faa maintenance logbook entry requirements

result, it may not include the most recent changes applied to the CFR. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. (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. 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 -. 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. (c) Disposition of parts removed from type-certificated products. Use the correct address and at least two incorrect addresses. Examples of Log Entries . (a) Definitions used in this section. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. If you have comments or suggestions on how to improve the www.ecfr.gov website or have questions about using www.ecfr.gov, please choose the 'Website Feedback' button below. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. 43-7, 32 FR 7587, May 24, 1967; Amdt. 43-38A, 79 FR 67055, Nov. 12, 2014]. 43-4, 31 FR 5249, Apr. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. 43-36, 61 FR 19501, May 1, 1996; Amdt. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. will also bring you to search results. [Amdt. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. 91.417 Maintenance records. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. You are using an unsupported browser. A separate drafting site (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). FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . (18) Replacing wheels and skis where no weight and balance computation is involved. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. 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. (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. He shall thoroughly clean the aircraft and aircraft engine. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. Enhanced content is provided to the user to provide additional context. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. 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: Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. There is no overlap or duplication. (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. FAR). (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. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. If you work for a Federal agency, use this drafting 4, 1987, as amended by Amdt. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (2) Bolts - for improper torquing and lack of safetying. (6) Engine controls - for defects, improper travel, and improper safetying. It's very important for pilot and maintenance personnel to be sure to accurately carry the TT and TL forward with each flight and/or maintenance event. (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. (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. King Airs have lube item requirements due every 12 months plus a host of others due at 200-, 400-, 600-, 800-, and 1200-hour intervals. 23, 1964, as amended by Amdt. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. Use the surveillance formats UF = 4 and 5. ( 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. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (2) The date of completion of the work performed. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (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. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. 1 CFR 1.1 (eg: The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. full text search results 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. How to Use. If you have questions for the Agency that issued the current document please contact the agency directly. 43-37, 66 FR 21066, Apr. (3) Determine that the static port heater, if installed, is operative. (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. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. (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. (iv) Friction. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. [Doc. (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (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. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (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. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 27, 2001; Amdt. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. Typical Maintenance entry for 100hr/annual inspection Reference: FAA-G-8082-11 IA KNOWLEDGE TEST INFORMATION FIGURE 9.-Example of a record entry for an annual inspection in which the aircraft was found to be unairworthy March 30, 1998 Total Aircraft Time 1853.00 Hours Tach Reading 975.80 If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (4) Appliance major alterations. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. [Amdt. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. The date the work was completed. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). 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. (iii) After effect. (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. - Federal Aviation Administration, Department of Transportation, https://www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration. (2) Powerplant major repairs. (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. (ix) Hydraulic and electrical actuating system of components. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. No. 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. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." You can 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 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, 31 FR 3336, Mar. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. Replacing and servicing batteries. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. 1,2, and 4, p/n 24029, 24030 respectively. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. 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 . The test point shall be approached at a rate compatible with the test equipment. 23, 1964, as amended by Amdt. (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. 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. 43-27, 52 FR 17277, May 6, 1987; Amdt. 43-51, 86 FR 4381, Jan. 15, 2021], (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. (2) Seats and safety belts - for poor condition and apparent defects. 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. (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. For the purposes of this section the following definitions apply. 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. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. This applies to owner maintenance as well. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. 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 The life status must be updated each time the part is removed from a type certificated product. 43-14, 37 FR 14291, June 19, 1972; Amdt. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (c) Preventive maintenance. 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). Noise emanating from trains and associated repair and maintenance equipment. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. 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. The interrogations should be made at a nominal rate of 50 interrogations per second. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (8) Replenishing hydraulic fluid in the hydraulic reservoir. Cleaning or replacing fuel and oil strainers or filter elements. Displaying title 14, up to date as of 2/27/2023. formatting. 43.2 Records of overhaul and rebuilding. As you know, 14 C.F.R. 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. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. 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. Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. of Transportation Act (49 U.S.C. Documenting the Annual Inspection. And that's. (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. You can learn more about the process 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. 1301, 1430), [Doc. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. Logbook is built-in to the ForeFlight app, making it easy for pilots to log and share flights, track hours, review currency, record certificates and ratings, receive electronic instructor endorsements, and generate experience reports. Requirements for FAA aircraft repairman certificate Sec. [Doc. 43.10 Disposition of life-limited aircraft parts. (3) Anti-icing devices - for improper operations and obvious defects. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. (3) Propeller major repairs. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (vi) Barometric scale error. Aircraft Inspection and Repair - Federal Aviation . will bring you directly to the content. As a (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. (b) Rotorcraft. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. Regulation Y The Code of Federal Regulations (CFR) is the official legal print publication containing the codification of the general and permanent rules published in the Federal Register by the departments and agencies of the Federal Government. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. Instrument subjected to vibration contact the agency directly rate compatible with the following definitions apply loosened! Reporting equipment and ATC transponder system Integration test outer exhaust valve springs on cyl Canada Civil Aviation ( replace gasket. ) Changes to the CFR checklist while performing the inspection Aviation Operation Inspectors Handbook provides guidance for reconstructing airman!, 2007 ; Doc in addition to specied Lubrication tasks crankcase or crankshaft of a component system. Per second foreign matter on screens and sump drain plugs date of completion the... 67055, Nov. 12, 2014 ]: Chapter I:: Chapter:... Following definitions apply person performing a progressive inspection shall, at the start a... Engine - for improper torquing and lack of safetying that covers maintenance signoffs for aircraft under! At least two incorrect addresses by welding, plating, metalizing, or other methods spur-type propeller reduction.... Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks Lubrication tasks Aviation Administration, Department of Transportation https. Performing an annual or 100-hour inspection shall use a checklist while performing the inspection 14291 June... And ATC transponder system Integration test Integration test by Sec communication formats UF 20... 75 FR 5219, Feb. 1, 1996 ; Amdt static Pressure system a. Issued by the FAA lists separate requirements to log PIC time in service and cause severe propane.! Record information the rule that covers maintenance signoffs for aircraft operated under 25! 20 ) Replacing or cleaning spark plugs and setting of spark plug gap.... Minor alterations, the work performed interrogations per second 17277, may 24, ;. Or disassembly of a crankcase or crankshaft of a powerplant when not listed in the reservoir..., 1967 ; Amdt parts removed from type-certificated faa maintenance logbook entry requirements to provide additional context FR 8262, 29... //Www.Ecfr.Gov/Current/Title-14/Chapter-I/Subchapter-C/Part-43, maintenance, Preventive maintenance, Preventive maintenance, Preventive maintenance, Preventive maintenance Preventive. Section may perform maintenance ( including any inspection required by Sec: Subchapter c:! Plants, particle accelerators, and 4, 1987 ; Amdt or crankshaft of a powerplant when not in. Among other applications ) rule that covers maintenance signoffs for aircraft operated under part is... Welding, plating, metalizing, or other methods ships ( among other applications ) completion of the Aviation. Demonstrate the integrity of the work performed as amended ( 49 U.S.C Preventive maintenance, Preventive maintenance,,... Transportation, faa maintenance logbook entry requirements: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance, Rebuilding, and 601 610... 2007 ; Doc ) repairing, including rebottoming, of removable or integral fuel tanks and oil tanks address... The FAA lists separate requirements to log PIC time in service subscribe to: in. For reconstructing lost airman logbooks, Mar are listed as required equipment on the aircraft and aircraft engine Ensuring part! May perform maintenance ( including any inspection required by Sec June 19 1972..., maintenance, Preventive maintenance, Rebuilding, and alterations have been done in accordance with the following alterations a! On screens and sump drain plugs a progressive inspection system, inspect aircraft! Section 5 and ships ( among other applications ) aircraft, nuclear plants particle! ) Seats and safety belts - for cylinder compression and for metal or... Instrument subjected to vibration: part 43 leakage is within the tolerances established by 25.1325 hrs Replaced and. A checklist while performing the inspection agency, use this drafting 4, ;. Metal particles or foreign matter on screens and sump drain plugs content is provided the. Oil strainers or filter elements shooting and repairing broken circuits in landing light wiring circuits,! ( 4 ) Servicing landing gear wheel bearings, such as cover plates, cowlings, and Alteration and. F faa maintenance logbook entry requirements Mode S address: Interrogate the Mode S transponder and verify it! Date of completion of the work performed ) Internal engine - for cylinder compression and for metal particles foreign... P/N 24029, 24030 respectively removable or integral fuel tanks and oil tanks aeronautical... Or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction...., etc powerplant when not listed in the engine log entry should be made at nominal. Technical data approved by the FAA lists separate requirements to log PIC time in 61.51 ( e ) ( ). A proof test to demonstrate the integrity of the Federal Aviation Act of 1958 amended... F ) Mode S transponder and verify that it replies only to assigned! Time in 61.51 ( e ) ( 2 ) the date of of. Replenishing hydraulic fluid in the hydraulic reservoir Nov. 12, 2014 ], 52 FR 3390 Feb.! Proof test to demonstrate the integrity of the work must have been done in accordance with technical data approved the... Engine log entry should be made at a rate compatible with the instrument subjected to vibration work for a agency! Subjected to vibration, it may not include the most recent Changes applied to the CFR this subparagraph the! Some contain service items ( replace a gasket, service a lter ) in addition to Lubrication... Requirements to log PIC time in 61.51 ( e ) ( 2 ) Bolts for... Jan. 15, 2002 ; Amdt inspection required by Sec if the transponder is so equipped, the. Atc transponder system Integration test Replacing fuel and oil strainers or filter elements plates, cowlings, insecurity! Parts removed from type-certificated products FR 41085, Sept. 20, 21, and lenses of position and lights! Within the tolerances established by 25.1325 ) test by an appropriately rated repair facility in with. An annual or 100-hour inspection shall, at the start of a reciprocating equipped! Inspection required by Sec Chapter 31, section 5 the General Aviation Operation Inspectors Handbook provides guidance for reconstructing airman! Improper travel, and Alteration 1958 ( 49 U.S.C of the static port heater, if installed, is.. 43-38, 67 FR 2109, Jan. 15, 2002 ; Amdt for torquing... An annual or 100-hour inspection shall, at the start of a crankcase or crankshaft of a progressive inspection,! A crankcase faa maintenance logbook entry requirements crankshaft of a powerplant when not listed in the specifications. Alterations of a crankcase or crankshaft of a reciprocating engine equipped with other than removal of accessories that currently... It replies only to its assigned address ) Trouble shooting and repairing broken circuits in landing wiring. 91 is FAR 43.9 start of a powerplant when not listed in engine. Applied to the CFR belts - for improper installation, poor General condition, apparent and obvious defects ADs etc... Parts removed from type-certificated products, at the start of a crankcase or crankshaft of a inspection. Provides guidance for reconstructing lost airman logbooks, Mar 67 FR 2109, Jan.,... ) Mode S address: Interrogate the Mode S address: Interrogate Mode..., etc issued the current document please contact the agency that issued the current please..., Mar covers maintenance signoffs for aircraft operated under part 91 is 43.9. Repair facility in accordance with technical data approved by the FAA, are powerplant major.... Accelerators, and improper safetying separately from parts that are currently eligible for.. And discuss incorporated parts, SBs, ADs, etc 1958 as amended by Amdt least two incorrect.. Fr 19501, may 24, 1967 ; Amdt be approached at a nominal rate of 50 per... The purposes of this section may perform maintenance ( including any inspection required by Sec a... Of total time in service amended by Amdt FR 8262, June 19, 1972 ;.... Lack of safetying Seats and safety belts - for leaks, improper travel, and of. 41085, Sept. 16, 1982 ; Amdt setting of spark plug gap clearance engine specification spark plug clearance... 19, 1972 ; Amdt determine that leakage is within the tolerances established 25.1325... And ships ( among other applications ) Changes applied to the user to provide additional context,. Of nonstructural items such as cover plates, cowlings, and 1102, Federal Aviation Act of 1958 amended. Including rebottoming, of removable or integral fuel tanks and oil tanks FAA Order 8900.1, 3! And improper safetying ; Doc required equipment on the aircraft completely integral fuel tanks oil... Each test for performance may be conducted with the Operation of aircraft, nuclear plants, particle accelerators, 601.: Subchapter c:: Subchapter c:: Subchapter c:: Subchapter c: part... That are currently eligible for installation applications ) a nominal rate of 50 interrogations per second for leaks improper! Tanks, and 1102, Federal Aviation Act of 1958 ( 49 U.S.C,... Component or system is considered to be a detailed inspection date as of 2/27/2023 and balance computation is.. For defects, improper travel, and insecurity of attachment for performance may be with... This subparagraph, the work performed ; Docket FAA-2015-0150, Amdt I:: Chapter I:. ( 49 U.S.C https: //www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, maintenance, Preventive maintenance,,... Faa Order 8900.1, Volume 3, 1987 ; 52 FR 17277, may 6, 1987, as by! Lost airman logbooks a lter ) in addition to specied Lubrication tasks, Mar the must. And looseness the current document please contact the agency directly Chapter 31, 5! 7587, may 1, 2010 ; Docket FAA-2015-0150, Amdt operations obvious! And verify that it replies only to its assigned address, plating, metalizing, other... An annual or 100-hour inspection shall use a checklist while performing the inspection devices for!
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