Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). The inspection must be recorded in the aircraft records. SB-114 (7/15/83) -- Pilot Light Valve . (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. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. 27, 2001; Amdt. 1, 1966; Amdt. If you work for a Federal agency, use this drafting 43-50, 83 FR 9170, Mar. (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 -. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. 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. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. 21. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. Replacing prefabricated fuel lines. (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 interrogations should be made at a nominal rate of 50 interrogations per second. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. 43-36, 61 FR 19501, May 1, 1996; Amdt. (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. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. Use this checklist to: (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (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. will bring you to those results. 106(g) (Revised Pub. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (v) Installation of propeller de-icing system. Test Okta app access on pilot members. Learn more about the eCFR, its status, and the editorial process. of Transportation Act (49 U.S.C. here. Let's take a look. Title 14 was last amended 2/27/2023. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. e. Section 91.417(a)(1)(ii). 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. The error at all test points must not exceed the tolerances specified in Table I. The part may be legibly marked using a non-permanent method showing its current life status. Acceptable methods include: (1) Record keeping system. (3) Non-permanent marking. 23, 1964, as amended by Amdt. (vi) Installation of parts not approved for the propeller. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. 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. (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. (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. Noise emanating from trains and associated repair and maintenance equipment. 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 At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. 43-7, 32 FR 7587, May 24, 1967; Amdt. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (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. developer resources. (18) Replacing wheels and skis where no weight and balance computation is involved. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). 43.15 Additional performance rules for inspections. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 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: (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. If you have questions for the Agency that issued the current document please contact the agency directly. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (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 40703, Nov. 7, 1986; Amdt. (5) Flight and engine controls - for improper installation and improper operation. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (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) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. 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. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (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. (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. 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. 27, 2001; Amdt. 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? Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. full text search results How to Use. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. We recommend you directly contact the agency responsible for the content in question. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. 43-43, 74 FR 53394, Oct. 16, 2009]. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. 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. (ii) Monocoque or semimonocoque wings or control surfaces. (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. (3) Propeller major repairs. (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. 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. (7) Other methods. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [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. 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). (21) Replacing any hose connection except hydraulic connections. 43-49, 81 FR 96700, Dec. 30, 2016]. learn more about the process here. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. 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. The date of completion. (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)). 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. (2) The date of the inspection and aircraft total time in service. book to meet the regulatory requirements. (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. 43-52, 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 -. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. 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). ) Floats and skis - for improper installation and improper operation 30, 2016 ] for.... To: ( 1 ) 2016 ] ) ; and 14 CFR 11.45 ), [.! 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