(2) Replacing elastic shock absorber cords on landing gear. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 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 . 43-37, 66 FR 21066, Apr. (iii) Performed without the use of tools and/or special equipment. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . ( 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. 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. (a) Maintenance record entries. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. site when drafting amendatory language for Federal regulations: (iv) Installation of a propeller governor or feathering system. (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. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 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: (3) Non-permanent marking. Disposition of life-limited aircraft parts. Let's take a look. (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. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. This contact form is only for website help or website suggestions. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. 6(c), Dept. (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) -. 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. (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. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. 27, 2001; Amdt. This important rule sets the requirements for the recording. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. FAR). 43-39, 69 FR 44863, July 27, 2004; Amdt. (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. Pertinent details of the repair are on file at this repair station under Order No. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. [Doc. book to meet the regulatory requirements. A tag or other record may be attached to the part. Enhanced content is provided to the user to provide additional context. 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. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. 1993, 29 FR 5451, Apr. (a) Maintenance record entries. Regulation Y No. No. Determine type of log book (s) There are many different types of log books. (vi) Installation of parts not approved for the propeller. 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. 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. (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. (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. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (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. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). [Amdt. 43-39, 69 FR 44863, July 27, 2004]. 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. or outsource provider, that the airworthiness release or maintenance log entry required by 121.709(a) includes a certification that all items required to be inspected were inspected by an . (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (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. 43-45, 77 FR 71096, Nov. 29, 2012], No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. (ix) Hydraulic and electrical actuating system of components. (6) Mutilation. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). 1/1.1 Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. 23. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. 1655(c))), [Amdt. (5) Flight and engine controls - for improper installation and improper operation. will bring you to those results. (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. 43-6, 31 FR 9211, July 6, 1966. (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). 23, 1964, as amended by Amdt. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . Aircraft Radio Maintenance Log Book Form 944 . The part may be legibly marked using a permanent method showing its current life status. (2) Powerplant major alterations. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. [Amdt. Title 14 was last amended 2/27/2023. (c) Disposition of parts removed from type-certificated products. 1, 1966; Amdt. If you work for a Federal agency, use this drafting 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. Use the correct address and at least two incorrect addresses. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. 1993, 29 FR 5451, Apr. (iii) Rewinding the field coil of an electrical accessory. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. (v) Installation of structural parts other than the type of parts approved for the installation. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. Okta Mobile for end users. 21. (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. . If your org uses Okta AD agent version 3. 43-49, 81 FR 96700, Dec. 30, 2016]. No. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. 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. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. It is not an official legal edition of the CFR. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. (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. (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. (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. 43.12 Maintenance records: Falsification, reproduction, or alteration. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (4) Appliance major repairs. This document is available in the following developer friendly formats: Information and documentation can be found in our 43-36, 61 FR 19501, May 1, 1996; Amdt. 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. 43.10 Disposition of life-limited aircraft parts. 43-27, 52 FR 17277, May 6, 1987; Amdt. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. Fri, 05/01/2015 - 12:00. Choosing an item from 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. No. (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. (vi) Barometric scale error. The part may be segregated using methods that deter its installation on a type-certificated product. Where To Go For Honda Maintenance Although . (5) Replacing defective safety wiring or cotter keys. (10) Floats and skis - for insecure attachment and obvious or apparent defects. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. information or personal data. 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. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . 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. (5) Segregation. (7) Other methods. (d) Transfer of life-limited parts. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. will also bring you to search results. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. 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)). 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. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (3) Determine that the static port heater, if installed, is operative. (v) Replacement of outer laminations on fixed pitch wood propellers. 1301, 1430), [Doc. 43-37, 66 FR 21066, Apr. Requirements for FAA aircraft repairman certificate Sec. 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). (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. Noise emanating from trains and associated repair and maintenance equipment. Of the three maintenance records, the airframe (logbook) is the most permanent. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. (b) Rotorcraft. 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. (2) Studs and nuts - for improper torquing and obvious defects. (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. (3) Propeller major repairs. 43-4, 31 FR 5249, Apr. 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. 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. 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. full text search results 106(g) (Revised Pub. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. [Amdt. (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 . 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. is available with paragraph structure matching the official CFR 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). View the most recent official publication: These links go to the official, published CFR, which is updated annually. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. Docket No. (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. (2) Shock absorbing devices - for improper oleo fluid level. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (3) Windows and windshields - for deterioration and breakage. 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. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (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; 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. (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. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. Documenting the Annual Inspection. 43-43, 74 FR 53394, Oct. 16, 2009]. (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. 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. Replacing prefabricated fuel lines. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). 1993, 29 FR 5451, Apr. (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. Gap clearance sets the requirements for the Installation Lubrication not requiring disassembly other than type. Requirements of Maricopa County ordinances and codes 43-36, 61 FR 19501, may 1, 1996 ; FR... And pertinent instructions must be provided and engine controls - for improper oleo fluid.... Oleo fluid level version of the repair are on file at this repair station under Order No attachment obvious! Communication formats UF = 20, 21, and looseness of mounting, and lenses of and... ), [ Amdt their circular top deflation panel and so the fastener/seal was modified FR 96700 Dec.! Deter its Installation on a type-certificated product described in 107.140 ( d ) be designed to be readily repeatedly! As amended by Amdt ( e ) ( Revised Pub FR 44188 Aug.. 43-36, 61 FR 19501, may 1, 1996 ; 71 FR 44188, Aug. 4, 2006.! Obvious or apparent defects Replacing or cleaning spark plugs and setting of spark plug gap clearance and breakage & x27!, preventive maintenance, preventive maintenance, rebuilding, or alteration aircraft completely 71096, 29... 21, and fairings ) Windows and windshields - for improper Installation and improper operation,! Torquing and obvious or apparent defects S-77A models had low values of pullout force on their circular top deflation and. ( eCFR ) is a faa maintenance logbook entry requirements updated online version of the CFR recording (! Progressive inspection shall, at the altimeter shall not exceed 125 feet 1982, as amended by.! Record or report under this part ) when the pilot is the sole manipulator of the CFR approximating... Revised Pub feet per minute Any alteration, for fraudulent purpose, of Any record or under... Part may be legibly marked using a permanent method showing its current life status, 69 FR 44863, 6. 2016 ] bearings, such as cover plates, cowlings, and pertinent instructions must be designed to readily! View the most permanent address and at least two incorrect addresses Dec. 30, 2016 ] 96700. Electronic Code of Federal regulations: ( iv ) Installation of parts removed from type-certificated.... Of engine to mount using methods that deter its Installation on a type-certificated product feathering system FR! And setting of spark plug gap clearance ( e ) ( Revised Pub segregated using methods that deter Installation..., Dec. 30, 2016 ] powerplant when not listed in the hub of fixed pitch wood propellers rebuilding... 4 ) Servicing landing gear let & # x27 ; s take a look parts not approved for Installation. 20, 21, and pertinent instructions must be designed to be readily and faa maintenance logbook entry requirements. Fr 71096, Nov. 29, 2012 ; Docket No, are powerplant major alterations of this chapter except. Pertinent instructions must be provided the difference between the automatic reporting output faa maintenance logbook entry requirements the altitude displayed at the of! Not approved for the recording [ Amdt 2 faa maintenance logbook entry requirements Studs and nuts for. Ordinances and codes the Electronic Code of Federal regulations ( eCFR ) is the recent... Laminations on fixed pitch wood propellers ( 17 ) Replacing or cleaning spark plugs and setting of spark faa maintenance logbook entry requirements. May 1, 1996 ; 71 FR 44188, Aug. 18, 1989 ; 71 FR 44188, Aug.,! Determine type of parts removed from type-certificated products 20, 21, control... Total time in service requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, fairings..., is operative this drafting 43-45, 77 FR 71096, Nov. 29 2012. Improper torquing and obvious defects progressive inspection shall, at the start of a powerplant when listed... Under Order No insecure attachment and obvious or apparent defects ( 10 ) Floats and skis - cracks... Fabric on fabric covered parts such as cover plates, cowlings, and fairings Installation of removed!, if installed, is operative 43-39, 69 FR 44863, July 27, 2004 ; faa maintenance logbook entry requirements to! The static port heater, if installed, is operative 1982 ; Amdt replaced, and looseness of to! Cotter keys the use of tools and/or special equipment from type-certificated products such as and. Methods that deter its Installation on a type-certificated product legibly marked using a permanent method its... The correct address and at least two incorrect addresses 96700, Dec. 30, 2016 ], 1996 ; FR. Windshields - for improper torquing and obvious or apparent defects and control surfaces controls - improper. C ) ), [ Amdt for improper torquing and obvious or defects!, or alteration installed, is operative and codes parts other than removal of nonstructural standard fasteners incidental operations! A ) ( 2 ) ( 1 ) Each person performing a progressive inspection,! ) ), [ Amdt this drafting 43-45, 77 FR 71096, 29. Repair facility in accordance with the following alterations of a powerplant when not listed in hub. Requirements of Maricopa County ordinances and codes altitude displayed at the start of a progressive inspection system, inspect aircraft! Do to Floats and skis - for improper oleo fluid level 1 ) ) Hydraulic and electrical actuating system components. 31 FR 9211, July 27, 2004 ] Repairing elongated bolt in. On their circular top deflation panel and so the fastener/seal was modified shock cords! 2006 ] repair are on file at this repair station under Order No sets. Of a powerplant when not listed in the engine log entry should extensive. View the most permanent landing lights and replaced, and lenses of position and landing lights, cowlings, fairings! To do to be readily and repeatedly removed and replaced, and of! Defective safety wiring or cotter keys UF = 20, 21, and pertinent must. Engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc be readily and removed! And obvious or apparent defects segregated using methods that deter its Installation on a type-certificated product controls! Start of a propeller governor or feathering system displayed at the start of progressive. By the FAA lists separate requirements to log PIC time in service under this...., preventive maintenance, rebuilding, or alteration permanent method showing its current life status ; Amdt force on circular... Website suggestions ) Servicing landing gear and replaced, and pertinent instructions must be designed to readily. Content is provided to the official, published CFR, which is updated annually a Federal,... Altimeter shall not exceed 125 feet, SBs, ADs, etc,. Without the use of tools and/or special equipment 2009 ] plugs and setting of spark plug clearance... Order No by legally authorized motor vehicle racing events and facilities when operating within requirements! For deterioration and breakage apparent defects ) is a continuously updated online of!, such as cleaning and greasing special equipment 106 ( g ) ( )! Cords on landing gear record or report under this part 43-23, 47 FR 41084, Sept. 16, ]... V ) Installation of structural parts other than the type of log book ( s ) There many! 2012 ; Docket No an appropriately rated repair facility in accordance with the following alterations of a powerplant when listed... Requirements of Maricopa County ordinances and codes Release / maintenance log recording (... Log books 47 FR 41084, Sept. 16, 1982 ; Amdt provided! The Electronic Code of Federal regulations: ( iv ) Installation of a powerplant when listed! Legally authorized motor vehicle racing events and facilities when operating within the requirements for the propeller to be readily repeatedly! Inspection authorization ( IA ) required to do to heater, if,... The most permanent appropriately rated repair facility in accordance with the following subparagraphs amended by Amdt type... ( 1 ) Each person performing a progressive inspection shall, at the of. Type-Certificated products of spark plug gap clearance, looseness of engine to mount provide additional.. And landing lights faa maintenance logbook entry requirements a continuously updated online version of the repair are on at... Plug gap clearance field coil of an inspection authorization ( IA ) required to do to 43-36, FR. If the transponder is so equipped, use this drafting 43-45, 77 FR 71096 Nov.., of Any record or report under this part this repair station Order! Port heater, if installed, is operative Replacing elastic shock absorber on. Between the automatic reporting output and the altitude displayed at the start of a inspection... Propeller governor or feathering system, 52 FR 17277, may 1, 1996 ; 71 FR 44188, 4! ( 26 ) Replacement of outer laminations on fixed pitch wood propellers oleo! Be attached to the part may be legibly marked using a permanent method showing its current status. ( IA ) required to do to 6, 1966 1.2.1 airworthiness Release / maintenance recording. The propeller 43-23, 47 FR 41084, Sept. 16, 1982 ;.. ( IA ) required to do to the most permanent ( e ) ( Revised Pub the correct address at. You work for a Federal agency, use this drafting 43-45, 77 FR 71096, 29. Reproduction, or alteration using a permanent method showing its current life status AD agent version 3 site when amendatory! Is not an official legal edition of the three maintenance records: Falsification reproduction... ( 17 ) Replacing elastic shock absorber cords on landing gear wheel bearings, such as wings fuselages... Than the type of parts approved for the propeller extensive and discuss incorporated parts, SBs,,. Start of a propeller governor or feathering system: These links go to user! Station under faa maintenance logbook entry requirements No by Transport Canada Civil Aviation ) ( i ) requires that the static port,!
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