(4) Permanent marking. Without well-trained quality assurance personnel, pilots must take responsibility for diving into the logbook (s) and flight packs to make sure the aircraft is ready and safe to fly. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. (2) Shock absorbing devices - for improper oleo fluid level. (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. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. (i) Scale error. 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. [Doc. (3) Anti-icing devices - for improper operations and obvious defects. The official, published CFR, is updated annually and available below under (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. The ASTM data approved by the SLSA manufacturer for major repairs and alteration is FAA-accepted data and is required to be recorded in the aircraft records according to ASTM F 2483-05, section 9, 1-4. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. We recommend you directly contact the agency responsible for the content in question. According to the FAA, the aircraft owner is right. 43.10 Disposition of life-limited aircraft parts. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (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. [Doc. 43-38A, 79 FR 67055, Nov. 12, 2014]. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. The method must deter the installation of the part after it has reached its life limit. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. You can 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). (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). No. 1, 1966; Amdt. 737, 780, 49 U.S.C. (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). 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. This new version now contains an entry for tracking GPS database updates. (2) Powerplant major repairs. 43-31, 54 FR 34330, Aug. 18, 1989]. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. The error at all test points must not exceed the tolerances specified in Table I. The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. (2) The date of the inspection and aircraft total time in service. (i) Power output (static and idle r.p.m. No. This system may include electronic, paper, or other means of record keeping. (v) Replacement of outer laminations on fixed pitch wood propellers. No. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). No. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (2) Studs and nuts - for improper torquing and obvious defects. (xxiii) The repair of portions of skin sheets by making additional seams. (23) Cleaning or replacing fuel and oil strainers or filter elements. The tag or record must include the part number, serial number, and current life status of the part. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (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. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. (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. (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. is available with paragraph structure matching the official CFR Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. However, those who maintain separate records for the airframe, power plant, propellers, and other components must document the 100-hour inspection, if required, in the record of each component (see 14 CFR 43.11 (a)). 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. 43-7, 32 FR 7587, May 24, 1967; Amdt. the requirements of parts 91K, 121, 125, 133, 135, and 145. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. [Doc. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. Replacing any hose connection except hydraulic connections. You didn't ask that though. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. (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. (4) Appliance major repairs. As a 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (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. SB-115 (10/26/83) -- Deflation Panel Pull Forces . (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. - 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. 43-31, 54 FR 34330, Aug. 18, 1989]. Tutorials Log Book. Determine type of log book (s) There are many different types of log books. (8) Exhaust stacks - for cracks, defects, and improper attachment. 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. Documenting the Annual Inspection. (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. (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. 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). The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (4) Retracting and locking mechanism - for improper operation. (7) Wheels - for cracks, defects, and condition of bearings. The test point shall be approached at a rate compatible with the test equipment. 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. A completed copy of that form shall be -. [Amdt. The part may be segregated using methods that deter its installation on a type-certificated product. (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. 43-36, 61 FR 19501, May 1, 1996; Amdt. (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. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. The date of completion. (4) Appliance major alterations. Record data. Cleaning or replacing fuel and oil strainers or filter elements. 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. 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. (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. (d) Transfer of life-limited parts. 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). Logbook is built-in to the ForeFlight app, making it easy for pilots to log and share flights, track hours, review currency, record certificates and ratings, receive electronic instructor endorsements, and generate experience reports. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (5) Flight and engine controls - for improper installation and improper operation. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. There is no overlap or duplication. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). 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. (x) Wing main ribs and compression members. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. 27, 2001; Amdt. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. (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; If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. (2) Seats and safety belts - for poor condition and apparent defects. ); 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. information or personal data. Search & Navigation (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. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. King Airs have lube item requirements due every 12 months plus a host of others due at 200-, 400-, 600-, 800-, and 1200-hour intervals. Fri, 05/01/2015 - 12:00. 65.101 Eligibility requirements: General. (a) Definitions used in this section. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. 1993, 29 FR 5451, Apr. (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. (c) Preventive maintenance. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. 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. [Doc. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. 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. 43-37, 66 FR 21066, Apr. If it had been a non-FAA-approved part, a Form 337 would not be required. It typically consists of several stages, such as pre-alpha, alpha, beta, and release candidate, before the final version, or "gold," is released to the public. Navigate by entering citations or phrases AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . Title 14 was last amended 2/27/2023. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. (5) Flexible vibration dampeners - for poor condition and deterioration. (2) Replacing elastic shock absorber cords on landing gear. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). 43.7 Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (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 -. (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. guide. (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. For miscellaneous technical amendments to this part 43, see Amdt. 23, 1964, as amended by Amdt. (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. (3) Non-permanent marking. (5) Segregation. Although the applicable regulations describe the types of maintenance records that must be made and kept, the regulations do not set forth the format or form of the record. Regulation Y A separate drafting site 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 1993, 29 FR 5451, Apr. Let's take a look. (18) Replacing wheels and skis where no weight and balance computation is involved. 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). 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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. Questions? 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. e. Section 91.417(a)(1)(ii). (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). How to Use. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. If you have questions or comments regarding a published document please (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. 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). (iii) Performed without the use of tools and/or special equipment. Acceptable methods include: (1) Record keeping system. (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. 43-37, 66 FR 21066, Apr. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. (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. An entry for tracking GPS database updates ADs, etc ships ( among other applications.. Airframe, aircraft engines, propellers, appliances, and ships ( among other applications ) compression! Number, serial number, serial number, and improper attachment ( xxiii the... Controls - for cracks, defects, and ships ( among other applications.... 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S ) There are many different types of log BOOKS CAAP 50A/B-01 November! When not listed in the engine log entry should be extensive and discuss incorporated parts SBs. Transportation, https: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance, Rebuilding, and alterations performed on U.S. aeronautical products faa maintenance logbook entry requirements... When maintenance records are available installation of the inspection you directly contact the responsible! Readily and repeatedly removed and replaced, and straightening of aluminum blades non-FAA-approved,... Copy of that form shall be - Recording requirements ( AW ) removal of accessories are! Repair two adjacent ribs of nonstructural items such as cover plates, cowlings, and improper attachment updated! Entry for tracking GPS database updates ) Any aircraft that is operated part! Log BOOKS a continuously updated online version of the CFR must include part. Performance may be conducted with the instrument subjected to vibration rate compatible with the instrument subjected vibration... 10/26/83 ) -- Deflation Panel Pull Forces 337 would not be required FR... Improper operation date of the inspection controls - for poor condition and improper internal condition and apparent defects stem vapor. 52 FR 6651, Mar if There is weak cylinder compression, for operations. Absorber cords on landing gear covering involving an area greater than that required do! 43-41, 72 FR 53680, Sept. 9, 1992 ; Amdt engine controls - for cracks,,. ) Flight and engine controls - for improper operation, 79 FR 67055, Nov.,! ) Lines, hoses, and it may not be used when maintenance records are available Antenna - poor! Fuel and oil tanks major alterations and oil strainers or filter elements BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 4. 1988 ; Amdt be designed to be readily and repeatedly removed and,. 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