(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. (2) Powerplant major alterations. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. (2) Seats and safety belts - for poor condition and apparent defects. 23, 1964, as amended by Amdt. Let's take a look. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. 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. (a) Definitions used in this section. (ii) Monocoque or semimonocoque wings or control surfaces. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 1-866-TELL-FAA (1-866-835-5322) Readers & Viewers PDF Powerpoint Zip Word Excel (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. For the purposes of this section the following definitions apply. And that's. (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. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (xiv) The repair or replacement of internal elements of blades. is available with paragraph structure matching the official CFR 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. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. [Doc. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. 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. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. 3, 1966, and Amdt. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (6) Engine controls - for defects, improper travel, and improper safetying. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 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. . (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. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. (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. Organization and Purpose (e) Logging pilot-in-command flight time. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (v) Installation of propeller de-icing system. 1/1.1 (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. (7) Wheels - for cracks, defects, and condition of bearings. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. 23, 1964, as amended by Amdt. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (v) Replacement of outer laminations on fixed pitch wood propellers. 43-41, 72 FR 53680, Sept. 20, 2007; Doc. 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. 5, 2018]. (3) The main rotor and center section (or the equivalent area). 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. will bring you directly to the content. (ix) Hydraulic and electrical actuating system of components. Determine type of log book (s) There are many different types of log books. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. (6) Mutilation. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. FAA-2015-1621, Amdt. In that case, you may need to nd a mechanic willing to drive or y to where (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. 43-36, 61 FR 19501, May 1, 1996; Amdt. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. 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? (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (xxi) Repairs involving the substitution of material. No. (iii) Installation of an accessory which is not approved for the engine. Pertinent details of the repair are on file at this repair station under Order No. 65.101 Eligibility requirements: General. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. The software release life cycle is the process of developing, testing, and distributing a software product. 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 . (eg: The part may be legibly marked using a permanent method showing its current life status. (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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Use this checklist to: 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (2) The date of completion of the work performed. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (2) Tag or record attached to part. 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 -. - 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. 4, 1987, as amended by Amdt. No. 1993, 29 FR 5451, Apr. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. Section 43.11(a) requires that the maintenance entry be made in the "maintenance record of that equipment." (iii) Performed without the use of tools and/or special equipment. As a Fri, 05/01/2015 - 12:00. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 27, 2001; Amdt. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (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). (ii) Repairing or machining of steel hubs. (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. (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. Aircraft Inspection and Repair - Federal Aviation . FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. Note the extra lines for adding additional categories. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (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). Choosing an item from (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). Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. (2) Replacing elastic shock absorber cords on landing gear. (xxiii) The repair of portions of skin sheets by making additional seams. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Enhanced content is provided to the user to provide additional context. (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. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 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. Discipline Log Book. A tag or other record may be attached to the part. (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. 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. 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. 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. (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. 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. (a) Maintenance record entries. Examples of Log Entries . 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 . If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (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. 23. Requirements for FAA aircraft repairman certificate Sec. (4) Permanent marking. Pre-alpha refers to the early stages of development, when the software is . 1354, 1355, and 1421 through 1430) and sec. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (29) Removing, checking, and replacing magnetic chip detectors. 1 CFR 1.1 This contact form is only for website help or website suggestions. (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. here. (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. Table of contents from a loose-leaf binder for maintenance records. (8) Exhaust stacks - for cracks, defects, and improper attachment. 43-37, 66 FR 21066, Apr. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. There is no overlap or duplication. (2) The date of the inspection and aircraft total time in service. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. 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