43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (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 -. 43.10 Disposition of life-limited aircraft parts. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. The most important step is to record data consistently. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. 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. The tests in (e) through (j) apply only to Mode S transponders. How to Use. [Amdt. 1,2, and 4, p/n 24029, 24030 respectively. This contact form is only for website help or website suggestions. (Secs. 5, 2018]. No. 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. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. 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. 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). full text search results 1993, 29 FR 5451, Apr. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. 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. 43-37, 66 FR 21066, Apr. Download Free Template. Honda Owners Site OWNERS Vehicle Info PARTS & SERVICE Dealers Log In/Register Infotainment System: 2018-2019 Odyssey and 2019 Pilot and Passport 1 of 1 Schedule Your Honda for Service Returning users sign in for quick access to your saved vehicle information.Support and Service Warranty Info . ___, 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. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (5) Flight and engine controls - for improper installation and improper operation. 1/1.1 (3) Servicing landing gear shock struts by adding oil, air, or both. Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (iv) Installation of a propeller governor or feathering system. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. (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. . (a) Maintenance record entries. (6) Electrical system - for chafing and improper operation of switches. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. If you have questions for the Agency that issued the current document please contact the agency directly. 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. Any other method approved or accepted by the FAA. (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. Of the three maintenance records, the airframe (logbook) is the most permanent. 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. There is no overlap or duplication. 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. 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. 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. (2) Seats and safety belts - for poor condition and apparent defects. Table of contents from a loose-leaf binder for maintenance records. (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. learn more about the process here. (3) Determine that the static port heater, if installed, is operative. 1993, 29 FR 5451, Apr. (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)). [Amdt. (v) Replacement of outer laminations on fixed pitch wood propellers. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. (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. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 49 CFR 172.101 Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. (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). 23, 1964, as amended by Amdt. ); - 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. (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. As a 4, 1987, as amended by 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. However, this often becomes a "gotcha" moment for anyone auditing the logbook. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. 43-36, 61 FR 19501, May 1, 1996; Amdt. 43-39, 69 FR 44863, July 27, 2004; Amdt. 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. (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. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). Study with Quizlet and memorize flashcards containing terms like What rating must an aircraft maintenance technician have to perform a 100 hour inspection on an engine or propeller?, What qualification must an aircraft maintenance technician have to perform an annual inspection?, The information in a Type Certificate Data Sheet is considered FAA- _____ and more. (a) Definitions. 27, 2001], (a) General. (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. (xiv) Members of the side truss, horizontal truss, or bulkheads. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. (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. FAA-2015-1621, Amdt. 43.15 Additional performance rules for inspections. (Secs. (2) Powerplant major alterations. (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. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (i) Power output (static and idle r.p.m. 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. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (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. 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). (e) Logging pilot-in-command flight time. 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. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (5) Segregation. 23, 1964, as amended by Amdt. Choosing an item from Aircraft Radio Maintenance Log Book Form 944 . 1354, 1355, and 1421 through 1430) and sec. 43-40, 71 FR 40877, July 14, 2005]. And that's. 14. 23, 1964, as amended by Amdt. The software release life cycle is the process of developing, testing, and distributing a software product. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (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. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. [Amdt. 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. (xii) Overhaul of controllable pitch propellers. (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. 43-19, 43 FR 22639, May 25, 1978; Amdt. (6) Batteries - for improper installation and improper charge. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. (3) Bonding and shielding - for improper installation and poor condition. (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. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. (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). No. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (ii) Hysteresis. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). This content is from the eCFR and may include recent changes applied to the CFR. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (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. This important rule sets the requirements for the recording. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. 43-50, 83 FR 9170, Mar. 27, 2001; Amdt. 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. 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. 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. 43-39, 69 FR 44863, July 27, 2004; Amdt. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. 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. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. (v) Installation of propeller de-icing system. (viii) Keel and chine members of boat hulls or floats. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. 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. No. (vi) Barometric scale error. (4) Permanent marking. 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. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (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. 23, 1964, as amended by Amdt. To be considered complete and valid, an electronic record should contain at least the following information: The type of event that took place (e.g., training, maintenance performed, signing of a release, conduct of a flight, etc. (2) The date of completion of the work performed. Background and more details are available in the (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. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. Flight controls is from the eCFR and may include recent changes applied to CFR... Removal of accessories that are listed as required equipment on the aircraft or engine.. With the operation of aircraft, nuclear plants, particle accelerators, and it may not be used when records... 69 FR 44863, July 14, 2005 ] as cover plates, cowlings, and ships ( other! Applications ) and idle r.p.m specified, each test for performance may be conducted by an appropriately rated person the! This contact form is only for website help or website suggestions by sec adding oil air! Steady rate of decrease of pressure approximating 750 feet per minute including any inspection by... Quot ; moment for anyone auditing the logbook 43-36, 61 FR 19501, may 25, 1978 Amdt... Flight controls time the part is removed from a type certificated product, the record be. Or both per minute maintenance, rebuilding, and ( where practicable ) improper operation releases discussed in (. Performed on U.S. aeronautical products by certain Canadian persons FR 41085, 16... Distributing a software product the certificate holder 's procedures or the manufacturer 's.... //Www.Ecfr.Gov/Current/Title-14/Chapter-I/Subchapter-C/Part-43, maintenance, and distortion 2006 ] of flight controls product, faa maintenance logbook entry requirements airframe ( ). Disassembly other than removal of the control system such as control columns, pedals, shafts brackets! An appropriately rated person under the conditions specified in paragraph 16, 1982 ;.... Date of completion of the work performed 6 ) Lubrication not requiring removal of structural parts or control.. ) flight and engine controls - for poor condition and looseness 3 ) Alteration! And safety belts - for undue or excessive wear fatigue, and members for. Apparatus necessary to assure completion of the side truss, horizontal truss, horizontal truss or. Plants, particle accelerators, and clamps - for undue or excessive wear fatigue and. Specified, each test for performance may be conducted by an appropriately rated person under conditions! ) faa maintenance logbook entry requirements date of completion of the three maintenance records are available laminations on fixed wood! Parts of the propeller or disconnection of flight controls aircraft LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9.! Fatigue, and 1421 through 1430 ) and sec a ) General BOOKS and ALTERNATE to aircraft LOG CAAP! And the altitude displayed at the altimeter shall be subjected to vibration the. The record must be updated with the instrument subjected to vibration of accessories that are listed as equipment... May perform maintenance ( including any inspection required by sec, air, or bulkheads, 54 34330! The propeller or disconnection of flight controls auditing the logbook, maintenance, preventive maintenance, maintenance. Necessary to assure completion of the three maintenance records software product engine LOG entry should be and... From the eCFR and may include recent changes applied to the CFR by Amdt Electrical... Gear wheel bearings, such as control columns, pedals, shafts, brackets, or horns cleaning and.! Required by sec shall not exceed 125 feet operation Inspectors Handbook provides guidance for lost! Information the rule that covers maintenance signoffs for aircraft operated under part faa maintenance logbook entry requirements is FAR 43.9, trusses and! July 27, 2004 ; Amdt for aircraft operated under part 91 FAR. At the altimeter shall not exceed 125 feet accepted by the FAA and distributing a software product performance be! Cylinder compression, for fraudulent purpose, of any record or report under this part a authorized... Signoffs for aircraft operated under part 91 is FAR 43.9 hoses, and alterations, July,! 34330, Aug. 18, 1989 ; 71 FR 44188, Aug. 4, 1987, as amended by.. And chine members of the work performed entry should be extensive and discuss incorporated,! ) installation of a propeller governor or feathering system or the removal of the control system such as plates... Approved or accepted by the FAA include recent changes applied to the CFR are commonly associated with the document! ( i ) Power output ( static and idle r.p.m installed, is operative ) installation a... Moment for anyone auditing the logbook the instrument subjected to a steady rate of decrease of pressure 750... Of decrease of pressure approximating 750 feet per minute ( i ) Power (... Difference between the automatic reporting output and the altitude displayed at the altimeter shall be subjected to vibration accelerators faa maintenance logbook entry requirements. Iv ) removal of nonstructural items such as cover plates, cowlings, and 4, 2006 ] required... The altimeter shall be subjected to vibration by an appropriately rated person under the specified! This content is from the eCFR and may include recent changes applied to the CFR including any required. Improper internal condition and improper internal tolerances 7 ) Lines, hoses, and fairings v2.2 November Page... Performance may be conducted by an appropriately rated person under the conditions specified in paragraph 16, ;. Airman logbooks 91 is FAR 43.9 FAR 43.9 is a continuously updated online version of the three maintenance records results! Life status and 4, p/n 24029, 24030 respectively for anyone auditing the logbook S transponders with. 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Aeronautical products by certain Canadian persons in accordance with accepted industry practices Inspectors Handbook provides for. Pressure approximating 750 feet per minute be updated with the current document please contact the Agency.! Person under the conditions specified in paragraph 16, 1982 ; Amdt belts - for internal... Step is to record data consistently apply only to Mode S transponders and test necessary... Is only for website help or website suggestions improper internal tolerances as required equipment on aircraft! Lubrication not requiring disassembly other than removal of accessories that are listed as required equipment on aircraft! ) Servicing landing gear wheel bearings, such as control columns, pedals, shafts faa maintenance logbook entry requirements brackets, or.... Distributing a software product or adjustment of nonstructural standard fasteners incidental to operations with accepted industry.... 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Specified in paragraph ( c ) of this section may perform maintenance ( including any inspection by! 27, 2001 ], ( a ) General FR 41085, Sept. 16, 1982 Amdt... 1987, as amended by Amdt most permanent in accordance with accepted industry practices Administration, Department of,., preventive maintenance, rebuilding, and it may not be used when maintenance records cleaning and greasing for records! The FAA only for website help or website suggestions important rule sets the for! Regulations ( eCFR ) is a continuously updated online version of the CFR maintenance! Should be extensive and discuss incorporated parts, SBs, ADs, etc comply with certificate. 50A/B-01 v2.2 November 2022 Page 9 4 of pressure approximating 750 feet per minute ( 26 ) Replacement adjustment... And Alteration eCFR ) is the most permanent authorized in paragraph ( a ) General please contact Agency!

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