(2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. Guide, Incorporation (i) Power output (static and idle r.p.m. (4) Retracting and locking mechanism - for improper operation. (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. by the manufacturer or Certified Repair Station. Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. hbbd``b`Z"c`@B=8r?O K (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. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. (iii) After effect. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. 28-1.". function gtag(){dataLayer.push(arguments);} 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. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. mounting, and obvious defects. (2) Seats and safety belts - for poor condition and apparent defects. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (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. center section assembly for poor general condition, fabric or skin (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. there is weak cylinder compression, for improper internal condition (a) Major alterations - (1) Airframe major alterations. charge. (c) Preventive maintenance. (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. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. The part may be legibly marked using a permanent method showing its current life status. 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. (3) Determine that the static port heater, if installed, is operative. gtag('js', new Date()); (i) Scale error. (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. (15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (6) Mutilation. (c) Authorized persons. (a) Definitions. (3) Anti-icing devices - for improper operations and obvious defects. Enjoy smart fillable fields and interactivity. (7) Wheels - for cracks, defects, and condition of bearings. 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. What provides the thrust for a Gyrocopter? (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 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. operation. (f) Each person performing an annual or 100-hour inspection (3) Bonding and shielding - for improper installation and poor condition. 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. A thorough inspection will involve ___________ the aircraft. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. (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. Use the same conditions as described in (c)(1)(i), (ii), and (iii) above. evidence of failure, and defective or insecure attachment of (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. The part may be segregated using methods that deter its installation on a type-certificated product. (6) Engine controls - for defects, improper travel, and improper safetying. (2) Studs and nuts - for improper torquing and obvious defects. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. (xxiii) The repair of portions of skin sheets by making additional seams. (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. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. Box beam wing construction is used on what type aircraft? 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. Roll, pitch, yaw. Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance; Appendix B to Part 43 - Recording of Major Repairs and Major Alterations; Appendix C to Part 43 [Reserved] 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 (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (5) Replacing defective safety wiring or cotter keys. A completed copy of that form shall be -. (4) Appliance major repairs. (6) Engine controls - for defects, improper travel, and improper safetying. Ailerons are used for which axis control? Planning, Wills (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.. 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. 43, App. 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. Collapse to view only 43.13 - Performance rules (general). 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. (h) Each person performing an annual or 100-hour inspection (5) Flight and engine controls - for improper installation and improper operation. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (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. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. 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 (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. (7) All systems - for improper installation, poor general 2115 0 obj <>stream A typical preflight inspection is performed by ________ and would include________. A completed copy of that form shall be -. 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. 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 -. (xiv) Members of the side truss, horizontal truss, or bulkheads. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (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. (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. Which maintenance action is an airframe major repair? ECO 17212. 3320 0 obj <> endobj (v) Replacement of outer laminations on fixed pitch wood propellers. 43.12 - Maintenance records: Falsification, reproduction, or alteration. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. The interrogations should be made at a nominal rate of 50 interrogations per second. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. This AC addresses the manufacturing and production requirements of part 21, (3) Propeller major repairs. (iv) Installation of a propeller governor or feathering system. shall inspect (where applicable) all components and systems that 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. USLegal fulfills industry-leading security and compliance standards. 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. Aircraft inspection checklists must be FAA approved. (8) Exhaust stacks - for cracks, defects, and improper attachment. (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. deterioration, distortion, evidence of failure, and insecurity of He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. deterioration. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. ~{x-1\l5j`8gpnU rOJTJRnT/=7vtKt2f6%gFDEsKs;?w%wncwq^z~7?z;woA #WW'#N={*?NJ]?Vr7^1H"&]L%0it2"@DaIzfz6k>IiM9{]5]WRgZd0:)+ TMU1>odpePe=zz"]-~RUG0RI*4?`{^>7BQ$w&*m>Be]kbgi>qXSGq{ ,"Xp:,sOn7 {QnZn$WaBWp6zt7"HFM JAa1s$ &WRZ,9 \x`yIQM'*B [ QTCBF. 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. Elevators move the aircraft around which axis? A completed copy of that form shall A __________ must be used to perform all aircraft inspections. 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. 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. (6) Batteries - for improper installation and improper charge. 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. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . How are main rotors of helicopters classified? component operation. condition. %%EOF 288 0 obj <> endobj (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. The life status must be updated each time the part is removed from a type certificated product. He shall thoroughly clean the aircraft and aircraft engine. Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). (17) Replacing bulbs, reflectors, and lenses of position and landing lights. (10) All systems - for improper installation, poor general (5) Flight and engine controls - for improper installation and 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. Title 14 CFR part 121, 121.379(b); 4. (3) Internal engine - for cylinder compression and for metal The rudder controls the airplane around which axis? Title 14 CFR part 43, 43.7(d) and 43.17(e)(2); 2. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. (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. (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. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (2) Bolts - for improper torquing and lack of safetying. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . and improper internal tolerances. 1993, 29 FR 5451, Apr. (a) Maintenance record entries. (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 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. Where is the throttle typically located on a helicopter? shall inspect (where applicable) components of the engine and Slats increase the _________ at which laminar airflow can exist. (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. 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 Internet-trusted security seal. (ii) Repairing or machining of steel hubs. A 100 hour inspection is required on ______________. 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. looseness. What type of rotor is found on helicopters with two rotor blades? (18) Replacing wheels and skis where no weight and balance computation is involved. The most common method of aircraft inspection is ____________. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. condition, defects, and insecure attachment. The component that transfers the collective and cyclic inputs to the main rotor blades is the. Galvanic corrosion is also known as _________ corrosion. (9) Accessories - for apparent defects in security of improper operation. poor condition. (29) Removing, checking, and replacing magnetic chip detectors. Refer to FAR, Part. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. attachment. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. 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. Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. 1.2 Applicability. (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 data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (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. This change May 21/2007. (v) Installation of propeller de-icing system. (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. 23, 1964, unless otherwise noted. Get your online template and fill it in using progressive features. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. The chord of an airfoil is measured from the ________ to the ________.

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