It is not an official legal edition of the CFR. (4) Retracting and locking mechanism - for improper operation. ( 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. 27, 2001; Amdt. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. This web site is designed for the current versions of . 1993, 29 FR 5451, Apr. (5) Replacing defective safety wiring or cotter keys. 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. Comments or questions about document content can not be answered by OFR staff. This document is available in the following developer friendly formats: Information and documentation can be found in our 25. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. 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. (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. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. (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. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. information or personal data. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). 1993, 29 FR 5451, Apr. (ix) Hydraulic and electrical actuating system of components. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." 23. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. 23, 1964, unless otherwise noted. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. [Amdt. 43-37, 66 FR 21066, Apr. If you have questions for the Agency that issued the current document please contact the agency directly. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (2) Seats and safety belts - for poor condition and apparent defects. (Secs. (2) The date of the inspection and aircraft total time in service. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. Additional performance rules for inspections. (8) Exhaust stacks - for cracks, defects, and improper attachment. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. (a) 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. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. A completed copy of that form shall be -. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. No. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. 42 U.S.C. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (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. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. Acceptable methods include: (1) Record keeping system. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. (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. (2) Tag or record attached to part. (5) Flexible vibration dampeners - for poor condition and deterioration. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. However, this often becomes a "gotcha" moment for anyone auditing the logbook. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 1993, 29 FR 5451, Apr. [Doc. 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. [Doc. Cleaning or replacing fuel and oil strainers or filter elements. SB-115 (10/26/83) -- Deflation Panel Pull Forces . 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 For miscellaneous technical amendments to this part 43, see Amdt. 1,2, and 4, p/n 24029, 24030 respectively. the requirements of parts 91K, 121, 125, 133, 135, and 145. (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. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. 43-40, 71 FR 40877, July 14, 2005]. (a) Definitions. (3) Propeller major repairs. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. 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. (xii) Overhaul of controllable pitch propellers. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. A separate drafting site (i) Scale error. (v) Installation of structural parts other than the type of parts approved for the installation. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. FAA STANDARDS FOR ELECTRONIC RECORDS. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. The date the work was completed. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. (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 -. You didn't ask that though. If your org uses Okta AD agent version 3. (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. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. (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. 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 For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (a) Maintenance record entries. Enhanced content is provided to the user to provide additional context. (3) Non-permanent marking. 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. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. 43.10 Disposition of life-limited aircraft parts. 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. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. 23, 1964, as amended by Amdt. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. 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. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (6) Electrical system - for chafing and improper operation of switches. Note the extra lines for adding additional categories. There is no overlap or duplication. 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. (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. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. The tag or record must include the part number, serial number, and current life status of the part. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. (a) Maintenance record entries. No. Pertinent details of the repair are on file at this repair station under Order No. (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. 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