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
Engines. The original Engine or Suitable Replacement Engine (in case of Total Loss) is in the configuration as permitted under this Agreement installed on the Aircraft shall comply with the following:
(a) have no less than 4,500 Cycles scheduled life remaining in respect of Engine LLPs and no more than 110% of the Aircraft total Flight Hours and Cycles since new. Engine Life Limited Parts will be supported by certification documentation necessary to demonstrate traceability back to birth.
(b) will have accumulated no more than 7,000 Flight Hours and 7,000 Cycles since new or last Engine Performance Restoration shop visit.
(c) shall be serviceable and capable of full rated performance without limitations throughout the entire operating envelop of the Aircraft as defined in the EASA AFM. Each Engine shall have at least 25C sea level hot day EGT margin;
(d) all items beyond the Engine Manufacturer’s in-service limits will be repaired;
(e) will have just completed at the Redelivery Location on or about the Redelivery Date an all module, hot and cold section video borescope inspection. Lessee will also have just completed in respect of each Engine an inspection of each magnetic chip detector, laboratory oil sample analysis, main oil screen and oil and fuel filter inspections. Any defects discovered in such inspections which exceed the Engine Manufacturer’s in-service limits shall be corrected at the Lessee’s expense. No Engine shall be “on watch” for any reason requiring any special or out of sequence inspection or reduced interval inspections. Each such Engine will comply with and have been maintained in accordance with the Agreed Maintenance Programme without waiver or exceptions. All items beyond the Engine manufacturer’s in-service limits shall be repaired; and
(f) have trend or condition monitoring data over at least the previous year; if Engine trend or condition monitoring data indicates a rate of acceleration in performance deterioration over at least the previous ninety days, which is higher than normal based on the maintenance experience of the Engine Manufacturer in operating the same model of engines, under similar conditions, the Lessee will, prior to redelivery, cause to be corrected such conditions which are determined to have exceeded tolerances defined for such engines in the Manufacturer’s maintenance manual or are otherwise determined to be causing such performance deterioration.
Engines. At the date of redelivery, no individual Engine shall ***** A maximum power assurance run will be carried out on each Engine following completion of the redelivery check. Following the acceptance flight, a video recorded borescope of all modules in each of the Engines will be completed by an agency selected by Lessor at Lessor’s cost.
Engines. In the event any engine not owned by Lessor shall be installed on the Aircraft on any Return Occasion, without limiting Lessee's obligations under the -92- 94 Tax Indemnification Agreement, such engine shall be of the same model and equivalent modification status as the Engines or, at Lessee's option, an IAE engine of an improved model suitable for installation and use on the Airframe without diminishing the value, remaining useful life or utility of such Airframe, in each such case having a value, remaining useful life and utility at least equal to (as determined in accordance with the Appraisal Procedure), and be in an operating condition as good as the Engines, assuming the Engines were in the condition and repair as required by the terms hereof immediately prior to such termination and shall conform to the return condition requirements set forth in this Section 16 and Exhibit E, and Lessee, at its own expense and concurrently with such delivery, shall cause such engine to become an Engine by complying with Section 11(b) hereof. Lessee's obligation to comply with the terms of this Section 16(c) shall be conditioned on Lessor's transferring to Lessee all of Lessor's right, title and interest in and to any Engine not installed on the Aircraft at the Return Occasion "AS IS, WHERE IS," without any representation, warranty or recourse of any kind whatsoever, express or implied, except a warranty that such Engine is free and clear of Lessor's Liens.
Engines. (a) Each Engine is installed on the Aircraft and has not less than Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal. The expected life remaining is to be determined by inspection and checks accomplished before Delivery taking account, where available, of:
(i) full borescope inspection;
(ii) analysis of trend data;
(iii) SLOATL assessment or minimum last [***] qualifying flights (excluding the first flight of the day);
(iv) maximum power assurance ground runs;
(v) technical log analysis for a minimum of the previous [***] months of operation;
(vi) previous shop visit assessment (if applicable); and
(vii) in accordance with manufacturer’s maintenance manual.
(b) Following the demonstration flight provided for by Section 2 of this Appendix G, each Engine has just completed at the Delivery Location a complete video borescope inspection of all Engine gas path modules (that inspection performed at Sublessor’s expense) and a power assurance run (performed at Sublessor’s expense) in accordance with Manufacturer’s maintenance manual, in each case Sublessor shall use commercially reasonable efforts to ensure that Sublessee may have one representative present to witness the inspections. Any Discrepancies discovered exceeding the Engine manufacturer’s in-service limits have been corrected at Sublessor’s expense. Sublessor shall have provided a DVD (or other electronic media) of the borescope inspections it had performed to Sublessee. No Engine is on “watch” for any reason requiring any special or out of sequence inspection. Each Engine complies with the operations specification of the previous operator without waiver or exceptions and there being no items beyond the Engine manufacturer’s in-service limits;
(c) Each Engine Life-Limited Part has not less than the Minimum Engine LLP Cycles remaining in accordance with the manufacturer’s then current limitations for the part number in question, and is supported by certification documentation necessary to demonstrate Back-To-Birth Traceability; for this purpose, “Life Limited Part” means a component with an ultimate life which cannot be restored through appropriate maintenance approved by the State of Design of the manufacturer;
Engines. Maintenance Payments for Engine Performance Restoration (not repair) shall be paid for ***** The rate shall be established from the applicable matrix below based on the anticipated Flight Hour to Cycle ratio and region of operation: V2527E-A5 SelectOne (or better) 27,000 lbs. thrust – from Delivery through the first Engine Performance Restoration of the core modules – US $ / FH: 5% Derate ***** ***** ***** ***** ***** ***** ***** 10% Derate ***** ***** ***** ***** ***** ***** ***** 15% Derate ***** ***** ***** ***** ***** ***** ***** 20% Derate ***** ***** ***** ***** ***** ***** ***** V2527E-A5 SelectOne 27,000 lbs. thrust – as a mature Engine following the first Engine Performance Restoration of the core modules – US $ / FH:
Engines. All fire engines shall be regularly and routinely staffed with one
(1) officer and three (3) firefighters. At 0800 hours and 2000 hours, all fire engines shall be staffed with one officer and three firefighters.
Engines. An exclusive license, with the right to grant sublicenses and franchises to make, use or sell to others, throughout the Territory within the Field of Use under the Patent Rights and Technical Information subject to the payment of royalties as provided herein, to make or retrofit motorcycle engines that incorporate the CSRV Valve System in accordance with the Technical Specifications, and to sell, lease or otherwise dispose of such motorcycle engines; and
Engines. The Engines covered by this Agreement are set forth on Exhibit B. During the term of this Agreement. GE shall [*****] of both Rate Per EFH and Supplemental Work Services for the Engines.
Engines. Two CFM Model ________ series engines bearing manufacturer's serial numbers ________ and ________, respectively, installed on the Aircraft. ENGINE MANUFACTURER - CFM International, Inc., a Delaware corporation, and its successors and assigns.
