(7) Wheels - for cracks, defects, and condition of bearings. In the event of a discharge resulting from a spill of hazardous substances or oil from a construction site (Parts III.A.3.c.iii and Part III.A.3.c.iv), where the release is an amount equal to or in excess of a reporting quantity established under either 40 CFR Part 110, 40 CFR Part 117, or 40 CFR Part 302, occurring during Service, Contact (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (b) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other evidence of failure, and defective or insecure attachment of fittings. (3) Servicing landing gear shock struts by adding oil, air, or both. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. 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. 14 CFR 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 | Electronic Code of Federal Regulations (e-CFR) | US Law | LII / Legal Information Institute LII Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. (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. mounting. Which type of inspection program do the 14 CFR part 121 Airlines use? The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. Enjoy smart fillable fields and interactivity. & Estates, Corporate - (4) Control mechanisms - for improper operation, insecure (c) Disposition of parts removed from type-certificated products. (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. (2) Seats and safety belts - for poor condition and apparent attachment. Every part of an aircraft must be planned to carry the load imposed upon it. (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. Title 14 CFR Appendix D to Part 43Scope and detail of items (as applicable to the particular aircraft) to be included in annual and 100-hour inspections A properly written checklist, such as the one shown in this site, includes all the items of Appendix D. Theft, Personal The pilot, walking around the aircraft A special Inspection may include the following: Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. (2) Powerplant major alterations. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (j) Each person performing an annual or 100-hour inspection (2) Powerplant major repairs. The chord of an airfoil is measured from the ________ to the ________. (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). ( 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. shall inspect (where applicable) components of the engine and Sign off for an annual inspection can be done by who? If there is weak cylinder compression, for improper internal condition and improper internal tolerances. 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. Use the surveillance formats UF = 4 and 5. view historical versions Title 14 Chapter I Subchapter C Part 43 View Full Text Previous Next Top (7) Wheels - for cracks, defects, and condition of bearings. operation. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. (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. (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. E 14 CFR Ch. Where are technical descriptions of certificated propellers found? Which type of aircraft structures reduce fuel consumpution and increase range? AC. defects. (8) Exhaust stacks - for cracks, defects, and improper attachment. 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. Title 14 - Aeronautics and Space CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION SUBCHAPTER C - AIRCRAFT PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION 43.15 Additional performance rules for inspections. With US Legal Forms the process of creating legal documents is anxiety-free. (b) Applicability. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. (v) Replacement of outer laminations on fixed pitch wood propellers. (a) Major alterations - (1) Airframe major alterations. (xv) Main seat support braces and brackets. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (9) Accessories - for apparent defects in security of mounting. With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Decrease engine output RPM to optimum rotor RPM. inspection plates, access doors, fairing, and cowling. (iii) Rewinding the field coil of an electrical accessory. The method must deter the installation of the part after it has reached its life limit. (c) Preventive maintenance. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. %PDF-1.6 % (5) Flight and engine controls - for improper installation and improper operation. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. (v) Installation of propeller de-icing system. (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. fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other 14 CFR Part 43 AppendixD When must an Airworthiness Directive (AD) be complied with after it becomes effective? (e) Approval requirements. Wing braces are the main structural member of a wing. (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. (7) Wheels - for cracks, defects, and condition of bearings. Title 14 was last amended 2/02/2023. (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. My Account, Forms in Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. 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. particles or foreign matter on screens and sump drain plugs. Cowl flaps are movable parts of the cowling that open and close in order to: Primary flight control surfaces need to be balanced so they do not: Flight control surfaces must be balanced whenever: When the airplane is turned left the aileron on the pilot's __________ points up. Title 14 CFR part 135, 135.437(b . (b) Listing of discrepancies and placards. 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. The leading editor is already at your fingertips providing you with various useful instruments for submitting a Part 43 Appendix D. The following tips, combined with the editor will assist you with the entire process. 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". '; (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. (23) Cleaning or replacing fuel and oil strainers or filter elements. 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (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. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). (2) Seats and safety belts - for poor condition and apparent defects. installation and improper operation. 4. 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? 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". (2) Systems and components - for improper installation, apparent (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. 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. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (3) Bonding and shielding - for improper installation and poor condition. The primary flight controls on a fixed wing aircraft are: Which of the controls match the following actions? Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). component operation. USLegal received the following as compared to 9 other form sites. This system may include electronic, paper, or other means of record keeping. An aircraft Type Certificate Data Sheet contains. (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. (d) Progressive inspection. radio group: (1) Radio and electronic equipment - for improper installation (3) Determine that the static port heater, if installed, is operative. Ensures that a website is free of malware attacks. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. During an annual inspection, if a defect is found which makes the aircraft un-airworthy, the person disapproving must, provide a written notice of the defect to the owner. 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