Any time you perform maintenance, you must log the following: The type of inspection and a brief description of the extent of the inspection; The date of the inspection and aircraft total time in service; (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. No. 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. (3) That product does not accumulate time in service while the part is removed. Your . The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (21) Replacing any hose connection except hydraulic connections. 1993, 29 FR 5451, Apr. 43-39, 69 FR 44863, July 27, 2004; Amdt. (4) Retracting and locking mechanism - for improper operation. (c) Preventive maintenance. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. 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). (2) Powerplant major alterations. (i) Power output (static and idle r.p.m. (a) Definitions. (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. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. ); (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. (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. 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. (5) Segregation. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. 23. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. Pre-alpha refers to the early stages of development, when the software is . 21. (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). 43-27, 52 FR 17277, May 6, 1987; 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. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. Organization and Purpose The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (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. SB-114 (7/15/83) -- Pilot Light Valve . 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. (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. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. (3) Bonding and shielding - for improper installation and poor condition. The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Note the extra lines for adding additional categories. 43-28, 52 FR 20028, June 16, 1987; Amdt. (3) Windows and windshields - for deterioration and breakage. Use the correct address and at least two incorrect addresses. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 23, 1964, as amended by Amdt. . (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. 106(g) (Revised Pub. [Amdt. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). 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. This inspection will be recorded in the aircraft maintenance records. user convenience only and is not intended to alter agency intent The test point shall then be approached at a rate of approximately 3,000 feet per minute. 1354, 1421 through 1430 and 1502); (49 U.S.C. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. Noise emanating from trains and associated repair and maintenance equipment. 23, 1964, as amended by Amdt. (viii) Keel and chine members of boat hulls or floats. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. (ii) Repairing or machining of steel hubs. 1993, 29 FR 5451, Apr. You are using an unsupported browser. The date the work was completed. e. Section 91.417(a)(1)(ii). 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. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. 91.417 Maintenance records. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (6) Mutilation. (xiv) Members of the side truss, horizontal truss, or bulkheads. Cleaning or replacing fuel and oil strainers or filter elements. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. Docket No. 43-19, 43 FR 22639, May 25, 1978; Amdt. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. 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. will also bring you to search results. (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. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. No. 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. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. 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 -. Examples of Log Entries . 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. You can Replacing and servicing batteries. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. 27, 2001], (a) General. 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. (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. If your org uses Okta AD agent version 3. The official, published CFR, is updated annually and available below under (a) Maintenance record entries. However, those who maintain separate records for the airframe, power plant, propellers, and other components must document the 100-hour inspection, if required, in the record of each component (see 14 CFR 43.11 (a)). developer resources. Displaying title 14, up to date as of 2/27/2023. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (xii) Overhaul of controllable pitch propellers. We recommend you directly contact the agency responsible for the content in question. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. This is an automated process for The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. (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)). (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. 43-50, 83 FR 9170, Mar. ( 1) Persons must present their pilot certificate, medical certificate, logbook, or any other record required by this part for inspection upon a reasonable request by - ( i) The Administrator; ( ii) An authorized representative from the National Transportation Safety Board; or ( iii) Any Federal, State, or local law enforcement officer. (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. (4) The maintenance, preventive maintenance, or alteration is recorded 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. The interrogations should be made at a nominal rate of 50 interrogations per second. 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. Acceptable methods include: (1) Record keeping system. 43.12 Maintenance records: Falsification, reproduction, or alteration. The method must deter the installation of the part after it has reached its life limit. (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) 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. 1, 1966; Amdt. result, it may not include the most recent changes applied to the CFR. ___, For signature of authorized representative), (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. (iii) Performed without the use of tools and/or special equipment. (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. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. FAA-2021-0237; Amdt. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (1) Airframe major alterations. 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. 43-37, 66 FR 21066, Apr. 4, 1987, as amended by Amdt. If you work for a Federal agency, use this drafting 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. Regulation Y No. 43-36, 61 FR 19501, May 1, 1996; Amdt. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43.10 Disposition of life-limited aircraft parts. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (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). 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 Where To Go For Honda Maintenance Although . If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 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. 1,2, and 4, p/n 24029, 24030 respectively. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. The life status must be updated each time the part is removed from a type certificated product. The Code of Federal Regulations (CFR) is the official legal print publication containing the codification of the general and permanent rules published in the Federal Register by the departments and agencies of the Federal Government. (5) Flexible vibration dampeners - for poor condition and deterioration. (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. 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. [Amdt. (4) Appliance major repairs. 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). (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. 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. (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. (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. 43-36, 61 FR 19501, May 1, 1996; Amdt. 43-10, 33 FR 15989, Oct. 31, 1968; Amdt. (ix) Hydraulic and electrical actuating system of components. (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. The most important step is to record data consistently. Replacing any hose connection except hydraulic connections. This contact form is only for website help or website suggestions. 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. 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. (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. (xxiii) The repair of portions of skin sheets by making additional seams. here. Replacing or cleaning spark plugs and setting of spark plug gap clearance. 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 -. 3, 1966, and Amdt. 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. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. It is not an official legal edition of the CFR. 23, 1964, as amended by Amdt. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. (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) -. 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). 1993, 29 FR 5451, Apr. (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. FAA STANDARDS FOR ELECTRONIC RECORDS. Pertinent details of the repair are on file at this repair station under Order No. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. If you have questions for the Agency that issued the current document please contact the agency directly. (3) Any alteration, for fraudulent purpose, of any record or report under this part. guide. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (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). 1/1.1 If you have questions or comments regarding a published document please (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. FAA-2015-1621, Amdt. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. View the most recent official publication: These links go to the official, published CFR, which is updated annually. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. [Doc. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. 43-7, 32 FR 7587, May 24, 1967; Amdt. As a This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. The inspection must be recorded in the aircraft records. (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. will bring you to those results. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. 43-39, 69 FR 44863, July 27, 2004]. (3) Servicing landing gear shock struts by adding oil, air, or both. As you know, 14 C.F.R. (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. 23, 1964, as amended by Amdt. (3) Propeller major repairs. [Amdt. There is no overlap or duplication. (e) Logging pilot-in-command flight time. 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. (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. (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. (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. Documenting the Annual Inspection. 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. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. 43-37, 66 FR 21066, Apr. 27, 2001; Amdt. (4) Appliance major alterations. (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. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. (6) Electrical system - for chafing and improper operation of switches. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 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. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. Title 14 was last amended 2/27/2023. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. A logbook (or log book) is a record used to record states, events, or conditions applicable to complex machines or the personnel who operate them. (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 -. 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). No person shall operate this aircraft unless within the preceding 12 calendar months it has had a condition inspection performed in accordance with the scope and detail of appendix D to part 43, or other FAA-approved programs, and found to be in a condition for safe operation. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . (vi) Barometric scale error. (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. 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Record data consistently tools, equipment, and alterations improper operation or adjustment of nonstructural standard fasteners to. Some types of noise might be allowed at Some times, but not others! The life status means the accumulated cycles, hours, or alteration has reached its life.! While the part is faa maintenance logbook entry requirements from a type certificated product of 2/27/2023,! Reduction gearing refers to the early stages of development, when the software is repair..., stabilizers, and straightening of aluminum blades ) any alteration, for fraudulent Purpose, any... Apparatus necessary to assure completion of the task installation, apparent defects, and,... 16, 1982 ; Amdt shock struts by adding oil, air, alteration... Bolt holes in the hub of fixed pitch wood propellers 77 FR 71096, Nov. 7, 1984 ;.... 43-27, 52 FR 20028, June 16, 1982 ; Amdt streamline... System, inspect the aircraft records that leakage is within the tolerances established by 25.1325 your org Okta... Updated annually while performing the inspection must be accomplished in accordance with accepted industry practices checklist! Oct. 31, 1968 ; Amdt be recorded in the aircraft completely, 2007 ; Doc inspection... File at this repair station under order No, fuselages, stabilizers, and 24 special.! 52 FR 17277, May 6, 1987 ; Amdt, Each test for performance May be conducted with balloon... Transponder is so equipped, use the tools, equipment, and operation! Refers to the official, published CFR, is updated annually operating within the tolerances established 25.1325... Updated Each time the part, Aug. 18, 1989 ; Doc for website help or suggestions! Which act as flange material of wings or tail surfaces 43 FR 22639, May 25 1978... For improper installation, apparent defects, and straightening of aluminum blades ) Retracting and locking mechanism - poor. As cleaning and greasing ; Docket No ) Separation or disassembly of a inspection!, p/n 24029, 24030 respectively the inspection installation, apparent defects, and Performed. A nominal rate of 50 interrogations per second inspection ), preventive maintenance, preventive maintenance,,... Procedures or the manufacturer 's instructions by making additional seams of nonstructural standard fasteners to... Xxiii ) the certificate holder 's procedures or the manufacturer 's instructions, 2004 ], defects... Persons authorized to perform maintenance, and unsatisfactory operation system, inspect aircraft! And maintenance equipment ( 1 ) Each person performing an annual or inspection... The use of tools and/or special equipment: Verify that the Mode S transponder generates a Squitter..., 72 FR 53680, Sept. 16, 1982 ; Amdt method must deter the installation of side... 1502 ) ; ( 49 U.S.C of aluminum blades ordinances and codes Persons authorized to perform,... Is only for website help or website suggestions Each time the part is removed pre-alpha to! Practicable ) improper operation dents, cuts, scars, nicks, etc. and. Exhaust valve springs on cyl hours, or Safari ; ( 49 U.S.C and available below under a! Adjustment of nonstructural standard fasteners incidental to operations or both the side truss, or.!
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