(xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. [Doc. Note the extra lines for adding additional categories. (ii) Monocoque or semimonocoque wings or control surfaces. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (18) Replacing wheels and skis where no weight and balance computation is involved. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (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). 27, 2001; Amdt. 3, 1966, and Amdt. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. (2) Replacing elastic shock absorber cords on landing gear. According to the FAA, the aircraft owner is right. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. (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). In that case, you may need to nd a mechanic willing to drive or y to where (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (xiv) The repair or replacement of internal elements of blades. guide. ); He shall thoroughly clean the aircraft and aircraft engine. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. The tests in (e) through (j) apply only to Mode S transponders. (2) Bolts - for improper torquing and lack of safetying. (a) Definitions used in this section. 43-37, 66 FR 21066, Apr. information or personal data. (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. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 43-43, 74 FR 53394, Oct. 16, 2009]. 65.101 Eligibility requirements: General. How to Use. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. (ii) Repairing or machining of steel hubs. (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. 4, 1987, as amended by Amdt. The part may be legibly marked using a non-permanent method showing its current life status. 43-36, 61 FR 19501, May 1, 1996; Amdt. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. 23, 1964, as amended by Amdt. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. 23, 1964, as amended by Amdt. 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. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (3) Non-permanent marking. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. This web site is designed for the current versions of Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. 23. 43-49, 81 FR 96700, Dec. 30, 2016]. 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. (2) Powerplant major repairs. For the purposes of this section the following definitions apply. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. 43-4, 31 FR 5249, Apr. 1993, 29 FR 5451, Apr. Maintenance records: Falsification, reproduction, or alteration. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. The signature constitutes the approval for return to service only for the work performed. 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. (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. (e) Logging pilot-in-command flight time. Before the permit is issued, an FAA inspector may personally inspect the aircraft, or require it to be inspected by an FAA certificated A&P mechanic or an appropriately certificated repair station, to determine its safety for the intended flight. (xiv) Members of the side truss, horizontal truss, or bulkheads. 6(c), Dept. Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, 135.411(a)(1), and 135.419 of this chapter). The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (eg: The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. Of the three maintenance records, the airframe (logbook) is the most permanent. The inspection must be recorded in the aircraft records. Title 14 was last amended 2/27/2023. (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. 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. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. e. Section 91.417(a)(1)(ii). Log books that comply with this CAAP do not need to be submitted to CASA for approval however; a proposed alternative to a log book or section of a log . [Doc. Replacing or cleaning spark plugs and setting of spark plug gap clearance. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 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. 3. (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. (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. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). (xxi) Repairs involving the substitution of material. 1354, 1355, and 1421 through 1430) and sec. It's very important for pilot and maintenance personnel to be sure to accurately carry the TT and TL forward with each flight and/or maintenance event. (c) Preventive maintenance. (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. 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faa maintenance logbook entry requirements