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). (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. 27, 2001; Amdt. For the purposes of this section the following definitions apply. 1 CFR 1.1 49 CFR 172.101 (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). The tag or record must include the part number, serial number, and current life status of the part. (2) Powerplant major alterations. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (xiv) Members of the side truss, horizontal truss, or bulkheads. Where To Go For Honda Maintenance Although . The part may be segregated using methods that deter its installation on a type-certificated product. 21. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. (iv) Complete disassembly of complex hydraulic power valves. (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. Replacing or cleaning spark plugs and setting of spark plug gap clearance. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. Determine type of log book (s) There are many different types of log books. (a) Definitions used in this section. No. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (xv) Main seat support braces and brackets. (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). 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. 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. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 1-866-TELL-FAA (1-866-835-5322) Readers & Viewers PDF Powerpoint Zip Word Excel (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. (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. 1993, 29 FR 5451, Apr. 42 U.S.C. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. The date of completion. Record data. through logbooks usually kept in the maintenance hangar. (3) Non-permanent marking. A tag or other record may be attached to the part. here. 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: (1) A description (or reference to data acceptable to the Administrator) of work performed. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (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). (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. (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). 24. (2) The date of the inspection and aircraft total time in service. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. 43-28, 52 FR 20028, June 16, 1987; Amdt. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. Cleaning or replacing fuel and oil strainers or filter elements. (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. 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. (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. 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). 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (3) Bonding and shielding - for improper installation and poor condition. (c) Disposition of parts removed from type-certificated products. (c) Preventive maintenance. (a) Except for work performed in accordance with 91.411 and 91.413, each registered owner or operator shall keep the following records for the periods specified in paragraph (b) of this section . (iii) Performed without the use of tools and/or special equipment. SB-115 (10/26/83) -- Deflation Panel Pull Forces . Pre-alpha refers to the early stages of development, when the software is . 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 43-23, 47 FR 41085, Sept. 16, 1982]. This content is from the eCFR and may include recent changes applied to the CFR. 1/1.1 (3) The main rotor and center section (or the equivalent area). (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. 43-50, 83 FR 9170, Mar. will bring you to those results. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. This web site is designed for the current versions of The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). 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. Any other method approved or accepted by the FAA. [Amdt. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. 43-39, 69 FR 44863, July 27, 2004; Amdt. 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. (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. The tests in (e) through (j) apply only to Mode S transponders. Examples of Log Entries . 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. If it had been a non-FAA-approved part, a Form 337 would not be required. (viii) Keel and chine members of boat hulls or floats. 23, 1964, as amended by Amdt. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. 1993, 29 FR 5451, Apr. (b) Listing of discrepancies and placards. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. 43-6, 31 FR 9211, July 6, 1966. (4) Appliance major alterations. ); (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. (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. (3) Anti-icing devices - for improper operations and obvious defects. Use this checklist to: (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. Fr 44863, July 6, 1966, nicks, etc., and life. There are many different types of log book ( s ) There are many different of. 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Faa.Gov Home ATTENTION: the Flight Standards Information Management System ( FSIMS ) is decommissioned Please https!