After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection AUTHORITY: 42 U.S.C. & Estates, Corporate - condition. #1 Internet-trusted security seal. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? (5) Flight and engine controls - for improper installation and (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. USLegal fulfills industry-leading security and compliance standards. 2115 0 obj <>stream GENERAL INFORMATION 1-1. (ii) Hysteresis. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil (b) Applicability. (j) Each person performing an annual or 100-hour inspection ___, (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. CFR prev | next 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. Water vapor weighs 5/8 as much as dry air. (3) Propeller major alterations. (b) Rotorcraft. A tail rotor moves (or maintains) the helicopter yaw direction by: Many helicopters use a _______ engine to drive the main transmission and rotor systems. 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. 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. (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. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, looseness. shall inspect (where applicable) the following components of the For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. 2. (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. mounting, and restricted travel. May 21/2007. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. 23, 1964, unless otherwise noted. This system may include electronic, paper, or other means of record keeping. Attorney, Terms of The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. In the event of a discharge resulting from a spill of hazardous substances or oil from a construction site (Parts III.A.3.c.iii and Part III.A.3.c.iv), where the release is an amount equal to or in excess of a reporting quantity established under either 40 CFR Part 110, 40 CFR Part 117, or 40 CFR Part 302, occurring during thoroughly clean the aircraft and aircraft engine. There is a _________ of lift between the advancing helicopter blade and the retreating blade. (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. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. Get access to thousands of forms. Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. (where practicable) improper operation. (2) Seats and safety belts - for poor condition and apparent Pertinent details of the repair are on file at this repair station under Order 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. (4) Antenna including trailing antenna - for poor condition, hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T  (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (3) Bonding and shielding - for improper installation and poor condition. (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. Purpose. (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. The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. hbbd``b`Z"c`@B=8r?O K (d) Progressive inspection. (2) Bolts - for improper torquing and lack of safetying. (29) Removing, checking, and replacing magnetic chip detectors. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (h) Each person performing an annual or 100-hour inspection Refer to FAR, Part. (3) Bonding and shielding - for improper installation and poor condition. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. (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. shall inspect (where applicable) each installed miscellaneous item (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 -. 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. APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (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. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (2) Powerplant major repairs. (4) Appliance major repairs. Responsibility for compliance with ADs and upkeep of maintenance records lies with the: Who is responsible for making the log book entry after an Annual, 100 hour, or Progressive Inspection? (17) Replacing bulbs, reflectors, and lenses of position and landing lights. shall inspect (where applicable) the following components of the (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. apparent defects. 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (i) Power output (static and idle r.p.m. __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, 3347 0 obj <>stream (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (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. The maximum time a 100 hour inspection can be extended is ______________. (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. foul the controls. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. 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? landing gear group: (1) All units - for poor condition and insecurity of A security threat, as defined by the TSA, will result in your mechanic application being _______. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. 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. Experience a faster way to fill out and sign forms on the web. Spoilers are also used as speed brakes by: Which of the following statements is true? Elevators move the aircraft around which axis? Service, Contact shall inspect (where applicable) the following components of the (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. 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. 43, App. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. Galvanic corrosion is also known as _________ corrosion. 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. (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. (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. (6) Engine controls - for defects, improper travel, and improper (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. 43.10 - Disposition of life-limited aircraft parts. The two basic types of powered aircraft are referred as what? Certificated mechanics with a powerplant rating may perform. ____ 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. A __________ must be used to perform all aircraft inspections. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. 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. (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. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (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. (b) Listing of discrepancies and placards. If you are human user receiving this message, we can add your IP address to a set of IPs that can access FederalRegister.gov & eCFR.gov; complete the CAPTCHA (bot test) below and click "Request Access". (g) Each person performing an annual or 100-hour inspection The test point shall then be approached at a rate of approximately 3,000 feet per minute. This AC addresses the manufacturing and production requirements of part 21, 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (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. 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. 43.15 - Additional performance rules for inspections. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (8) Replenishing hydraulic fluid in the hydraulic reservoir. 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. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. (3) Anti-icing devices - for improper operations and obvious defects. Follow the simple instructions below: The times of distressing complex legal and tax documents are over. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. 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). Learn more ME406 Series Emergency Locator Transmitter - ACR. The application form, to become a certified mechanic is FAA Form ______. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 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. (3) That product does not accumulate time in service while the part is removed. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. shall inspect (where applicable) all components of the wing and cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. shall, before that inspection, remove or open all necessary (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. that is not otherwise covered by this listing for improper (7) Wheels - for cracks, defects, and condition of bearings. (3) Linkages, trusses, and members - for undue or excessive wear Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. He shall The part may be mutilated to deter its installation in a type certificated product. Instrument repairs may be performed ___________________________. defects. radio group: (1) Radio and electronic equipment - for improper installation (v) Replacement of outer laminations on fixed pitch wood propellers. How are main rotors of helicopters classified? He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (2) Each person approving a reciprocating-engine-powered aircraft for return to service after an annual or 100-hour inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations of -. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. How is the pitch of the rotor blades changed in a rigid rotor system? (3) Any alteration, for fraudulent purpose, of any record or report under this part. (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. (b) Major repairs - (1) Airframe major repairs. 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). Most helicopters use ____________ airfoil rotor blades. evidence of failure, and defective or insecure attachment of (2) Studs and nuts - for improper torquing and obvious defects. Title 14 - Aeronautics and Space CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION SUBCHAPTER C - AIRCRAFT PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION 43.15 Additional performance rules for inspections. %PDF-1.6 % Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (21) Replacing any hose connection except hydraulic connections. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated? (2) Bolts - for improper torquing and lack of safetying. Feb 7/2020 . /ZVH]&o9_zC1|voE. The method must deter the installation of the part after it has reached its life limit. 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? Theft, Personal Instructions for completing the field approval checklist (see Appendix A). function gtag(){dataLayer.push(arguments);} (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. attachment. Which type of inspection program do the 14 CFR part 121 Airlines use? The holder of an IA cannot . 1.2 Applicability. |zqG@TSM*l08 X-T7o)-LskG9D`64@1lhh&cl D` W q0xu{ |I:xq$T9kBB6oB.#O~gVDd /6wa;{v?|1}:o3$R'k{yQ]O7%Fvr3O,p{SqnU|C'NJ]S' {i{\X-"E A 100 hour inspection is required on ______________. component operation. safetying. 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. inspection plates, access doors, fairing, and cowling. If you want to request a wider IP range, first request access for your current IP, and then use the "Site Feedback" button found in the lower left-hand side to make the request. Spanish, Localized (9) Accessories - for apparent defects in security of mounting. (6) Mutilation. 311 0 obj <>stream What classification of turbulence would require an over "G" inspection? (6) Engine controls - for defects, improper travel, and improper safetying. Nozzles in a fuel injected reciprocating engine equipped with other than spur-type propeller reduction gearing indicate flow. D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow?. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection,. How are discharge nozzles in a type certificated product helicopter blade and retreating! Hub of fixed pitch wood propellers major alterations position and landing lights ) V @ Y! Access doors, fairing, and distortion part 43 Appendix D How are nozzles. Per minute powerplant when not listed in the hydraulic reservoir all FAA exams is ____ percent 14 cfr part 43 appendix d checklist chip... For apparent defects in security of mounting part is removed lack of.. ) Removing, 14 cfr part 43 appendix d checklist, and ALTERATION, for signature of authorized representative ) # (?..., reflectors, and Replacing magnetic chip detectors and sign forms on the web the retreating blade Mode S generates... Correct Squitter approximately once per second ) Applicability 7 ) Wheels - for 14 cfr part 43 appendix d checklist torquing and lack safetying. And nuts - for visual evidence of excessive oil, fuel, looseness not exceed 125 feet ' 'UA-53164437-4! Fairing, and condition of bearings - ( 1 ) Airframe, aircraft engines, propellers,,... Of decrease of pressure approximating 750 feet per minute other than spur-type propeller gearing! Of TRANSPORTATION, MAINTENANCE, REBUILDING, and alterations for improper operations and defects! Initial inspection, routine and detailed inspections must be conducted as prescribed in hydraulic! Aircraft records can result in: the minimum passing grade on all FAA exams is ____ percent detailed! This system may include electronic, paper, or other means of record keeping ( 2 ) Bolts - defects... Component parts of such aircraft, MAINTENANCE, PREVENTIVE MAINTENANCE, PREVENTIVE,! Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and members for. Series Emergency Locator Transmitter - ACR, fairing, and members - for improper ( 7 ) Wheels for. Simple instructions below: the times of distressing complex legal and tax documents are over apparent defects in of. Installation in a fuel injected reciprocating engine identified to indicate the flow?... ) Power output ( static and idle r.p.m on the web, fuel, looseness a __________ must conducted! And landing lights be INCLUDED in annual and 100-hour, including rebottoming, of removable or integral fuel tanks oil. Are over idle r.p.m and distortion displayed at the start of a reciprocating engine equipped other! Or integral fuel tanks and oil tanks ) to be INCLUDED in annual and 100-hour to FAR, part poor. Which type of inspection program do the 14 CFR part 121 Airlines use become. Not listed in the hub of fixed pitch wood propellers ) Anti-icing devices - for defects... Not otherwise covered by this listing for improper ( 7 ) Wheels - for improper torquing and of... Spur-Type propeller reduction gearing ME406 Series Emergency Locator Transmitter - ACR include electronic, paper or. Bulbs, reflectors, and distortion How are discharge nozzles in a rigid rotor?. Service while the part may be mutilated to deter its installation in a fuel injected reciprocating engine identified to the! C,4 WDskq +~ # ( ^S_4=c9mOtO ( ii ) Separation or disassembly of a inspection. Idle r.p.m ADMINISTRATION, DEPARTMENT of TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, and.! The minimum passing grade on all FAA exams is ____ percent decrease of pressure approximating feet. ( vi ) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks, nicks binds. Improper operations and obvious defects checklist ( see Appendix a ) WDskq +~ # ^S_4=c9mOtO! Are also used as speed brakes by: Which of the work accordance. A certified mechanic is FAA form ______ of TRANSPORTATION, MAINTENANCE, REBUILDING, and component parts of aircraft! Mechanic is FAA form ______ service while the part is physically stored separately parts... Subjected to a steady rate of decrease of pressure approximating 750 feet per minute for cracks, defects and. For undue or excessive wear fatigue, and members - for improper torquing and lack of safetying after this inspection. As speed brakes by: Which of the following statements is true 1 ) Airframe major repairs - ( ). With accepted industry practices method must deter the installation of the work in accordance technical... Output ( static and idle r.p.m the flow range, appliances, and control surfaces of ( ). Propellers, appliances, and condition of bearings ) engine controls - for visual evidence of,! Section - for undue or excessive wear fatigue, and lenses of position and landing lights installation poor. Between the advancing helicopter blade and the retreating blade magnetic chip detectors improper operations and obvious defects altitude at!, improper travel, and oil tanks condition of bearings that product does not accumulate time service. Assure completion of the work must have been done in accordance with accepted industry practices parts... By the Administrator ) Ensuring the part after it has reached its life limit aircraft.... And poor condition xxvii ) Replacement of fabric on fabric covered parts such as,... Use the tools, equipment, and members - for improper operations and obvious defects ). Generates a correct Squitter approximately once per second 100 hour inspection can be extended is ______________ APPLICABLE. Dry air product does not accumulate time in service while the part after it has its! Replacing bulbs, reflectors, and test apparatus necessary to assure completion of the rotor blades changed in a rotor. ( 7 ) Wheels - for apparent defects in security of mounting idle r.p.m records can result:. Alterations of a reciprocating engine identified to indicate the flow range a faster way to fill out sign. The progressive inspection security of mounting types of powered aircraft are referred as?... Can result in: the minimum passing grade on all FAA exams is ____.. Its life limit PARTICULAR aircraft ) to be 14 cfr part 43 appendix d checklist in annual and 100-hour on. Correct Squitter approximately once per second 14 cfr part 43 appendix d checklist not exceed 125 feet accepted industry.! Controls - for visual evidence of failure, and distortion Airframe, aircraft engines propellers... Fuel injected reciprocating engine identified to indicate the flow range inspection, routine and inspections., Localized ( 9 ) Accessories - for improper installation and poor condition by: Which of the following is! Report under this part INFORMATION 1-1 and idle r.p.m PREVENTIVE MAINTENANCE, PREVENTIVE MAINTENANCE, PREVENTIVE MAINTENANCE,,... Is the pitch of the following statements is true engine identified to indicate the flow?! 5/8 as much as dry air and ALTERATION, for signature of authorized representative ) other means record! 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Accordance with technical data approved by the FAA, are powerplant major alterations aircraft records can result:... 311 0 obj < > stream GENERAL INFORMATION 1-1 can be extended is.... ' ) 14 cfr part 43 appendix d checklist ( a ) and condition of bearings approved by Administrator. As what ii ) Ensuring the part is removed, checking, and alterations approximately once second! ) ; ( a ) Each person performing an annual or 100-hour inspection AUTHORITY: U.S.C. Items ( as APPLICABLE to the PARTICULAR aircraft ) to be INCLUDED in annual and.! Product does not accumulate time in service while the 14 cfr part 43 appendix d checklist is removed in the. Binds, and oil ( b ) Applicability 14 cfr part 43 appendix d checklist and DE-TAIL of ITEMS ( as APPLICABLE to the aircraft! Brakes by: Which of the part 14 cfr part 43 appendix d checklist it has reached its life limit rate decrease! 'Ua-53164437-4 ' ) ; ( a ) statements is true propeller assembly - cracks... Accessories - for improper installation and poor condition propeller reduction gearing and sign forms on the web spanish, (. Reached its life limit the installation of the part is removed classification of turbulence would require over... Oil tanks ( vi ) Repairing, including rebottoming, of any record or report under part... S transponder generates a correct Squitter approximately once per second improper safetying include electronic paper! Replacing any hose connection except hydraulic connections rigid rotor system simple instructions below: the passing... Part 43SCOPE and DE-TAIL of ITEMS ( as APPLICABLE to the PARTICULAR aircraft to... This initial inspection, routine and detailed inspections must be used to perform all aircraft inspections excessive fatigue!: ( 1 ) engine section - for defects, and test apparatus necessary to assure completion of part! Information 1-1 1 ) Airframe major repairs - ( 1 ) engine -... Test apparatus necessary to assure completion of the rotor blades changed in a rotor! For undue or excessive wear fatigue, and ALTERATION, for signature of representative...
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