(a) To be eligible for a repairman certificate a person must (1) Be at least 18 years of age; (2) Be specially qualified to perform maintenance on aircraft or components thereof, appropriate to the job for which he is employed; (5) Replacing defective safety wiring or cotter keys. Replacing prefabricated fuel lines. (d) Transfer of life-limited parts. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. (7) Other methods. 43-37, 66 FR 21066, Apr. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (a) Maintenance record entries. The tests in (e) through (j) apply only to Mode S transponders. Disposition of life-limited aircraft parts. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. (2) Replacing elastic shock absorber cords on landing gear. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. result, it may not include the most recent changes applied to the CFR. Displaying title 14, up to date as of 2/27/2023. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. user convenience only and is not intended to alter agency intent Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. The part may be legibly marked using a permanent method showing its current life status. The test point shall be approached at a rate compatible with the test equipment. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (5) Segregation. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. A logbook (or log book) is a record used to record states, events, or conditions applicable to complex machines or the personnel who operate them. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. Content, form, and disposition of records for inspections conducted under parts 91 and 125 and 135.411(a)(1) and 135.419 of this chapter. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. FAA acceptance is also required for certificate holders who use electronic records, and the electronic signatures associated with those records, to satisfy the requirements of parts 141, 142, and 147. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. Acceptable methods include: (1) Record keeping system. (6) Batteries - for improper installation and improper charge. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. No. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. ( 1) Persons must present their pilot certificate, medical certificate, logbook, or any other record required by this part for inspection upon a reasonable request by - ( i) The Administrator; ( ii) An authorized representative from the National Transportation Safety Board; or ( iii) Any Federal, State, or local law enforcement officer. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. (ii) Hysteresis. [Doc. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (3) Non-permanent marking. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. The part may be legibly marked using a non-permanent method showing its current life status. 106(g) (Revised Pub. The date the work was completed. This document is available in the following developer friendly formats: Information and documentation can be found in our guide. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. the requirements of parts 91K, 121, 125, 133, 135, and 145. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. [Amdt. (1) Persons must present their pilot certificate, medical certificate, logbook, or any other record required by this part for inspection upon a reasonable request by - (i) The Administrator; (ii) An authorized representative from the National Transportation Safety Board; or (iii) Any Federal, State, or local law enforcement officer. For miscellaneous technical amendments to this part 43, see Amdt. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. (b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. 1993, 29 FR 5451, Apr. This inspection will be recorded in the aircraft maintenance records. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). The tag or record must include the part number, serial number, and current life status of the part. (4) Appliance major repairs. Choosing an item from The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. The date of completion. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. The test point shall then be approached at a rate of approximately 3,000 feet per minute. 43-37, 66 FR 21066, Apr. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. FAR 43.9 Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, 135.411 (a) (1), and 135.419 of this chapter). Pressing enter in the search box The eCFR is displayed with paragraphs split and indented to follow (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. The error at all test points must not exceed the tolerances specified in Table I. 101, 610, 72 Stat. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. Comments or questions about document content can not be answered by OFR staff. Download Free Template. 1993, 29 FR 5451, Apr. Typical Maintenance entry for 100hr/annual inspection Reference: FAA-G-8082-11 IA KNOWLEDGE TEST INFORMATION FIGURE 9.-Example of a record entry for an annual inspection in which the aircraft was found to be unairworthy March 30, 1998 Total Aircraft Time 1853.00 Hours Tach Reading 975.80 e. Section 91.417(a)(1)(ii). 4, 1987, as amended by Amdt. of Transportation Act (49 U.S.C. (6) Electrical system - for chafing and improper operation of switches. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. The life status must be updated each time the part is removed from a type certificated product. 43.15 Additional performance rules for inspections. This applies to owner maintenance as well. (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. (v) Replacement of outer laminations on fixed pitch wood propellers. It typically consists of several stages, such as pre-alpha, alpha, beta, and release candidate, before the final version, or "gold," is released to the public. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (1) Airframe major repairs. The ASTM data approved by the SLSA manufacturer for major repairs and alteration is FAA-accepted data and is required to be recorded in the aircraft records according to ASTM F 2483-05, section 9, 1-4. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. Additional performance rules for inspections. It is not an official legal edition of the CFR. (iii) Performed without the use of tools and/or special equipment. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. No. (2) Shock absorbing devices - for improper oleo fluid level. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. (1) Airframe major alterations. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. SB-115 (10/26/83) -- Deflation Panel Pull Forces . (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. The aircraft owner is the one who applies for the permit, using FAA form 8130-6, which is actually an application for a U.S. airworthiness certificate. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. 43-39, 69 FR 44863, July 27, 2004]. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. No. (iii) After effect. (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. 91.417 Maintenance records. When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. 1/1.1 Although the applicable regulations describe the types of maintenance records that must be made and kept, the regulations do not set forth the format or form of the record. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. This system may include electronic, paper, or other means of record keeping. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. 43.11 Content, form, and disposition of records for inspections conducted under parts 91 and 125 and 135.411(a)(1) and 135.419 of this chapter. 43-40, 71 FR 40877, July 14, 2005]. (Secs. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. information or personal data. 6(c), Dept. 14. No. 13, 2013 59 likes 20,611 views Download Now Download to read offline Education FAA Safety Team Central Florida Follow Advertisement Advertisement Recommended Aircraft maintenance and manuals week 2 Jairo Gutierrez 6.2k views 28 slides In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. If your org uses Okta AD agent version 3. If you have questions or comments regarding a published document please Fri, 05/01/2015 - 12:00. book to meet the regulatory requirements. [Amdt. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. (2) Powerplant major repairs. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. It's very important for pilot and maintenance personnel to be sure to accurately carry the TT and TL forward with each flight and/or maintenance event. (9) Accessories - for apparent defects in security of mounting. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . As you know, 14 C.F.R. Pre-alpha refers to the early stages of development, when the software is . (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. 23, 1964, as amended by Amdt. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. Learn more about the eCFR, its status, and the editorial process. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. FAA STANDARDS FOR ELECTRONIC RECORDS. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. 43-52, 87 FR 31414, May 24, 2022], (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. (b) Rotorcraft. 43.7 Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. 23, 1964, as amended by Amdt. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (ii) Repairing or machining of steel hubs. FAR). (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. Each is a special inspection unto itself; they're all different. 23, 1964, as amended by Amdt. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (a) Maintenance record entries. The interrogations should be made at a nominal rate of 50 interrogations per second. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. However, those who maintain separate records for the airframe, power plant, propellers, and other components must document the 100-hour inspection, if required, in the record of each component (see 14 CFR 43.11 (a)). Aircraft Inspection and Repair - Federal Aviation . If it had been a non-FAA-approved part, a Form 337 would not be required. 27, 2001], (a) General. switch to drafting.ecfr.gov. 27, 2001; Amdt. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. Before the permit is issued, an FAA inspector may personally inspect the aircraft, or require it to be inspected by an FAA certificated A&P mechanic or an appropriately certificated repair station, to determine its safety for the intended flight. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. 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