Common use of Engineering Documentation Clause in Contracts

Engineering Documentation. a) A current list of Engine and APU Service Bulletins, Engineering Orders, major repairs and Supplemental Type Certificates accomplished on each Engine and the APU. A current list of Airframe Engineering Orders, major repairs and Supplemental Type Certificates accomplished on the Airframe. For appliances, a current list of A.D. related Service Bulletins, major repairs, Supplemental Type Certificates and Engineering Orders are required; b) Legible copies of the detailed dirty fingerprint work card accomplishment documentation for each Airframe, appliance, Engine and APU Service Bulletin, Engineering Order, major repair and Supplemental Type Certificate accomplished on the Aircraft, each Engine and the APU, to include the following: i) SB number and revision number; ii) SB title; iii) Aircraft serial number, Engine serial number, APU serial number, appliance serial number as applicable; iv) Engineering documentation reference; v) Manufacturer’s Service Bulletin reference and cross-references where appropriate; vi) Specify terminated or repetitive status; vii) Date of accomplishment of each portion of such engineering document; viii) Date of last maintenance accomplishment, if repetitive; ix) Name and serial number of the internal maintenance form used to document accomplishment, if applicable; x) Statement of the means by which compliance was accomplished (e.g., modified, repaired, inspected); c) FAA or EASA approvals (DER Form 8110-3, Form 8100-9 or EASA Part 21 approval sheet, if applicable) for modifications or alterations not covered by manufacturer’s Service Bulletins (including appliances, if applicable); d) A current copy of all Engineering documentation related to all Aircraft alterations, repairs and configuration changes. This shall include documentation for work done by the previous owner(s) and operators(s), the manufacturer or any vendor; e) Data packages covering all designed repairs or alterations that do not have manufacturer approval, including the submittal to the FAA or EASA for an STC or EASA Part 21 approval sheet, if applicable. The data packages shall include the following: i) engineering orders; ii) drawings; iii) parts lists; iv) installation documentation; v) engineering analysis as submitted to obtain the STC approval; vi) all manual supplements (MM, IPC, WD, AFM); vii) maintenance program supplements; viii) any and all reference documents referenced by documents contained in this section 4(e); f) Engineering deviations records, if any, applicable to the airframe, Engines and APU, components and piece parts; and g) Digital Flight Data Recorder System technical description

Engineering Documentation. (a) A current list (in paper and workable electronic format) of Airframe, appliance, Engine and APU Service Bulletins, Engineering Orders, major repairs and Supplemental Type Certificates accomplished on the Aircraft, each Engine and the APU. A current list of Airframe Engineering Orders, major repairs and Supplemental Type Certificates accomplished on the Airframe. For appliances, a current list of A.D. only AD related Service Bulletins, major repairs, Supplemental Type Certificates Bulletins and Engineering Orders are required;. (b) Legible copies of the detailed dirty fingerprint work card accomplishment documentation for each Airframe, appliance, Engine and APU Service Bulletin, Engineering Order, major repair and Supplemental Type Certificate accomplished on the Aircraft, each Engine and the APU, to include the following: (i) SB number and revision number; (ii) SB title; (iii) Aircraft serial number, Engine serial number, APU serial number, appliance serial number as applicable; (iv) Engineering documentation reference; (v) Manufacturer’s Service Bulletin reference and cross-references where appropriate; (vi) Specify terminated or repetitive status; (vii) Date of initial accomplishment of each portion of such engineering document; (viii) Date of last maintenance accomplishment, if repetitive; (ix) Name and serial number of the internal maintenance form used to document accomplishment, if applicable;; and (x) Statement of the means by which compliance was accomplished (e.g., modified, repaired, inspected);. (c) EASA or FAA or EASA approvals (DER Form 8110-3, 3 or Form 8100-9 or EASA Part 21 approval sheet, if applicable9) for modifications or alterations not covered by manufacturer’s Service Bulletins (including appliances, if applicable);. (d) A current copy of all Engineering documentation related to all Aircraft alterations, repairs and configuration changes. This shall include documentation for work done by the previous owner(s) and operators(s), the manufacturer or any vendor;seller. (e) Data packages covering all non-manufacturer/non-FAA/non-EASA designed repairs or alterations that do not have manufacturer approvalalterations, including the submittal to the FAA or EASA for an STC or EASA Part 21 approval sheetForm 337, if applicable. The data packages shall include the following: (i) engineering orders; (ii) drawings; (iii) parts lists; (iv) installation documentation; (v) engineering analysis as submitted to obtain the STC or Form 337 approval; (vi) all manual supplements (MM, IPC, WD, AFM); (vii) maintenance program supplements;; and (viii) any and all reference documents referenced by documents contained in this section 4(e(4);. (f) Engineering deviations records, if any, applicable to the airframe, Engines and APU, components and piece parts; and. (g) Digital Flight Data Recorder System technical description.