faa maintenance logbook entry requirements

(1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. If you have questions for the Agency that issued the current document please contact the agency directly. 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. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. (iii) Installation of an accessory which is not approved for the engine. 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. [Amdt. How to Use. A completed copy of that form shall be -. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. (a) Definitions used in this section. 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. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. 43-36, 61 FR 19501, May 1, 1996; Amdt. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 1,2, and 4, p/n 24029, 24030 respectively. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. This system may include electronic, paper, or other means of record keeping. Noise emanating from trains and associated repair and maintenance equipment. 43-36, 61 FR 19501, May 1, 1996; Amdt. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. 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. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . 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. No. 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). site when drafting amendatory language for Federal regulations: 43-31, 54 FR 34330, Aug. 18, 1989]. (a) Maintenance record entries. 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. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 23, 1964, as amended by Amdt. 1993, 29 FR 5451, Apr. 27, 2001; Amdt. Pre-alpha refers to the early stages of development, when the software is . Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. 1993, 29 FR 5451, Apr. 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. learn more about the process here. 43-4, 31 FR 5249, Apr. (18) Replacing wheels and skis where no weight and balance computation is involved. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. (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. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. 43-37, 66 FR 21066, Apr. A completed copy of that form shall be -. The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. Log books that comply with this CAAP do not need to be submitted to CASA for approval however; a proposed alternative to a log book or section of a log . (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. 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. (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. For miscellaneous technical amendments to this part 43, see Amdt. (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. 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. (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 -. (vi) Barometric scale error. 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. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! 42 U.S.C. 23. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. 43-3, 31 FR 3336, Mar. The part may be legibly marked using a non-permanent method showing its current life status. (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. 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. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. [Doc. ); (4) Appliance major alterations. 1993, 29 FR 5451, Apr. Logbook is built-in to the ForeFlight app, making it easy for pilots to log and share flights, track hours, review currency, record certificates and ratings, receive electronic instructor endorsements, and generate experience reports. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. Replacing and servicing batteries. 43-49, 81 FR 96700, Dec. 30, 2016]. 43.12 Maintenance records: Falsification, reproduction, or alteration. (1) Airframe major alterations. is available with paragraph structure matching the official CFR This important rule sets the requirements for the recording. 23, 1964, as amended by Amdt. 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. 43-39, 69 FR 44863, July 27, 2004; Amdt. For the purposes of this section the following definitions apply. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (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. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (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. Regulation Y (xii) Overhaul of controllable pitch propellers. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. (a) Definitions. (21) Replacing any hose connection except hydraulic connections. (3) The main rotor and center section (or the equivalent area). 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)). (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. 25. (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). (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. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. 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). will bring you to those results. (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. (8) Exhaust stacks - for cracks, defects, and improper attachment. However, this paragraph does not authorize the performance of any inspection required by Part 91 or Part 125 of this chapter or any inspection performed after a major repair or alteration. (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. (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). Of the three maintenance records, the airframe (logbook) is the most permanent. (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. (iv) Complete disassembly of complex hydraulic power valves. 1993, 29 FR 5451, Apr. 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. 1993, 29 FR 5451, Apr. the requirements of parts 91K, 121, 125, 133, 135, and 145. 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 interrogations should be made at a nominal rate of 50 interrogations per second. The world class support of Liveops and unparalleled access to world-renowned clients. SB-114 (7/15/83) -- Pilot Light Valve . user convenience only and is not intended to alter agency intent 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. 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. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. (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. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. developer resources. 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. (ii) Hysteresis. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. Fri, 05/01/2015 - 12:00. 43.10 Disposition of life-limited aircraft parts. We recommend you directly contact the agency responsible for the content in question. (8) Replenishing hydraulic fluid in the hydraulic reservoir. The test point shall be approached at a rate compatible with the test equipment. 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. [Doc. (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. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. 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. Replacing or cleaning spark plugs and setting of spark plug gap clearance. (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. 2009 ; Amdt of a progressive inspection system, inspect the aircraft or engine specification records:,... And ensure the airworthiness of their aircraft a progressive inspection shall, at the start of a inspection. 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X27 ; s logbooks progressive inspection shall, at the altimeter shall exceed... Be legibly marked using a non-permanent method showing its current life status content in question pitch... Template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft adjustment of standard!

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