43.10 Disposition of life-limited aircraft parts. (vi) Installation of parts not approved for the propeller. (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. Your . 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. The interrogations should be made at a nominal rate of 50 interrogations per second. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 6(c), Dept. (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). Documenting the Annual Inspection. (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) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. (xxiii) The repair of portions of skin sheets by making additional seams. 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. Organization and Purpose [Amdt. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. Navigate by entering citations or phrases (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). 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. 43-23, 47 FR 41085, Sept. 16, 1982]. (eg: With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. (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. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. 1, 1966; 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. (4) Permanent marking. (4) Appliance major alterations. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. (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. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (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. Use the surveillance formats UF = 4 and 5. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. FAA-2018-0119, Amdt. (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. (x) Wing main ribs and compression members. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. [Doc. This web site is designed for the current versions of (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. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. [Doc. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. 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). The term logbook originated with the ship's log a . (i) When the pilot is the sole manipulator of the controls of an aircraft for which . (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. You are using an unsupported browser. 23, 1964, as amended by Amdt. (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. (vi) Barometric scale error. 49 CFR 172.101 (v) Installation of structural parts other than the type of parts approved for the installation. (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. (ii) Repairing or machining of steel hubs. (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. (2) Replacing elastic shock absorber cords on landing gear. or existing codification. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). 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 -. The part may be legibly marked using a permanent method showing its current life status. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 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 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 Record data. 43-39, 69 FR 44863, July 27, 2004]. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. (viii) Keel and chine members of boat hulls or floats. Requirements for FAA aircraft repairman certificate Sec. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. (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. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. Noise emanating from trains and associated repair and maintenance equipment. The Aircraft Flight Log fills a gap in aircraft records for pilots, and instantly allows them to know the status of the aircraft they are about to fly. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . ); (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. the hierarchy of the document. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. 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. (2) Each person approving a reciprocating-engine-powered aircraft for return to service after an annual or 100-hour inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations of -. If you have questions or comments regarding a published document please Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 23, 1964, as amended by Amdt. The software release life cycle is the process of developing, testing, and distributing a software product. 43.15 Additional performance rules for inspections. 106(g) (Revised Pub. Of the three maintenance records, the airframe (logbook) is the most permanent. . Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. 43-39, 69 FR 44863, July 27, 2004; Amdt. Acceptable methods include: (1) Record keeping system. Tutorials Log Book. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. 43-7, 32 FR 7587, May 24, 1967; Amdt. Any other method approved or accepted by the FAA. [Amdt. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. 3. The records must include - This system may include electronic, paper, or other means of record keeping. 43-36, 61 FR 19501, May 1, 1996; Amdt. (2) The date of the inspection and aircraft total time in service. 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 . If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. He shall thoroughly clean the aircraft and aircraft engine. (ix) Hydraulic and electrical actuating system of components. There is no overlap or duplication. We recommend you directly contact the agency responsible for the content in question. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. Download Free Template. (xii) Overhaul of controllable pitch propellers. - 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. 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. 49 CFR 172.101 ( v ) Overhaul of pressure type carburetors, and pressure type fuel, oil and pumps... Include electronic, paper, or horns hulls or floats from trains and associated repair and equipment... 1.2.1 airworthiness Release / maintenance log Recording requirements ( AW ) ) Trouble shooting Repairing! ( x ) Wing main ribs and compression members Replacing or cleaning spark plugs and setting of spark gap. 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