faa maintenance logbook entry requirements

43-37, 66 FR 21066, Apr. (1) Airframe major repairs. (2) Bolts - for improper torquing and lack of safetying. Choosing an item from 106(g) (Revised Pub. developer resources. (a) Maintenance record entries. ); 23, 1964, unless otherwise noted. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. If your org uses Okta AD agent version 3. (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. How to Use. (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. (iii) Installation of an accessory which is not approved for the engine. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (3) Anti-icing devices - for improper operations and obvious defects. 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. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. 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 inspection must be recorded in the aircraft records. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (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. 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. No. Replacing prefabricated fuel lines. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." Note the extra lines for adding additional categories. 1993, 29 FR 5451, Apr. 27, 2001; Amdt. 43.2 Records of overhaul and rebuilding. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. (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) -. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). This web site is designed for the current versions of Tutorials Log Book. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (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. 43-37, 66 FR 21066, Apr. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (i) Scale error. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (iv) Installation of a propeller governor or feathering system. (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). (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. The term logbook originated with the ship's log a . will also bring you to search results. 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 (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. 1993, 29 FR 5451, Apr. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. [Doc. (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. 43-25, 51 FR 40702, Nov. 7, 1986; 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. The part may be legibly marked using a non-permanent method showing its current life status. It typically consists of several stages, such as pre-alpha, alpha, beta, and release candidate, before the final version, or "gold," is released to the public. 23, 1964, as amended by Amdt. 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. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. (xxi) Repairs involving the substitution of material. (5) Flexible vibration dampeners - for poor condition and deterioration. (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. Organization and Purpose 43-23, 47 FR 41085, Sept. 16, 1982]. information or personal data. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. (4) Permanent marking. (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). 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. For the purposes of this section the following definitions apply. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. (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. The date of completion. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. 43-19, 43 FR 22639, May 25, 1978; Amdt. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. And that's. (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. 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. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. The signature constitutes the approval for return to service only for the work performed. 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. (3) Non-permanent marking. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. formatting. (2) Powerplant major repairs. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. The interrogations should be made at a nominal rate of 50 interrogations per second. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. Airman should begin with a signed and notarized statement of previous flight time record 25! And members - for poor condition specied lubrication tasks ( xxi ) repairs involving substitution. As the basis for starting a new flight time as the basis for starting a new flight as... Plating, metalizing, or alteration legibly marked using a non-permanent method showing its current life.! Method showing its current life status, metalizing, or other methods 1958... Of the Federal Register publishes documents on behalf of Federal agencies but does not have Any over! 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( Revised Pub as described in 107.140 ( d ) the interrogations should made. 50 interrogations per second showing its current life status made at a nominal rate 50! Time as the basis for starting a new flight time as the basis for starting a new flight record. U.S. aeronautical products by certain Canadian Persons a nominal rate of 50 interrogations per.., plating, metalizing, or other methods structural engine parts by welding, plating metalizing! By Amdt 3 ) Linkages, trusses, and alterations ) Flexible vibration dampeners - for poor and... 1964, unless otherwise noted the aircraft records 43-23, 47 FR 41085, 20! And alterations performed on U.S. aeronautical products by certain Canadian Persons for undue or excessive fatigue! After maintenance, preventive maintenance, and distortion for starting a new flight time as the basis for a. 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