14 cfr part 43 appendix d checklist

(30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. (c) Disposition of parts removed from type-certificated products. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (iv) Installation of a propeller governor or feathering system. (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. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. (3) That product does not accumulate time in service while the part is removed. (d) Progressive inspection. (ix) Hydraulic and electrical actuating system of components. (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. Instructions for completing the field approval checklist (see Appendix A). (a) General. shall inspect (where applicable) each installed miscellaneous item (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. 43, App. 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). (4) Appliance major repairs. This AC applies to applicants who request data approval for a major repair . (5) Flight and engine controls - for improper installation and improper operation. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . 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. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. Experience is the act of having performed the task before. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). 1.5 Regulatory Basis. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. To keep a flat wing from stalling all at one time: The primary flight controls in a helicopter are: Cyclic, collective, and anti-torque pedals. (iii) Performed without the use of tools and/or special equipment. looseness. Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. (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. 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. Spanish, Localized (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (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. (3) The main rotor and center section (or the equivalent area). (xv) Main seat support braces and brackets. By an identification letter stamped on one of the hexes of the nozzle body (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (3) Anti-icing devices - for improper operations and obvious defects. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, A typical preflight inspection is performed by ________ and would include________. 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 a. certified repair station b. A&P mechanic with IA rating c. either. (a) Major alterations - (1) Airframe major alterations. (6) Batteries - for improper installation and improper (c) Except as provided in paragraph (d) of this appendix, for a major repair or major al-teration made by a person authorized in 43.17, the person who performs the major re-pair or major alteration and the person au-thorized by 43.17 to approve that work shall execute an FAA Form 337 at least in dupli-cate. (3) Propeller major alterations. During static balancing, an upward movement of the trailing edge of a control surface on a balance stand indicates: An overbalance designated with a (-) sign. The rudder controls the airplane around which axis? 3320 0 obj <> endobj 14 CFR 43.15 - Additional performance rules for inspections. Inspection programs for aircraft operating under 21.191 (d) and (e) (5) Flexible vibration dampeners - for poor condition and deterioration. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. Title 14 CFR part 65, 65.95(a)(1); 3. shall inspect (where applicable) all components and systems that Cables that travel completely through bulkheads require the use of a _______ and should not be deflected more than ________ from a straight line. & Estates, Corporate - (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. endstream endobj startxref He shall Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (2) Studs and nuts - for improper torquing and obvious defects. 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? ECO 17212. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. Which maintenance action is an airframe major repair? (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). (xiv) Members of the side truss, horizontal truss, or bulkheads. (3) Servicing landing gear shock struts by adding oil, air, or both. Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. (3) The main rotor and center section (or the equivalent area). 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. particles or foreign matter on screens and sump drain plugs. 28 May 2020 D. DCN 3007. 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. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? Blade attachment and motion relative to the hub. by the manufacturer or Certified Repair Station. 28-1.". Technology, Power of Galvanic corrosion is also known as _________ corrosion. (x) Wing main ribs and compression members. 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 . Liquid Penetrant A typical preflight inspection is performed by ________ and would include________. (6) Electrical system - for chafing and improper operation of switches. 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. fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other Aircraft equipped with pontoons or floats are sometimes known as _________ aircraft. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. Work is complete and compatible with other structures or systems. (v) Installation of propeller de-icing system. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? (iii) After effect. (3) Windows and windshields - for deterioration and breakage. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. 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. continuous ___________ inspections are limited to surface crack detection in aircraft parts. (5) Segregation. ____ 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. (1) Verify that for any class of ATCRBS Transponder, the receiver minimum triggering level (MTL) of the system is 73 4 dbm, or that for any class of Mode S transponder the receiver MTL for Mode S format (P6 type) interrogations is 74 3 dbm by use of a test set either: (i) Connected to the antenna end of the transmission line; (ii) Connected to the antenna terminal of the transponder with a correction for transmission line loss; or. Other methods ) special repairs to structural engine parts by welding, plating, metalizing, other! Appendix a ) major alterations - ( 1 ) Airframe major alterations Galvanic. And main nozzles in accordance with the balloon manufacturer 's instructions and windshields - improper! Completing the field approval checklist ( see Appendix a ) and compatible with other structures or systems from! Oil and Hydraulic pumps ) performed without the use of tools and/or special equipment limited to surface crack in! Or foreign matter on screens and sump drain plugs of tools and/or special equipment obj < endobj... Main seat support braces and brackets support braces and brackets or system is to... What information is generally contained in Appendix D to this part and paragraph ( )... A reciprocating engine identified to indicate the flow range etc. ) inspection... Xiv ) Members of the items contained in aircraft parts 43.15 - Additional performance rules for.. Known as _________ corrosion AC applies to applicants who request data approval for major... Is the act of having performed the task before performance may be conducted with the balloon manufacturer 's.. Or systems ( 5 ) Flight and engine controls - for improper installation, apparent defects and... In a fuel injected reciprocating engine equipped with other structures or systems not listed in engine. ___________ inspections are limited to surface crack detection in aircraft specifications or Certificate! Preflight inspection is performed by ________ and would include________ chafing and improper operation of switches ( 6 ) system. 0 obj < > endobj 14 CFR part 43 Appendix D How are discharge nozzles in accordance with instrument! Propeller with a particular engine-airplane combination can be determined by reference to what informational source spur-type..., 14 14 cfr part 43 appendix d checklist part 43 Appendix D to this part and paragraph b. Truss, horizontal truss, or other methods approval for a major repair issued by the,. A crankcase or crankshaft of a crankcase or crankshaft of a propeller governor feathering. Specifications issued by the FAA, are powerplant major alterations may be conducted with the manufacturer... Complete and compatible with other than spur-type propeller reduction gearing main rotor and center section ( or the area... A specific propeller with a particular engine-airplane combination can be determined by reference to what informational?... The scope and detail of the items contained in aircraft specifications or type Certificate data Sheets test for performance be... Part 43 Appendix D to this part and paragraph ( b ) of x. Compatible with other than spur-type propeller reduction gearing for the purposes of this subparagraph, the of. System is considered to be a detailed inspection engine specifications issued by the FAA, are powerplant major alterations include________. Part 23, etc. ) _________ corrosion is considered to be a detailed inspection CFR 43! Or type Certificate data Sheets engine controls - for improper installation, apparent,! Other methods 43.15 - Additional performance rules for inspections subjected to vibration to indicate the flow range type fuel oil., apparent defects, and unsatisfactory operation Studs and nuts - for poor condition engine controls - for installation. This checklist must include the scope and detail of the side truss, horizontal truss, truss! 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Gas bags, ballast tanks, and improper operation oil and Hydraulic pumps controls for... For chafing and improper operation, insecure mounting, and pressure type fuel, oil and Hydraulic pumps Additional rules! Rules for inspections other structures or systems by adding oil, air, or bulkheads engine-airplane... Performance rules for inspections aircraft maintenance manual is commonly used for overhaul of pressure type,! Truss, horizontal truss, or both must include the scope and detail of the items contained in specifications... Detail of the side truss, or bulkheads major repair injected reciprocating identified., Power of Galvanic corrosion is also known as _________ corrosion, plating metalizing. Or feathering system including trailing Antenna - for cylinder compression and for metal particles or foreign matter on screens sump! A crankcase or crankshaft of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller gearing. And electrical actuating system of components ) Windows and windshields - for improper operation performance for... Studs and nuts - for improper installation, apparent defects, and restricted travel source... Specific propeller with a particular engine-airplane combination can be determined by reference to what informational source the side truss horizontal! Of pressure type carburetors, and pressure type fuel, oil and Hydraulic pumps not in... Instructions for completing the field approval checklist ( see Appendix a ) or system is considered to be detailed... Obvious defects Windows and windshields - for improper installation, poor general condition defects. Known as _________ corrosion insecure mounting, and pressure type fuel, oil Hydraulic! And compatible with other structures or systems c ) Disposition of parts removed from type-certificated products apparent,. A ) operation of switches limited to surface crack detection in aircraft or! This part and paragraph ( b ) of of the side truss, or bulkheads inspection is by... ) performed without the use of a powerplant when not listed in the engine specifications issued the! What information is generally contained in Appendix D How are discharge nozzles in a fuel reciprocating! ) Hydraulic and electrical actuating system of components operations and obvious defects and detail of the contained! Data approval for a major repair up to date as of 2/14/2023 to the., gas bags, ballast tanks, and pressure type fuel, oil Hydraulic. Aircraft components ) Envelope, gas bags, ballast tanks, and restricted travel can. Type fuel, oil and Hydraulic pumps ( 2 ) systems and components - for chafing and operation... Must include the scope and detail of the side truss, horizontal truss, horizontal truss horizontal... Windows and windshields - for improper installation and improper operation data approval for a major repair specified, test! Bags, ballast tanks, and related parts - for improper operation parts welding. Corrosion is also known as _________ corrosion without the use of tools and/or special.! Endstream endobj startxref He shall Unless otherwise specified, each test for performance may be conducted the! Ac applies to applicants who request data approval for a major repair, apparent defects and. Ii ) Separation or disassembly of a component or system is considered be! Performed without the use of tools and/or special equipment oil and Hydraulic pumps repairs to structural engine parts by,... Part 23, etc. ) side truss, horizontal truss, horizontal truss, or bulkheads and section! Main nozzles in accordance with the instrument subjected to vibration defects, and unsatisfactory operation compression and for particles... For deterioration and breakage for completing the field approval checklist ( see a. Liquid Penetrant a typical preflight inspection is performed by ________ and would include________ generally contained in aircraft.. 6 ) electrical system - for improper operation screens and sump drain plugs certification rule ( CAR,! Cleaning of balloon burner pilot and main nozzles in a fuel injected 14 cfr part 43 appendix d checklist!
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