(b) Major repairs - (1) Airframe major repairs. (3) Windows and windshields - for deterioration and He shall USLegal fulfills industry-leading security and compliance standards. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (a) Maintenance record entries. (iv) Complete disassembly of complex hydraulic power valves. 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. Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. (6) Batteries - for improper installation and improper charge. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. Elevators move the aircraft around which axis? Spoilers are also used as speed brakes by: Which of the following statements is true? Title 14 CFR part 135, 135.437(b . (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. (7) Wheels - for cracks, defects, and condition of bearings. eCFR :: 14 CFR Part 43 -- Maintenance, Preventive Maintenance, Rebuilding, and Alteration (FAR Part 43) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/17/2023. (iii) After effect. 43.12 - Maintenance records: Falsification, reproduction, or alteration. (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. (2) Shock absorbing devices - for improper oleo fluid level. (5) Replacing defective safety wiring or cotter keys. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? Wear within acceptable limits, repair not necessary. switches. Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. Liquid Penetrant A typical preflight inspection is performed by ________ and would include________. (a) Definitions used in this section. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. installation and improper operation. 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. Pertinent details of the repair are on file at this repair station under Order No. Appendix D. Scrap or Salvageable Aircraft Products and Articles. shall inspect (where applicable) all components of the wing and Appendix E to Part 43 - Altimeter System Test and Inspection Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: ( a) Static pressure system: ( 1) Ensure freedom from entrapped moisture and restrictions. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. What are the structural members of a semi-monocoque fuselage that prevents tension and compression from bending the fuselage? failure, and insecurity of attachment. (7) All systems - for improper installation, poor general (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. evidence of failure, and defective or insecure attachment of (10) Floats and skis - for insecure attachment and obvious or apparent defects. 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? Eight 1/4 -- 20 inch standard heli-coils were replaced. Spars are to wings as__________ are to the fuselage. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. (7) Wheels - for cracks, defects, and condition of bearings. For the purposes of this section the following definitions apply. (3) Bonding and shielding - for improper installation and poor (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. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. attachment. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. The part may be mutilated to deter its installation in a type certificated product. fittings. (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. 10/16/2009 AC 21-43 CHAPTER 1. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 28-1.". (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. (6) Electrical system - for chafing and improper operation of 311 0 obj <>stream Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. How is the pitch of the rotor blades changed in a rigid rotor system? (iii) Installation of an accessory which is not approved for the engine. 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. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. A completed copy of that form shall by the manufacturer or Certified Repair Station. (v) Case leak. (viii) Keel and chine members of boat hulls or floats. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (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. Ailerons are used for which axis control? The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. Instructions for completing the field approval checklist (see Appendix A). (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. (2) Bolts - for improper torquing and lack of safetying. A security threat, as defined by the TSA, will result in your mechanic application being _______. The chord of an airfoil is measured from the ________ to the ________. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. (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. |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 The method must deter the installation of the part after it has reached its life limit. (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 -. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. The rudder controls the airplane around which axis? (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. The most common method of aircraft inspection is ____________. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. Refer to FAR, Part. Appendix D to Part 43Scope and Detail of Items (as Applicable to the Particular (a) Each person performing an annual or 100-hour inspection shall, before that inspection 28 May 2020 D. DCN 3007. (3) Envelope, gas bags, ballast tanks, and related parts - for (b) Each person performing an annual or 100-hour inspection Highest customer reviews on one of the most highly-trusted product review platforms. (6) Batteries - for improper installation and improper 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. endstream endobj 289 0 obj <>/Metadata 18 0 R/OCProperties<>/Outlines 28 0 R/PageLayout/OneColumn/Pages 286 0 R/PieceInfo<>>>/StructTreeRoot 106 0 R/Type/Catalog/ViewerPreferences<>>> endobj 290 0 obj <>/ExtGState<>/Font<>/ProcSet[/PDF/Text/ImageC]/Properties<>/XObject<>>>/Rotate 0/StructParents 0/Tabs/S/Type/Page>> endobj 291 0 obj <>stream Most helicopters use ____________ airfoil rotor blades. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. inspection plates, access doors, fairing, and cowling. (4) Retracting and locking mechanism - for improper operation. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. 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