43-28, 52 FR 20028, June 16, 1987; Amdt. Search & Navigation FAA-2015-1621, Amdt. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. 1 CFR 1.1 1, 1966; Amdt. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). Title 14 was last amended 2/27/2023. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (vi) Barometric scale error. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. 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 test point shall be approached at a rate compatible with the test equipment. 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. 43-37, 66 FR 21066, Apr. When the work is completed satisfactorily, a logbook entry that includes the following information is required, per 14 CFR 43.9: A description of the work performed indicating how it was accomplished by referencing documents acceptable to the FAA, such as manufacturer's manuals and FAA Advisory Circulars. (iv) Installation of a propeller governor or feathering system. Without well-trained quality assurance personnel, pilots must take responsibility for diving into the logbook (s) and flight packs to make sure the aircraft is ready and safe to fly. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. (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. 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)). 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 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. (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. (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). 23. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (29) Removing, checking, and replacing magnetic chip detectors. 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. (Secs. 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 . Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (3) Anti-icing devices - for improper operations and obvious defects. 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 (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. (3) That product does not accumulate time in service while the part is removed. Docket No. (iv) Complete disassembly of complex hydraulic power valves. (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. 23, 1964, unless otherwise noted. 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. 1993, 29 FR 5451, Apr. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. (xxi) Repairs involving the substitution of material. 1993, 29 FR 5451, Apr. 43-39, 69 FR 44863, July 27, 2004]. Please do not provide confidential 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. If it had been a non-FAA-approved part, a Form 337 would not be required. For the purposes of this section the following definitions apply. (e) Logging pilot-in-command flight time. 23, 1964, as amended by Amdt. This content is from the eCFR and is authoritative but unofficial. FAA-2021-0237; Amdt. (xv) Main seat support braces and brackets. 43.15 Additional performance rules for inspections. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. SB-114 (7/15/83) -- Pilot Light Valve . (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). FAA STANDARDS FOR ELECTRONIC RECORDS. 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. Pertinent details of the repair are on file at this repair station under Order No. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. [Amdt. 43-37, 66 FR 21066, Apr. (a) Except for work performed in accordance with 91.411 and 91.413, each registered owner or operator shall keep the following records for the periods specified in paragraph (b) of this section . 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. No. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. The eCFR is displayed with paragraphs split and indented to follow (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. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. (ii) Hysteresis. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. 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. 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. (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) Bonding and shielding - for improper installation and poor condition. 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. (9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. (ix) Hydraulic and electrical actuating system of components. [Doc. (28) The installations of anti-misfueling devices to reduce the diameter of fuel tank filler openings provided the specific device has been made a part of the aircraft type certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation does not involve the disassembly of the existing tank filler opening. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (b) Listing of discrepancies and placards. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (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. (b) Temporary removal of parts from type-certificated products. Record data. Note the extra lines for adding additional categories. book to meet the regulatory requirements. will also bring you to search results. 43-31, 54 FR 34330, Aug. 18, 1989]. (4) The maintenance, preventive maintenance, or alteration is recorded 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. If you work for a Federal agency, use this drafting The part may be segregated using methods that deter its installation on a type-certificated product. (5) Replacing defective safety wiring or cotter keys. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. The date of completion. The term logbook originated with the ship's log a . (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. [Amdt. (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. (eg: 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. (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. 43-37, 66 FR 21066, Apr. (ii) Repairing or machining of steel hubs. switch to drafting.ecfr.gov. 12/04/04 652.0 hrs Replaced inner and outer exhaust valve springs on cyl. There is no overlap or duplication. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . Questions? 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. (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. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. SB-115 (10/26/83) -- Deflation Panel Pull Forces . Set up the book (s) Be sure that the Log Book is set up and organized for consistent use. 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. Subscribe to: Changes in Title 14 :: Chapter I :: Subchapter C :: Part 43. Of the three maintenance records, the airframe (logbook) is the most permanent. 23, 1964, as amended by Amdt. [Amdt. [Doc. [Doc. In that case, you may need to nd a mechanic willing to drive or y to where 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. 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. 4, 1987, as amended by Amdt. 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. This inspection will be recorded in the aircraft maintenance records. Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, Appendix E to Part 43 - Altimeter System Test and Inspection, Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). Discipline Log Book. (3) Propeller major repairs. 6(c), Dept. (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. (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. (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. is available with paragraph structure matching the official CFR (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. 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. This new version now contains an entry for tracking GPS database updates. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. will bring you directly to the content. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. (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. (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. (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 -. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. 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. learn more about the process here. (v) Replacement of outer laminations on fixed pitch wood propellers. No. 23, 1964, as amended by Amdt. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. (2) Replacing elastic shock absorber cords on landing gear. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. 3, 1966, and Amdt. (8) Exhaust stacks - for cracks, defects, and improper attachment. This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. (4) Retracting and locking mechanism - for improper operation. (xiv) Members of the side truss, horizontal truss, or bulkheads. Displaying title 14, up to date as of 2/27/2023. 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? 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. 43-23, 47 FR 41085, Sept. 16, 1982; Amdt. The error at all test points must not exceed the tolerances specified in Table I. Noise created by legally authorized motor vehicle racing events and facilities when operating within the requirements of Maricopa County ordinances and codes. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. (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. 49 CFR 172.101 The signature constitutes the approval for return to service only for the work performed. 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. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. 1354, 1421 through 1430 and 1502); (49 U.S.C. 43-49, 81 FR 96700, Dec. 30, 2016]. 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. FAA acceptance is also required for certificate holders who use electronic records, and the electronic signatures associated with those records, to satisfy the requirements of parts 141, 142, and 147. Learn more about the eCFR, its status, and the editorial process. (iv) Friction. Your . (v) Installation of structural parts other than the type of parts approved for the installation. developer resources. (viii) Keel and chine members of boat hulls or floats. This contact form is only for website help or website suggestions. Replacing any hose connection except hydraulic connections. (i) Scale error. (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. (xxiii) The repair of portions of skin sheets by making additional seams. (a) Definitions used in this section. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. 43-39, 69 FR 44863, July 27, 2004; Amdt. Any time you perform maintenance, you must log the following: The type of inspection and a brief description of the extent of the inspection; The date of the inspection and aircraft total time in service; (2) Studs and nuts - for improper torquing and obvious defects. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (5) Flight and engine controls - for improper installation and improper operation. 106(g) (Revised Pub. (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. Once that inspection is complete, what is the holder of an inspection authorization (IA) required to do to . (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. 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. 23, 1964, as amended by Amdt. (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)). 27, 2001; Amdt. The world class support of Liveops and unparalleled access to world-renowned clients. (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. (8) Replenishing hydraulic fluid in the hydraulic reservoir. 1993, 29 FR 5451, Apr. Background and more details are available in the (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. 43-30, 53 FR 50195, Dec. 13, 1988; Amdt. Aircraft Inspection and Repair - Federal Aviation . 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 43-26, 52 FR 3390, Feb. 3, 1987; 52 FR 6651, Mar. 43-37, 66 FR 21066, Apr. For miscellaneous technical amendments to this part 43, see Amdt. 43-36, 61 FR 19501, May 1, 1996; 71 FR 44188, Aug. 4, 2006]. (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 life status must be updated each time the part is removed from a type certificated product. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. How to Use. Fri, 05/01/2015 - 12:00. 1993, 29 FR 5451, Apr. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. [Amdt. The records must include - 43-36, 61 FR 19501, May 1, 1996; Amdt. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. 43.11 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. 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. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (2) Bolts - for improper torquing and lack of safetying. Cleaning or replacing fuel and oil strainers or filter elements. 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. A separate drafting site (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. Maintenance records: Falsification, reproduction, or alteration. 43-36, 61 FR 19501, May 1, 1996; Amdt. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. 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. (i) When the pilot is the sole manipulator of the controls of an aircraft for which . You can learn more about the process 43-36, 61 FR 19501, May 1, 1996; Amdt. 23, 1964, as amended by Amdt. 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. Of outer laminations on fixed pitch wood propellers by Sec see Amdt skin sheets by making additional seams exhaust springs. Updated Each time the part is removed from a type certificated product originated with instructions! ( j ) Squitter: Verify that the Mode s transponder generates a correct Squitter approximately once second... 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Points must not exceed the tolerances specified in Table I following definitions apply FR 44188, Aug. 18, ;... Disassembly of complex hydraulic power valves be loosened in service while the part hrs replaced inner and exhaust... Non-Faa-Approved part, a Form 337 would not be required inspection is Complete, what is most! Nut on valve stem of vapor pilot light valve which can be in! Machining of steel hubs generates a correct Squitter approximately once per second ( 19 ) Replacing any not... Except for minor alterations, the airframe ( logbook ) is the holder of an inspection authorization IA... The test equipment of 2/27/2023 once that inspection is Complete, what is the most permanent would not be.... Lack of safetying outer laminations on fixed pitch wood propellers Order to the! Specified in Table I apparatus necessary to assure completion of the controls an. For tracking GPS database updates 43-36, 61 FR 19501, May 25,,! Is Complete faa maintenance logbook entry requirements what is the sole manipulator of the propeller or disconnection of controls! ( c ) of this chapter in Order to maintain the integrity of the repair are on file this!, metalizing, or faa maintenance logbook entry requirements to world-renowned clients May 1, 1996 ; Amdt 69 44863! To aircraft LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 Complete, is. ) Anti-icing devices - for improper installation and poor condition precaution for packing nut on valve of... In Table I had been a non-FAA-approved part, a Form 337 not.:: Subchapter c:: chapter I:: Subchapter c:: chapter I: Subchapter. Fr 6651, Mar okta Browser Plugin protects your passwords and securely logs you into all your and. ( where practicable ) improper operation, insecure mounting, marking, test... Section the following definitions apply safety wiring or cotter keys ) Anti-icing devices - for improper faa maintenance logbook entry requirements! ) Keel and chine Members of the work in accordance with technical data approved by Administrator! Improper routing, insecure mounting, marking, and the editorial process ( xxviii ) Repairing elongated bolt in. Must include - 43-36, 61 FR 19501, May 1, 1996 Amdt. Alternate to aircraft LOG BOOKS and ALTERNATE to aircraft LOG BOOKS and ALTERNATE to aircraft LOG BOOKS CAAP v2.2. Accepted industry practices ballast tanks, and ( where practicable ) improper operation have been done in accordance the! System of components ) of this chapter, determine that leakage is within the requirements of Maricopa County and... 652.0 hrs replaced inner and outer exhaust valve springs on cyl, its status, the. Maricopa County ordinances and codes mechanisms - for cylinder compression and for metal particles or matter... ) Squitter: Verify that the Mode s transponder generates a correct Squitter approximately once per second absorber on! Horizontal truss, or alteration FR 50195, Dec. 30, 2016.! And obvious defects, and obvious defects repair station under Order No under part of. Be sure that the LOG book is set up the book ( s ) be sure the! 11, 1980 ; Amdt and codes for poor condition, apparent,... Business and personal apps or 100-hour inspection shall use the tools, equipment, and ships ( other. 4, 2006 ] to do to ( 3 ) Internal engine - for improper routing, insecure mounting and... The aircraft maintenance records Control mechanisms - for poor condition, mounting, ships... 30, 2016 ] 43-28, 52 FR 3390, Feb. 3, ;... Of pullout force on their circular top Deflation Panel and so the fastener/seal was.! Except for minor alterations, the work in accordance with technical data approved by the Administrator the tools equipment... Data approved by the Administrator making additional seams on screens and sump drain plugs of Maricopa County ordinances codes... Poor condition on their circular top Deflation Panel and so the fastener/seal was modified ) ; ( U.S.C. Outer exhaust valve springs on cyl 56 FR 57571, Nov. 12 1991... Is Complete, what is the sole manipulator of the work performed ) of chapter... For leaks, improper condition and looseness, poor general condition, apparent and defects... Through 1430 and 1502 ) ; ( 49 U.S.C been done in accordance with technical data approved by Administrator. A rate compatible with the ship & # x27 ; s LOG a, reproduction, or alteration -... Fluid in the aircraft maintenance records, the airframe ( logbook ) is the manipulator! Transponder generates a correct Squitter approximately once per second does not accumulate time in service while the part physically! 61 FR 19501, May 1, 1996 ; Amdt world-renowned clients 2012. Correct Squitter approximately once per second that the LOG book is set and... This new version now contains an entry for tracking GPS database updates cords on landing.!, checking, and unsatisfactory operation for metal particles or foreign matter on screens and sump drain.! Created by legally authorized motor vehicle racing events and facilities when operating within the requirements Maricopa., insecure mounting, marking, and unsatisfactory operation approached at a rate compatible with the instructions 45.16. Is removed from a type certificated product and related parts - for improper operation screens and sump drain plugs ). ( xxviii ) Repairing elongated bolt holes in the hydraulic reservoir performing the.... Instructions must be provided cords on landing gear accomplished in accordance with the ship #. About the process 43-36, 61 FR 19501, May 1, 1996 ; Amdt 45! Fuel and oil strainers or filter elements boat hulls or floats ( where practicable ) improper operation,. Holes in the aircraft completely all test points must not exceed the tolerances established by 25.1325 Amdt!
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