106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. Pt. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). (h) Each person performing an annual or 100-hour inspection 28-1.". (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. Workmanship meets the requirements of 14 CFR part 43, 43.13 (the aircraft or product is equal to its original or properly altered condition). Title 14 was last amended 2/02/2023. (2) Tag or record attached to part. 3. 14 CFR Appendix D to Part 43 - Scope and Detail of. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. shall inspect (where applicable) the following components of the (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. The part may be mutilated to deter its installation in a type certificated product. (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. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. (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 -. condition. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. a. certified repair station b. A&P mechanic with IA rating c. either. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? The __________ is used to thoroughly service a component after it is removed from an aircraft. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (i) ATCRBS-Only All-Call Interrogation: Interrogate the Mode S transponder with the ATCRBS-only all-call interrogation (0.8 microsecond P4 pulse) and verify that no reply is generated. Us, Delete 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. or hydraulic leaks, and sources of such leaks. The life status must be updated each time the part is removed from a type certificated product. CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. Instrument repairs may be performed ___________________________. H,Ht001300Ff l;
Spoilers are also used as speed brakes by: Which of the following statements is true? (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. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (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 -. (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. insecure mounting, and improper operation. Airspeed limitations for a specific aircraft are found in the __________. (a) Maintenance record entries. |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 tail rotor moves (or maintains) the helicopter yaw direction by: Many helicopters use a _______ engine to drive the main transmission and rotor systems. Ifyou believe that this page should betaken down, please follow our DMCA take down process, Ensure the security ofyour data and transactions, Georgia Interim Lien Waiver And Release2013 Sub Sub - Benning, Georgia Final Lien Waiver And Release 2013 Sub Sub - Benning, 2nd Tier Subcontractor/Supplier List - Level 3 Construction, Daigger Automated Microplate Reader Operations Manual PDF, Identity SOURCE: Docket No. (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. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. The tests in (e) through (j) apply only to Mode S transponders. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). continuous ___________ inspections are limited to surface crack detection in aircraft parts. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, 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. Title 14 CFR part 121, 121.379(b); 4. PRINCIPLE CHANGES. (5) Flight and engine controls - for improper installation and improper operation. (6) Engine controls - for defects, improper travel, and improper safetying. 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. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (3) Anti-icing devices - for improper operations and obvious (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (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) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. (3) Anti-icing devicesfor improper oper- Ensure the info you add to the Part 43 Appendix D is updated and correct. landing gear group: (1) All units - for poor condition and insecurity of A tag or other record may be attached to the part. The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. (g) Each person performing an annual or 100-hour inspection Technology, Power of (4) Permanent marking. (3) Any alteration, for fraudulent purpose, of any record or report under this part. fabric or skin deterioration, distortion, evidence of failure, looseness. (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. fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other Explanation of Changes. (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. function gtag(){dataLayer.push(arguments);} 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. attachment. (2) Studs and nuts - for improper torquing and obvious 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). A completed copy of that form shall be -. What type of rotor is found on helicopters with two rotor blades? Spanish, Localized Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. mounting, and restricted travel. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (6) Batteries - for improper installation and improper charge. shall inspect (where applicable) each installed miscellaneous item (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. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ 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". Pertinent details of the repair are on file at this repair station under Order No. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. The repair of portions of skin sheets by making additional seams. (iii) Performed without the use of tools and/or special equipment. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. Access the most extensive library of templates available. In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. Instructions for completing the field approval checklist (see Appendix A). (7) Wheels - for cracks, defects, and condition of bearings. (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 rudder controls the airplane around which axis? attachment. (ix) Hydraulic and electrical actuating system of components. (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. TopTenReviews wrote "there is such an extensive range of documents covering so many topics that it is unlikely you would need to look anywhere else". (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. (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. 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. The material's internal resistance or counterforce that opposes deformation is called: When the lift force is in equilibrium with the weight force, the aircraft: What type of stress resists a crushing force? The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. 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. Learn more Get This Form Now! 'r28J].@J)V@!Y(c,4
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