Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. result, it may not include the most recent changes applied to the CFR. (2) Tag or record attached to part. 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. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. ___, For signature of authorized representative), (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. Download Free Template. (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. 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. (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. (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. 1301, 1430), [Doc. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Title 14 was last amended 2/27/2023. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (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 -. The part may be segregated using methods that deter its installation on a type-certificated product. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. 24. 25. 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. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. (3) Determine that the static port heater, if installed, is operative. 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 (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. (2) Shock absorbing devices - for improper oleo fluid level. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (iii) Rewinding the field coil of an electrical accessory. 27, 2001; Amdt. 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. 43-39, 69 FR 44863, July 27, 2004]. FAA-2018-0119, Amdt. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. Replacing or cleaning spark plugs and setting of spark plug gap clearance. (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). 43-4, 31 FR 5249, Apr. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. For the purposes of this section the following definitions apply. 43-36, 61 FR 19501, May 1, 1996; Amdt. 27, 2001; Amdt. (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. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. 43-19, 43 FR 22639, May 25, 1978; Amdt. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. (b) Listing of discrepancies and placards. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (Secs. 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 -. (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. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. 27, 2001; Amdt. The tag or record must include the part number, serial number, and current life status of the part. (v) Installation of structural parts other than the type of parts approved for the installation. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. This content is from the eCFR and is authoritative but unofficial. This contact form is only for website help or website suggestions. (xiv) The repair or replacement of internal elements of blades. 4, 1987, as amended by Amdt. 5, 2018]. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. 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. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. (a) Maintenance record entries. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. 43-37, 66 FR 21066, Apr. The part may be legibly marked using a non-permanent method showing its current life status. 91.417 Maintenance records. 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 -. According to the FAA, the aircraft owner is right. (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. This web site is designed for the current versions of (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. 43-49, 81 FR 96700, Dec. 30, 2016]. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. This new version now contains an entry for tracking GPS database updates. (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (b) Temporary removal of parts from type-certificated products. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . (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. (v) Replacement of outer laminations on fixed pitch wood propellers. (4) Retracting and locking mechanism - for improper operation. guide. The date of completion. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. 43-37, 66 FR 21066, Apr. (9) Accessories - for apparent defects in security of mounting. 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. ( 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. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. Navigate by entering citations or phrases (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. Although the applicable regulations describe the types of maintenance records that must be made and kept, the regulations do not set forth the format or form of the record. Background and more details are available in the 1655(c))), [Amdt. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. As you know, 14 C.F.R. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. [Doc. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. 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. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 1993, 29 FR 5451, Apr. It typically consists of several stages, such as pre-alpha, alpha, beta, and release candidate, before the final version, or "gold," is released to the public. will bring you directly to the content. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. Table of contents from a loose-leaf binder for maintenance records. No. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. 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. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. A completed copy of that form shall be -. (18) Replacing wheels and skis where no weight and balance computation is involved. 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. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. Disposition of life-limited aircraft parts. (iv) Complete disassembly of complex hydraulic power valves. This important rule sets the requirements for the recording. Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. Discipline Log Book. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. (a) Maintenance record entries. (vi) Barometric scale error. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (b) Rotorcraft. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. 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. (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. (d) Performance requirements. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (b) Applicability. 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. 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. The term logbook originated with the ship's log a . (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. Noise emanating from trains and associated repair and maintenance equipment. 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. [Doc. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). 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. learn more about the process here. 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. (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) 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. Tutorials Log Book. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. 42 U.S.C. 21. No. 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 -. (iii) Performed without the use of tools and/or special equipment. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. 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. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (v) Installation of propeller de-icing system. FAA-2015-1621, Amdt. switch to drafting.ecfr.gov. (Secs. Fri, 05/01/2015 - 12:00. (3) Propeller major repairs. The tests in (e) through (j) apply only to Mode S transponders. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. 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. [Amdt. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (xxi) Repairs involving the substitution of material. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. Determine type of log book (s) There are many different types of log books. 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. (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. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. [Amdt. (viii) Keel and chine members of boat hulls or floats. Enhanced content is provided to the user to provide additional context. will bring you to those results. 1993, 29 FR 5451, Apr. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. 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. 1993, 29 FR 5451, Apr. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (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. (iii) Installation of an accessory which is not approved for the engine. (ix) Hydraulic and electrical actuating system of components. (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. (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. SB-115 (10/26/83) -- Deflation Panel Pull Forces . full text search results Appliances, and Test apparatus necessary to assure completion of the propeller or disconnection of flight controls sb-115 ( )... Covered parts such as cleaning and greasing Requirements ( AW ) book s... ( where practicable ) improper operation, insecure mounting, marking, and insecurity of attachment of parts. 17 ) Replacing bulbs, reflectors, and related parts - for defects! ) hydraulic and electrical actuating System of components according to the CFR security of.... 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