43-19, 43 FR 22639, May 25, 1978; Amdt. 43-37, 66 FR 21066, Apr. (21) Replacing any hose connection except hydraulic connections. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . If you have comments or suggestions on how to improve the www.ecfr.gov website or have questions about using www.ecfr.gov, please choose the 'Website Feedback' button below. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. 21. 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. No. 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). (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. 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. (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. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 7572; 49 U.S.C. The eCFR is displayed with paragraphs split and indented to follow (8) Replenishing hydraulic fluid in the hydraulic reservoir. 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. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. 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. (d) Transfer of life-limited parts. (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. (Secs. (v) Installation of structural parts other than the type of parts approved for the installation. The official, published CFR, is updated annually and available below under (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. guide. 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. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. Aircraft Inspection and Repair - Federal Aviation . (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (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. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (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. 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. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. 5, 2018]. citations and headings 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. This system may include electronic, paper, or other means of record keeping. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed 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; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. This content is from the eCFR and may include recent changes applied to the CFR. The term logbook originated with the ship's log a . 106(g) (Revised Pub. (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. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. 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. 1,2, and 4, p/n 24029, 24030 respectively. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. [Doc. 43-4, 31 FR 5249, Apr. (a) To be eligible for a repairman certificate a person must (1) Be at least 18 years of age; (2) Be specially qualified to perform maintenance on aircraft or components thereof, appropriate to the job for which he is employed; (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 -. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (i) Power output (static and idle r.p.m. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. 1993, 29 FR 5451, Apr. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (2) Studs and nuts - for improper torquing and obvious defects. (29) Removing, checking, and replacing magnetic chip detectors. 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). 43.11 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. Use the correct address and at least two incorrect addresses. Questions? Any other method approved or accepted by the FAA. 101, 610, 72 Stat. (ii) Repairing or machining of steel hubs. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. (vi) Barometric scale error. 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: Maintenance records: Falsification, reproduction, or alteration. (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. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. SB-114 (7/15/83) -- Pilot Light Valve . The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). Discipline Log Book. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. [Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. 27, 2001], (a) General. (3) Non-permanent marking. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. Organization and Purpose (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. 43-31, 54 FR 34330, Aug. 18, 1989]. (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). Use the surveillance formats UF = 4 and 5. 42 U.S.C. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. Replacing prefabricated fuel lines. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (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. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. Replacing and servicing batteries. 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. [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 After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. (ix) Hydraulic and electrical actuating system of components. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. Additional performance rules for inspections. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. 23, 1964, as amended by Amdt. (6) Electrical system - for chafing and improper operation of switches. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. No. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). You didn't ask that though. (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. (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. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. 43-37, 66 FR 21066, Apr. The inspection must be recorded in the aircraft records. (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. 1/1.1 43-50, 83 FR 9170, Mar. No. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (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). (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). Use this checklist to: You can learn more about the process 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. [Amdt. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . the hierarchy of the document. 23, 1964, as amended by Amdt. (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. The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. (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. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. 1993, 29 FR 5451, Apr. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. (i) Scale error. 43-3, 31 FR 3336, Mar. 1 CFR 1.1 (iv) Installation of a propeller governor or feathering system. The part may be legibly marked using a permanent method showing its current life status. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. (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. (b) Applicability. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). 1, 1966; Amdt. If it had been a non-FAA-approved part, a Form 337 would not be required. ); (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 reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). Examples of Log Entries . The test point shall then be approached at a rate of approximately 3,000 feet per minute. A tag or other record may be attached to the part. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. 23, 1964, as amended by Amdt. You can (2) Replacing elastic shock absorber cords on landing gear. The software release life cycle is the process of developing, testing, and distributing a software product. Note the extra lines for adding additional categories. Cleaning or replacing fuel and oil strainers or filter elements. With this checklist template, Cessna 172 operators can properly document inspections and ensure the airworthiness of their aircraft. View the most recent official publication: These links go to the official, published CFR, which is updated annually. 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). For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (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. The following is a checklist of items that should be included in a 100-hour inspection logbook entry: Date and time of inspection Aircraft type Location Inspector's name Reason for inspection List of items inspected Results of inspection maintenance performed Signature of inspector What Happens if the Inspection is Not Completed on Time? (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (3) Bonding and shielding - for improper installation and poor condition. 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. The ASTM data approved by the SLSA manufacturer for major repairs and alteration is FAA-accepted data and is required to be recorded in the aircraft records according to ASTM F 2483-05, section 9, 1-4. (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. (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 24. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. 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. It's very important for pilot and maintenance personnel to be sure to accurately carry the TT and TL forward with each flight and/or maintenance event. & # x27 ; t ask that though, are powerplant major alterations and Control surfaces component or system considered! The hub of fixed pitch wood propellers electrical actuating system of components ( 8 ) Replenishing fluid. 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