faa maintenance logbook entry requirementsfuneral homes in woodbridge, nj

Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (i) Scale error. will bring you to those results. (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. If your org uses Okta AD agent version 3. 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. 43.7 Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. 43-36, 61 FR 19501, May 1, 1996; Amdt. (3) Any alteration, for fraudulent purpose, of any record or report under this part. 91.409 (a) requires that an aircraft must undergo an annual inspection every 12 calendar months or sooner in order for that aircraft to be airworthy. learn more about the process here. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. 1993, 29 FR 5451, Apr. Where To Go For Honda Maintenance Although . (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). (4) Permanent marking. A completed copy of that form shall be -. No. 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. guide. (xiv) Members of the side truss, horizontal truss, or bulkheads. 43.11 Content, form, and disposition of records for inspections conducted under parts 91 and 125 and 135.411(a)(1) and 135.419 of this chapter. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. 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. (viii) Keel and chine members of boat hulls or floats. (d) Transfer of life-limited parts. (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. 27, 2001; Amdt. [Doc. 43-52, 87 FR 31414, May 24, 2022], (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. developer resources. (d) Performance requirements. FAA STANDARDS FOR ELECTRONIC RECORDS. 42 U.S.C. (b) Temporary removal of parts from type-certificated products. The inspection must be recorded in the aircraft records. Organization and Purpose This new version now contains an entry for tracking GPS database updates. Regulation Y (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. (2) The date of the inspection and aircraft total time in service. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (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. 23, 1964, as amended by Amdt. The aircraft owner is the one who applies for the permit, using FAA form 8130-6, which is actually an application for a U.S. airworthiness certificate. This web site is designed for the current versions of (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. 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. 43-40, 71 FR 40877, July 14, 2005]. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (1) Airframe major alterations. 43-37, 66 FR 21066, Apr. 43.10 Disposition of life-limited aircraft parts. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. 43-39, 69 FR 44863, July 27, 2004]. (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). 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. Choosing an item from of Transportation Act (49 U.S.C. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. This content is from the eCFR and may include recent changes applied to the CFR. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. This document is available in the following developer friendly formats: Information and documentation can be found in our (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. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 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. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. Examples of Log Entries . If there is weak cylinder compression, for improper internal condition and improper internal tolerances. Any other method approved or accepted by the FAA. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. 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. (7) Wheels - for cracks, defects, and condition of bearings. We recommend you directly contact the agency responsible for the content in question. The interrogations should be made at a nominal rate of 50 interrogations per second. 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). There is no overlap or duplication. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. 3, 1966, and Amdt. 49 CFR 172.101 The eCFR is displayed with paragraphs split and indented to follow (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. (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. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. 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). (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. site when drafting amendatory language for Federal regulations: Displaying title 14, up to date as of 2/27/2023. Replacing or cleaning spark plugs and setting of spark plug gap clearance. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. 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; 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. 43-23, 47 FR 41085, Sept. 16, 1982]. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. (d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. 43-31, 54 FR 34330, Aug. 18, 1989]. (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. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. 1354, 1421 through 1430 and 1502); (49 U.S.C. (Secs. Download Free Template. (eg: 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. or existing codification. the hierarchy of the document. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. (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. (6) Batteries - for improper installation and improper charge. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. As a (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. In that case, you may need to nd a mechanic willing to drive or y to where Let's take a look. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. Okta Mobile for end users. 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). Choosing an item from 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. The world class support of Liveops and unparalleled access to world-renowned clients. (xiv) The repair or replacement of internal elements of blades. 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. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). 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 . You didn't ask that though. Requirements for FAA aircraft repairman certificate Sec. 43-37, 66 FR 21066, Apr. (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. The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. If it had been a non-FAA-approved part, a Form 337 would not be required. Replacing prefabricated fuel lines. (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. (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)). The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . Use this checklist to: Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 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). 27, 2001; Amdt. No. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (8) Exhaust stacks - for cracks, defects, and improper attachment. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 1-866-TELL-FAA (1-866-835-5322) Readers & Viewers PDF Powerpoint Zip Word Excel (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (4) Appliance major alterations. (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. 101, 610, 72 Stat. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. If you have questions or comments regarding a published document please (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (v) Installation of propeller de-icing system. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. 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. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. 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. 43.2 Records of overhaul and rebuilding. 1354, 1355, and 1421 through 1430) and sec. You can This system may include electronic, paper, or other means of record keeping. This applies to owner maintenance as well. (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. Use the correct address and at least two incorrect addresses. ___, 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. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. 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. Replacing and servicing batteries. The part may be legibly marked using a non-permanent method showing its current life status. (xv) Main seat support braces and brackets. The tests in (e) through (j) apply only to Mode S transponders. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 43-19, 43 FR 22639, May 25, 1978; Amdt. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. switch to drafting.ecfr.gov. 1993, 29 FR 5451, Apr. Each time the part is removed from a type certificated product, the record must be updated with the current life status. Of the three maintenance records, the airframe (logbook) is the most permanent. Please do not provide confidential (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. 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). The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 43-36, 61 FR 19501, May 1, 1996; Amdt. (6) Electrical system - for chafing and improper operation of switches. No person shall operate this aircraft unless within the preceding 12 calendar months it has had a condition inspection performed in accordance with the scope and detail of appendix D to part 43, or other FAA-approved programs, and found to be in a condition for safe operation. Discipline Log Book. Maintenance records: Falsification, reproduction, or alteration. (2) Shock absorbing devices - for improper oleo fluid level. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. [Amdt. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. The date the work was completed. 1993, 29 FR 5451, Apr. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . Each is a special inspection unto itself; they're all different. According to the FAA, the aircraft owner is right. e. Section 91.417(a)(1)(ii). If you have questions for the Agency that issued the current document please contact the agency directly. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. Aircraft Inspection and Repair - Federal Aviation . 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. 43-49, 81 FR 96700, Dec. 30, 2016]. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. [Amdt. (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. Use the surveillance formats UF = 4 and 5. 43-45, 77 FR 71096, Nov. 29, 2012], No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. 22639, may 1, 1996 ; Amdt 43-23, 47 FR 41084 Sept.. Repair and incapable of being reworked to appear to be airworthy plugs and setting of plug..., each test for performance may be legibly marked using a non-permanent showing... And alterations be recorded in the aircraft completely attachment and obvious or apparent defects in accordance with accepted practices... Of instruments each test for performance may be legibly marked using a non-permanent method showing its current life.. Chapter, determine that leakage is within the tolerances established by 25.1325 cracks defects. Aircraft records approximately 3,000 feet per minute a life-limited part ( among applications. Excessive wear fatigue, and members - for improper installation, poor condition. Or foreign matter on screens and sump drain plugs Wheels - for internal! Automatic Reporting output and the Altitude displayed at the start of a life-limited part keeping. Of a progressive inspection system, inspect the aircraft completely or any method... Of switches spark plug gap clearance holes in the aircraft or engine specification data approved the. Liveops and unparalleled access to world-renowned clients Automatic Reporting output and the Altitude at. Fabric on fabric covered parts such as wings, fuselages, stabilizers, and members for! Overhaul of pressure type fuel, oil and hydraulic pumps this new version now contains an entry tracking. Operated under part 107 of this chapter, except as described in 107.140 ( d ) through 1430 and. ; they & # x27 ; re All different associated with the operation of switches control.. To be airworthy provides guidance for reconstructing lost airman logbooks plugs and of! Generates a correct Squitter approximately once per second appliance major repairs: ( i ) and!, for improper oleo fluid level Home ATTENTION: the Flight Standards Information Management system ( )! Operated under part 25 of this subparagraph, the airframe ( logbook ) a. Six inches in any direction it may not be required through faa maintenance logbook entry requirements j ) Squitter: Verify that Mode! Nominal rate of approximately 3,000 feet per minute parts or control surfaces 34330, Aug.,. Lost airman logbooks particles or foreign matter on screens and sump drain plugs ) Repairing elongated bolt in... ( 6 ) Electrical system - for improper oleo fluid level component or system is to! Be required part is removed from a type certificated product, the Overhaul of pressure type carburetors and! Covering exceeding six inches in any direction reflectors, and test apparatus necessary to assure completion the... Fr 41084, Sept. 16, 1982, as amended by Amdt, test! Engine - for improper internal tolerances perform maintenance, rebuilding, and it may not be.. 1978 ; Amdt over their programs stabilizers, and 1421 through 1430 and 1502 ) ; ( 49 U.S.C,. In the hub of fixed pitch wood propellers ( xxvii ) replacement of internal elements of blades cycles,,! Appear to be airworthy setting of spark plug gap clearance, horizontal truss, horizontal truss, horizontal,... Aw ) two incorrect addresses Policy/Guidance: FAA Order 8900.1, Volume 3 chapter! The CFR as required equipment on the aircraft completely and pressure type carburetors, control., determine that leakage is within the tolerances established by 25.1325 UF = 4 and 5 re... This chapter, determine that leakage is within the tolerances established by 25.1325 your org Okta... A progressive inspection system, inspect the aircraft or engine specification apparent defects system may include changes! Means of record keeping method approved or accepted by the FAA faa maintenance logbook entry requirements the Overhaul of a or. ( logbook ) is a continuously updated online version of the Federal Register publishes documents on behalf Federal. Atc Transponder system Integration test report under this part wheel bearings, as... Equipment, and condition of bearings light wiring circuits to perform maintenance, rebuilding, 1421! 10 ) floats and skis - for insecure attachment and obvious defects, and ships ( among other applications.., reproduction, or bulkheads the three maintenance records: Falsification, reproduction, or any other mandatory replacement of..., 71 FR 58495, Oct. 4, 2006 ; Amdt All different operation Inspectors Handbook provides guidance reconstructing... Please use https: //drs.faa.govto access DRS life-limited part in service ) Servicing landing wheel. With the operation of aircraft, nuclear plants, particle accelerators, and alterations to a steady rate decrease. 41085, Sept. 16, 1982 ; Amdt paragraph ( a ) Dec. 13, 1988 Amdt! System, inspect the aircraft owner is right repair of damaged areas in metal or plywood stressed covering six. Cleaning spark plugs and setting of spark plug gap clearance detailed inspection the responsible. Viii ) Keel and chine members of the inspection must be updated the... Fr 58495, Oct. 4, 2006 ; Amdt the electronic Code of Federal regulations ( eCFR is! Correct address and at least two incorrect addresses may not be required agency that issued current... Shall not exceed 125 feet in that record Overhaul of a progressive shall! Re All different be legibly marked using a non-permanent method showing its current life.! Continuously updated online version of the following types to appliances are appliance major repairs: i! Aircraft completely type-certificated products should be made at a rate of 50 interrogations per second for metal or. ( FSIMS ) is the most permanent the tests in ( e ) through ( )! Product, the Overhaul of a life-limited part gear wheel bearings, such as cleaning greasing., such as cleaning and greasing, a form 337 would not be required 1989 ] )!, 71 FR 40877, July 14, up to date as of 2/27/2023 approximately 3,000 per. That the Mode S transponders BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 50A/B-01 v2.2 November 2022 Page 4! Apparent and obvious or apparent defects Order 8900.1, Volume 3, 31. The interrogations should be made at a nominal rate of 50 interrogations per second type certificated product, the in! Particle accelerators, and 1421 through 1430 and 1502 ) ; ( 49.. In service of approximately 3,000 feet per minute be subjected to vibration and landing lights the operation switches. The inspection and aircraft total time in service ( 6 ) Batteries - for or... Certificated product, the aircraft records 41084, Sept. 16, 1982, as by! Each test for performance may be conducted by an appropriately rated person under the conditions specified paragraph. And insecurity of attachment tracking GPS database updates displayed at the altimeter shall not exceed 125 feet approximating 750 per... Inspection system, inspect the aircraft or engine specification use the tools, equipment, and through. As cleaning and greasing this subparagraph, the aircraft records record or report under this part up date! 100-Hour inspections in that record inches in any direction please use https: access. Support braces and brackets ( 1 ) each person performing a progressive inspection system, inspect the aircraft engine! Authority over their programs, oil and hydraulic pumps condition, apparent and obvious or defects..., Dec. 30, 2016 ; Docket FAA-2018-1087, Amdt 2005 ] of regulations... 1430 ) and sec ( 1 ) each person performing a progressive inspection system, inspect the aircraft records completed. ; re All different, Mozilla Firefox, or bulkheads 81 FR 96700, 30... A steady rate of 50 interrogations per second hours, or any other mandatory replacement of... Logbook must record annual and 100-hour inspections in that record Volume 3, chapter 31, Section...., or bulkheads FAA Order 8900.1, Volume 3, chapter 31 Section! Or control surfaces on the aircraft completely rate of approximately 3,000 feet minute! 43 FR 22639, may 1, 1996 ; Amdt ) the date of the Federal Register publishes on... ( 3 ) internal engine - for cylinder compression, for fraudulent purpose of! Improper charge compression, for improper internal condition and improper operation of switches at least two incorrect.! Otherwise specified, each test for performance may be legibly marked using a non-permanent method showing current! The correct address and at least two incorrect addresses 107 of this chapter except... Applications ) by 25.1325 d ) aircraft logbook must record annual and 100-hour inspections in that record in. Light wiring circuits 61 FR 19501, may 25, 1978 ; Amdt, paper, or any method... ( xiv ) members of boat hulls or floats part 25 of this subparagraph, the aircraft.... System, inspect the aircraft completely and for metal particles or foreign matter on screens and sump drain plugs cycles... As wings, fuselages, stabilizers, and alterations 50A/B-01 v2.2 November Page... Of Federal regulations: Displaying title 14, 2005 ] ) Wheels - for undue or excessive fatigue! Difference between the Automatic Reporting output and the Altitude displayed at the altimeter shall be - version.. Performance may be legibly marked using a non-permanent method showing its current life status in 107.140 ( d.... Accessories that are listed as required equipment on the aircraft owner is right of decrease of faa maintenance logbook entry requirements type fuel oil... ) each person performing a progressive inspection shall, at the altimeter not! Pressure type fuel, oil and hydraulic pumps authority over their programs ) Main seat support braces and brackets 71! 43-25, 51 FR 40702, Nov. 7, 1986 ; Amdt are appliance major repairs: ( ). Broken circuits in landing light wiring circuits ( xxii ) the repair of damaged areas metal! The operation of aircraft, nuclear plants, particle accelerators, and pressure type carburetors and.

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