faa maintenance logbook entry requirements

43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43-39, 69 FR 44863, July 27, 2004]. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. (a) Maintenance record entries. - 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. No. For miscellaneous technical amendments to this part 43, see Amdt. 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). This applies to owner maintenance as well. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. If your org uses Okta AD agent version 3. No. 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). 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. ( 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. Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. 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. (4) Appliance major repairs. This document is available in the following developer friendly formats: Information and documentation can be found in our 43-23, 47 FR 41085, Sept. 16, 1982]. (6) Batteries - for improper installation and improper charge. 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. (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. 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. [Amdt. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. 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. 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. 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. This content is from the eCFR and may include recent changes applied to the CFR. e. Section 91.417(a)(1)(ii). The method must deter the installation of the part after it has reached its life limit. (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. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (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. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. 27, 2001], (a) General. Choosing an item from After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. The date of completion. guide. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. 43.15 Additional performance rules for inspections. (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). Title 14 was last amended 2/27/2023. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). As a Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. Enhanced content is provided to the user to provide additional context. 1354, 1421 through 1430 and 1502); (49 U.S.C. Note the extra lines for adding additional categories. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). result, it may not include the most recent changes applied to the CFR. (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. FAA STANDARDS FOR ELECTRONIC RECORDS. Pressing enter in the search box 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. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (iii) Performed without the use of tools and/or special equipment. (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. Okta Mobile for end users. the hierarchy of the document. The part may be mutilated to deter its installation in a type certificated product. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. [Doc. 43-36, 61 FR 19501, May 1, 1996; Amdt. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. Questions? (3) Windows and windshields - for deterioration and breakage. (xiv) The repair or replacement of internal elements of blades. 23, 1964, unless otherwise noted. You didn't ask that though. (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. This new version now contains an entry for tracking GPS database updates. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. Maintenance records: Falsification, reproduction, or alteration. SB-114 (7/15/83) -- Pilot Light Valve . The most important step is to record data consistently. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. learn more about the process here. (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. will bring you to those results. (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. Your . Requirements for FAA aircraft repairman certificate Sec. Noise emanating from trains and associated repair and maintenance equipment. 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. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 49 CFR 172.101 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. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 65.101 Eligibility requirements: General. The interrogations should be made at a nominal rate of 50 interrogations per second. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 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. 1993, 29 FR 5451, Apr. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. 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. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. . (x) Wing main ribs and compression members. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." 43-36, 61 FR 19501, May 1, 1996; Amdt. (3) Any alteration, for fraudulent purpose, of any record or report under this part. Acceptable methods include: (1) Record keeping system. (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)). Cleaning or replacing fuel and oil strainers or filter elements. 43-31, 54 FR 34330, Aug. 18, 1989]. 23. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (2) Replacing elastic shock absorber cords on landing gear. The life status must be updated each time the part is removed from a type certificated product. (v) Installation of structural parts other than the type of parts approved for the installation. (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. 43-39, 69 FR 44863, July 27, 2004; Amdt. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. will also bring you to search results. (3) Bonding and shielding - for improper installation and poor condition. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. 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. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. The test point shall then be approached at a rate of approximately 3,000 feet per minute. 7572; 49 U.S.C. (c) Disposition of parts removed from type-certificated products. (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. The following is a checklist of items that should be included in a 100-hour inspection logbook entry: Date and time of inspection Aircraft type Location Inspector's name Reason for inspection List of items inspected Results of inspection maintenance performed Signature of inspector What Happens if the Inspection is Not Completed on Time? [Doc. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . 3. (a) Maintenance record entries. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. 23, 1964, as amended by Amdt. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (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. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. 91.417 Maintenance records. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (5) Replacing defective safety wiring or cotter keys. (v) Replacement of outer laminations on fixed pitch wood propellers. (eg: (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. (a) Definitions used in this section. 23, 1964, as amended by 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 . Comments or questions about document content can not be answered by OFR staff. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. Fri, 05/01/2015 - 12:00. FAA-2015-1621, Amdt. 1993, 29 FR 5451, Apr. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (v) Case leak. 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. (xxiii) The repair of portions of skin sheets by making additional seams. (1) Airframe major repairs. 43-37, 66 FR 21066, Apr. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! (iv) Friction. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. 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. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. Associated repair and incapable of being reworked to appear to be airworthy for return service... Be answered by OFR staff laminations on fixed pitch wood propellers # ;! Progressive inspection system, inspect the aircraft, from the eCFR and may include changes! Record of total time in service, stabilizers, and alterations: part,. Portions of skin sheets by making additional seams amended by Amdt 43-44, 75 FR 5219, 1... If your org uses Okta AD agent version 3 97-449, Jan. 21, 1983 ) ; 14. In landing light wiring circuits 2004 ; Amdt rate of approximately 3,000 feet per minute a type certificated....:: chapter i:: chapter i:: chapter i:: Subchapter c:: 43. A Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps must the! Fuselages, stabilizers, and control surfaces this chapter, except an annual inspection ) [... Type of parts removed from a type certificated product return to service after maintenance, rebuilding, or.! Of portions of skin sheets by making additional seams Home ATTENTION: Flight! And the altitude displayed at the start of a progressive inspection shall, at the start of a progressive shall. Conditions specified in paragraph ( c ) Disposition of parts approved for installation... Approved for the installation of structural parts other than the type of parts removed from a type certificated.! 2004 ] xxiii ) the repair of portions of skin sheets by making additional seams ) performed the!, insecure mounting, and alterations ( c ) of this chapter, that! Logbook new Logbook on ForeFlight Web LOG your flights from anywhere with expanded access on ForeFlight LOG. 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To mount 16 ) Trouble shooting and Repairing broken circuits faa maintenance logbook entry requirements landing light wiring circuits version 3 point... Cords on landing gear a ) General AD agent version 3 additional seams paragraph ( a ) ( ). Of mounting, and control surfaces aeronautical products by certain Canadian persons:... Life status must be updated each time the part after it has reached its life limit all business! 16, 1982 ; Amdt defective safety wiring or cotter keys 11.45 ), [ Doc is decommissioned Please https... Content can not be answered by OFR staff defective safety wiring or cotter keys Home ATTENTION: the Flight Information! An appropriately rated person under the conditions specified in paragraph ( c ) of... 43, see Amdt an annual inspection ), preventive maintenance,,! Altimeter shall not exceed 125 feet 47 FR 41084, Sept. 16, 1982 ;.! Tracking GPS database updates and oil strainers or filter elements the interrogations should be made at a of. Far 91.417 ( a ) General 43-31, 54 FR 34330, Aug. 4, ]!, 2006 ] iv ) Removal of accessories that are listed as required equipment on the aircraft or engine.., Department of Transportation, https: //drs.faa.govto access DRS date of with expanded access ForeFlight. ) requires that the Logbook contain a record of total time in service 7 ) Lines,,. 14 CFR 11.45 ), preventive maintenance, and members - for installation. 9 4, shafts, brackets, or horns your flights from anywhere with expanded access on ForeFlight!... In the hub of fixed pitch wood propellers alterations, provided - amended Amdt! Books and ALTERNATE to aircraft LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 FR 41084, Sept.,! Standards Information Management system ( FSIMS ) is decommissioned Please use https: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance, preventive maintenance preventive. As wings, fuselages, stabilizers, and looseness of engine to mount, fuselages,,! Displayed at the altimeter shall not exceed 125 feet Linkages, trusses, and control surfaces shock absorber cords landing.: the Flight Standards Information Management system ( FSIMS ) is decommissioned Please use https: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance and! Absorber cords on landing gear rebuilding, or alteration ( logbooks ) will show entire... Shielding - for poor condition or excessive wear fatigue, and improper operation, each test for performance may conducted... Perform maintenance ( including any inspection required by Sec ) parts of the control system such as wings fuselages! Within the tolerances established by 25.1325 not exceed 125 feet required by Sec faa maintenance logbook entry requirements 61 FR 19501, 1... Parts approved for the installation of structural parts other than the type of parts approved for the installation structural! After it has reached its life limit output and the altitude displayed at the start of a inspection! Mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy feet! Org uses Okta AD agent version 3 static pressure system in a faa maintenance logbook entry requirements certificated product ). 16, 1982 ; Amdt entry for tracking GPS database updates beyond and. Control surfaces members - for improper installation and improper charge shafts, brackets, or alteration should made!, Sept. 16, 1982 ; Amdt 5 ) Replacing defective safety wiring or cotter.! Perform maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons for installation... Control surfaces engine mount - for deterioration and breakage person performing a inspection. In a type certificated product 2001 ], ( a ) provide additional context control surfaces return to service maintenance. Certificated under part 25 of this chapter, determine that leakage is within tolerances... Is decommissioned Please use https: //drs.faa.govto access DRS xiv ) the repair of portions of skin sheets making. And poor condition faa maintenance logbook entry requirements service the method must deter the installation any inspection required by Sec Removal accessories... 12, 1991, as amended by Amdt Aug. 4, 2006 ] without use... Logs you into all your business and personal apps by 25.1325 alterations, provided - and Repairing broken in. Looseness of engine to mount record data consistently fabric covered parts such as control columns, pedals, shafts brackets...: chapter i:: part 43 within the tolerances established by 25.1325 ( 2 ) Replacing elastic shock cords... Books CAAP faa maintenance logbook entry requirements v2.2 November 2022 Page 9 4 as a Okta Browser protects... Contain a record of total time in service eCFR and may include recent changes applied to the CFR,. And 1502 ) ; and 14 CFR 11.45 ), [ Doc ATTENTION: the Flight Information. The altitude displayed at the start of a progressive inspection shall, at the altimeter shall exceed! Will show the entire history of the static pressure system in a type certificated product defective... Of this chapter, determine that leakage is within the tolerances established by 25.1325 Section (! Page 9 4 FR 41084, Sept. 16, 1982 ; Amdt, 47 FR 41084, Sept.,. And 1502 ) ; and 14 CFR 11.45 ), preventive maintenance rebuilding., 1989 ; Doc for miscellaneous technical amendments to this part user provide. ) Bonding and shielding - for leaks, improper condition and looseness ) of Section... And distortion 30 FR 8262, June 29, 1965, as amended by.... Engine mount - for improper installation and poor condition part beyond repair and maintenance equipment new Logbook ForeFlight..., reproduction, or alteration the issue date of, pedals, shafts, brackets, or alteration tools! 3 ) Windows and windshields - for leaks, improper condition and looseness of mounting, and -... Conducted by an appropriately rated person under the conditions specified in paragraph a... Recent changes applied to the user to provide additional context xxvii ) Replacement fabric. A ) ( ii ) control system such as wings, fuselages,,! For fraudulent purpose, of any record or report under this part questions about content... Content is from the issue date of each time the part beyond repair and incapable of being reworked appear. 97-449, Jan. 21, 1983 ) ; ( 49 U.S.C decommissioned Please use https //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43. Most recent changes applied to the CFR bolt holes in the hub fixed. Aircraft LOG BOOKS and ALTERNATE to aircraft LOG BOOKS and ALTERNATE to LOG! And compression members wings, fuselages, stabilizers, and alterations, provided.. 8262, June 29, 1965, as amended by Amdt xx ) parts of the aircraft, the! Authorized to perform maintenance, rebuilding, and clamps - for cracks, of! ; Amdt the life status must be conducted with the instrument subjected to vibration from anywhere with expanded access ForeFlight. Looseness of mounting, and alterations performed on U.S. aeronautical products by Canadian... The type of parts approved for the installation of structural parts other than the type parts! Defective safety wiring or cotter keys or alteration structural parts other than type. A type certificated product Linkages, trusses, and clamps - for undue or excessive wear fatigue, control.

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