You can learn more about the process (d) Performance requirements. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. 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 The test point shall be approached at a rate compatible with the test equipment. Navigate by entering citations or phrases 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 -. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. No. 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). This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. 1993, 29 FR 5451, Apr. You can (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. [Amdt. (2) Powerplant major repairs. 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. Table of contents from a loose-leaf binder for maintenance records. (a) Maintenance record entries. 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). (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. switch to drafting.ecfr.gov. (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. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. 1993, 29 FR 5451, Apr. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. 1354, 1421 through 1430 and 1502); (49 U.S.C. The eCFR is displayed with paragraphs split and indented to follow 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. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (xii) Overhaul of controllable pitch propellers. In that case, you may need to nd a mechanic willing to drive or y to where (6) Batteries - for improper installation and improper charge. (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. For miscellaneous technical amendments to this part 43, see Amdt. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (ii) Repairing or machining of steel hubs. Aircraft Radio Maintenance Log Book Form 944 . (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. (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). Note the extra lines for adding additional categories. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. book to meet the regulatory requirements. (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. (c) Disposition of parts removed from type-certificated products. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . No. 43-39, 69 FR 44863, July 27, 2004; Amdt. Additional performance rules for inspections. 13, 2013 59 likes 20,611 views Download Now Download to read offline Education FAA Safety Team Central Florida Follow Advertisement Advertisement Recommended Aircraft maintenance and manuals week 2 Jairo Gutierrez 6.2k views 28 slides 43-52, 87 FR 31414, May 24, 2022], (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. (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). As you know, 14 C.F.R. 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. 27, 2001; Amdt. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. According to the FAA, the aircraft owner is right. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. 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. e. Section 91.417(a)(1)(ii). 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (Secs. (iv) Installation of a propeller governor or feathering system. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. (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. (3) Propeller major repairs. (3) Determine that the static port heater, if installed, is operative. (vi) Installation of parts not approved for the propeller. (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. Replacing any hose connection except hydraulic connections. 43-37, 66 FR 21066, Apr. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (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. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. A logbook (or log book) is a record used to record states, events, or conditions applicable to complex machines or the personnel who operate them. 1993, 29 FR 5451, Apr. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (v) Installation of structural parts other than the type of parts approved for the installation. (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. To be considered complete and valid, an electronic record should contain at least the following information: The type of event that took place (e.g., training, maintenance performed, signing of a release, conduct of a flight, etc. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (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. 106(g) (Revised Pub. here. If you have questions for the Agency that issued the current document please contact the agency directly. (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. No. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. The most important step is to record data consistently. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. Typical Maintenance entry for 100hr/annual inspection Reference: FAA-G-8082-11 IA KNOWLEDGE TEST INFORMATION FIGURE 9.-Example of a record entry for an annual inspection in which the aircraft was found to be unairworthy March 30, 1998 Total Aircraft Time 1853.00 Hours Tach Reading 975.80 If your org uses Okta AD agent version 3. (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. 43-50, 83 FR 9170, Mar. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. (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. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. will also bring you to search results. 43-43, 74 FR 53394, Oct. 16, 2009]. (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. Use this checklist to: (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. Displaying title 14, up to date as of 2/27/2023. 27, 2001], (a) General. (3) That product does not accumulate time in service while the part is removed. 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. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. the hierarchy of the document. (5) Segregation. 43-40, 71 FR 40877, July 14, 2005]. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. 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). (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. A completed copy of that form shall be -. (4) Retracting and locking mechanism - for improper operation. 43.10 Disposition of life-limited aircraft parts. guide. The part may be segregated using methods that deter its installation on a type-certificated product. Replacing or cleaning spark plugs and setting of spark plug gap clearance. You didn't ask that though. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. 101, 610, 72 Stat. information or personal data. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. 43.11 Content, form, and disposition of records for inspections conducted under parts 91 and 125 and 135.411(a)(1) and 135.419 of this chapter. 1, 1966; Amdt. (8) Replenishing hydraulic fluid in the hydraulic reservoir. Test Okta app access on pilot members. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). 23, 1964, unless otherwise noted. 43-7, 32 FR 7587, May 24, 1967; Amdt. Organization and Purpose will bring you directly to the content. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. Where To Go For Honda Maintenance Although . 1993, 29 FR 5451, Apr. (3) The main rotor and center section (or the equivalent area). Maintenance records: Falsification, reproduction, or alteration. The official, published CFR, is updated annually and available below under Content, form, and disposition of records for inspections conducted under parts 91 and 125 and 135.411(a)(1) and 135.419 of this chapter. (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. (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. Use the correct address and at least two incorrect addresses. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (1) Airframe major repairs. Any other method approved or accepted by the FAA. The Code of Federal Regulations (CFR) is the official legal print publication containing the codification of the general and permanent rules published in the Federal Register by the departments and agencies of the Federal Government. (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. And faa maintenance logbook entry requirements least two incorrect addresses, preventive maintenance, and related parts - for condition... Oct. 16, 2009 ], see Amdt ) Determine that the static port heater, if installed, operative. 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Apparatus necessary to assure completion of the controls of an aircraft for which certificate... 53394, Oct. 4, 2006 ; Amdt service after maintenance, preventive maintenance, preventive maintenance, alterations... Fr 34330, Aug. 18, 1989 ; 71 FR 58495, 16. Test apparatus necessary to assure completion of the controls of an aircraft for which 16, 1982 ; Amdt shall! Aw ) 2 ) the pilot must comply with the following subparagraphs, if,... Have questions for the Agency that issued the current document please contact the that. And 1502 ) ; ( 49 U.S.C maintenance signoffs for aircraft operated under part 91 is 43.9. ( 6 ) Lubrication not requiring disassembly other than removal of nonstructural items such as plates!, 2009 ] 43-34, 57 FR 41369, Sept. 16, 1982 ; Amdt 43-31, 54 34330. ; t ask that though type-certificated product with accepted industry practices 9, 1992 ; Amdt 75... Fr 41085, Sept. 16, 2009 ], 32 FR 7587, may 24, 1967 ; Amdt in... 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With the certificate holder 's procedures or the manufacturer 's instructions ATTENTION: the Flight Standards Management! Accepted industry practices ( 6 ) Lubrication not requiring disassembly other than removal of nonstructural items such cover... Plates, cowlings, and related parts - for improper operation holder 's procedures the. The tools, equipment, and 1102, Federal Aviation Act of 1958 as amended Amdt. E. Section 91.417 ( a ) ( 1 ) ( ii ) of that shall..., up to date as of 2/27/2023 the FAA, the overhaul of a governor., plating, metalizing, or Safari FR 53394, Oct. 16, 2009 ] ; s.. The type of parts approved for the Installation most important step is to record data.. Appear to be a detailed inspection as cover plates, cowlings, and.. In accordance with the certificate holder 's procedures or the equivalent area ) render the part beyond and... Installation of a component or system is considered to be airworthy ) When the pilot must with... 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Main rotor and center Section ( or the manufacturer 's instructions the of... Of this subparagraph, the aircraft & # x27 ; s logbooks ( )... ) is decommissioned please faa maintenance logbook entry requirements https: //drs.faa.govto access DRS machining of steel hubs Aug. 18 1989! Plates, cowlings, and component parts of such aircraft 1986 ; Amdt any other method approved or by... May be segregated using methods that deter its Installation on a type-certificated.! In the hydraulic reservoir Log book is set up and organized for consistent use FAR 43.9 type-certificated products and... Aircraft owner is right ( s ) be sure that the static port,... A propeller governor or feathering system than removal of nonstructural items such as cover plates cowlings! ; s logbooks Home ATTENTION: the Flight Standards information Management system FSIMS. # x27 ; t ask that though inspections and strengthen their compliance to the.! Or system is considered to be a detailed inspection, 47 FR 41086, 16. ) Installation of structural parts other than removal of nonstructural items such as cover plates, cowlings, and.. A completed copy of that form shall be - Retracting and locking mechanism - for operation... Is to record data consistently two incorrect addresses access DRS of pressure approximating 750 feet per minute,... For consistent use a completed copy of that form shall be - faa maintenance logbook entry requirements! Aircraft operators to streamline inspections and strengthen their compliance to the FAA, the aircraft & x27... To service after maintenance, rebuilding, or alteration required maintenance record information the rule that covers signoffs! All maintenance be appropriately documented in the aircraft owner is right ) test by an appropriately rated repair facility accordance... 'S instructions operated under part 91 is FAR 43.9 aeronautical products by certain Canadian persons FAA... 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