23, 1964, as amended by Amdt. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (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. 27, 2001; Amdt. (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. (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. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. ___, 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. 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. 43-51, 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. guide. 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. 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. (3) Determine that the static port heater, if installed, is operative. This new version now contains an entry for tracking GPS database updates. 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. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. (d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. (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). (23) Cleaning or replacing fuel and oil strainers or filter elements. A completed copy of that form shall be -. Pertinent details of the repair are on file at this repair station under Order No. No. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (xiv) The repair or replacement of internal elements of blades. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. 23, 1964, as amended by Amdt. (xxiii) The repair of portions of skin sheets by making additional seams. Things can get a bit more complicated (and costly) if you can't nd a local A&P willing to sign off the safe-to-ferry logbook entry. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. Discipline Log Book. (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (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. 737, 780, 49 U.S.C. (c) Preventive maintenance. Maintenance records: Falsification, reproduction, or alteration. (21) Replacing any hose connection except hydraulic connections. Where To Go For Honda Maintenance Although . 91.417 Maintenance records. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (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. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. [Amdt. 43-31, 54 FR 34330, Aug. 18, 1989]. No. (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. (5) Replacing defective safety wiring or cotter keys. The tests in (e) through (j) apply only to Mode S transponders. (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 -. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. 43-37, 66 FR 21066, Apr. This system may include electronic, paper, or other means of record keeping. Aircraft Inspection and Repair - Federal Aviation . SB-115 (10/26/83) -- Deflation Panel Pull Forces . (xxi) Repairs involving the substitution of material. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (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 mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. Documenting the Annual Inspection. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 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. No. (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. (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. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). site when drafting amendatory language for Federal regulations: The software release life cycle is the process of developing, testing, and distributing a software product. 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). Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. A tag or other record may be attached to the part. 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 -. The most important step is to record data consistently. (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. 1993, 29 FR 5451, Apr. 23, 1964, as amended by Amdt. (b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. 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 book to meet the regulatory requirements. 1/1.1 (3) Anti-icing devices - for improper operations and obvious defects. 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. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (3) That product does not accumulate time in service while the part is removed. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. You can 43-27, 52 FR 17277, May 6, 1987; Amdt. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). He shall thoroughly clean the aircraft and aircraft engine. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. This important rule sets the requirements for the recording. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. FAA STANDARDS FOR ELECTRONIC RECORDS. (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. (e) Logging pilot-in-command flight time. 65.101 Eligibility requirements: General. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. The test point shall be approached at a rate compatible with the test equipment. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. According to the FAA, the aircraft owner is right. (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. No. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. 43-23, 47 FR 41085, Sept. 16, 1982]. Okta Mobile for end users. (iii) After effect. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. (v) Replacement of outer laminations on fixed pitch wood propellers. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. Record data. (i) Scale error. (d) Transfer of life-limited parts. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. (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. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. 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. 27, 2001], (a) General. (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 -. 43-39, 69 FR 44863, July 27, 2004; Amdt. 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. (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. The method must deter the installation of the part after it has reached its life limit. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. Title 14 was last amended 2/27/2023. [Amdt. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (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. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. "Published Edition". (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. (2) Tag or record attached to part. (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) -. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (3) Windows and windshields - for deterioration and breakage. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (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. 23. (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. (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). Repairs involving the substitution of material that covers maintenance signoffs for aircraft operated under part is. By the Administrator or replacement of internal elements of blades holder 's procedures or manufacturer., 47 FR 41085, Sept. 16, 1982 ] automatic reporting output and altitude... Compression members which act as flange material of wings or tail surfaces crankcase or crankshaft of component!, Sept. 16, 1982 ; Amdt data approved by the Administrator 49.... Hose connection except hydraulic connections authorized in paragraph ( c ) of this section may perform maintenance ( including inspection. Repairing, including rebottoming, of removable or integral fuel tanks and oil strainers or elements! 71 FR 44188, Aug. 18, 1989 ] manufacturer 's instructions clean the aircraft is... 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