43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. 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. (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. ( 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. (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. 43-39, 69 FR 44863, July 27, 2004; Amdt. No. 43-4, 31 FR 5249, Apr. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. (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. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. Fri, 05/01/2015 - 12:00. (ii) Hysteresis. 43-7, 32 FR 7587, May 24, 1967; Amdt. will also bring you to search results. 1993, 29 FR 5451, Apr. The world class support of Liveops and unparalleled access to world-renowned clients. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. (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. FAR). 23, 1964, unless otherwise noted. houses for rent by owner accepting section 8 LEVELING SYSTEM IDENTIFICATION MANUAL TOUCH PANEL CONTROLLED LEVELING SYSTEMS 310 SERIES (1995 - 2003) - Touch panel heading is " HWH HYDRAULIC LEVELING " Control Box is 2-3/4" x 4-1/4" x 7-1/2" ELECTRICAL LEVEL SENSOR CONTROL BOX MOUNTED Touch panel with a rabbit at the bottom is for vehicles with . The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (ii) Repairing or machining of steel hubs. Disposition of life-limited aircraft parts. Tutorials Log Book. 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. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. Replacing and servicing batteries. (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. e. Section 91.417(a)(1)(ii). (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 -. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. He shall thoroughly clean the aircraft and aircraft engine. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. 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. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (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)). FAA-2021-0237; Amdt. 1354, 1421 through 1430 and 1502); (49 U.S.C. 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. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. developer resources. 43-39, 69 FR 44863, July 27, 2004; Amdt. 24. (xiv) The repair or replacement of internal elements of blades. 43-37, 66 FR 21066, Apr. In that case, you may need to nd a mechanic willing to drive or y to where FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. [Doc. Documenting the Annual Inspection. Aircraft Radio Maintenance Log Book Form 944 . (3) Windows and windshields - for deterioration and breakage. (8) Replenishing hydraulic fluid in the hydraulic reservoir. 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. (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. site when drafting amendatory language for Federal regulations: No. View the most recent official publication: These links go to the official, published CFR, which is updated annually. (3) Any alteration, for fraudulent purpose, of any record or report under this part. [Amdt. (e) Logging pilot-in-command flight time. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. . formatting. Major Alterations, Major Repairs, and Preventive Maintenance, Recording of Major Repairs and Major Alterations, Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. The most important step is to record data consistently. The test point shall be approached at a rate compatible with the test equipment. (2) Powerplant major alterations. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. - Federal Aviation Administration, Department of Transportation, https://www.ecfr.gov/current/title-14/chapter-I/subchapter-C/part-43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration. (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. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. (a) Definitions. The part may be legibly marked using a non-permanent method showing its current life status. 43-36, 61 FR 19501, May 1, 1996; Amdt. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (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. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Background and more details are available in the 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. [Doc. (v) Replacement of outer laminations on fixed pitch wood propellers. 43-37, 66 FR 21066, Apr. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. (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. (a) Except for work performed in accordance with 91.411 and 91.413, each registered owner or operator shall keep the following records for the periods specified in paragraph (b) of this section . (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. Examples of Log Entries . As you know, 14 C.F.R. 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. The aircraft owner is the one who applies for the permit, using FAA form 8130-6, which is actually an application for a U.S. airworthiness certificate. (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. Replacing or cleaning spark plugs and setting of spark plug gap clearance. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. 27, 2001], (a) General. [Doc. (9) Accessories - for apparent defects in security of mounting. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (xiv) Members of the side truss, horizontal truss, or bulkheads. 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. (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; (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. Without well-trained quality assurance personnel, pilots must take responsibility for diving into the logbook (s) and flight packs to make sure the aircraft is ready and safe to fly. 106(g) (Revised Pub. FAA acceptance is also required for certificate holders who use electronic records, and the electronic signatures associated with those records, to satisfy the requirements of parts 141, 142, and 147. 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. 1993, 29 FR 5451, Apr. 43-3, 31 FR 3336, Mar. (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. 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. (b) Temporary removal of parts from type-certificated products. (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). A mechanic can be the one to solicit the ferry permit on the owner's behalf if the owner supplies a signed letter of authorization. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. This content is from the eCFR and may include recent changes applied to the CFR. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. 23, 1964, as amended by Amdt. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 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. 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. 43-45, 77 FR 71096, Nov. 29, 2012], No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (5) Flight and engine controls - for improper installation and improper operation. (3) Propeller major alterations. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). (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. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. (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. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. (iii) Rewinding the field coil of an electrical accessory. through logbooks usually kept in the maintenance hangar. (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. As a 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. (a) Definitions used in this section. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. 1354, 1355, and 1421 through 1430) and sec. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. This web site is designed for the current versions of If your org uses Okta AD agent version 3. (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). Title 14 was last amended 2/27/2023. 101, 610, 72 Stat. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. No. (6) Engine controls - for defects, improper travel, and improper safetying. (2) The date of the inspection and aircraft total time in service. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. If it had been a non-FAA-approved part, a Form 337 would not be required. If you have questions or comments regarding a published document please 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. 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 . Each time the part is removed from a type certificated product, the record must be updated with the current life status. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. 43-51, 86 FR 4381, Jan. 15, 2021], (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. The records must include - 23. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. Classroom Visitor Log Book. 43-23, 47 FR 41085, Sept. 16, 1982]. Pertinent details of the repair are on file at this repair station under Order No. (6) Batteries - for improper installation and improper charge. Any other method approved or accepted by the FAA. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. information or personal data. The tag or record must include the part number, serial number, and current life status of the part. 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.
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