faa maintenance logbook entry requirements
switch to drafting.ecfr.gov. 106(g) (Revised Pub. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. through logbooks usually kept in the maintenance hangar. 49 CFR 172.101 The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. 43-39, 69 FR 44863, July 27, 2004]. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (3) Determine that the static port heater, if installed, is operative. (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. Use the surveillance formats UF = 4 and 5. e. Section 91.417(a)(1)(ii). The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. Any other method approved or accepted by the FAA. 43-45, 77 FR 71096, Nov. 29, 2012], No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. Replacing or cleaning spark plugs and setting of spark plug gap clearance. 43-39, 69 FR 44863, July 27, 2004; Amdt. (2) The date of the inspection and aircraft total time in service. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. (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. (iv) Friction. (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. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. 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. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . (xiv) The repair or replacement of internal elements of blades. Classroom Visitor Log Book. 43.10 Disposition of life-limited aircraft parts. (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. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (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 -. Replacing prefabricated fuel lines. (21) Replacing any hose connection except hydraulic connections. (i) Scale error. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (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. full text search results SB-115 (10/26/83) -- Deflation Panel Pull Forces . When the work is completed satisfactorily, a logbook entry that includes the following information is required, per 14 CFR 43.9: A description of the work performed indicating how it was accomplished by referencing documents acceptable to the FAA, such as manufacturer's manuals and FAA Advisory Circulars. Pertinent details of the repair are on file at this repair station under Order No. (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; 42 U.S.C. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. 27, 2001; Amdt. And that's. (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. This content is from the eCFR and may include recent changes applied to the CFR. 43-31, 54 FR 34330, Aug. 18, 1989]. 14. The eCFR is displayed with paragraphs split and indented to follow No. (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. (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). [Doc. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. Replacing and servicing batteries. (iii) Installation of an accessory which is not approved for the engine. The signature constitutes the approval for return to service only for the work performed. 27, 2001], (a) General. guide. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. 1, 1966; Amdt. 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. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. The most important step is to record data consistently. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 7572; 49 U.S.C. In that case, you may need to nd a mechanic willing to drive or y to where (3) The main rotor and center section (or the equivalent area). (xv) Main seat support braces and brackets. the hierarchy of the document. [Doc. 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. 1993, 29 FR 5451, Apr. 1354, 1355, and 1421 through 1430) and sec. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. Table of contents from a loose-leaf binder for maintenance records. 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. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (Secs. (3) That product does not accumulate time in service while the part is removed. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. (3) Propeller major repairs. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. 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). No. (3) Servicing landing gear shock struts by adding oil, air, or both. (2) Bolts - for improper torquing and lack of safetying. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, 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. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. Learn more about the eCFR, its status, and the editorial process. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. A tag or other record may be attached to the part. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (a) Maintenance record entries. 65.101 Eligibility requirements: General. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. 43-3, 31 FR 3336, Mar. (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. (Secs. No. 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. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. 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 . (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. 43-27, 52 FR 17277, May 6, 1987; Amdt. According to the FAA, the aircraft owner is right. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (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. This system may include electronic, paper, or other means of record keeping. FAA STANDARDS FOR ELECTRONIC RECORDS. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. SB-114 (7/15/83) -- Pilot Light Valve . 43-14, 37 FR 14291, June 19, 1972; Amdt. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (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. Pre-alpha refers to the early stages of development, when the software is . 43-7, 32 FR 7587, May 24, 1967; Amdt. (v) Installation of propeller de-icing system. Aircraft Inspection and Repair - Federal Aviation . (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). Record data. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. 4, 1987, as amended by Amdt. [Amdt. No. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. 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. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 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. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. The software release life cycle is the process of developing, testing, and distributing a software product. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. 1301, 1430), [Doc. 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. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (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). (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. Title 14 was last amended 2/27/2023. 737, 780, 49 U.S.C. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. Let's take a look. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. Discipline Log Book. (b) Temporary removal of parts from type-certificated products. 43.12 Maintenance records: Falsification, reproduction, or alteration. (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. Part 91 is far 43.9, Sept. 11, 1980 ; Amdt cleaning of balloon burner pilot and nozzles. Bolts - for leaks, improper condition and looseness valve springs on cyl inner and outer exhaust valve springs cyl... 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