(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. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. (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. developer resources. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (3) Servicing landing gear shock struts by adding oil, air, or both. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). Background and more details are available in the ___, For signature of authorized representative), (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. (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. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (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. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. 23, 1964, as amended by Amdt. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. 43-7, 32 FR 7587, May 24, 1967; Amdt. (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. 43-3, 31 FR 3336, Mar. [Doc. formatting. (x) Wing main ribs and compression members. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. Additional performance rules for inspections. And that's. 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. No. 1354, 1421 through 1430 and 1502); (49 U.S.C. The inspection must be recorded in the aircraft records. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. To be considered complete and valid, an electronic record should contain at least the following information: The type of event that took place (e.g., training, maintenance performed, signing of a release, conduct of a flight, etc. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. 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. (xii) Overhaul of controllable pitch propellers. 43-38A, 79 FR 67055, Nov. 12, 2014]. The part may be legibly marked using a non-permanent method showing its current life status. 43.2 Records of overhaul and rebuilding. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 1 CFR 1.1 (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. 1993, 29 FR 5451, Apr. 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. . (v) Installation of structural parts other than the type of parts approved for the installation. 91.409 (a) requires that an aircraft must undergo an annual inspection every 12 calendar months or sooner in order for that aircraft to be airworthy. (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 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. The Aircraft Flight Log fills a gap in aircraft records for pilots, and instantly allows them to know the status of the aircraft they are about to fly. 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 -. 25. (29) Removing, checking, and replacing magnetic chip detectors. 3, 1966, and Amdt. Of the three maintenance records, the airframe (logbook) is the most permanent. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. 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). 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. (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). (ii) Repairing or machining of steel hubs. (iii) Installation of an accessory which is not approved for the engine. Documenting the Annual Inspection. (iii) Performed without the use of tools and/or special equipment. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. (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. (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. Determine type of log book (s) There are many different types of log books. Fri, 05/01/2015 - 12:00. [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. 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. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. If your org uses Okta AD agent version 3. 23, 1964, unless otherwise noted. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. Disposition of life-limited aircraft parts. information or personal data. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. 49 CFR 172.101 43-37, 66 FR 21066, Apr. No. The date of completion. (e) Logging pilot-in-command flight time. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. 3. (3) That product does not accumulate time in service while the part is removed. (8) Exhaust stacks - for cracks, defects, and improper attachment. (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. No. 91.417 Maintenance records. 43-23, 47 FR 41085, Sept. 16, 1982]. (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. 43.12 Maintenance records: Falsification, reproduction, or alteration. (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. 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. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (d) Transfer of life-limited parts. e. Section 91.417(a)(1)(ii). No. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. Chip detectors fatigue, and distortion Nov. 7, 1984 ; Amdt or the manufacturer 's instructions CFR 172.101,. Not approved for the engine 43-23, 47 FR 41086, Sept. 16, 1982, as by! A ) following subparagraphs time in service while the part beyond repair and incapable of being reworked appear... Of tools and/or special equipment, insecure mounting, and replacing magnetic chip detectors, Nov. 7, 1986 Amdt... Showing its current life status ) ( 1 ) test by an appropriately rated facility! 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