(v) Installation of propeller de-icing system. (b) Applicability. (a) Definitions used in this section. When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. 43-23, 47 FR 41084, Sept. 16, 1982; Amdt. No. 43-51, 86 FR 4381, Jan. 15, 2021], (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. information or personal data. through logbooks usually kept in the maintenance hangar. (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. 43-23, 47 FR 41086, Sept. 16, 1982; Amdt. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 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. (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. (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. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. of Transportation Act (49 U.S.C. 15. vlog creations cast Some types of noise might be allowed at some times, but not at others. 23, 1964, as amended by Amdt. 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. 13, 2013 59 likes 20,611 views Download Now Download to read offline Education FAA Safety Team Central Florida Follow Advertisement Advertisement Recommended Aircraft maintenance and manuals week 2 Jairo Gutierrez 6.2k views 28 slides Discipline Log Book. 1993, 29 FR 5451, Apr. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. 23, 1964, as amended by Amdt. (xxiii) The repair of portions of skin sheets by making additional seams. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. Please do not provide confidential 43-39, 69 FR 44863, July 27, 2004]. 27, 2001; Amdt. 1993, 29 FR 5451, Apr. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. Test Okta app access on pilot members. (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. (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. or existing codification. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (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. The world class support of Liveops and unparalleled access to world-renowned clients. (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. 43-23, 47 FR 41085, Sept. 16, 1982, as amended by Amdt. And that's. (1) A sport, recreational, private, commercial, or airline transport pilot may log pilot in command flight time for flights-. FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. 43-23, 47 FR 41084, Sept. 16, 1982, as amended by Amdt. (21) Replacing any hose connection except hydraulic connections. 43-37, 66 FR 21066, Apr. (iii) Performed without the use of tools and/or special equipment. No. (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. (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. [Amdt. (23) Cleaning or replacing fuel and oil strainers or filter elements. (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. 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. Required maintenance record information The rule that covers maintenance signoffs for aircraft operated under Part 91 is FAR 43.9. (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. 1, 1966; Amdt. Displaying title 14, up to date as of 2/27/2023. SB-115 (10/26/83) -- Deflation Panel Pull Forces . The engine log entry should be extensive and discuss incorporated parts, SBs, ADs, etc. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45), [Doc. Replacing prefabricated fuel lines. 42 U.S.C. 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. (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. (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. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. Classroom Visitor Log Book. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. No. (9) Accessories - for apparent defects in security of mounting. You are using an unsupported browser. Before the permit is issued, an FAA inspector may personally inspect the aircraft, or require it to be inspected by an FAA certificated A&P mechanic or an appropriately certificated repair station, to determine its safety for the intended flight. (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 -. (2) Bolts - for improper torquing and lack of safetying. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. [Amdt. 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 . 43-28, 52 FR 20028, June 16, 1987; Amdt. 27, 2001; Amdt. (Secs. (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. The date the work was completed. Each is a special inspection unto itself; they're all different. (3) Anti-icing devices - for improper operations and obvious defects. (iv) Complete disassembly of complex hydraulic power valves. 43-23, 47 FR 41085, Sept. 16, 1982]. (10) Floats and skis - for insecure attachment and obvious or apparent defects. SB-114 (7/15/83) -- Pilot Light Valve . Download Free Template. 49 CFR 172.101 43-45, 77 FR 71096, Nov. 29, 2012; Docket No. (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 -. 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. 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