ENGINES, APU AND LANDING GEAR Sample Clauses

ENGINES, APU AND LANDING GEAR. 5.1. Prior to Return and following the redelivery flight for the Aircraft, Lessor shall have the right to accomplish a complete borescope inspection of the compressor, turbine, and combustion sections of each Engine and the APU, to be performed by Lessor’s representative or, at Lessor’s expense, an agency selected by Lessor. All defects discovered as a result of such inspections, which exceed the Manufacturer’s allowable limits for an installed engine or auxiliary power unit shall be corrected at Lessee’s expense.

ENGINES, APU AND LANDING GEAR. 5.1. Lessee may (i) witness and accept Lessor’s borescope inspection of the Engines and APU in connection with the redelivery of the Aircraft by Prior Operator, or (ii) may accomplish a complete borescope inspection of the compressor, turbine, and combustion sections of each Engine and the APU, to be performed by Lessee’s representative or, at Lessee’s expense, an agency selected by Lessee. All defects discovered as a result of such inspections, which exceed the Manufacturer’s allowable limits for an installed engine or auxiliary power unit shall be corrected at Lessor’s expense.

ENGINES, APU AND LANDING GEAR. The Aircraft will be returned with Lessor’s Engines, APU and Landing Gear installed and with the same equipment as at Delivery, subject only to those replacements, additions and Modifications permitted under this Lease.

ENGINES, APU AND LANDING GEAR. 5.1. Lessee may (i) witness and accept Lessor’s borescope inspection of the Engines and APU in connection with the redelivery of the Aircraft by Prior Operator, or (ii) may accomplish a complete borescope inspection of the compressor, turbine, and combustion sections of each Engine and the APU, to be performed by Lessee’s representative or, at Lessee’s expense, an agency selected by Lessee. All defects discovered as a result of such inspections, which exceed the Manufacturer’s allowable limits for an installed engine or auxiliary power unit shall be corrected at Lessor’s expense. Notwithstanding anything to the contrary herein, solely with respect to the Engine bearing Manufacturer’s serial number V12778 (“ESN V12778”), in the event that any damage to the combustion section of ESN V12778 exceeds the Manufacturer’s allowable limits during the Lease Term and ESN V12778 is not inducted for a performance restoration as a result of such damage, and provided that such damage was not caused by the negligence of Lessee or any Person using or having possession, custody or control of the Aircraft and/or ESN V12778, Lessor shall contribute (by way of reimbursement to Lessee, or payment to Lessee’s maintenance provider, as directed by Lessee) towards Lessee’s Actual Costs solely related to the repair to the combustion section promptly following receipt by Lessor of an invoice and documentation reasonably acceptable to Lessor providing evidence of such repair(s) and the cost associated therewith. Lessor’s contribution amount is to be determined by calculating the total labor and material costs of the repair (at Lessee’s Actual Cost) of the combustion section divided by the total number of Flight Hours accumulated by ESN V12778 at the time of the repair multiplied by the total Flight Hours accumulated by ESN V12778 at Delivery. For the avoidance of doubt, in the event ESN V12778 is inducted for a performance restoration as a result of such damage to the combustion chamber, Lessor shall contribute to the cost of such performance restoration pursuant to Section 2.A(vi) of Appendix 2C to the Lease and not pursuant to this Section 5.1.