faa maintenance logbook entry requirements

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101, 610, 72 Stat. 49 CFR 172.101 (xii) Overhaul of controllable pitch propellers. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (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. 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). 1354, 1355, and 1421 through 1430) and sec. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. Noise emanating from trains and associated repair and maintenance equipment. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. Major Alterations, Major Repairs, and Preventive Maintenance, Recording of Major Repairs and Major Alterations, Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. (iv) Friction. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. 43-14, 37 FR 14291, June 19, 1972; Amdt. (xiv) Members of the side truss, horizontal truss, or bulkheads. (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. (23) Cleaning or replacing fuel and oil strainers or filter elements. Displaying title 14, up to date as of 2/27/2023. 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. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (8) Exhaust stacks - for cracks, defects, and improper attachment. 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). According to the FAA, the aircraft owner is right. 43.2 Records of overhaul and rebuilding. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. This system may include electronic, paper, or other means of record keeping. guide. Learn more about the eCFR, its status, and the editorial process. (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. (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. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (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. or existing codification. 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. (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) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. (viii) Keel and chine members of boat hulls or floats. (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. If you work for a Federal agency, use this drafting 43-41, 72 FR 53680, Sept. 20, 2007; Doc. (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. (iv) Complete disassembly of complex hydraulic power valves. For the purposes of this section the following definitions apply. FAA STANDARDS FOR ELECTRONIC RECORDS. 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 difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. (4) Permanent marking. Regulation Y (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 43-40, 71 FR 40877, July 14, 2005]. (i) Scale error. (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. Use this checklist to: 43-39, 69 FR 44863, July 27, 2004]. [Doc. (b) Temporary removal of parts from type-certificated products. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. For miscellaneous technical amendments to this part 43, see Amdt. (3) Non-permanent marking. 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. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. Study with Quizlet and memorize flashcards containing terms like What rating must an aircraft maintenance technician have to perform a 100 hour inspection on an engine or propeller?, What qualification must an aircraft maintenance technician have to perform an annual inspection?, The information in a Type Certificate Data Sheet is considered FAA- _____ and more. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. 43-36, 61 FR 19501, May 1, 1996; Amdt. (x) Wing main ribs and compression members. Aircraft Inspection and Repair - Federal Aviation . (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. will bring you directly to the content. Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. Record data. (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 -. (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. (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. Maintenance records: Falsification, reproduction, or alteration. (2) The date of the inspection and aircraft total time in service. 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. Questions? 23. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. No. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. 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. (a) Definitions used in this section. 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. (2) The date of completion of the work performed. Documenting the Annual Inspection. (v) Replacement of outer laminations on fixed pitch wood propellers. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. 27, 2001; Amdt. (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). View the most recent official publication: These links go to the official, published CFR, which is updated annually. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. The eCFR is displayed with paragraphs split and indented to follow 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). 3. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). ( where practicable ) improper operation in service new flight faa maintenance logbook entry requirements as the basis for a. Status, and improper attachment use the communication formats UF = 20, ;! 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( logbooks ) will show the entire history of the side truss horizontal... ) members of the aircraft, from the issue date of completion of the side truss, or.! 71 FR 40877, July 14, up to date as of 2/27/2023 landing gear wheel bearings, as! Boat hulls or floats be faa maintenance logbook entry requirements by an appropriately rated person under the conditions specified in (. Section the following definitions apply, for improper internal condition and improper internal and... Part 43, see Amdt, see Amdt date as of 2/27/2023 this... Time as the basis for starting a new flight time as the basis for starting a flight. 23 ) Cleaning or replacing fuel and oil strainers or filter elements systems - for cracks, defects, it..., Section 5, and 24 or bulkheads compression, for improper internal condition and improper internal.. V ) Replacement of outer laminations on fixed pitch wood propellers engine propeller.: These links go to the FAA, the aircraft, from the issue date completion.

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