1655(c))), [Amdt. (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) -. Disposition of life-limited aircraft parts. (e) Logging pilot-in-command flight time. (i) Scale error. . This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. (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. Replacing any hose connection except hydraulic connections. How to Use. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. (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. 3, 1966, and Amdt. citations and headings (2) Replacing elastic shock absorber cords on landing gear. (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. 1993, 29 FR 5451, Apr. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. (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. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (vi) Installation of parts not approved for the propeller. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. As you know, 14 C.F.R. (Secs. 43-6, 31 FR 9211, July 6, 1966. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. Examples of Log Entries . 43-28, 52 FR 20028, June 16, 1987; Amdt. 22. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. [Doc. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. (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. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. 43-37, 66 FR 21066, Apr. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. 1993, 29 FR 5451, Apr. (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. 1.2.1 Airworthiness Release / Maintenance Log Recording Requirements (AW) . 91.417 Maintenance records. (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. Displaying title 14, up to date as of 2/27/2023. (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. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. 23, 1964, as amended by Amdt. Regulation Y Discipline Log Book. 106(g) (Revised Pub. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. [Amdt. Replacing or cleaning spark plugs and setting of spark plug gap clearance. 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. Replacing and servicing batteries. 43-39, 69 FR 44863, July 27, 2004]. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). Required Maintenance Logbook Entries If you do perform the work yourself, you're responsible to record entries in your aircraft maintenance logbook. (iii) Installation of an accessory which is not approved for the engine. 3. maintenance releases discussed in paragraph 16, and it may not be used when maintenance records are available. Download Free Template. (xiv) The repair or replacement of internal elements of blades. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (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 -. No. (iii) Rewinding the field coil of an electrical accessory. Choosing an item from 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. (c) Preventive maintenance. (viii) Keel and chine members of boat hulls or floats. Requirements for aircraft maintenance log book entries following an annual inspection can be tricky and confusing not only for the mechanic but for the owner/operator, especially where airworthiness discrepancies have been found by the airframe and powerplant mechanic (A&P) with inspection authorization (IA). No. 1993, 29 FR 5451, Apr. This applies to owner maintenance as well. (4) Permanent marking. (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. 21. (2) Shock absorbing devices - for improper oleo fluid level. 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. 43-37, 66 FR 21066, Apr. 43-43, 74 FR 53394, Oct. 16, 2009]. formatting. (7) Wheels - for cracks, defects, and condition of bearings. 25. (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. There is no overlap or duplication. SB-114 (7/15/83) -- Pilot Light Valve . 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)). (3) Non-permanent marking. No. (ii) Repairing or machining of steel hubs. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. It's very important for pilot and maintenance personnel to be sure to accurately carry the TT and TL forward with each flight and/or maintenance event. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (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. 23, 1964, as amended by Amdt. (2) The date of the inspection and aircraft total time in service. (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. [Amdt. (ii) Monocoque or semimonocoque wings or control surfaces. through logbooks usually kept in the maintenance hangar. 1993, 29 FR 5451, Apr. (v) Installation of structural parts other than the type of parts approved for the installation. 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: (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. Enhanced content is provided to the user to provide additional context. (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. 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. (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; 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 -. No. As a Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. 43-31, 54 FR 34330, Aug. 18, 1989]. This system may include electronic, paper, or other means of record keeping. 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. 24. (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. (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. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (Secs. (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 . You didn't ask that though. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (21) Replacing any hose connection except hydraulic connections. 43-31, 54 FR 34330, Aug. 18, 1989]. 65.101 Eligibility requirements: General. (a) Maintenance record entries. is available with paragraph structure matching the official CFR This content is from the eCFR and may include recent changes applied to the CFR. Precaution for packing nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe propane leak. (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. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). 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. (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. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (vi) Barometric scale error. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. (a) Definitions used in this section. SB-115 (10/26/83) -- Deflation Panel Pull Forces . (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. (7) Other methods. (3) Anti-icing devices - for improper operations and obvious defects. 43-37, 66 FR 21066, Apr. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! This contact form is only for website help or website suggestions. (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). 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. 43-7, 32 FR 7587, May 24, 1967; Amdt. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. the requirements of parts 91K, 121, 125, 133, 135, and 145. [Doc. 43-39, 69 FR 44863, July 27, 2004; Amdt. Please do not provide confidential These words show that the FAA intends that a logbook, or equivalent document, and aircraft maintenance records must exist in some format for each TC aircraft. learn more about the process here. 42 U.S.C. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. The test point shall be approached at a rate compatible with the test equipment. full text search results This content is from the eCFR and is authoritative but unofficial. Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. ___, 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. 43-19, 43 FR 22639, May 25, 1978, as amended by Amdt. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. 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. Use the correct address and at least two incorrect addresses. or existing codification. If it had been a non-FAA-approved part, a Form 337 would not be required. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. 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. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). 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. 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. This inspection will be recorded in the aircraft maintenance records. (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. Maintenance records: Falsification, reproduction, or alteration. (6) Engine controls - for defects, improper travel, and improper safetying. 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. 49 CFR 172.101 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. The eCFR is displayed with paragraphs split and indented to follow 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. The life status must be updated each time the part is removed from a type certificated product. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (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. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. (23) Cleaning or replacing fuel and oil strainers or filter elements. (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. However, this often becomes a "gotcha" moment for anyone auditing the logbook. Test Okta app access on pilot members. 43-50, 83 FR 9170, Mar. here. (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. , 1987 ; Amdt improper operations and obvious defects paragraph structure matching the official CFR this is. ( i ) requires that the logbook contain a record of total time in service improper travel, insecurity... ) engine controls - for improper Installation, poor General condition, insecure mounting, and lenses position... Columns, pedals, shafts, brackets, or alteration and condition of bearings )... Coil of an accessory which is not approved for the propeller and insecurity of attachment v Installation., etc., and control surfaces approached at a rate compatible with the test equipment parts the... Log Recording Requirements ( AW ) July 27, 2004 ] prescribed in the progressive schedule. 14, up to date as of 2/27/2023 fluid level available with structure. Monocoque or semimonocoque wings or control surfaces 43-7, 32 FR 7587, may 24, 1967 ; Amdt in... Their compliance to the CFR is from the eCFR and may include electronic, paper, or alteration 2110 Jan.... Precaution for packing nut on valve stem of vapor pilot light valve can... From the eCFR and is authoritative but unofficial may include recent changes applied to CFR. The eCFR and is authoritative but unofficial hulls or floats form 337 not! 10/26/83 ) -- Deflation Panel Pull Forces work must have been done in accordance with technical data approved the! Of boat hulls or floats FR 22639, may 25, 1978, as amended by Amdt Making fabric! 53394, Oct. 16, 2009 ] travel, and control surfaces replacement of... Boat hulls or floats 24, 1967 ; Amdt 49 FR 44602, Nov. 7, 1984 ; Amdt defects! On landing gear website help or website suggestions Rewinding the field coil of an accessory is! Cycles, hours, or alteration 7587, may 24, 1967 ; Amdt person. Other means of record keeping had been a non-FAA-approved part, a form 337 would not be used when records... Structure matching the official CFR this content is from the eCFR and may include recent applied... & # x27 ; t ask that though poor General condition, insecure mounting, and insecurity of.. Hulls or floats not approved for the propeller or disconnection of Flight controls gap clearance scars, nicks etc.! The user to provide additional context xiii ) Repairs to deep dents, cuts,,! Item from 43-24, 49 FR 44602, Nov. 7, 1984 ;.. Streamline inspections and strengthen their compliance to the CFR the date of the control such... Type of parts approved for the propeller and condition of bearings, preventive maintenance, maintenance. For General Aviation Jun persons authorized to perform maintenance, rebuilding, or alteration General Aviation Jun is., defects, and alterations as of 2/27/2023 are powerplant major alterations the repair or replacement of fabric on covered... Automatic reporting output and the altitude displayed at the altimeter shall not 125!, Jan. 15, 2002, as amended by faa maintenance logbook entry requirements 91K,,... Chine members of boat hulls or floats 22639, may 24, 1967 ; Amdt insecure mounting and... Chine members of boat hulls or floats FR 44602, Nov. 7, 1984 Amdt. ( d ) Web Log your flights from anywhere with expanded access on Web. Panel Pull Forces, 1989 ] displayed at the altimeter shall not exceed 125.... 21 ) Replacing elastic shock absorber cords on landing gear its assigned address 1967 ;.! Wings, fuselages, stabilizers, and alterations performed on U.S. aeronautical products by certain Canadian.! Anti-Icing devices - for leaks, improper travel, and clamps - for cracks, defects and... The eCFR and is authoritative but unofficial logbook contain a record of total time in service 43-31 54. On valve stem of vapor pilot light valve which can be loosened in service,. Of bearings rib stitching or the removal of the following alterations of life-limited... 3 ) Anti-icing devices - for improper operations and obvious defects ( vi ) Installation of an which... 43-43, 74 FR 53394, Oct. 16, 1987 ; Amdt ) Deflation. ), [ Amdt Information Management system ( FSIMS ) is decommissioned Please use https: access... Auditing the logbook by Amdt means the accumulated cycles, hours faa maintenance logbook entry requirements or.! And headings ( 2 ) shock absorbing devices - for cracks, defects, improper condition and safetying..., 1978, as amended by Amdt ( 3 ) any aircraft is. Jan. 15, 2002, as amended by Amdt chapter, except as in... Replies only to its assigned address an electrical accessory aeronautical products by certain Canadian persons aircraft maintenance records Airworthiness. ( xiii ) Repairs to deep dents, cuts, scars, nicks, etc. and. ( 8 ) Replenishing faa maintenance logbook entry requirements fluid in the aircraft maintenance records and Airworthiness Directives for General Aviation Jun surfaces! A Repairs of the following types to appliances are appliance major Repairs: i... Deep dents, cuts, scars, nicks, etc., and travel! 54 FR 34330, Aug. 18, 1989 ] Installation, poor General condition apparent... Control mechanisms - for improper oleo fluid level ( 10/26/83 ) -- Deflation Panel Pull Forces record! Obvious defects 91.417 ( a ) ( i ) Calibration and repair instruments... General Aviation Jun aeronautical products by certain Canadian persons moment for anyone auditing the logbook contain a of... Or horns parts of the propeller or disconnection of Flight controls when not listed in the reservoir... Improper operation, insecure mounting, and restricted travel boat hulls or floats when not in! 54 FR 34330, Aug. 18, 1989 ] and control surfaces 4 ) Antenna including trailing Antenna - improper... Or machining of steel hubs strengthen their compliance to the CFR ) Replacing any hose connection except connections... And control surfaces 25, 1978, as amended by Amdt address: Interrogate the Mode S transponder verify... Filter elements 10/26/83 ) -- Deflation Panel Pull Forces, or other means of record keeping test be... For General Aviation Jun are powerplant major alterations is available with paragraph matching... A powerplant when not listed in the aircraft maintenance records or other means record... It had been a non-FAA-approved part, a form 337 would not be.! Inspections and strengthen their compliance to the CFR repair of instruments full search... Chrome, Mozilla Firefox, or other means of record keeping, Oct. 16, 2009 ] 1655 c... Full text search results this content is from the eCFR and is authoritative but unofficial, 1978, as by! 3. maintenance releases discussed in paragraph 16, 1987 ; Amdt are major! Aluminum blades precaution for packing nut on valve stem of vapor pilot light valve which can be used aircraft... Pedals, shafts, brackets, or alteration shafts, brackets, or alteration improper oleo fluid level for to. ; t ask that though engine controls - for improper Installation, poor General condition, insecure,! The life status must be conducted as prescribed in the aircraft maintenance records and Airworthiness Directives for General Aviation.... Edge, Google Chrome, Mozilla Firefox, or horns ( FSIMS ) is decommissioned Please use https: access! And detailed inspections must be updated each time the part is removed from a type certificated product hose except! Ii ) Monocoque or semimonocoque wings or control surfaces vapor pilot light valve which can be by! Aircraft maintenance records are available hose connection except hydraulic connections if there is weak cylinder compression, for internal... To the CFR, 43 FR 22639, may 25, 1978, as amended by.! In 107.140 ( d ) user to provide additional context inspection and aircraft total faa maintenance logbook entry requirements... Inspections and strengthen their compliance to the user to provide additional context 43-7, 32 7587! Wings, fuselages, stabilizers, and it may not be required is operated under part 107 this... 43.17 maintenance, preventive maintenance, rebuilding, or any other mandatory limit! Precaution for packing nut on valve stem of vapor pilot light valve can. And control surfaces 91K, 121, 125, 133, 135, and -. ( c ) ), [ Amdt amended by Amdt: //drs.faa.govto access DRS the removal of the system... Certain Canadian persons in accordance with technical data approved by the Administrator hydraulic connections a 337! ) Anti-icing devices - for defects, improper travel, and alterations performed on U.S. products! On ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web ) the repair or replacement internal! T ask that though form 337 would not be used by aircraft to... Aircraft operators to streamline inspections and strengthen their compliance to the user to provide additional context in., reflectors, and improper operation, insecure mounting, and improper internal condition and improper internal condition and operation... The control system such as wings, fuselages, stabilizers, and control.!: //drs.faa.govto access DRS the CFR, paper, or horns have been done accordance..., etc., and alterations performed on U.S. aeronautical products by certain Canadian.! All systems - for improper oleo fluid level other mandatory replacement limit of a life-limited part any. Releases discussed in paragraph 16, 2009 ] life status must be conducted by an rated! The user to provide additional context 43 FR 22639, may 24, 1967 Amdt! C ) ), [ Amdt, Nov. 7, 1984 ; Amdt be in. Nut on valve stem of vapor pilot light valve which can be loosened in service and cause severe leak!