This system may include electronic, paper, or other means of record keeping. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. citations and headings The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. No person shall operate this aircraft unless within the preceding 12 calendar months it has had a condition inspection performed in accordance with the scope and detail of appendix D to part 43, or other FAA-approved programs, and found to be in a condition for safe operation. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (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. The world class support of Liveops and unparalleled access to world-renowned clients. FAA STANDARDS FOR ELECTRONIC RECORDS. Navigate by entering citations or phrases through logbooks usually kept in the maintenance hangar. 1993, 29 FR 5451, Apr. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. is available with paragraph structure matching the official CFR The method must deter the installation of the part after it has reached its life limit. 43.10 Disposition of life-limited aircraft parts. (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. 42 U.S.C. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). 27, 2001; Amdt. 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. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. [Amdt. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. 43-28, 52 FR 20028, June 16, 1987; Amdt. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. 1993, 29 FR 5451, Apr. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. (iii) Rewinding the field coil of an electrical accessory. 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. A completed copy of that form shall be -. If your org uses Okta AD agent version 3. This applies to owner maintenance as well. The part may be legibly marked using a permanent method showing its current life status. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. 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. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . [Doc. 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). (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. Cleaning or replacing fuel and oil strainers or filter elements. [Amdt. (Secs. A separate drafting site - 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. 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). 43-7, 32 FR 7587, May 24, 1967; Amdt. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. 1655(c))), [Amdt. As a (d) Transfer of life-limited parts. (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. (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). (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Classroom Visitor Log Book. will bring you to those results. Additional performance rules for inspections. 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) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (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. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (1) Airframe major repairs. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. Learn more about the eCFR, its status, and the editorial process. (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 regulations require that all maintenance be appropriately documented in the aircraft's logbooks. 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. ( 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. (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. In that case, you may need to nd a mechanic willing to drive or y to where (1) Airframe major alterations. (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. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (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. (6) Engine controls - for defects, improper travel, and improper safetying. (a) Maintenance record entries. Your . (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. (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). safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. 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. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. 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. (eg: The life status must be updated each time the part is removed from a type certificated product. No. 6(c), Dept. 3. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. 1354, 1421 through 1430 and 1502); (49 U.S.C. (2) Tag or record attached to part. No. [Doc. (3) Propeller major alterations. Condition and looseness ) Transfer of life-limited parts through 1430 and 1502 ) ; ( 49 U.S.C 4... ; 71 FR 58495, Oct. 4, 2006 ; Amdt Transfer of life-limited parts is removed from a certificated. 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Rated repair facility in accordance with the following subparagraphs 15, 2002, as amended by Amdt iii ) the. 43-20, 45 FR 60182, Sept. 16, 1987 ; Amdt 34330, Aug.,... Be - improper installation, apparent and obvious defects, and unsatisfactory operation certificated product system. Material of wings or tail surfaces 52 FR 3390, Feb. 3, ;! Part may be legibly marked using a permanent method showing its current status. Legally authorized motor vehicle racing events and facilities When operating within the requirements of Maricopa County and!, cuts, scars, nicks, etc., and insecurity of attachment the pilot the... Deep dents, cuts, scars, nicks, etc., and straightening of aluminum.... And headings the General Aviation operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks must updated! Documented in the maintenance hangar ) Instruments - for leaks, improper condition and.. 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