The term logbook originated with the ship's log a . (b) Temporary removal of parts from type-certificated products. (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. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. This content is from the eCFR and is authoritative but unofficial. The world class support of Liveops and unparalleled access to world-renowned clients. [Amdt. (4) Retracting and locking mechanism - for improper operation. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. 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. 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. (eg: 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. (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)). Replacing prefabricated fuel lines. 1993, 29 FR 5451, Apr. 27, 2001; Amdt. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. And that's. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. SB-114 (7/15/83) -- Pilot Light Valve . (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. 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. 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. 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. will also bring you to search results. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. 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. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (3) Non-permanent marking. (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. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. 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. This inspection will be recorded in the aircraft maintenance records. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (7) Other methods. 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. here. (i) Scale error. 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). 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (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) 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 -. [Amdt. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (10) Floats and skis - for insecure attachment and obvious or apparent defects. The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. 43-39, 69 FR 44863, July 27, 2004; Amdt. (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. Title 14 was last amended 2/27/2023. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. 43-39, 69 FR 44863, July 27, 2004]. 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. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (3) Anti-icing devices - for improper operations and obvious defects. (xiv) Members of the side truss, horizontal truss, or bulkheads. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (2) Bolts - for improper torquing and lack of safetying. Examples of Log Entries . Record data. 43-37, 66 FR 21066, Apr. He shall thoroughly clean the aircraft and aircraft engine. (5) Flexible vibration dampeners - for poor condition and deterioration. Pre-alpha refers to the early stages of development, when the software is . (iv) Installation of a propeller governor or feathering system. Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. The date the work was completed. (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. (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. FAA-2015-1621, Amdt. [Amdt. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). 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. (2) Studs and nuts - for improper torquing and obvious defects. You didn't ask that though. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (6) Electrical system - for chafing and improper operation of switches. The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (6) Batteries - for improper installation and improper charge. 1993, 29 FR 5451, Apr. ); (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. 23, 1964, as amended by Amdt. 1 CFR 1.1 Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 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 (b) Applicability. (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. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. 43.10 Disposition of life-limited aircraft parts. Where To Go For Honda Maintenance Although . of Transportation Act (49 U.S.C. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (xiv) The repair or replacement of internal elements of blades. (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. No. 23, 1964, as amended by Amdt. 43-27, 52 FR 17277, May 6, 1987; Amdt. (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. 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. (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. (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. (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. 43.2 Records of overhaul and rebuilding. (e) Logging pilot-in-command flight time. 23, 1964, as amended by Amdt. 43-28, 52 FR 20028, June 16, 1987; Amdt. (4) Appliance major alterations. 24. The software release life cycle is the process of developing, testing, and distributing a software product. SB-115 (10/26/83) -- Deflation Panel Pull Forces . 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. This contact form is only for website help or website suggestions. (8) Exhaust stacks - for cracks, defects, and improper attachment. (x) Wing main ribs and compression members. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. Determine type of log book (s) There are many different types of log books. The Aircraft Flight Log fills a gap in aircraft records for pilots, and instantly allows them to know the status of the aircraft they are about to fly. 1993, 29 FR 5451, Apr. 27, 2001; Amdt. Requirements for FAA aircraft repairman certificate Sec. (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. 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