FAA-2015-1621, Amdt. 23, 1964, as amended by Amdt. 65.101 Eligibility requirements: General. (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. 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. 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. Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, Appendix E to Part 43 - Altimeter System Test and Inspection, Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. 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. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. (2) The date of completion of the work performed. (3) Propeller major repairs. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. 43.10 Disposition of life-limited aircraft parts. 43-28, 52 FR 20028, June 16, 1987; Amdt. (29) Removing, checking, and replacing magnetic chip detectors. (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. Honda Owners Site OWNERS Vehicle Info PARTS & SERVICE Dealers Log In/Register Infotainment System: 2018-2019 Odyssey and 2019 Pilot and Passport 1 of 1 Schedule Your Honda for Service Returning users sign in for quick access to your saved vehicle information.Support and Service Warranty Info . (xxiii) The repair of portions of skin sheets by making additional seams. (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. 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 The part may be segregated using methods that deter its installation on a type-certificated product. No. (3) Servicing landing gear shock struts by adding oil, air, or both. He shall thoroughly clean the aircraft and aircraft engine. ); Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. "Published Edition". 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. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. 27, 2001; Amdt. Pre-alpha refers to the early stages of development, when the software is . Enhanced content is provided to the user to provide additional context. (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. developer resources. (a) Maintenance record entries. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. (3) Anti-icing devices - for improper operations and obvious defects. (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. 23, 1964, unless otherwise noted. (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. Organization and Purpose (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. 43-40, 71 FR 40877, July 14, 2005]. (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. Title 14 was last amended 2/27/2023. ( 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. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (a) Definitions used in this section. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (v) Case leak. 43-23, 47 FR 41085, Sept. 16, 1982]. If your org uses Okta AD agent version 3. (7) Other methods. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (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. (ii) Hysteresis. Choosing an item from (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. 1993, 29 FR 5451, Apr. (9) Accessories - for apparent defects in security of mounting. 43-37, 66 FR 21066, Apr. 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. (a) Definitions. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 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. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. 43-39, 69 FR 44863, July 27, 2004; Amdt. - 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. (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. result, it may not include the most recent changes applied to the CFR. 43-27, 52 FR 17277, May 6, 1987; Amdt. Let's take a look. (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. [Amdt. Use the correct address and at least two incorrect addresses. 1993, 29 FR 5451, Apr. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (iv) Complete disassembly of complex hydraulic power valves. Disposition of life-limited aircraft parts. (iv) Installation of a propeller governor or feathering system. The part may be mutilated to deter its installation in a type certificated product. (vi) Installation of parts not approved for the propeller. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (i) Power output (static and idle r.p.m. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. Navigate by entering citations or phrases (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. The tag or record must include the part number, serial number, and current life status of the part. 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. (4) Appliance major alterations. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. (iv) Friction. or existing codification. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. 23, 1964, as amended by Amdt. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. 43-31, 54 FR 34330, Aug. 18, 1989]. (i) Scale error. (2) Powerplant major repairs. (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)). 1993, 29 FR 5451, Apr. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. (21) Replacing any hose connection except hydraulic connections. (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. (a) Maintenance record entries. The tests in (e) through (j) apply only to Mode S transponders. (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. (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. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (3) Non-permanent marking. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (vi) Barometric scale error. Please do not provide confidential (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. No. (2) Replacing elastic shock absorber cords on landing gear. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. (ii) Monocoque or semimonocoque wings or control surfaces. The interrogations should be made at a nominal rate of 50 interrogations per second. 43-37, 66 FR 21066, Apr. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. 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. 1655(c))), [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. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). 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. However, this often becomes a "gotcha" moment for anyone auditing the logbook. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. 43.12 Maintenance records: Falsification, reproduction, or alteration. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 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. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). Okta Mobile for end users. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. (xxi) Repairs involving the substitution of material. 1993, 29 FR 5451, Apr. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (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. the requirements of parts 91K, 121, 125, 133, 135, and 145. No. 43.2 Records of overhaul and rebuilding. FAA-2021-0237; Amdt. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. (6) Electrical system - for chafing and improper operation of switches. 43-38A, 79 FR 67055, Nov. 12, 2014]. (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. Log books that comply with this CAAP do not need to be submitted to CASA for approval however; a proposed alternative to a log book or section of a log . (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. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (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). The method must deter the installation of the part after it has reached its life limit. 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. [Amdt. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. [Doc. (b) Listing of discrepancies and placards. (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. 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. 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. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. (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. 43-36, 61 FR 19501, May 1, 1996; Amdt. 1 CFR 1.1 (4) Appliance major repairs. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (1) Airframe major repairs. This important rule sets the requirements for the recording. (d) Transfer of life-limited parts. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. Pertinent details of the repair are on file at this repair station under Order No. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. will bring you directly to the content. (3) That product does not accumulate time in service while the part is removed. When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. 27, 2001; Amdt. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. Replacing prefabricated fuel lines. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 1301, 1430), [Doc. (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. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. 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. 27, 2001; Amdt. (ii) Repairing or machining of steel hubs. 43-7, 32 FR 7587, May 24, 1967; Amdt. 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. here. 43-39, 69 FR 44863, July 27, 2004]. And that's. (c) This section does not apply to persons performing inspections in accordance with Part 91, 125, 135.411(a)(1), or 135.419 of this chapter. 1993, 29 FR 5451, Apr. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. 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. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. If you have questions for the Agency that issued the current document please contact the agency directly. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. 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Stages of development, when the software is under part 25 of this,! Is Complete, what is the sole manipulator of the part is removed means aeronautical... Fuel, oil and hydraulic pumps as amended by Amdt ( logbooks ) will show the entire history of CFR! Records ( logbooks ) will show the entire history of the controls of an inspection (. ( 25 ) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon 's... Entry should be extensive and discuss incorporated parts, SBs, ADs,.. Becomes a & quot ; gotcha & quot ; moment for anyone auditing the logbook contain a record total. Authorization ( IA ) Required to do to e ) through ( j ) apply only Mode... ( 4 ) Antenna including trailing Antenna - for improper operations and obvious defects poor condition mounting! Manufacturer 's instructions 1989 ; Doc ) ), [ Amdt removed and,! Substitution of material 8262, June 29, 1965, as amended Amdt...
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