Common use of Engines Clause in Contracts

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. Each Engine will be installed on the Aircraft and will comply with the following: (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; shall have been maintained in accordance with the Lessee's Maintenance Program; (ii) analysis of trend data; shall be in compliance with all mandatory service bulletins and ADs affecting such Engine and having a final compliance or termination date during the Term (without regard to any deferrals that may be granted); (iii) SLOATL assessment shall be free and clear of all Liens arising by act or minimum last [***] qualifying flights (excluding the first flight of the day); omission of, or suffered to exist by, Lessee; and (iv) maximum power assurance ground runs; shall contain the same Parts (vor substitutes or replacements therefor, as provided in the Aircraft Lease Agree ment) 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 manualas initially delivered to Lessee. (b) Following If, at the demonstration flight provided for end of the Term, the Engines are subject to an "Engine Maintenance Agreement" (as defined by Section 2 of this Appendix Gthe Aircraft Lease Agree ment), and such Engine Maintenance Agreement has been effectively assigned to Lessor, Lessee shall return each Engine has just completed in such condition as shall make such Engine eligible for continued maintenance under the Engine Maintenance Agreement. If, at the Delivery Location end of the Term, the Engines are not subject to an Engine Maintenance Agreement (or such Agreement has not been effectively assigned to Lessor): (i) each of the Engines (pursuant to Lessee's Maintenance Program) shall have a complete video minimum of half-time until the next scheduled overhaul, based on the Engine Manufacturer's published data over the immediately prior 12 months; (ii) any mandatory service bulletins or ADs that have been deferred shall be incorporated before the Return, (iii) no Engine shall be "on watch;" and each Engine shall perform within the Engine Manufacturer's recommended operating limitations. To the extent that, at the end of the Term, any of the life limited parts of the Engines are not covered by an Engine Maintenance Agreement (which has been assigned to Lessor), such life limited parts shall have a remaining life of at least 2,500 Cycles. (c) Prior to the Return Date (unless an Engine Maintenance Agreement is in effect), a borescope inspection of all each Engine gas path modules (that inspection performed shall be conducted by a qualified technician acceptable to Lessor, at Sublessor’s expense) Lessor's expense and a power assurance run (performed at Sublessor’s expense) in accordance with Manufacturer’s maintenance manual, the presence of Lessor's designated technical representative. Any defects discovered 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 such inspection which exceed the Engine manufacturer’s Manufacturer's in-service limits have been shall be corrected at Sublessor’s expense. Sublessor shall have provided a DVD (or other electronic media) by Lessee, prior to Return of the borescope inspections it had performed Aircraft, at no cost 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;Lessor.

Engines. (a) Each Engine is installed on In the Aircraft and has event any engine 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 owned by Lessor shall be determined by inspection and checks accomplished before Delivery taking account, where available, of: returned with an Airframe in lieu of an Engine: (i) full borescope inspection; if the reason therefor is other than that an Event of Loss has occurred to such Engine, such engine shall be satisfactory to Lessor, in its reasonable discretion, free and clear of Liens, suitable for use on such Airframe and shall have a value and utility at least equal to, be in as good operating condition, and meet the return conditions provided herein (including the incorporation of all airworthiness directives and alert service bulletins which Lessee is required to effect under this Lease, and equivalent modification status, service bulletins status, and overall condition, and no greater number of accumulated flight hours, cycles, and time since last complete engine refurbishment, as the Engine that should have been returned, assuming such Engine which should have been returned was in the condition and repair as required by the terms hereof immediately prior to such required return); and (ii) analysis if the reason therefor is that an Event of trend data; Loss has occurred to such Engine, such engine shall be free and clear of Liens, suitable for use on such Airframe and shall have a value and utility at least equal to, be in as good operating condition, and meet the return conditions provided herein (iii) SLOATL assessment or minimum including the incorporation of all airworthiness directives and alert service bulletins which Lessee is required to effect under this Lease, and equivalent modification status, service bulletins status, and overall condition, and no greater number of accumulated flight hours, cycles, and time since last [***] qualifying flights (excluding complete engine refurbishment, as the first flight of Engine that should have been returned, assuming such Engine which should have been returned was in 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 applicablecondition and repair as required by terms hereof immediately prior to such required return); and , in either case, Lessee shall, at its own expense and concurrently with such delivery, furnish Lessor with a xxxx of sale, in form and substance reasonably satisfactory to Lessor, for each such engine and with evidence of Lessee’s title to such engine (viiincluding, if requested, an opinion of Lessee’s counsel) and take such other action as Lessor may reasonably request in accordance order that title to such engine shall be duly and properly vested in Lessor. Upon full compliance with manufacturer’s maintenance manual. (b) Following the demonstration flight provided this Section 5 and passage of title to such engine to Lessor, such engine shall be an Engine for by Section 2 all purposes of this Appendix GLease and Lessor shall transfer, each or cause to be transferred, to Lessee all Lessor’s right, title and interest in an Engine has just completed constituting part of the Aircraft so returned but not installed on such Aircraft at the Delivery Location time of such return, without any representation, warranty or recourse of any kind whatsoever, express or implied, except a complete video borescope inspection of all Engine gas path modules (warranty 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 such Engine is on “watch” for any reason requiring any special free and clear of Liens which result from the Lessor’s own acts or out of sequence inspection. Each Engine complies with omissions or from claims against the operations specification of the previous operator without waiver Lessor not to be paid 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 indemnified against by the State of Design of Lessee hereunder or not related to the manufacturer;transaction contemplated by this Lease.

Engines. In the event that any Engine does not meet the conditions set forth in Section II (ab) 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 above, for each such Engine Lessee shall pay Lessor an amount equal to the sum of (i) the current estimated cost of the next scheduled "hot section" inspection (including in such estimated cost, all required replacements of life limited parts) multiplied by the fraction wherein the numerator shall be the greater of (A) zero and (B) the remainder of (x) the actual number of operating hours since the previous hot section inspection; , minus (y) 50% of the total operating hours allowable between hot section inspections, and the denominator shall be the total operating hours allowable between hot section inspections, plus (ii) analysis of trend data; (iii) SLOATL assessment or minimum last [***] qualifying flights (excluding for each such Engine, the first flight product of the day); (iv) maximum power assurance ground runs; (v) technical log analysis for a minimum current estimated cost of the next scheduled major overhaul (including in such estimated cost, all required replacements of life limited parts) multiplied by the fraction wherein the numerator shall be the greater of (A) zero and (B) the remainder of (x) the actual number of hours of operation since the previous [***] months major overhaul minus (y) 50% of operation; the total operating hours allowable between major overhauls, and the denominator shall be the total operating hours allowable between major overhauls. Notwithstanding the foregoing, the requirements of Section II (vib)(i) previous shop visit assessment (if applicable); and (vii) in accordance with manufacturer’s maintenance manual. above and the final sentence of Section II (b) Following above (but solely with respect to the demonstration flight Engines) shall be deemed to have been satisfied if at the time of return of the Engines (x) the Engines being returned to Lessor shall be covered by a service and maintenance contract in form and substance satisfactory to Lessor which provides for the maintenance and/or overhaul of the Engines ("Maintenance Contract"), (y) either (i) adequate reserves for future required maintenance and/or overhaul shall have been provided for by Section 2 of this Appendix G, each Engine has just completed at the Delivery Location a complete video borescope inspection of pursuant to such Maintenance Contract or (ii) all Engine gas path modules (that inspection performed at Sublessor’s expense) amounts due and a power assurance run (performed at Sublessor’s expense) in accordance with Manufacturer’s maintenance manual, in each case Sublessor payable pursuant to such Maintenance Contract 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 paid in full through the date of return and (z) the entity which provides the maintenance and/or overhaul services under such Maintenance shall have provided a DVD either (i) recognize the transfer by Lessee to Lessor of the rights and interests of Lessor (or other electronic mediaits designee) under such Maintenance Contract or (ii) acknowledge the rights and interests of the borescope inspections it had performed to Sublessee. No Engine is on “watch” for any reason requiring any special Lessor (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; (cits designee) 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;under such Maintenance Contract.

Engines. Each Engine will be installed on the Aircraft and will be accompanied by all documentation Lessor may require to evidence that title thereto is properly vested in Lessor and: (a) Each Engine is installed on the Aircraft and has not each life limited part within each Engine will have no less than Minimum Engine Flight Hours and Minimum Engine Cycles expected life 50% of the hours or cycles remaining to until the next expected removal. The expected scheduled 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 limited part replacement as such Engine 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 manualpart had on delivery. (b) Following the demonstration flight provided for by Section 2 of this Appendix GEach Engine will, each Engine has just completed at the Delivery Location Lessor's option and expense, have had a complete hot (including combustion chamber) and cold section video borescope inspection of all Engine gas path modules (that inspection performed at Sublessor’s expense) boroscope inspection, 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 's maintenance manual and all items beyond such manufacturer's limits have been corrected will be repaired at Sublessor’s Lessee's expense. Sublessor shall have provided a DVD (or other electronic media) of the borescope inspections it had performed to Sublessee. No Engine is will be "on “watch” " for any reason requiring any special or out of sequence inspection. Each . (a) above, if Lessee wishes to redeliver an Engine complies to Lessor with less life so remaining, Lessee shall give written notice to Lessor no later than sixty (60) days prior to the operations specification Expiration Date, and: (i) Lessor may, at its sole option, accept or reject such nonconforming delivery by requiring Lessee to perform a premature Hot Section Refurbishment Inspection and shop visit and utilize the Engine Maintenance Reserves (if such work qualifies for contribution by Lessor pursuant to Section 7.2) held by Lessor under the Lease; or (ii) At Lessee's sole option, if Lessor agrees to accept such nonconforming redelivery, Lessor shall accept redelivery 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 Engines 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 such condition with an ultimate life which cannot be restored through appropriate maintenance approved by the State of Design of the manufacturer;additional payment (in addition to Maintenance Reserves otherwise payable per Engine)

Engines. Each Engine will: (a) Each Engine is installed on the Aircraft and has have not less than the 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 removal 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 each 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 LLPs 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 release life remaining. The expected life remaining will be determined by the inspection and checks accomplished by Lessor in accordance with the Lease; (b) be free of all Security Interests, other than Security Interests granted by Lessor; (c) have undergone the inspections as set forth in Section 1.1(b) and (c) herein. If any inspection procedure identifies any Engine defect(s), Lessee will immediately notify Lessor in writing, correct such defect(s) at Lessee’s cost and provide evidence satisfactory to Lessor that defects have been corrected in accordance with the EMM and the Maintenance Program; (d) be prepared for shipment by (i) capping and plugging all openings, (ii) preserving the Engine for 90 days or more storage and (iii) otherwise preparing the Engine for shipment in accordance with Manufacturer’s recommendations; (e) be zero time since the last complete hot and cold section video borescope inspection in accordance with Manufacturer’s and the Related Airframe manufacturer’s then current limitations for maintenance manual and will be in compliance with requirements of the part number in questionEMM, Lessee’s operations specifications, and is supported by certification documentation necessary to demonstrate Back-To-Birth Traceability; for this purposethe requirements and recommendations of the Air Authority; (f) together with installed components, “Life Limited Part” means a component with an ultimate life which cannot be restored through appropriate subject to any reduced frequency inspections in comparison to the Related Airframe manufacturer’s maintenance approved by manual limits; (g) immediately prior to redelivery, will have the State of Design required EGT Margin. In addition, the EGT Margin shall be sufficient, and the Engine shall otherwise be in a condition, to permit the operation of the Engine for at least the Minimum Engine Flight Hours and the Minimum Engine Cycles until its next expected Engine Refurbishment. The Engine shall have performance characteristics consistent with engines of a similar manufacturer, made, model, thrust, age and time since performance restoration and, if (i) fresh from an Engine Refurbishment, be zero time since a full parameter test cell run which will demonstrate, including at full take-off power, performance characteristics consistent with Lessee’s approved Related Airframe operating requirements, or (ii) the Engine has been removed from an aircraft immediately prior to redelivery, will have performed a full parameter test cell run or on-wing maximum power assurance run, at Lessor’s election, demonstrating maximum permitted power take-off performance as per Lessee’s Related Airframe operating requirement. In all cases, the engine condition monitoring (ECM) data will be available for Lessor’s review, will cover periods of installation sufficient to have initialized a baseline on the trend plot and will exhibit no abnormal trends or acceleration in the deterioration of the performance of the Engine; (h) Lessee will bear all costs of packaging, including the provision of an engine shipping stand, transportation, including the return of the engine stand to Lessee (if applicable), insurance duties, taxes and other costs associated with the return of the Engine, Delivered Duty Paid (Incoterms 2000) to the Redelivery Location. Any vehicles and trailers used for shipment of the Engine shall be air ride equipped. On a given shipment, such vehicle shall be dedicated to the Engine belonging solely to Lessor; except, that (i) the Engine or other related equipment may be off-loaded at the Redelivery Location without disturbing any of the additional items included in such shipment; and (ii) Lessee shall not handle or reposition any of the additional items included in such shipment on such vehicle; (i) have no defect which places less than the Engine Flight Hours Restriction and the Engine Cycles Restriction of remaining life, each including in respect of LLPs, pursuant to Manufacturer’s or Air Authority’s requirements until removal.

Engines. In the event that any Engine does not meet the conditions set forth in Section II (ab) 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 above, for each such Engine Lessee shall pay Lessor an amount equal to the sum of (i) the current estimated cost of the next scheduled “hot section” inspection (including in such estimated cost, all required replacements of life limited parts) multiplied by the fraction wherein the numerator shall be the greater of (A) zero and (B) the remainder of (x) the actual number of operating hours since the previous hot section inspection; , minus (y) 50% of the total operating hours allowable between hot section inspections, and the denominator shall be the total operating hours allowable between hot section inspections, plus (ii) analysis of trend data; (iii) SLOATL assessment or minimum last [***] qualifying flights (excluding for each such Engine, the first flight product of the day); (iv) maximum power assurance ground runs; (v) technical log analysis for a minimum current estimated cost of the next scheduled major overhaul (including in such estimated cost, all required replacements of life limited parts) multiplied by the fraction wherein the numerator shall be the greater of (A) zero and (B) the remainder of (x) the actual number of hours of operation since the previous [***] months major overhaul minus (y) 50% of operation; the total operating hours allowable between major overhauls, and the denominator shall be the total operating hours allowable between major overhauls. Notwithstanding the foregoing, the requirements of Section II (vib)(i) previous shop visit assessment (if applicable); and (vii) in accordance with manufacturer’s maintenance manual. above and the final sentence of Section II (b) Following above (but solely with respect to the demonstration flight Engines) shall be deemed to have been satisfied if at the time of return of the Engines (x) the Engines being returned to Lessor shall be covered by a service and maintenance contract in form and substance satisfactory to Lessor which provides for the maintenance and/or overhaul of the Engines (“Maintenance Contract”), (y) either (i) adequate reserves for future required maintenance and/or overhaul shall have been provided for by Section 2 of this Appendix G, each Engine has just completed at the Delivery Location a complete video borescope inspection of pursuant to such Maintenance Contract or (ii) all Engine gas path modules (that inspection performed at Sublessor’s expense) amounts due and a power assurance run (performed at Sublessor’s expense) in accordance with Manufacturer’s maintenance manual, in each case Sublessor payable pursuant to such Maintenance Contract 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 paid in full through the date of return and (z) the entity which provides the maintenance and/or overhaul services under such Maintenance shall have provided a DVD either (i) recognize the transfer by Lessee to Lessor of the rights and interests of Lessor (or other electronic mediaits designee) under such Maintenance Contract or (ii) acknowledge the rights and interests of the borescope inspections it had performed to Sublessee. No Engine is on “watch” for any reason requiring any special Lessor (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; (cits designee) 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;under such Maintenance Contract.