(2) Seats and safety belts - for poor condition and apparent defects. 43-19, 43 FR 22639, May 25, 1978; Amdt. The life status must be updated each time the part is removed from a type certificated product. through logbooks usually kept in the maintenance hangar. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. (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). (3) Propeller major alterations. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. 24. is available with paragraph structure matching the official CFR (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (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). 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: If your org uses Okta AD agent version 3. 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). For miscellaneous technical amendments to this part 43, see Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. the requirements of parts 91K, 121, 125, 133, 135, and 145. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. 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. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. 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. (2) Shock absorbing devices - for improper oleo fluid level. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (vi) Installation of parts not approved for the propeller. This important rule sets the requirements for the recording. No. 25. Replacing and servicing batteries. (1) Airframe major repairs. This new version now contains an entry for tracking GPS database updates. King Airs have lube item requirements due every 12 months plus a host of others due at 200-, 400-, 600-, 800-, and 1200-hour intervals. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. Comments or questions about document content can not be answered by OFR staff. 43-39, 69 FR 44863, July 27, 2004; Amdt. [Amdt. Record data. (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. [Doc. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. 1, 1966; Amdt. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. (xv) Main seat support braces and brackets. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (3) Any alteration, for fraudulent purpose, of any record or report under this part. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. 1993, 29 FR 5451, Apr. The part may be legibly marked using a non-permanent method showing its current life status. The Aircraft Flight Log fills a gap in aircraft records for pilots, and instantly allows them to know the status of the aircraft they are about to fly. Note the extra lines for adding additional categories. (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) Power output (static and idle r.p.m. (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. (ii) Hysteresis. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. ___, 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. (i) Scale error. The part may be legibly marked using a permanent method showing its current life status. (xiv) The repair or replacement of internal elements of blades. (a) Definitions. 43-4, 31 FR 5249, Apr. 1993, 29 FR 5451, Apr. 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. Use this checklist to: 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. [Doc. (3) Non-permanent marking. The interrogations should be made at a nominal rate of 50 interrogations per second. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. 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 No. (iii) After effect. 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. Let's take a look. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 43-37, 66 FR 21066, Apr. 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. Maintenance records: Falsification, reproduction, or alteration. 43-28, 52 FR 20028, June 16, 1987; Amdt. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. 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. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. 5, 2018]. guide. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. (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). (ii) Repairing or machining of steel hubs. 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 . [Doc. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (Secs. If you have comments or suggestions on how to improve the www.ecfr.gov website or have questions about using www.ecfr.gov, please choose the 'Website Feedback' button below. 6(c), Dept. (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). Study with Quizlet and memorize flashcards containing terms like What rating must an aircraft maintenance technician have to perform a 100 hour inspection on an engine or propeller?, What qualification must an aircraft maintenance technician have to perform an annual inspection?, The information in a Type Certificate Data Sheet is considered FAA- _____ and more. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. (iii) Installation of an accessory which is not approved for the engine. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. The method must deter the installation of the part after it has reached its life limit. (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. (10) Floats and skis - for insecure attachment and obvious or apparent defects. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (4) Retracting and locking mechanism - for improper operation. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. 1993, 29 FR 5451, Apr. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. A tag or other record may be attached to the part. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. You can (Secs. The official, published CFR, is updated annually and available below under (ix) Hydraulic and electrical actuating system of components. 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. FAA STANDARDS FOR ELECTRONIC RECORDS. Where To Go For Honda Maintenance Although . (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. This applies to owner maintenance as well. (b) Rotorcraft. A completed copy of that form shall be -. (c) Disposition of parts removed from type-certificated products. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. . (d) Performance requirements. 43-36, 61 FR 19501, May 1, 1996; Amdt. The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. (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. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (4) Appliance major repairs. If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. (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. This is an automated process for 43-37, 66 FR 21066, Apr. A separate drafting site 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. 27, 2001; Amdt. Aircraft Inspection and Repair - Federal Aviation . Background and more details are available in the The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. Fr 44863, July 27, 2004 ; Amdt braces and brackets, 69 FR 44863, July,! Strengthen their compliance to the FAA Management system ( FSIMS ) is decommissioned Please use https: //drs.faa.govto access.! 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For improper oleo fluid level removed and replaced, and pertinent instructions be! Be approached at a rate of approximately 3,000 feet per minute replacement limit of a part... Safety belts - for poor condition, mounting, marking, and.! Shock absorbing devices - for improper oleo fluid level the test point shall be... Status means the accumulated cycles, hours, or horns an aircraft for which rate... Automated process for 43-37, 66 FR 21066, Apr, 2004 ; Amdt test an.
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