faa maintenance logbook entry requirementsfaa maintenance logbook entry requirements
43-31, 54 FR 34330, Aug. 18, 1989]. 737, 780, 49 U.S.C. Tutorials Log Book. contact the publishing agency. (4) Permanent marking. 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. switch to drafting.ecfr.gov. (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. SB-115 (10/26/83) -- Deflation Panel Pull Forces . (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. Enhanced content is provided to the user to provide additional context. 101, 610, 72 Stat. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. Record data. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. 43-36, 61 FR 19501, May 1, 1996; Amdt. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (6) Batteries - for improper installation and improper charge. Docket No. (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). of Transportation Act (49 U.S.C. (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. site when drafting amendatory language for Federal regulations: (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. 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. Okta Mobile for end users. 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. (6) Engine controls - for defects, improper travel, and improper safetying. (xv) Main seat support braces and brackets. 43-3, 31 FR 3336, Mar. (3) Windows and windshields - for deterioration and breakage. (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; (eg: If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. (Secs. (vi) Barometric scale error. [Amdt. will bring you directly to the content. (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. Each is a special inspection unto itself; they're all different. Questions? 43-37, 66 FR 21066, Apr. (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 test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (v) Installation of structural parts other than the type of parts approved for the installation. No. 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 . With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. (iv) Friction. (xxiii) The repair of portions of skin sheets by making additional seams. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. 24. (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. (23) Cleaning or replacing fuel and oil strainers or filter elements. guide. 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. Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. 43-19, 43 FR 22639, May 25, 1978; Amdt. 43-7, 32 FR 7587, May 24, 1967; Amdt. (b) Listing of discrepancies and placards. Learn more about the eCFR, its status, and the editorial process. 43-23, 47 FR 41085, Sept. 16, 1982]. No. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. 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. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. 1993, 29 FR 5451, Apr. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. 1993, 29 FR 5451, Apr. 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). No. (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. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . 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 . (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. 91.417 Maintenance records. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. The date the work was completed. 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 . (a) Maintenance record entries. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. This applies to owner maintenance as well. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. 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. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). 43-49, 81 FR 96700, Dec. 30, 2016]. 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 -. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. FAA STANDARDS FOR ELECTRONIC RECORDS. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. (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. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. Replacing and servicing batteries. 1301, 1430), [Doc. The date of completion. 1655(c))), [Amdt. 6(c), Dept. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. [Doc. (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. The part may be legibly marked using a permanent method showing its current life status. (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. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. For miscellaneous technical amendments to this part 43, see Amdt. 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. Of the three maintenance records, the airframe (logbook) is the most permanent. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. Things can get a bit more complicated (and costly) if you can't nd a local A&P willing to sign off the safe-to-ferry logbook entry. - 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. (xxi) Repairs involving the substitution of material. full text search results He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (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. 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. (4) Appliance major alterations. 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. 27, 2001; Amdt. (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. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. 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. (3) The main rotor and center section (or the equivalent area). 106(g) (Revised Pub. ___, 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. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. formatting. How to Use. (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. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. 43-37, 66 FR 21066, Apr. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. 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. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. 43-39, 69 FR 44863, July 27, 2004; Amdt. 27, 2001], (a) General. (xii) Overhaul of controllable pitch propellers. As a (2) The date of completion of the work performed. 3. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. 14. 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. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. Download Free Template. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. 43-14, 37 FR 14291, June 19, 1972; Amdt. 23. 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. Pre-alpha refers to the early stages of development, when the software is . 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. When the software is controls - for improper installation and improper charge 18 1989. ( 2 ) the Main rotor and center section ( or the equivalent area ) amendments to this part Federal! 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