Life Limited Parts. Frontier and RAI shall each cooperate with one another in order to manage and minimize engine life limited parts (“LLP”) expenses for Covered Aircraft. To that end, RAI shall provide annual projections of LLP requirements and supplemental notice of specific engine maintenance events which require LLP replacement as they are scheduled. Frontier may, at its option and with RAI's consent (which consent shall not be unreasonably withheld) provide or arrange the provision of used serviceable LLPs that otherwise meet RAI's specifications and reasonable minimum cycle-remaining requirements, to be incorporated into a Covered Aircraft. In connection with the withdrawal of any Covered Aircraft from the capacity purchase provisions of this Agreement (whether at the end of such aircraft's scheduled term or otherwise), Frontier shall pay RAI for the pro-rata cost (based on useful life and using the then-current catalogue price for LLPs) of all LLPs consumed for all Scheduled Flights by such Covered Aircraft under this Agreement, and RAI shall pay Frontier for the pro-rata cost (based on useful life and using the then-current catalogue price for LLPs) of all LLPs provided by Frontier and incorporated into such Covered Aircraft pursuant to the previous sentence and not consumed for any Scheduled Flights under this Agreement.
Life Limited Parts. All replacement Life Limited Parts will have complete back to birth traceability. GE will provide Customer with information about the previous owners for each replacement Life Limited Part if so applicable and requested. No replacement Life Limited Parts will be incident/accident-related, as evidenced by GE to Customer in accordance with the Customer’s General Maintenance Manual.
Life Limited Parts. Life Limited Parts (LLPs) as specified by Aircraft, Airframe, Engine, and Appliance Type Data Sheets and Time Controlled Components identified by MPD shall possess all historic Aircraft Records necessary to establish origin, date, hours and cycles at each installation and removal, last shop visit findings and Return to Service where applicable, in addition to total service and authenticity.
Life Limited Parts as specified by the Aircraft and Engines types certificates shall be provided with appropriate documents and records that identify current status, life history (removal and installation), total time in service, authenticity and origin back to manufacturer.
Life Limited Parts. LLP received by GE without the necessary records required in Paragraph 5.1.8 above that relate to LLP, shall be replaced by GE at Copa’s expense as stated therein, following the time period allowed for Copa to provide such records, as stated herein.
Life Limited Parts. 1 1.10 Tires and Brakes....................................... 1 1.11 Paint.................................................. 1 1.12
Life Limited Parts. With respect to (1) all Airframe life and calendar controlled components, have a minimum of one year, and 3,000 Airframe Flight Hours and 2,000 Airframe Cycles remaining to next scheduled removal or inspection (in accordance with the Approved Maintenance Program), but (a) if a component has a life, overhaul or check interval limit that is less than the above-stated hours, cycles or calendar time requirement (in accordance with the Approved Maintenance Program), then such component shall have a full check interval remaining and (b) "on- condition" and "condition-monitored" components shall be serviceable and shall have no indication of incipient faults and (2) no Engine life- limited parts shall have less than 2,000 Engine Cycles remaining until the next scheduled removal or replacement.
Life Limited Parts. Life Limited Parts control is the responsibility of the Operator. The approved maintenance organisation will have to provide the operator with all the necessary information about the LLP removal/installation so that the Operator may update its records (see also paragraph 3.20 "Exchange of information").
Life Limited Parts. (a) Each life limited part shall have at least the same number of hours remaining (subject to a minimum of one year) as they had upon the Aircraft's entry into revenue service by Lessee. EXHIBIT E-1 TO LEASE AGREEMENT RETURN CERTIFICATE ------------------ On this ____ day of _____________________, ____ FRONTIER AIRLINES, INC. ("Lessee") hereby returns the below-described Aircraft for all purposes under that certain Operating Lease Agreement dated as of November __, 1996 (the "Lease"), between Lessee and FIRST SECURITY BANK, NATIONAL ASSOCIATION,not individually but solely as Owner Trustee. Capitalized terms used herein and not otherwise defined herein shall have the same meaning as in the Lease. Lessor hereby acknowledges that it has found the below-described Aircraft or Airframe to comply with all return conditions set forth in the Lease and acknowledges return of the below-described Aircraft. Airframe: -------- Manufacturer's Serial Number __________ U.S. Registration Number __________ Total Hours __________ Total Cycles __________ Hours since last D Check __________ Cycles since last D check __________ Months since last D check __________ Hours since last C Check __________ Cycles since last C check __________ Months since last C check __________ Pounds of fuel on board __________ Gallons of oil on board __________ Engine Serial Nos.: ____ ____ ____ ____ Total Hours ____ ____ ____ ____ Total Cycles ____ ____ ____ ____ Hours since last Shop Visit ____ ____ ____ ____ Cycles since last Shop Visit ____ ____ ____ ____
Life Limited Parts. 1.9.1 With respect to each Airframe life and calendar controlled component, have a minimum of 12 months, and 3,200 Airframe Flight Hours and 1,500 Airframe Cycles remaining to next scheduled test, inspection or removal (in accordance with the Approved Maintenance Program), but (1) if a component has a life, overhaul or check interval limit that is less than the above-stated hours, cycles or calendar time requirement (in accordance with the Approved Maintenance Program), then such component shall have a full check interval remaining and (2) "on-condition" and "condition-monitored" components shall be fully functioning in accordance with manufacturer's specifications and shall have been operationally checked and tested during the Final Maintenance and shall have no indication of incipient faults. All Airframe life and calendar controlled components shall on average be no older in hours or cycles than the Aircraft and in no case shall any single such Part be more than six month's older in hours or cycles than the Aircraft, provided that, without limiting the foregoing, each component shall have the same or more recent part or dash number as the component installed on the Aircraft on the Delivery Date.
1.9.2 No Engine life-limited Parts shall have less than 3,000 Engine Cycles remaining until the next scheduled removal or replacement.
