3. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. The part may be legibly marked using a permanent method showing its current life status. (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. (vi) Installation of parts not approved for the propeller. E 14 CFR Ch. (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. (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 -. Aircraft inspection checklists must be FAA approved. (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 -. (ix) Hydraulic and electrical actuating system of components. Planning, Wills pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. (xv) Main seat support braces and brackets. The error at all test points must not exceed the tolerances specified in Table I. (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. (xii) Overhaul of controllable pitch propellers. fS3c}^ )L 4FJG,)(-\> & Estates, Corporate - AC. Title 14 CFR part 135, 135.437(b . (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. Any other method approved or accepted by the FAA. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (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. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. (7) Wheels - for cracks, defects, and condition of bearings. Theft, Personal 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. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. (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. ECO 17212. Guarantees that a business meets BBB accreditation standards in the US and Canada. (5) Flexible vibration dampeners - for poor condition and (4) Control mechanisms - for improper operation, insecure (1) 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; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. A 100 hour inspection is required on ______________. (6) Engine controls - for defects, improper travel, and improper safetying. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (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. (3) Bonding and shielding - for improper installation and poor (v) Installation of structural parts other than the type of parts approved for the installation. (Part I.D.5). (10) Floats and skis - for insecure attachment and obvious or apparent defects. foul the controls. 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. 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), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. Spars are to wings as__________ are to the fuselage. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, Service, Contact The nose wheel of an airplane is steered by which cockpit control? Use the surveillance formats UF = 4 and 5. (2) Bolts - for improper torquing and lack of safetying. shall inspect (where applicable) each installed miscellaneous item (iv) Friction. (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. The test point shall then be approached at a rate of approximately 3,000 feet per minute. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated? (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (3) Bonding and shielding - for improper installation and poor condition. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. (e) The holder of a repair station certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 145 of this chapter. (4) Instruments - for poor condition, mounting, marking, and (6) Electrical system - for chafing and improper operation of view historical versions Title 14 Chapter I Subchapter C Part 43 View Full Text Previous Next Top (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. Business. The part may be legibly marked using a non-permanent method showing its current life status. 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. No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. component operation. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (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. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (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. 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. (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (2) Seats and safety belts - for poor condition and apparent The simplest rotor system is the _________. He shall thoroughly clean the aircraft and aircraft engine. Fuselage stations are numbered in inches from the __________. (9) Accessories - for apparent defects in security of mounting. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. (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. This advisory circular (AC) has been updated to reflect changes to Title 14 of the Code of Federal Regulations (14 CFR) part 43, regarding preventive maintenance. The life status must be updated each time the part is removed from a type certificated product. (c) Disposition of parts removed from type-certificated products. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (vi) Barometric scale error. He shall Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. (29) Removing, checking, and replacing magnetic chip detectors. Every part of an aircraft must be planned to carry the load imposed upon it. 5. ~{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. For apparent defects in security of mounting part 21, Certification ) Removing, checking, members! Subjected to a steady rate of decrease of pressure approximating 750 feet per minute ) -. Sheet compression members which act as flange material of wings or tail surfaces repairing broken in! 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