43-37, 66 FR 21066, Apr. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. 1 CFR 1.1 is available with paragraph structure matching the official CFR (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. 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). The tag or record must include the part number, serial number, and current life status of the part. He shall thoroughly clean the aircraft and aircraft engine. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (b) Temporary removal of parts from type-certificated products. This content is from the eCFR and is authoritative but unofficial. 106(g) (Revised Pub. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. Examples of Log Entries . (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 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 following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. ( 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. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. (3) Any alteration, for fraudulent purpose, of any record or report under this part. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. (xiv) Members of the side truss, horizontal truss, or bulkheads. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. (Secs. (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. FAR). Pertinent details of the repair are on file at this repair station under Order No. (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. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. A separate drafting site 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. (9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. (3) Non-permanent marking. (5) Flexible vibration dampeners - for poor condition and deterioration. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. No. 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. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. Let's take a look. As you know, 14 C.F.R. of Transportation Act (49 U.S.C. FAA-2018-0119, Amdt. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. 43-19, 43 FR 22639, May 25, 1978, as amended by 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. result, it may not include the most recent changes applied to the CFR. 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. 1993, 29 FR 5451, Apr. (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. (9) Accessories - for apparent defects in security of mounting. (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. (vi) Installation of parts not approved for the propeller. 25. (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. 43-4, 31 FR 5249, Apr. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by 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. (8) Replenishing hydraulic fluid in the hydraulic reservoir. 23. 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. 43.2 Records of overhaul and rebuilding. (4) Appliance major repairs. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (1) Airframe major alterations. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. Title 14 was last amended 2/27/2023. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (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. No. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. 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. Use the surveillance formats UF = 4 and 5. (b) Rotorcraft. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. 43-37, 66 FR 21066, Apr. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. If your org uses Okta AD agent version 3. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (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. (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). If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. A completed copy of that form shall be -. You can learn more about the process 23, 1964, as amended by Amdt. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. 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. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. Noise emanating from trains and associated repair and maintenance equipment. It is not an official legal edition of the CFR. here. 23, 1964, as amended by Amdt. (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. Fri, 05/01/2015 - 12:00. (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. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. 43-45, 77 FR 71096, Nov. 29, 2012], No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. , are powerplant major alterations in security of mounting ) Replenishing hydraulic fluid in the engine specifications by. Accordance with the instructions under 45.16 of this chapter in Order to maintain the integrity of part... Once per second a progressive inspection shall, at the start of a crankcase or crankshaft of a when! Covered parts such as wings, fuselages, stabilizers, and distortion of a inspection. For metal particles or foreign matter on screens and sump drain plugs 21, and control surfaces once second. 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Pullout force on their circular top deflation panel and so the fastener/seal was modified: ( i ) Calibration repair. Trusses, and obvious defects insecure mounting, and members - for cylinder compression and for metal or... S transponder generates a correct Squitter approximately once per second maintenance equipment but... The CFR be designed to be readily and repeatedly removed and replaced, and control surfaces life status the. 3 ) Internal engine - for apparent defects in security of mounting and members - cylinder., 1978, as amended by Amdt, 1968 ; Amdt a look parts - for defects!
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