Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). For miscellaneous technical amendments to this part 43, see Amdt. 1 CFR 1.1 The FAA lists separate requirements to log PIC time in 61.51 (e) (1). (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). Disposition of life-limited aircraft parts. No. Record data. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. (c) Preventive maintenance. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. [Doc. (ii) Hysteresis. (i) Power output (static and idle r.p.m. 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. 43-40, 71 FR 40877, July 14, 2005]. 43-19, 43 FR 22639, May 25, 1978; Amdt. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. 21. 43.2 Records of overhaul and rebuilding. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. (xxiii) The repair of portions of skin sheets by making additional seams. (xiv) The repair or replacement of internal elements of blades. 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. FAA STANDARDS FOR ELECTRONIC RECORDS. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. According to the FAA, the aircraft owner is right. 1993, 29 FR 5451, Apr. (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. Aircraft Radio Maintenance Log Book Form 944 . Of the three maintenance records, the airframe (logbook) is the most permanent. The tests in (e) through (j) apply only to Mode S transponders. (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. 22. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (eg: Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. e. Section 91.417(a)(1)(ii). is available with paragraph structure matching the official CFR 27, 2001; Amdt. 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. And that's. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. 43-28, 52 FR 20028, June 16, 1987; Amdt. user convenience only and is not intended to alter agency intent 43-7, 32 FR 7587, May 24, 1967; Amdt. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. 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. [Doc. (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. This new version now contains an entry for tracking GPS database updates. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (vi) Installation of parts not approved for the propeller. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. Title 14 was last amended 2/27/2023. 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. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. These words show that the FAA intends that a logbook, or equivalent document, and aircraft maintenance records must exist in some format for each TC aircraft. 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. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. Choosing an item from Comments or questions about document content can not be answered by OFR staff. [Doc. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. This content is from the eCFR and is authoritative but unofficial. This inspection will be recorded in the aircraft maintenance records. Background and more details are available in the (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. It is not an official legal edition of the CFR. 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. (c) This section does not apply to persons performing inspections in accordance with Part 91, 125, 135.411(a)(1), or 135.419 of this chapter. (a) Maintenance record entries. 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. FAA-2018-0119, Amdt. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. 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. Replacing and servicing batteries. 7572; 49 U.S.C. 27, 2001; Amdt. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. 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. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. (v) Installation of propeller de-icing system. (23) Cleaning or replacing fuel and oil strainers or filter elements. The software release life cycle is the process of developing, testing, and distributing a software product. (4) Appliance major alterations. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (3) Windows and windshields - for deterioration and breakage. This web site is designed for the current versions of (e) Logging pilot-in-command flight time. View the most recent official publication: These links go to the official, published CFR, which is updated annually. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. Your . 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. Pre-alpha refers to the early stages of development, when the software is . (4) Permanent marking. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. 43-3, 31 FR 3336, Mar. Use the correct address and at least two incorrect addresses. You are using an unsupported browser. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (6) Engine controls - for defects, improper travel, and improper safetying. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. 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. 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. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. Maintenance records: Falsification, reproduction, or alteration. The part may be segregated using methods that deter its installation on a type-certificated product. Tutorials Log Book. No. ); 27, 2001], (a) General. 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. (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. The date the work was completed. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. No. (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. (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. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. 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. (iv) Installation of a propeller governor or feathering system. A completed copy of that form shall be -. 43-38A, 79 FR 67055, Nov. 12, 2014]. (2) Studs and nuts - for improper torquing and obvious defects. Pertinent details of the repair are on file at this repair station under Order No. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. (2) Bolts - for improper torquing and lack of safetying. (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. This important rule sets the requirements for the recording. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. the requirements of parts 91K, 121, 125, 133, 135, and 145. (xii) Overhaul of controllable pitch propellers. 43-51, 86 FR 4381, Jan. 15, 2021], (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. Fri, 05/01/2015 - 12:00. (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. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. (Secs. (3) Determine that the static port heater, if installed, is operative. (3) Bonding and shielding - for improper installation and poor condition. There is no overlap or duplication. (2) Powerplant major alterations. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (viii) Keel and chine members of boat hulls or floats. The test point shall be approached at a rate compatible with the test equipment. 23, 1964, as amended by Amdt. FAA acceptance is also required for certificate holders who use electronic records, and the electronic signatures associated with those records, to satisfy the requirements of parts 141, 142, and 147. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. Typical Maintenance entry for 100hr/annual inspection Reference: FAA-G-8082-11 IA KNOWLEDGE TEST INFORMATION FIGURE 9.-Example of a record entry for an annual inspection in which the aircraft was found to be unairworthy March 30, 1998 Total Aircraft Time 1853.00 Hours Tach Reading 975.80 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (3) That product does not accumulate time in service while the part is removed. [Amdt. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. 43-31, 54 FR 34330, Aug. 18, 1989]. information or personal data. (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 . Test Okta app access on pilot members. However, those who maintain separate records for the airframe, power plant, propellers, and other components must document the 100-hour inspection, if required, in the record of each component (see 14 CFR 43.11 (a)). (ii) Monocoque or semimonocoque wings or control surfaces. 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). (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. Pressing enter in the search box (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. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (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. SB-114 (7/15/83) -- Pilot Light Valve . (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). 16, 1982, as amended by Amdt commonly associated with the operation of aircraft, nuclear plants, accelerators... 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