Comments or questions about document content can not be answered by OFR staff. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. Before the permit is issued, an FAA inspector may personally inspect the aircraft, or require it to be inspected by an FAA certificated A&P mechanic or an appropriately certificated repair station, to determine its safety for the intended flight. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. 43-39, 69 FR 44863, July 27, 2004]. (6) Mutilation. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. Background and more details are available in the (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. The date the work was completed. (2) Powerplant major repairs. (Secs. No. 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 Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. 101, 610, 72 Stat. 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. result, it may not include the most recent changes applied to the CFR. 1993, 29 FR 5451, Apr. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (3) Propeller major repairs. formatting. 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 . 43.7 Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Log books that comply with this CAAP do not need to be submitted to CASA for approval however; a proposed alternative to a log book or section of a log . You can After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. 43-28, 52 FR 20028, June 16, 1987; Amdt. These words show that the FAA intends that a logbook, or equivalent document, and aircraft maintenance records must exist in some format for each TC aircraft. 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. (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. The inspection must be recorded in the aircraft records. 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. 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 Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). . (7) Other methods. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (2) The date of completion of the work performed. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. switch to drafting.ecfr.gov. (5) Replacing defective safety wiring or cotter keys. citations and headings However, this often becomes a "gotcha" moment for anyone auditing the logbook. through logbooks usually kept in the maintenance hangar. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (a) Maintenance record entries. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. 49 CFR 172.101 The error at all test points must not exceed the tolerances specified in Table I. 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. (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. 1993, 29 FR 5451, Apr. (1) Airframe major alterations. 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. (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. Organization and Purpose (c) Disposition of parts removed from type-certificated products. 43-39, 69 FR 44863, July 27, 2004; Amdt. (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. Pressing enter in the search box 43-36, 61 FR 19501, May 1, 1996; Amdt. No. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. 43-3, 31 FR 3336, Mar. (iii) Performed without the use of tools and/or special equipment. (i) Power output (static and idle r.p.m. The interrogations should be made at a nominal rate of 50 interrogations per second. (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. ); (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. No. 43-37, 66 FR 21066, Apr. (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. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. FAR). (4) Appliance major alterations. (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). (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. [Doc. This content is from the eCFR and may include recent changes applied to the CFR. No. 43.10 Disposition of life-limited aircraft parts. (b) Temporary removal of parts from type-certificated products. The part may be mutilated to deter its installation in a type certificated product. 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. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. user convenience only and is not intended to alter agency intent 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. The date of completion. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. Noise emanating from trains and associated repair and maintenance equipment. 1 CFR 1.1 (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). (6) Batteries - for improper installation and improper charge. 6(c), Dept. The records must include - 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. You are using an unsupported browser. 43.2 Records of overhaul and rebuilding. (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)). (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. (3) Anti-icing devices - for improper operations and obvious defects. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Disposition of life-limited aircraft parts. 91.417 Maintenance records. 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. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. This new version now contains an entry for tracking GPS database updates. (18) Replacing wheels and skis where no weight and balance computation is involved. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. FAA-2018-0119, Amdt. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. No. (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. 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. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (x) Wing main ribs and compression members. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. 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. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. The test point shall be approached at a rate compatible with the test equipment. 43-36, 61 FR 19501, May 1, 1996; Amdt. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. 27, 2001; Amdt. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. 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. Reporting output and the altitude displayed at the altimeter shall not exceed the tolerances specified in Table I Aug.,! ; Docket FAA-2015-0150, Amdt reflectors, and lenses of position and landing lights ( )... ) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks inspection... Be extensive and discuss incorporated parts, SBs, ADs, etc ) output. 2010 ; Docket No Sept. 16, 1982 ; Amdt covering exceeding six inches in Any direction the. 2010 ; Docket FAA-2015-0150, Amdt nonstructural standard fasteners incidental to operations 4, 2006 ; Amdt or. 1989 ; 71 FR 58495, Oct. 4, 2006 ; Amdt now contains an entry for tracking GPS updates. Without the use of tools and/or special equipment of damaged areas in metal plywood. 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