(4) Engine mount - for cracks, looseness of mounting, and or hydraulic leaks, and sources of such leaks. Feb 7/2020 . A thorough inspection will involve ___________ the aircraft. 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. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. USLegal fulfills industry-leading security and compliance standards. Any other method approved or accepted by the FAA. APPENDIX Appendix A - Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance, APPENDIX Appendix B - Appendix B to Part 43 - Recording of Major Repairs and Major Alterations, APPENDIX Appendix C - Appendix C to Part 43 [Reserved], APPENDIX Appendix D - Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, APPENDIX Appendix E - Appendix E to Part 43 - Altimeter System Test and Inspection, APPENDIX Appendix F - Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. (c) Authorized persons. The scope of a 100 hour inspection, and annual inspection is ___________. defects, and unsatisfactory operation. The part may be legibly marked using a non-permanent method showing its current life status. (3) Propeller major repairs. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. Most helicopters use ____________ airfoil rotor blades. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (iv) Friction. Ensures that a website is free of malware attacks. 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. (h) Each person performing an annual or 100-hour inspection (7) Wheels - for cracks, defects, and condition of bearings. (3) Servicing landing gear shock struts by adding oil, air, or both. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. Which type of flap slides aft to increase the total area of the wing? poor condition. The pilot, walking around the aircraft A special Inspection may include the following: (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. 295 0 obj <>/Filter/FlateDecode/ID[<77FD95543FEA6A4D8B7894588A4166BA>]/Index[288 24]/Info 287 0 R/Length 56/Prev 48674/Root 289 0 R/Size 312/Type/XRef/W[1 2 1]>>stream (9) Accessories - for apparent defects in security of mounting. APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? AC. (2) The date of the inspection and aircraft total time in service. (ii) Hysteresis. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. Learn more Get This Form Now! endstream endobj startxref radio group: (1) Radio and electronic equipment - for improper installation Most airplanes today are built using a ___________ fuselage. 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. 3335 0 obj <>/Filter/FlateDecode/ID[]/Index[3320 28 3615 1]/Info 3319 0 R/Length 87/Prev 1015044/Root 3321 0 R/Size 3616/Type/XRef/W[1 2 1]>>stream (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. (j) Each person performing an annual or 100-hour inspection view historical versions Title 14 Chapter I Subchapter C Part 43 View Full Text Previous Next Top (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? (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 -. Refer to FAR, Part. Spanish, Localized What provides the thrust for a Gyrocopter? (b) Major repairs - (1) Airframe major repairs. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. 5. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). (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. Use the correct address and at least two incorrect addresses. (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. that is not otherwise covered by this listing for improper LLC, Internet (5) Flight and engine controls - for improper installation and improper operation. 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. (3) Bonding and shielding - for improper installation and poor condition. (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. Eight 1/4 -- 20 inch standard heli-coils were replaced. (2) Tag or record attached to part. 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 mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. (7) Wheels - for cracks, defects, and condition of bearings. (xxiii) The repair of portions of skin sheets by making additional seams. The altimeter shall be kept at this pressure for at least 1 minute, but not more than 10 minutes, before the test reading is taken. (iii) After effect. (e) Each person performing an annual or 100-hour inspection ____ 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. (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 holder of an IA cannot . May 21/2007. (5) Replacing defective safety wiring or cotter keys. (b) The tests required by paragraph (a) . For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. 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. (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. 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. 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. thoroughly clean the aircraft and aircraft engine. Acceptable methods include: (1) Record keeping system. Theft, Personal 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 test point shall be approached at a rate compatible with the test equipment. 288 0 obj <> endobj (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). (v) Installation of structural parts other than the type of parts approved for the installation. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (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. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (xii) Overhaul of controllable pitch propellers. This should only be necessary once for each IP address you access the site from. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. Collapse to view only 43.13 - Performance rules (general). (5) Flexible vibration dampeners - for poor condition and (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. The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. 2. A 100 hour inspection is required on ______________. (10) Floats and skis - for insecure attachment and obvious or apparent defects. Purpose. (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 -. (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. (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)). The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). Get access to thousands of forms. 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. He shall The life status must be updated each time the part is removed from a type certificated product. (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 -. 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. 7572; 49 U.S.C. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. USLegal has been awarded the TopTenREVIEWS Gold Award 9 years in a row as the most comprehensive and helpful online legal forms services on the market today. (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. The two basic types of powered aircraft are referred as what? 'wV:D 4MKb!l?`Jnm>M$GG`[Qb,cPJ'9@_)FB hxJXH$J}1 98}S:pD>.Uq[/g-9y~Reu T.AD::o@8]RfZ>28j \vd,DIE:DvH@wbEhZr17L?sWo8V' *ffQ$ ='|;\]Qru1z%[oWz|_x%l7dGzPtg8[SiN}_l,rf~!o7NIqaMhtosb3!M&Ml{Eo)plz^G>}m,k5_[6}Gg]5w8g+iR`}5)@c:. (>N>dmZyO^:ZUpR`o0Q'B(a^5)ST|18M z:bbLV`> )`8Lb A typical preflight inspection is performed by ________ and would include________. shall inspect (where applicable) the following components of the CFR prev | next (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. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. (5) Flight and engine controls - for improper installation and AUTHORITY: 42 U.S.C. improper operation. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. #1 Internet-trusted security seal. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. (xiv) The repair or replacement of internal elements of blades. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. 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 . operation. (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 mechanic, and the repairman certifications are considered to be different classifications by the FAA: A mechanic must hold their license for ____ years to be eligible for an Inspection Authorization. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. (5) Flexible vibration dampeners - for poor condition and deterioration. Ifyou believe that this page should betaken down, please follow our DMCA take down process, Ensure the security ofyour data and transactions, Georgia Interim Lien Waiver And Release2013 Sub Sub - Benning, Georgia Final Lien Waiver And Release 2013 Sub Sub - Benning, 2nd Tier Subcontractor/Supplier List - Level 3 Construction, Daigger Automated Microplate Reader Operations Manual PDF, Identity (5) Segregation. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. (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. 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. (8) Exhaust stacks - for cracks, defects, and improper 43.15 Additional performance rules for inspections. A Part 147 school student may take the required FAA exams prior to graduation from that school. (3) Bonding and shielding - for improper installation and poor & Estates, Corporate - (b) Applicability. (4) Instruments - for poor condition, mounting, marking, and (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. (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. Appendix D. Scrap or Salvageable Aircraft Products and Articles. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. A ________ may request to see your mechanic certificate. (6) Engine controls - for defects, improper travel, and improper (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). Aircraft inspection checklists must be FAA approved. (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. 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. attachment. (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. Roll, pitch, yaw. 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