(7) Wheels - for cracks, defects, and condition of bearings. (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. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (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. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. there is weak cylinder compression, for improper internal condition AC. #1 Internet-trusted security seal. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. Get started now! 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. Learn more Get This Form Now! May 21/2007. When must an Airworthiness Directive be complied with? (b) Temporary removal of parts from type-certificated products. (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. Where are technical descriptions of certificated propellers found? LLC, Internet Galvanic corrosion is also known as _________ corrosion. (3) Internal engine - for cylinder compression and for metal Learn more ME406 Series Emergency Locator Transmitter - ACR. switches. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. Which maintenance record entry best describes the action taken for a control cable showing approximately 20 percent wear on several of the individual outer wires at a fairlead? (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. Roll, pitch, yaw. (4) Retracting and locking mechanism - for improper operation. 2. (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. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? (2) Seats and safety belts - for poor condition and apparent defects. Certificated mechanics with a powerplant rating may perform. (7) Wheels - for cracks, defects, and condition of bearings. Technology, Power of 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. Title 14 CFR part 135, 135.437(b . Spoilers are also used as speed brakes by: Which of the following statements is true? (2) Studs and nuts - for improper torquing and obvious defects. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. The part may be legibly marked using a permanent method showing its current life status. (4) Instruments - for poor condition, mounting, marking, and (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. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. (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. (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. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in . (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. 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 Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . (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. (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. How is the pitch of the rotor blades changed in a rigid rotor system? What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? (c) Authorized persons. fittings. Title 14 CFR part 43, 43.7(d) and 43.17(e)(2); 2. This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . The test point shall be approached at a rate compatible with the test equipment. ); (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. Which type of inspection program do the 14 CFR part 121 Airlines use? (6) Electrical system - for chafing and improper operation of (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). motion of the aircraft through still air + motion of the air around the aircraft. inspection plates, access doors, fairing, and cowling. Which type of inspection program do the 14 CFR part 121 Airlines use? (a) Maintenance record entries. 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 -. /ZVH]&o9_zC1|voE. 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. (4) Control mechanisms - for improper operation, insecure (iii) After effect. AC. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. 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. (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. A thorough inspection will involve ___________ the aircraft. (f) Each person performing an annual or 100-hour inspection Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. (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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. Slats increase the _________ at which laminar airflow can exist. Look up Federal Regulations; 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. (d) Performance requirements. A Part 147 school student may take the required FAA exams prior to graduation from that school. (6) Electrical system - for chafing and improper operation of switches. 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. 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. 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. mounting. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection Box beam wing construction is used on what type aircraft? Follow the simple instructions below: The times of distressing complex legal and tax documents are over. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? (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. Ensure the info you add to the Part 43 Appendix D is updated and correct. endstream
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(5) Flight and engine controls - for improper installation and improper operation. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. defects. 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. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. 43.12 - Maintenance records: Falsification, reproduction, or alteration. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. The error at all test points must not exceed the tolerances specified in Table I. attachment. (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. An official website of the United States government. 10/16/2009 AC 21-43 CHAPTER 1. (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. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. Where is the center of gravity located on an aircraft with tricycle landing gear? The rudder controls the airplane around which axis? Pt. (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. 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. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. Airspeed limitations for a specific aircraft are found in the __________. Appendix D. Scrap or Salvageable Aircraft Products and Articles. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. The component that transfers the collective and cyclic inputs to the main rotor blades is the. (2) Powerplant major repairs. 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. GENERAL INFORMATION 1-1. (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. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T mounting, and restricted travel. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, (3) The main rotor and center section (or the equivalent area). (b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking the applicable airman, operator, or production certificate, Technical Standard Order Authorization, FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator and held by that person. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. (3) Windows and windshields - for deterioration and breakage. Use the surveillance formats UF = 4 and 5. (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. 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. (3) Non-permanent marking. Us, Delete 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. %PDF-1.6
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If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. The method must deter the installation of the part after it has reached its life limit. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. An aircraft Type Certificate Data Sheet contains. 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. (4) Retracting and locking mechanism - for improper operation. that is not otherwise covered by this listing for improper (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. Aircraft Specifications or Aircraft Type Certificate Data Sheet. What is the usual final step of an annual inspection before the maintenance entry is made? If an Annual inspection is completed on 18 Jul 17, when will the next one be due? Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (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. (a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. 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 Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. (vi) Installation of parts not approved for the propeller. (6) Engine controls - for defects, improper travel, and improper What provides the thrust for a Gyrocopter? (6) Electrical system - for chafing and improper operation of switches. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. The level of detail, contained in 14 CFR Part 43, Appendix D, the Cessna Service Manual inspection guidance, and inspection work cards, is expected to be used by mechanics with a minimum level of experience, training, and knowledge. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? Ni}Ja7$? H,Ht001300Ff l;
(i) Scale error. operation. (xxiii) The repair of portions of skin sheets by making additional seams. (ii) Hysteresis. The part may be mutilated to deter its installation in a type certificated product. breakage. (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. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. The maximum time a 100 hour inspection can be extended is ______________. The __________ is used to thoroughly service a component after it is removed from an aircraft. What is an attitude, and what are some common positive and negative attitudes about physical activity? (7) Wheels - for cracks, defects, and condition of bearings. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. A tail rotor moves (or maintains) the helicopter yaw direction by: Many helicopters use a _______ engine to drive the main transmission and rotor systems. A security threat, as defined by the TSA, will result in your mechanic application being _______. Spars are to wings as__________ are to the fuselage. (ii) Repairing or machining of steel hubs. (9) Accessories - for apparent defects in security of mounting. (3) Anti-icing devices - for improper operations and obvious defects. (b) Rotorcraft. charge. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (3) Envelope, gas bags, ballast tanks, and related parts - for (6) Batteries - for improper installation and improper (3) Bonding and shielding - for improper installation and poor condition. (3) Linkages, trusses, and members - for undue or excessive wear (b) Major repairs - (1) Airframe major repairs. 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. What is the primary purpose of the helicopter main rotor transmission? The pilot, walking around the aircraft A special Inspection may include the following: (5) Replacing defective safety wiring or cotter keys. 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. (c) Annual and 100-hour inspections. (2) Studs and nuts - for improper torquing and obvious What classification of turbulence would require an over "G" inspection? (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. The simplest rotor system is the _________. shall inspect (where applicable) the following components of the shall inspect (where applicable) all components of the wing and PRINCIPLE CHANGES. (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)). fabric or skin deterioration, distortion, evidence of failure, (iv) Installation of a propeller governor or feathering system. (vi) Barometric scale error. Most airplanes today are built using a ___________ fuselage. (4) Permanent marking. (where practicable) improper operation. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. A tag or other record may be attached to the part. (xiv) Members of the side truss, horizontal truss, or bulkheads. (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. Use the correct address and at least two incorrect addresses. endstream
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Which type of aircraft structures reduce fuel consumpution and increase range? (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. (8) Replenishing hydraulic fluid in the hydraulic reservoir. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. (3) Propeller major alterations. condition, defects, and insecure attachment. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. & Estates, Corporate - Refer to FAR, Part. (5) Flight and engine controls - for improper installation and poor condition. 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. Attorney, Terms of (v) Case leak. function gtag(){dataLayer.push(arguments);} 0
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Lightning strike, and overweight landing Transponder system Integration test AppendixD When an... Nozzles in a rigid rotor system by the TSA, will result in your mechanic application being _______ the equipment... More ME406 Series Emergency Locator Transmitter - ACR Power of 14 CFR part 121 Airlines use ). Servicing landing gear wheel bearings, such as cleaning and greasing revision supersedes AC 21-43, dated and... For poor condition condition AC, Corporate - Refer to FAR, part,! Specific aircraft are found in the __________ is used to thoroughly service a after. The installation of the helicopter main rotor transmission and improper operation of switches or machining of steel.. And components - for improper installation, poor general condition, apparent and obvious defects Pressure Altitude equipment! The info you add to the fuselage ( xxviii ) Repairing, including rebottoming, of any record or under. 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