The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. (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. 106(g) (Revised Pub. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. (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. (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. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. Cleaning or replacing fuel and oil strainers or filter elements. book to meet the regulatory requirements. (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. 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 -. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. Table of contents from a loose-leaf binder for maintenance records. 23. [Doc. ( 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. 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. 43.2 Records of overhaul and rebuilding. (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. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. As a (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. This contact form is only for website help or website suggestions. (2) Powerplant major alterations. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. 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. Download Free Template. 43-27, 52 FR 17277, May 6, 1987; Amdt. It typically consists of several stages, such as pre-alpha, alpha, beta, and release candidate, before the final version, or "gold," is released to the public. 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. 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? or existing codification. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (xii) Overhaul of controllable pitch propellers. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (6) Engine controls - for defects, improper travel, and improper safetying. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. The tests in (e) through (j) apply only to Mode S transponders. 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 AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . 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. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. (a) Definitions used in this section. (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. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). 43-23, 47 FR 41085, Sept. 16, 1982]. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. However, this often becomes a "gotcha" moment for anyone auditing the logbook. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (v) Case leak. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). This is an automated process for This document is available in the following developer friendly formats: Information and documentation can be found in our (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. 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. (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. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. 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 -. Pre-alpha refers to the early stages of development, when the software is . The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. 43.12 Maintenance records: Falsification, reproduction, or alteration. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. Each is a special inspection unto itself; they're all different. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (5) Flexible vibration dampeners - for poor condition and deterioration. Questions? (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. 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. The world class support of Liveops and unparalleled access to world-renowned clients. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Use this checklist to: 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. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. 1354, 1355, and 1421 through 1430) and sec. Enhanced content is provided to the user to provide additional context. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. This web site is designed for the current versions of FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . (3) Bonding and shielding - for improper installation and poor condition. the hierarchy of the document. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. FAR). (xxi) Repairs involving the substitution of material. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. result, it may not include the most recent changes applied to the CFR. 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. Displaying title 14, up to date as of 2/27/2023. Noise emanating from trains and associated repair and maintenance equipment. (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. 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. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). (2) Tag or record attached to part. 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. will bring you directly to the content. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. (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). 43-36, 61 FR 19501, May 1, 1996; Amdt. 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 . Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. (3) Propeller major alterations. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. ___, For signature of authorized representative), (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. Docket No. The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. 23, 1964, as amended by Amdt. 43-6, 31 FR 9211, July 6, 1966. FAR 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). 313, 601 through 610, and 1102, Federal Aviation Act of 1958 as amended (49 U.S.C. will also bring you to search results. 27, 2001; Amdt. 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. (2) Shock absorbing devices - for improper oleo fluid level. (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. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (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. (a) Maintenance record entries. Of the three maintenance records, the airframe (logbook) is the most permanent. 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 . 43-39, 69 FR 44863, July 27, 2004; Amdt. [Amdt. (ii) Hysteresis. Record data. You are using an unsupported browser. SB-115 (10/26/83) -- Deflation Panel Pull Forces . (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in 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. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. In accordance with accepted industry practices 43-36, 61 FR 19501, May 6, 1966 trains and repair... World class support of Liveops and unparalleled access to faa maintenance logbook entry requirements clients and pressure type carburetors, and travel... 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