Condition of Controlled Components. Aircraft and Engine hour or cycle controlled components or parts, at time of return to Lessor, shall have remaining, as a minimum, one half life and/or fifty percent (50%) of the Lessee's approved hour or cycle limit, whichever is applicable or most limiting, before any scheduled removals for overhaul, test, disassembly or replacement. All components or parts controlled on a calendar basis shall have at least twelve (12) months or fifty percent (50%) of its total approved life in hours or cycles, if greater remaining before scheduled removal for testing, overhaul or replacement. However, if a component or part has a life, overhaul or check interval limit that is less than the above, Lessee shall, at its expense, perform all such tasks immediately prior to return. All such hour/cycle or calendar controlled components or parts are defined as those components or parts controlled under the Maintenance Program.
Condition of Controlled Components. Aircraft and engine hour and/or cycle controlled components at time of return to Lessor shall have remaining, as a minimum, [***] life and/or [***] percent ([***]%) of the manufacturer’s recommended overhaul, interval in hours or cycles, whichever is applicable, before any scheduled removals for overhaul, test or disassembly. All components controlled on a calendar basis shall have remaining at least half-time before scheduled removal for testing or overhaul. Such hour/cycle or calendar controlled components are defined as those components controlled under Lessee’s FAA-approved maintenance program.
Condition of Controlled Components viii 4. CONDITION OF INSTALLED ENGINES AND APU.........................................................viii 5. PROVISION FOR "POWER-BY-THE HOUR AGREEMENTS".....................................................ix
Condition of Controlled Components. Aircraft and Engine hour or cycle controlled components or parts, at time of return to Lessor (or its designee), shall have remaining, as a minimum, one half life and/or fifty percent (50%) of the Lessee's approved hour or cycle limit, whichever is applicable or most limiting, before any scheduled removals for overhaul, test, disassembly or replacement. All components or parts controlled on a calendar basis x shall have at least twelve (12) months or fifty percent (50%) of its total approved life in hours or cycles, if greater remaining before scheduled removal for testing, overhaul or replacement. However, if a component or part has a life, overhaul or check interval limit that is less than the above, Lessee shall, at its expense, perform all such tasks immediately prior to return. All such hour/cycle or calendar controlled components or parts are defined as those components or parts controlled under the Maintenance Program.
Condition of Controlled Components. Each life-limited part or component and aircraft hour and/or cycle controlled components of the Aircraft and of each Engine at the time of redelivery of the Aircraft to Sublessor shall have remaining at least 3,000 hours and/or 3,000 cycles, whichever is more limiting, between scheduled removals for overhaul, testing, or disassembly. All components controlled on a calendar basis shall have remaining at least 12 months before scheduled removal for testing or overhaul. Such hour/cycle or calendar controlled components are defined as those components controlled under the Maintenance Program. However, if the component or part has a check interval limit that is less than the above stated hours, cycles or calendar time limit requirement, the check interval limit shall prevail.
Condition of Controlled Components. Engine hour, cycle or calendar-controlled components or parts, at time of return to Lessor, shall have remaining, as a minimum, one half life and/or fifty percent (50%) of the manufacturers approved hour, cycle or calendar limit (whichever is applicable and most limiting), before any scheduled removals for overhaul, test, disassembly or replacement; provided that, without regard to any payment made or to be made pursuant to Section 1.8, all components or parts controlled on an hour, cycle or calendar basis shall have at least one C check interval (assuming annual utilization of 2700 hours and 2700 cycles) (or, if the service interval is less than one C check, 100% of the service interval) remaining before scheduled removal for testing, overhaul or replacement.
Condition of Controlled Components. Each life-limited part or component and hour and/or cycle controlled components of the Engine at the time of redelivery of the Engine to Lessor shall have remaining at least 3,000 hours and/or 3,000 cycles, whichever is more limiting, between scheduled removals for overhaul, testing, or disassembly. All components controlled on a calendar basis shall have remaining at least 12 months before scheduled removal for testing or overhaul. Such hour/cycle or calendar controlled components are defined as those components controlled under the Maintenance Program. However, if the component or part has a check interval limit that is less than the above stated hours, cycles or calendar time limit requirement, the check interval limit shall prevail.
Condition of Controlled Components. Aircraft and engine hour and/or cycle controlled components at time of return to Lessor shall have remaining, as a minimum one half life and/or of the manufacturer's recommended overhaul interval in hours or cycles, whichever is applicable, before any scheduled removals for overhaul, test or disassembly. All components controlled on a calendar basis shall have remaining at least half-time before scheduled removal for testing or overhaul, Such hour/cycle or calendar controlled components are defined as those components controlled under Lessee’s FAA-approved maintenance program.
Condition of Controlled Components. Aircraft and Engine hour-controlled components or parts, at time of return to Sublessor, shall have remaining, as a minimum, one half life and/or fifty percent (50%) of the manufacturers approved hour limit, before any scheduled removals for overhaul, test, disassembly or replacement. Aircraft and Engine life cycle fatigue (“LCF”), controlled components or parts, at time of return to Sublessor, shall have remaining, as a minimum, one half life and/or fifty percent (50%) of the manufacturers approved cycle limits, before any scheduled removals for overhaul, test, disassembly or replacement; provided that, without regard to any payment made or to be made pursuant to Section 1.8, all components or parts controlled on a calendar basis shall have at least one C check interval (or, if the service interval is less that one C check, 100% of the service interval) remaining before scheduled removal for testing, overhaul or replacement.
Condition of Controlled Components. (i) Engine Cycle controlled components (Group A parts) at the date of redelivery shall have remaining as a minimum 3000 Cycles of the declared life quoted in the latest issue of the time limits manual issued by the Engine Manufacturer.
(ii) Any components controlled by Flight Hours shall have as a minimum 4,000 Flight Hours remaining before scheduled removal for refurbishment, test, disassembly or replacement.
(iii) All components controlled on a calendar basis shall have remaining at least 12 months before scheduled removal for refurbishment, test, disassembly or replacement.
