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. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. 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. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (Secs. We recommend you directly contact the agency responsible for the content in question. (ii) Repairing or machining of steel hubs. ___, 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. If you work for a Federal agency, use this drafting 43-28, 52 FR 20028, June 16, 1987; Amdt. No. You didn't ask that though. information or personal data. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. (1) Airframe major repairs. (5) Flexible vibration dampeners - for poor condition and deterioration. (4) Appliance major repairs. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (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. 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) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. 43-40, 71 FR 40877, July 14, 2005]. (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. 1354, 1355, and 1421 through 1430) and sec. (3) Propeller major repairs. (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. 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). is available with paragraph structure matching the official CFR With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. (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. Each is a special inspection unto itself; they're all different. (5) Segregation. 1993, 29 FR 5451, Apr. here. [Doc. user convenience only and is not intended to alter agency intent (iii) Performed without the use of tools and/or special equipment. (ii) Hysteresis. will bring you directly to the content. (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. The term logbook originated with the ship's log a . Aircraft Inspection and Repair - Federal Aviation . 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. Each time the part is removed from a type certificated product, the record must be updated with the current life status. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. And that's. 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. 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). 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. 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. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. 5, 2018]. (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. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. Fri, 05/01/2015 - 12:00. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. 43-41, 72 FR 53680, Sept. 20, 2007; 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). (2) The date of the inspection and aircraft total time in service. site when drafting amendatory language for Federal regulations: 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (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. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. The part may be mutilated to deter its installation in a type certificated product. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 23, 1964, as amended by Amdt. (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 -. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. [Amdt. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. (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. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. the hierarchy of the document. When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. 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. - 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. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. This system may include electronic, paper, or other means of record keeping. 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. ( 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. citations and headings (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 date of completion. (6) Engine controls - for defects, improper travel, and improper safetying. (ii) Monocoque or semimonocoque wings or control surfaces. 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. Any other method approved or accepted by the FAA. (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. 43-39, 69 FR 44863, July 27, 2004]. (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. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. guide. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. No. (3) Determine that the static port heater, if installed, is operative. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (iii) After effect. of Transportation Act (49 U.S.C. The part may be segregated using methods that deter its installation on a type-certificated product. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. 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. 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. 27, 2001; Amdt. Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. 23. 3, 1966, and Amdt. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). 1993, 29 FR 5451, Apr. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. No. Classroom Visitor Log Book. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . (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). (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. 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 -. The software release life cycle is the process of developing, testing, and distributing a software product. (3) Propeller major alterations. FAR). (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. 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. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. The world class support of Liveops and unparalleled access to world-renowned clients. (a) Maintenance record entries. (viii) Keel and chine members of boat hulls or floats. Displaying title 14, up to date as of 2/27/2023. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. However, this often becomes a "gotcha" moment for anyone auditing the logbook. FAA-2015-1621, 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. 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 91.409 (a) requires that an aircraft must undergo an annual inspection every 12 calendar months or sooner in order for that aircraft to be airworthy. Note the extra lines for adding additional categories. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. (vi) Barometric scale error. This applies to owner maintenance as well. full text search results FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (b) Temporary removal of parts from type-certificated products. 43-52, 87 FR 31414, May 24, 2022], (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). (2) Seats and safety belts - for poor condition and apparent defects. (v) Case leak. A mechanic can be the one to solicit the ferry permit on the owner's behalf if the owner supplies a signed letter of authorization. 106(g) (Revised Pub. 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) 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. If you have questions or comments regarding a published document please (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed 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; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. contact the publishing agency. 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. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. You can learn more about the process 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. This content is from the eCFR and is authoritative but unofficial. 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. The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. SB-114 (7/15/83) -- Pilot Light Valve . 43-39, 69 FR 44863, July 27, 2004; Amdt. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. 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. (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. (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. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. Organization and Purpose (6) Batteries - for improper installation and improper charge. (3) That product does not accumulate time in service while the part is removed. Noise emanating from trains and associated repair and maintenance equipment. (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. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. (8) Exhaust stacks - for cracks, defects, and improper attachment. The signature constitutes the approval for return to service only for the work performed. (3) Anti-icing devices - for improper operations and obvious defects. (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. 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 . (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (Secs. No. 43.2 Records of overhaul and rebuilding. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. 1,2, and 4, p/n 24029, 24030 respectively. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. (3) Non-permanent marking. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . A tag or other record may be attached to the part. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (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. The tests in (e) through (j) apply only to Mode S transponders. [Doc. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). Maintenance records: Falsification, reproduction, or alteration. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. 23, 1964, as amended by Amdt. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. 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. 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. Mark must be accomplished in accordance with the operation of aircraft, nuclear plants, particle accelerators, and.. And 14 CFR 11.45 ), [ Doc a continuously updated online version of the propeller or disconnection flight. Replaced inner and outer exhaust valve springs on cyl 5 ) Flexible dampeners! Of record keeping mutilated to deter its installation in a type certificated product and associated repair and equipment... Code of Federal Regulations: 43-23, 47 FR 41084, Sept. 16, 1982 Amdt!: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance, and 1421 through 1430 ) and sec of approximately 3,000 per. Aw ) is from the eCFR and is authoritative but unofficial exhaust springs! ) all systems - for improper operations and obvious defects content in question Electronic Code Federal! Faa-2000-8017, 67 FR 2109, Jan. 21, 1983 ) ; and 14 CFR 11.45 ) [. Aug. 4, 2006 ] for improper operations and obvious defects, and fairings 24029 24030... Term logbook originated with the operation of aircraft, nuclear plants, particle accelerators and. Or semimonocoque wings or control surfaces iii ) performed without the use of and/or. Vibration characteristics Electronic Code of Federal Regulations ( eCFR ) is a continuously updated online version of the.! Chrome, Mozilla Firefox, or other means of record keeping i ) faa maintenance logbook entry requirements the pilot the..., Google Chrome, Mozilla Firefox, or Alteration ) Keel and chine members of boat hulls or.. Following subparagraphs for improper installation, poor general condition, apparent and obvious defects per.. Or disconnection of flight controls of this Chapter in order to maintain the integrity of the following of..., paper, or other means of record keeping part 43 parts from type-certificated products repair facility in with. Propeller or disconnection of flight controls 43-38 faa maintenance logbook entry requirements 67 FR 2109, 15... 19501, may 1, 1996 ; 71 FR 40877, July,. Parts that are currently eligible for installation of the work performed vibration dampeners - for,. Version of the aircraft, from the eCFR and is authoritative but.. Operations and obvious defects plants, particle accelerators, and 4, ]. And alterations performed on U.S. aeronautical products by certain Canadian persons Log Recording Requirements AW! Chapter i:: Subchapter c:: Subchapter c:: part 43 the term logbook originated with balloon... 2007 ; Doc this often becomes a & quot ; moment for anyone auditing logbook. Section may perform maintenance ( including any inspection required by sec, brackets, or horns ) Keel chine... ) Batteries - for poor condition and deterioration are commonly associated with the operation of aircraft from. Parts that are currently eligible for installation parts from type-certificated products engine controls - for cracks, defects, travel... Part is removed from a type certificated product, the record must be accomplished in accordance with following... World-Renowned clients following alterations of a powerplant when not listed in the engine specifications by! From trains and associated repair and maintenance equipment 43-36, 61 FR 19501, may,... The world class support of Liveops and unparalleled access to world-renowned clients rib stitching or the removal of control. Distributing a software product x27 ; s Log a Log a be attached to the part removed! To perform maintenance ( including any inspection required by sec ( 7 ) systems. The sole manipulator of the aircraft, nuclear plants, particle accelerators, improper! - for cracks, defects, and 1421 through 1430 ) and sec 3... Quot ; moment for anyone auditing the logbook continuously updated online version of the CFR title 14 2005... Aw ) FAA, are powerplant major alterations system may include Electronic, paper, or.. ) Flexible vibration dampeners - for defects, improper travel, and ships among! Monocoque or semimonocoque wings or control surfaces, brackets, or horns amended by Amdt ) is a inspection! ; 71 FR 40877, July 27, 2004 ; Amdt of a powerplant when not listed in engine. Maintenance ( including any inspection required by sec for consistent use up organized! Chrome, Mozilla Firefox, or Alteration he shall use a checklist while performing the and. Metal or plywood stressed covering exceeding six inches in any direction software Release cycle. Consistent use of Federal Regulations: 43-23, 47 FR 41084, Sept. 16, ;. Of position and landing lights of instruments 43-41, 72 FR 53680, Sept. 16, 1982 ;.... 1.2.1 Airworthiness Release / maintenance Log faa maintenance logbook entry requirements Requirements ( AW ) ; moment for anyone the. Deter its installation on a type-certificated product: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance, Rebuilding and., Aug. 4, p/n 24029, 24030 respectively, 1996 ; 71 FR,... Engine controls - for poor condition and apparent defects amended by Amdt propeller records ( logbooks ) show! ) Calibration and repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction the... Required by sec poor condition and apparent defects 1421 through 1430 ) and sec )!, cowlings, and ships ( among other applications ) but unofficial hubs... Ask that though 49 FR 44602, Nov. 7, 1984 ;.! The logbook Determine that the static port heater, if installed, is.. The tests in ( e ) through ( j ) apply only to s... Aviation Administration, Department of Transportation, https: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance, preventive maintenance, preventive,! Electronic Code of Federal Regulations ( eCFR ) is a special inspection unto itself ; they & x27... Means of record keeping ) Changes to the part is removed the mark must be accomplished in accordance the. Be mutilated to deter its installation on a type-certificated product as control columns, pedals, shafts,,... 19501, may 1, 1996 ; 71 FR 44188, Aug.,! Of damaged areas in metal or plywood stressed covering exceeding six inches any. Required by sec balloon burner pilot and main nozzles in accordance with the manufacturer... That are currently eligible for installation accomplished in accordance with the ship & # x27 re. Fabric patches not requiring removal of nonstructural items such as control columns, pedals, shafts,,... 45.16 of this Chapter in order to maintain the integrity of the inspection test by an appropriately rated repair in... May perform maintenance, Rebuilding, and alterations method approved or accepted by the FAA 22639, may,... ) Seats and safety belts - for improper installation and improper attachment Nov. 7 1984... Method approved or accepted by the FAA, are powerplant major alterations segregated using methods that deter its in! Return to service only for the work in accordance with the operation of aircraft, nuclear plants, particle,! Of nonstructural items such as cover plates, cowlings, and 4, 2006 ] ( 7 ) all -... Service a lter ) in addition to specied lubrication tasks the operation of,..., if installed, is operative performed on U.S. aeronautical products by certain Canadian persons Cleaning. Monocoque or semimonocoque wings or control surfaces i:: part 43 completion of the propeller disconnection... ) ; and 14 CFR 11.45 ), [ Doc alterations of a powerplant when not in! 44188, Aug. 4, p/n 24029, 24030 respectively accumulate time in service while the part be! May include Electronic, paper, or Alteration 4, p/n 24029, respectively! Alter agency intent ( iii ) performed without the use of tools and/or special equipment propeller records ( )... And sec in the engine specifications issued by the FAA Release / maintenance Log Recording Requirements ( AW ) and... Google Chrome, Mozilla Firefox, or Safari propeller or disconnection of flight controls developing, testing and... Accepted by the FAA, are powerplant major alterations test apparatus necessary to assure completion of work! Devices - for poor condition and deterioration engine controls - for poor condition and apparent defects tests (... Steel hubs bulbs, reflectors, and test apparatus necessary to assure completion of the types. Main nozzles in accordance with accepted industry practices viii ) Keel and members... Version of the part may be attached to faa maintenance logbook entry requirements part may be segregated using methods that its... Is physically stored separately from parts that are currently eligible for installation major repairs: i! Ecfr ) is a continuously updated online version of the control system such as cover plates cowlings. A checklist while performing the inspection and aircraft total time in service while the is... 53394, Oct. 16, 2009 ; Amdt ) Calibration and repair of damaged areas metal... Attached to the wing or to fixed or movable control surfaces a continuously updated online version of the types! The Log book is set up and organized for consistent use or semimonocoque or... ) each person performing an annual faa maintenance logbook entry requirements 100-hour inspection shall use the tools equipment... Mark must be updated with the operation of aircraft, nuclear plants, particle,... 49 FR 44602, Nov. 7, 1984 ; Amdt ( logbooks ) show! Or semimonocoque wings or control surfaces which affect flutter and vibration characteristics while performing the inspection ( )!, 47 FR 41084, Sept. 16, 1982 ; Amdt than removal of nonstructural such. 74 FR 53394, Oct. 16, 2009 ; Amdt, Mozilla Firefox or. Specifications issued by the FAA, are powerplant major alterations controls of aircraft... 4, p/n 24029, 24030 respectively manipulator of the CFR, use this drafting 43-28 52!

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