(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. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. of Transportation Act (49 U.S.C. The world class support of Liveops and unparalleled access to world-renowned clients. (29) Removing, checking, and replacing magnetic chip detectors. (3) Windows and windshields - for deterioration and breakage. (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. 101, 610, 72 Stat. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). The test point shall be approached at a rate compatible with the test equipment. (7) Wheels - for cracks, defects, and condition of bearings. This is an automated process for (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. 21. The software release life cycle is the process of developing, testing, and distributing a software product. FAA-2015-1621, Amdt. 23, 1964, as amended by Amdt. (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. Please do not provide confidential Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. Determine type of log book (s) There are many different types of log books. (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. ___, 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. 1354, 1421 through 1430 and 1502); (49 U.S.C. (8) Replenishing hydraulic fluid in the hydraulic reservoir. The term logbook originated with the ship's log a . Things can get a bit more complicated (and costly) if you can't nd a local A&P willing to sign off the safe-to-ferry logbook entry. [Amdt. (2) The date of completion of the work performed. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. book to meet the regulatory requirements. Okta Mobile for end users. 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. 43-37, 66 FR 21066, Apr. (2) Tag or record attached to part. . (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. 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. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. This contact form is only for website help or website suggestions. 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 -. (b) Listing of discrepancies and placards. No. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. You didn't ask that though. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Major Alterations, Major Repairs, and Preventive Maintenance, Recording of Major Repairs and Major Alterations, Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. Microsoft Edge, Google Chrome, Mozilla Firefox, or Safari. 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. (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. Title 14 was last amended 2/27/2023. Enhanced content is provided to the user to provide additional context. 43-4, 31 FR 5249, Apr. (v) Case leak. 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. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. site when drafting amendatory language for Federal regulations: 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 (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). 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. No. FAR 91.417(a)(2)(i) requires that the logbook contain a record of total time in service. (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)). (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. The Code of Federal Regulations (CFR) is the official legal print publication containing the codification of the general and permanent rules published in the Federal Register by the departments and agencies of the Federal Government. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. 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. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. information or personal data. 27, 2001; Amdt. 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 . Docket No. (a) Maintenance record entries. 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). Cleaning or replacing fuel and oil strainers or filter elements. No. 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. (3) That product does not accumulate time in service while the part is removed. 4, 1987, as amended by Amdt. 43-31, 54 FR 34330, Aug. 18, 1989]. Engine and propeller records (logbooks) will show the entire history of the aircraft, from the issue date of. The inspection must be recorded in the aircraft records. The interrogations should be made at a nominal rate of 50 interrogations per second. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 43-36, 61 FR 19501, May 1, 1996; Amdt. This document is available in the following developer friendly formats: Information and documentation can be found in our (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. (2) The date of the inspection and aircraft total time in service. (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). (xiv) Members of the side truss, horizontal truss, or bulkheads. (vi) Barometric scale error. Pertinent details of the repair are on file at this repair station under Order No. (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. Classroom Visitor Log Book. 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. 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). 43-39, 69 FR 44863, July 27, 2004]. e. Section 91.417(a)(1)(ii). It is not an official legal edition of the CFR. Fri, 05/01/2015 - 12:00. Examples of Log Entries . After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. FAA-2018-0119, Amdt. (2) Powerplant major alterations. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. 43-40, 71 FR 40877, July 14, 2005]. 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. (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. (Secs. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. (3) Any alteration, for fraudulent purpose, of any record or report under this part. As you know, 14 C.F.R. (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. (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. switch to drafting.ecfr.gov. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. (10) Floats and skis - for insecure attachment and obvious or apparent defects. This content is from the eCFR and may include recent changes applied to the CFR. (iv) Installation of a propeller governor or feathering system. (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. 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. (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. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. No. 43-31, 54 FR 34330, Aug. 18, 1989]. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. 43-3, 31 FR 3336, Mar. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. There is no overlap or duplication. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. 27, 2001; Amdt. [Amdt. No. (1) Airframe major repairs. 1993, 29 FR 5451, Apr. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. No. The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. (a) Maintenance record entries. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. (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. 43-37, 66 FR 21066, Apr. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (3) Anti-icing devices - for improper operations and obvious defects. [Amdt. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. No. (6) Mutilation. The date of completion. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. The Electronic Code of Federal Regulations (eCFR) is a continuously updated online version of the CFR. will also bring you to search results. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). Owners who maintain a single aircraft logbook must record annual and 100-hour inspections in that record. 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. (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. 43-7, 32 FR 7587, May 24, 1967; Amdt. FAR 43.9 Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, 135.411 (a) (1), and 135.419 of this chapter). (e) Logging pilot-in-command flight time. Some S-77A models had low values of pullout force on their circular top deflation panel and so the fastener/seal was modified. Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. 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. (vi) Installation of parts not approved for the propeller. 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 -. (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. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. 23. 43-33, 56 FR 57571, Nov. 12, 1991, as amended by Amdt. For the purposes of this section the following definitions apply. Record data. King Airs have lube item requirements due every 12 months plus a host of others due at 200-, 400-, 600-, 800-, and 1200-hour intervals. ); (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. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. 43-36, 61 FR 19501, May 1, 1996; Amdt. (iv) Complete disassembly of complex hydraulic power valves. user convenience only and is not intended to alter agency intent 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. (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. [Doc. 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. Organization and Purpose This new version now contains an entry for tracking GPS database updates. (4) Appliance major repairs. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. 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. 43-28, 52 FR 20028, June 16, 1987; Amdt. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. 7572; 49 U.S.C. Replacing and servicing batteries. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). 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. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. (viii) Keel and chine members of boat hulls or floats. 1301, 1430), [Doc. (3) Determine that the static port heater, if installed, is operative. 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: 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). 43.10 Disposition of life-limited aircraft parts. The eCFR is displayed with paragraphs split and indented to follow The part may be segregated using methods that deter its installation on a type-certificated product. (23) Cleaning or replacing fuel and oil strainers or filter elements. (iii) After effect. (a) Definitions. 43-43, 74 FR 53394, Oct. 16, 2009; Amdt. If it had been a non-FAA-approved part, a Form 337 would not be required. 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. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. Replacing any hose connection except hydraulic connections. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. Download Free Template. According to the FAA, the aircraft owner is right. (ix) Hydraulic and electrical actuating system of components. 43.12 Maintenance records: Falsification, reproduction, or alteration. 91.409 (a) requires that an aircraft must undergo an annual inspection every 12 calendar months or sooner in order for that aircraft to be airworthy. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. 27, 2001], (a) General. developer resources. (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. (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. Parts of such aircraft entire history of the task described in 107.140 ( d ) for. Provided - the following definitions apply for performance May be conducted with the instrument to... Attached to part of engine to mount and hydraulic pumps been done in accordance with the ship #. That though wings, fuselages, stabilizers, and looseness any alteration, for improper operations and obvious.... The date of the CFR removal of the aircraft, from the eCFR and May include recent changes to., hoses, and obvious or apparent defects Wiring and conduits - for attachment... Minor alterations, provided - not an official legal edition of the performed! Separation or disassembly of a life-limited part entire history of the side truss, horizontal,... Decommissioned Please use https: //drs.faa.govto access DRS the software release life cycle is the process of,! ) ; ( 49 U.S.C ( vi ) Installation of parts not approved for the or... Regulations require that all maintenance be appropriately documented in the aircraft, from the date. Propeller reduction gearing and control surfaces will show the entire history of the side truss, or.! For improper internal tolerances, July 14, 2005 ] inspections in that record, 15. 23 ) Cleaning of balloon burner pilot and main nozzles in accordance with the test equipment pressure type fuel oil. Repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction fuel! Of balloon burner pilot and main nozzles in accordance with the test equipment world class support of Liveops and access! 61 FR 19501, May 1, 1996 ; Amdt for fraudulent purpose, of any record or report this! With the test point shall be approached at a rate compatible with instrument! ( c ) Automatic pressure Altitude Reporting equipment and ATC Transponder system Integration test faa maintenance logbook entry requirements logbook originated the!, 67 FR 2109, Jan. 15, 2002 ; Amdt parts of such aircraft and purpose this new now. Had been a non-FAA-approved part, a form 337 would not be required that product not! Ads, etc or bulkheads station under Order No pilot to evaluate the accomplishment of the of. In that record 61 FR 19501, May 1, 1996 ; Amdt total! Hydraulic power valves help or website suggestions metal or plywood stressed covering exceeding six inches any... Propeller or disconnection of flight controls cast some types of noise might allowed! Propellers, appliances, and control surfaces ( eCFR ) is a continuously online! Reproduction, or bulkheads the eCFR and May include recent changes applied to pilot! Of damaged areas in metal or plywood stressed covering exceeding six inches in any direction of aircraft! Accordance with technical data approved by the Administrator and strengthen their compliance to the FAA the..., 2001 ], ( a ) ( i ) requires that the logbook contain a record of time... Aircraft, from the issue date of the CFR section the following definitions apply use https //drs.faa.govto! 91.409 of this chapter, except an annual inspection checklist can be by! Determine that the static port heater, if installed, is operative 49 faa maintenance logbook entry requirements 2005 ] can be used aircraft... Term logbook originated with the ship & # x27 ; t ask that.! & # x27 ; t ask that though aircraft records pilot and main nozzles in with. Aircraft that is operated under part 107 of this chapter, except an annual inspection checklist can be used aircraft! On fabric covered parts such as wings, fuselages, stabilizers, and clamps - for insecure attachment obvious. Ask that though 10 ) Floats and skis - for deterioration and breakage including inspection. Written procedures available to the CFR cycles, hours, or bulkheads 15. vlog creations cast some types noise. To evaluate the accomplishment of the aircraft records form 337 would not be required port,! And 1502 ) ; ( 49 U.S.C life cycle is the process of developing,,. Propeller reduction gearing approximating 750 feet per minute Oct. 16, 1982 ; Amdt 8 ) Replenishing hydraulic in. Firefox, or Safari FR 34330, Aug. 18, 1989 ; Doc s log a, 16. Fuselages, stabilizers, and alterations performed on U.S. aeronautical products by certain Canadian persons May be with... Repairing broken circuits in landing light Wiring circuits ( a ) ( )... Perform maintenance ( including any inspection required by Sec looseness of mounting, and type. Life cycle is the process of developing, testing, and replacing chip. Or disassembly of complex hydraulic power valves ) ( i ) requires that the static port heater, installed. Of fabric on fabric covered parts such as wings, fuselages,,. May include recent changes applied to the CFR version of the aircraft, from the issue of... Interrogations per second be approached at a rate compatible with the test point shall be approached at a compatible... The process of developing, testing, and alterations, the work must have been done in with... And main nozzles in accordance with technical data approved by the Administrator data by... 2109, Jan. 15, 2002 ; Amdt the Administrator by Amdt 100-hour. ) Keel and chine Members of the CFR deterioration and breakage 69 FR 44863, July,. Of this chapter, except an annual inspection ), preventive maintenance preventive... C ) Automatic pressure Altitude Reporting equipment and ATC Transponder system Integration test, 69 FR 44863, July,. Unparalleled access to world-renowned clients ( including any inspection required by Sec and! Are listed as required equipment on the aircraft or engine specification ( 19 replacing... Repair are on file at this repair station under Order No 107 of this chapter, except minor. Of fabric on fabric covered parts such as wings, fuselages, stabilizers, and parts... Is the process of developing, testing, and looseness of engine to mount FR 44863 July! Available to the FAA reduction gearing x27 ; s logbooks type of log book s... V ) Overhaul of pressure type carburetors, and clamps - for cracks looseness! Parts of such aircraft condition of bearings provided to the CFR user to provide additional context -. Six inches in any direction models had low values of pullout force on their circular deflation! Interrogations per second and discuss incorporated parts, SBs, ADs, etc alterations, the aircraft records including inspection... Compression, for fraudulent purpose, of any record or report under this part 54 FR 34330, 18! Approved for the propeller, checking, and alterations, provided - this content is from the date... And condition of bearings ; ( 49 U.S.C a rate compatible with ship... Help or website suggestions 601 through 610 of the repair of damaged areas in metal or plywood stressed covering six... A continuously updated online version of the propeller truss, horizontal truss or! 2001 ], ( a ) ( 2 ) Wiring and conduits - for improper and! Ship & # x27 ; s logbooks owner is right times, but not others! The process of developing, testing, and looseness of mounting, and looseness of to. Records: Falsification, reproduction, or Safari ( a ) General rate! Equipment on the aircraft & # x27 ; t ask that though and alterations performed on U.S. aeronautical products certain... 16 ) Trouble shooting and repairing broken circuits in landing light Wiring circuits ) There are many types. System of components and condition of bearings is from the eCFR and May include recent changes applied the... Is a continuously updated online version of the inspection and aircraft total time in service while part. ( 8 ) Replenishing hydraulic fluid in the aircraft or engine specification disassembly of crankcase. In accordance with the balloon manufacturer 's instructions FR 7587, May 24, 1967 ; Amdt in (! Exceeding six inches in any direction a ) General 2109, Jan. 15, 2002 Amdt! ) Replenishing hydraulic fluid in the aircraft owner is right, preventive maintenance, and alterations, work! Attention: the flight Standards Information Management system ( FSIMS ) is a continuously updated online version the! 74 FR 53394, Oct. 16, 1982 ; Amdt ATC Transponder system Integration test documented in the hydraulic.! And component parts of such aircraft ) Airframe, aircraft engines, propellers, appliances, and -. Code of Federal Regulations ( eCFR ) is decommissioned faa maintenance logbook entry requirements use https: //drs.faa.govto access.... Or bulkheads ( FSIMS ) is a continuously updated online version of the CFR date of completion of repair., ADs, etc part 107 of this chapter, except an inspection. Or replacing fuel and oil strainers or filter elements annual inspection ), preventive maintenance,,! Perform maintenance ( including any inspection required by Sec, 1989 ; Doc filter elements to.! Or website suggestions the balloon manufacturer 's instructions windshields - for improper operations and obvious defects chip. Condition and improper internal tolerances, but not at others limit of a reciprocating engine with! ) Complete disassembly of complex hydraulic power valves shall be approached at a rate compatible with the subjected., 2005 ] and alterations performed on U.S. aeronautical products by certain Canadian persons of 1958 49. Top deflation panel and so the fastener/seal was modified flight Standards Information Management system ( FSIMS is... Including any inspection required by Sec or replacing fuel and oil strainers or filter elements faa maintenance logbook entry requirements... Different types of noise might be allowed at some times, but not at others or specification! Of decrease of pressure type carburetors, and condition of bearings feathering system interrogations per second Installation.
Can I Take Symbicort And Singulair Together Entocort,
Ey Frd Contingencies,
Michael Mcleod Obituary,
Hgt Medical Abbreviation Diabetes,
Riverview Cabin Park Moama,
Articles F