Common use of Engines Clause in Contracts

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. The original (a) Each Engine (or Suitable a Replacement Engine (in case of Total Lossas and to the extent permitted by Section 1.2(b)) is in the configuration as permitted under this Agreement will be installed on the Aircraft shall 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: (ai) have no less than 4,500 Cycles scheduled life remaining in respect full borescope inspection; (ii) analysis of Engine LLPs and no more than 110% 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 Aircraft total Flight Hours and Cycles since new. Engine Life Limited Parts will be supported by certification documentation necessary previous three (3) months' of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to demonstrate traceability back to birth.the manufacturer's maintenance manual; (b) will have accumulated no more than 7,000 Flight Hours and 7,000 Cycles since new or last Engine Performance Restoration shop visit. (cFollowing the demonstration flight provided for by Section 1.1(d) 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 this Schedule 6 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 accomplished at the Redelivery Location on or about the Redelivery Date an all module, hot and cold section a complete video borescope inspection. Lessee will also have just completed in respect of each Engine an inspection of each magnetic chip detectorall Engine gas path modules, laboratory oil sample analysiswhich inspection shall be performed at Lessor's expense, main oil screen and oil a power assurance run performed at Lessee's expense in accordance with the Lessee's Maintenance Program or Manufacturer's maintenance manual and fuel filter inspections. Any any defects discovered in such inspections which exceed the Engine Manufacturer’s 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 Lessee’s expenseReturn Occasion. No Engine shall be “on "watch” " for any reason requiring any special or out of sequence inspection or reduced interval inspectionsinspection. Each such Engine will shall comply with and have been maintained in accordance with the Agreed Maintenance Programme operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer’s 's in-service limits shall be repaired; and; (fc) If the Aircraft Lease Agreement specifies Minimum Engine LLP Cycles, each Engine Life-Limited Part will have trend or condition monitoring data over at least not less than the previous yearMinimum 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; if Engine trend or condition monitoring data indicates for this purpose "Life Limited Part" means a rate component with an ultimate life which cannot be restored through appropriate maintenance approved by the State of acceleration in performance deterioration over at least the previous ninety days, which is higher than normal based on the maintenance experience 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 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.Life-Limited Part was new;

Engines. The original (a) Each Engine or Suitable Replacement Engine (in case of Total Loss) is in the configuration as permitted under this Agreement will be installed on the Aircraft shall comply and will 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 will be determined by the inspection and checks accomplished by Sublessor in accordance with the followingSublease including: (ai) have no less than 4,500 Cycles scheduled life remaining in respect full borescope inspection; (ii) analysis of Engine LLPs and no more than 110% trend data; (iii) sea level outside air temperature limit assessment or minimum last [***] qualifying flights (excluding the first flight of the Aircraft total Flight Hours and Cycles since new. Engine Life Limited Parts will be supported by certification documentation necessary 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) reference to demonstrate traceability back to birth.the manufacturer’s maintenance manual; (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 Following the entire operating envelop demonstration flight provided for by Section 18.6 of the Aircraft as defined in the EASA AFM. Each Sublease, each Engine shall have just accomplished at least 25C sea level hot day EGT margin; (d) the Return Location a complete video borescope inspection of all items beyond Engine gas path modules, which inspection shall be performed at Sublessor’s expense, and a power assurance run performed at Sublessee’s expense in accordance with the Engine Maintenance Program or 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 maintenance manual 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 any discrepancies discovered in such inspections which exceed the Engine Manufacturermanufacturer’s in-service limits shall be corrected at the LesseeSublessee’s expense. Sublessee shall cause such borescope inspections to be performed and to be recorded on videotape by an agency selected by Sublessor and shall provide Sublessor with a copy of such videotape on the Return. No Engine shall be on “on watch” for any reason requiring any special or out of sequence inspection or reduced interval inspectionsinspection. Each such Engine will shall comply with and have been maintained in accordance with the Agreed Maintenance Programme operations specification of Sublessee without waiver or exceptions. All items beyond the Engine manufacturer’s in-service limits shall be repaired; and; (fc) Each Engine Life-Limited Part will have trend or condition monitoring data over at least not less than the previous yearMinimum 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; if Engine trend or condition monitoring data indicates for this purpose, “Life Limited Part” means a rate component with an ultimate life which cannot be restored through appropriate maintenance approved by the state of acceleration in performance deterioration over at least the previous ninety days, which is higher than normal based on the maintenance experience design 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.manufacturer;

Engines. The original (a) Each Engine (or Suitable a Replacement Engine (in case of Total Lossas and to the extent permitted by Section 1.2(b)) is in the configuration as permitted under this Agreement will be installed on the Aircraft shall 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: (ai) have no less than 4,500 Cycles scheduled life remaining in respect full borescope inspection; (ii) analysis of Engine LLPs and no more than 110% 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 Aircraft total Flight Hours and Cycles since new. Engine Life Limited Parts will be supported by certification documentation necessary previous three (3) months’ of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to demonstrate traceability back to birth.the manufacturer’s maintenance manual; (b) will have accumulated no more than 7,000 Flight Hours and 7,000 Cycles since new or last Engine Performance Restoration shop visit. (cFollowing the demonstration flight provided for by Section 1.1(d) 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 this Schedule 6 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 accomplished at the Redelivery Location on or about the Redelivery Date an all module, hot and cold section a complete video borescope inspection. Lessee will also have just completed in respect of each Engine an inspection of each magnetic chip detectorall Engine gas path modules, laboratory oil sample analysiswhich inspection shall be performed at Lessor’s expense, main oil screen and oil a power assurance run performed at Lessee’s expense in accordance with the Lessee’s Maintenance Program or Manufacturer’s maintenance manual and fuel filter inspections. Any any defects discovered in such inspections which exceed the Engine Manufacturermanufacturer’s in-service limits shall be corrected at the 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 “on watch” for any reason requiring any special or out of sequence inspection or reduced interval inspectionsinspection. Each such Engine will shall comply with and have been maintained in accordance with the Agreed Maintenance Programme operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer’s in-service limits shall be repaired; and; (fc) If the Aircraft Lease Agreement specifies Minimum Engine LLP Cycles, each Engine Life-Limited Part will have trend or condition monitoring data over at least not less than the previous yearMinimum 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; if Engine trend or condition monitoring data indicates for this purpose “Life Limited Part” means a rate component with an ultimate life which cannot be restored through appropriate maintenance approved by the State of acceleration in performance deterioration over at least the previous ninety days, which is higher than normal based on the maintenance experience 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 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.Life-Limited Part was new;

Engines. The original (i) Each Engine or Suitable Replacement Engine (in case of Total Loss) is in the configuration as permitted under this Agreement will be installed on the Aircraft shall and comply with the following: (a) : If the Aircraft Lease Agreement specifies a Minimum Engine Flight Hours and/or Minimum Engine Cycles, each Engine will have no not less than 4,500 Cycles scheduled life remaining in respect of the Minimum Engine LLPs and no more than 110% of the Aircraft total Flight Hours and Minimum Engine Cycles since newexpected life remaining to the next expected removal and the life limited parts shall have not less than the Minimum Engine Cycles release life remaining. Engine Life Limited Parts The expected life remaining will be supported determined by certification documentation necessary the inspection and checks accomplished by Lessee in accordance with Lease which shall include the following (historic data to demonstrate traceability back 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 engine manufacturer as an appropriate means to birthdetermine engine condition (e.g. CFM 56 test CESM 15); (iv) maximum power assurance runs; (v) technical log analysis for a minimum of the preceding 3 months of operation; (vi) previous shop visit assessment (if applicable); and (vii) reference to the manufacturers maintenance manual. (bii) will have accumulated no more than 7,000 Flight Hours and 7,000 Cycles since new or last Engine Performance Restoration shop visit. (cFollowing the demonstration flight provided for by Section 2.2(a)(d) 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 this Schedule 4, Part 2, 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 accomplished at the Redelivery Delivery Location on or about the Redelivery Date an all module, hot and cold section a complete video borescope inspection. Lessee will also have just completed in respect of each Engine an inspection of each magnetic chip detectorall Engine gas path modules, laboratory oil sample analysiswhich inspection shall be performed at Lessor's expense, main oil screen and oil a power assurance run performed at Lessor's expense in accordance with the Manufacturer's maintenance manual and fuel filter inspections. Any any defects discovered in such inspections which exceed the Engine Manufacturer’s manufacturer's in-service limits shall be corrected at Lessor's expense. Lessor shall cause such borescope inspections to be performed and to be recorded on videotape by an agency mutually acceptable to Lessor and Lessee and Lessor shall provide Lessee with a copy of such videotape on the Lessee’s expenseDelivery Date. No Engine shall be “on "watch” " for any reason requiring any special or out of sequence inspection or reduced interval inspectionsinspection. Each such Engine will shall comply with and have been maintained in accordance with the Agreed Maintenance Programme operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer’s 's in-service limits shall be repaired; and; (fiii) If the Aircraft Lease Agreement specifies Minimum Engine LLP Cycles, each Engine Life-Limited Part will have trend or condition monitoring data over at least not less than the previous yearMinimum 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; if Engine trend or condition monitoring data indicates for this purpose "Life Limited Part" means a rate component with an ultimate life which cannot be restored through appropriate maintenance approved by the State of acceleration in performance deterioration over at least the previous ninety days, which is higher than normal based on the maintenance experience Design of the Engine Manufacturer 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 operating relation to 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.Life Limited Part occurred since new;

Engines. The original Each Engine (or Suitable a Replacement Engine (in case of Total Lossas and to the extent permitted by Section 1.2(b)) is in the configuration as permitted under this Agreement will be installed on the Aircraft shall and comply with the following: (a) If the Aircraft Lease Agreement specifies a Minimum Engine Flight Hours and/or Minimum Engine Cycles, each Engine will have no not less than 4,500 Cycles scheduled life remaining in respect of the Minimum Engine LLPs and no more than 110% of the Aircraft total Flight Hours and Minimum Engine Cycles since newexpected life remaining to the next scheduled removal. Engine Life Limited Parts The expected life remaining will be supported determined by certification documentation necessary third party mutually acceptable to demonstrate traceability back both Lessor and Lessee (at Lessor's cost) or by the Engine Manufacturer, in each case based on the inspection and checks to birth.be performed at the Return Occasion in accordance with the Lease; (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 location for Lessor's acceptance on or about the Redelivery Date an all module, Return Occasion a hot (including combustion chamber) and cold section video borescope inspection. Lessee will also have just completed , which inspection shall be performed at Lessor's expense, and a power assurance run performed at Lessee's expense in respect of each Engine an inspection of each magnetic chip detector, laboratory oil sample analysis, main oil screen accordance with the Lessee's Maintenance Program or Manufacturer's Maintenance Planning Document and oil and fuel filter inspections. Any any defects discovered in such inspections which exceed the Engine Manufacturer’s 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 Lessee’s expenseReturn Occasion. No Engine shall be “on "watch” " for any reason reason, requiring any special or out of sequence inspection or reduced interval inspectionsinspection. Each such Engine will shall comply with and have been maintained in accordance with the Agreed Maintenance Programme 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 Component Cycles, each Engine Life-Limited Component will have not less than the Minimum Component Cycles remaining 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 "Engine Life-Limited Component" means a component with an ultimate life which cannot be restored through appropriate maintenance; 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. The original (a) Each Engine or Suitable Replacement Engine (in case of Total Loss) is in the configuration as permitted under this Agreement installed on the Aircraft shall will comply with the following: 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: (a1) have no less than 4,500 Cycles scheduled life remaining in respect full borescope inspection; (2) analysis of Engine LLPs and no more than 110% trend data; (3) sea level outside air temperature limit assessment or minimum last (10) qualifying flights (excluding the first flight of the Aircraft total Flight Hours and Cycles since new. Engine Life Limited Parts will be supported by certification documentation necessary day); (4) a test cell run; (5) technical log analysis for a minimum of the previous 3 months’ of operation; (6) previous shop visit assessment (if applicable); and (7) reference to demonstrate traceability back to birththe Lessee’s Maintenance Program. (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) The Final Inspection provided for by Section 1.1 of this Schedule 6 shall be serviceable completed, and capable as part of full rated performance without limitations throughout the entire operating envelop of the Aircraft as defined in the EASA AFM. Each such Final Inspection, 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 accomplished at the Redelivery Location on or about the Redelivery Date an all module, hot and cold section a complete video borescope inspection. Lessee will also have just completed in respect of each Engine an inspection of each magnetic chip detectorall Engine gas path modules, laboratory oil sample analysiswhich inspection shall be performed at Lessor’s expense, main oil screen and oil a test cell run performed at Lessee’s expense in accordance with the Lessee’s Maintenance Program or Manufacturer’s maintenance manual and fuel filter inspections. Any any defects discovered in such inspections which exceed the Engine Manufacturermanufacturer’s in-service limits shall be corrected at the 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 “on watch” for any reason requiring any special or out of sequence inspection or reduced interval inspectionsinspection. Each such Engine will shall comply with and have been maintained in accordance with the Agreed Maintenance Programme operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer’s in-service limits shall be repaired; and. (fc) Each Engine Life-Limited Part will have trend or condition monitoring data over at least not less than the previous yearMinimum 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; if Engine trend or condition monitoring data indicates for this purpose “Life Limited Part” means a rate component with an ultimate life which cannot be restored through appropriate maintenance approved by the State of acceleration in performance deterioration over at least the previous ninety days, which is higher than normal based on the maintenance experience Design 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 deteriorationmanufacturer.

Engines. The original Each Engine (or Suitable a Replacement Engine (in case of Total Lossas and to the extent permitted by Section 1.2(b)) is in the configuration as permitted under this Agreement will be installed on the Aircraft shall and comply with the following: (a) If the Aircraft Lease Agreement specifies a Minimum Engine Flight Hours and/or Minimum Engine Cycles, each Engine will have no not less than 4,500 Cycles scheduled life remaining in respect of the Minimum Engine LLPs and no more than 110% of the Aircraft total Flight Hours and Minimum Engine Cycles since newexpected life remaining to the next scheduled removal. Engine Life Limited Parts The expected life remaining will be supported determined by certification documentation necessary third party mutually acceptable to demonstrate traceability back both Lessor and Lessee (at Lessor's cost) or by the Engine Manufacturer, in each case based on the inspection and checks to birth.be performed at the Return Occasion in accordance with the Lease; (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 location for Lessor's acceptance on or about the Redelivery Date an all module, Return Occasion a hot (including combustion chamber) and cold section video borescope inspection. Lessee will also have just completed , which inspection shall be performed at Lessor's expense, and a power assurance run performed at Lessee's expense in respect of each Engine an inspection of each magnetic chip detector, laboratory oil sample analysis, main oil screen accordance with the Lessee's Maintenance Program or Manufacturer's Maintenance Planning Document and oil and fuel filter inspections. Any any defects discovered in such inspections which exceed the Engine Manufacturer’s 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 Lessee’s expenseReturn Occasion. No Engine shall be “on "watch” " for any reason requiring any special or out of sequence inspection or reduced interval inspectionsinspection. Each such Engine will shall comply with and have been maintained in accordance with the Agreed Maintenance Programme 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 Component Cycles, each Engine Life-Limited Component will have not less than the Minimum Component Cycles remaining 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 "Engine Life-Limited Component" means a component with an ultimate life which cannot be restored through appropriate maintenance; 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. The original Each Engine (or Suitable a Replacement Engine (in case of Total Lossas and to the extent permitted by Section 1.2(b)) is in the configuration as permitted under this Agreement will be installed on the Aircraft shall and comply with the following: (a) If the Aircraft Lease Agreement specifies a Minimum Engine Flight Hours and/or Minimum Engine Cycles, each Engine will have no not less than 4,500 Cycles scheduled life remaining in respect of the Minimum Engine LLPs and no more than 110% of the Aircraft total Flight Hours and Minimum Engine Cycles since newexpected life remaining to the next expected removal. Engine Life Limited Parts The expected life remaining will be supported determined by certification documentation necessary third party mutually acceptable to demonstrate traceability back both Lessor and Lessee (at Lessor's cost) or by the Engine Manufacturer, in each case based on the inspection and checks to birth.be performed at the Return Occasion in accordance with the Lease; (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 location for Lessor's acceptance on or about the Redelivery Date an all module, Return Occasion a hot (including combustion chamber) and cold section video borescope inspection. Lessee will also have just completed , which inspection shall be performed at Lessor's expense, and a power assurance run performed at Lessee's expense in respect of each Engine an inspection of each magnetic chip detector, laboratory oil sample analysis, main oil screen accordance with the Lessee's Maintenance Program or Manufacturer's Maintenance Planning Document and oil and fuel filter inspections. Any any defects discovered in such inspections which exceed the Engine Manufacturer’s 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 Lessee’s expenseReturn Occasion. No Engine shall be “on "watch” " for any reason requiring any special or out of sequence inspection or reduced interval inspectionsinspection. Each such Engine will shall comply with and have been maintained in accordance with the Agreed Maintenance Programme 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 Component Cycles, each Engine Life-Limited Component will have not less than the Minimum Component Cycles remaining 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 "Engine Life-Limited Component" means a component with an ultimate life which cannot be restored through appropriate maintenance; 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. 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 5,000 Cycles scheduled life remaining in respect of Engine LLPs Life Limited Parts 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 10,000 Flight Hours and 7,000 6,500 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 25oC sea level hot day EGT marginmargin and will not have accumulated more than 110% of the accumulated calendar time, Flight Hours and Cycles of the Airframe; (d) all items beyond the Engine Manufacturer’s in-service limits will be repaired; (e) will have just completed at the Redelivery Location location for the Lessor’s acceptance on or about the Redelivery Date redelivery date an all module, hot and cold section video borescope inspection. The 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. The original Each 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 followingwill: (a) have no not less than 4,500 Cycles scheduled the Minimum Engine Flight Hours life remaining in respect of Engine LLPs to the next expected removal and no more than 110% each of the Aircraft total Flight Hours and LLPs shall have not less than the Engine Cycles since newRestriction release life remaining. Engine Life Limited Parts The expected life remaining will be supported determined by certification documentation necessary to demonstrate traceability back to birth.the inspection and checks accomplished by Lessor in accordance with the Lease; (b) will have accumulated no more be free of all Security Interests, other than 7,000 Flight Hours and 7,000 Cycles since new or last Engine Performance Restoration shop visit.Security Interests granted by Lessor; (c) shall have undergone the inspections as set forth in Section 1.1(b) and (c) herein. If any inspection procedure identifies any Engine defect(s) that causes the Engine to be serviceable unserviceable, Lessee will immediately notify Lessor in writing, correct such defect(s) at Lessee's cost and capable of full rated performance without limitations throughout provide evidence satisfactory to Lessor that defects have been corrected in accordance with the entire operating envelop of EMM and the Aircraft as defined in the EASA AFM. Each Engine shall have at least 25C sea level hot day EGT marginMaintenance Program; (d) all items beyond the Engine be prepared for shipment for long-term storage in accordance with Manufacturer’s in-service limits will be repaired's recommendations; (e) will have just completed at be zero time since the Redelivery Location on or about the Redelivery Date an all module, last complete 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 Manufacturer's and the Agreed Maintenance Programme without waiver or exceptions. All items beyond Related Airframe manufacturer's maintenance manual and will be in compliance with requirements of the Engine manufacturer’s in-service limits shall be repaired; andEMM, Lessee's operations specifications, and the requirements and recommendations of the Air Authority; (f) have trend or condition monitoring data over at least together with installed components, not be subject to any reduced frequency inspections in comparison to 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 Related Airframe manufacturer's maintenance experience of the Engine Manufacturer in operating the same model of engines, under similar conditions, the Lessee will, manual limits; (g) immediately prior to redelivery, cause will have the 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 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 corrected such conditions zero time since a full parameter test cell run which are determined 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 an on-wing maximum power assurance run 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 exceeded tolerances defined for such engines 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 Minimum Engine Flight Hours and the Engine Cycles Restriction of remaining life, each including in respect of LLPs, pursuant to Manufacturer’s maintenance manual 's or are otherwise determined to be causing such performance deteriorationAir Authority's requirements until removal.

Engines. The original Each Engine (or Suitable a Replacement Engine (in case of Total Lossas and to the extent permitted by Section 1.2(b)) is in the configuration as permitted under this Agreement will be installed on the Aircraft shall and comply with the following: (a) If the Aircraft Lease Agreement specifies a Minimum Engine Flight Hours and/or Minimum Engine Cycles, each Engine will have no not less than 4,500 Cycles scheduled life remaining in respect of the Minimum Engine LLPs and no more than 110% of the Aircraft total Flight Hours and Minimum Engine Cycles since newexpected life remaining to the next expected removal. Engine Life Limited Parts The expected life remaining will be supported determined by certification documentation necessary third party mutually acceptable to demonstrate traceability back both Lessor and Lessee (at Lessor's cost) or by the Engine Manufacturer, in each case based on the inspection and checks to birth.be performed at the Return Occasion in accordance with the Lease; (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 location for Lessor's acceptance on or about the Redelivery Date an all module, Return Occasion a hot (including combustion chamber) and cold section video borescope inspection. Lessee will also have just completed , which inspection shall be performed at Lessor's expense, and a power assurance run performed at Lessee's expense in respect of each Engine an inspection of each magnetic chip detector, laboratory oil sample analysis, main oil screen accordance with the Lessee's Maintenance Program or Manufacturer's Maintenance Planning Document and oil and fuel filter inspections. Any any defects discovered in such inspections which exceed the Engine Manufacturer’s 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 Lessee’s expenseReturn Occasion. No Engine shall be “on "watch” " for any reason requiring any special or out of sequence inspection or reduced interval inspectionsinspection. Each such Engine will shall comply with and have been maintained in accordance with the Agreed Maintenance Programme operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer’s 's in-service limits shall be repaired; and; (fc) If the Aircraft Lease Agreement specifies Minimum Component Cycles, each Engine Life-Limited Component will have trend or condition monitoring data over at least not less than the previous year; if Engine trend or condition monitoring data indicates a rate of acceleration in performance deterioration over at least Minimum Component Cycles remaining per the previous ninety days, which is higher than normal based on manufacturer's then current limitations for 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.part

Engines. The original (a) Each Engine (or Suitable a Replacement Engine (in case of Total Lossas and to the extent permitted by Clause 1.2(b)) is in the configuration as permitted under this Agreement will be installed on the Aircraft shall and comply with the following: (ai) Each Engine will have no not less than 4,500 Cycles scheduled life remaining in respect of the Minimum Engine LLPs and no more than 110% of the Aircraft total Flight Hours and Minimum Engine Cycles since newexpected life remaining to the next removal. Engine Life Limited Parts The expected life remaining will be supported determined by certification documentation necessary to demonstrate traceability back to birth.the inspection and checks accomplished in accordance with the Lease as listed below: (ii) borescope inspection; (iii) engine condition monitoring sage data; (iv) OATL assessment or minimum last ten (10) Flight Hours; (v) ground runs; (vi) technical log analysis; and 07c043 CTA (vii) previous shop visit assessment (if applicable); (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, a hot (including combustion chamber) and cold section video borescope inspection. Lessee will also have just completed , which inspection shall be performed at Lessor’s expense, and a power assurance run performed at Lessee’s expense in respect of each Engine an inspection of each magnetic chip detector, laboratory oil sample analysis, main oil screen accordance with the Lessee’s Maintenance Program or Manufacturer’s maintenance manual and oil and fuel filter inspections. Any any defects discovered in such inspections which exceed the Engine Manufacturermanufacturer’s in-service limits shall be corrected at the 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 “on watch” for any reason requiring any special or out of sequence inspection or reduced interval inspectionsinspection. Each such Engine will shall comply with and have been maintained in accordance with the Agreed Maintenance Programme operations specification of Lessee without waiver or exceptions. All items beyond the Engine manufacturer’s in-service limits shall be repaired; (c) Each Engine Life-Limited Part will have not less than the Minimum Engine LLP Cycles remaining 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; 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.