Manager, Small Airplanes Standards Branch, Policy and Innovation Division, Aircraft Certification Service. RELATED REQUIREMENTS. 12/23/2020, 41 documents in the last year, 10 All powered aircraft with a MCTOW of 5700 Kg or less and standard or restricted category airworthiness certificates. Amendment 23-64 established airworthiness requirements based on the level of safety of amendment 23-63 regulations, except for areas addressing loss of control and icing where the safety level was increased. If the proposed certificate holder will be owned by a partnership, each member of the partnership must be a U S citizen, if owned by a corporation or association created or organized under the laws of the United States or of any State, Territory, or possession of the United States, the president and two-thirds or more of the board of directors and other managing officers thereof must be a citizen of the United States and at least 75 per cent of the voting in… In promulgating part 23, amendment 23-64 [3] EASA AMC-20 - General Acceptable Means of Compliance for Airworthiness of Products, Parts and Appliances EASA CS-26 - Additional airworthiness specifications for Operations Acceptance of maintenance tasks carried out by pilots - Part 145 caters for certain maintenance tasks to be carried out by a suitably qualified pilot. This document has been published in the Federal Register. daily Federal Register on FederalRegister.gov will remain an unofficial The President of the United States manages the operations of the Executive branch of Government through Executive orders. Additional Resources • Aircraft are designed for operation within an operating envelope, which depends on speed and structural load factors. 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, 357 corresponding official PDF file on govinfo.gov. The Federal Aviation Administration ( FAA ) expects this rule will enable faster installation of innovative, safety-enhancing technologies into small airplanes, while reducing costs for the aviation industry. This site displays a prototype of a “Web 2.0” version of the daily Richard Sheng, in Systems Engineering for Aerospace, 2019. This proposed AD was prompted by reports that, during investigation of a fuel leak, fatigue cracking was found on the forward inboard side of … has no substantive legal effect. These markup elements allow the user to see how the document follows the 2. The aircraft must meet the requirements of the original type certificate. These tools are designed to help you understand the official document For example, applicants with novel designs, such as unmanned airplanes or vertical takeoff and landing airplanes that are outside the scope and applicability of these consensus standards must propose alternative means of compliance, applicable to their designs, to be accepted under § 23.2010. Effective: on Issue . The FAA maintains a list of accepted means of compliance on the FAA website at https://www.faa.gov/​aircraft/​air_​cert/​design_​approvals/​small_​airplanes/​small_​airplanes_​regs/​. “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.”. 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. the current document as it appeared on Public Inspection on Each document posted on the site includes a link to the Compliance with these revisions is required by 14 CFR 91.403(c). AIRWORTHINESS - DEFINITIONS . Page last modified: October 24, 2017 1:04:43 PM EDT, This page was originally published at: https://www.faa.gov/aircraft/air_cert/airworthiness_certification/std_awcert/std_awcert_regs/regs/, Get Form 337, Major Repair and Alteration, Certification Procedures for Products and Parts, Airworthiness Standards: Normal Category Airplanes, Airworthiness Standards: Transport Category Airplanes, Airworthiness Standards: Normal Category Rotorcraft, Airworthiness Standards: Transport Category Rotorcraft, Airworthiness Standards: Manned Free Balloons, Scope and Detail of Items to be Included in Annual and 100-Hour Inspections. Document Drafting Handbook should verify the contents of the documents against a final, official provide legal notice to the public or judicial notice to the courts. We’ve made big changes to make the eCFR easier to use. Procedures for certification of aeronautical products (aircraft, engines and propellers) are published in each state. 23.2135: ASTM F3264-19, section 5.8, combined with the changes in the following table: 23.2150: ASTM F3264-19, section 5.11, after replacing ASTM F3180/F3180M-19 with ASTM F3180/F3180M-16. Today this evolution continues with the single largest update to the design and airworthiness requirements for service aircraft since the inception of DS970 in 1983. Add an FAA-accepted means of compliance for the windshield luminous transmittance aspects of § 23.2600, such as the provisions of § 23.775(e), amendment 23-49. The current part 23 airworthiness standards are largely prescriptive, meaning that they describe detailed design requirements, and are based on airplane … 23.2500: ASTM F3264-19, section 9.1, combined with the following changes: 1. SAR-39.3 Effectivity (a) This SAR-39 was first issued on and became 23.2415: ASTM F3264-19, section 8.4, combined with the following changes: 2. 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. Overseas Territories Aviation Circulars are issued to provide advice, guidance and information on standards, practices and procedures necessary to support Overseas Territory Aviation requirements. 09/21/2020 at 8:45 am. NEW ZEALAND CIVIL AIRWORTHINESS REQUIREMENTS VOLUME 2 AIRWORTHINESS DIRECTIVES SECTION A GLIDERS EIRAVION OY PIK 20 AD SCHEDULE In addition to the ADs scheduled below, relevant ADs in the ‘AIRCRAFT GENERAL’ AD Schedule and any other relevant ADs in Section C ‘COMPONENTS AND EQUIPMENT’ shall be complied with * More information and documentation can be found in our 23.2600: ASTM F3264-19, section 10.1, combined with the following changes: 1. 1) Coordinate with the operator/applicant to schedule inspection of the aircraft. Applicants may also propose alternative means of compliance for FAA review and possible acceptance. The documents posted on this site are XML renditions of published Federal Before issuing a standard or special airworthiness certificate, or a special flight permit, ODA unit members must inspect the aircraft, and document the results of the inspection as described in FAA Order 8130.2 ( PDF ) . Ref Public Law 104-113 as amended by Public Law 107-107. The Public Inspection page regulatory information on FederalRegister.gov with the objective of Federal Register. maintenance performed on its aircraft, and the mechanic is responsible for the performance of maintenance and airworthiness of the aircraft). Since the “1” aeroplane certification level column, the “L” stall speed column, and the “D” meteorological column for 4.2.1 all contain white circles, then that subsection is not applicable; however, for an aircraft with an ATC of 1SRMLDLN, 4.2.1 would be applicable since the “M” stall speed column does not contain a white circle.”. [FR Doc. Order 8040.1 Airworthiness Directives Order 8040.5 Airworthiness Directive Process for Mandatory Continuing Airworthiness Information Order 8110.103 Alternate Methods of Compliance Order 8100.5 Aircraft Certification Service Mission, Responsibilities, Relationships, and Programs 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". AR 95-1() establishes policy and procedures for Army aircraft operations. for better understanding how a document is structured but ASTM issues editorial changes—denoted by a superscript epsilon in the standard designation (e.g., F3235-17ε1)—to correct information that does not change the meaning or intent of a standard. on 1.0 General Guidelines and Requirements. documents in the last year, 648 Notices in this series will also be used to introduce new requirements. documents in the last year, 67 23.2615: ASTM F3264-19, section 10.4, combined with the changes in the following table: 23.2620: ASTM F3264-19, sections 5.15 AND 10.5. 29 February 2012 . Continuing Airworthiness of Aircraft is the responsibility of the owner or operator of aircraft. In some cases, the Administrator finds sections of ASTM Standard F3264-19, “Standard Specification for Normal Category Aeroplanes Certification,” without changes, are accepted as means of complying with the airworthiness requirements of amendment 23-64, within the scope and applicability of the consensus standards. Aircraft Aging 7. The requirements are the same. Overview 3. on The President of the United States issues other types of documents, including but not limited to; memoranda, notices, determinations, letters, messages, and orders. ... AC 23-19 Airframe Guide for Certification of Part 23 Airplanes AC 23-21 Airworthiness Compliance Checklists Used to Substantiate The Airworthiness Review Report is a collection of data on the status of the build standard and continued airworthiness of an aircraft that will assist organisations and regulators in their assessment of the aircraft during the Certificate of Airworthiness process. It is not an official legal edition of the Federal ASTM policy is that a consensus standard should be reviewed in its entirety by the responsible subcommittee and must be balloted for reapproval, revision, or withdrawal, within five years of its last approval date. The FAA reviewed 35 published ASTM consensus standards, developed by ASTM Committee F44, as the basis for means of compliance to 65 sections Start Printed Page 59401of part 23, amendment 23-64. the FAA has been working with industry and other stakeholders lop consensus standards for use as a means of compliance in certificating small airplanes under Title 14, Code of Federal Regulations (14 CFR) part 23. The Public Inspection page may also 1. We invite you to try out our new beta eCFR site at https://ecfr.federalregister.gov. documents in the last year, 951 12/23/2020, 304 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. B. ADs have the same authority as FARs, and as such, compliance with an Airworthiness Directive is … and services, go to Here is a typical AD compliance record that could be used for a general aviation aircraft, or a large transport aircraft. Short Title Compliance Due at A/F Hrs/ Date E FE NA Operators of U.S.-registered airplanes are required by general airworthiness and operational regulations to perform maintenance using methods 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 Aircraft Modifications 8. Requirements for compliance with other applicable parts of Title 14 of the Code of Federal Regulations (14 CFR) may also apply, depending upon the aircraft type, previous certifications (14 CFR part 43, § 43.1 (b) (1)), and the operational purpose of the Special Airworthiness Certificate. Compliance with necessary requirements: Aircraft, or any of its parts, is designed and built according to the studies and tested criteria to fly in safe conditions. This ensures that the aircraft complies with airworthiness standards and safe operating conditions. Type Certificate Data Sheet (TCDS) = Documents issued by the FAA that describe the aircraft’s airworthiness requirements for a specific type, make, and model. Registration and Re-Registration Requirements 3. GENERAL REQUIREMENTS (ACE SYSTEM PARAMETERS) and DETAILED GUIDANCE (ACE SYSTEM METHOD OF COMPLIANCE pairs (sections 4 and 5 respectively in this handbook, organized by correlating paragraph numbers) could be directly put into an airworthiness document. The work flow for issuance of these certificates must meet FAA requirements, including an inspection of the aircraft and review of the aircraft build records. documents in the last year, 789 Purpose. Technical Information 1. documents in the last year, by the Environmental Protection Agency On August 30, the final rule overhauling airworthiness standards for general aviation airplanes published in December of 2016 officially went into effect. Airplanes certificated under part 23 are typically used for recreation, training, personal travel, and limited commercial applications. Register documents. 12/23/2020, 202 39.69 Airworthiness Directives compliance 13 39.71 Alternative means of compliance with mandatory continued airworthiness requirements 13 Subpart E — Aircraft Records 14 39.73 Maintenance and continuing airworthiness records 14 39.75 Retention of records 15 39.77 Transfer of maintenance records 16 39.79 Technical log 16 The Airworthiness Review Report is a collection of data on the status of the build standard and continued airworthiness of an aircraft that will assist organisations and regulators in their assessment of the aircraft during the Certificate of Airworthiness process. In general, this AC covers 14 ... AC 23-19 Airframe Guide for Certification of Part 23 Airplanes AC 23-21 Airworthiness Compliance Checklists Used to Substantiate • Affects continued airworthiness issues and/or safety improvements for transport airplanes addressed via operational rules • Supports the ability of operators to comply with the operational rule requirements • May apply to TC, STC holders, and certain applicants, as appropriate • May Require actions of DAHs, such as: – compliance plan, Inspect the Aircraft. Federal Register issue. This prototype edition of the on FederalRegister.gov developer tools pages. Order 8040.1, Airworthiness Directives Order 8040.5, Airworthiness Directive Process for Mandatory Continuing Airworthiness Information Order 8100.5, Aircraft Certification Service Mission, Responsibilities, Relationships, and Programs Order 8110.103, Alternative Methods of Compliance … Jurisdictional heterogeneity. See 14 CFR 39 for the a more detailed definition of an AD and the associated compliance requirements. documents in the last year, 23 Requirement: To ensure that passenger and crew compartment interior materials meet the Revisions to consensus standards serving as the basis for means of compliance accepted by this notice will not be automatically accepted and will require further FAA acceptance in order for the revisions to be an accepted means of compliance. Add an FAA-accepted means of compliance for the pilot compartment view with formation of fog or frost aspects of § 23.2600, such as the provisions of § 23.773(b), amendment 23-45. For all single-engined aircraft with a Malaysian Certificate of Airworthiness equipped with an engine-driven electrical generating system, compliance with paragraph 2.2 and 2.3, or with a DCA approved alternative providing an equivalent level of airworthiness is required not later than 01 July 1998. About the Federal Register AMA: 549/1B Date: 1 April 1996 Subject: Amateur-Built Aircraft: General 1. Achieving this level of safety through compliance with amendment 23-64—for a given certification project—may require use of additional means of compliance beyond those accepted by this notice, depending on the details of the specific design. Open for Comment, Requirements for Certain Transactions Involving Convertible Virtual Currency or Digital Assets, Economic Sanctions & Foreign Assets Control, Consistency and Transparency in Considering Benefits and Costs in the Clean Air Act Rulemaking Process, Presidential Policy Directive 6 (Space Policy), “National Strategy for Space Nuclear Power and Propulsion”, Light-Walled Rectangular Pipe and Tube From Mexico, Commerce in Explosives; 2020 Annual List of Explosive Materials, Alcohol, Tobacco, Firearms, and Explosives Bureau, Promoting Beautiful Federal Civic Architecture, Subpart G—Flightcrew Interface and Other Information, https://www.federalregister.gov/d/2020-17911, MODS: Government Publishing Office metadata, https://www.faa.gov/​aircraft/​air_​cert/​design_​approvals/​small_​airplanes/​small_​airplanes_​regs/​, https://www.federalregister.gov/​documents/​2016/​12/​30/​2016-30246/​revision-of-airworthiness-standards-for-normal-utility-acrobatic-and-commuter-category-airplanes, FAA Section 4.3.2 “Unless otherwise required, it shall be possible to carry out the following maneuvers without requiring the application of temporary one-hand control forces exceeding those specified in Table 1, appropriate for the type of control. This repetition of headings to form internal navigation links documents in the last year, 37 offers a preview of documents scheduled to appear in the next day's legal research should verify their results against an official edition of An FAA-accepted means of compliance for the powerplant instruments aspects of § 23.2615, such as the provisions of § 23.1305, amendment 23-52. ADs have the same authority as FARs, and as such, compliance with an Airworthiness Directive is … i) For aircraft registered in Malaysia, Airworthiness Notices issued by DCA. Counts are subject to sampling, reprocessing and revision (up or down) throughout the day. Flight School Requirements 6. (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. Add: An FAA accepted means of compliance for the turbine engine installation ice protection requirement of § 23.2415, on airplanes not approved for flight into known icing, such as the provisions of F3120/F3120M-19 section 7.2 and 7.3 (regardless of the operation requirements in F3120/F3120M-19 Table 1). Individual downloads or reprints of a standard (single or multiple copies, or special compilations and other related technical information) may be obtained through www.astm.org or contacting ASTM at (610) 832-9585 (phone), (610) 832-9555 (fax), or through service@astm.org (email). Requirements 2.1. of the issuing agency. publication in the future. Additionally, all civil aircraft must meet the following requirements: (1) The aircraft must have an effective U.S. registration certificate on board during all operations as required by FAR Section 91.203. Due to errors identified in the Aircraft Type Code compliance matrix tables, applicability of individual requirements of standards must be established with the Small Airplane Standards Branch. Since all applicable columns are empty for 4.1, that subsection is applicable to the aircraft. Aircraft Certification Requirements. The OFR/GPO partnership is committed to presenting accurate and reliable This Circular relates to OTAR Parts 21 and 39. Means of Compliance Accepted in this Policy: The following is a list of part 23, amendment 23-64, sections followed by their corresponding means of compliance accepted by this notice. Delete ASTM F3264-19, section 9.1.1.2(a). Document page views are updated periodically throughout the day and are cumulative counts for this document. Submit a formal comment. documents in the last year, by the International Trade Administration The applicant must also obtain Ministerial permit to import the aircraft … on 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 Each ICAO contracting state then establishes its own legal framework to implement the internationally agreed standards and recommended practices. See https://www.faa.gov/​aircraft/​air_​cert/​design_​approvals/​small_​airplanes/​small_​airplanes_​regs/​. Compliance with these revisions is required by 14 CFR 91.403(c). For complete information about, and access to, our official publications 3.3.2.3 The exporting country shall provide a Noise Certificate. 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. Airworthiness is defined by the JSP553 Military Airworthiness Regulations (2006) Edition 1 Change 5 as: “The ability of an aircraft or other airborne equipment or system to operate without significant hazard to aircrew, ground crew, passengers (where relevant) or to the general public over which such airborne systems are flown.” This feature is not available for this document. 39.69 Airworthiness Directives compliance 13 39.71 Alternative means of compliance with mandatory continued airworthiness requirements 13 Subpart E — Aircraft Records 14 39.73 Maintenance and continuing airworthiness records 14 39.75 Retention of records 15 39.77 Transfer of maintenance records 16 39.79 Technical log 16 Restrictive maintenance requirements and airworthiness limitations are necessary operating conditions its own legal framework to implement the agreed. Model 777 airplanes may also propose alternative means of compliance accepted by this notice are one,... 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