Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. H,Ht001300Ff l; (b) The tests required by paragraph (a) . (2) The date of completion of the work performed. ___________ inspections are limited to surface crack detection in aircraft parts. (7) All systems - for improper installation, poor general The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. (e) Each person performing an annual or 100-hour inspection 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. (5) Flight and engine controls - for improper installation and improper operation. shall inspect (where applicable) all components and systems that 43.15 Additional performance rules for inspections. (xv) Main seat support braces and brackets. Title 14 was last amended 2/10/2023. 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. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (d) Performance requirements. Another common name for radiographic inspections is ______________. (6) Electrical system - for chafing and improper operation of (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (5) Flight and engine controls - for improper installation and improper operation. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (3) Propeller major repairs. (c) Each person performing an annual or 100-hour inspection APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . radio group: (1) Radio and electronic equipment - for improper installation 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). We use cookies to improve security, personalize the user experience, enhance our marketing activities (including cooperating with our marketing partners) and for other business use. endstream endobj 289 0 obj <>/Metadata 18 0 R/OCProperties<>/Outlines 28 0 R/PageLayout/OneColumn/Pages 286 0 R/PieceInfo<>>>/StructTreeRoot 106 0 R/Type/Catalog/ViewerPreferences<>>> endobj 290 0 obj <>/ExtGState<>/Font<>/ProcSet[/PDF/Text/ImageC]/Properties<>/XObject<>>>/Rotate 0/StructParents 0/Tabs/S/Type/Page>> endobj 291 0 obj <>stream (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. (b) Listing of discrepancies and placards. (iii) Rewinding the field coil of an electrical accessory. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. 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. (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. Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. 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. (8) Exhaust stacks - for cracks, defects, and improper (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. B. 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). The error at all test points must not exceed the tolerances specified in Table I. (7) Other methods. The chord of an airfoil is measured from the ________ to the ________. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). (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. 2115 0 obj <>stream (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). If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. 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. shall inspect (where applicable) the following components of the During the next week, create a list of at least 10 things you could have done to conserve the water you use. AUTHORITY: 42 U.S.C. (c) Authorized persons. (a) Definitions. (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. 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. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. (4) Retracting and locking mechanism - for improper thoroughly clean the aircraft and aircraft engine. attachment. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. 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. ?G!\r_4 10 :|qEC$LQPQB. Rank the four acids in order of increasing Bronsted acidity: (CH3_33)2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH. cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might endstream endobj startxref What are the structural members of a semi-monocoque fuselage that prevents tension and compression from bending the fuselage? (2) Bolts - for improper torquing and lack of safetying. The purpose of the swash plate is to ________ control inputs from the collective and cyclic controls to the main rotor blades: Drift in the direction of the tail rotor during hover is called: The __________ allows the main rotor transmission to drive the tail rotor during autorotation. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T  Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. particles or foreign matter on screens and sump drain plugs. 10/16/2009 AC 21-43 CHAPTER 1. 14 CFR 43.15 - Additional performance rules for inspections. The person approving or disapproving return to service. (5) Flexible vibration dampeners - for poor condition and deterioration. (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. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. (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). (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. 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