faa maintenance logbook entry requirements

(h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). You are using an unsupported browser. (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. Okta Mobile for end users. (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). (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (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. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. (xxiii) The repair of portions of skin sheets by making additional seams. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. 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. Things can get a bit more complicated (and costly) if you can't nd a local A&P willing to sign off the safe-to-ferry logbook entry. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. (2) Shock absorbing devices - for improper oleo fluid level. 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. No. (Secs. (8) Exhaust stacks - for cracks, defects, and improper attachment. 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 . FAA-2015-1621, Amdt. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. This content is from the eCFR and is authoritative but unofficial. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. 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. (a) Definitions. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. ( 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. [Doc. View the most recent official publication: These links go to the official, published CFR, which is updated annually. user convenience only and is not intended to alter agency intent (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. The method must deter the installation of the part after it has reached its life limit. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. However, this often becomes a "gotcha" moment for anyone auditing the logbook. (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). With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. Of the three maintenance records, the airframe (logbook) is the most permanent. (2) Powerplant major alterations. Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, Appendix E to Part 43 - Altimeter System Test and Inspection, Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. Use this checklist to: 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. (xiv) Members of the side truss, horizontal truss, or bulkheads. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. full text search results 43-40, 71 FR 40877, July 14, 2005]. 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. 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. Search & Navigation Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. As you know, 14 C.F.R. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). 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. 23, 1964, as amended by Amdt. 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). (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. switch to drafting.ecfr.gov. (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. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. Replacing and servicing batteries. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. (3) Determine that the static port heater, if installed, is operative. [Amdt. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 42 U.S.C. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. 1354, 1355, and 1421 through 1430) and sec. 43-43, 74 FR 53394, Oct. 16, 2009]. 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). 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (2) Seats and safety belts - for poor condition and apparent defects. 43-36, 61 FR 19501, May 1, 1996; Amdt. 101, 610, 72 Stat. 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). (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. ); (9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 43-7, 32 FR 7587, May 24, 1967; Amdt. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. 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. (xii) Overhaul of controllable pitch propellers. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. FAA-2018-0119, Amdt. Displaying title 14, up to date as of 2/27/2023. (4) Permanent marking. (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 -. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (3) The main rotor and center section (or the equivalent area). (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). 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. 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. 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 -. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. (v) Case leak. (b) Temporary removal of parts from type-certificated products. [Amdt. [Amdt. (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. 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. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. You didn't ask that though. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. will bring you directly to the content. (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. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. No. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). Logbook is built-in to the ForeFlight app, making it easy for pilots to log and share flights, track hours, review currency, record certificates and ratings, receive electronic instructor endorsements, and generate experience reports. (2) Bolts - for improper torquing and lack of safetying. With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. 23, 1964, as amended by Amdt.

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