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. (3) Windows and windshields - for deterioration and breakage. (iii) Rewinding the field coil of an electrical accessory. 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. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ (v) Case leak. AUTHORITY: 42 U.S.C. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. (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. shall inspect (where applicable) the following components of the Aircraft inspection checklists must be FAA approved. (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. ____ 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. 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). (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (5) Replacing defective safety wiring or cotter keys. With US Legal Forms the process of creating legal documents is anxiety-free. (3) Envelope, gas bags, ballast tanks, and related parts - for Elevators move the aircraft around which axis? radio group: (1) Radio and electronic equipment - for improper installation 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 Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. 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. When must an Airworthiness Directive be complied with? 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. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (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. (2) Bolts - for improper torquing and lack of safetying. (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. (f) Each person performing an annual or 100-hour inspection Use the correct address and at least two incorrect addresses. 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? 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. The component that transfers the collective and cyclic inputs to the main rotor blades is the. 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. 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. failure, and insecurity of attachment. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. A __________ must be used to perform all aircraft inspections. A tail rotor moves (or maintains) the helicopter yaw direction by: Many helicopters use a _______ engine to drive the main transmission and rotor systems. 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. Spanish, Localized (21) Replacing any hose connection except hydraulic connections. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (e) Approval requirements. __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, (3) Anti-icing devices - for improper operations and obvious defects. (3) Anti-icing devices - for improper operations and obvious pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . Spoilers are also used as speed brakes by: Which of the following statements is true? A completed copy of that form shall be -. ~{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. (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. A tag or other record may be attached to the part. '; gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection breakage. (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. (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. The test point shall be approached at a rate compatible with the test equipment. CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. (i) Scale error. 288 0 obj <> endobj 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. The __________ is used to thoroughly service a component after it is removed from an aircraft. condition, defects, and insecure attachment. If work performed on an aircraft has been done satisfactorily, the signature of an authorized person on the maintenance records for maintenance or alterations performed constitutes: approval for return to service only for the work performed. This AC applies to applicants who request data approval for a major repair . (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. 2. This advisory circular (AC) has been updated to reflect changes to Title 14 of the Code of Federal Regulations (14 CFR) part 43, regarding preventive maintenance. Title 14 was last amended 2/10/2023. Look up Federal Regulations; By an identification letter stamped on one of the hexes of the nozzle body If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (3) Propeller major alterations. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (xii) Overhaul of controllable pitch propellers. (b) Each person performing an annual or 100-hour inspection (6) Batteries - for improper installation and improper charge. ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. (xv) Main seat support braces and brackets. (iv) Installation of a propeller governor or feathering system. (2) Replacing elastic shock absorber cords on landing gear. USLegal fulfills industry-leading security and compliance standards. (d) Each person performing an annual or 100-hour inspection (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. Get started now! (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. B. (2) Studs and nuts - for improper torquing and obvious What are three characteristics of a sprawling stance? (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. The tests in (e) through (j) apply only to Mode S transponders. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. 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 -. (3) Servicing landing gear shock struts by adding oil, air, or both. Wing braces are the main structural member of a wing. (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. 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. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). AC. Follow the simple instructions below: The times of distressing complex legal and tax documents are over. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. 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. He shall thoroughly clean the aircraft and aircraft engine. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. (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. 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. fatigue, and distortion. Highest customer reviews on one of the most highly-trusted product review platforms. APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . Box beam wing construction is used on what type aircraft? The method must deter the installation of the part after it has reached its life limit. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. 2115 0 obj <>stream (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. What type of rotor is found on helicopters with two rotor blades? 43, App. The holder of an IA cannot . Instrument repairs may be performed ___________________________. This should only be necessary once for each IP address you access the site from. Which of the following contains a minimum checklist for 100-hour inspections of engines? (d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. (c) Preventive maintenance. (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. component operation. attachment. Handbook, DUI (5) Flight and engine controls - for improper installation and improper operation. Airworthiness Directives are issued primarily to: 1) A Supplemental Type Certificate may be issued to more than one applicant for the same design change, providing each applicant shows compliance with the applicable airworthiness requirement (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. 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. poor condition. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). (a) Major alterations - (1) Airframe major alterations. (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) -. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). This revision supersedes AC 21-43, dated 10/16/2009 and has been updated to reflect . Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (b) Applicability. (b) The tests required by paragraph (a) . (2) Shock absorbing devices - for improper oleo fluid level. Use the surveillance formats UF = 4 and 5. (b) Rotorcraft. (9) Accessories - for apparent defects in security of mounting. Each time the part is removed from a type certificated product, the record must be updated with the current life status. What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? 10/16/2009 AC 21-43 CHAPTER 1. looseness of engine to mount. (3) That product does not accumulate time in service while the part is removed. 3320 0 obj <> endobj f-``0>, % D1@ 6 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. Learn more ME406 Series Emergency Locator Transmitter - ACR. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. and insecure mounting. An official website of the United States government. A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. a. certified repair station b. A&P mechanic with IA rating c. either. 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? 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. (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. looseness. (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). An aircraft Type Certificate Data Sheet contains. A completed copy of that form shall be -. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. 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. However, this paragraph does not authorize the performance of any inspection required by Part 91 or Part 125 of this chapter or any inspection performed after a major repair or alteration. (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. . (2) Seats and safety belts - for poor condition and apparent What provides the thrust for a Gyrocopter? (3) Anti-icing devicesfor improper oper- (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (iii) After effect. operation. 43.7 - Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. %%EOF The part may be legibly marked using a permanent method showing its current life status. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. inspection plates, access doors, fairing, and cowling. view historical versions Title 14 Chapter I Subchapter F Part 91 Subpart E 91.411 Previous Next Top eCFR Content 91.411 Altimeter system and altitude reporting equipment tests and inspections. 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 -. 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. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. shall inspect (where applicable) the following components of the (5) Flexible vibration dampeners - for poor condition and deterioration. shall inspect (where applicable) the following components of the 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 . make up the complete empennage assembly for poor general condition, ?G!\r_4 10 :|qEC$LQPQB. (2) Studs and nuts - for improper torquing and obvious defects. The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. Planning, Wills This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. Cowl flaps are movable parts of the cowling that open and close in order to: Primary flight control surfaces need to be balanced so they do not: Flight control surfaces must be balanced whenever: When the airplane is turned left the aileron on the pilot's __________ points up. Title 14 CFR part 43, 43.7(d) and 43.17(e)(2); 2. (4) Instruments - for poor condition, mounting, marking, and continuous ___________ inspections are limited to surface crack detection in aircraft parts. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. hb```b`` |,.`f`(Tcz&^@@@#Tt$PInb`^ U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. 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. 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. Access the most extensive library of templates available. (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. Where are technical descriptions of certificated propellers found? Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? insecure mounting, and improper operation. The most common method of aircraft inspection is ____________. 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Access the site from title 14 CFR part 43 AppendixD When must an Airworthiness Directive ( )! ________ from the rest of the aircraft maintenance manual is commonly used overhaul...