AS 13100:2021 pdf AESQ Quality Management System Requirements for Aero Engine Design and Production Organizations

AS 13100:2021 pdf AESQ Quality Management System Requirements for Aero Engine Design and Production Organizations
1. SCOPE
This standard establishes supplemental requirements for 9100 and 9145 and applies to any organization receiving it as part of a Purchase Order or other contractual document from a customer.
AS13100 also provides details of the Reference Materials (RM13xxx) developed by the SAE G-22 AESQ committee and listed in Section 2 – Applicable Documents, that can also be used by organizations in conjunction with this standard.
2. APPLICABLE DOCUMENTS
The following publications form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of other publications shall be the issue in effect on the date of the purchase order. In the event of conflict between the text of this document and references cited herein, the text of this document takes precedence.
Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.NOTE: *Internationally harmonized standards developed under the authority of the IAQG and listed here, as SAE International “AS” publications. Equivalent versions may be published by other standards bodies (e.g., European Committee for Standardization (CEN), Japanese Standards Association/Society of Japanese Aerospace companies (JSA/SJAC).
2.2 AESQ Publications
The AESQ Reference Manuals have been created to support the requirements of AS13100 by providing examples of acceptable means of compliance. These documents provide methodologies, templates, and case studies of the application of key processes required by the standard. The intent of these Reference Manuals is to standardize the processes and language for quality across the Aero Engine supply chain. In each case alternative approaches may be used if they meet the same intent and are agreed with the customer.
2.4 Other Publications
Copies of ISO documents are available online at https://webstore.ansi.org/.Copies of APQP documents are available at www.aiag.org. Copies of AWS documents are available from https://www.aws.org/standards. Copies of European Union Aviation Safety Agency (EASA) CS documents are available from https://www.easa.europa.eu/. Copies of VDA and EN standards are available from https://www.en-standard.eu/. Copies of NAS standards are available from https://www.aia- aerospace.org/standards. Copies of SNT document is available from https://www.asnt.org/.
A part, an assembly, installation equipment, launch equipment, recovery equipment, or support equipment for an aircraft or
aviation weapon system, that contains a characteristic, which failure, malfunction, or absence of could cause a catastrophic
or critical failure resulting in the loss of, or serious damage to, the aircraft, or weapon system, an unacceptable risk of
personal injury or loss of life, or an un-commanded engine shutdown that jeopardizes safety.
NOTE 1: Catastrophic – A failure that could result in death, permanent total disability, and/or financial loss exceeding a defined contractual limit.
NOTE 2: Critical – A failure that could result in permanent partial disability and/or injuries or occupational illness resulting in hospitalization of at least three personnel.
NOTE 3: Life Limited Part – Per 14CFR 33.70 engine, Life Limited Parts (LLP) are rotor and major static structural parts whose primary failure is likely to result in a hazardous engine effect. Typically, engine LLP include, but are not limited to, disks, spacers, hubs, shafts, high pressure casings, and nonredundant mount components. LLP are equivalent to Engine Critical Parts under EASA certification per CS-E 510 and 515.
NOTE 4: Sensitive Part – Sensitive Parts (SP) are part’s whose failure may, but is not likely to, result in a hazardous engine effect. The types of SP identified are a function of the specific engine architecture and therefore will vary from engine to engine.