Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). Replacing any hose connection except hydraulic connections. will bring you to those results. 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 -. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Download Free Template. 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. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. 43-37, 66 FR 21066, Apr. 91.417 Maintenance records. 24. (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. (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. No. (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. 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. 23. (Secs. (5) Flexible vibration dampeners - for poor condition and deterioration. (1) Airframe major repairs. Examples of Log Entries . (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. 43-39, 69 FR 44863, July 27, 2004; Amdt. (6) Mutilation. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (2) Seats and safety belts - for poor condition and apparent defects. 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 . Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. 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. (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. Replacing or cleaning spark plugs and setting of spark plug gap clearance. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. For miscellaneous technical amendments to this part 43, see Amdt. Any other method approved or accepted by the FAA. book to meet the regulatory requirements. 4, 1987, as amended by Amdt. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. There is no overlap or duplication. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (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. The eCFR is displayed with paragraphs split and indented to follow No. 3, 1966, and Amdt. (xiv) Members of the side truss, horizontal truss, or bulkheads. 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. (a) Maintenance record entries. 27, 2001; Amdt. (v) Case leak. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. Use the correct address and at least two incorrect addresses. (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. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (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) -. (1) Airframe major alterations. 43-31, 54 FR 34330, Aug. 18, 1989]. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. 6(c), Dept. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. Background and more details are available in the AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . 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. [Doc. (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. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (2) The date of the inspection and aircraft total time in service. (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. Title 14 was last amended 2/27/2023. (iv) Installation of a propeller governor or feathering system. 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 (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (b) Applicability. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. 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 The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. 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: (1) A description (or reference to data acceptable to the Administrator) of work performed. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 1993, 29 FR 5451, Apr. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 1993, 29 FR 5451, Apr. [Doc. 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. Organization and Purpose (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). (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. [Amdt. This content is from the eCFR and may include recent changes applied to the CFR. 1993, 29 FR 5451, Apr. 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. The error at all test points must not exceed the tolerances specified in Table I. (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. 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. 43-37, 66 FR 21066, Apr. the requirements of parts 91K, 121, 125, 133, 135, and 145. SB-114 (7/15/83) -- Pilot Light Valve . 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. How to Use. FAA-2021-0237; Amdt. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Determine type of log book (s) There are many different types of log books. (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. (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. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. [Amdt. (23) Cleaning or replacing fuel and oil strainers or filter elements. (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. full text search results (2) Shock absorbing devices - for improper oleo fluid level. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. Let's take a look. 43-23, 47 FR 41085, Sept. 16, 1982]. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. (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. FAR 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). Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. (2) Tag or record attached to part. (iii) After effect. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. 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. (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) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. 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