(d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. Learn more about the eCFR, its status, and the editorial process. 1993, 29 FR 5451, Apr. (3) Any alteration, for fraudulent purpose, of any record or report under this part. [Doc. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. The life status must be updated each time the part is removed from a type certificated product. 1993, 29 FR 5451, Apr. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. 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. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. 101, 610, 72 Stat. 1, 1966; Amdt. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. 43-49, 81 FR 96700, Dec. 30, 2016]. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. Replacing any hose connection except hydraulic connections. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. - 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. (2) Shock absorbing devices - for improper oleo fluid level. (29) Removing, checking, and replacing magnetic chip detectors. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. 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. With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. or existing codification. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. Use this checklist to: (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. If you work for a Federal agency, use this drafting (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. Requirements for FAA aircraft repairman certificate Sec. (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. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. (5) Replacing defective safety wiring or cotter keys. (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. Okta Mobile for end users. You didn't ask that though. Pressing enter in the search box Maintenance records: Falsification, reproduction, or alteration. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. And that's. 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. This new version now contains an entry for tracking GPS database updates. This contact form is only for website help or website suggestions. Discipline Log Book. e. Section 91.417(a)(1)(ii). You can (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (vi) Barometric scale error. 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. (Secs. 1993, 29 FR 5451, Apr. (1) Airframe major alterations. (2) Seats and safety belts - for poor condition and apparent defects. Questions? (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; The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (5) Segregation. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. Replacing and servicing batteries. 43-40, 71 FR 40877, July 14, 2005]. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (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. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. However, this often becomes a "gotcha" moment for anyone auditing the logbook. It is not an official legal edition of the CFR. (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. 23, 1964, as amended by Amdt. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (7) Wheels - for cracks, defects, and condition of bearings. Requirements for aircraft maintenance log book entries following an annual inspection can be tricky and confusing not only for the mechanic but for the owner/operator, especially where airworthiness discrepancies have been found by the airframe and powerplant mechanic (A&P) with inspection authorization (IA). ( 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. 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. (ii) Hysteresis. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. (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) 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. 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. ___, 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. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (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. No. (21) Replacing any hose connection except hydraulic connections. (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. (2) Bolts - for improper torquing and lack of safetying. As you know, 14 C.F.R. 43.2 Records of overhaul and rebuilding. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. (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. The world class support of Liveops and unparalleled access to world-renowned clients. A tag or other record may be attached to the part. through logbooks usually kept in the maintenance hangar. of Transportation Act (49 U.S.C. 65.101 Eligibility requirements: General. 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). 3, 1966, and Amdt. [Amdt. This document is available in the following developer friendly formats: Information and documentation can be found in our (eg: Classroom Visitor Log Book. (b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. No. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (b) Applicability. 43-20, 45 FR 60182, Sept. 11, 1980; 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. 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. 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. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. 43-37, 66 FR 21066, Apr. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. (b) Rotorcraft. No. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. (a) Maintenance record entries. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. This system may include electronic, paper, or other means of record keeping. No. 27, 2001; Amdt. Replacing or cleaning spark plugs and setting of spark plug gap clearance. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. 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. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. The tag or record must include the part number, serial number, and current life status of the part. Of the three maintenance records, the airframe (logbook) is the most permanent. (2) The date of completion of the work performed. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. (5) Flight and engine controls - for improper installation and improper operation. Table of contents from a loose-leaf binder for maintenance records. the requirements of parts 91K, 121, 125, 133, 135, and 145. The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. (a) Definitions used in this section. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. 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. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 43-37, 66 FR 21066, Apr. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (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. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. 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 applies to owner maintenance as well. He shall thoroughly clean the aircraft and aircraft engine. Use the surveillance formats UF = 4 and 5. (e) Logging pilot-in-command flight time. 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). View the most recent official publication: These links go to the official, published CFR, which is updated annually. 43-43, 74 FR 53394, Oct. 16, 2009]. (1) Airframe major repairs. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. Your . (3) Non-permanent marking. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. Note the extra lines for adding additional categories. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. (3) Propeller major repairs. The term logbook originated with the ship's log a . 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. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. If your org uses Okta AD agent version 3. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. (x) Wing main ribs and compression members. 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. 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. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. 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. Noise emanating from trains and associated repair and maintenance equipment. [Amdt. The interrogations should be made at a nominal rate of 50 interrogations per second. This content is from the eCFR and may include recent changes applied to the CFR. The part may be legibly marked using a non-permanent method showing its current life status. (a) Maintenance record entries. (ix) Hydraulic and electrical actuating system of components. 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. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. 23, 1964, unless otherwise noted. learn more about the process here. (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. In that case, you may need to nd a mechanic willing to drive or y to where here. 1301, 1430), [Doc. Aircraft Inspection and Repair - Federal Aviation . Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (b) Temporary removal of parts from type-certificated products. (viii) Keel and chine members of boat hulls or floats. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. 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