(10) All systems - for improper installation, poor general condition, defects, and insecure attachment. [Doc. 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: The date of completion. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. The date the work was completed. (2) Replacing elastic shock absorber cords on landing gear. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (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. 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. (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. (3) Determine that the static port heater, if installed, is operative. [Amdt. (5) Flexible vibration dampeners - for poor condition and deterioration. (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. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . The method must deter the installation of the part after it has reached its life limit. Noise emanating from trains and associated repair and maintenance equipment. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. 43-50, 83 FR 9170, Mar. citations and headings Your . 43-41, 72 FR 53680, Sept. 20, 2007; Doc. [Doc. 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 . A completed copy of that form shall be -. 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 . ___, 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. (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. This is an automated process for 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. (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. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. Maintenance records: Falsification, reproduction, or alteration. 43.7 Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (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). 7572; 49 U.S.C. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. 6(c), Dept. (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. result, it may not include the most recent changes applied to the CFR. According to the FAA, the aircraft owner is right. (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 life status must be updated each time the part is removed from a type certificated product. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. 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. (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). If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (3) Propeller major alterations. (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. (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. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. (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. (xiv) The repair or replacement of internal elements of blades. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. 43-27, 52 FR 17277, May 6, 1987; Amdt. learn more about the process here. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. 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. 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. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. The part may be mutilated to deter its installation in a type certificated product. Use this checklist to: 24. 43-36, 61 FR 19501, May 1, 1996; Amdt. 23, 1964, as amended by Amdt. This inspection will be recorded in the aircraft maintenance records. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. (7) Wheels - for cracks, defects, and condition of bearings. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Documenting the Annual Inspection. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. 1993, 29 FR 5451, Apr. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. This important rule sets the requirements for the recording. Acceptable methods include: (1) Record keeping system. (2) Powerplant major repairs. FAA-2018-0119, Amdt. (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. (5) Replacing defective safety wiring or cotter keys. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 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 1,2, and 4, p/n 24029, 24030 respectively. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. Enhanced content is provided to the user to provide additional context. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. Regulation Y We recommend you directly contact the agency responsible for the content in question. 1993, 29 FR 5451, Apr. No. No. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. The tag or record must include the part number, serial number, and current life status of the part. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (1) Airframe major repairs. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. FAA-2015-1621, Amdt. (Secs. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. A separate drafting site The error at all test points must not exceed the tolerances specified in Table I. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. 1655(c))), [Amdt. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. 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. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. 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. (v) Installation of structural parts other than the type of parts approved for the installation. (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 -. "Published Edition". (2) The date of completion of the work performed. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. No. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. However, this paragraph does not authorize the performance of any inspection required by Part 91 or Part 125 of this chapter or any inspection performed after a major repair or alteration. 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 -. The most important step is to record data consistently. 23. Additional performance rules for inspections. (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. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. (3) Non-permanent marking. (ii) Repairing or machining of steel hubs. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. Record data. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. Replacing prefabricated fuel lines. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). (23) Cleaning or replacing fuel and oil strainers or filter elements. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. 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. 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. (iii) Performed without the use of tools and/or special equipment. 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