(eg: 1993, 29 FR 5451, Apr. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. No. 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. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. (a) Except for work performed in accordance with 91.411 and 91.413, each registered owner or operator shall keep the following records for the periods specified in paragraph (b) of this section . 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. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. This new version now contains an entry for tracking GPS database updates. We recommend you directly contact the agency responsible for the content in question. (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). 43-36, 61 FR 19501, May 1, 1996; Amdt. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (e) Logging pilot-in-command flight time. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. 1993, 29 FR 5451, Apr. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (a) Maintenance record entries. (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) The date of the inspection and aircraft total time in service. 4, 1987, as amended by Amdt. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. formatting. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. information or personal data. 43-37, 66 FR 21066, Apr. (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. 42 U.S.C. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. If you have comments or suggestions on how to improve the www.ecfr.gov website or have questions about using www.ecfr.gov, please choose the 'Website Feedback' button below. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (1) Airframe major repairs. (ii) Monocoque or semimonocoque wings or control surfaces. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. No. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. [Doc. [Amdt. 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. 91.417 Maintenance records. (2) Seats and safety belts - for poor condition and apparent defects. 1354, 1421 through 1430 and 1502); (49 U.S.C. (18) Replacing wheels and skis where no weight and balance computation is involved. 43-37, 66 FR 21066, Apr. The part may be segregated using methods that deter its installation on a type-certificated product. Table of contents from a loose-leaf binder for maintenance records. The error at all test points must not exceed the tolerances specified in Table I. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. 43-39, 69 FR 44863, July 27, 2004]. (xxiii) The repair of portions of skin sheets by making additional seams. 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 -. (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. user convenience only and is not intended to alter agency intent (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. 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) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (28) The installations of anti-misfueling devices to reduce the diameter of fuel tank filler openings provided the specific device has been made a part of the aircraft type certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation does not involve the disassembly of the existing tank filler opening. 1301, 1430), [Doc. Displaying title 14, up to date as of 2/27/2023. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. Replacing and servicing batteries. Fri, 05/01/2015 - 12:00. switch to drafting.ecfr.gov. Use this checklist to: (iv) Complete disassembly of complex hydraulic power valves. 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. [Amdt. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (c) Preventive maintenance. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (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. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. FAA-2015-1621, Amdt. This web site is designed for the current versions of The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. or existing codification. 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. You are using an unsupported browser. The signature constitutes the approval for return to service only for the work performed. Logbook is built-in to the ForeFlight app, making it easy for pilots to log and share flights, track hours, review currency, record certificates and ratings, receive electronic instructor endorsements, and generate experience reports. Organization and Purpose 23. 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). (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. (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). (Secs. (d) Performance requirements. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (6) Electrical system - for chafing and improper operation of switches. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. 21. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. No. When the work is completed satisfactorily, a logbook entry that includes the following information is required, per 14 CFR 43.9: A description of the work performed indicating how it was accomplished by referencing documents acceptable to the FAA, such as manufacturer's manuals and FAA Advisory Circulars. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). If you have questions for the Agency that issued the current document please contact the agency directly. (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. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. While performing the inspection through 1430 and 1502 ) ; ( 49 U.S.C 3... 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