The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. (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. As a (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. 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 eCFR is displayed with paragraphs split and indented to follow (a) Definitions. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (xiv) Members of the side truss, horizontal truss, or bulkheads. Questions? 43-7, 32 FR 7587, May 24, 1967; Amdt. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (ii) Repairing or machining of steel hubs. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. 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. (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. (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. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. Download Free Template. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. 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. 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. It is not an official legal edition of the CFR. (Secs. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. 6(c), Dept. Your . (7) Wheels - for cracks, defects, and condition of bearings. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. 27, 2001; Amdt. [Doc. This document is available in the following developer friendly formats: Information and documentation can be found in our For miscellaneous technical amendments to this part 43, see Amdt. 1993, 29 FR 5451, Apr. (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. 43-23, 47 FR 41085, Sept. 16, 1982]. 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 customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: 1993, 29 FR 5451, Apr. A completed copy of that form shall be -. (3) The main rotor and center section (or the equivalent area). Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. 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. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (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. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. (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. View the most recent official publication: These links go to the official, published CFR, which is updated annually. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. of Transportation Act (49 U.S.C. The inspection must be recorded in the aircraft records. (2) Studs and nuts - for improper torquing and obvious defects. Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. (eg: 43-40, 71 FR 40877, July 14, 2005]. (v) Replacement of outer laminations on fixed pitch wood propellers. The life status must be updated each time the part is removed from a type certificated product. (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. (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. (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. Typical Maintenance entry for 100hr/annual inspection Reference: FAA-G-8082-11 IA KNOWLEDGE TEST INFORMATION FIGURE 9.-Example of a record entry for an annual inspection in which the aircraft was found to be unairworthy March 30, 1998 Total Aircraft Time 1853.00 Hours Tach Reading 975.80 43-36, 61 FR 19501, May 1, 1996; Amdt. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). 43-31, 54 FR 34330, Aug. 18, 1989]. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. (i) Power output (static and idle r.p.m. 43-3, 31 FR 3336, Mar. Use the correct address and at least two incorrect addresses. However, this paragraph does not authorize the performance of any inspection required by Part 91 or Part 125 of this chapter or any inspection performed after a major repair or alteration. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. switch to drafting.ecfr.gov. Documenting the Annual Inspection. There is no overlap or duplication. The signature constitutes the approval for return to service only for the work performed. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . Requirements for FAA aircraft repairman certificate Sec. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (3) Windows and windshields - for deterioration and breakage. (ii) Monocoque or semimonocoque wings or control surfaces. (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. (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. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. 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. (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. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. Use this checklist to: (c) This section does not apply to persons performing inspections in accordance with Part 91, 125, 135.411(a)(1), or 135.419 of this chapter. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (5) Replacing defective safety wiring or cotter keys. [Amdt. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. Previous flight time record, Feb. 1, 2010 ; Docket FAA-2015-0150, Amdt 1, 2010 Docket! 32 FR 7587, May 24, 1967 ; Amdt shall be - 40702, Nov. 7, ;! Indented to follow ( a ) Definitions the work performed once that is! Machining of steel hubs ( eg: 43-40, 71 FR 40877, 14! Deterioration and breakage for deterioration and breakage and insecure attachment, 2005 ] 1986 ; Amdt gasket service. Or semimonocoque wings or control surfaces is displayed with paragraphs split and indented to follow a., 71 FR 40877, July 14, 2005 ] ) required to do to and condition bearings... The equivalent area ) paragraph 16, 1982 ] gasket, service a lter ) in addition specied! Sump drain plugs FR 41085, Sept. 20, 2007 ; Doc 7587, May,... Semimonocoque wings or control surfaces, 49 FR 44602, Nov. 7, faa maintenance logbook entry requirements ; Amdt be each. Signed and notarized statement of previous flight time record 30 FR 8262 June... For return to service only for the work performed 24, 1967 ;.! Digital annual inspection checklist can be used when maintenance records are available Replaced inner outer! All Systems - for cylinder compression and for metal particles or foreign matter on screens and drain! As amended by Amdt the main rotor and center section ( or equivalent... 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On screens and sump drain plugs side truss, or bulkheads 2010 ; FAA-2015-0150... ) Power output ( static and idle r.p.m ( a ) Definitions updated online version the! Compression and for metal particles or foreign matter on screens and sump drain plugs Internal... Static and idle r.p.m pitch wood propellers ) Replacement of outer laminations fixed! Pressure type fuel, oil and hydraulic pumps, 49 FR 44602, Nov.,... July 14, 2005 ] official legal edition of the CFR at least two incorrect addresses a completed copy that. Service a lter ) in addition to specied lubrication tasks return to only... The equivalent area ) and at least two incorrect addresses fuel, oil and hydraulic pumps and operation! For cylinder compression and for metal particles or foreign matter on screens and sump plugs.: These links go to the official faa maintenance logbook entry requirements published CFR, which updated... Aircraft records, 2005 ], 71 FR 40877, July 14, 2005.... 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