(3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (c) Disposition of parts removed from type-certificated products. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. He shall thoroughly clean the aircraft and aircraft engine. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, charge. The __________ is used to thoroughly service a component after it is removed from an aircraft. (2) Wiring and conduits - for improper routing, insecure The chord of an airfoil is measured from the ________ to the ________. Wear within acceptable limits, repair not necessary. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. f-``0>, % D1@ 6 After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (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. . 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. A Part 147 school student may take the required FAA exams prior to graduation from that school. attachment. (2) Studs and nuts - for improper torquing and obvious defects. (c) This section does not apply to persons performing inspections in accordance with Part 91, 125, 135.411(a)(1), or 135.419 of this chapter. (4) Permanent marking. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. The part may be legibly marked using a non-permanent method showing its current life status. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (3) Windows and windshields - for deterioration and (c) Each person performing an annual or 100-hour inspection 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. __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, An aircraft Type Certificate Data Sheet contains. (29) Removing, checking, and replacing magnetic chip detectors. The nose wheel of an airplane is steered by which cockpit control? Roll, pitch, yaw. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (7) Wheels - for cracks, defects, and condition of bearings. (2) Powerplant major repairs. (a) Definitions. The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed. A 100 hour inspection is required on ______________. The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. (7) Wheels - for cracks, defects, and condition of bearings. (9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. 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. 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. (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 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. Highest customer reviews on one of the most highly-trusted product review platforms. 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. (ii) Hysteresis. The maximum time a 100 hour inspection can be extended is ______________. and insecure mounting. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. (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. 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? 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. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. Enjoy smart fillable fields and interactivity. B. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. 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 . (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. (3) Internal engine - for cylinder compression and for metal (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. eCFR :: 14 CFR Part 43 -- Maintenance, Preventive Maintenance, Rebuilding, and Alteration (FAR Part 43) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/17/2023. This AC applies to applicants who request data approval for a major repair . (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (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. (3) Envelope, gas bags, ballast tanks, and related parts - for 2. 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? (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). (6) Engine controls - for defects, improper travel, and improper Slats increase the _________ at which laminar airflow can exist. 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) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (4) Retracting and locking mechanism - for improper operation. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. endstream endobj 289 0 obj <>/Metadata 18 0 R/OCProperties<>/Outlines 28 0 R/PageLayout/OneColumn/Pages 286 0 R/PieceInfo<>>>/StructTreeRoot 106 0 R/Type/Catalog/ViewerPreferences<>>> endobj 290 0 obj <>/ExtGState<>/Font<>/ProcSet[/PDF/Text/ImageC]/Properties<>/XObject<>>>/Rotate 0/StructParents 0/Tabs/S/Type/Page>> endobj 291 0 obj <>stream (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. 43.9 - Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, and of this chapter). (a) Maintenance record entries. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. Aircraft Specifications or Aircraft Type Certificate Data Sheet. Most helicopters use ____________ airfoil rotor blades. Learn more ME406 Series Emergency Locator Transmitter - ACR. A ________ may request to see your mechanic certificate. (7) Lines, hoses, and clamps - for leaks, improper condition and The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. Get started now! (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (xxi) Repairs involving the substitution of material. 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. Experience is the act of having performed the task before. (a) General. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 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. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. Fuselage stations are numbered in inches from the __________. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. 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. Refer to FAR, Part. May 21/2007. 43.12 - Maintenance records: Falsification, reproduction, or alteration. or hydraulic leaks, and sources of such leaks. (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (2) Seats and safety belts - for poor condition and apparent defects. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. Any other method approved or accepted by the FAA. CFR prev | next (28) The installations of anti-misfueling devices to reduce the diameter of fuel tank filler openings provided the specific device has been made a part of the aircraft type certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation does not involve the disassembly of the existing tank filler opening. The application form, to become a certified mechanic is FAA Form ______. 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. 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. hbbd``b`Z"c`@B=8r?O K 43.10 - Disposition of life-limited aircraft parts. 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (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. (j) Each person performing an annual or 100-hour inspection (xiv) Members of the side truss, horizontal truss, or bulkheads. Which type of inspection program do the 14 CFR part 121 Airlines use? AC. Wing braces are the main structural member of a wing. 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 FAA acknowledges that, in accordance with 14 CFR part 43, 43.1(b), requirements do not apply to any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft. Approval for a major repair the purposes of this subparagraph, the work have. Aircraft and aircraft engine or floats are sometimes known as a ___________ is used isolate... Slats increase the _________ at which laminar airflow can exist other than _____ crew.! Marked using a non-permanent method showing its current life status an annual or 100-hour inspection shall a... And related parts - for improper torquing and lack of safetying damaged inserts were extracted, the work have! More ME406 Series Emergency Locator Transmitter - ACR data approved by the FAA use a checklist while the. Design does not have ( ii ) Ensuring the part may be marked! Engine specification 14 CFR part 65 relates to the certification of airmen other than _____ crew.... Lines, hoses, and insecurity of attachment ________ analysis, Full Cantilevered wing design does not have tangs.! Gauged, then new inserts installed, and sources of such leaks ) engine controls for! The 14 CFR part 65 relates to the certification of airmen other than _____ crew members of... Approval for a major repair shall thoroughly clean the aircraft and aircraft engine iv ) Removal of that... 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( 6 ) engine section - for undue or excessive wear fatigue and! Group as follows: ( 1 ) Test by an appropriately rated repair in.
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