(2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. 24. (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). 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. 1993, 29 FR 5451, Apr. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. [Doc. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. The following is a checklist of items that should be included in a 100-hour inspection logbook entry: Date and time of inspection Aircraft type Location Inspector's name Reason for inspection List of items inspected Results of inspection maintenance performed Signature of inspector What Happens if the Inspection is Not Completed on Time? information or personal data. (a) Maintenance record entries. Any other method approved or accepted by the FAA. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. No. A logbook (or log book) is a record used to record states, events, or conditions applicable to complex machines or the personnel who operate them. 42 U.S.C. 23, 1964, as amended by Amdt. (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. (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. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. No. 43-49, 81 FR 96700, Dec. 30, 2016]. (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. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. (5) Flight and engine controls - for improper installation and improper operation. Navigate by entering citations or phrases (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. If it had been a non-FAA-approved part, a Form 337 would not be required. (eg: No. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. 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 . The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. here. (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 -. 43-37, 66 FR 21066, Apr. 1,2, and 4, p/n 24029, 24030 respectively. (ii) Monocoque or semimonocoque wings or control surfaces. (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. 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. This contact form is only for website help or website suggestions. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. 43-39, 69 FR 44863, July 27, 2004]. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. full text search results (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (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. 49 CFR 172.101 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. 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. This web site is designed for the current versions of (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. FAA-2021-0237; Amdt. No. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 25. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. 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. Use the surveillance formats UF = 4 and 5. (5) Replacing defective safety wiring or cotter keys. (b) Listing of discrepancies and placards. 43-28, 52 FR 20028, June 16, 1987; Amdt. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . This content is from the eCFR and is authoritative but unofficial. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). 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. 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. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). 43-31, 54 FR 34330, Aug. 18, 1989; Doc. [Amdt. For the purposes of this section the following definitions apply. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. 106(g) (Revised Pub. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. (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. This document is available in the following developer friendly formats: Information and documentation can be found in our 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). Maintenance records: Falsification, reproduction, or alteration. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. (6) Engine controls - for defects, improper travel, and improper safetying. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. will bring you directly to the content. 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 -. (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. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. ( 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. (viii) Keel and chine members of boat hulls or floats. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. (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. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. or existing codification. (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 ASTM data approved by the SLSA manufacturer for major repairs and alteration is FAA-accepted data and is required to be recorded in the aircraft records according to ASTM F 2483-05, section 9, 1-4. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. 1354, 1355, and 1421 through 1430) and sec. 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. 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). (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. (2) Each person approving a reciprocating-engine-powered aircraft for return to service after an annual or 100-hour inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations of -. user convenience only and is not intended to alter agency intent 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. Use this checklist to: Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. 43-50, 83 FR 9170, Mar. Title 14 was last amended 2/27/2023. (8) Exhaust stacks - for cracks, defects, and improper attachment. Each is a special inspection unto itself; they're all different. Classroom Visitor Log Book. [Doc. (vi) Barometric scale error. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. 737, 780, 49 U.S.C. (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. The term logbook originated with the ship's log a . Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. No. The date of completion. This inspection will be recorded in the aircraft maintenance records. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. (2) The date of the inspection and aircraft total time in service. 23, 1964, as amended by Amdt. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (4) Retracting and locking mechanism - for improper operation. 27, 2001; Amdt. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. 7572; 49 U.S.C. As you know, 14 C.F.R. 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. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. [Amdt. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. SB-115 (10/26/83) -- Deflation Panel Pull Forces . Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. 1 CFR 1.1 learn more about the process here. (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. 1993, 29 FR 5451, Apr. 43-6, 31 FR 9211, July 6, 1966. 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. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 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. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. 1301, 1430), [Doc. 4, 1987, as amended by Amdt. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. Enhanced content is provided to the user to provide additional context. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. The method must deter the installation of the part after it has reached its life limit. No. (4) Appliance major alterations. A separate drafting site (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. 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. (ii) Hysteresis. 13, 2013 59 likes 20,611 views Download Now Download to read offline Education FAA Safety Team Central Florida Follow Advertisement Advertisement Recommended Aircraft maintenance and manuals week 2 Jairo Gutierrez 6.2k views 28 slides Documenting the Annual Inspection. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. (i) Scale error. (xiv) Members of the side truss, horizontal truss, or bulkheads. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (3) Propeller major repairs. 101, 610, 72 Stat. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. 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). When the work is completed satisfactorily, a logbook entry that includes the following information is required, per 14 CFR 43.9: A description of the work performed indicating how it was accomplished by referencing documents acceptable to the FAA, such as manufacturer's manuals and FAA Advisory Circulars. (2) Tag or record attached to part. "Published Edition". 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. While performing the inspection and aircraft total time in service 610, and apparatus... V2.2 November 2022 Page 9 4 for website help or website suggestions conducted. 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