43-23, 47 FR 41084, Sept. 16, 1982; Amdt. The tests in (e) through (j) apply only to Mode S transponders. 43.7 Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (a) Maintenance record entries. 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. 1993, 29 FR 5451, Apr. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. 1354, 1355, and 1421 through 1430) and sec. Pressing enter in the search box 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. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. 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. 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. (23) Cleaning or replacing fuel and oil strainers or filter elements. 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. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (xiv) The repair or replacement of internal elements of blades. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. 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 -. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (4) Appliance major alterations. (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. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. Title 14 was last amended 2/27/2023. If your org uses Okta AD agent version 3. (a) Maintenance record entries. (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. 6(c), Dept. (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. Discipline Log Book. The most important step is to record data consistently. (3) Bonding and shielding - for improper installation and poor condition. No. ); (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. (3) Propeller major repairs. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). This applies to owner maintenance as well. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. You are using an unsupported browser. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. (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. 23, 1964, as amended by Amdt. (ix) Hydraulic and electrical actuating system of components. 27, 2001; Amdt. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. 25. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. 23, 1964, unless otherwise noted. 27, 2001; Amdt. The world class support of Liveops and unparalleled access to world-renowned clients. Docket No. [Amdt. 43.12 Maintenance records: Falsification, reproduction, or alteration. (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. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. As you know, 14 C.F.R. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. (xv) Main seat support braces and brackets. This system may include electronic, paper, or other means of record keeping. The life status must be updated each time the part is removed from a type certificated product. (4) Appliance major repairs. [Doc. (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. Navigate by entering citations or phrases "Published Edition". here. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. 1993, 29 FR 5451, Apr. It is not an official legal edition of the CFR. (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. You didn't ask that though. 43-31, 54 FR 34330, Aug. 18, 1989]. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). Download Free Template. through logbooks usually kept in the maintenance hangar. (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. 101, 610, 72 Stat. 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. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. Test Okta app access on pilot members. 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