(f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. |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. poor condition. During an annual inspection, if a defect is found which makes the aircraft un-airworthy, the person disapproving must, provide a written notice of the defect to the owner. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). attachment. 5. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. Where should you find this entry? shall inspect (where applicable) the following components of the (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. APPENDIX D TO FAR PART 43 SCOPE AND DETAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100HOUR INSPECTIONS(a) Each person performing an annual or 100hour inspection. (9) Accessories - for apparent defects in security of mounting. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (Part I.D.5). %PDF-1.6 % (i) Each person performing an annual or 100-hour inspection (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. A security threat, as defined by the TSA, will result in your mechanic application being _______. (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 -. 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. insecure attachment, improper component installation, and improper (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. 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. (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). The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. The interrogations should be made at a nominal rate of 50 interrogations per second. An official website of the United States government. A ________ helicopter has two rotors on the same mast. SOURCE: Docket No. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. The part may be legibly marked using a permanent method showing its current life status. 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. mounting, and obvious defects. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. During static balancing, an upward movement of the trailing edge of a control surface on a balance stand indicates: An overbalance designated with a (-) sign. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (6) Batteries - for improper installation and improper (23) Cleaning or replacing fuel and oil strainers or filter elements. Guide, Incorporation Title 14 was last amended 2/10/2023. (vi) Barometric scale error. by the manufacturer or Certified Repair Station. %PDF-1.6 % When must an Airworthiness Directive be complied with? (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (ii) Repairing or machining of steel hubs. The maximum time a 100 hour inspection can be extended is ______________. (7) All systems - for improper installation, poor general Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (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. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. The __________ is used to thoroughly service a component after it is removed from an aircraft. How is the pitch of the rotor blades changed in a rigid rotor system? (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (6) Engine controls - for defects, improper travel, and improper safetying. (7) Lines, hoses, and clamps - for leaks, improper condition and What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated? The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. A thorough inspection will involve ___________ the aircraft. (d) Each person performing an annual or 100-hour inspection (6) Engine controls - for defects, improper travel, and improper attachment. Which type of flap slides aft to increase the total area of the wing? radio group: (1) Radio and electronic equipment - for improper installation breakage. failure, and insecurity of attachment. (2) Shock absorbing devices - for improper oleo fluid level. Where is the throttle typically located on a helicopter? A 100 hour inspection is required on ______________. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. component operation. APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . (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. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (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 -. thoroughly clean the aircraft and aircraft engine. Title 14 CFR part 135, 135.437(b . If there is weak cylinder compression, for improper internal condition and improper internal tolerances. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. 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 (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). 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. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. Slats increase the _________ at which laminar airflow can exist. 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. Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. (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. 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. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. evidence of failure, and defective or insecure attachment of (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. 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). and found to comply with paragraph (c), appendix E, of part 43 of this chapter. hbbd``b $ @$8MO;b nHH (4) Permanent marking. Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. 7572; 49 U.S.C. (a) General. Spanish, Localized In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. Spars are to wings as__________ are to the fuselage. (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. (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. 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. 1.5 Regulatory Basis. 1.2 Applicability. (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) -. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (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. Handbook, DUI (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. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). shall inspect (where applicable) the following components of the Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. Instructions for completing the field approval checklist (see Appendix A). (2) Powerplant major repairs. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. (6) Electrical system - for chafing and improper operation of 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. Each time the part is removed from a type certificated product, the record must be updated with the current life status. (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. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. 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. fabric or skin deterioration, distortion, evidence of failure, and insecure mounting. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). What is designed to reduce drag created by wing tip vortices? 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. 295 0 obj <>/Filter/FlateDecode/ID[<77FD95543FEA6A4D8B7894588A4166BA>]/Index[288 24]/Info 287 0 R/Length 56/Prev 48674/Root 289 0 R/Size 312/Type/XRef/W[1 2 1]>>stream An aircraft Type Certificate Data Sheet contains. The person approving or disapproving return to service. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. What classification of turbulence would require an over "G" inspection? (5) Flexible vibration dampeners - for poor condition and deterioration. Which maintenance record entry best describes the action taken for a control cable showing approximately 20 percent wear on several of the individual outer wires at a fairlead? (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. Any other method approved or accepted by the FAA. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. Feb 7/2020 . Elevators move the aircraft around which axis? (e) Each person performing an annual or 100-hour inspection 23, 1964, unless otherwise noted. (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. (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) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. 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. view historical versions Title 14 Chapter I Subchapter F Part 91 Subpart E 91.411 Previous Next Top eCFR Content 91.411 Altimeter system and altitude reporting equipment tests and inspections. Most helicopters use ____________ airfoil rotor blades. (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. (5) Flexible vibration dampeners - for poor condition and 2115 0 obj <>stream The FAA acknowledges that, in accordance with 14 CFR part 43, 43.1(b), requirements do not apply to 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. 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 Which type of aircraft structures reduce fuel consumpution and increase range? (d) Performance requirements. particles or foreign matter on screens and sump drain plugs. (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. __Pass __Fail (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, function gtag(){dataLayer.push(arguments);} The test point shall be approached at a rate compatible with the test equipment. 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To thoroughly service a component after it is removed from an aircraft insecure and.