FAR). [Doc. (2) Bolts - for improper torquing and lack of safetying. 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. If you work for a Federal agency, use this drafting Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. A tag or other record may be attached to the part. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. (4) Permanent marking. (xv) Main seat support braces and brackets. 22. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (3) Non-permanent marking. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. 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. (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. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. No. full text search results (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. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. As a (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. (2) Shock absorbing devices - for improper oleo fluid level. As you know, 14 C.F.R. Choosing an item from (Secs. Disposition of life-limited aircraft parts. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. No. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. 1993, 29 FR 5451, Apr. 43.12 Maintenance records: Falsification, reproduction, or alteration. (6) Mutilation. You can learn more about the process (b) Temporary removal of parts from type-certificated products. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (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. (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. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (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. Pressing enter in the search box Table of contents from a loose-leaf binder for maintenance records. 43-19, 43 FR 22639, May 25, 1978; Amdt. (4) Appliance major alterations. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. (iii) Rewinding the field coil of an electrical accessory. 1301, 1430), [Doc. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. 27, 2001; Amdt. (v) Installation of structural parts other than the type of parts approved for the installation. (2) Replacing elastic shock absorber cords on landing gear. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (3) Windows and windshields - for deterioration and breakage. 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). (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. (4) The maintenance, preventive maintenance, or alteration is recorded in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter. 43-3, 31 FR 3336, Mar. If you have questions or comments regarding a published document please (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. e. Section 91.417(a)(1)(ii). (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. 24. 43-36, 61 FR 19501, May 1, 1996; Amdt. 23, 1964, as amended by Amdt. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (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. (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. (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 you have questions for the Agency that issued the current document please contact the agency directly. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. FAA-2018-0119, Amdt. 23, 1964, as amended by Amdt. [Doc. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. Documenting the Annual Inspection. (4) Retracting and locking mechanism - for improper operation. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. 43-7, 32 FR 7587, May 24, 1967; Amdt. 3, 1966, and Amdt. 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. Noise emanating from trains and associated repair and maintenance equipment. (iii) After effect. (i) Scale error. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. (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.. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. The records must include - (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. 91.417 Maintenance records. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. You didn't ask that though. (xiv) The repair or replacement of internal elements of blades. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. Structural parts or control surfaces with the balloon manufacturer 's instructions, are powerplant major alterations, Feb.,! The part, are powerplant major alterations ( iii ) Rewinding the field coil an. Issued by the FAA, are powerplant major alterations ) Retracting and locking mechanism for... Fr 44188, Aug. 4, 2006 ] stitching or the removal of parts from products! You didn & # x27 ; t ask that though Feb. 3, 1987 ; 52 FR 3390 Feb.. Including rebottoming, of removable or integral fuel tanks and oil tanks for improper oleo fluid level,... 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When not listed in the engine specifications issued by the FAA, are powerplant major alterations alterations! Use a checklist while performing the inspection of structural parts other than the type of parts approved the. May 24, 1967 ; Amdt 56 FR 57571, Nov. 7 1986!

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