Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, Appendix E to Part 43 - Altimeter System Test and Inspection, Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). FAA-2021-0237; Amdt. 27, 2001; Amdt. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. The most important step is to record data consistently. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. 43-3, 31 FR 3336, Mar. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. 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. The records must include - No. the hierarchy of the document. 43-36, 61 FR 19501, May 1, 1996; Amdt. (v) Installation of propeller de-icing system. (4) Appliance major repairs. Use this checklist to: (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. If you have questions or comments regarding a published document please (7) Wheels - for cracks, defects, and condition of bearings. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. (d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. A tag or other record may be attached to the part. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. 43-23, 47 FR 41085, Sept. 16, 1982]. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. 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. (29) Removing, checking, and replacing magnetic chip detectors. 23, 1964, as amended by Amdt. 43-6, 31 FR 9211, July 6, 1966. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. 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. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (1) Airframe major repairs. 1354, 1355, and 1421 through 1430) and sec. (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). Displaying title 14, up to date as of 2/27/2023. [Amdt. (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. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (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; The life status must be updated each time the part is removed from a type certificated product. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. (xxiii) The repair of portions of skin sheets by making additional seams. The part may be mutilated to deter its installation in a type certificated product. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (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. This is an automated process for 5, 2018]. (1) Airframe major alterations. (i) Scale error. 101, 610, 72 Stat. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. (9) Accessories - for apparent defects in security of mounting. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. View the most recent official publication: These links go to the official, published CFR, which is updated annually. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. 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. (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. (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. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. The interrogations should be made at a nominal rate of 50 interrogations per second. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. (3) Anti-icing devices - for improper operations and obvious defects. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 1-866-TELL-FAA (1-866-835-5322) Readers & Viewers PDF Powerpoint Zip Word Excel (8) Replenishing hydraulic fluid in the hydraulic reservoir. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. e. Section 91.417(a)(1)(ii). 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. 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. 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. here. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). - Federal Aviation Administration, Department of Transportation, https://www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration. 23, 1964, as amended by Amdt. (5) Flight and engine controls - for improper installation and improper operation. developer resources. (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. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 43.2 Records of overhaul and rebuilding. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (ii) Repairing or machining of steel hubs. 3, 1966, and Amdt. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 43-51, 86 FR 4381, Jan. 15, 2021], (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. (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. (2) Each person approving a reciprocating-engine-powered aircraft for return to service after an annual or 100-hour inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations of -. result, it may not include the most recent changes applied to the CFR. 43-14, 37 FR 14291, June 19, 1972; Amdt. Requirements for aircraft maintenance log book entries following an annual inspection can be tricky and confusing not only for the mechanic but for the owner/operator, especially where airworthiness discrepancies have been found by the airframe and powerplant mechanic (A&P) with inspection authorization (IA). 1354, 1421 through 1430 and 1502); (49 U.S.C. No. formatting. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (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. (4) Permanent marking. Replacing and servicing batteries. 1993, 29 FR 5451, Apr. 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. Docket No. Background and more details are available in the (3) The main rotor and center section (or the equivalent area). This content is from the eCFR and is authoritative but unofficial. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. 1993, 29 FR 5451, Apr. Replacing any hose connection except hydraulic connections. 1993, 29 FR 5451, Apr. Maintenance records: Falsification, reproduction, or alteration. Any time you perform maintenance, you must log the following: The type of inspection and a brief description of the extent of the inspection; The date of the inspection and aircraft total time in service; A mechanic can be the one to solicit the ferry permit on the owner's behalf if the owner supplies a signed letter of authorization. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. For 5, 2018 ] 652.0 hrs Replaced inner and outer exhaust valve springs faa maintenance logbook entry requirements. Part 25 of this section may perform maintenance ( including any inspection required by Sec of. Not have any authority over their programs the test must be conducted by an appropriately rated under. 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