Common use of Condition of Installed Engines and APU Clause in Contracts

Condition of Installed Engines and APU. At time of return, each Engine shall be capable of certificated, full rated performance and its life limited parts ("LLP") will have at least fifty percent (50%) of cycles between installation and replacement under the Maintenance Program. (a) Time remaining - Each Engine shall have completed no more than 2,500 flight hours since new or since its last full performance restoration shop visit at which it was subject to a full engine management program rework, based on the reliability goals set out in the Rolls-Xxxxx Xxxxxx workscope guide, which currently state that the workscope is designed to give 30 degrees centigrade of exhaust gas temperature margin and 5,000 flight hours of on-wing life. To the extent that the shop workscope guide is amended in the future to include different reliability goals then the engine shall have at least fifty percent (50%) of the on-wing hours remaining in accordance with such amended shop workscope guide.

Condition of Installed Engines and APU. At time of return, each Engine shall be capable of certificated, full rated performance and its life limited parts ("LLP") will have at least fifty percent (50%) of cycles between installation and replacement under the Maintenance Program. (a) Time remaining - Each Engine shall have completed no more than 2,500 flight hours since new or since its last full performance restoration shop visit at which it was subject to a full engine management program rework, based on the reliability goals set out in the Rolls-Xxxxx Xxxxxx workscope guide, which currently state that the workscope is designed to give 30 degrees centigrade of exhaust gas temperature margin and 5,000 flight hours of on-wing life. To the extent that the shop workscope guide is amended in the future to include different reliability goals then the engine shall have at least fifty percent (50%) of the on-wing hours remaining in accordance with such amended shop workscope guide.

Condition of Installed Engines and APU. At time of return, each Engine shall be capable of certificated, full rated performance and its life limited parts ("LLP") will have at least fifty percent (50%) of cycles between installation and replacement under the Maintenance Programremaining before replacement. (a) Time remaining TIME REMAINING - Each Engine shall have completed no more than 2,500 two thousand five hundred (2500) flight hours since new or since its last full performance restoration shop visit at which it was subject to a full engine management program rework, based on the reliability goals set out in the Rolls-Xxxxx Xxxxxx XX Xxxxxxx workscope guide, which currently state that the workscope is designed to give 30 degrees centigrade of exhaust gas temperature margin and 5,000 flight hours of on-wing life. To the extent that the shop workscope guide is amended in the future to include different reliability goals then the engine Engine shall have at least fifty percent (50%) of the on-wing hours remaining in accordance with such amended shop workscope guide.

Condition of Installed Engines and APU. At time of return, each Engine shall be capable of certificated, full rated performance and its life limited parts ("LLP") will have at least fifty percent (50%) of cycles between installation and replacement under the Maintenance Programremaining before replacement. (a) Time remaining - Each Engine shall have completed no more than 2,500 two thousand five hundred (2500) flight hours since new or since its last full performance restoration shop visit at which it was subject to a full engine management program rework, based on the reliability goals set out in the Rolls-Xxxxx Xxxxxx Royce Alison workscope guide, which currently state that the workscope statx xxxx xxx xorkscope is designed to give 30 degrees centigrade of exhaust gas temperature margin and 5,000 flight hours of on-wing life. To the extent that the shop workscope guide is amended in the future to include different reliability goals then the engine shall have at least fifty percent (50%) of the on-wing hours remaining in accordance with such amended shop workscope guide.

Condition of Installed Engines and APU. At time of return, each Engine shall be capable of certificated, full rated performance and its life limited parts ("LLP") will have at least fifty percent (50%) of cycles between installation and replacement under the Maintenance Programremaining before replacement. (a) Time remaining - Each Engine shall have completed no more than 2,500 two thousand five hundred (2500) flight hours since new or since its last full performance restoration shop visit at which it was subject to a full engine management program rework, based on the reliability goals set out in the Rolls-Xxxxx Xxxxxx RR Alison workscope guide, which currently state that the workscope is designed to give 30 degrees centigrade of exhaust gas temperature margin and 5,000 flight hours of on-wing life. To the extent that the shop workscope guide is amended in the future to include different reliability goals then the engine shall have at least fifty percent (50%) of the on-wing hours remaining in accordance with such amended shop workscope guide.

Condition of Installed Engines and APU. At time of return, each Engine shall be capable of certificated, full rated performance and its life limited parts ("LLP") will have at least fifty percent (50%) of cycles between installation and replacement under the Maintenance Programremaining before replacement. (a) Time remaining - Each Engine shall have completed no more than 2,500 two thousand five hundred (2,500) flight hours since new or since its last full performance restoration shop visit at which it was subject to a full engine management program rework, based on the reliability goals set out in the Rolls-Xxxxx Xxxxxx Royce Alison workscope guide, which currently state that the workscope statx xxxx xxx xorkscope is designed to give 30 degrees centigrade of exhaust gas temperature margin and 5,000 flight hours of on-wing life. To the extent that the shop workscope guide is amended in the future to include different reliability goals then the engine shall have at least fifty percent (50%) of the on-wing hours remaining in accordance with such amended shop workscope guide.

Condition of Installed Engines and APU. At time of return, each Engine shall be capable of certificated, full rated performance and its life limited parts ("LLP") will have at least fifty percent (50%) of cycles between installation and replacement under the Maintenance Programremaining before replacement. (a) Time remaining - Each Engine shall have completed no more than 2,500 two thousand five hundred (2,500) flight hours since new or since its last full performance restoration shop visit at which it was subject to a full engine management program rework, based on the reliability goals set out in the Rolls-Xxxxx Xxxxxx workscope guide, which currently state that the workscope is designed to give 30 degrees centigrade of exhaust gas temperature margin and 5,000 flight hours of on-wing life. To the extent that the shop workscope guide is amended in the future to include different reliability goals then the engine shall have at least fifty percent (50%) of the on-wing hours remaining in accordance with such amended shop workscope guide.

Condition of Installed Engines and APU. At time of return, each Engine shall be capable of certificated, full rated performance and its life limited parts ("LLP") will have at least fifty percent (50%) of cycles between installation and replacement under the Maintenance Programremaining before replacement. (a) Time remaining - Each Engine shall have completed no more than 2,500 two thousand five hundred (2,500) flight hours since new or since its last full performance restoration shop visit at which it was subject to a full engine management program rework, based on the reliability goals set out in the Rolls-Xxxxx Xxxxxx Royce Alison workscope guide, which currently state that currexxxx xxxxx xhat the workscope is designed to give 30 degrees centigrade of exhaust gas temperature margin and 5,000 flight hours of on-wing life. To the extent that the shop workscope guide is amended in the future to include different reliability goals then the engine shall have at least fifty percent (50%) of the on-wing hours remaining in accordance with such amended shop workscope guide.