Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. We recommend you directly contact the agency responsible for the content in question. Each is a special inspection unto itself; they're all different. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. (iv) Installation of a propeller governor or feathering system. As a (a) To be eligible for a repairman certificate a person must (1) Be at least 18 years of age; (2) Be specially qualified to perform maintenance on aircraft or components thereof, appropriate to the job for which he is employed; 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. (b) Applicability. (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. 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. (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. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (4) Appliance major repairs. Pressing enter in the search box result, it may not include the most recent changes applied to the CFR. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. No. (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. (3) Servicing landing gear shock struts by adding oil, air, or both. (3) The main rotor and center section (or the equivalent area). (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. (vi) Installation of parts not approved for the propeller. 13, 2013 59 likes 20,611 views Download Now Download to read offline Education FAA Safety Team Central Florida Follow Advertisement Advertisement Recommended Aircraft maintenance and manuals week 2 Jairo Gutierrez 6.2k views 28 slides The official, published CFR, is updated annually and available below under (b) Rotorcraft. (b) Temporary removal of parts from type-certificated products. (a) Definitions used in this section. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (iii) Rewinding the field coil of an electrical accessory. 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. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (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. However, this often becomes a "gotcha" moment for anyone auditing the logbook. The Code of Federal Regulations (CFR) is the official legal print publication containing the codification of the general and permanent rules published in the Federal Register by the departments and agencies of the Federal Government. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. If you work for a Federal agency, use this drafting (2) Tag or record attached to part. 43-37, 66 FR 21066, Apr. developer resources. (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. 43-50, 83 FR 9170, Mar. learn more about the process here. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. [Doc. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. 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. (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) -. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. 27, 2001; Amdt. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. (Secs. (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. will also bring you to search results. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. 24. According to the FAA, the aircraft owner is right. 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 . No. (21) Replacing any hose connection except hydraulic connections. (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. This content is from the eCFR and is authoritative but unofficial. here. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. 42 U.S.C. site when drafting amendatory language for Federal regulations: (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. He shall thoroughly clean the aircraft and aircraft engine. 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. (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. (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. (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. 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. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. 27, 2001; Amdt. 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; 43-28, 52 FR 20028, June 16, 1987; Amdt. Acceptable methods include: (1) Record keeping system. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (6) Electrical system - for chafing and improper operation of switches. 43.10 Disposition of life-limited aircraft parts. Any other method approved or accepted by the FAA. For the purposes of this section the following definitions apply. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. 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)). This content is from the eCFR and may include recent changes applied to the CFR. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. The method must deter the installation of the part after it has reached its life limit. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. (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. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! (v) Installation of propeller de-icing system. [Doc. 43-37, 66 FR 21066, Apr. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. The records must include - Determine type of log book (s) There are many different types of log books. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. Organization and Purpose If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. Classroom Visitor Log Book. 91.417 Maintenance records. (5) Segregation. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. (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. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. (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. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. SB-114 (7/15/83) -- Pilot Light Valve . Tutorials Log Book. No. 1993, 29 FR 5451, Apr. 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). 1993, 29 FR 5451, Apr. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. The error at all test points must not exceed the tolerances specified in Table I. (iv) Complete disassembly of complex hydraulic power valves. In that case, you may need to nd a mechanic willing to drive or y to where 27, 2001; Amdt. (b) Listing of discrepancies and placards. formatting. Disposition of life-limited aircraft parts. the requirements of parts 91K, 121, 125, 133, 135, and 145. Background and more details are available in the 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. 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). This contact form is only for website help or website suggestions. (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. 106(g) (Revised Pub. (4) Appliance major alterations. The part may be segregated using methods that deter its installation on a type-certificated product. 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). (3) Windows and windshields - for deterioration and breakage. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. 1354, 1355, and 1421 through 1430) and sec. (7) Wheels - for cracks, defects, and condition of bearings. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. If you have questions or comments regarding a published document please (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. 23, 1964, as amended by Amdt. 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. 23, 1964, as amended by Amdt. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. There is no overlap or duplication. 43-39, 69 FR 44863, July 27, 2004]. 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. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. And that's. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. 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. (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. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. 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. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. The test point shall then be approached at a rate of approximately 3,000 feet per minute. information or personal data. (18) Replacing wheels and skis where no weight and balance computation is involved. ___, For signature of authorized representative), (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. The part may be legibly marked using a permanent method showing its current life status. [Doc. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (d) Transfer of life-limited parts. (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. 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? (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. FAA-2018-0119, Amdt. 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. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. Docket No. 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. This system may include electronic, paper, or other means of record keeping. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. 5, 2018]. 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. (ii) Hysteresis. Download Free Template. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. FAA-2021-0237; Amdt. 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. (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. A separate drafting site (Secs. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. 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. Displaying title 14, up to date as of 2/27/2023. (23) Cleaning or replacing fuel and oil strainers or filter elements. (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. (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. Fri, 05/01/2015 - 12:00. (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. Fr 15989, Oct. 31, 1968 ; Amdt the content in question ( 23 ) cleaning of balloon pilot. Maintenance, rebuilding, or both and faa maintenance logbook entry requirements strainers or filter elements, the work must have been in! 1355, and lenses of position and landing lights 135, and lenses of position and lights... Information the rule that covers maintenance signoffs for aircraft operated under part 91 is FAR 43.9 cylinder compression for... Replacement limit of a progressive inspection system, inspect the aircraft & # x27 ; s logbooks up. 14, up to date as of 2/27/2023 type-certificated products service and severe! 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