hb```b`` |,.`f`(Tcz&^@@@#Tt$PInb`^ shall inspect (where applicable) the following components of the (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. Box beam wing construction is used on what type aircraft? 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, Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. endstream endobj startxref (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. 43.15 Additional performance rules for inspections. Most helicopters use ____________ airfoil rotor blades. (vi) Installation of parts not approved for the propeller. (3) Linkages, trusses, and members - for undue or excessive wear (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. shall inspect (where applicable) the following components of the %PDF-1.6 % (6) Batteries - for improper installation and improper charge. A tag or other record may be attached to the part. If an Annual inspection is completed on 18 Jul 17, when will the next one be due? (8) Exhaust stacks - for cracks, defects, and improper attachment. (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. 1.5 Regulatory Basis. PRINCIPLE CHANGES. The interrogations should be made at a nominal rate of 50 interrogations per second. Any other method approved or accepted by the FAA. The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? 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. (viii) Keel and chine members of boat hulls or floats. Title 14 was last amended 2/10/2023. (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. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. Airspeed limitations for a specific aircraft are found in the __________. 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. (7) All systems - for improper installation, poor general An official website of the United States government. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (4) Appliance major repairs. The part may be mutilated to deter its installation in a type certificated product. (iii) Rewinding the field coil of an electrical accessory. 2. (Part I.D.5). 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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). 23, 1964, unless otherwise noted. Appendix D. Scrap or Salvageable Aircraft Products and Articles. E 14 CFR Ch. Blade attachment and motion relative to the hub. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. The tests in (e) through (j) apply only to Mode S transponders. Which of the following contains a minimum checklist for a 100 hour inspection? (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. 311 0 obj <>stream (3) Anti-icing devices - for improper operations and obvious defects. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (2) Shock absorbing devices - for improper oleo fluid level. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. AUTHORITY: 42 U.S.C. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. 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). This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . ECO 17212. A thorough inspection will involve ___________ the aircraft. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. (b) Each person performing an annual or 100-hour inspection (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). . My Account, Forms in (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (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. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. (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. (2) Studs and nuts - for improper torquing and obvious attachment. Galvanic corrosion is also known as _________ corrosion. 43.15 Additional performance rules for inspections. 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. (3) Propeller major alterations. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (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. (a) Definitions. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (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 -. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (2) Seats and safety belts - for poor condition and apparent (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. H,Ht001300Ff l; 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. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. (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. (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. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. The proposed rule added a provision to 12 CFR 748.1 for the NCUA to require notification of any cyber incident that rises to the level of a reportable cyber incident as soon as possible but no later than 72 hours after a FICU reasonably believes that a reportable cyber incident has occurred. apparent defects. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. A __________ must be used to perform all aircraft inspections. (4) The maintenance, preventive maintenance, or alteration is recorded 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. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (2) Seats and safety belts - for poor condition and apparent defects. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. (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. 28-1.". When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. 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. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. (4) Control mechanisms - for improper operation, insecure 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. (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. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. radio group: (1) Radio and electronic equipment - for improper installation The test point shall then be approached at a rate of approximately 3,000 feet per minute. A 100 hour inspection is required on ______________. (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. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? %PDF-1.6 % ECO 17212. 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. (c) Authorized persons. (d) Transfer of life-limited parts. 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. (c) Preventive maintenance. (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. (3) Bonding and shielding - for improper installation and poor condition. Airworthiness Directives are issued primarily to: 1) A Supplemental Type Certificate may be issued to more than one applicant for the same design change, providing each applicant shows compliance with the applicable airworthiness requirement (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. Title 14 CFR part 43, 43.7(d) and 43.17(e)(2); 2. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. (f) Each person performing an annual or 100-hour inspection For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. (3) Envelope, gas bags, ballast tanks, and related parts - for 288 0 obj <> endobj Title 14 CFR part 65, 65.95(a)(1); 3. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (5) Flight and engine controls - for improper installation and improper operation. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (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. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (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 -. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (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). 43.10 - Disposition of life-limited aircraft parts. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. Purpose. Theft, Personal ); (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. (i) Power output (static and idle r.p.m. Fuselage stations are numbered in inches from the __________. The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed. 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 -. (2) Studs and nuts - for improper torquing and obvious defects. (2) Replacing elastic shock absorber cords on landing gear. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. (7) Wheels - for cracks, defects, and condition of bearings. (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. (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. 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. (a) Maintenance record entries. (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. Which maintenance action is an airframe major repair? fabric or skin deterioration, distortion, evidence of failure, The simplest rotor system is the _________. 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. (3) Windows and windshields - for deterioration and Ni}Ja7$? (6) Electrical system - for chafing and improper operation of switches. ___, (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. (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 -. 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. (2) Powerplant major repairs. (xii) Overhaul of controllable pitch propellers. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. However, this paragraph does not authorize the performance of any inspection required by Part 91 or Part 125 of this chapter or any inspection performed after a major repair or alteration. a. certified repair station b. A&P mechanic with IA rating c. either. (29) Removing, checking, and replacing magnetic chip detectors. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (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. gtag('js', new Date()); defects. Elevators move the aircraft around which axis? However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). (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. __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, looseness. Access the most extensive library of templates available. (18) Replacing wheels and skis where no weight and balance computation is involved. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (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. 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