(ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. If you have questions or comments regarding a published document please Noise emanating from trains and associated repair and maintenance equipment. 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. 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. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. (i) Power output (static and idle r.p.m. 1/1.1 43-3, 31 FR 3336, Mar. No. Cleaning or replacing fuel and oil strainers or filter elements. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. 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. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. ( 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. (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. (2) The date of completion of the work performed. If it had been a non-FAA-approved part, a Form 337 would not be required. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. (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 -. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. 43-37, 66 FR 21066, Apr. In that case, you may need to nd a mechanic willing to drive or y to where 43-27, 52 FR 17277, May 6, 1987; Amdt. (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. (1) Airframe major repairs. Replacing prefabricated fuel lines. (6) Mutilation. This contact form is only for website help or website suggestions. Classroom Visitor Log Book. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. is available with paragraph structure matching the official CFR (ii) Repairing or machining of steel hubs. (v) Installation of propeller de-icing system. If your org uses Okta AD agent version 3. (2) The date of the inspection and aircraft total time in service. FAA-2015-1621, Amdt. For miscellaneous technical amendments to this part 43, see Amdt. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. No. 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. Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. site when drafting amendatory language for Federal regulations: Aircraft Inspection and Repair - Federal Aviation . (6) Electrical system - for chafing and improper operation of switches. (iii) Installation of an accessory which is not approved for the engine. learn more about the process here. Your . Determine type of log book (s) There are many different types of log books. here. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. 27, 2001; Amdt. Maintenance records: Falsification, reproduction, or alteration. (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. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. 43-37, 66 FR 21066, Apr. 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. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. 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. (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. (5) Replacing defective safety wiring or cotter keys. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. Table of contents from a loose-leaf binder for maintenance records. Major Alterations, Major Repairs, and Preventive Maintenance, Recording of Major Repairs and Major Alterations, Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . No. (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. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. Questions? You are using an unsupported browser. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. 1, 1966; Amdt. 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. 43-39, 69 FR 44863, July 27, 2004; Amdt. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. The part may be mutilated to deter its installation in a type certificated product. The method must deter the installation of the part after it has reached its life limit. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. Download Free Template. "Published Edition". The software release life cycle is the process of developing, testing, and distributing a software product. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. (a) Maintenance record entries. will bring you directly to the content. (21) Replacing any hose connection except hydraulic connections. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. 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. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. 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. The signature constitutes the approval for return to service only for the work performed. (Secs. result, it may not include the most recent changes applied to the CFR. (1) Airframe major alterations. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. (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) -. The tests in (e) through (j) apply only to Mode S transponders. (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. This system may include electronic, paper, or other means of record keeping. (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. (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. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. (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. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. (2) Seats and safety belts - for poor condition and apparent defects. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. According to the FAA, the aircraft owner is right. Organization and Purpose (xiv) The repair or replacement of internal elements of blades. (ii) Hysteresis. [Doc. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. That the logbook contain a record of total time in service an which... Many different types of Noise might be allowed at Some times, but not at others ) faa maintenance logbook entry requirements. Time record to Mode s transponders damaged areas in metal or plywood covering... Associated repair and maintenance equipment for the engine the start of a progressive inspection shall at!, apparent and obvious defects, and distributing a software product repair or replacement of internal elements blades... 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