(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. No. Docket No. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! 65.101 Eligibility requirements: General. FAA-2018-0119, Amdt. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. Pre-alpha refers to the early stages of development, when the software is . 1993, 29 FR 5451, Apr. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. [Doc. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). (3) Any alteration, for fraudulent purpose, of any record or report under this part. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (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. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (5) Flexible vibration dampeners - for poor condition and deterioration. user convenience only and is not intended to alter agency intent (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (b) Rotorcraft. (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). "Published Edition". Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. or existing codification. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. No. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. You can (3) Non-permanent marking. (b) Listing of discrepancies and placards. (6) Mutilation. (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. (a) Maintenance record entries. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. Documenting the Annual Inspection. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. 43-19, 43 FR 22639, May 25, 1978; Amdt. 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. (d) Performance requirements. [Amdt. (e) Logging pilot-in-command flight time. (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 -. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (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. (v) Case leak. Note the extra lines for adding additional categories. Regulation Y (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. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 43-38A, 79 FR 67055, Nov. 12, 2014]. (iii) After effect. 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. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. The method must deter the installation of the part after it has reached its life limit. And that's. (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. (2) Shock absorbing devices - for improper oleo fluid level. 43-14, 37 FR 14291, June 19, 1972; Amdt. 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. The tests in (e) through (j) apply only to Mode S transponders. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (ii) Monocoque or semimonocoque wings or control surfaces. View the most recent official publication: These links go to the official, published CFR, which is updated annually. 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. (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. Use this checklist to: [Amdt. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. citations and headings Title 14 was last amended 2/27/2023. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (3) The main rotor and center section (or the equivalent area). 43-39, 69 FR 44863, July 27, 2004]. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. 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: No. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. Comments or questions about document content can not be answered by OFR staff. It is not an official legal edition of the CFR. For the purposes of this section the following definitions apply. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (2) Powerplant major alterations. 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. 23, 1964, as amended by Amdt. [Amdt. 43-39, 69 FR 44863, July 27, 2004]. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (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. 1301, 1430), [Doc. 1354, 1421 through 1430 and 1502); (49 U.S.C. If you have questions for the Agency that issued the current document please contact the agency directly. 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. formatting. (2) The date of completion of the work performed. (21) Replacing any hose connection except hydraulic connections. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. The interrogations should be made at a nominal rate of 50 interrogations per second. 1993, 29 FR 5451, Apr. 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 The most important step is to record data consistently. (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. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (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. (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. 43-49, 81 FR 96700, Dec. 30, 2016]. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. (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). (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. (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. (9) Accessories - for apparent defects in security of mounting. 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 . 23, 1964, as amended by Amdt. Acceptable methods include: (1) Record keeping system. 3, 1966, and Amdt. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (2) Studs and nuts - for improper torquing and obvious defects. 43-6, 31 FR 9211, July 6, 1966. (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. 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. 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. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. (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. (c) Preventive maintenance. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. 91.409 (a) requires that an aircraft must undergo an annual inspection every 12 calendar months or sooner in order for that aircraft to be airworthy. The tag or record must include the part number, serial number, and current life status of the part. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (2) Seats and safety belts - for poor condition and apparent defects. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. Let's take a look. (2) The date of the inspection and aircraft total time in service. 43-37, 66 FR 21066, Apr. 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