A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 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. (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. (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 -. (8) Exhaust stacks - for cracks, defects, and improper (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (3) Servicing landing gear shock struts by adding oil, air, or both. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ Ensures that a website is free of malware attacks. fatigue, and distortion. |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 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. (2) Seats and safety belts - for poor condition and apparent defects. (3) Determine that the static port heater, if installed, is operative. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. (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. (v) Overhaul of pressure type carburetors, and pressure type fuel, oil and hydraulic pumps. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. Which of the following contains a minimum checklist for a 100 hour inspection? The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (viii) Keel and chine members of boat hulls or floats. What type of rotor is found on helicopters with two rotor blades? What is designed to reduce drag created by wing tip vortices? hbbd``b`Z"c`@B=8r?O K Water vapor weighs 5/8 as much as dry air. shall inspect (where applicable) all components of the wing and AC. (7) Other methods. 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. installation and improper operation. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Work is complete and compatible with other structures or systems. (ii) The inspections and maintenance tasks are performed in accordance with instructions contained by the special inspection and preventive maintenance program approved as part of the aircraft's type design or supplemental type design. Most helicopters use ____________ airfoil rotor blades. (x) Wing main ribs and compression members. (2) Wiring and conduits - for improper routing, insecure Wear within acceptable limits, repair not necessary. (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. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. (3) Windows and windshields - for deterioration and breakage. CFR prev | next (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. shall inspect (where applicable) each installed miscellaneous item The error at all test points must not exceed the tolerances specified in Table I. This change The holder of an IA cannot . What are three characteristics of a sprawling stance? The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? (b) The tests required by paragraph (a) . USLegal received the following as compared to 9 other form sites. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. (b) Temporary removal of parts from type-certificated products. 43.15 Additional performance rules for inspections. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. The part may be legibly marked using a non-permanent method showing its current life status. (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. (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 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. (ii) Hysteresis. Which maintenance action is an airframe major repair? (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. and insecure mounting. (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. 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. (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. ~{x-1\l5j`8gpnU rOJTJRnT/=7vtKt2f6%gFDEsKs;?w%wncwq^z~7?z;woA #WW'#N={*?NJ]?Vr7^1H"&]L%0it2"@DaIzfz6k>IiM9{]5]WRgZd0:)+ TMU1>odpePe=zz"]-~RUG0RI*4?`{^>7BQ$w&*m>Be]kbgi>qXSGq{ ,"Xp:,sOn7 {QnZn$WaBWp6zt7"HFM JAa1s$ &WRZ,9 \x`yIQM'*B [ QTCBF. (b) Applicability. (5) Segregation. Every part of an aircraft must be planned to carry the load imposed upon it. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. operation. (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. The test point shall be approached at a rate compatible with the test equipment. Experience a faster way to fill out and sign forms on the web. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. 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. (vi) Barometric scale error. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (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.. 43.2 - Records of overhaul and rebuilding. insecure mounting, and improper operation. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. radio group: (1) Radio and electronic equipment - for improper installation (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. 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