log Book/Master Record of Installation/Removals G005 Complete copies of all APU Shop Visit Reports & Reason for Removal G006 Statement of APU Hours to Aircraft Flying Hours G007 LLP Status and Full Traceability to birth G008 APU Borescope Report G009 Last On-Wing/Health Check Data sheets (if applicable) G010 Last Test Cell Run G011 Blank G012 Certified Incident and Accident Statement with respect to the APU
APU. Lessee will return the Aircraft's installed APU in good and efficient operating condition in accordance with the manufacturer's specifications and those of the Maintenance Program, ordinary wear and tear alone excepted. Immediately prior to the return of the Aircraft the APU shall be inspected and all items requiring repair or replacement shall be repaired or replaced at Lessee's expense. Any operational discrepancies of the APU shall be corrected in accordance with the Maintenance Program at Lessee's expense prior to the return of the Aircraft to Lessor.
APU. The APU shall be in a serviceable condition and have accumulated not more than 2,000 APU Hours since its last shop visit for heavy repair (as defined by the APU manufacturer) (subject to paragraph 8 of Schedule “1” hereto).
APU. The auxiliary power unit of the Aircraft ("APU") shall be in serviceable condition.

Related to APU

  • Engine A. Any internal repairs or replacement of internal components, or replacement of engine assembly.

  • Engines POSITION SERIAL NO. TOTAL HOURS TOTAL CYCLES HRS/CYCLES SINCE LAST SHOP VISIT Time Remaining to Next LIFE LIMITED PART REMOVAL PART NAME HOURS CYCLES MSN MSN

  • Aircraft This peril includes self-propelled missiles and spacecraft.

  • Spares The Contractor shall ensure that the Contractor’s operational base at the Site is at all times stocked with spare parts for the Contractor's Equipment that meet the requirements of the Contract, together with all necessary or desirable packing and marking for that purpose and that such spare parts are sufficient to ensure that the Work /services can continue in the event of failure of the Contractor’s Equipment.

  • Substitution of Engines Upon the occurrence of an Event of Loss with respect to an Engine under circumstances in which an Event of Loss with respect to the Airframe has not occurred, the Owner shall promptly (and in any event within fifteen (15) days after such occurrence) give the Indenture Trustee written notice of such Event of Loss. The Owner shall have the right at its option at any time, on at least five (5) Business Days’ prior notice to the Indenture Trustee, to substitute, and if an Event of Loss shall have occurred with respect to an Engine under circumstances in which an Event of Loss with respect to the Airframe has not occurred, shall within one hundred and twenty (120) days of the occurrence of such Event of Loss substitute, a Replacement Engine for any Engine. In such event, immediately upon the effectiveness of such substitution and without further act, (i) the replaced Engine shall thereupon be free and clear of all rights of the Indenture Trustee and the Lien of this Trust Indenture and shall no longer be deemed an Engine hereunder and (ii) such Replacement Engine shall become subject to this Trust Indenture and be deemed part of the Aircraft for all purposes hereof to the same extent as the replaced Engine. Such Replacement Engine shall be an engine manufactured by Engine Manufacturer that is the same model as the Engine to be replaced thereby, or an improved model, and that is suitable for installation and use on the Airframe, and that has a value, utility and remaining useful life (without regard to hours and cycles remaining until overhaul) at least equal to the Engine to be replaced thereby (assuming that such Engine had been maintained in accordance with this Trust Indenture). The Owner’s right to make a replacement hereunder shall be subject to the fulfillment (which may be simultaneous with such replacement) of the following conditions precedent at the Owner’s sole cost and expense, and the Indenture Trustee agrees to cooperate with the Owner to the extent necessary to enable it to timely satisfy such conditions: (i) an executed counterpart of each of the following documents shall be delivered to the Indenture Trustee: (A) a Trust Indenture Supplement covering the Replacement Engine, which shall have been duly filed for recordation pursuant to the Act or such other applicable law of the jurisdiction other than the United States in which the Aircraft of which such Engine is a part is registered in accordance with Section 4.02(e), as the case may be; (B) a full warranty ▇▇▇▇ of sale (as to title), covering the Replacement Engine, executed by the former owner thereof in favor of the Owner (or, at the Owner’s option, other evidence of the Owner’s ownership of such Replacement Engine, reasonably satisfactory to the Indenture Trustee); and (C) UCC financing statements covering the security interests created by this Trust Indenture (or any similar statements or other documents required to be filed or delivered pursuant to the laws of the jurisdiction in which such Aircraft may be registered) as are deemed necessary or desirable by counsel for the Indenture Trustee to protect the security interests of the Indenture Trustee in the Replacement Engine; (ii) the Owner shall cause to be delivered to the Indenture Trustee an opinion of counsel to the effect that the Lien of this Trust Indenture continues to be in full force and effect with respect to the Replacement Engine and such evidence of compliance with the insurance provisions of Section 4.06 with respect to such Replacement Engine as the Indenture Trustee shall reasonably request; (iii) promptly after the filing of the Trust Indenture Supplement, the Owner shall have caused to be furnished to the Indenture Trustee an opinion of the Owner’s aviation law counsel reasonably satisfactory to the Indenture Trustee addressed to the Indenture Trustee as to the due filing for recordation of the Trust Indenture Supplement with respect to such Replacement Engine under the Act or such other applicable law of the jurisdiction other than the United States in which the Aircraft is registered in accordance with Section 4.02(e), as the case may be, and the registration (which the Owner shall have caused to be effected) with the International Registry of the sale to the Owner of such Replacement Engine (if occurring after February 28, 2006) and the International Interest granted under such Trust Indenture Supplement with respect to such Replacement Engine; and (iv) the Owner shall have furnished to the Indenture Trustee a certificate of a qualified aircraft engineer (who may be an employee of the Owner) or an independent appraiser certifying that such Replacement Engine has a value and utility and remaining useful life (without regard to hours and cycles remaining until overhaul) at least equal to the Engine so replaced (assuming that such Engine had been maintained in accordance with this Trust Indenture). Upon satisfaction of all conditions to such substitution, (x) the Indenture Trustee shall execute and deliver to the Owner such documents and instruments, prepared at the Owner’s expense, as the Owner shall reasonably request to evidence the release of such replaced Engine from the Lien of this Trust Indenture, (y) the Indenture Trustee shall assign to the Owner all claims it may have against any other Person relating to any Event of Loss giving rise to such substitution and (z) the Owner shall receive all insurance proceeds (other than those reserved to others under Section 4.06(b)) and proceeds in respect of any Event of Loss giving rise to such replacement to the extent not previously applied to the purchase price of the Replacement Engine as provided in Section 4.05(d).