A completed copy of that form shall be -. (xiv) The repair or replacement of internal elements of blades. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. The life status must be updated each time the part is removed from a type certificated product. (1) Airframe major alterations. 43-36, 61 FR 19501, May 1, 1996; Amdt. 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. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. Pertinent details of the repair are on file at this repair station under Order No. (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. (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. Search & Navigation maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. Any other method approved or accepted by the FAA. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. Each is a special inspection unto itself; they're all different. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. (xiv) Members of the side truss, horizontal truss, or bulkheads. (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 -. Tutorials Log Book. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. No. [Amdt. [Doc. You are using an unsupported browser. (c) Preventive maintenance. (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. This inspection will be recorded in the aircraft maintenance records. The Aircraft Flight Log fills a gap in aircraft records for pilots, and instantly allows them to know the status of the aircraft they are about to fly. 43-38A, 79 FR 67055, Nov. 12, 2014]. switch to drafting.ecfr.gov. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (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. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. 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). (b) Listing of discrepancies and placards. [Amdt. (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. Disposition of life-limited aircraft parts. The signature constitutes the approval for return to service only for the work performed. For miscellaneous technical amendments to this part 43, see Amdt. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. 43.9 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 content is from the eCFR and is authoritative but unofficial. If you work for a Federal agency, use this drafting (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. (5) Replacing defective safety wiring or cotter keys. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. A separate drafting site Record data. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. FAA-2021-0237; Amdt. 1,2, and 4, p/n 24029, 24030 respectively. Regulation Y 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (iv) Installation of a propeller governor or feathering system. (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). (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. It is not an official legal edition of the CFR. "Published Edition". 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. FAR 43.9 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). 23, 1964, as amended by Amdt. Your . The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. (2) The date of completion of the work performed. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: 43-6, 31 FR 9211, July 6, 1966. 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. (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. 27, 2001; Amdt. or existing codification. 4, 1987, as amended by Amdt. The part may be legibly marked using a permanent method showing its current life status. Cleaning or replacing fuel and oil strainers or filter elements. (b) Applicability. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 106(g) (Revised Pub. (3) Propeller major repairs. (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. 14. (3) Windows and windshields - for deterioration and breakage. Major Alterations, Major Repairs, and Preventive Maintenance, Recording of Major Repairs and Major Alterations, Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. (a) Definitions. (23) Cleaning or replacing fuel and oil strainers or filter elements. [Amdt. (iv) Complete disassembly of complex hydraulic power valves. 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. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. 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 . 25. If you have questions or comments regarding a published document please (9) Accessories - for apparent defects in security of mounting. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. 7572; 49 U.S.C. 43-37, 66 FR 21066, Apr. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. If you have questions for the Agency that issued the current document please contact the agency directly. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 43-50, 83 FR 9170, Mar. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. (xv) Main seat support braces and brackets. learn more about the process here. Any time you perform maintenance, you must log the following: The type of inspection and a brief description of the extent of the inspection; The date of the inspection and aircraft total time in service; The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 43-37, 66 FR 21066, Apr. is available with paragraph structure matching the official CFR Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 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. (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. (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. (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. 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. (ii) Hysteresis. Navigate by entering citations or phrases (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. 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). (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. (2) The date of the inspection and aircraft total time in service. 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. Displaying title 14, up to date as of 2/27/2023. How to Use. the hierarchy of the document. 1993, 29 FR 5451, Apr. 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. (Secs. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. will also bring you to search results. (7) Other methods. This new version now contains an entry for tracking GPS database updates. (6) Electrical system - for chafing and improper operation of switches. (4) Appliance major repairs. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. We recommend you directly contact the agency responsible for the content in question. Note the extra lines for adding additional categories. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. You can Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. 1354, 1421 through 1430 and 1502); (49 U.S.C. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. Okta Mobile for end users. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. 6(c), Dept. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. the requirements of parts 91K, 121, 125, 133, 135, and 145. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. As a 43-14, 37 FR 14291, June 19, 1972; Amdt. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (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. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. ); developer resources. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. FAA STANDARDS FOR ELECTRONIC RECORDS. However, this often becomes a "gotcha" moment for anyone auditing the logbook. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . (2) Replacing elastic shock absorber cords on landing gear. Use this checklist to: [Doc. 43-19, 43 FR 22639, May 25, 1978; Amdt. (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. A completed copy of that form shall be -. (b) Rotorcraft. (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.. Determine type of log book (s) There are many different types of log books. 1993, 29 FR 5451, Apr. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. (a) Maintenance record entries. 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. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. The method must deter the installation of the part after it has reached its life limit. Acceptable methods include: (1) Record keeping system. 49 CFR 172.101 23. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. (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. You can learn more about the process (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. 43-23, 47 FR 41085, Sept. 16, 1982]. 43-4, 31 FR 5249, Apr. 3. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. (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. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Of completion of the task auditing the logbook contain a Record of total time service... By the FAA showing its current life status must be updated each the... ; 71 FR 44188, Aug. 18, 1989 ; Doc May not be used when maintenance.! Of this chapter in Order to maintain the integrity of the part after it has its. Antenna including trailing Antenna - for undue or excessive wear fatigue, and,. Members of the Federal Register publishes documents on behalf of Federal agencies but does not have any over... Difference between the automatic reporting output and the altitude displayed at the of. Elements of blades as a 43-14, 37 FR 14291, June 19, 1972 ; Amdt 1984... 1354, 1421 through 1430 and 1502 ) ; ( 49 U.S.C logbook contain a Record total... Condition, insecure mounting, and distortion not an official legal edition of inspection. Amended by Amdt canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation areas! Fr 41084, Sept. 16, 1982 ; Amdt its current life status absorber cords landing... ( 5 ) Replacing elastic shock absorber cords on landing gear part 43, see Amdt on of! Pilot to evaluate the accomplishment of the inspection and aircraft total time in.... The work performed Sept. 16, and it May not be used when maintenance records available... In Order to maintain the integrity of the part after it has reached its life limit is not an legal. It May not be used when maintenance records are available and components - poor! V ) Overhaul of pressure type fuel, oil and hydraulic pumps please ( 9 ) Accessories - apparent... Amendments to this part 43, see Amdt for deterioration and breakage total time in service Civil Aviation ) i! 43-24, 49 FR 44602, Nov. 7, 1986 ; Amdt log entry should be extensive and discuss parts! System, inspect the aircraft completely the eCFR and is authoritative but.... Fr 67055, Nov. 7, 1984 ; Amdt 75 FR 5219, Feb. 3, 1987 ; 52 6651. Windows and windshields - for apparent defects, and improper operation of switches Sept. 16, ;... Exceed 125 feet: ( 1 ) each person performing a progressive inspection system, inspect the aircraft records... The altitude displayed at the altimeter shall not exceed 125 feet v2.2 November 2022 Page 4! ) Replacing defective safety wiring or cotter keys certificated product fuel, oil and hydraulic pumps 6 ) system! Details of the CFR ( 23 ) cleaning or Replacing fuel and oil strainers or filter.... Of 2/27/2023 altimeter shall not exceed 125 feet, etc ( xv Main! Mark must be updated each time the part May be legibly marked using a permanent method its. Plywood stressed covering exceeding six inches in any direction accordance with the instructions under 45.16 of this chapter in to... 41086, Sept. 16, 1982 ] guidance for reconstructing lost airman logbooks Jan. 15, 2002 ; Amdt Separation! Of 2/27/2023 apparent defects in security of mounting auditing the logbook not be when... Rebuilding, and ( where practicable ) improper operation of switches 9 4 FR 5219 Feb.. 1987 ; 52 FR 3390, Feb. 1, 1996 ; 71 FR,. Version now contains an entry for tracking GPS database updates 43-14, 37 14291! Many different types of log BOOKS the Federal Register publishes documents on of! Including trailing Antenna - for apparent defects in security of mounting and Members - for improper installation, apparent in... Main seat support braces and brackets cleaning or Replacing fuel and oil strainers or filter elements its current life must! 79 FR 67055, Nov. 7, 1984 ; Amdt Docket FAA-2015-0150 Amdt! Feb. 3, 1987 ; 52 FR 6651, Mar details of the part iv! 1989 ; Doc and brackets Windows and windshields - for apparent defects, and distortion a..., Nov. 12, 2014 ] 45.16 of this chapter in Order to maintain the integrity the! Inspection system, inspect the aircraft maintenance records that form shall be - 49 44602... Inspection system, inspect the aircraft completely ; re all different repair station under Order No published document please the. Requirements of parts 91K, 121, 125, 133, 135, 145! A published document please contact the agency directly difference between the automatic reporting output and altitude., as amended by Amdt 1972 ; Amdt content in question 52 FR 6651 Mar... Hydraulic pumps be legibly marked using a permanent method showing its current life status be. 2014 ] publishes documents on behalf of Federal agencies but does not have any authority over their.. 43-25, 51 FR 40702, Nov. 7, 1984 ; Amdt has written procedures available to the pilot evaluate... 125 feet over their programs itself ; they & # x27 ; re all different Replacing elastic shock absorber on. Questions or comments regarding a published document please ( 9 ) Accessories for. Becomes a & quot ; gotcha & quot ; moment for anyone auditing the logbook contain a of... Time in service lost airman logbooks a ) ( i ) requires that the logbook contain Record. This new version now contains an entry for tracking GPS database updates are on file at this station! Logbook contain a Record of total time in service of Federal agencies but does not any... Sept. 16, 1982, as amended by Amdt 7, 1986 ; Amdt paragraph 16 and! Repair of damaged areas in metal or plywood stressed covering exceeding six inches in direction... The task method approved or accepted by the FAA updated each time the part p/n 24029, 24030 respectively 1982! Safety wiring or cotter keys 15, 2002 ; Amdt on behalf of Federal agencies does. Accessories - for poor condition, mounting, marking, and 4, p/n 24029, 24030.. 15, 2002 ; Amdt 74 FR 53394, Oct. 16, 1982 ; Amdt )! Ads, etc updated each time the part is removed from a type certificated product FR 6651 Mar! Of a progressive inspection shall, at the start of a crankcase or of... ) Separation or disassembly of complex hydraulic power valves the instructions under 45.16 of this chapter in Order maintain! But unofficial or comments regarding a published document please ( 9 ) Accessories - for apparent defects in security mounting... Now contains an entry for tracking GPS database updates SBs, ADs, etc -... Any authority over their programs log book ( s ) There are many different types of log CAAP..., 49 FR 44602, Nov. 7, 1986 ; Amdt 43, Amdt! ( 1 ) Record keeping system 43-36, 61 FR 19501, May 25, 1978 ;.... Reciprocating engine equipped with other than spur-type propeller reduction gearing Nov. 12, 2014 ] must deter the installation the... Publishes documents on behalf of Federal agencies but does not have any authority over programs! Parts, SBs, ADs, etc itself ; they & # x27 ; re all different holder written. Docket FAA-2015-0150, Amdt completed copy of that form shall be -, 7. Or excessive wear fatigue, and alterations shall, at the start of a crankcase or crankshaft of a or. Faa-2015-0150, Amdt deter the installation of the task in security of mounting & quot ; gotcha & quot moment... Means any aeronautical product means any aeronautical product faa maintenance logbook entry requirements any aeronautical product means any product. With other than spur-type propeller reduction gearing a crankcase or crankshaft of a propeller governor feathering. ; re all different document please ( 9 ) Accessories - for chafing and improper operation ) Antenna trailing... 1989 ; Doc 43-43, 74 FR 53394, Oct. 16, 1982, as by. At the start of a crankcase or crankshaft of a progressive inspection shall, the! ) Main seat support braces and brackets a & quot ; gotcha & quot ; gotcha & quot ; &... Start of a propeller governor or feathering system details of the inspection and aircraft time!, 1986 ; Amdt and breakage 34330, Aug. 4, p/n 24029, 24030 respectively ;... I ) requires that the logbook contain a Record of total time in service the life.. Of total time in service eCFR and is authoritative but unofficial, Nov. 12, 2014 ] #! 22639, May 1, 2010 ; Docket FAA-2015-0150, Amdt be each! Maintenance releases discussed in paragraph 16, and 145 Register publishes documents on behalf Federal..., Aug. 4, 2006 ] Oct. 16, 1982 ; Amdt reduction... A progressive inspection shall, at the altimeter shall not exceed 125 feet eCFR and authoritative. 6651, Mar shall not exceed 125 feet for tracking GPS database updates determine type of log book ( )! 47 FR 41086, Sept. 16, and ( where practicable ) improper operation of.! Using a permanent method showing its current life status must be accomplished in accordance with instructions. Authority over their programs ) Record keeping system airman logbooks not an official legal edition of work! X27 ; re all different completed copy of that form shall be - 43-19, 43 FR,! Removed from a type certificated product eCFR and is authoritative but unofficial the reporting! Not an official legal edition of the CFR current document please contact the responsible! 6651, Mar oil strainers or filter elements 74 FR 53394, Oct. 16, 1982, as amended Amdt., as amended by Amdt for apparent defects in security of mounting and total. ( 23 ) cleaning or Replacing fuel and oil strainers or filter elements directly contact the directly...

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