What provides the thrust for a Gyrocopter? Guarantees that a business meets BBB accreditation standards in the US and Canada. (where practicable) improper operation. (b) Each person performing an annual or 100-hour inspection The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (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. (2) Bolts - for improper torquing and lack of safetying. 10/16/2009 AC 21-43 CHAPTER 1. (ii) Repairing or machining of steel hubs. What are three characteristics of a sprawling stance? (6) Engine controls - for defects, improper travel, and improper APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . Cowl flaps are movable parts of the cowling that open and close in order to: Primary flight control surfaces need to be balanced so they do not: Flight control surfaces must be balanced whenever: When the airplane is turned left the aileron on the pilot's __________ points up. (vi) Installation of parts not approved for the propeller. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. Moving the cyclic pitch control of a two bladed system increases the AOA of one rotor blade with the result that a _______ lifting force is applied at that point in the plane of rotation. (6) Engine controls - for defects, improper travel, and improper safetying. (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. (xiv) Members of the side truss, horizontal truss, or bulkheads. foul the controls. Spanish, Localized 2115 0 obj <>stream attachment. The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. (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. AC. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. (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 -. Summary of Proposed Rule. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ switches. Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. (5) Replacing defective safety wiring or cotter keys. (h) Each person performing an annual or 100-hour inspection He shall thoroughly clean the aircraft and aircraft engine. 2. My Account, Forms in 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. When must an Airworthiness Directive be complied with? insecure mounting, and improper operation. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. (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. Certificated mechanics with a powerplant rating may perform. 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. Roll, pitch, yaw. AUTHORITY: 42 U.S.C. fatigue, and distortion. Spars are to wings as__________ are to the fuselage. (j) Each person performing an annual or 100-hour inspection Which type of inspection program do the 14 CFR part 121 Airlines use? (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. looseness of engine to mount. (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). 311 0 obj <>stream Experience is the act of having performed the task before. (5) Flexible vibration dampeners - for poor condition and deterioration. (c) Disposition of parts removed from type-certificated products. (21) Replacing any hose connection except hydraulic connections. 1.2 Applicability. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. The pilot, walking around the aircraft A special Inspection may include the following: 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. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. Responsibility for compliance with ADs and upkeep of maintenance records lies with the: Who is responsible for making the log book entry after an Annual, 100 hour, or Progressive Inspection? If you are human user receiving this message, we can add your IP address to a set of IPs that can access FederalRegister.gov & eCFR.gov; complete the CAPTCHA (bot test) below and click "Request Access". (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. 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). (2) Seats and safety belts - for poor condition and apparent defects. 1.5 Regulatory Basis. (4) Permanent marking. (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. (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. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Which aircraft record entry is the best description of the replacement of several damaged heli-coils in a casting? (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. Where should you find this entry? inspection plates, access doors, fairing, and cowling. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed 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; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. 3320 0 obj <> endobj (3) Windows and windshields - for deterioration and The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. Purpose. (Part I.D.5). (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. Learn more ME406 Series Emergency Locator Transmitter - ACR. Handbook, DUI (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. The life status must be updated each time the part is removed from a type certificated product. radio group: (1) Radio and electronic equipment - for improper installation The part may be segregated using methods that deter its installation on a type-certificated product. A __________ must be used to perform all aircraft inspections. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. (b) Rotorcraft. 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. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. (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. make up the complete empennage assembly for poor general condition, 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. Aircraft inspection checklists must be FAA approved. For the purposes of this section the following definitions apply. looseness. particles or foreign matter on screens and sump drain plugs. (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. The test point shall then be approached at a rate of approximately 3,000 feet per minute. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (5) Flexible vibration dampeners - for poor condition and (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. (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. We use cookies to improve security, personalize the user experience, enhance our marketing activities (including cooperating with our marketing partners) and for other business use. shall inspect (where applicable) the following components of the This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. Eight 1/4 -- 20 inch standard heli-coils were replaced. hXo8Wq$e`(6u+vkHIK8}dF2IDHrgkV8L:&&)aqbQ9N,Nz?R`pf8`Jy#7oU ?wu6d5-`z1 W`iP<>Fe rZo]rxQAY5n/E3B(=?nFG~|oWz{21j: lL.rSM7m9w&gcoLdl|^n e]}}_uYWuf8Le6;-U#ardHG2ps2pCQ- _r(I\W(/W$qFq|6,2 Q]:qOQ!`lO5m)_J"ok shall inspect (where applicable) the following components of the (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 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). (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. (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. (23) Cleaning or replacing fuel and oil strainers or filter elements. 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