Common use of Engine Records Clause in Contracts

Engine Records. a) Engine log book or Engine Data Submittal; b) Current Disk Sheet (LLP Sheet) signed and certified; c) Manufacturer Delivery Documents; d) Complete historical engine/ module shop visit reports and Engine Performance Restoration reports, for all Engine Performance Restorations; e) Dirty finger print shop work cards and material data sheets covering the last overhaul of each module, for all shop visits; f) On Wing Repair records; g) Engine Log Book/ Master Records of Installation/Removals; h) Last Borescope Report, including video if available; i) Test Cell Run Report; j) Certified Statement that Engines are not involved in an accident; k) Certified “On-Watch” statement; l) List of “On-Watch Items” items requiring repetitive inspections; m) List of repetitive inspections that are not required by AD; n) List of technical variances or maintenance requirements unique to the particular Engine; o) Engine Trend Monitoring data for the last 12 months of operation; p) Last engine run and power assurance report; q) All Life Limited Parts (LLPs) will have complete life traceability of time consumed (Cycles and/or Flight Hours as applicable) since new. Such traceability shall include historical removal and installation documentation of each LLP in respect of each Engine or module where such LLP had been installed and where time has been consumed. Each removal and installation document will evidence LLP total Flight Hours and LLP total Cycles accumulated in each Engine or module; r) Each LLP will have a signed and certified cover page including engine or module total Flight Hours, total Cycles, part total Flight Hours, total Cycles and date for each removal and installation depicting the life of the part since new. Notwithstanding, any LLPs replaced during the term of the lease will have the most recent FAA 8130-3 tag or JAA Form 1, as applicable, used to install such LLP into the applicable Engine or module; s) Engine manufacturer’s or FAA or EASA approved data shall be provided for any discrepancies outside of the Engine Manufacturer’s Engine Manual shop limits that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: i) Approval form; ii) Complete description of the discrepancy; iii) Supporting analysis and documentation; and t) Engine manufacturer’s or FAA or EASA approved data shall be provided for any repairs not in accordance with the Engine Manufacturer’s Engine Manual that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: i) Approval form; ii) Complete description of repair; iii) Supporting analysis and documentation.

Engine Records. (FOR EACH ENGINE) (a) Engine log book or Engine Data Submittal;Certified statement as to following: (i) time and cycles since new (ii) time and cycles since overhaul on each engine module (iii) flying hours and cycles in lessee’s operation (b) Current Disk Sheet Engine Master Record (LLP Sheet) signed record of installation and certified;removal and accumulated flight time and cycles for Engine and each module installed at Redelivery Date) (c) List of Operator Modifications Incorporated, if any including supporting documentation with Manufacturer Delivery Documents;approval (d) Complete historical engine/ module List of all Major Repairs and Alterations, if any (e) Check/Inspection Status (f) Accessory Status sheet with certified TSO for each rotable item installed (g) Last overhaul tags (or copies) for each of the accessory rotables (h) Engine Build Specifications (i) (Repair, overhaul and inspection documents such as JAA form 1, FAA 8130-3 and FAA form 337 for each shop visit reports and (minimum acceptable is shop visit history through last Engine Performance Restoration reportsshop visit and if different, for all Engine Performance Restorations; e) Dirty finger print shop work cards and material data sheets covering the last overhaul of each module, ) (j) List of current Line Replaceable Units (LRU)/QEC Items missing from engine (if applicable for all shop visits;a spare Engine redelivery or off-wing Engine) f) On Wing Repair records; g(k) Engine Log Book/ Master Records of Installation/Removals;Condition Monitoring Report for the three (3) months prior to redelivery h(l) Last Borescope Reportthree (3) months of aircraft flight/technical logs to which engine was fitted (m) Reason for last engine removal, including video if available;engine change paperwork and date of engine removal i(n) Most recent certified engine borescope (videotaped) (o) Most recent fuel, oil sampling, magnetic chip detector and vibration survey results (p) Most recent on-wing ground performance run specifying engine OATL (outside air temperature limit) at rated thrust (q) Last certified Test Cell Run Report;specifying engine OATL j) Certified Statement that Engines are not involved in an accident; k) Certified “On-Watch” statement; l) List of “On-Watch Items” items requiring repetitive inspections; m) List of repetitive inspections that are not required by AD; n) List of technical variances or maintenance requirements unique to the particular Engine; o(r) Engine Trend Monitoring data for the last 12 months of operation;Oil used p) Last engine run and power assurance report; q) All Life Limited Parts (LLPs) will have complete life traceability of time consumed (Cycles and/or Flight Hours as applicable) since new. Such traceability shall include historical removal and installation documentation of each LLP in respect of each Engine or module where such LLP had been installed and where time has been consumed. Each removal and installation document will evidence LLP total Flight Hours and LLP total Cycles accumulated in each Engine or module; r) Each LLP will have a signed and certified cover page including engine or module total Flight Hours, total Cycles, part total Flight Hours, total Cycles and date for each removal and installation depicting the life of the part since new. Notwithstanding, any LLPs replaced during the term of the lease will have the most recent FAA 8130-3 tag or JAA Form 1, as applicable, used to install such LLP into the applicable Engine or module; s) Engine manufacturer’s or FAA or EASA approved data shall be provided for any discrepancies outside of the Engine Manufacturer’s Engine Manual Any incidents during operation since last performance restoration shop limits that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: i) Approval form; ii) Complete description of the discrepancy; iii) Supporting analysis and documentation; and t) Engine manufacturer’s or FAA or EASA approved data shall be provided for any repairs not in accordance visit with the Engine Manufacturer’s Engine Manual that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: i) Approval form; ii) Complete description of repair; iii) Supporting analysis and documentationaction taken i.e. IFSD/FOD/oil loss etc.

Engine Records. (a) Engine log book or Engine Data Submittal; (b) Current Disk Sheet (LLP Sheet) signed and certified; (c) Manufacturer Delivery Documents; (d) Complete copies of all historical engine/ module shop visit reports and Engine Performance Restoration reports, for all Engine Performance Restorationsengine last shop visit report; (e) Dirty Copies of all dirty finger print shop work cards and material data sheets covering the last overhaul of each module, for all shop visits; (f) On Wing Repair records; (g) Engine Log Book/ Master Records of Installation/Removals; (h) Last Borescope Report, including video if available; (i) Test Cell Run ReportReport for any shop visit; (j) Certified If the Engines have not been involved in an incident, certified Statement that Engines are not involved in an accident; (k) Certified “On-Watch” statement; (l) List of “On-Watch Items” items requiring repetitive inspections; (m) List of repetitive inspections that are not required by AD; (n) List of technical variances or maintenance requirements unique to the particular Engine; (o) Engine Trend Monitoring data Certified Accessory LRU List with Approved Release to Service Certification (FAA 8130-3 or JAA/EASA Form 1) for the last 12 months of operationinstalled LRU’s; (p) Last engine run and power assurance report; (q) All Life Limited Parts (“LLPs”) will have complete life traceability of time consumed (Cycles cycles and/or Flight Hours hours as applicable) since new. Such traceability shall include historical removal and installation documentation of each LLP in respect of each Engine or module where such LLP had been installed and where time has been consumed. Each removal and installation document will evidence LLP total Flight Hours hours and LLP total Cycles cycles accumulated in each Engine or module; (r) Each LLP will have a signed and certified cover page including engine or module total Flight Hourshours, total Cyclescycles, part total Flight Hourshours, total Cycles cycles and date for each removal and installation depicting the life of the part since new. Notwithstanding, any LLPs replaced during the term of the lease will have the most recent FAA 8130-3 tag or JAA JAA/EASA Form 1, as applicable, used to install such LLP into the applicable Engine or module; (s) Engine manufacturerManufacturer’s or FAA or EASA approved data shall be provided for any discrepancies outside of the Engine Manufacturer’s Engine Manual shop limits that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: (i) Approval form; (ii) Complete description of the discrepancy;; and (iii) Supporting analysis and documentation; and (t) Engine manufacturer’s Manufacturer’s, EASA or FAA or EASA approved data shall be provided for any repairs not in accordance with the Engine Manufacturer’s Engine Manual that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: (i) Approval form; (ii) Complete description of repair;; and (iii) Supporting analysis and documentation. (a) Certified Statement on Status of APU; (b) In house modifications (if applicable); (c) Approved Release to Service Certification for installed units; (d) APU Log Book/ Master Record of Installation/ Removals; (e) Complete copies of all APU Shop Visit Reports & reason for removal; (f) Copies of all dirty finger print shop work cards and material data sheets covering the last overhaul of the APU; (g) Statement of APU hours to Aircraft Flying hours (if applicable); (h) Last APU Borescope Report; (i) Last Test Run Report for any shop visit; (j) All Life Limited Parts will have complete life traceability of time consumed (cycles and/or hours as applicable) since new. Such traceability shall include historical removal and installation documentation of each LLP in respect of each APU where such LLP had been installed and where time has been consumed. Each removal and installation document will evidence LLP total hours and LLP total Cycles accumulated in each Engine or module; (k) Each LLP will have a signed and certified cover page including engine or module total hours, total Cycles, part total hours, total Cycles and date for each removal and installation depicting the life of the part since new. Notwithstanding, any LLPs replaced during the term of the lease will have the most recent FAA 8130-3 tag or JAA/EASA Form 1, as applicable, used to install such LLP into the applicable APU; (l) APU manufacturer’s, EASA or FAA approved data shall be provided for any discrepancies outside of the APU Manufacturer’s Engine Manual shop limits that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: (i) Approval form; (ii) Complete description of the discrepancy; and (iii) Supporting analysis and documentation; and (m) APU manufacturer’s or FAA approved data shall be provided for any repairs not in accordance with the APU Manufacturer’s Engine Manual that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: (i) Approval form; (ii) Complete description of repair; and (iii) Supporting analysis and documentation.

Engine Records. (a) Engine log book or Engine Data Submittal; (b) Current Disk Sheet (LLP Sheet) signed and certified; (c) Manufacturer Delivery Documents; (d) Complete copies of all historical engine/ module shop visit reports and Engine Performance Restoration reports, for all Engine Performance Restorationsengine last shop visit report; (e) Dirty Copies of all dirty finger print shop work cards and material data sheets covering the last overhaul of each module, for all shop visits; (f) On Wing Repair records; (g) Engine Log Book/ Master Records of Installation/Removals; (h) Last Borescope Report, including video if available; (i) Last Test Cell Run ReportReport for any shop visit; (j) Certified If the Engines have not been involved in an incident, certified Statement that Engines are not involved in an accident; (k) Certified “On-Watch” statement; (l) List of “On-Watch Items” items requiring repetitive inspections; (m) List of repetitive inspections that are not required by AD; (n) List of technical variances or maintenance requirements unique to the particular Engine; (o) Certified Accessory LRU List with Approved Release to Service Certification (FAA 8130-3 or JAA/EASA Form 1) for installed LRU’s; (p) Engine Trend Monitoring data for the last 12 months of operationoperation (it being agreed that Lessor and Lessee shall discuss in good faith the cost in connection with the provision of such report prior to Redelivery); p(q) Last engine run and power assurance report; q(r) All Life Limited Parts (“LLPs”) will have complete life traceability of time consumed (Cycles cycles and/or Flight Hours hours as applicable) since new. Such traceability shall include historical removal and installation documentation of each LLP in respect of each Engine or module where such LLP had been installed and where time has been consumed. Each removal and installation document will evidence LLP total Flight Hours hours and LLP total Cycles cycles accumulated in each Engine or module; r(s) Each LLP will have a signed and certified cover page including engine or module total Flight Hourshours, total Cyclescycles, part total Flight Hourshours, total Cycles cycles and date for each removal and installation depicting the life of the part since new. Notwithstanding, any LLPs replaced during the term of the lease will have the most recent FAA 8130-3 tag or JAA JAA/EASA Form 1, as applicable, used to install such LLP into the applicable Engine or module; s(t) Engine manufacturer’s Manufacturer’s, EASA or FAA or EASA approved data shall be provided for any discrepancies outside of the Engine Manufacturer’s Engine Manual shop limits that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: (i) Approval form; (ii) Complete description of the discrepancy;; and (iii) Supporting analysis and documentation; and; t(u) Engine manufacturerManufacturer’s or FAA or EASA approved data shall be provided for any repairs not in accordance with the Engine Manufacturer’s Engine Manual that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: (i) Approval form; (ii) Complete description of repair;; and (iii) Supporting analysis and documentation.

Engine Records. (a) Engine log book or Engine Data Submittal; (b) Current Disk Sheet (LLP Sheet) signed and certified; (c) Manufacturer Delivery Documents; (d) Complete copies of all historical engine/ module shop visit reports and Engine Performance Restoration reports, for all Engine Performance Restorationsengine last shop visit report; (e) Dirty Copies of all dirty finger print shop work cards and material data sheets covering the last overhaul of each module, for all shop visits; (f) On Wing Repair records; (g) Engine Log Book/ Master Records of Installation/Removals; (h) Last Borescope Report, including video if available; (i) Test Cell Run ReportReport for any shop visit; (j) Certified If the Engines have not been involved in an incident, certified Statement that Engines are not involved in an accident; (k) Certified “On-Watch” statement; (l) List of “On-Watch Items” items requiring repetitive inspections; (m) List of repetitive inspections that are not required by AD; (n) List of technical variances or maintenance requirements unique to the particular Engine; (o) Certified QEC rotable parts list with Approved Release to Service Certification (FAA 8130-3 or JAA/EASA Form 1 for each QEC rotable part; (p) Certified Accessory LRU List with Approved Release to Service Certification (FAA 8130-3 or JAA/EASA Form 1) for installed LRU’s; (q) Engine Trend Monitoring data for the last 12 months of operation; p(r) Last engine run and power assurance report; q(s) All Life Limited Parts (“LLPs”) will have complete life traceability of time consumed (Cycles cycles and/or Flight Hours hours as applicable) since new. Such traceability shall include historical removal and installation documentation of each LLP in respect of each Engine or module where such LLP had been installed and where time has been consumed. Each removal and installation document will evidence LLP total Flight Hours hours and LLP total Cycles cycles accumulated in each Engine or module; r(t) Each LLP will have a signed and certified cover page including engine or module total Flight Hourshours, total Cyclescycles, part total Flight Hourshours, total Cycles cycles and date for each removal and installation depicting the life of the part since new. Notwithstanding, any LLPs replaced during the term of the lease will have the most recent FAA 8130-3 tag or JAA JAA/EASA Form 1, as applicable, used to install such LLP into the applicable Engine or module; s(u) Engine manufacturerManufacturer’s or FAA French DGAC or EASA German LBA approved data shall be provided for any discrepancies outside of the Engine Manufacturer’s Engine Manual shop limits that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: (i) Approval form; (ii) Complete description of the discrepancy; (iii) Supporting analysis and documentation; and t(v) Engine manufacturerManufacturer’s or FAA French DGAC or EASA German LBA approved data shall be provided for any repairs not in accordance with the Engine Manufacturer’s Engine Manual that documents approval for unlimited continued service, without time limitations for removal, repair or replacement, or have any special or distinct inspection requirements. The data shall include: (i) Approval form; (ii) Complete description of repair;; and (iii) Supporting analysis and documentation.