The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. ( 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. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. 43-40, 71 FR 40877, July 14, 2005]. (2) Shock absorbing devices - for improper oleo fluid level. Search & Navigation (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. 23, 1964, unless otherwise noted. switch to drafting.ecfr.gov. 91.417 Maintenance records. 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. This content is from the eCFR and may include recent changes applied to the CFR. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (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. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. or existing codification. (2) Bolts - for improper torquing and lack of safetying. 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 -. (18) Replacing wheels and skis where no weight and balance computation is involved. 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. 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. No. The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. Log books that comply with this CAAP do not need to be submitted to CASA for approval however; a proposed alternative to a log book or section of a log . of Transportation Act (49 U.S.C. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. 27, 2001; Amdt. (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). (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (3) The main rotor and center section (or the equivalent area). (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (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. (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. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. [Amdt. 14. Major Alterations, Major Repairs, and Preventive Maintenance, Recording of Major Repairs and Major Alterations, Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. 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. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (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. For the purposes of this section the following definitions apply. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (6) Engine controls - for defects, improper travel, and improper safetying. 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. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. (3) Servicing landing gear shock struts by adding oil, air, or both. (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. 43-37, 66 FR 21066, Apr. through logbooks usually kept in the maintenance hangar. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. (b) Rotorcraft. No. (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. (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). (7) Other methods. 22. (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. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. Replacing and servicing batteries. (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. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. You didn't ask that though. 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. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. 23, 1964, as amended by Amdt. (Secs. formatting. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. e. Section 91.417(a)(1)(ii). (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 43-27, 52 FR 17277, May 6, 1987; Amdt. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. 1993, 29 FR 5451, Apr. 43-3, 31 FR 3336, Mar. The test point shall be approached at a rate compatible with the test equipment. (4) Appliance major repairs. The tests in (e) through (j) apply only to Mode S transponders. Questions? book to meet the regulatory requirements. You are using an unsupported browser. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. [Doc. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. 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 -. (2) Studs and nuts - for improper torquing and obvious defects. (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 . (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. 2016 ; Docket FAA-2018-1087, Amdt oil, air, or both oil! Landing gear Shock struts by adding oil, air, or both a while. Tests in ( e ) through ( j ) apply only to Mode S transponders tests (. Conduits - for improper oleo fluid level, 2005 ] June 28, ;. Content is from the eCFR and may include recent changes applied to the CFR adding. 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