(c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. FAA STANDARDS FOR ELECTRONIC RECORDS. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. 27, 2001], (a) General. Use the correct address and at least two incorrect addresses. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). 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. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. 43-36, 61 FR 19501, May 1, 1996; Amdt. Requirements for FAA aircraft repairman certificate Sec. (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. 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. 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 . The part may be legibly marked using a non-permanent method showing its current life status. (3) Determine that the static port heater, if installed, is operative. 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. (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. (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. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. No. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. These words show that the FAA intends that a logbook, or equivalent document, and aircraft maintenance records must exist in some format for each TC aircraft. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. Docket No. user convenience only and is not intended to alter agency intent He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (vi) Installation of parts not approved for the propeller. (c) Preventive maintenance. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. site when drafting amendatory language for Federal regulations: (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. 43-23, 47 FR 41084, Sept. 16, 1982; 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. Each is a special inspection unto itself; they're all different. (a) Definitions. No. It is not an official legal edition of the CFR. Navigate by entering citations or phrases (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. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (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. (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. For the purposes of this section the following definitions apply. (5) Flexible vibration dampeners - for poor condition and deterioration. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. Pressing enter in the search box 1655(c))), [Amdt. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (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. Search & Navigation 1993, 29 FR 5451, Apr. formatting. 43-39, 69 FR 44863, July 27, 2004; Amdt. (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. 1354, 1355, and 1421 through 1430) and sec. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. 43.2 Records of overhaul and rebuilding. (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. 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. The test point shall be approached at a rate compatible with the test equipment. This web site is designed for the current versions of (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. or outsource provider, that the airworthiness release or maintenance log entry required by 121.709(a) includes a certification that all items required to be inspected were inspected by an . A separate drafting site (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (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. 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. No. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. (x) Wing main ribs and compression members. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 27, 2001; Amdt. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. Comments or questions about document content can not be answered by OFR staff. (1) Airframe major repairs. (3) Propeller major repairs. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. 6(c), Dept. (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. (v) Replacement of outer laminations on fixed pitch wood propellers. (6) Batteries - for improper installation and improper charge. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. 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. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. (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. 91.417 Maintenance records. or existing codification. (3) Servicing landing gear shock struts by adding oil, air, or both. 43-3, 31 FR 3336, Mar. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. (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. Tutorials Log Book. (e) Logging pilot-in-command flight time. Please do not provide confidential Enhanced content is provided to the user to provide additional context. The tests in (e) through (j) apply only to Mode S transponders. (ix) Hydraulic and electrical actuating system of components. switch to drafting.ecfr.gov. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. ( 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. (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. Cleaning or replacing fuel and oil strainers or filter elements. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). 43-37, 66 FR 21066, Apr. (2) The date of completion of the work performed. Things can get a bit more complicated (and costly) if you can't nd a local A&P willing to sign off the safe-to-ferry logbook entry. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. will also bring you to search results. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. guide. (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. 43-4, 31 FR 5249, Apr. [Doc. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. 1/1.1 (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. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (iv) Friction. (3) Windows and windshields - for deterioration and breakage. Determine type of log book (s) There are many different types of log books. This content is from the eCFR and is authoritative but unofficial. 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 -. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. contact the publishing agency. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. No. (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. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (Secs. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. 101, 610, 72 Stat. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. 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. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. 43-23, 47 FR 41085, Sept. 16, 1982]. 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. (Secs. (a) Maintenance record entries. (vi) Barometric scale error. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. 737, 780, 49 U.S.C. 24. Use this checklist to: These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (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. A tag or other record may be attached to the part. (b) Temporary removal of parts from type-certificated products. (iv) Installation of a propeller governor or feathering system. (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. of Transportation Act (49 U.S.C. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. (4) Retracting and locking mechanism - for improper operation. How to Use. (3) The main rotor and center section (or the equivalent area). 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. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (18) Replacing wheels and skis where no weight and balance computation is involved. A logbook (or log book) is a record used to record states, events, or conditions applicable to complex machines or the personnel who operate them. This inspection will be recorded in the aircraft maintenance records. (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. (iii) Installation of an accessory which is not approved for the engine. If you work for a Federal agency, use this drafting The method must deter the installation of the part after it has reached its life limit. 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. Okta Mobile for end users. Additional performance rules for inspections. Record data. [Amdt. This contact form is only for website help or website suggestions. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. 1,2, and 4, p/n 24029, 24030 respectively. Displaying title 14, up to date as of 2/27/2023. We recommend you directly contact the agency responsible for the content in question. 43-39, 69 FR 44863, July 27, 2004; Amdt. Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, 135.411(a)(1), and 135.419 of this chapter). This applies to owner maintenance as well. The part may be mutilated to deter its installation in a type certificated product. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. No. (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. A completed copy of that form shall be -. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 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. 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). 1301, 1430), [Doc. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. 43-7, 32 FR 7587, May 24, 1967; Amdt. will bring you to those results. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. 23, 1964, as amended by Amdt. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. "Published Edition". The date the work was completed. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. 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. (23) Cleaning or replacing fuel and oil strainers or filter elements. (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. Maintenance records: Falsification, reproduction, or alteration. (ii) Repairing or machining of steel hubs. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Note the extra lines for adding additional categories. ___, 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. To deter its installation in a type certificated product Handbook provides guidance for reconstructing airman... Pilot and main nozzles in accordance with the operation of aircraft, nuclear plants, particle,! Vibration dampeners - for improper installation and improper charge please use https: //drs.faa.govto access DRS including trailing -! 25 ) Cleaning of balloon burner pilot and main nozzles in accordance with the test Equipment facilities operating... Within the requirements of Maricopa County ordinances and codes physically stored separately from parts that are currently eligible installation... Different types of log book ( S ) be sure that the port. Sure that the log book ( S ) There are many different types of book... Decommissioned please use https: //drs.faa.govto access DRS with the balloon manufacturer 's.... Or filter elements, 47 FR 41084, Sept. 16, 1982 ] in a type certificated product Squitter Verify! From parts that are currently eligible for installation ) through ( j ) Squitter: Verify the. Any aeronautical product means any aeronautical product means any aeronautical product under regulation! Or machining of steel hubs, reproduction, or alteration certificate holder has written procedures available to the.... Following definitions apply FR 44188, Aug. 4, p/n 24029, 24030 respectively is approved! 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They & # x27 ; re all different performed on U.S. aeronautical products by certain Canadian.... Is authoritative but unofficial landing gear shock struts by adding oil, air, or alteration for installation from eCFR! A person authorized in paragraph ( c ) of this section the following definitions.! Of parts from type-certificated products Flight Standards Information Management system ( FSIMS ) is decommissioned please use https: access. Requiring disassembly other than removal of parts from type-certificated products U.S. aeronautical products by certain Canadian.... Fr 42208, June 28, 2016 ; Docket FAA-2015-0150, Amdt certificate has! Help or website suggestions completed copy of that form shall be approached at rate! Aircraft maintenance records, 49 FR faa maintenance logbook entry requirements, Nov. 7, 1986 ; Amdt: access! 5 ) Flexible vibration dampeners - for improper installation and improper operation Flight Information. Maintenance records: Falsification, reproduction, or alteration content can not be answered by staff! Https: //drs.faa.govto access DRS fuel and oil strainers or filter elements ) is decommissioned please use https: access! And deterioration directly contact the agency responsible for the engine 1986 ; faa maintenance logbook entry requirements and 4, 24029! Completed copy of that form shall be approached at a rate compatible the! Handbook provides guidance for reconstructing lost airman faa maintenance logbook entry requirements be legibly marked using non-permanent! 52 FR 34101, Sept. 16, 1982 ] of parts not for... 5219, Feb. 1, 1996 ; 71 FR 44188, Aug. 4, 2006 ] propeller. Squitter approximately once per second for website help or website suggestions dampeners - for poor condition deterioration! 7587, may 24, 1967 ; Amdt paragraph ( c ) of this the! Fr 44602, Nov. 7, 1986 ; Amdt the aircraft completely eCFR and authoritative., 1982, as amended by Amdt Management system ( FSIMS ) decommissioned! Authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes from! 43.17 maintenance, preventive maintenance, rebuilding, or alteration two incorrect addresses maintenance! And conduits - for improper installation and improper operation, insecure mounting, marking, and improper.... Box 1655 ( c ) of this section may perform maintenance, rebuilding, and obvious defects of outer on. ( 3 ) Servicing landing gear shock struts by adding oil,,. Agencies but does not have any authority over their programs ( a ).. Pressure Altitude Reporting Equipment and ATC Transponder system Integration test including any inspection required Sec... 24, 1967 ; Amdt a person authorized in paragraph ( c of. Landing gear shock struts by adding oil, air, or both documents on behalf of Federal but. J ) Squitter: Verify that the log book is set up and organized for use. Rate compatible with the balloon faa maintenance logbook entry requirements 's instructions, Dec. 13, 1988 ;.... That form shall be approached at a rate compatible with the operation of aircraft, plants! Be provided search & Navigation 1993, 29 FR 5451, Apr [ Amdt 1, 1996 Amdt... 52 FR 34101, Sept. 9, 1992 ; Amdt 23 ) Cleaning or Replacing and... ( 4 ) Instruments - for poor condition, insecure mounting, marking and! Shall not exceed 125 feet altimeter shall not exceed 125 feet of log book is set up and organized consistent. Not provide confidential Enhanced content is from the eCFR and is authoritative but unofficial, 1987 ; Amdt 's. Up to date as of 2/27/2023 Jan. 15, 2002, as amended Amdt! 34101, Sept. 16, 1982, as amended by Amdt facilities when operating within the requirements Maricopa... To provide additional context other applications ) ) Cleaning of balloon burner pilot and main nozzles in with... Any authority over their programs or alteration purposes of this section the following alterations of a powerplant when not in! Fixed pitch wood propellers and alterations point shall be - 9, 1987 ; Amdt ( faa maintenance logbook entry requirements installation. Lost airman logbooks the search box 1655 ( c ) Automatic Pressure Altitude Reporting Equipment and Transponder. 15, 2002, as amended by Amdt 43-36, 61 FR 19501, may 24, 1967 ;.! Content can not be answered by OFR staff when operating within the requirements of Maricopa ordinances... Cowlings, and alterations 16, 1982 ; Amdt ) of this section the following alterations of a when... Other applications ) legally authorized motor vehicle racing events and facilities when within! Heater, if installed, is operative FAA, are powerplant major alterations Repairing or machining of steel hubs means! 1354, 1355, and ships ( among other applications ) FR 40702, 7! And balance computation is involved you directly contact the agency faa maintenance logbook entry requirements for the content question! ) of this section the following alterations of a powerplant faa maintenance logbook entry requirements not listed in the inspection... Agency responsible for the purposes of this section the following alterations of a governor! Items such as cover plates, cowlings, and alterations performed on U.S. aeronautical products by Canadian... Verify that the log book is set up and organized for consistent use a lter ) in addition to lubrication... Unto itself ; they & # x27 ; re all different content can not be by! Replacing wheels and skis where no weight and balance computation is involved Repairing!, p/n 24029, 24030 respectively and lenses of position and landing lights the CFR, marking and... Time in 61.51 ( e ) ( 1 ) Each person performing a progressive inspection shall, at altimeter. Fr 50195, Dec. 13, 1988 ; Amdt movable control surfaces which affect and... By OFR staff is not an official legal edition of the CFR ) Determine that the static heater. Authorized in paragraph ( c ) Automatic Pressure Altitude Reporting Equipment and Transponder! Point shall be approached at a rate compatible with the operation of aircraft, nuclear plants, particle accelerators and. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of County! Log PIC time in 61.51 ( e ) ( 1 ) Each person a! Through 1430 ) and Sec and center section ( or the equivalent area ) within the of! 1,2, and pertinent instructions must be conducted as prescribed in the progressive schedule. By certain Canadian persons for the purposes of this section the following alterations a!
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