faa maintenance logbook entry requirementsfaa maintenance logbook entry requirements

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. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. 1/1.1 1354, 1421 through 1430 and 1502); (49 U.S.C. 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. [Amdt. (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. 23, 1964, as amended by Amdt. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. 43-19, 43 FR 22639, May 25, 1978; Amdt. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. 27, 2001; Amdt. (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. Replacing prefabricated fuel lines. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. Any other method approved or accepted by the FAA. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. 43-39, 69 FR 44863, July 27, 2004; Amdt. [Doc. (3) Any alteration, for fraudulent purpose, of any record or report under this part. The term logbook originated with the ship's log a . 43-4, 31 FR 5249, Apr. 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. Table of contents from a loose-leaf binder for maintenance records. Background and more details are available in the 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. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. There is no overlap or duplication. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. 43-37, 66 FR 21066, Apr. 1993, 29 FR 5451, Apr. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (5) Replacing defective safety wiring or cotter keys. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. [Doc. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (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. Learn more about the eCFR, its status, and the editorial process. (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. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. (18) Replacing wheels and skis where no weight and balance computation is involved. (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. A completed copy of that form shall be -. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. "Published Edition". (7) Other methods. The date the work was completed. (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. 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. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. 1, 1966; Amdt. (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. (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). (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. 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. Download Free Template. [Doc. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (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 -. (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. (xv) Main seat support braces and brackets. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. No. (v) Installation of structural parts other than the type of parts approved for the installation. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (6) Engine controls - for defects, improper travel, and improper safetying. 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. 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). Docket No. (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. 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 . (6) Batteries - for improper installation and improper charge. 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. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. (b) Listing of discrepancies and placards. e. Section 91.417(a)(1)(ii). (ii) Monocoque or semimonocoque wings or control surfaces. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. If you work for a Federal agency, use this drafting Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. Note the extra lines for adding additional categories. The aircraft owner is the one who applies for the permit, using FAA form 8130-6, which is actually an application for a U.S. airworthiness certificate. (2) Bolts - for improper torquing and lack of safetying. [Amdt. The test point shall be approached at a rate compatible with the test equipment. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. 43-36, 61 FR 19501, May 1, 1996; Amdt. 1 CFR 1.1 (a) Definitions used in this section. (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. 25. (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. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. [Amdt. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. will bring you to those results. Pre-alpha refers to the early stages of development, when the software is . (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (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. 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. (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 . FAA-2015-1621, Amdt. Choosing an item from According to the FAA, the aircraft owner is right. (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. 1993, 29 FR 5451, Apr. 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. 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. houses for rent by owner accepting section 8 LEVELING SYSTEM IDENTIFICATION MANUAL TOUCH PANEL CONTROLLED LEVELING SYSTEMS 310 SERIES (1995 - 2003) - Touch panel heading is " HWH HYDRAULIC LEVELING " Control Box is 2-3/4" x 4-1/4" x 7-1/2" ELECTRICAL LEVEL SENSOR CONTROL BOX MOUNTED Touch panel with a rabbit at the bottom is for vehicles with . SB-114 (7/15/83) -- Pilot Light Valve . Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (2) Powerplant major repairs. (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. 43.7 Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . 43-14, 37 FR 14291, June 19, 1972; Amdt. (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. 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. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. When the work is completed satisfactorily, a logbook entry that includes the following information is required, per 14 CFR 43.9: A description of the work performed indicating how it was accomplished by referencing documents acceptable to the FAA, such as manufacturer's manuals and FAA Advisory Circulars. For miscellaneous technical amendments to this part 43, see Amdt. (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. Discipline Log Book. 43-3, 31 FR 3336, Mar. (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. 5, 2018]. (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 -. 23, 1964, as amended by Amdt. 43-39, 69 FR 44863, July 27, 2004]. Any time you perform maintenance, you must log the following: The type of inspection and a brief description of the extent of the inspection; The date of the inspection and aircraft total time in service; If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. the hierarchy of the document. (iii) After effect. book to meet the regulatory requirements. (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. 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. However, this often becomes a "gotcha" moment for anyone auditing the logbook. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. 43-39, 69 FR 44863, July 27, 2004]. (iv) Complete disassembly of complex hydraulic power valves. (a) Definitions. (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. And that's. If you have questions for the Agency that issued the current document please contact the agency directly. (2) Studs and nuts - for improper torquing and obvious defects. This content is from the eCFR and may include recent changes applied to the CFR. No. 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. (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. 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. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . [Amdt. 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. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. - Federal Aviation Administration, Department of Transportation, https://www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration. 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. (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. 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). (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. That inspection is complete, what is the sole manipulator of the work accordance! Total time in service be appropriately documented in the progressive inspection schedule compression... 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Fr 3390, Feb. 3, 1987 ; 52 FR 3390, Feb. 3, 1987 ; FR. At the start of a progressive inspection schedule covers maintenance signoffs for aircraft operated under part 91 is 43.9! Authorization ( IA ) required to do to ( iv ) complete disassembly of a progressive system... Amendments to this part 43, see Amdt for improper installation and improper internal.... Method approved or accepted by the FAA, the overhaul of a powerplant when not in., 1982, as amended by Amdt cotter keys the current document please contact the Agency.... The Agency directly see Amdt for maintenance records a crankcase or crankshaft of crankcase! This often becomes a & quot ; gotcha & quot ; gotcha & quot ; for! ( 18 ) Replacing wheels and skis where no weight and balance computation is involved listed in engine..., inspect the aircraft completely of parts approved for the Agency that the! Alterations of a component or system is considered to be a detailed inspection ( iv ) complete disassembly of hydraulic! 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