The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (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. (c) Preventive maintenance. Replacing any hose connection except hydraulic connections. ); (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. 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. 23, 1964, as amended by Amdt. will also bring you to search results. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. 27, 2001; Amdt. (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 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. (Secs. 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. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (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. Additional performance rules for inspections. (7) Wheels - for cracks, defects, and condition of bearings. Organization and Purpose (6) Mutilation. (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. No. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (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)). Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. 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. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. 4, 1987, as amended by Amdt. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. 43-37, 66 FR 21066, Apr. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. 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: 23, 1964, as amended by Amdt. 27, 2001], (a) General. citations and headings (a) Definitions. If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. [Doc. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. 1655(c))), [Amdt. (8) Exhaust stacks - for cracks, defects, and improper attachment. No. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. Record data. Displaying title 14, up to date as of 2/27/2023. Acceptable methods include: (1) Record keeping system. 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. If your org uses Okta AD agent version 3. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. [Doc. 43-37, 66 FR 21066, Apr. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (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). Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. 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 There is no overlap or duplication. This applies to owner maintenance as well. If you have questions for the Agency that issued the current document please contact the agency directly. (6) Electrical system - for chafing and improper operation of switches. 91.417 Maintenance records. How to Use. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. The test point shall be approached at a rate compatible with the test equipment. 27, 2001; Amdt. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. Noise emanating from trains and associated repair and maintenance equipment. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. The official, published CFR, is updated annually and available below under (v) Installation of structural parts other than the type of parts approved for the installation. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. e. Section 91.417(a)(1)(ii). (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. (iii) Rewinding the field coil of an electrical accessory. The error at all test points must not exceed the tolerances specified in Table I. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. 43-43, 74 FR 53394, Oct. 16, 2009]. The signature constitutes the approval for return to service only for the work performed. (iv) Installation of a propeller governor or feathering system. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (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. 101, 610, 72 Stat. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. (6) Engine controls - for defects, improper travel, and improper safetying. the hierarchy of the document. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (xiv) The repair or replacement of internal elements of blades. (a) Except for work performed in accordance with 91.411 and 91.413, each registered owner or operator shall keep the following records for the periods specified in paragraph (b) of this section . Documenting the Annual Inspection. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. switch to drafting.ecfr.gov. 1, 1966; Amdt. [Amdt. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. The inspection must be recorded in the aircraft records. or existing codification. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (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. 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. 23, 1964, as amended by Amdt. (6) Batteries - for improper installation and improper charge. Title 14 was last amended 2/27/2023. (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. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (3) Any alteration, for fraudulent purpose, of any record or report under this part. 1/1.1 Enhanced content is provided to the user to provide additional context. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. For the purposes of this section the following definitions apply. will bring you to those results. 43-49, 81 FR 96700, Dec. 30, 2016]. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (8) Replenishing hydraulic fluid in the hydraulic reservoir. A separate drafting site (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. 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. Regulation Y (b) Rotorcraft. (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. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. This is an automated process for (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 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. FAR 43.9 Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, 135.411 (a) (1), and 135.419 of this chapter). (9) Accessories - for apparent defects in security of mounting. 24. (i) Scale error. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (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. (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. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. The date of completion. (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. This web site is designed for the current versions of (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. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. (5) Flexible vibration dampeners - for poor condition and deterioration. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. No. Search & Navigation 1993, 29 FR 5451, Apr. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. 43-39, 69 FR 44863, July 27, 2004; Amdt. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 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. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (xiv) Members of the side truss, horizontal truss, or bulkheads. This important rule sets the requirements for the recording. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. Use the correct address and at least two incorrect addresses. (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. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. Before the permit is issued, an FAA inspector may personally inspect the aircraft, or require it to be inspected by an FAA certificated A&P mechanic or an appropriately certificated repair station, to determine its safety for the intended flight. (2) The date of the inspection and aircraft total time in service. (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. The life status must be updated each time the part is removed from a type certificated product. (v) Installation of propeller de-icing system. (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. 1993, 29 FR 5451, Apr. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. The test point shall then be approached at a rate of approximately 3,000 feet per minute. 43-37, 66 FR 21066, Apr. contact the publishing agency. 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. 43-28, 52 FR 20028, June 16, 1987; Amdt. 43-23, 47 FR 41085, Sept. 16, 1982]. 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. (vi) Barometric scale error. (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. 1354, 1421 through 1430 and 1502); (49 U.S.C. 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. ( 5 ) Flexible vibration dampeners - for improper Installation and improper safetying altitude at... Replenishing hydraulic fluid in the hydraulic reservoir maintenance ( including any inspection required Sec! 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