Use the surveillance formats UF = 4 and 5. You can learn more about the process (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. Table of contents from a loose-leaf binder for maintenance records. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (1) Airframe major repairs. Choosing an item from Aircraft Radio Maintenance Log Book Form 944 . (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. In that case, you may need to nd a mechanic willing to drive or y to where (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. will also bring you to search results. (ii) Hysteresis. 43-23, 47 FR 41085, Sept. 16, 1982]. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. (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.. This content is from the eCFR and may include recent changes applied to the CFR. 43-37, 66 FR 21066, Apr. (5) Replacing defective safety wiring or cotter keys. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 43-27, 52 FR 17277, May 6, 1987; Amdt. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. Any other method approved or accepted by the FAA. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. Additional performance rules for inspections. Organization and Purpose 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). 27, 2001; Amdt. If you have comments or suggestions on how to improve the www.ecfr.gov website or have questions about using www.ecfr.gov, please choose the 'Website Feedback' button below. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (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. (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. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (i) Power output (static and idle r.p.m. You didn't ask that though. (2) Studs and nuts - for improper torquing and obvious defects. Replacing any hose connection except hydraulic connections. 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. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. (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. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (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. [Amdt. user convenience only and is not intended to alter agency intent (2) Seats and safety belts - for poor condition and apparent defects. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (ii) Repairing or machining of steel hubs. There is no overlap or duplication. 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. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. Pressing enter in the search box (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. 43-4, 31 FR 5249, Apr. 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. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. [Amdt. (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. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. The term logbook originated with the ship's log a . A tag or other record may be attached to the part. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. According to the FAA, the aircraft owner is right. 106(g) (Revised Pub. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. 43-2, 30 FR 8262, June 29, 1965, as amended by 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. result, it may not include the most recent changes applied to the CFR. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. e. Section 91.417(a)(1)(ii). (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. Discipline Log Book. As you know, 14 C.F.R. [Amdt. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (ix) Hydraulic and electrical actuating system of components. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. (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 -. (a) Maintenance record entries. 43-37, 66 FR 21066, Apr. (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. (5) Flexible vibration dampeners - for poor condition and deterioration. ( 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. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. 27, 2001; Amdt. No. [Amdt. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. 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