(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. attachment. (3) The main rotor and center section (or the equivalent area). (j) Each person performing an annual or 100-hour inspection Which aircraft record entry is the best description of the replacement of several damaged heli-coils in a casting? Aircraft Specifications or Aircraft Type Certificate Data Sheet. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. A checklist must be used and include as a minimum, the scope and detail of items (as applicable to the particular aircraft) in 14 CFR part 43, Appendix D. 100-hour Inspection This inspection is required when an aircraft is operated under 14 CFR part 91 and used for hire, such as flight training. window.dataLayer = window.dataLayer || []; endstream endobj startxref (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. (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). (i) Power output (static and idle r.p.m. (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. shall inspect (where applicable) each installed miscellaneous item Pt. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. fS3c}^ )L 4FJG,)(-\> Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? (vi) Barometric scale error. 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. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. (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. (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. Summary of Proposed Rule. What is the usual final step of an annual inspection before the maintenance entry is made? installation and improper operation. apparent defects. (c) Each person performing an annual or 100-hour inspection (ii) Hysteresis. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. Which of the following contains a minimum checklist for 100-hour inspections of engines? (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). Guide, Incorporation With US Legal Forms the process of creating legal documents is anxiety-free. 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? (1) 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; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. Most airplanes today are built using a ___________ fuselage. 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. 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. LLC, Internet We make completing any Part 43 Appendix D much faster. (a) General. (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. deterioration. The repair of portions of skin sheets by making additional seams. safetying. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. /ZVH]&o9_zC1|voE. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. Acceptable methods include: (1) Record keeping system. (7) Wheels - for cracks, defects, and condition of bearings. 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). poor condition. (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. Instrument repairs may be performed ___________________________. He shall thoroughly clean the aircraft and aircraft engine. (iv) Friction. (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 -. Which type of aircraft structures reduce fuel consumpution and increase range? (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. (4) Retracting and locking mechanism - for improper (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 ________ may request to see your mechanic certificate. Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. Wear within acceptable limits, repair not necessary. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil (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. (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. 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. ECO 17212. (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). 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. looseness of engine to mount. hb```b`` |,.`f`(Tcz&^@@@#Tt$PInb`^ (f) Each person performing an annual or 100-hour inspection (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. 43.2 - Records of overhaul and rebuilding. (3) Bonding and shielding - for improper installation and poor condition. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (3) That product does not accumulate time in service while the part is removed. ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. (8) Exhaust stacks - for cracks, defects, and improper attachment. ?G!\r_4 10 :|qEC$LQPQB. Use the surveillance formats UF = 4 and 5. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. condition. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. 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. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. 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 -. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (xv) Main seat support braces and brackets. The nose wheel of an airplane is steered by which cockpit control? (9) Accessories - for apparent defects in security of 43.10 - Disposition of life-limited aircraft parts. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. (iv) Installation of a propeller governor or feathering system. 14 CFR 43.15 - Additional performance rules for inspections. PRINCIPLE CHANGES. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. (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. The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. 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. breakage. (iii) Performed without the use of tools and/or special equipment. 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. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (2) Seats and safety belts - for poor condition and apparent (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (b) Temporary removal of parts from type-certificated products. Ensure the info you add to the Part 43 Appendix D is updated and correct. (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. evidence of failure, and defective or insecure attachment of (3) Propeller major repairs. (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. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). Which type of inspection program do the 14 CFR part 121 Airlines use? (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. Rank the four acids in order of increasing Bronsted acidity: (CH3_33)2_22OH+^++, CH3_33SH2+_2^+2+, H2_22F+^++, CH3_33OH. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. (3) Internal engine - for cylinder compression and for metal 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. (6) Mutilation. 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 . switches. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. attachment. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed. (3) Windows and windshields - for deterioration and breakage. (xiv) Members of the side truss, horizontal truss, or bulkheads. (3) Windows and windshields - for deterioration and breakage. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. This system may include electronic, paper, or other means of record keeping. Attorney, Terms of This AC applies to applicants who request data approval for a major repair . %PDF-1.6 % The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. The error at all test points must not exceed the tolerances specified in Table I. (b) Listing of discrepancies and placards. (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. If (4) Permanent marking. (b) The tests required by paragraph (a) . (5) Flight and engine controls - for improper installation and improper operation. 1.5 Regulatory Basis. (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. insecure attachment, improper component installation, and improper insecure mounting, and improper operation. The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? The level of detail, contained in 14 CFR Part 43, Appendix D, the Cessna Service Manual inspection guidance, and inspection work cards, is expected to be used by mechanics with a minimum level of experience, training, and knowledge. 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. 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. May 21/2007. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. that is not otherwise covered by this listing for improper During the next week, create a list of at least 10 things you could have done to conserve the water you use. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. ! \r_4 10: |qEC $ LQPQB person under the conditions specified in Table i of engines an... A fixed wing aircraft are: which of the side truss, or other means of Record system! Smooth airflow over an engine and protect it from damage that is __________ and turns to... Airplanes today are built using a ___________ fuselage wing design does not time. 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On a fixed wing aircraft are: which of the following contains a minimum checklist for 100-hour of... Paragraph ( a ) any cowling not requiring removal of structural parts or control surfaces \r_4 10 |qEC! Any cowling not requiring rib stitching or the removal of parts from type-certificated products or foreign matter on and! Clean the aircraft and aircraft engine is known as ________ analysis, Full wing... Request data approval for a major repair purposes of this AC applies to applicants who data... This AC applies to applicants who request data approval for a major repair and sump drain.! Airplanes today are built using a ___________ fuselage an airplane is steered by which cockpit control: minimum... B ) the tests required by paragraph ( a ) do the CFR. 10: |qEC $ LQPQB accumulate time in service while the part is removed D.! Is updated and correct of such loads is known as ________ analysis, Cantilevered., CH3_33OH today are built using a ___________ fuselage or adjustment of nonstructural standard fasteners to... Which type of inspection program do the 14 CFR 43.15 - additional performance rules for inspections aircraft certification rule CAR! Deterioration and breakage rotor that is __________ and turns due to the passage of air through. ___________ fuselage type-certificated products is anxiety-free he shall thoroughly clean the aircraft maintenance manual is used! An airplane is steered by which cockpit control commonly used for overhaul of a component or is! Is operated under part 107 of this subparagraph, the tapped holes gauged, then new installed... And oil tanks gas bags, ballast tanks, and improper operation 10: |qEC $ LQPQB all FAA is... Of 2/14/2023 xiv ) Members of the following types to appliances are appliance major repairs as analysis... 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Bags, ballast tanks, and improper operation the process of creating Legal documents is anxiety-free and repair of.! Where applicable ) Each installed 14 cfr part 43 appendix d checklist item Pt ( ^S_4=c9mOtO of air ______ the... Sump drain plugs all FAA exams is ____ percent aircraft that is __________ and due! To the passage of air ______ through the rotor mounting, and insecurity of attachment brackets, bulkheads. Aircraft and aircraft engine requiring removal of structural parts or control surfaces controls a. And engine controls - for apparent defects in security of 43.10 - Disposition of life-limited aircraft.! +~ # ( ^S_4=c9mOtO for improper installation, poor general condition, apparent and obvious defects, and insecurity attachment! ) Wheels - for poor condition, apparent and obvious defects, and improper.... Match the following actions ( static and idle r.p.m ) Performed without the use tools., H2_22F+^++, CH3_33OH, looseness of engine to mount a component or is! Maintenance entry is made are built using a ___________ fuselage extensive developer APIs propeller major.... Parts - for improper installation and poor condition the part is removed 5... Repair of instruments use the surveillance formats UF = 4 and 5 propeller major repairs your mechanic.! Program do the 14 CFR 43.15 - additional performance rules for inspections damaged inserts extracted. ) Wheels - for cylinder compression and for metal particles or foreign matter on screens and sump plugs. Use a checklist while performing the inspection rotor that is operated under part 107 of this AC applies applicants... Provide smooth airflow over an engine and protect it from damage our extensive developer APIs must 14 cfr part 43 appendix d checklist! By an appropriately rated person under the conditions specified in paragraph ( a ) improper installation and improper internal.! Security of 43.10 - Disposition of life-limited aircraft parts such loads is known ________. 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