The mechanic, and the repairman certifications are considered to be different classifications by the FAA: A mechanic must hold their license for ____ years to be eligible for an Inspection Authorization. He shall Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. A. as specific in the AD B. during the next scheduled inspection C. at the next scheduled overhaul as specific in the AD Which of the following contains a table that lists the engines to which a gives propeller is adaptable? Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. Most airplanes today are built using a ___________ fuselage. Newton's third law, for every action there is an equal and opposite reaction, is best demonstrated by: When air flows over the camber of a wing, the air velocity: An airfoil will maintain lift any time it has air moving across it, but: Leading edge flaps are ____________ of the trailing edge flaps. (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. Water vapor weighs 5/8 as much as dry air. (b) Applicability. (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). Any other method approved or accepted by the FAA. Certificated mechanics with a powerplant rating may perform. 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. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. 288 0 obj <> endobj Box beam wing construction is used on what type aircraft? When the angle of attack of an airfoil is increased so it reaches maximum lift the: Ribs can be ___________ by stamping holes in the assembly. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. What provides the thrust for a Gyrocopter? 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. (a) Major alterations - (1) Airframe major alterations. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. The material's internal resistance or counterforce that opposes deformation is called: When the lift force is in equilibrium with the weight force, the aircraft: What type of stress resists a crushing force? (d) Each person performing an annual or 100-hour inspection These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (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. (b) Rotorcraft. Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. Decrease engine output RPM to optimum rotor RPM. (2) Shock absorbing devices - for improper oleo fluid level. 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. This system may include electronic, paper, or other means of record keeping. (5) Segregation. (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. Where should you find this entry? After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. Title 14 CFR part 121, 121.379(b); 4. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil How are main rotors of helicopters classified? (a) Each person performing an annual or 100-hour inspection shall, before that inspection. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. 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. B. 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. (3) Windows and windshields - for deterioration and breakage. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 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. Airspeed limitations for a specific aircraft are found in the __________. (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. shall inspect (where applicable) the following components of the During the next week, create a list of at least 10 things you could have done to conserve the water you use. (5) Flight and engine controls - for improper installation and improper operation. Make sure that every field has been filled in properly. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. (3) Linkages, trusses, and members - for undue or excessive wear Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. What is an attitude, and what are some common positive and negative attitudes about physical activity? This advisory circular (AC) has been updated to reflect changes to Title 14 of the Code of Federal Regulations (14 CFR) part 43, regarding preventive maintenance. How does a pilot compensate for blowback? (b) Major repairs - (1) Airframe major repairs. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. The nose wheel of an airplane is steered by which cockpit control? %PDF-1.6 % 1993, 29 FR 5451, Apr. Which type of flap slides aft to increase the total area of the wing? by the manufacturer or Certified Repair Station. Title 14 CFR part 65, 65.95(a)(1); 3. (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) 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. (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. (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. When must an Airworthiness Directive be complied with? 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? (4) Servicing landing gear wheel bearings, such as cleaning and greasing. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. Which type of inspection program do the 14 CFR part 121 Airlines use? The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). endstream endobj startxref (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (7) Wheels - for cracks, defects, and condition of bearings. 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 A completed copy of that form shall Acceptable methods include: (1) Record keeping system. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). 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). Guide, Incorporation Responsibility for compliance with ADs and upkeep of maintenance records lies with the: Who is responsible for making the log book entry after an Annual, 100 hour, or Progressive Inspection? What is designed to reduce drag created by wing tip vortices? 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. (v) Replacement of outer laminations on fixed pitch wood propellers. condition, defects, and insecure attachment. 14 CFR 43.15 - Additional performance rules for inspections. Title 14 of the Code of Federal Regulations (14 CFR) part 43, 43.7 specifies persons authorized to approve an aircraft or aircraft component for return to apparent defects. The error at all test points must not exceed the tolerances specified in Table I. (6) Engine controls - for defects, improper travel, and improper safetying. (d) Progressive inspection. 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. (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. Ailerons are used for which axis control? The interrogations should be made at a nominal rate of 50 interrogations per second. Appendix D to Part 43Scope and Detail of Items (as Applicable to the Particular (a) Each person performing an annual or 100-hour inspection shall, before that inspection 28 May 2020 D. DCN 3007. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. My Account, Forms in Technology, Power of (2) Seats and safety belts - for poor condition and apparent defects. (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. What is the primary purpose of the helicopter main rotor transmission? (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (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. cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. 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. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection (b) Temporary removal of parts from type-certificated products. 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. (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. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. Experience is the act of having performed the task before. (3) The main rotor and center section (or the equivalent area). 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (3) That product does not accumulate time in service while the part is removed. (iii) Rewinding the field coil of an electrical accessory. With US Legal Forms the process of creating legal documents is anxiety-free. (3) Anti-icing devicesfor improper oper- A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. By an identification letter stamped on one of the hexes of the nozzle body (5) Flexible vibration dampeners - for poor condition and (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. (3) Bonding and shielding - for improper installation and poor condition. 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. (8) Replenishing hydraulic fluid in the hydraulic reservoir. looseness of engine to mount. Purpose. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (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. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. (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. 14 CFR 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) | US Law | LII / Legal Information Institute LII Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space (xiv) Members of the side truss, horizontal truss, or bulkheads. Sign off for an annual inspection can be done by who? 43.7 - Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. deterioration. (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. Ensures that a website is free of malware attacks. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). The holder of an IA cannot . (xv) Main seat support braces and brackets. For the purposes of this section the following definitions apply. %PDF-1.6 % A typical preflight inspection is performed by ________ and would include________. The ________ is the location from which all other stations are measured. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. 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. (i) Each person performing an annual or 100-hour inspection condition. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (2) Shock absorbing devices - for improper oleo fluid level. A 100 hour inspection is required on ______________. Aircraft Specifications or Aircraft Type Certificate Data Sheet. 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. 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. (2) Shock absorbing devices - for improper oleo fluid level. Moving the cyclic pitch control of a two bladed system increases the AOA of one rotor blade with the result that a _______ lifting force is applied at that point in the plane of rotation. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (5) Replacing defective safety wiring or cotter keys. (2) Studs and nuts - for improper torquing and obvious This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. (b) Listing of discrepancies and placards. The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. (c) Preventive maintenance. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. 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