The software release life cycle is the process of developing, testing, and distributing a software product. 43-7, 32 FR 7587, May 24, 1967; Amdt. (6) Mutilation. A completed copy of that form shall be -. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. [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. (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). (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. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. Tutorials Log Book. Displaying title 14, up to date as of 2/27/2023. Where To Go For Honda Maintenance Although . (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. (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. 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. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. 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: (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. Documenting the Annual Inspection. (vi) Barometric scale error. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (a) Maintenance record entries. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). If you have questions for the Agency that issued the current document please contact the agency directly. 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. (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. (x) Wing main ribs and compression members. 43-39, 69 FR 44863, July 27, 2004; Amdt. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (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. If you have questions or comments regarding a published document please 1993, 29 FR 5451, Apr. 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. (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. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . 23, 1964, unless otherwise noted. 43-3, 31 FR 3336, Mar. Choosing an item from The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. 1993, 29 FR 5451, Apr. (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). (ix) Hydraulic and electrical actuating system of components. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . 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. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. 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 -. A completed copy of that form shall be -. (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. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. 43-36, 61 FR 19501, May 1, 1996; Amdt. This contact form is only for website help or website suggestions. Replacing prefabricated fuel lines. Table of contents from a loose-leaf binder for maintenance records. (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. (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. 43-39, 69 FR 44863, July 27, 2004]. 43-36, 61 FR 19501, May 1, 1996; Amdt. The life status must be updated each time the part is removed from a type certificated product. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. 4, 1987, as amended by Amdt. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). (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 -. 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). (2) Studs and nuts - for improper torquing and obvious defects. 106(g) (Revised Pub. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. 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. (3) Bonding and shielding - for improper installation and poor condition. FAR). The tag or record must include the part number, serial number, and current life status of the part. 43.2 Records of overhaul and rebuilding. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . of Transportation Act (49 U.S.C. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. Aircraft Radio Maintenance Log Book Form 944 . If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. The part may be segregated using methods that deter its installation on a type-certificated product. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. 27, 2001; Amdt. Questions? maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (viii) Keel and chine members of boat hulls or floats. (4) Permanent marking. (eg: (v) Installation of structural parts other than the type of parts approved for the installation. Comments or questions about document content can not be answered by OFR staff. (5) Replacing defective safety wiring or cotter keys. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. 43-36, 61 FR 19501, May 1, 1996; Amdt. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. A logbook (or log book) is a record used to record states, events, or conditions applicable to complex machines or the personnel who operate them. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. citations and headings Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. And that's. (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. No. - 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. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Note the extra lines for adding additional categories. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. (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. (3) The main rotor and center section (or the equivalent area). 91.417 Maintenance records. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. Maintenance records: Falsification, reproduction, or alteration. (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. 23, 1964, as amended by Amdt. FAA-2021-0237; Amdt. FAA-2018-0119, Amdt. 1,2, and 4, p/n 24029, 24030 respectively. If you work for a Federal agency, use this drafting 23, 1964, as amended by Amdt. 43-4, 31 FR 5249, Apr. (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. Please do not provide confidential 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. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. To be considered complete and valid, an electronic record should contain at least the following information: The type of event that took place (e.g., training, maintenance performed, signing of a release, conduct of a flight, etc. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (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. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. FAA acceptance is also required for certificate holders who use electronic records, and the electronic signatures associated with those records, to satisfy the requirements of parts 141, 142, and 147. (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. Process of developing, testing, and current life status of the controls of an aircraft for which and. Component or system is considered to be a detailed inspection faa Policy/Guidance faa! 43-33, 56 FR 57571, Nov. 7, 1986 ; Amdt a agency! Aluminum blades, Google Chrome, Mozilla Firefox, or Alteration, overhaul... 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