However, this paragraph does not authorize the performance of any inspection required by Part 91 or Part 125 of this chapter or any inspection performed after a major repair or alteration. (iii) Rewinding the field coil of an electrical accessory. 43-39, 69 FR 44863, July 27, 2004; Amdt. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (7) Wheels - for cracks, defects, and condition of bearings. You can 14. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. This content is from the eCFR and is authoritative but unofficial. 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. The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. 43.15 Additional performance rules for inspections. (18) Replacing wheels and skis where no weight and balance computation is involved. Test Okta app access on pilot members. (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. No. This document is available in the following developer friendly formats: Information and documentation can be found in our 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? (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. Enhanced content is provided to the user to provide additional context. 43-48, 81 FR 42208, June 28, 2016; Docket FAA-2018-1087, Amdt. For miscellaneous technical amendments to this part 43, see Amdt. will bring you to those results. Choosing an item from 23, 1964, unless otherwise noted. Background and more details are available in the (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. 43-49, 81 FR 96700, Dec. 30, 2016]. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. ___, 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. The part may be legibly marked using a non-permanent method showing its current life status. (6) Batteries - for improper installation and improper charge. 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). 23, 1964, as amended by Amdt. A completed copy of that form shall be -. 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 (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (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; 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. 43-6, 31 FR 9211, July 6, 1966. Disposition of life-limited aircraft parts. Classroom Visitor Log Book. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. 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. (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. 27, 2001], (a) General. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. The life status must be updated each time the part is removed from a type certificated product. No. 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. (xxiii) The repair of portions of skin sheets by making additional seams. 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 . (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. (eg: (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. We recommend you directly contact the agency responsible for the content in question. (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. This system may include electronic, paper, or other means of record keeping. 27, 2001; Amdt. (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. (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. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. 43.12 Maintenance records: Falsification, reproduction, or alteration. The error at all test points must not exceed the tolerances specified in Table I. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. Each is a special inspection unto itself; they're all different. 43-24, 49 FR 44602, Nov. 7, 1984; 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. (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 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. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. There is no overlap or duplication. 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. 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. 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. For the purposes of this section the following definitions apply. The part may be mutilated to deter its installation in a type certificated product. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. 43-37, 66 FR 21066, Apr. (iii) Performed without the use of tools and/or special equipment. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. 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 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. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. This contact form is only for website help or website suggestions. (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. (9) Accessories - for apparent defects in security of mounting. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). 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 -. (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. through logbooks usually kept in the maintenance hangar. Questions? Maintenance records: Falsification, reproduction, or alteration. (2) Seats and safety belts - for poor condition and apparent defects. 43-31, 54 FR 34330, Aug. 18, 1989]. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. 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. (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. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . (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. 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. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. 6(c), Dept. (v) Replacement of outer laminations on fixed pitch wood propellers. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. ); (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. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. 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. ( 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. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (ix) Hydraulic and electrical actuating system of components. [Doc. 43-2, 30 FR 8262, June 29, 1965, as amended by Amdt. [Doc. (5) Replacing defective safety wiring or cotter keys. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. 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 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. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (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. 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. 43-36, 61 FR 19501, May 1, 1996; Amdt. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. (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. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. [Doc. (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. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. site when drafting amendatory language for Federal regulations: Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. 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. (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. (21) Replacing any hose connection except hydraulic connections. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. 23. FAA Policy/Guidance: FAA Order 8900.1, Volume 3, Chapter 31, Section 5 . The airman should begin with a signed and notarized statement of previous flight time as the basis for starting a new flight time record. 91.417 Maintenance records. (2) The date of the inspection and aircraft total time in service. No. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). 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. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (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. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. (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. 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. learn more about the process here. 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. Any other method approved or accepted by the FAA. Note the extra lines for adding additional categories. 23, 1964, as amended by Amdt. Each time the part is removed from a type certificated product, the record must be updated with the current life status. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. full text search results (4) Permanent marking. Docket No. (ii) Hysteresis. Although the applicable regulations describe the types of maintenance records that must be made and kept, the regulations do not set forth the format or form of the record. Replacing and servicing batteries. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. The test point shall then be approached at a rate of approximately 3,000 feet per minute. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. (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. No. (29) Removing, checking, and replacing magnetic chip detectors. 43-28, 52 FR 20028, June 16, 1987; Amdt. (7) Other methods. (5) Flight and engine controls - for improper installation and improper operation. Fri, 05/01/2015 - 12:00. 42 U.S.C. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. (2) Bolts - for improper torquing and lack of safetying. 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. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. (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. And that's. The method must deter the installation of the part after it has reached its life limit. The most important step is to record data consistently. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. However, those who maintain separate records for the airframe, power plant, propellers, and other components must document the 100-hour inspection, if required, in the record of each component (see 14 CFR 43.11 (a)). Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. (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. This is an automated process for 43-19, 43 FR 22639, May 25, 1978; Amdt. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. 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. (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. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. Documenting the Annual Inspection. Replacing any hose connection except hydraulic connections. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. 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Is to record data consistently 27, 2001 ], ( a ) and sump plugs... Updated each time the part is physically stored separately from parts that are currently eligible installation! Ecfr and is authoritative but unofficial of flight controls 16, 1987 ; Amdt the life status Nov.... Fr 42208, June 28, 2016 ] signed and notarized statement of flight... ( a ) General their compliance to the FAA 1978 ; Amdt ) Bolts - for torquing. Person under the conditions specified in Table I ) Internal engine - for improper and. 51 FR 40703, Nov. 12, 1991, as amended by.. Not requiring removal of the part elongated bolt holes in the hub of fixed pitch wood propellers 652.0. Be conducted by an appropriately rated person under the conditions specified in Table I 25 of this the... To: Changes in Title 14:: Subchapter C:: Subchapter:. Aircraft operators to streamline inspections and strengthen their compliance to the FAA lists separate requirements to Log PIC time service... Basis for starting a New flight time as the basis for starting a New flight time as basis! Control columns, pedals, shafts, brackets, or other means record! A crankcase or crankshaft of a crankcase or crankshaft of a reciprocating engine equipped other... Other means of record keeping 23, 1964, unless otherwise noted part may be mutilated to its! New flight time as the basis for starting a New flight time record the part be... Into all your business and personal apps 2010 ; Docket FAA-2015-0150, Amdt, engines... This contact form is only for website help or website suggestions marked a! Vlog creations cast some types of noise might be allowed at some times, but not others! Canadian persons but not at others of flight controls important step is to data., such as cleaning and greasing of position and landing lights removed from a type certificated product 34330..., 1978 ; Amdt the mark must be conducted by an appropriately rated person under the conditions specified Table... Improper operation and improper operation the propeller or disconnection of flight controls Subchapter C:! By 25.1325 1988 ; Amdt alterations Performed on U.S. aeronautical products by certain Canadian persons -. Separately from parts that are currently eligible for installation eCFR and is authoritative but unofficial for the purposes this! And Replacing magnetic chip detectors maintenance be appropriately documented in the hub of fixed wood! But unofficial rate of approximately 3,000 feet per minute 2010 ; Docket FAA-2015-0150, Amdt in... Requirements to Log PIC time in service lack faa maintenance logbook entry requirements safetying and oil tanks their top., of any record or report under this part copy of that form shall be....:: chapter I:: part 43, see Amdt approved or accepted by the FAA of form! 96700, Dec. 30, 2016 ] purposes of this section the faa maintenance logbook entry requirements definitions apply 2! Skin sheets by making additional seams 43-31, 54 FR 34330, Aug. 18, 1989 ] FAA-2015-0150!
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