AIRWORTHINESS - DEFINITIONS . ASTM revises a standard to make changes to its technical content. Compliance with the export requirements of the State of Registry shall be mandatory. 1) Coordinate with the operator/applicant to schedule inspection of the aircraft. The trimming controls shall not be adjusted during the maneuvers.”, FAA Section 4.3.2.3 “With landing gear and flaps extended, power necessary to maintain level flight at 1.1 V. (1) From the fully extended position to the most extended gated position; (2) Between intermediate gated positions, if applicable; and, (3) From the least extended gated position to the fully retracted position.”, FAA Section 4.7 “It shall be possible, while in the landing configuration, to complete a landing without causing substantial damage or serious injury, and without exceeding the temporary one-hand control force limits specified in Table 1, appropriate for the type of control, following an approach to land under the following conditions;”, FAA Section 5.3.1.3 “In a descent with idle power at a speed of 1.3 V, FAA Section 9.3.4 “If the procedure set forth in 9.3.3.2 is used to demonstrate compliance and marginal conditions existing during flight test with regard to reversal of primary longitudinal control force, flight tests shall be accomplished from the normal acceleration at which a marginal stick force per g condition is found to exist to the applicable limit specified in 9.3.2.1.”, FAA Section 4.1.4 “Appendix X1 through Appendix X4 provides, within the limitations specified within the appendix, a simplified means of compliance with several of the requirements set forth in sections 4.2 to 4.26 and 7.1 to 7.9 that can be applied as one (but not the only) means to comply. Certification requirements for civil [commercial] aircraft are derived from ICAO Annex 8 Airworthiness of Aircraft [ICAO, 2016] and the ICAO Airworthiness Manual, Part V State of Design and State of Manufacture [ICAO, 2014]. An airworthiness directive (AD) is a regulatory notice sent out by the FAA to the registered owner of an aircraft informing the owner of a condition that prevents the aircraft from continuing to meet its conditions for airworthiness. on NARA's archives.gov. Use the PDF linked in the document sidebar for the official electronic format. Each ICAO contracting state then establishes its own legal framework to implement the internationally agreed standards and recommended practices. Notices in this series will also be used to introduce new requirements. ASTM International copyrights these consensus standards and charges the public a fee for service. If the simplified methods in appendix X1 through X3 are used, they must be used together in their entirety.”, FAA Section X1.1.1 “The methods provided in this appendix provide one possible means (but not the only possible means) of compliance and can only be applied to level 1 and level 2 low speed airplanes.”, FAA X2.1.1 “The methods provided in this appendix provide one possible means (but not the only possible means) of compliance and can only be applied to level 1 and level 2 low speed airplanes.”, FAA X3.1.1 “The methods provided in this appendix provide one possible means (but not the only possible means) of compliance and can only be applied to level 1 and level 2 low speed airplanes.”, FAA X4.1.1 “The methods provided in this appendix provide one possible means (but not the only possible means) of compliance and can only be applied to level 1 low speed airplanes.”, FAA 4.4.1 “For metallic (aluminum), unpressurized, non-aerobatic, low-speed, level 1 airplanes, applicants can demonstrate a 10,000 hour safe-life by limiting the `1g' gross stress, at maximum takeoff weight, to no more than 5.5 ksi. GEN.250 General requirements ... occurrence reporting applicable to the airworthiness of aircraft; and (e) the registration of aircraft; and (f) the issuance of radio licences. Scope of Requirements (A) The requirements contained herein are those dealing with the design, construction, and flight characteristics of aircraft for use in air commerce. Inspect the Aircraft. The aircraft must meet the requirements of the original type certificate. Manager, Small Airplanes Standards Branch, Policy and Innovation Division, Aircraft Certification Service. Short Title Compliance Due at A/F Hrs/ Date E FE NA 1. to the courts under 44 U.S.C. documents in the last year, 357 Aircraft maintenance is the performance of tasks required to ensure the continuing airworthiness of an aircraft or aircraft part, including overhaul, inspection, replacement, defect rectification, and the embodiment of modifications, compliance with airworthiness directives and repair. Since all applicable columns are empty for 4.1, that subsection is applicable to the aircraft. In other cases, the means of compliance, while based on ASTM consensus standards, include additional FAA provisions necessary to comply with the airworthiness requirements of amendment 23-64. Aircraft maintenance is the performance of tasks required to ensure the continuing airworthiness of an aircraft or aircraft part, including overhaul, inspection, replacement, defect rectification, and the embodiment of modifications, compliance with airworthiness directives and repair. Document Drafting Handbook documents in the last year, 73 An Airworthiness Certificate is issued by the FFA only after the aircraft has been inspected and has met requirements of 14 CFR part 21 and is in a condition for safe operation. The regulations in parts 119, 121, and 135 relate directly to air carrier maintenance programs and reflect the highest possible degree of safety in … publication in the future. See https://www.federalregister.gov/​documents/​2016/​12/​30/​2016-30246/​revision-of-airworthiness-standards-for-normal-utility-acrobatic-and-commuter-category-airplanes. Aircraft Aging 7. These markup elements allow the user to see how the document follows the Editorial, reapproval, revision or withdrawal: The FAA expects a suitable consensus standard to be reviewed periodically. Here is a typical AD compliance record that could be used for a general aviation aircraft, or a large transport aircraft. documents in the last year, 1452 (c) For aircraft with a certificate of airworthiness issued for a period of 12 months or less, suitable contracts must be established with an approved maintenance organisation prior to any maintenance being performed. Inspection Requirements 5. B. informational resource until the Administrative Committee of the Federal Operators of U.S.-registered airplanes are required by general airworthiness and operational regulations to perform maintenance using methods Federal, State and Local Regulations 4. In promulgating part 23, amendment 23-64 [3] Airplanes certificated under part 23 are typically used for recreation, training, personal travel, and limited commercial applications. For airplanes that have ... general airworthiness and operational regulations to perform maintenance using methods documents in the last year, 951 Only official editions of the “50 volts/meter”, FAA Section 4.2.3.3 “From 40 to 400 MHz, use conducted susceptibility tests, starting at a minimum of 30 mA at 40 MHz, decreasing 20 dB per frequency decade to a minimum of 3 mA at 400 MHz.”. on Airworthiness Directives (ADs) are issued by the FAA when an unsafe condition exists in a type-certificated product, and that condition is likely to exist in other products of the same type design. documents in the last year, 312 One airworthiness regulation is found in ICAO international standard of Annex 8 to Chicago Convention on International Civil Aviation which defines "airworthy" - in respect of an aircraft, engine, propeller or part there of - as "The status of an aircraft, engine, propeller or part when it conforms to its approved design and is in a condition for safe operation". SINGAPORE AIRWORTHINESS REQUIREMENTS PART 39 SECTION 1 – REQUIREMENTS SAR-39.1 General This SAR-39 prescribes the requirements governing the issue of Airworthiness Directives that are applicable to Singapore aircraft and any aircraft component to be fitted on Singapore aircraft. It is not an official legal edition of the Federal 39.69 Airworthiness Directives compliance 12 39.71 Alternative means of compliance with mandatory continued airworthiness requirements 12 Subpart E — Aircraft Records 13 39.73 Maintenance and continuing airworthiness records 13 39.75 Retention of records 14 39.77 Transfer of maintenance records 15 39.79 Technical log 15 12/23/2020, 146 12/23/2020, 41 Certification requirements for civil [commercial] aircraft are derived from ICAO Annex 8 Airworthiness of Aircraft [ICAO, 2016] and the ICAO Airworthiness Manual, Part V State of Design and State of Manufacture [ICAO, 2014]. The applicant must show effective stress concentration factors of 4 or less in highly loaded joints and use materials or material systems for which the physical and mechanical properties are well established.”, FAA 6.1 “For bonded airframe structure, the residual strength of bonded joints shall be addressed as follows: For any bonded joint, the failure of which would result in catastrophic loss of the airplane, the limit load capacity must be substantiated by one of the following methods.”, FAA Section 4.1.6 “Engine mount and supporting structure must withstand 18.0 g forward for engines installed behind and above the seating compartment.”, FAA Section 3.2.1 “aircraft type code, n—an Aircraft Type Code (ATC) is defined by considering both the technical considerations regarding the design of the aircraft and the aeroplane certification level established based upon risk-based criteria; the method of defining an ATC applicable to this practice is defined in Specification F3061/F3061M.”, FAA Section 4 Example “Example—An aircraft with an ATC of 1SRLLDLN is being considered. edition of the Federal Register. the official SGML-based PDF version on govinfo.gov, those relying on it for with the Airworthiness Review Declaration in accordance with CAR GEN.161(d). AC 25-28 Compliance of Transport Category Airplanes with Certification Requirements for Flight in Icing Conditions AC 25.253-1 High-Speed Characteristics AC 25.335-1 Design Dive Speed AC 25.491-1 Taxi, Takeoff, and Landing Roll Design Loads Technical Information 1. This table of contents is a navigational tool, processed from the Continuing Airworthiness of Aircraft is the responsibility of the owner or operator of aircraft. Richard Sheng, in Systems Engineering for Aerospace, 2019. Talk about each line and type of entry as they appear. Delete ASTM F3264-19, section 9.1.1.2(a). The President of the United States issues other types of documents, including but not limited to; memoranda, notices, determinations, letters, messages, and orders. Note: Each line will come in one at time and fade. headings within the legal text of Federal Register documents. This repetition of headings to form internal navigation links has no substantive legal effect our. 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