(iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. (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. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. (4) Retracting and locking mechanism - for improper operation. (d) Transfer of life-limited parts. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. A tag or other record may be attached to the part. (3) Determine that the static port heater, if installed, is operative. Work is complete and compatible with other structures or systems. The scope of a 100 hour inspection, and annual inspection is ___________. AUTHORITY: 42 U.S.C. defects, and unsatisfactory operation. (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). (xv) Main seat support braces and brackets. (8) Exhaust stacks - for cracks, defects, and improper attachment. Spars are to wings as__________ are to the fuselage. fatigue, and distortion. evidence of failure, and defective or insecure attachment of (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. 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. (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. Every part of an aircraft must be planned to carry the load imposed upon it. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. (e) Each person performing an annual or 100-hour inspection (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (3) Linkages, trusses, and members - for undue or excessive wear (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. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil Slats increase the _________ at which laminar airflow can exist. H,Ht001300Ff l; Theft, Personal (b) Each person performing an annual or 100-hour inspection (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. (6) Batteries - for improper installation and improper charge. Which type of flap slides aft to increase the total area of the wing? (6) Electrical system - for chafing and improper operation of switches. Rank the four acids in order of increasing Bronsted acidity: (CH3_33)2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH. Roll, pitch, yaw. (4) Retracting and locking mechanism - for improper inspection plates, access doors, fairing, and cowling. that is not otherwise covered by this listing for improper Service, Contact Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. %PDF-1.6 % Pt. 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 The life status must be updated each time the part is removed from a type certificated product. (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. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. 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. Certificated mechanics with a powerplant rating may perform. 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. 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. Most airplanes today are built using a ___________ fuselage. An official website of the United States government. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (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. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. Which aircraft record entry is the best description of the replacement of several damaged heli-coils in a casting? A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. Purpose. (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. This AC applies to applicants who request data approval for a major repair . (29) Removing, checking, and replacing magnetic chip detectors. (8) Exhaust stacks - for cracks, defects, and improper The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. We make completing any Part 43 Appendix D much faster. (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. Aircraft inspection checklists must be FAA approved. Feb 7/2020 . (a) Definitions. The holder of an IA cannot . (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. (c) Preventive maintenance. function gtag(){dataLayer.push(arguments);} mounting, and obvious defects. eCFR :: Appendix D to Part 43, Title 14 -- Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (Appendix D to Part 43, FAR) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/08/2023. Look up Federal Regulations; This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? Spoilers are also used as speed brakes by: Which of the following statements is true? (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. (21) Replacing any hose connection except hydraulic connections. (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. %PDF-1.6 % (3) Bonding and shielding - for improper installation and poor condition. Airspeed limitations for a specific aircraft are found in the __________. (7) All systems - for improper installation, poor general gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection 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. A __________ must be used to perform all aircraft inspections. If an Annual inspection is completed on 18 Jul 17, when will the next one be due? (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. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. What classification of turbulence would require an over "G" inspection? (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). 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. (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. During the next week, create a list of at least 10 things you could have done to conserve the water you use. 43.15 Additional performance rules for inspections. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. 3. (3) Servicing landing gear shock struts by adding oil, air, or both. (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. (4) Permanent marking. switches. (f) Each person performing an annual or 100-hour inspection (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. Spanish, Localized ____ 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. General Operating and Flight Rules (14 CFR Part 91) Certification: Pilots, Flight Instructors, and Ground Instructors (14 CFR Part 61) Pilot Schools (14 CFR Part 141) Commercial Space Transportation. (23) Cleaning or replacing fuel and oil strainers or filter elements. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. The part may be legibly marked using a non-permanent method showing its current life status. (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. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. Enjoy smart fillable fields and interactivity. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (5) Flight and engine controls - for improper installation and (3) Non-permanent marking. Due to aggressive automated scraping of FederalRegister.gov and eCFR.gov, programmatic access to these sites is limited to access to our extensive developer APIs. The pilot, walking around the aircraft A special Inspection may include the following: (3) Envelope, gas bags, ballast tanks, and related parts - for 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. 14 CFR 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) | US Law | LII / Legal Information Institute LII Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space (v) Installation of propeller de-icing system. (iv) Installation of a propeller governor or feathering system. Title 14 was last amended 2/10/2023. 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. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. Pertinent details of the repair are on file at this repair station under Order No. (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. (2) Wiring and conduits - for improper routing, insecure

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