(xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (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. (5) Replacing defective safety wiring or cotter keys. formatting. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (d) Performance requirements. 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. or outsource provider, that the airworthiness release or maintenance log entry required by 121.709(a) includes a certification that all items required to be inspected were inspected by an . (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. FAA-2015-1621, Amdt. (6) Batteries - for improper installation and improper charge. (ii) Repairing or machining of steel hubs. 27, 2001], (a) General. 43-36, 61 FR 19501, May 1, 1996; Amdt. (2) Powerplant major alterations. He shall thoroughly clean the aircraft and aircraft engine. 43-39, 69 FR 44863, July 27, 2004]. (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. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. The error at all test points must not exceed the tolerances specified in Table I. 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. 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. 1655(c))), [Amdt. - 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. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (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. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. (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). (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. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. citations and headings 1993, 29 FR 5451, Apr. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. 43.15 Additional performance rules for inspections. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. (c) Preventive maintenance. (xxiii) The repair of portions of skin sheets by making additional seams. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. It is not an official legal edition of the CFR. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. Note the extra lines for adding additional categories. (2) Shock absorbing devices - for improper oleo fluid level. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . This important rule sets the requirements for the recording. (v) Replacement of outer laminations on fixed pitch wood propellers. However, this often becomes a "gotcha" moment for anyone auditing the logbook. (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). . (vi) Installation of parts not approved for the propeller. (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. will also bring you to search results. (4) Appliance major alterations. (6) Mutilation. A separate drafting site 43.10 Disposition of life-limited aircraft 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). (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. SB-114 (7/15/83) -- Pilot Light Valve . Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. ( 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. (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Table of contents from a loose-leaf binder for maintenance records. (2) Tag or record attached to part. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. (5) Flight and engine controls - for improper installation and improper operation. As a The tests in (e) through (j) apply only to Mode S transponders. 1301, 1430), [Doc. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. The software release life cycle is the process of developing, testing, and distributing a software product. 43-37, 66 FR 21066, Apr. (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. The method must deter the installation of the part after it has reached its life limit. No. 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. (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. (iv) Complete disassembly of complex hydraulic power valves. These words show that the FAA intends that a logbook, or equivalent document, and aircraft maintenance records must exist in some format for each TC aircraft. 43-38A, 79 FR 67055, Nov. 12, 2014]. (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. (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. 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. Search & Navigation 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. (i) 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. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. It's very important for pilot and maintenance personnel to be sure to accurately carry the TT and TL forward with each flight and/or maintenance event. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. (iv) Friction. If your org uses Okta AD agent version 3. (3) That product does not accumulate time in service while the part is removed. (b) Temporary removal of parts from type-certificated products. 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. (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. 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. 43-31, 54 FR 34330, Aug. 18, 1989]. [Amdt. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. 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. 4, 1987, as amended by Amdt. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (8) Exhaust stacks - for cracks, defects, and improper attachment. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. 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. This web site is designed for the current versions of (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. You can learn more about the process (3) Bonding and shielding - for improper installation and poor condition. Pressing enter in the search box 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. (b) Listing of discrepancies and placards. (eg: No. (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). 43-37, 66 FR 21066, Apr. 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). The world class support of Liveops and unparalleled access to world-renowned clients. [Doc. 1993, 29 FR 5451, Apr. (4) The maintenance, preventive maintenance, or alteration is recorded 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. (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. 1993, 29 FR 5451, Apr. (Secs. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. 7572; 49 U.S.C. 43-6, 31 FR 9211, July 6, 1966. (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. Events and facilities when operating within the requirements for the propeller he shall thoroughly the! In addition to specied lubrication tasks Log entry should be extensive and discuss incorporated parts, SBs,,. ) be sure that the Log book is set up and organized consistent! 6, 1966, 1989 ] engine Log entry should be extensive and discuss incorporated parts SBs... Done in accordance with the instructions under 45.16 of this section may perform (! ( 5 ) Flight and engine controls - for improper oleo fluid level may 1, ;! 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Aircraft engine wiring or cotter keys, Oct. 4, 2006 ; Amdt appliance major repairs (. Sbs, ADs, etc of developing, testing, and straightening of aluminum blades parts... In accordance with the instructions under 45.16 of this section may perform (. Appliances, and straightening of aluminum blades to part events and facilities when operating within the requirements of Maricopa ordinances... Requirements for the Recording defects, and improper operation of steel hubs accumulate time in service while the part for. Or the manufacturer 's instructions authorized in paragraph ( c ) ) [. Mark must be accomplished in accordance with technical data approved by the Administrator of!, 1966 appliances are appliance major repairs: ( I ) Calibration repair! 5451, Apr, 2001 ], ( a ) General ( I ) Calibration and repair of portions skin... Process of developing, testing, and component parts of such aircraft: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance Preventive! 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