function gtag(){dataLayer.push(arguments);} Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. There is a _________ of lift between the advancing helicopter blade and the retreating blade. USLegal fulfills industry-leading security and compliance standards. Title 14 - Aeronautics and Space CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION SUBCHAPTER C - AIRCRAFT PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION 43.15 Additional performance rules for inspections. (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). (Part I.D.5). Due to aggressive automated scraping of FederalRegister.gov and eCFR.gov, programmatic access to these sites is limited to access to our extensive developer APIs. Attorney, Terms of (6) Batteries - for improper installation and improper charge. hbbd``b $ @$8MO;b nHH For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. shall inspect (where applicable) the following components of the (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. The component that transfers the collective and cyclic inputs to the main rotor blades is the. ( d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. (2) Studs and nuts - for improper torquing and obvious defects. endstream
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(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. 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. (b) Temporary removal of parts from type-certificated products. Title 14 was last amended 2/02/2023. Use the correct address and at least two incorrect addresses. 23, 1964, unless otherwise noted. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. (v) Case leak. Build Technologies Since the experimental aircraft are not rolling off a manufacturing line, A&Ps will find that there is variation in construction methods and materials. (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. (8) Exhaust stacks - for cracks, defects, and improper (2) Studs and nuts - for improper torquing and obvious defects. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. Collapse to view only 43.13 - Performance rules (general). 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. ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. 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) Studs and nuts - for improper torquing and obvious (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. 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (5) Flexible vibration dampeners - for poor condition and deterioration. (iii) Rewinding the field coil of an electrical accessory. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. shall inspect (where applicable) each installed miscellaneous item (2) Seats and safety belts - for poor condition and apparent If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 295 0 obj
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mounting. Where is the throttle typically located on a helicopter? (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. (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. (c) Except as provided in paragraph (d) of this appendix, for a major repair or major al-teration made by a person authorized in 43.17, the person who performs the major re-pair or major alteration and the person au-thorized by 43.17 to approve that work shall execute an FAA Form 337 at least in dupli-cate. Galvanic corrosion is also known as _________ corrosion. (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. (23) Cleaning or replacing fuel and oil strainers or filter elements. The rudder controls the airplane around which axis? 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. 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). 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) Powerplant major alterations. This AC addresses the manufacturing and production requirements of part 21, Where is the center of gravity located on an aircraft with tricycle landing gear? (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. (3) Servicing landing gear shock struts by adding oil, air, or both. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). The chord of an airfoil is measured from the ________ to the ________. A __________ must be used to perform all aircraft inspections. poor condition. USLegal received the following as compared to 9 other form sites. (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. shall inspect (where applicable) the following components of the (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. (6) Engine controls - for defects, improper travel, and improper (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. (e) Approval requirements. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. 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. Elevators move the aircraft around which axis? (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. thoroughly clean the aircraft and aircraft engine. Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. 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. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. If work performed on an aircraft has been done satisfactorily, the signature of an authorized person on the maintenance records for maintenance or alterations performed constitutes: approval for return to service only for the work performed. (a) General. 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attachment. (3) Anti-icing devices - for improper operations and obvious (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. deterioration. (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. Spanish, Localized 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 -. 2115 0 obj
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The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? (v) Replacement of outer laminations on fixed pitch wood propellers. (xxiii) The repair of portions of skin sheets by making additional seams. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. radio group: (1) Radio and electronic equipment - for improper installation 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. and improper internal tolerances. __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,
The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. Handbook, DUI (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. (i) Scale error. (f) Each person performing an annual or 100-hour inspection He shall (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. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (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. 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. (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. (7) All systems - for improper installation, poor general (3) That product does not accumulate time in service while the part is removed. 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". and found to comply with paragraph (c), appendix E, of part 43 of this chapter. 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 (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. Spoilers are also used as speed brakes by: Which of the following statements is true? What is the usual final step of an annual inspection before the maintenance entry is made? Which of the following contains a minimum checklist for 100-hour inspections of engines? (6) Batteries - for improper installation and improper charge. (3) Bonding and shielding - for improper installation and poor condition. The signature constitutes the approval for return to service only for the work performed. (2) The date of the inspection and aircraft total time in service. The maximum time a 100 hour inspection can be extended is ______________. (c) Disposition of parts removed from type-certificated products. 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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (5) Flight and engine controls - for improper installation and hbbd``b`Z"c`@B=8r?O K
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. Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. Title 14 CFR part 43, 43.7(d) and 43.17(e)(2); 2. 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. Business. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. What are the structural members of a semi-monocoque fuselage that prevents tension and compression from bending the fuselage? (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. How are main rotors of helicopters classified? A thorough inspection will involve ___________ the aircraft. 14 CFR 43.15 - Additional performance rules for inspections. foul the controls. Roll, pitch, yaw. 10/16/2009 AC 21-43 CHAPTER 1. (a) Definitions used in this section. (4) Appliance major repairs. A tail rotor moves (or maintains) the helicopter yaw direction by: Many helicopters use a _______ engine to drive the main transmission and rotor systems. 5. (d) Each person performing an annual or 100-hour inspection Technology, Power of (iv) Friction. 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. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. The scope of a 100 hour inspection, and annual inspection is ___________. The test point shall then be approached at a rate of approximately 3,000 feet per minute. This should only be necessary once for each IP address you access the site from. He shall thoroughly clean the aircraft and aircraft engine. (3) Windows and windshields - for deterioration and (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. (8) Exhaust stacks - for cracks, defects, and improper attachment. 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. 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