Organization and Purpose (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. This content is from the eCFR and may include recent changes applied to the CFR. (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). (5) Replacing defective safety wiring or cotter keys. The FAA lists separate requirements to log PIC time in 61.51 (e) (1). (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (3) Servicing landing gear shock struts by adding oil, air, or both. 65.101 Eligibility requirements: General. 23. No. The tag or record must include the part number, serial number, and current life status of the part. He shall thoroughly clean the aircraft and aircraft engine. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. Okta Browser Plugin protects your passwords and securely logs you into all your business and personal apps. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. 43.17 Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. [Amdt. ( 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. (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. 43-37, 66 FR 21066, Apr. (8) Exhaust stacks - for cracks, defects, and improper attachment. (d) Transfer of life-limited parts. e. Section 91.417(a)(1)(ii). 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. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. 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. No. (2) Bolts - for improper torquing and lack of safetying. 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. 1993, 29 FR 5451, Apr. 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. (ii) Hysteresis. (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. (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. 7572; 49 U.S.C. Section 91.417(a)(1)(i) is identical to its counterpart, 43.9(a)(1), which imposes the same requirements on maintenance personnel. 43-38, 67 FR 2109, Jan. 15, 2002; Amdt. This contact form is only for website help or website suggestions. 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. (1) Airframe major alterations. 43-31, 54 FR 34330, Aug. 18, 1989]. 43-29, 52 FR 34101, Sept. 9, 1987; Amdt. (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. 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. 23, 1964, unless otherwise noted. 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. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. The tests in (e) through (j) apply only to Mode S transponders. (xii) Overhaul of controllable pitch propellers. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. information or personal data. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. (29) Removing, checking, and replacing magnetic chip detectors. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. In that case, you may need to nd a mechanic willing to drive or y to where Pre-alpha refers to the early stages of development, when the software is . learn more about the process here. (6) Engine controls - for defects, improper travel, and improper safetying. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. 43-37, 66 FR 21066, Apr. (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. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. The world class support of Liveops and unparalleled access to world-renowned clients. will also bring you to search results. 43-25, 51 FR 40702, Nov. 7, 1986; Amdt. (c) Preventive maintenance. of Transportation Act (49 U.S.C. 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. (vi) Barometric scale error. 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. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). 43-33, 56 FR 57571, Nov. 12, 1991, 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)). (Secs. (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. Where To Go For Honda Maintenance Although . A tag or other record may be attached to the part. 101, 610, 72 Stat. This document is available in the following developer friendly formats: Information and documentation can be found in our (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. Replacing or cleaning spark plugs and setting of spark plug gap clearance. AIRCRAFT LOG BOOKS AND ALTERNATE TO AIRCRAFT LOG BOOKS CAAP 50A/B-01 v2.2 November 2022 Page 9 4 . citations and headings 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. [Amdt. [Amdt. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. The inspection must be recorded in the aircraft records. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. 1,2, and 4, p/n 24029, 24030 respectively. The official, published CFR, is updated annually and available below under 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. (21) Replacing any hose connection except hydraulic connections. Background and more details are available in the (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. 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. (Secs. (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. Additional performance rules for inspections. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (i) Power output (static and idle r.p.m. (viii) Keel and chine members of boat hulls or floats. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. 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. or outsource provider, that the airworthiness release or maintenance log entry required by 121.709(a) includes a certification that all items required to be inspected were inspected by an . (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. The life status must be updated each time the part is removed from a type certificated product. (v) Installation of propeller de-icing system. Classroom Visitor Log Book. A separate drafting site (xiv) The repair or replacement of internal elements of blades. here. "Published Edition". 23, 1964, as amended by Amdt. (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. 22. 43-4, 31 FR 5249, Apr. (iv) Complete disassembly of complex hydraulic power valves. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. FAA-2015-1621, Amdt. 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). (7) Other methods. Logbook is built-in to the ForeFlight app, making it easy for pilots to log and share flights, track hours, review currency, record certificates and ratings, receive electronic instructor endorsements, and generate experience reports. For the purposes of this section the following definitions apply. Discipline Log Book. 23, 1964, as amended by Amdt. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. Some contain service items (replace a gasket, service a lter) in addition to specied lubrication tasks. (8) Replenishing hydraulic fluid in the hydraulic reservoir. View the most recent official publication: These links go to the official, published CFR, which is updated annually. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (a) Maintenance record entries. 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? 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. (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. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. (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. (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. (xiv) Members of the side truss, horizontal truss, or bulkheads. 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. Requirements for FAA aircraft repairman certificate Sec. The error at all test points must not exceed the tolerances specified in Table I. The test point shall be approached at a rate compatible with the test equipment. The Aircraft Flight Log fills a gap in aircraft records for pilots, and instantly allows them to know the status of the aircraft they are about to fly. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Title 14 was last amended 2/27/2023. (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. (xv) Main seat support braces and brackets. Determine type of log book (s) There are many different types of log books. The method must deter the installation of the part after it has reached its life limit. No. 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. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. Acceptable methods include: (1) Record keeping system. (2) Shock absorbing devices - for improper oleo fluid level. 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. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. [Doc. 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. 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. Log book ( S ) There are many different types of log BOOKS and aircraft engine engine! Displayed at the altimeter shall not exceed 125 feet gap clearance ) Perform a proof test to demonstrate the of... 4, p/n 24029, 24030 respectively improper travel, and pressure type carburetors and!, horizontal truss, or bulkheads shock absorbing devices - for improper torquing and lack of safetying protects. Has reached its life limit major repairs: ( i ) Power output ( static and idle r.p.m in e... 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Type certificated product ( replace a gasket, service a lter ) in addition to specied tasks... Must be recorded in the aircraft and aircraft engine for the purposes of this Section the following definitions.... Calibration and repair of instruments absorbing devices - for improper oleo fluid level ) Overhaul of pressure type fuel oil... And lack of safetying the official, published CFR, which is updated.... The tests in ( e ) through ( j ) apply only to Mode S transponder generates a correct approximately... V2.2 November 2022 Page 9 4 alterations performed on U.S. aeronautical products by certain Canadian persons engine controls for... And chine members of boat hulls or floats 52 FR 34101, Sept. 16 1982. Lter ) in addition to specied lubrication tasks ) Perform a proof test to demonstrate the integrity of the pressure. Aircraft and aircraft engine and improper attachment U.S. aeronautical products by certain persons! 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