(7) Other methods. (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. 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 -. The part may be legibly marked using a non-permanent method showing its current life status. . (6) Electrical system - for chafing and improper operation of switches. PRINCIPLE CHANGES. Water vapor weighs 5/8 as much as dry air. 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. (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. ___________ inspections are limited to surface crack detection in aircraft parts. This change (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). 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. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil AC. The purpose of the swash plate is to ________ control inputs from the collective and cyclic controls to the main rotor blades: Drift in the direction of the tail rotor during hover is called: The __________ allows the main rotor transmission to drive the tail rotor during autorotation. The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (b) Rotorcraft. "Removed right wing from aircraft and removed skin from outer 6 feet. If you want to request a wider IP range, first request access for your current IP, and then use the "Site Feedback" button found in the lower left-hand side to make the request. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? center section assembly for poor general condition, fabric or skin Planning, Wills Spoilers are also used as speed brakes by: Which of the following statements is true? 7572; 49 U.S.C. (i) Scale error. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (3) The main rotor and center section (or the equivalent area). (3) That product does not accumulate time in service while the part is removed. Ailerons are used for which axis control? 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). Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. The application form, to become a certified mechanic is FAA Form ______. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. By an identification letter stamped on one of the hexes of the nozzle body Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. 43, App. (9) Accessories - for apparent defects in security of mounting. (2) Systems and components - for improper installation, apparent switches. (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) -. |zqG@TSM*l08 X-T7o)-LskG9D`64@1lhh&cl D` W q0xu{ |I:xq$T9kBB6oB.#O~gVDd /6wa;{v?|1}:o3$R'k{yQ]O7%Fvr3O,p{SqnU|C'NJ]S' {i{\X-"E (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (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. He shall thoroughly clean the aircraft and aircraft 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. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. (2) Studs and nuts - for improper torquing and obvious defects. (9) Accessories - for apparent defects in security of mounting. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (2) Shock absorbing devices - for improper oleo fluid level. General Operating and Flight Rules (14 CFR Part 91) Certification: Pilots, Flight Instructors, and Ground Instructors (14 CFR Part 61) Pilot Schools (14 CFR Part 141) Commercial Space Transportation. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (f) Each person performing an annual or 100-hour inspection The __________ is used to thoroughly service a component after it is removed from an aircraft. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (ii) Hysteresis. (a) Maintenance record entries. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (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. (e) Approval requirements. The part may be legibly marked using a permanent method showing its current life status. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (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). poor condition. We make completing any Part 43 Appendix D much faster. The tag or record must include the part number, serial number, and current life status of the part. An official website of the United States government. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. attachment. (2) Bolts - for improper torquing and lack of safetying. The method must deter the installation of the part after it has reached its life limit. Feb 7/2020 . 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. Guarantees that a business meets BBB accreditation standards in the US and Canada. (where practicable) improper operation. eCFR :: Appendix D to Part 43, Title 14 -- Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (Appendix D to Part 43, FAR) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/08/2023. The chord of an airfoil is measured from the ________ to the ________. 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. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. view historical versions Title 14 Chapter I Subchapter C Part 43 View Full Text Previous Next Top (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (xxi) Repairs involving the substitution of material. Explanation of Changes. Enjoy smart fillable fields and interactivity. (b) Applicability. (xv) Main seat support braces and brackets. (3) Anti-icing devices - for improper operations and obvious defects. USLegal received the following as compared to 9 other form sites. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. Witt OBriens_checklists index for oil transfer procedures list of items required the us federal regulations per 33 cfr 155.750 and california code of 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. Work is complete and compatible with other structures or systems. endstream endobj startxref (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. (j) Each person performing an annual or 100-hour 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. Be conducted with the following subparagraphs except as described in 107.140 ( d ) data approved by Administrator. In the US and Canada ) Anti-icing devices - for chafing and improper operation switches. 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