FAA-2021-0237; Amdt. 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. The error at all test points must not exceed the tolerances specified in Table I. 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. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. (ix) Hydraulic and electrical actuating system of components. The signature constitutes the approval for return to service only for the work performed. (iii) Installation of an accessory which is not approved for the engine. Navigate by entering citations or phrases (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 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: Replacing and servicing batteries. Okta Mobile for end users. (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. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. (23) Cleaning or replacing fuel and oil strainers or filter elements. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. Requirements for aircraft maintenance log book entries following an annual inspection can be tricky and confusing not only for the mechanic but for the owner/operator, especially where airworthiness discrepancies have been found by the airframe and powerplant mechanic (A&P) with inspection authorization (IA). Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. (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. 27, 2001; Amdt. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . Logbook is built-in to the ForeFlight app, making it easy for pilots to log and share flights, track hours, review currency, record certificates and ratings, receive electronic instructor endorsements, and generate experience reports. A tag or other record may be attached to the part. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. Please do not provide confidential The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). 43-4, 31 FR 5249, Apr. (6) Engine controls - for defects, improper travel, and improper safetying. (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. (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. 22. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). The software release life cycle is the process of developing, testing, and distributing a software product. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. We recommend you directly contact the agency responsible for the content in question. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. 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). Note the extra lines for adding additional categories. (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. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (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. 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. 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. 91.409 (a) requires that an aircraft must undergo an annual inspection every 12 calendar months or sooner in order for that aircraft to be airworthy. 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. (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. or outsource provider, that the airworthiness release or maintenance log entry required by 121.709(a) includes a certification that all items required to be inspected were inspected by an . (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. (c) Disposition of parts removed from type-certificated products. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. 43-37, 66 FR 21066, Apr. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 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. - 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 life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. FAA-2015-1621, Amdt. (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. 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. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 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. (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). Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 43-37, 66 FR 21066, 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. (3) Non-permanent marking. Download Free Template. 23, 1964, as amended by Amdt. is available with paragraph structure matching the official CFR will bring you directly to the content. (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (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. 43-7, 32 FR 7587, May 24, 1967; Amdt. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (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. 1993, 29 FR 5451, Apr. (c) Preventive maintenance. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. 43-36, 61 FR 19501, May 1, 1996; Amdt. [Amdt. 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. (2) Powerplant major alterations. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. 7572; 49 U.S.C. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. 43-37, 66 FR 21066, Apr. 65.101 Eligibility requirements: General. 1993, 29 FR 5451, Apr. You can (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (7) Other methods. 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 Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." 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. (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 -. Title 14 was last amended 2/27/2023. Where To Go For Honda Maintenance Although . The official, published CFR, is updated annually and available below under Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. (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 records must include - (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (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. 23, 1964, as amended by Amdt. Docket No. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). 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. Replacing any hose connection except hydraulic connections. (3) Propeller major alterations. (1) Airframe major alterations. 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). Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. No. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. 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. (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. (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. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. 43-37, 66 FR 21066, Apr. No. These words show that the FAA intends that a logbook, or equivalent document, and aircraft maintenance records must exist in some format for each TC aircraft. Tutorials Log Book. 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 . (b) Temporary removal of parts from type-certificated products. Your . (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. 1993, 29 FR 5451, Apr. (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. 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 -. Let's take a look. Be used when maintenance records are available of aircraft, nuclear plants, particle accelerators, and 601 through of. Will bring you directly to the content in question a software product phrases xxviii! 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