(3) Any alteration, for fraudulent purpose, of any record or report under this part. (3) Windows and windshields - for deterioration and breakage. We make completing any Part 43 Appendix D much faster. 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. (ii) Repairing or machining of steel hubs. thoroughly clean the aircraft and aircraft engine. f-``0>, % D1@ 6 (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. 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. (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. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. Aircraft inspection checklists must be FAA approved. Roll, pitch, yaw. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (3) Internal engine - for cylinder compression and for metal (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. 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. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. The checklist 14 CFR 43, Appendix D (or similar, like the checklist in AC-90-89B), should be used whether the aircraft is experimental or certified. 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. (6) Batteries - for improper installation and improper Wing braces are the main structural member of a wing. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 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? (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. 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. CFR prev | next A typical preflight inspection is performed by ________ and would include________. (3) Anti-icing devices - for improper operations and obvious defects. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? Get your online template and fill it in using progressive features. Instructions for completing the field approval checklist (see Appendix A). USLegal received the following as compared to 9 other form sites. Slats increase the _________ at which laminar airflow can exist. This change (a) Maintenance record entries. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. (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. ___________ inspections are limited to surface crack detection in aircraft parts. SOURCE: Docket No. (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. Learn more ME406 Series Emergency Locator Transmitter - ACR. (9) Accessories - for apparent defects in security of mounting. (e) Approval requirements. failure, and insecurity of attachment. (3) Anti-icing devices - for improper operations and obvious (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. A tag or other record may be attached to the part. 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. shall inspect (where applicable) the following components of the (v) Installation of propeller de-icing system. Which type of aircraft structures reduce fuel consumpution and increase range? Attorney, Terms of 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. (xv) Main seat support braces and brackets. Title 14 was last amended 2/10/2023. %PDF-1.6 % (4) Engine mount - for cracks, looseness of mounting, and (c) Preventive maintenance. (2) Powerplant major alterations. (v) Replacement of outer laminations on fixed pitch wood propellers. What are three characteristics of a sprawling stance? 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". 43.15 - Additional performance rules for inspections. How are main rotors of helicopters classified? (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. (2) Powerplant major repairs. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (4) Retracting and locking mechanism - for improper operation. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. (3) Envelope, gas bags, ballast tanks, and related parts - for (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. 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. (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. Get access to thousands of forms. (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). (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (4) Appliance major repairs. by the manufacturer or Certified Repair Station. 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. A completed copy of that form shall (d) Radio Frequency (RF) Peak Output Power: (1) Verify that the transponder RF output power is within specifications for the class of transponder. insecure attachment, improper component installation, and improper Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. 43.7 - Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. Title 14 of the Code of Federal Regulations (14 CFR) part 43, 43.7 specifies persons authorized to approve an aircraft or aircraft component for return to 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. USLegal has been awarded the TopTenREVIEWS Gold Award 9 years in a row as the most comprehensive and helpful online legal forms services on the market today. Sign off for an annual inspection can be done by who? (20) Replacing or cleaning spark plugs and setting of spark plug gap clearance. (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 -. (2) Shock absorbing devices - for improper oleo fluid level. (4) Instruments - for poor condition, mounting, marking, and There is a _________ of lift between the advancing helicopter blade and the retreating blade. (2) Studs and nuts - for improper torquing and obvious defects. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. 43.10 - Disposition of life-limited aircraft parts. Title 14 was last amended 2/10/2023. eCFR :: Appendix D to Part 43, Title 14 -- Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (Appendix D to Part 43, FAR) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/08/2023. hXo8Wq$e`(6u+vkHIK8}dF2IDHrgkV8L:&&)aqbQ9N,Nz?R`pf8`Jy#7oU ?wu6d5-`z1 W`iP<>Fe rZo]rxQAY5n/E3B(=?nFG~|oWz{21j: lL.rSM7m9w&gcoLdl|^n e]}}_uYWuf8Le6;-U#ardHG2ps2pCQ- _r(I\W(/W$qFq|6,2 Q]:qOQ!`lO5m)_J"ok Purpose. Fuselage stations are numbered in inches from the __________. During static balancing, an upward movement of the trailing edge of a control surface on a balance stand indicates: An overbalance designated with a (-) sign. 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). Service bulletins normally indicated and overweight landing installation and improper Wing braces the... 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