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...
Engineering Documentation. 1. LESSOR shall provide a single, current list, in the English language (including the ADA list referenced in b. below) of engineering documentation covering the aircraft as listed below:
a. Service Bulletin status based on the Boeing provided summary of all Boeing service bulletins to the aircraft and consistent with the "reference only" status report provided during the initial inspection.
b. List of all Lufthansa initiated on-aircraft modifications consistent with the ADA list covering all Spec 100 ATA chapters. A current copy, in English, of all engineering orders listed on the ADA list shall be provided with appropriate certification stamp on the ADA list.
c. Major repairs list.
d. Supplemental Type Certificate list.
2. Data package covering all non-manufacturer/non-FAA-approved repairs or alterations, including the submittal to the LBA for an approval, if applicable.
Engineering Documentation. 1. A single, current list of Airframe, appliance, Engine and APU Service Bulletins, Engineering Orders, major repairs and Supplemental Type Certificates ("STC") accomplished on Aircraft, Engine and APU, including method and date of accomplishment, reference to engineering documentation, including related drawing and original signed documents where applicable shall be provided with information similar to that described in item B. 1.
2. A current copy of all Engineering documentation related to Aircraft alterations, repairs and configuration changes. This shall include documentation for work done by the manufacturer or any vendor. A current copy of all repairs that require follow-up action.
3. Data package covering all non-manufacturer / non-FAA-approved repairs or alterations, including the submittal to the FAA for an STC or Form 337, If applicable.
4. All open engineering deviations or Material Review Board ("MRB") records applicable to the Airframe, Engines and APU, components and piece parts.
5. Mapping of all exterior repairs and damage to the exterior of the Aircraft and Engines. Supporting data for each repair and damage shall be provided with information similar to items C-1 and C-2.
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. For appliances, only AD related Service 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) FAA or EASA approvals (as applicable) for modifications or alterations not covered by manufacturer’s Service Bulletins (including appliances).
(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 seller.
(e) Data packages covering all non-manufacturer/non-EASA/non-FAA-designed repairs or alterations, including the submittal to the FAA or EASA for an STC or Form 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);
(f) Engineering deviations records, if any, applicable to the airframe, Engines and APU, components and piece parts.
(g) Digital Flight Data Recorder System technical description.
Engineering Documentation. All hard copy engineering documents by Contractor or any of its Subcontractors or Sub-subcontractors shall be logically collated and indexed (e.g., Specifications, calculations, lists, etc.). Contractor shall present to Owner the engineering documents in hard back binders with front and back insert wallet, 3-post, expansion back from 5cm to 10 cm, 8 1/2” X 11” size sheets or 11” X 17” for Drawings, white colored. Binders shall not exceed 8cm in thickness. The contract number or project number, project title, Facility name, location, volume number and number of volumes shall be identified on the spine of the binder. All Contractor, Subcontractor and Sub-subcontractor documentation shall be individually numbered and registered by Contractor in Contractor’s Electronic Document Management System (“EDMS”). Integrity of any cross-references shall be maintained. Document number and document revision shall be consistent, complete and clearly visible on all documents/Drawings. Page numbers shall be clearly visible on multi-page documents. Document attributes shall be visible on the document front sheet or drawing. Documents originated electronically shall be supplied in both their native format (provided that Contractor shall use commercially reasonable efforts to obtain such native file format from Vendors in each case) and/or scanned image file. All engineering documents/Drawings shall be issued final according to their appropriate classification for As-Builts. All turnover documentation shall be issued with a formal handover transmittal. A complete document and Drawing index shall be provided both in hard copy and electronic versions.
Engineering Documentation. Non-proprietary specifications, functional descriptions and operating descriptions.
Engineering Documentation. (a) Lessor shall provide a single, current list in English language (except for the ADA list referenced in 3(a)(ii) below:
(i) Service Bulletin status based on the Boeing provided summary of all Boeing service bulletins to the Aircraft and consistent with the "reference only" status report provided during the initial inspection.
(ii) List of all Previous Operator initiated on- aircraft modifications consistent with the ADA list covering all Spec. 100 ATA chapters. A current copy of all engineering orders listed on the ADA list shall be provided with appropriate certification stamp on the ADA list.
(iii) Major repairs list
(iv) Supplement Type Certificate list
(b) Data package covering all non-manufacturer/non-Aviation Authority approved repairs or alterations, including the submittal to the Previous Operator's aviation authority for an approval, if applicable.
Engineering Documentation. All engineering documentation is stored, classified and accessed via a structured document hierarchy and document numbering system in the EDMS. The engineering documentation always reflects the latest change or modification. Older revisions of engineering documentation are retained and stored with the relevant revision information for a user defined period. All engineering documentation is produced using a documentation management system to ensure an accurate reflection of the system configuration and status at all times. All engineering documents managed by the document management system are dynamic. Engineering Document Management System • Any configuration change made to hardware and software is subsequently reflected in all engineering documentation. • The documents produced and maintained are an integral part of the project. No ambiguity or inconsistency exists between the programs/software loaded on the control system and the engineering documentation. • Automatic prevention of duplication of numbering or ambiguity is built into the system. The system contains master templates for each type of document produced or maintained. Employer’s Health And Safety Requirements The Contractor shall comply with all South African COVID19 regulations/law. The Contractor acts in accordance with the health and safety requirements stated in the Works Information. In carrying out its obligations to the Employer in terms of this contract; in providing the Works; in using Plant, Materials and Equipment; and while at the Site for any reason, the Contractor complies and procures and ensures the compliance by its employees, agents, Sub-Contractors and mandatories with:
Engineering Documentation. Engineering Documentation includes all written information which P-Com retains after production release of a product. This will vary based upon the type and complexity of each particular assembly, but will at a minimum include all documentation required by P-Com's ISO certified engineering process. Typical Engineering Documentation consists of:
Engineering Documentation. All engineering documentation is stored, classified and accessed via a structured document hierarchy and document numbering system in the EDMS. The engineering documentation always reflects the latest change or modification. Older revisions of engineering documentation are retained and stored with the relevant revision information for a user defined period. All engineering documentation is produced using a documentation management system to ensure an accurate reflection of the system configuration and status at all times. All engineering documents managed by the document management system are dynamic.
