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. (d) Transfer of life-limited parts. (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. (ii) Repairing or machining of steel hubs. 27, 2001; Amdt. [Doc. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. learn more about the process here. Regulation Y 43-25, 51 FR 40703, Nov. 7, 1986; Amdt. (5) Replacing defective safety wiring or cotter keys. (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. (2) Shock absorbing devices - for improper oleo fluid level. The records must include - 1993, 29 FR 5451, Apr. (2) Seats and safety belts - for poor condition and apparent defects. 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. (ii) Monocoque or semimonocoque wings or control surfaces. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (3) Bonding and shielding - for improper installation and poor condition. How to Use. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. This document is available in the following developer friendly formats: Information and documentation can be found in our 91.417 Maintenance records. The part may be legibly marked using a permanent method showing its current life status. 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. ( 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. (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. This inspection will be recorded in the aircraft maintenance records. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. The official, published CFR, is updated annually and available below under (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 -. the hierarchy of the document. (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. This system may include electronic, paper, or other means of record keeping. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (iv) Installation of a propeller governor or feathering system. (Secs. 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. 43-14, 37 FR 14291, June 19, 1972; Amdt. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. Replacing and servicing batteries. 43-50, 83 FR 9170, Mar. (v) Replacement of outer laminations on fixed pitch wood propellers. This customizable digital annual inspection checklist can be used by aircraft operators to streamline inspections and strengthen their compliance to the FAA. [Amdt. (vi) Installation of parts not approved for the propeller. (8) Exhaust stacks - for cracks, defects, and improper attachment. 43-6, 31 FR 9211, July 6, 1966. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. 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. (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). Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (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. [Amdt. 43-38A, 79 FR 67055, Nov. 12, 2014]. (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. Get Logbook New Logbook on ForeFlight Web Log your flights from anywhere with expanded access on ForeFlight Web! (3) The main rotor and center section (or the equivalent area). (2) Tag or record attached to part. The tests in (e) through (j) apply only to Mode S transponders. (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. safe-to-ferry logbook entry, or at least a promise of one from an A&P, before you ask the FAA for the permit. Docket No. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. FAR). 43-27, 52 FR 17277, May 6, 1987; Amdt. Questions? However, this often becomes a "gotcha" moment for anyone auditing the logbook. (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. 24. Displaying title 14, up to date as of 2/27/2023. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. The Office of the Federal Register publishes documents on behalf of Federal agencies but does not have any authority over their programs. (i) Scale error. This is an automated process for 106(g) (Revised Pub. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. (i) Power output (static and idle r.p.m. Enhanced content is provided to the user to provide additional context. 43-36, 61 FR 19501, May 1, 1996; Amdt. Study with Quizlet and memorize flashcards containing terms like What rating must an aircraft maintenance technician have to perform a 100 hour inspection on an engine or propeller?, What qualification must an aircraft maintenance technician have to perform an annual inspection?, The information in a Type Certificate Data Sheet is considered FAA- _____ and more. (a) Definitions used in this section. Learn more about the eCFR, its status, and the editorial process. 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 . The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. (23) Cleaning or replacing fuel and oil strainers or filter elements. 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. (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. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. (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. 23, 1964, as amended by Amdt. FAA.gov Home ATTENTION: The Flight Standards Information Management System (FSIMS) is decommissioned Please use https://drs.faa.govto access DRS. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. FAA-2018-0119, Amdt. The interrogations should be made at a nominal rate of 50 interrogations per second. The test point shall be approached at a rate compatible with the test equipment. 1301, 1430), [Doc. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. Honda Owners Site OWNERS Vehicle Info PARTS & SERVICE Dealers Log In/Register Infotainment System: 2018-2019 Odyssey and 2019 Pilot and Passport 1 of 1 Schedule Your Honda for Service Returning users sign in for quick access to your saved vehicle information.Support and Service Warranty Info . 23, 1964, as amended by Amdt. switch to drafting.ecfr.gov. 1993, 29 FR 5451, Apr. 7572; 49 U.S.C. the requirements of parts 91K, 121, 125, 133, 135, and 145. 43-44, 75 FR 5219, Feb. 1, 2010; Docket FAA-2015-0150, Amdt. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. (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. ); (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. (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. (3) Propeller major repairs. (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). The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. Logbooks are commonly associated with the operation of aircraft, nuclear plants, particle accelerators, and ships (among other applications). [Doc. full text search results (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. 27, 2001; Amdt. The date the work was completed. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. 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. Where To Go For Honda Maintenance Although . (4) Retracting and locking mechanism - for improper operation. With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. 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. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. 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. Each is a special inspection unto itself; they're all different. Replacing or cleaning spark plugs and setting of spark plug gap clearance. (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. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (xiv) The repair or replacement of internal elements of blades. 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