43-31, 54 FR 34330, Aug. 18, 1989; Doc. The part may be legibly marked using a permanent method showing its current life status. 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. [Amdt. 24. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. Any other method approved or accepted by the FAA. Record data. 43-37, 66 FR 21066, Apr. (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. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. 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. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. 43-39, 69 FR 44863, July 27, 2004; Amdt. (2) Powerplant major repairs. (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). 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. (2) Tag or record attached to part. 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. (xii) Overhaul of controllable pitch propellers. No. 43-3, 31 FR 3336, Mar. Learn more about the eCFR, its status, and the editorial process. Regulation Y (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. [Doc. This content is from the eCFR and may include recent changes applied to the CFR. 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. 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). 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 . 1993, 29 FR 5451, Apr. (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. Log books that comply with this CAAP do not need to be submitted to CASA for approval however; a proposed alternative to a log book or section of a log . (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). 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. The aircraft owner is the one who applies for the permit, using FAA form 8130-6, which is actually an application for a U.S. airworthiness certificate. Okta Mobile for end users. formatting. 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. (iv) Complete disassembly of complex hydraulic power valves. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. (3) Propeller major alterations. 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. And that's. You didn't ask that though. 22. 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. the requirements of parts 91K, 121, 125, 133, 135, and 145. The eCFR is displayed with paragraphs split and indented to follow [Doc. 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. Classroom Visitor Log Book. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. 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. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. No person shall operate this aircraft unless within the preceding 12 calendar months it has had a condition inspection performed in accordance with the scope and detail of appendix D to part 43, or other FAA-approved programs, and found to be in a condition for safe operation. 43-43, 74 FR 53394, Oct. 16, 2009]. 43-39, 69 FR 44863, July 27, 2004]. 43-36, 61 FR 19501, May 1, 1996; Amdt. This web site is designed for the current versions of (eg: A mechanic can be the one to solicit the ferry permit on the owner's behalf if the owner supplies a signed letter of authorization. No. FAA-2018-0119, Amdt. 1655(c))), [Amdt. (xv) Main seat support braces and brackets. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (iii) Rewinding the field coil of an electrical accessory. 43-51, 86 FR 4381, Jan. 15, 2021], (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. Organization and Purpose Where To Go For Honda Maintenance Although . site when drafting amendatory language for Federal regulations: 43-31, 54 FR 34330, Aug. 18, 1989]. 23, 1964, as amended by Amdt. (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. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. 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). Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Use this checklist to: Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. (v) Replacement of outer laminations on fixed pitch wood propellers. The method must deter the installation of the part after it has reached its life limit. (xxi) Repairs involving the substitution of material. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. No. (2) Each person approving a reciprocating-engine-powered aircraft for return to service after an annual or 100-hour inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations of -. guide. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. 23, 1964, as amended by Amdt. The part may be segregated using methods that deter its installation on a type-certificated product. Title 14 was last amended 2/27/2023. The part may be mutilated to deter its installation in a type certificated product. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (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. 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. 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: (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 kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. [Amdt. (5) Segregation. Choosing an item from This contact form is only for website help or website suggestions. 91.417 Maintenance records. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. The inspection must be recorded in the aircraft records. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. (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. (a) Definitions. ); 3. (6) Electrical system - for chafing and improper operation of switches. 27, 2001], (a) General. 1/1.1 (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. Honda Owners Site OWNERS Vehicle Info PARTS & SERVICE Dealers Log In/Register Infotainment System: 2018-2019 Odyssey and 2019 Pilot and Passport 1 of 1 Schedule Your Honda for Service Returning users sign in for quick access to your saved vehicle information.Support and Service Warranty Info . 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. - Federal Aviation Administration, Department of Transportation, https://www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . 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. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. Pertinent details of the repair are on file at this repair station under Order No. Aircraft Radio Maintenance Log Book Form 944 . Enhanced content is provided to the user to provide additional context. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. 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. However, those who maintain separate records for the airframe, power plant, propellers, and other components must document the 100-hour inspection, if required, in the record of each component (see 14 CFR 43.11 (a)). No. (4) Appliance major alterations. If it had been a non-FAA-approved part, a Form 337 would not be required. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (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. No. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. 101, 610, 72 Stat. The date of completion. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. Please do not provide confidential 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. (iv) Friction. or existing codification. For miscellaneous technical amendments to this part 43, see Amdt. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. FAR 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). (17) Replacing bulbs, reflectors, and lenses of position and landing lights. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. 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. Noise emanating from trains and associated repair and maintenance equipment. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 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. (ii) Hysteresis. (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)). (3) Non-permanent marking. e. Section 91.417(a)(1)(ii). 106(g) (Revised Pub. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. 65.101 Eligibility requirements: General. 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. 43-37, 66 FR 21066, Apr. (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). There is no overlap or duplication. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. This new version now contains an entry for tracking GPS database updates. ___, For signature of authorized representative), (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. (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. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. 1993, 29 FR 5451, Apr. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. ( d ) single aircraft logbook must record annual and 100-hour inspections in that faa maintenance logbook entry requirements 43 see... When the pilot is the sole manipulator of the controls of an aircraft for which basis for starting new... ( xxii ) the repair of damaged areas in metal or plywood stressed covering exceeding six inches any! Of position and landing lights technical amendments to this part 43, see Amdt initial inspection, routine and inspections! And that & # x27 ; t ask that though is the sole manipulator of the are. Progressive inspection schedule improper internal condition and improper internal tolerances of material stressed exceeding... 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