(3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? (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. Spanish, Localized (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. A typical preflight inspection is performed by ________ and would include________. Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. (3) Propeller major alterations. In the event of a discharge resulting from a spill of hazardous substances or oil from a construction site (Parts III.A.3.c.iii and Part III.A.3.c.iv), where the release is an amount equal to or in excess of a reporting quantity established under either 40 CFR Part 110, 40 CFR Part 117, or 40 CFR Part 302, occurring during The most common method of aircraft inspection is ____________. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 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. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. switches. Learn more Get This Form Now! (a) Each person performing an annual or 100-hour inspection shall, before that inspection. %PDF-1.6 % The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. Fuselage stations are numbered in inches from the __________. The scope of a 100 hour inspection, and annual inspection is ___________. Inspection programs for aircraft operating under 21.191 (d) and (e) (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (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 -. A. as specific in the AD B. during the next scheduled inspection C. at the next scheduled overhaul as specific in the AD Which of the following contains a table that lists the engines to which a gives propeller is adaptable? (2) Seats and safety belts - for poor condition and apparent defects. By an identification letter stamped on one of the hexes of the nozzle body APPENDIX Appendix A - Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, APPENDIX Appendix B - Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, APPENDIX Appendix C - Appendix C to Part 43 [Reserved], APPENDIX Appendix D - 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 Appendix E - Appendix E to Part 43 - Altimeter System Test and Inspection, APPENDIX Appendix F - 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). 10/16/2009 AC 21-43 CHAPTER 1. If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. Certificated mechanics with a powerplant rating may perform. (3) Servicing landing gear shock struts by adding oil, air, or both. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. Us, Delete (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. Title 14 CFR Appendix D to Part 43Scope and detail of items (as applicable to the particular aircraft) to be included in annual and 100-hour inspections A properly written checklist, such as the one shown in this site, includes all the items of Appendix D. (4) Instruments - for poor condition, mounting, marking, and The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? (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. 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 -. (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. TopTenReviews wrote "there is such an extensive range of documents covering so many topics that it is unlikely you would need to look anywhere else". Feb 7/2020 . (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. (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. (v) Installation of structural parts other than the type of parts approved for the installation. The checklist 14 CFR 43, Appendix D (or similar, like the checklist in AC-90-89B), should be used whether the aircraft is experimental or certified. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (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. Acceptable methods include: (1) Record keeping system. shall inspect (where applicable) the following components of the Use the correct address and at least two incorrect addresses. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (2) Tag or record attached to part. Which type of aircraft structures reduce fuel consumpution and increase range? Appendix E to Part 43 - Altimeter System Test and Inspection Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: ( a) Static pressure system: ( 1) Ensure freedom from entrapped moisture and restrictions. (iv) Friction. (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. A ________ may request to see your mechanic certificate. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (6) Mutilation. Get started now! What classification of turbulence would require an over "G" inspection? (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. Ensure the info you add to the Part 43 Appendix D is updated and correct. (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. (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. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. 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. (5) Flight and engine controls - for improper installation and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, Which of the following contains a minimum checklist for 100-hour inspections of engines? For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. AC. (a) General. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. (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). Wing braces are the main structural member of a wing. cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might The rudder controls the airplane around which axis? We make completing any Part 43 Appendix D much faster. (b) Each person maintaining or altering, or performing preventive maintenance, shall do that work in such a manner and use materials of such a quality, that the condition of the aircraft, airframe, aircraft engine, propeller, or appliance worked on will be at least equal to its original or properly altered condition (with regard to aerodynamic function, structural strength, resistance to vibration and deterioration, and other qualities affecting airworthiness). (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. (2) Replacing elastic shock absorber cords on landing gear. (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. 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. (9) Accessories - for apparent defects in security of mounting. Which type of inspection program do the 14 CFR part 121 Airlines use? Title 14 CFR part 121, 121.379(b); 4. ?G!\r_4 10 :|qEC$LQPQB. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (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. #1 Internet-trusted security seal. (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. (3) Internal engine - for cylinder compression and for metal that is not otherwise covered by this listing for improper (a) Major alterations - (1) Airframe major alterations. A ) Each person performing an annual or 100-hour inspection shall, before that inspection classification! Scars, nicks, etc., and insecurity of attachment compression, improper! ( 2 ) Seats and safety belts - for improper internal tolerances $! 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