Common use of APU Clause in Contracts

APU. 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) APU Shop Visit Reports & reason for removal, for all APU shop visits; f) Dirty finger print shop work cards and material data sheets for all APU shop visits; g) Statement of APU hours to Aircraft Flying hours (if applicable); h) APU Borescope Report; i) Last Test Run Report; j) 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 APU 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; k) Each LLP will have a signed and certified cover page including engine or module total 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 APU; l) APU manufacturer’s or FAA or EASA approved data shall be provided for any discrepancies outside of the APU manufacturer’s APU shop manual 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; m) APU manufacturer’s or FAA or EASA approved data shall be provided for any repairs not in accordance with the APU manufacturer’s APU shop 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; and n) Current disk sheet (LLP) signed and certified, if applicable.

APU. (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, for all APU shop visits; (f) Dirty Copies of all dirty finger print shop work cards and material data sheets for all APU shop visitscovering the last overhaul of the APU; (g) Statement of APU hours to Aircraft Flying hours (if applicable); (h) APU Borescope Report; (i) Last Test Run ReportReport for any shop visit; (j) 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 APU 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 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 Flight Hourshours, 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 JAA/EASA Form 1, as applicable, used to install such LLP into the applicable APU; (l) APU manufacturer’s or FAA French DGAC or EASA German LBA approved data shall be provided for any discrepancies outside of the APU manufacturerManufacturer’s APU Engine Manual shop manual 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 (m) APU manufacturer’s or FAA French DGAC or EASA German LBA approved data shall be provided for any repairs not in accordance with the APU manufacturerManufacturer’s APU shop manual 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; and n) Current disk sheet (LLP) signed and certified, if applicable.

APU. (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, for all APU shop visits; (f) Dirty Copies of all dirty finger print shop work cards and material data sheets for all APU shop visitscovering 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 ReportReport for any shop visit; (j) 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 APU 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 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 Flight Hourshours, 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 JAA/EASA Form 1, as applicable, used to install such LLP into the applicable APU; (l) APU manufacturer’s ’s, EASA or FAA or EASA approved data shall be provided for any discrepancies outside of the APU manufacturerManufacturer’s APU Engine Manual shop manual 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; (m) APU manufacturer’s or FAA or EASA approved data shall be provided for any repairs not in accordance with the APU manufacturerManufacturer’s APU shop manual 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; and n) Current disk sheet (LLP) signed and certified, if applicable.