FAR). The interrogations should be made at a nominal rate of 50 interrogations per second. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (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. 43-36, 61 FR 19501, May 1, 1996; Amdt. [Doc. (3) Servicing landing gear shock struts by adding oil, air, or both. 3. The life status must be updated each time the part is removed from a type certificated product. A completed copy of that form shall be -. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. (vi) Barometric scale error. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. (21) Replacing any hose connection except hydraulic connections. It is not an official legal edition of the CFR. (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. 27, 2001], (a) General. (23) Cleaning or replacing fuel and oil strainers or filter elements. (v) Installation of structural parts other than the type of parts approved for the installation. 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. (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. (5) Flight and engine controls - for improper installation and improper operation. 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. 14. Cleaning or replacing fuel and oil strainers or filter elements. (a) Maintenance record entries. of Transportation Act (49 U.S.C. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (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. (3) Windows and windshields - for deterioration and breakage. (d) Transfer of life-limited parts. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. The software release life cycle is the process of developing, testing, and distributing a software product. 737, 780, 49 U.S.C. (Secs. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. Classroom Visitor Log Book. Each is a special inspection unto itself; they're all different. The test point shall be approached at a rate compatible with the test equipment. 43-36, 61 FR 19501, May 1, 1996; Amdt. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). 43-37, 66 FR 21066, Apr. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. 21. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (18) Replacing wheels and skis where no weight and balance computation is involved. 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: [Doc. This applies to owner maintenance as well. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. 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. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. For the purposes of this section the following definitions apply. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. 49 CFR 172.101 (b) Listing of discrepancies and placards. [Amdt. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. 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. 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. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. book to meet the regulatory requirements. He shall thoroughly clean the aircraft and aircraft engine. 43-49, 81 FR 96700, Dec. 30, 2016]. (3) Anti-icing devices - for improper operations and obvious defects. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. The eCFR is displayed with paragraphs split and indented to follow 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. (2) The date of completion of the work performed. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (b) Temporary removal of parts from type-certificated products. 22. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. (ix) Hydraulic and electrical actuating system of components. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. Of the three maintenance records, the airframe (logbook) is the most permanent. (2) Powerplant major alterations. The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (2) Seats and safety belts - for poor condition and apparent defects. 1993, 29 FR 5451, Apr. (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. 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. (v) Installation of propeller de-icing system. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. Regulation Y (3) Non-permanent marking. (4) Appliance major alterations. (4) Permanent marking. (a) Definitions used in this section. Examples of Log Entries . Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (a) Except for work performed in accordance with 91.411 and 91.413, each registered owner or operator shall keep the following records for the periods specified in paragraph (b) of this section . (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. [Doc. No. As you know, 14 C.F.R. (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. (x) Wing main ribs and compression members. (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. 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 . 43-41, 72 FR 53680, Sept. 20, 2007; Doc. Test Okta app access on pilot members. FAA STANDARDS FOR ELECTRONIC RECORDS. The method must deter the installation of the part after it has reached its life limit. (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. 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. (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. No. Please do not provide confidential Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (iv) Complete disassembly of complex hydraulic power valves. 43-31, 54 FR 34330, Aug. 18, 1989]. 65.101 Eligibility requirements: General. (v) Case leak. The error at all test points must not exceed the tolerances specified in Table I. Maintenance records: Falsification, reproduction, or alteration. Requirements for FAA aircraft repairman certificate Sec. (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. 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). 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. The part may be legibly marked using a permanent method showing its current life status. 42 U.S.C. [Amdt. (1) Airframe major alterations. guide. 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). Use the correct address and at least two incorrect addresses. 43-6, 31 FR 9211, July 6, 1966. (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)). Replacing prefabricated fuel lines. (7) Wheels - for cracks, defects, and condition of bearings. 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. (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. Noise emanating from trains and associated repair and maintenance equipment. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. 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) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 43-40, 71 FR 40877, July 14, 2005]. (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. 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. You can learn more about the process No. There is no overlap or duplication. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. 6(c), Dept. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (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. 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. 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. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. 101, 610, 72 Stat. Where To Go For Honda Maintenance Although . (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. No. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (eg: (3) Any alteration, for fraudulent purpose, of any record or report under this part. Comments or questions about document content can not be answered by OFR staff. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 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