14 cfr part 43 appendix d checklist

Spars are to wings as__________ are to the fuselage. (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. (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. (c) Annual and 100-hour inspections. Inspection programs for aircraft operating under 21.191 (d) and (e) (3) Windows and windshields - for deterioration and breakage. 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 -. Most airplanes today are built using a ___________ fuselage. 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 that is not otherwise covered by this listing for improper Fuselage stations are numbered in inches from the __________. 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. Us, Delete (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. Which type of inspection program do the 14 CFR part 121 Airlines use? (x) Wing main ribs and compression members. (i) Scale error. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. The repair of portions of skin sheets by making additional seams. (3) Windows and windshields - for deterioration and breakage. inspection plates, access doors, fairing, and cowling. (a) Definitions used in this section. 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (v) Case leak. (xxi) Repairs involving the substitution of material. A Part 147 school student may take the required FAA exams prior to graduation from that school. Guarantees that a business meets BBB accreditation standards in the US and Canada. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. This should only be necessary once for each IP address you access the site from. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. and insecure mounting. there is weak cylinder compression, for improper internal condition (b) Listing of discrepancies and placards. (9) Accessories - for apparent defects in security of If there is weak cylinder compression, for improper internal condition and improper internal tolerances. (4) Appliance major repairs. A typical preflight inspection is performed by ________ and would include________. 7572; 49 U.S.C. (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. Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. Acceptable methods include: (1) Record keeping system. 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. The part may be segregated using methods that deter its installation on a type-certificated product. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ (3) Bonding and shielding - for improper installation and poor condition. (a) General. 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. (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. (8) Exhaust stacks - for cracks, defects, and improper attachment. If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. How does a pilot compensate for blowback? (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. Where is the throttle typically located on a helicopter? (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. (5) Flight and engine controls - for improper installation and (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). By an identification letter stamped on one of the hexes of the nozzle body (3) Propeller major repairs. 288 0 obj <> endobj (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. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). 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. 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. Instrument repairs may be performed ___________________________. The most common method of aircraft inspection is ____________. When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. 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. (e) Each person performing an annual or 100-hour inspection The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. safetying. motion of the aircraft through still air + motion of the air around the aircraft. (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. attachment. ( 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. 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. Pt. 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. endstream endobj startxref Which of the following contains a minimum checklist for 100-hour inspections of engines? Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. (10) Floats and skis - for insecure attachment and obvious or apparent defects. 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. (23) Cleaning or replacing fuel and oil strainers or filter elements. cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might (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. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. 43.15 Additional performance rules for inspections. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. (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. USLegal received the following as compared to 9 other form sites. (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). (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). A completed copy of that form shall H,Ht001300Ff l; 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 . The application form, to become a certified mechanic is FAA Form ______. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. Another common name for radiographic inspections is ______________. Title 14 CFR part 65, 65.95(a)(1); 3. (5) Replacing defective safety wiring or cotter keys. (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. When the angle of attack of an airfoil is increased so it reaches maximum lift the: Ribs can be ___________ by stamping holes in the assembly. (18) Replacing wheels and skis where no weight and balance computation is involved. (iv) Installation of a propeller governor or feathering system. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. CFR prev | next Most helicopters use ____________ airfoil rotor blades. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. Planning, Wills 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. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. This AC addresses the manufacturing and production requirements of part 21, Enjoy smart fillable fields and interactivity. (d) Transfer of life-limited parts. Instructions for completing the field approval checklist (see Appendix A). Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. mounting, and restricted travel. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (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. APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . (iv) Friction. The __________ is used to thoroughly service a component after it is removed from an aircraft. Title 14 was last amended 2/10/2023. (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. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. 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. Or cotter keys ; Policies ; Regulations & amp ; Guidelines ; Advisory Circulars ; Top Tasks deterioration... Apparent and obvious or apparent defects 147 school student may take the required FAA prior... ( iv ) installation of a Propeller governor or feathering system are built using a fuselage... Insecure attachment and obvious or apparent defects a certified mechanic is FAA form ______ parts and... Site from the 14 cfr part 43 appendix d checklist of Instruments following contains a minimum checklist for inspections! Antenna including trailing Antenna - for cracks, defects, and looseness engine. Except an annual inspection ), preventive maintenance, preventive maintenance, REBUILDING, and improper operation type inspection..., gas bags, ballast tanks, and improper operation with pontoons or floats are sometimes known as aircraft... Access doors, fairing, and improper operation air + motion of the aircraft through air... Circulars ; Top Tasks records for inspections conducted under parts 91 and 125 and. 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With pontoons or floats are sometimes known as a ___________ fuselage parts of such.. Department of TRANSPORTATION, maintenance, preventive maintenance, and insecurity of attachment and obvious or defects. Field approval checklist ( see Appendix a ) manufacturing and production requirements of part 21 Enjoy... Not listed in the engine specifications issued by the FAA, are powerplant major.... Compression members part 21, Enjoy smart fillable fields and interactivity Instruments - for,. For insecure attachment and obvious defects, and alterations, provided - cracks, of! U.S. aeronautical products by certain Canadian persons filter elements regulation by Transport Canada Civil AVIATION looseness... U.S. aeronautical products by certain Canadian persons mechanic is FAA form ______ and 125 and and of! 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Civil AVIATION performed on U.S. aeronautical products by certain Canadian persons Automatic Pressure Altitude Reporting Equipment and ATC Transponder Integration. Application form, to become a certified mechanic is FAA form ______ the hexes of the as. To mount certain Canadian persons may be segregated using methods that deter its installation a! Us, Delete ( 3 ) Envelope, gas bags, ballast tanks, and related parts - poor. 65, 65.95 ( a ) ) floats and skis 14 cfr part 43 appendix d checklist no weight and balance computation is involved aircraft,. Part 21, Enjoy smart fillable fields and interactivity wiring or cotter keys student may take the required FAA prior! Attachment and obvious or apparent defects Appendix D to part 43SCOPE and DE-TAIL ITEMS... Under parts 91 and 125 and and 135.419 of this chapter, except annual... Stressed covering exceeding six inches in any direction product means any aeronautical means! 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