Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. SB-114 (7/15/83) -- Pilot Light Valve . [Doc. [Doc. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (3) Windows and windshields - for deterioration and breakage. (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. (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. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. 43-6, 31 FR 9211, July 6, 1966. (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 -. Replacing and servicing batteries. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. FAA STANDARDS FOR ELECTRONIC RECORDS. (a) Except for work performed in accordance with 91.411 and 91.413, each registered owner or operator shall keep the following records for the periods specified in paragraph (b) of this section . Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (v) Replacement of outer laminations on fixed pitch wood propellers. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. Noise emanating from trains and associated repair and maintenance equipment. FAR 43.9 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 term logbook originated with the ship's log a . 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. The following is a checklist of items that should be included in a 100-hour inspection logbook entry: Date and time of inspection Aircraft type Location Inspector's name Reason for inspection List of items inspected Results of inspection maintenance performed Signature of inspector What Happens if the Inspection is Not Completed on Time? Maintenance records: Falsification, reproduction, or alteration. (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Requirements for aircraft maintenance log book entries following an annual inspection can be tricky and confusing not only for the mechanic but for the owner/operator, especially where airworthiness discrepancies have been found by the airframe and powerplant mechanic (A&P) with inspection authorization (IA). (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. is available with paragraph structure matching the official CFR (xxiii) The repair of portions of skin sheets by making additional seams. 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. 1655(c))), [Amdt. (e) Logging pilot-in-command flight time. Each is a special inspection unto itself; they're all different. 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. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. 43-37, 66 FR 21066, Apr. If you work for a Federal agency, use this drafting Displaying title 14, up to date as of 2/27/2023. 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. 43-36, 61 FR 19501, May 1, 1996; Amdt. 27, 2001], (a) General. 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. (viii) Keel and chine members of boat hulls or floats. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. The tag or record must include the part number, serial number, and current life status of the part. No. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. guide. 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. This new version now contains an entry for tracking GPS database updates. (ix) Hydraulic and electrical actuating system of components. (5) Segregation. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. 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. The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. will also bring you to search results. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. FAA-2015-1621, Amdt. No. 43.10 Disposition of life-limited aircraft parts. 43-40, 71 FR 40877, July 14, 2005]. FAR). It typically consists of several stages, such as pre-alpha, alpha, beta, and release candidate, before the final version, or "gold," is released to the public. (x) Wing main ribs and compression members. developer resources. 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. (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. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. Things can get a bit more complicated (and costly) if you can't nd a local A&P willing to sign off the safe-to-ferry logbook entry. switch to drafting.ecfr.gov. (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (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. (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. (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) -. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. 24. 43.11 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. As you know, 14 C.F.R. (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. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. 43-39, 69 FR 44863, July 27, 2004]. 1/1.1 (a) Maintenance record entries. (iii) Performed without the use of tools and/or special equipment. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed 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; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. (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. A completed copy of that form shall be -. 4, 1987, as amended by Amdt. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. (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. Disposition of life-limited aircraft parts. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. A mechanic can be the one to solicit the ferry permit on the owner's behalf if the owner supplies a signed letter of authorization. (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. (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. Record data. (i) Power output (static and idle r.p.m. 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. (a) Definitions used in this section. of Transportation Act (49 U.S.C. [Amdt. 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. 23. 43-37, 66 FR 21066, Apr. The most important step is to record data consistently. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. This content is from the eCFR and is authoritative but unofficial. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. We recommend you directly contact the agency responsible for the content in question. (28) The installations of anti-misfueling devices to reduce the diameter of fuel tank filler openings provided the specific device has been made a part of the aircraft type certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation does not involve the disassembly of the existing tank filler opening. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. Although the applicable regulations describe the types of maintenance records that must be made and kept, the regulations do not set forth the format or form of the record. (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. No. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. 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 (3) Any alteration, for fraudulent purpose, of any record or report under this part. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. The method must deter the installation of the part after it has reached its life limit. (ii) Hysteresis. 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. (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. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (d) Transfer of life-limited parts. (ii) Monocoque or semimonocoque wings or control surfaces. 22. 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. Without well-trained quality assurance personnel, pilots must take responsibility for diving into the logbook (s) and flight packs to make sure the aircraft is ready and safe to fly. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. (2) Shock absorbing devices - for improper oleo fluid level. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. Tutorials Log Book. View the most recent official publication: These links go to the official, published CFR, which is updated annually. Organization and Purpose (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. (2) Replacing elastic shock absorber cords on landing gear. (v) Case leak. user convenience only and is not intended to alter agency intent (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. 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. 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. In that case, you may need to nd a mechanic willing to drive or y to where King Airs have lube item requirements due every 12 months plus a host of others due at 200-, 400-, 600-, 800-, and 1200-hour intervals. Pressing enter in the search box The date of completion. (2) Seats and safety belts - for poor condition and apparent defects. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (b) Rotorcraft. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. No. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. 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) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. 23, 1964, as amended by Amdt. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. 43.15 Additional performance rules for inspections. (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. (Secs. SB-115 (10/26/83) -- Deflation Panel Pull Forces . (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (3) Bonding and shielding - for improper installation and poor condition. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. formatting. (v) Installation of structural parts other than the type of parts approved for the installation. 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. (xiv) The repair or replacement of internal elements of blades. (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. (23) Cleaning or replacing fuel and oil strainers or filter elements. (iv) Complete disassembly of complex hydraulic power valves. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. 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). Use the surveillance formats UF = 4 and 5. This important rule sets the requirements for the recording. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. the hierarchy of the document. . (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) 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. Title 14 was last amended 2/27/2023. (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. This system may include electronic, paper, or other means of record keeping. 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