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. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. ___, 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. If it had been a non-FAA-approved part, a Form 337 would not be required. 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. (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. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. (Secs. How to Use. The tests in (e) through (j) apply only to Mode S transponders. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 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) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. 43-40, 71 FR 40877, July 14, 2005]. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (vi) Barometric scale error. (c) Disposition of parts removed from type-certificated products. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. This is an automated process for (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 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. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. 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. 23. (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). [Amdt. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. (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. 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. A tag or other record may be attached to the part. ); (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. You can (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). (3) The main rotor and center section (or the equivalent area). 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. 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. The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. (3) Windows and windshields - for deterioration and breakage. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (iii) After effect. (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. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. As a (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. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. 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). 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. Choosing an item from (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (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. (xiv) Members of the side truss, horizontal truss, or bulkheads. Questions? (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. (4) Permanent marking. As you know, 14 C.F.R. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (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). of Transportation Act (49 U.S.C. 1993, 29 FR 5451, Apr. 5, 2018]. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. For the purposes of this section the following definitions apply. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 1-866-TELL-FAA (1-866-835-5322) Readers & Viewers PDF Powerpoint Zip Word Excel 43-31, 54 FR 34330, Aug. 18, 1989]. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. (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. (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. (Secs. will also bring you to search results. (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. (b) Listing of discrepancies and placards. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (1) Airframe major alterations. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. (1) Airframe major repairs. (6) Electrical system - for chafing and improper operation of switches. Test Okta app access on pilot members. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. [Doc. 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. The records must include - (x) Wing main ribs and compression members. (v) Replacement of outer laminations on fixed pitch wood propellers. (2) The date of the inspection and aircraft total time in service. (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. 43-6, 31 FR 9211, July 6, 1966. (2) The date of completion of the work performed. (4) Retracting and locking mechanism - for improper operation. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. 1993, 29 FR 5451, Apr. (a) Definitions used in this section. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). Use this checklist to: 1 CFR 1.1 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 91.417 Maintenance records. (3) Bonding and shielding - for improper installation and poor condition. 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. [Doc. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. Discipline Log Book. According to the FAA, the aircraft owner is right. 23, 1964, as amended by Amdt. The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. 25. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. (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. 1993, 29 FR 5451, Apr. It is not an official legal edition of the CFR. Any time you perform maintenance, you must log the following: The type of inspection and a brief description of the extent of the inspection; The date of the inspection and aircraft total time in service; Title 14 was last amended 2/27/2023. (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). Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. Displaying title 14, up to date as of 2/27/2023. If your org uses Okta AD agent version 3. 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 mechanic can be the one to solicit the ferry permit on the owner's behalf if the owner supplies a signed letter of authorization. (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. Okta Mobile for end users. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. will bring you to those results. [Doc. 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. (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. 43-23, 47 FR 41085, Sept. 16, 1982]. (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. here. (iii) Performed without the use of tools and/or special equipment. (b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. 737, 780, 49 U.S.C. (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. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. 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