The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. (3) Windows and windshields - for deterioration and breakage. A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. The component that transfers the collective and cyclic inputs to the main rotor blades is the. (4) Permanent marking. 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. Which type of flap slides aft to increase the total area of the wing? Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. defects. The part may be legibly marked using a non-permanent method showing its current life status. view historical versions Title 14 Chapter I Subchapter C Part 43 View Full Text Previous Next Top (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. (iii) Rewinding the field coil of an electrical accessory. Blade attachment and motion relative to the hub. (b) Rotorcraft. The part may be mutilated to deter its installation in a type certificated product. ___________ inspections are limited to surface crack detection in aircraft parts. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. deterioration. (6) Electrical system - for chafing and improper operation of After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. H,Ht001300Ff l; ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. attachment. (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. Forms, Real Estate 43.9 - Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, and of this chapter). (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. Where are technical descriptions of certificated propellers found? Certificated mechanics with a powerplant rating may perform. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. (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). (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. Experience is the act of having performed the task before. (4) Retracting and locking mechanism - for improper operation. (iii) Performed without the use of tools and/or special equipment. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. (i) Power output (static and idle r.p.m. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (xii) Overhaul of controllable pitch propellers. (2) Seats and safety belts - for poor condition and apparent (viii) Keel and chine members of boat hulls or floats. (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. (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. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T  cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might (3) Anti-icing devices - for improper operations and obvious AUTHORITY: 42 U.S.C. The holder of an IA cannot . Airspeed limitations for a specific aircraft are found in the __________. (iv) Friction. 43.15 - Additional performance rules for inspections. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. (f) Mode S Address: Interrogate the Mode S transponder and verify that it replies only to its assigned address. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. What classification of turbulence would require an over "G" inspection? The person approving or disapproving return to service. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. (where practicable) improper operation. 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. endstream endobj startxref (23) Cleaning or replacing fuel and oil strainers or filter elements. make up the complete empennage assembly for poor general condition, Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. 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). The tag or record must include the part number, serial number, and current life status of the part. (6) Electrical system - for chafing and improper operation of switches. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . (3) Windows and windshields - for deterioration and insecure mounting, and improper operation. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. Appendix F to Part 43 - ATC Transponder Tests and Inspections 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. condition, defects, and insecure attachment. (d) Transfer of life-limited parts. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. (c) Each person performing an annual or 100-hour inspection 4. What type of rotor is found on helicopters with two rotor blades? (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. Pt. Pertinent details of the repair are on file at this repair station under Order No. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. Learn more Get This Form Now! (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). /ZVH]&o9_zC1|voE. shall, before that inspection, remove or open all necessary (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? 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. safetying. Every part of an aircraft must be planned to carry the load imposed upon it. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. USLegal has been awarded the TopTenREVIEWS Gold Award 9 years in a row as the most comprehensive and helpful online legal forms services on the market today. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (3) Servicing landing gear shock struts by adding oil, air, or both. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. (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. charge. (xiv) The repair or replacement of internal elements of blades. there is weak cylinder compression, for improper internal condition A completed copy of that form shall Which of the following contains a minimum checklist for 100-hour inspections of engines? GENERAL INFORMATION 1-1. Instrument repairs may be performed ___________________________. (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. operation. component operation. 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? (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. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (6) Electrical system - for chafing and improper operation of switches. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (h) Each person performing an annual or 100-hour inspection (ii) Monocoque or semimonocoque wings or control surfaces. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. 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. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (v) Case leak. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. & Estates, Corporate - (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. (21) Replacing any hose connection except hydraulic connections. (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. (3) Bonding and shielding - for improper installation and poor 1993, 29 FR 5451, Apr. B. The application form, to become a certified mechanic is FAA Form ______. A Part 147 school student may take the required FAA exams prior to graduation from that school. Galvanic corrosion is also known as _________ corrosion. (2) Bolts - for improper torquing and lack of safetying. 2. (i) Power output (static and idle r.p.m. How is the pitch of the rotor blades changed in a rigid rotor system? The rudder controls the airplane around which axis? Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. . 3320 0 obj <> endobj (a) General. hb```b`` |,.`f`(Tcz&^@@@#Tt$PInb`^ (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. (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 -. (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. (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. (vi) Installation of parts not approved for the propeller. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). 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. 0 looseness of engine to mount. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (a) Each person performing an annual or 100-hour inspection shall, before that 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. This change (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. The part may be segregated using methods that deter its installation on a type-certificated product. (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. hbbd``b $ @$8MO;b nHH motion of the aircraft through still air + motion of the air around the aircraft. 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. (a) Definitions used in this section. 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. deterioration, distortion, evidence of failure, and insecurity of 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. (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. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. A typical preflight inspection is performed by ________ and would include________. (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). (c) Preventive maintenance. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. Another common name for radiographic inspections is ______________. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil Spanish, Localized An airplane with a nose and main landing gear is referred to as being: _________ ___________ and _________ _________ are used to move fowler flaps along their designed route of travel. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 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. Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. 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. inspection plates, access doors, fairing, and cowling. 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. (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. attachment. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. shall inspect (where applicable) the following components of the (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. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (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. (3) Anti-icing devices - for improper operations and obvious defects. Guarantees that a business meets BBB accreditation standards in the US and Canada. What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. Which type of inspection program do the 14 CFR part 121 Airlines use? Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. Ni}Ja7$? (xv) Main seat support braces and brackets. (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. (e) Approval requirements. E 14 CFR Ch. The method must deter the installation of the part after it has reached its life limit. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Wing braces are the main structural member of a wing. PRINCIPLE CHANGES. 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