Common use of Engines Clause in Contracts

Engines. (a) Each Engine (or a Replacement Engine as and to the extent permitted by Section 1.2(b)) will be installed on the Aircraft and comply with the following: If the Aircraft Lease Agreement specifies Minimum Engine Flight Hours and/or Minimum Engine Cycles and/or Minimum Engine LLP Cycles, each Engine will have not less than the Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts shall have 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 which shall include the following: (i) full borescope inspection; (ii) analysis of trend data; (iii) sea level outside air temperature limit assessment if recommended by the Manufacturer as an appropriate means to determine engine condition (e.g., CFM 56 test CESM 15); (iv) maximum power assurance ground runs; (v) technical log analysis for a minimum of the previous three (3) months' of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to the manufacturer's maintenance manual; (b) Following the demonstration flight provided for by Section 1.1(d) of this Schedule 6 each Engine shall have just accomplished at the Redelivery Location a complete video borescope inspection of all Engine gas path modules, which inspection shall be performed at Lessor's expense, and a power assurance run performed at Lessee's expense in accordance with the Lessee's Maintenance Program or Manufacturer's maintenance manual and any defects discovered in such inspections which exceed the Engine manufacturer's in-service limits shall be corrected at Lessee's expense. Lessee shall cause such borescope inspections to be performed and to be recorded on videotape by an agency selected by Lessor and shall provide Lessor with a copy of such videotape on the Return Occasion. No Engine shall be on "watch" for any reason requiring any special or out of sequence inspection. Each such Engine shall comply with the operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer's in-service limits shall be repaired; (c) If the Aircraft Lease Agreement specifies Minimum Engine LLP Cycles, each Engine Life-Limited Part will have 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 will be 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 and "Back-to-Birth Traceability" means certified documentation necessary to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Life Limited Part occurred since such Engine Life-Limited Part was new;

Engines. (a) Each Engine (or a Replacement Engine as and to the extent permitted by Section 1.2(b)) will be installed on the Aircraft and comply with the following: If the Aircraft Lease Agreement specifies Minimum Engine Flight Hours and/or Minimum Engine Cycles and/or Minimum Engine LLP Cycles, each Engine will have not less than the Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts shall have not less than the Minimum Engine LLP Cycles release life remainingremoval. The expected life remaining will be determined by the inspection and checks accomplished by Lessor Sublessor in accordance with the Lease which shall include the followingSublease including: (i) full borescope inspection; (ii) analysis of trend data; (iii) sea level outside air temperature limit assessment if recommended by or minimum last [***] qualifying flights (excluding the Manufacturer as an appropriate means to determine engine condition (e.g., CFM 56 test CESM 15first flight of the day); (iv) maximum power assurance ground runs; (v) technical log analysis for a minimum of the previous three (3) months' [***] months of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to the manufacturer's ’s maintenance manual; (b) Following the demonstration flight provided for by Section 1.1(d) 18.6 of this Schedule 6 the Sublease, each Engine shall have just accomplished at the Redelivery Return Location a complete video borescope inspection of all Engine gas path modules, which inspection shall be performed at Lessor's Sublessor’s expense, and a power assurance run performed at Lessee's Sublessee’s expense in accordance with the Lessee's Maintenance Program or Manufacturer's ’s maintenance manual and any defects discrepancies discovered in such inspections which exceed the Engine manufacturer's ’s in-service limits shall be corrected at Lessee's Sublessee’s expense. Lessee Sublessee shall cause such borescope inspections to be performed and to be recorded on videotape by an agency selected by Lessor Sublessor and shall provide Lessor Sublessor with a copy of such videotape on the Return OccasionReturn. No Engine shall be on "“watch" ” for any reason requiring any special or out of sequence inspection. Each such Engine shall comply with the operations specification of Lessee Sublessee without waiver or exceptions. All items beyond the Engine manufacturer's ’s in-service limits shall be repaired; (c) If the Aircraft Lease Agreement specifies Minimum Engine LLP Cycles, each Each Engine Life-Limited Part will have not less than the Minimum Engine LLP Cycles remaining in accordance with the manufacturer's ’s then current limitations for the part number in question, and will be supported by certification documentation necessary to demonstrate Back-toTo-Birth Traceabilitytraceability; for this purpose "purpose, “Life Limited Part" ” means a component with an ultimate life which cannot be restored through appropriate maintenance approved by the State state of Design design of the manufacturer and "Back-to-Birth Traceability" means certified documentation necessary to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Life Limited Part occurred since such Engine Life-Limited Part was newmanufacturer;

Engines. (a) Each Engine (or a Replacement Engine as and to the extent permitted by Section 1.2(b)) will be installed on the Aircraft and will comply with the following: If the Aircraft Lease Agreement specifies Minimum Engine Flight Hours and/or Minimum Engine Cycles and/or Minimum Engine LLP Cycles, each Engine will have not less than the Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts shall have 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 which shall include the following: (a) Each Engine (i) full borescope inspection; (ii) analysis of trend data; (iii) sea level outside air temperature limit assessment if recommended by the Manufacturer as an appropriate means to determine engine condition (e.g., CFM 56 test CESM 15); (iv) maximum power assurance ground runs; (v) technical log analysis for a minimum of the previous three (3) months' of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to the manufacturer's maintenance manual; (b) Following the demonstration flight provided for by Section 1.1(d) of this Schedule 6 each Engine shall have just accomplished at the Redelivery Location a complete video borescope inspection of all Engine gas path modules, which inspection shall be performed at Lessor's expense, and a power assurance run performed at Lessee's expense been maintained in accordance with the Lessee's Maintenance Program Program; (ii) 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) shall be free and clear of all Liens arising by act or omission of, or suffered to exist by, Lessee; and (iv) shall contain the same Parts (or substitutes or replacements therefor, as provided in the Aircraft Lease Agree ment) as initially delivered to Lessee. (b) If, at the end of the Term, the Engines are subject to an "Engine Maintenance Agreement" (as defined by the Aircraft Lease Agree ment), and such Engine Maintenance Agreement has been effectively assigned to Lessor, Lessee shall return each Engine in such condition as shall make such Engine eligible for continued maintenance under the Engine Maintenance Agreement. If, at the 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 minimum of half-time until the next scheduled overhaul, based on the Engine Manufacturer's maintenance manual 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 of each Engine shall be conducted by a qualified technician acceptable to Lessor, at Lessor's expense and in the presence of Lessor's designated technical representative. Any defects discovered in each such inspections inspection which exceed the Engine manufacturerManufacturer's in-service limits shall be corrected at by Lessee's expense. Lessee shall cause such borescope inspections , prior to be performed and to be recorded on videotape by an agency selected by Lessor and shall provide Lessor with a copy of such videotape on the Return Occasion. No Engine shall be on "watch" for any reason requiring any special or out of sequence inspection. Each such Engine shall comply with the operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer's in-service limits shall be repaired; (c) If the Aircraft Lease Agreement specifies Minimum Engine LLP Cycles, each Engine Life-Limited Part will have 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 will be 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 and "Back-to-Birth Traceability" means certified documentation necessary Aircraft, at no cost to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Life Limited Part occurred since such Engine Life-Limited Part was new;Lessor.

Engines. (a) Each Engine (or a Replacement Engine as and to the extent permitted by Section 1.2(b)) will be is installed on the Aircraft and comply with the following: If the Aircraft Lease Agreement specifies Minimum Engine Flight Hours and/or Minimum Engine Cycles and/or Minimum Engine LLP Cycles, each Engine will have has not less than the Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts shall have not less than the Minimum Engine LLP Cycles release life remainingremoval. The expected life remaining will is to be determined by the inspection and checks accomplished by Lessor in accordance with the Lease which shall include the followingbefore Delivery taking account, where available, of: (i) full borescope inspection; (ii) analysis of trend data; (iii) sea level outside air temperature limit SLOATL assessment if recommended by or minimum last [***] qualifying flights (excluding the Manufacturer as an appropriate means to determine engine condition (e.g., CFM 56 test CESM 15first flight of the day); (iv) maximum power assurance ground runs; (v) technical log analysis for a minimum of the previous three (3) months' [***] months of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to the in accordance with manufacturer's ’s maintenance manual;. (b) Following the demonstration flight provided for by Section 1.1(d) 2 of this Schedule 6 Appendix G, each Engine shall have has just accomplished completed at the Redelivery Delivery Location a complete video borescope inspection of all Engine gas path modules, which modules (that inspection shall be performed at Lessor's Sublessor’s expense, ) and a power assurance run (performed at Lessee's expense 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 Lessee's Maintenance Program or Manufacturer's maintenance manual and any defects inspections. Any Discrepancies discovered in such inspections which exceed exceeding the Engine manufacturer's ’s in-service limits shall be have been corrected at Lessee's Sublessor’s expense. Lessee Sublessor shall cause such have provided a DVD (or other electronic media) of the borescope inspections it had performed to be performed and to be recorded on videotape by an agency selected by Lessor and shall provide Lessor with a copy of such videotape on the Return OccasionSublessee. No Engine shall be is on "“watch" ” for any reason requiring any special or out of sequence inspection. Each such Engine shall comply complies with the operations specification of Lessee the previous operator without waiver or exceptions. All exceptions and there being no items beyond the Engine manufacturer's ’s in-service limits shall be repairedlimits; (c) If the Aircraft Lease Agreement specifies Minimum Engine LLP Cycles, each Each Engine Life-Limited Part will have has not less than the Minimum Engine LLP Cycles remaining in accordance with the manufacturer's ’s then current limitations for the part number in question, and will be is supported by certification documentation necessary to demonstrate Back-toTo-Birth Traceability; for this purpose "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 and "Back-to-Birth Traceability" means certified documentation necessary to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Life Limited Part occurred since such Engine Life-Limited Part was newmanufacturer;

Engines. (a) Each Engine (or a Replacement Engine as and to the extent permitted by Section 1.2(b)) will be installed on the Aircraft and comply with the following: : (a) If the Aircraft Lease Agreement specifies a Minimum Engine Flight Hours and/or Minimum Engine Cycles and/or Minimum Engine LLP Cycles, each Engine will have not less than the Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts shall have not less than the Minimum Engine LLP Cycles release life remainingremoval. The expected life remaining will be determined by third party mutually acceptable to both Lessor and Lessee (at Lessor's cost) or by the Engine Manufacturer, in each case based on the inspection and checks accomplished by Lessor to be performed at the Return Occasion in accordance with the Lease which shall include the following: (i) full borescope inspection; (ii) analysis of trend data; (iii) sea level outside air temperature limit assessment if recommended by the Manufacturer as an appropriate means to determine engine condition (e.g., CFM 56 test CESM 15); (iv) maximum power assurance ground runs; (v) technical log analysis for a minimum of the previous three (3) months' of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to the manufacturer's maintenance manualLease; (b) Following the demonstration flight provided for by Section 1.1(d) of this Schedule 6 each Each Engine shall have just accomplished completed at the Redelivery Location location for Lessor's acceptance on the Return Occasion a complete hot (including combustion chamber) and cold section video borescope inspection of all Engine gas path modulesinspection, which inspection shall be performed at Lessor's expense, and a power assurance run performed at Lessee's expense in accordance with the Lessee's Maintenance Program or Manufacturer's maintenance manual Maintenance Planning Document and any defects discovered in such inspections which exceed the Engine manufacturer's in-service limits shall be corrected at Lessee's expense. Lessee shall cause such borescope inspections to be performed and to be recorded on videotape by an agency selected by Lessor and shall provide Lessor with a copy of such videotape on the Return Occasion. No Engine shall be on "watch" for any reason requiring any special or out of sequence inspection. Each such Engine shall comply with the operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer's in-service limits shall be repaired; (c) If the Aircraft Lease Agreement specifies Minimum Engine LLP Component Cycles, each Engine Life-Limited Part Component will have not less than the Minimum Engine LLP Component Cycles remaining in accordance with per the manufacturer's then current limitations for the part number in question, and will be 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 and "Back-to-Birth Traceability" means certified documentation necessary to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Life Limited Part occurred since such Engine Life-Limited Part was new;part

Engines. (a) Each Engine (or a Replacement Engine as and to the extent permitted by Section 1.2(b)) will be installed on the Aircraft and comply with the following: If the Aircraft Lease Agreement specifies Minimum Engine Flight Hours and/or Minimum Engine Cycles and/or Minimum Engine LLP Cycles, each Each Engine will have not less than the Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts shall have 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 which shall include the following: (i1) full borescope inspection; (ii2) analysis of trend data; (iii3) sea level outside air temperature limit assessment if recommended by or minimum last (10) qualifying flights (excluding the Manufacturer as an appropriate means to determine engine condition (e.g., CFM 56 test CESM 15first flight of the day); (iv4) maximum power assurance ground runsa test cell run; (v5) technical log analysis for a minimum of the previous three (3) 3 months' ’ of operation; (vi6) previous shop visit assessment (if applicable); and (vii7) reference to the manufacturer's maintenance manual;Lessee’s Maintenance Program. (b) Following the demonstration flight The Final Inspection provided for by Section 1.1(d) 1.1 of this Schedule 6 shall be completed, and as part of such Final Inspection, each Engine shall have just accomplished at the Redelivery Location a complete video borescope inspection of all Engine gas path modules, which inspection shall be performed at Lessor's ’s expense, and a power assurance test cell run performed at Lessee's ’s expense in accordance with the Lessee's ’s Maintenance Program or Manufacturer's ’s maintenance manual and any defects discovered in such inspections which exceed the Engine manufacturer's ’s in-service limits shall be corrected at Lessee's ’s expense. Lessee shall cause such borescope inspections to be performed and to be recorded on videotape by an agency selected by Lessor and shall provide Lessor with a copy of such videotape on the Return Occasion. No Engine shall be on "“watch" ” for any reason requiring any special or out of sequence inspection. Each such Engine shall comply with the operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer's ’s in-service limits shall be repaired;. (c) If the Aircraft Lease Agreement specifies Minimum Engine LLP Cycles, each Each Engine Life-Limited Part will have not less than the Minimum Engine LLP Cycles remaining in accordance with the manufacturer's ’s then current limitations for the part number in question, and will be supported by certification documentation necessary to demonstrate Backback-to-Birth Traceabilitybirth 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 and "Back-to-Birth Traceability" means certified documentation necessary to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Life Limited Part occurred since such Engine Life-Limited Part was new;manufacturer.

Engines. (a) Each Engine (or a Replacement Engine as and to the extent permitted by Section 1.2(b)) will be installed on the Aircraft and comply with the following: If the Aircraft Lease Agreement specifies Minimum Engine Flight Hours and/or Minimum Engine Cycles and/or Minimum Engine LLP Cycles, each Engine will have not less than the Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts shall have 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 which shall include the following: (i) full borescope inspection; (ii) analysis of trend data; (iii) sea level outside air temperature limit assessment if recommended by the Manufacturer as an appropriate means to determine engine condition (e.g., CFM 56 test CESM 15); (iv) maximum power assurance ground runs; (v) technical log analysis for a minimum of the previous three (3) months' ’ of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to the manufacturer's ’s maintenance manual; (b) Following the demonstration flight provided for by Section 1.1(d) of this Schedule 6 each Engine shall have just accomplished at the Redelivery Location a complete video borescope inspection of all Engine gas path modules, which inspection shall be performed at Lessor's ’s expense, and a power assurance run performed at Lessee's ’s expense in accordance with the Lessee's ’s Maintenance Program or Manufacturer's ’s maintenance manual and any defects discovered in such inspections which exceed the Engine manufacturer's ’s in-service limits shall be corrected at Lessee's ’s expense. Lessee shall cause such borescope inspections to be performed and to be recorded on videotape by an agency selected by Lessor and shall provide Lessor with a copy of such videotape on the Return Occasion. No Engine shall be on "“watch" ” for any reason requiring any special or out of sequence inspection. Each such Engine shall comply with the operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer's ’s in-service limits shall be repaired; (c) If the Aircraft Lease Agreement specifies Minimum Engine LLP Cycles, each Engine Life-Limited Part will have not less than the Minimum Engine LLP Cycles remaining in accordance with the manufacturer's ’s then current limitations for the part number in question, and will be 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 and "“Back-to-Birth Traceability" ” means certified documentation necessary to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Life Limited Part occurred since such Engine Life-Limited Part was new;

Engines. (a) Each Engine (or a Replacement Engine as and to the extent permitted by Section Clause 1.2(b)) will be installed on the Aircraft and comply with the following: If the Aircraft Lease Agreement specifies Minimum Engine Flight Hours and/or Minimum Engine Cycles and/or Minimum Engine LLP Cycles, each : (i) Each Engine will have not less than the Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts shall have not less than the Minimum Engine LLP Cycles release life remainingremoval. The expected life remaining will be determined by the inspection and checks accomplished by Lessor in accordance with the Lease which shall include the followingas listed below: (iii) full borescope inspection; (ii) analysis of trend data; (iii) sea level outside air temperature limit assessment if recommended by the Manufacturer as an appropriate means to determine engine condition (e.g., CFM 56 test CESM 15)monitoring sage data; (iv) maximum power assurance OATL assessment or minimum last ten (10) Flight Hours; (v) ground runs; (vvi) technical log analysis for a minimum of the previous three (3) months' of operation;analysis; and 07c043 CTA (vivii) previous shop visit assessment (if applicable); and (vii) reference to the manufacturer's maintenance manual; (b) Following the demonstration flight provided for by Section 1.1(d) of this Schedule 6 each Each Engine shall have just accomplished completed at the Redelivery Location a complete hot (including combustion chamber) and cold section video borescope inspection of all Engine gas path modulesinspection, which inspection shall be performed at Lessor's ’s expense, and a power assurance run performed at Lessee's ’s expense in accordance with the Lessee's ’s Maintenance Program or Manufacturer's ’s maintenance manual and any defects discovered in such inspections which exceed the Engine manufacturer's ’s in-service limits shall be corrected at Lessee's ’s expense. Lessee shall cause such borescope inspections to be performed and to be recorded on videotape by an agency selected by Lessor and shall provide Lessor with a copy of such videotape on the Return Occasion. No Engine shall be on "“watch" ” for any reason requiring any special or out of sequence inspection. Each such Engine shall comply with the operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer's ’s in-service limits shall be repaired; (c) If the Aircraft Lease Agreement specifies Minimum Engine LLP Cycles, each Each Engine Life-Limited Part will have not less than the Minimum Engine LLP Cycles remaining in accordance with per the manufacturer's ’s then current limitations for the part number in question, and will be supported by certification documentation necessary to demonstrate Backback-to-Birth Traceabilitybirth 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 and "Back-to-Birth Traceability" means certified documentation necessary to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Life Limited Part occurred since such Engine Life-Limited Part was new;maintenance; and

Engines. (a) Each Engine (or a Replacement Engine as and to the extent permitted by Section 1.2(b)) will be installed on the Aircraft and comply with the following: : (a) If the Aircraft Lease Agreement specifies a Minimum Engine Flight Hours and/or Minimum Engine Cycles and/or Minimum Engine LLP Cycles, each Engine will have not less than the Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts shall have not less than the Minimum Engine LLP Cycles release life remainingscheduled removal. The expected life remaining will be determined by third party mutually acceptable to both Lessor and Lessee (at Lessor's cost) or by the Engine Manufacturer, in each case based on the inspection and checks accomplished by Lessor to be performed at the Return Occasion in accordance with the Lease which shall include the following: (i) full borescope inspection; (ii) analysis of trend data; (iii) sea level outside air temperature limit assessment if recommended by the Manufacturer as an appropriate means to determine engine condition (e.g., CFM 56 test CESM 15); (iv) maximum power assurance ground runs; (v) technical log analysis for a minimum of the previous three (3) months' of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to the manufacturer's maintenance manualLease; (b) Following the demonstration flight provided for by Section 1.1(d) of this Schedule 6 each Each Engine shall have just accomplished completed at the Redelivery Location location for Lessor's acceptance on the Return Occasion a complete hot (including combustion chamber) and cold section video borescope inspection of all Engine gas path modulesinspection, which inspection shall be performed at Lessor's expense, and a power assurance run performed at Lessee's expense in accordance with the Lessee's Maintenance Program or Manufacturer's maintenance manual Maintenance Planning Document and any defects discovered in such inspections which exceed the Engine manufacturer's in-service limits shall be corrected at Lessee's expense. Lessee shall cause such borescope inspections to be performed and to be recorded on videotape by an agency selected by Lessor and shall provide Lessor with a copy of such videotape on the Return Occasion. No Engine shall be on "watch" for any reason reason, requiring any special or out of sequence inspection. Each such Engine shall comply with the operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer's in-service limits shall be repaired; (c) If the Aircraft Lease Agreement specifies Minimum Engine LLP Component Cycles, each Engine Life-Limited Part Component will have not less than the Minimum Engine LLP Component Cycles remaining in accordance with per the manufacturer's then current limitations for the part number in question, and will be supported by certification documentation necessary to demonstrate Backback-to-Birth Traceabilitybirth traceability; for this purpose "Life Engine Life-Limited PartComponent" means a component with an ultimate life which cannot be restored through appropriate maintenance approved by the State of Design of the manufacturer and "Back-to-Birth Traceability" means certified documentation necessary to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Life Limited Part occurred since such Engine Life-Limited Part was new;maintenance; and

Engines. (ai) Each Engine (or a Replacement Engine as and to the extent permitted by Section 1.2(b)) will be installed on the Aircraft and comply with the following: If the Aircraft Lease Agreement specifies a Minimum Engine Flight Hours and/or Minimum Engine Cycles and/or Minimum Engine LLP Cycles, each Engine will have not less than the Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts parts shall have 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 Lessee in accordance with the Lease which shall include the following:following (historic data to the extent that it is available): (i) full borescope inspection; (ii) analysis of trend data; (iii) sea level outside air temperature limit assessment if recommended by the Manufacturer engine manufacturer as an appropriate means to determine engine condition (e.g., e.g. CFM 56 test CESM 15); (iv) maximum power assurance ground runs; (v) technical log analysis for a minimum of the previous three (3) months' preceding 3 months of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to the manufacturer's manufacturers maintenance manual;. (bii) Following the demonstration flight provided for by Section 1.1(d2.2(a)(d) of this Schedule 6 4, Part 2, each Engine shall have just accomplished at the Redelivery Delivery Location a complete video borescope inspection of all Engine gas path modules, which inspection shall be performed at Lessor's expense, and a power assurance run performed at LesseeLessor's expense in accordance with the Lessee's Maintenance Program or Manufacturer's maintenance manual and any defects discovered in such inspections which exceed the Engine manufacturer's in-service limits shall be corrected at LesseeLessor's expense. Lessee Lessor shall cause such borescope inspections to be performed and to be recorded on videotape by an agency selected by mutually acceptable to Lessor and Lessee and Lessor shall provide Lessor Lessee with a copy of such videotape on the Return OccasionDelivery Date. No Engine shall be on "watch" for any reason requiring any special or out of sequence inspection. Each such Engine shall comply with the operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer's in-service limits shall be repaired; (ciii) If the Aircraft Lease Agreement specifies Minimum Engine LLP Cycles, each Engine Life-Limited Part will have 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 will be supported by certification documentation necessary to demonstrate Back-toTo-Birth Traceabilitytraceability; 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 and "Back-toTo-Birth Traceability" means certified documentation necessary to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Life Limited Part occurred since such Engine Life-Limited Part was new;

Engines. (a) Each Engine (or a Replacement Engine as and to the extent permitted by Section 1.2(b)) will be installed on the Aircraft and comply with the following: : (a) If the Aircraft Lease Agreement specifies a Minimum Engine Flight Hours and/or Minimum Engine Cycles and/or Minimum Engine LLP Cycles, each Engine will have not less than the Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts shall have not less than the Minimum Engine LLP Cycles release life remainingremoval. The expected life remaining will be determined by third party mutually acceptable to both Lessor and Lessee (at Lessor's cost) or by the Engine Manufacturer, in each case based on the inspection and checks accomplished by Lessor to be performed at the Return Occasion in accordance with the Lease which shall include the following: (i) full borescope inspection; (ii) analysis of trend data; (iii) sea level outside air temperature limit assessment if recommended by the Manufacturer as an appropriate means to determine engine condition (e.g., CFM 56 test CESM 15); (iv) maximum power assurance ground runs; (v) technical log analysis for a minimum of the previous three (3) months' of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to the manufacturer's maintenance manualLease; (b) Following the demonstration flight provided for by Section 1.1(d) of this Schedule 6 each Each Engine shall have just accomplished completed at the Redelivery Location location for Lessor's acceptance on the Return Occasion a complete hot (including combustion chamber) and cold section video borescope inspection of all Engine gas path modulesinspection, which inspection shall be performed at Lessor's expense, and a power assurance run performed at Lessee's expense in accordance with the Lessee's Maintenance Program or Manufacturer's maintenance manual Maintenance Planning Document and any defects discovered in such inspections which exceed the Engine manufacturer's in-service limits shall be corrected at Lessee's expense. Lessee shall cause such borescope inspections to be performed and to be recorded on videotape by an agency selected by Lessor and shall provide Lessor with a copy of such videotape on the Return Occasion. No Engine shall be on "watch" for any reason requiring any special or out of sequence inspection. Each such Engine shall comply with the operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer's in-service limits shall be repaired; (c) If the Aircraft Lease Agreement specifies Minimum Engine LLP Component Cycles, each Engine Life-Limited Part Component will have not less than the Minimum Engine LLP Component Cycles remaining in accordance with per the manufacturer's then current limitations for the part number in question, and will be supported by certification documentation necessary to demonstrate Backback-to-Birth Traceabilitybirth traceability; for this purpose "Life Engine Life-Limited PartComponent" means a component with an ultimate life which cannot be restored through appropriate maintenance approved by the State of Design of the manufacturer and "Back-to-Birth Traceability" means certified documentation necessary to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Life Limited Part occurred since such Engine Life-Limited Part was new;maintenance; and

Engines. (a) Each Engine (or a Replacement Engine as and to the extent permitted by Section 1.2(b)) will be installed on the Aircraft and comply with the following: : (a) If the Aircraft Lease Agreement specifies a Minimum Engine Flight Hours and/or Minimum Engine Cycles and/or Minimum Engine LLP Cycles, each Engine will have not less than the Minimum Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts shall have not less than the Minimum Engine LLP Cycles release life remainingscheduled removal. The expected life remaining will be determined by third party mutually acceptable to both Lessor and Lessee (at Lessor's cost) or by the Engine Manufacturer, in each case based on the inspection and checks accomplished by Lessor to be performed at the Return Occasion in accordance with the Lease which shall include the following: (i) full borescope inspection; (ii) analysis of trend data; (iii) sea level outside air temperature limit assessment if recommended by the Manufacturer as an appropriate means to determine engine condition (e.g., CFM 56 test CESM 15); (iv) maximum power assurance ground runs; (v) technical log analysis for a minimum of the previous three (3) months' of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to the manufacturer's maintenance manualLease; (b) Following the demonstration flight provided for by Section 1.1(d) of this Schedule 6 each Each Engine shall have just accomplished completed at the Redelivery Location location for Lessor's acceptance on the Return Occasion a complete hot (including combustion chamber) and cold section video borescope inspection of all Engine gas path modulesinspection, which inspection shall be performed at Lessor's expense, and a power assurance run performed at Lessee's expense in accordance with the Lessee's Maintenance Program or Manufacturer's maintenance manual Maintenance Planning Document and any defects discovered in such inspections which exceed the Engine manufacturer's in-service limits shall be corrected at Lessee's expense. Lessee shall cause such borescope inspections to be performed and to be recorded on videotape by an agency selected by Lessor and shall provide Lessor with a copy of such videotape on the Return Occasion. No Engine shall be on "watch" for any reason requiring any special or out of sequence inspection. Each such Engine shall comply with the operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer's in-service limits shall be repaired; (c) If the Aircraft Lease Agreement specifies Minimum Engine LLP Component Cycles, each Engine Life-Limited Part Component will have not less than the Minimum Engine LLP Component Cycles remaining in accordance with per the manufacturer's then current limitations for the part number in question, and will be supported by certification documentation necessary to demonstrate Backback-to-Birth Traceabilitybirth traceability; for this purpose "Life Engine Life-Limited PartComponent" means a component with an ultimate life which cannot be restored through appropriate maintenance approved by the State of Design of the manufacturer and "Back-to-Birth Traceability" means certified documentation necessary to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Life Limited Part occurred since such Engine Life-Limited Part was new;maintenance; and