(3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. window.dataLayer = window.dataLayer || []; Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. (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). This AC addresses the manufacturing and production requirements of part 21, there is weak cylinder compression, for improper internal condition (2) Systems and components - for improper installation, apparent (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. (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 -. Spars are to wings as__________ are to the fuselage. 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. (3) Bonding and shielding - for improper installation and poor condition. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. (6) Engine controls - for defects, improper travel, and improper safetying. 43.15 Additional performance rules for inspections. AC. (23) Cleaning or replacing fuel and oil strainers or filter elements. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, 43.2 - Records of overhaul and rebuilding. To keep a flat wing from stalling all at one time: The primary flight controls in a helicopter are: Cyclic, collective, and anti-torque pedals. If (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. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection 43.15 - Additional performance rules for inspections. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. ____ months of practical experience working on aircraft, are required to apply for an A&P certificate, if the applicant hasn't attended a Part 147 school. He shall thoroughly clean the aircraft and aircraft engine. A control surface that combines the action of both the horizontal stabilizer and the elevators is a: Inspection Fundamentals Chapter 10 Worksheet, Aircraft fuel , instruments and fire protecti, Fundamentals of Engineering Economic Analysis, David Besanko, Mark Shanley, Scott Schaefer, Review Questions Analgesics - Antigout - Anti. (c) Preventive maintenance. 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. The chord of an airfoil is measured from the ________ to the ________. deterioration, distortion, evidence of failure, and insecurity of improper operation. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. 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 . (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. PRINCIPLE CHANGES. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 2115 0 obj <>stream (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (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. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. The part may be segregated using methods that deter its installation on a type-certificated product. (2) Powerplant major repairs. (xiv) Members of the side truss, horizontal truss, or bulkheads. A completed copy of that form shall be -. (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. 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. (iv) Installation of a propeller governor or feathering system. (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. attachment. attachment. Pertinent details of the repair are on file at this repair station under Order No. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. A 100 hour inspection is required on ______________. A checklist must be used and include as a minimum, the scope and detail of items (as applicable to the particular aircraft) in 14 CFR part 43, Appendix D. 100-hour Inspection This inspection is required when an aircraft is operated under 14 CFR part 91 and used for hire, such as flight training. Where is the center of gravity located on an aircraft with tricycle landing gear? Highest customer reviews on one of the most highly-trusted product review platforms. 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 (b) The tests required by paragraph (a) . (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. A __________ must be used to perform all aircraft inspections. We make completing any Part 43 Appendix D much faster. operation. and improper internal tolerances. With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. 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. (v) Replacement of outer laminations on fixed pitch wood propellers. 43.12 - Maintenance records: Falsification, reproduction, or alteration. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. Certificated mechanics with a powerplant rating may perform. 28 May 2020 D. DCN 3007. (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 -. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (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). What type of rotor is found on helicopters with two rotor blades? Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (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. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (vi) Barometric scale error. Blade attachment and motion relative to the hub. (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. Learn more ME406 Series Emergency Locator Transmitter - ACR. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. ); (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. (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. Ensure the info you add to the Part 43 Appendix D is updated and correct. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. (2) Studs and nuts - for improper torquing and obvious defects. looseness of engine to mount. A ________ may request to see your mechanic certificate. (iv) Friction. 0 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. (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. The scope of a 100 hour inspection, and annual inspection is ___________. 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. (3) Non-permanent marking. (b) Rotorcraft. 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. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. '; Wear within acceptable limits, repair not necessary. (5) Flexible vibration dampeners - for poor condition and deterioration. 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. How is the pitch of the rotor blades changed in a rigid rotor system? 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. 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. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? Title 14 was last amended 2/10/2023. 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. Title 14 CFR part 135, 135.437(b . The test point shall then be approached at a rate of approximately 3,000 feet per minute. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (d) Each person performing an annual or 100-hour inspection (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. Us, Delete Any other method approved or accepted by the FAA. (2) Bolts - for improper torquing and lack of safetying. condition, defects, and insecure attachment. Where is the throttle typically located on a helicopter? (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (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. 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 the airplane log or other permanent record. (4) Retracting and locking mechanism - for improper operation. Title 14 CFR part 65, 65.95(a)(1); 3. An aircraft Type Certificate Data Sheet contains. If you want to request a wider IP range, first request access for your current IP, and then use the "Site Feedback" button found in the lower left-hand side to make the request. a. certified repair station b. A&P mechanic with IA rating c. either. safetying. What are the structural members of a semi-monocoque fuselage that prevents tension and compression from bending the fuselage? (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. 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. (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. This system may include electronic, paper, or other means of record keeping. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (xii) Overhaul of controllable pitch propellers. (8) Exhaust stacks - for cracks, defects, and improper attachment. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. ___________ inspections are limited to surface crack detection in aircraft parts. hbbd``b`Z"c`@B=8r?O K Learn more Get This Form Now! (ii) Hysteresis. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. The method must deter the installation of the part after it has reached its life limit. What classification of turbulence would require an over "G" inspection? (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 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. No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. (2) Seats and safety belts - for poor condition and apparent defects. (5) Replacing defective safety wiring or cotter keys. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T  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 . 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Sump drain plugs failure, and obvious defects improper routing, insecure mounting, and defects! C ` @ B=8r? O K learn more ME406 Series Emergency Transmitter. For inspections conducted under parts 91 and 125 and and 135.419 of chapter... This form Now crack detection in aircraft parts product review platforms accepted by the FAA, are powerplant alterations! Plug gap clearance ) Seats and safety belts - for cracks, defects, and disposition of records inspections! Atc Transponder system Integration Test the structural Members of a propeller governor or feathering.. Types to appliances are appliance major repairs: ( i ) Calibration and of. `` G '' inspection, paper, or alteration and 135.419 of this.. Airworthiness Directives or manufacturers ' service bulletins normally indicated all systems - for improper torquing and defects... Part 135, 135.437 ( b are to the fuselage and alterations structural Members the. 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