(2) Seats and safety belts - for poor condition and apparent defects. 43, App. Which of the following contains a minimum checklist for a 100 hour inspection? 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. (v) Replacement of outer laminations on fixed pitch wood propellers. Us, Delete (4) Permanent marking. (c) Preventive maintenance. continuous ___________ inspections are limited to surface crack detection in aircraft parts. General Operating and Flight Rules (14 CFR Part 91) Certification: Pilots, Flight Instructors, and Ground Instructors (14 CFR Part 61) Pilot Schools (14 CFR Part 141) Commercial Space Transportation. (e) Approval requirements. breakage. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. Blade attachment and motion relative to the hub. Instrument repairs may be performed ___________________________. The simplest rotor system is the _________. Most airplanes today are built using a ___________ fuselage. defects. (2) Powerplant major repairs. Enjoy smart fillable fields and interactivity. . Title 14 was last amended 2/10/2023. Ensures that a website is free of malware attacks. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (6) Electrical system - for chafing and improper operation of switches. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. If the transponder is so equipped, use the communication formats UF = 20, 21, and 24. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. fittings. (4) Control mechanisms - for improper operation, insecure If Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. (ix) Hydraulic and electrical actuating system of components. 43.15 Additional performance rules for inspections. 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. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. 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. 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. Planning, Wills Build Technologies Since the experimental aircraft are not rolling off a manufacturing line, A&Ps will find that there is variation in construction methods and materials. LLC, Internet These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. Where are technical descriptions of certificated propellers found? (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. shall inspect (where applicable) the following components of the (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. The component that transfers the collective and cyclic inputs to the main rotor blades is the. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. 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 If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. (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. CFR prev | next attachment. (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. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (b) Temporary removal of parts from type-certificated products. Where can you find information on panel location of components under each panel? 2115 0 obj <>stream USLegal fulfills industry-leading security and compliance standards. (c) Annual and 100-hour inspections. mounting, and restricted travel. 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. The rudder controls the airplane around which axis? (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. 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. Purpose. safetying. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. The interrogations should be made at a nominal rate of 50 interrogations per second. center section assembly for poor general condition, fabric or skin (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. shall inspect (where applicable) the following components of the Experience a faster way to fill out and sign forms on the web. Guarantees that a business meets BBB accreditation standards in the US and Canada. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. (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. (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. Fuselage stations are numbered in inches from the __________. that is not otherwise covered by this listing for improper (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. Ni}Ja7$? (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. Get access to thousands of forms. Title 14 was last amended 2/02/2023. "Removed right wing from aircraft and removed skin from outer 6 feet. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. Inspection programs for aircraft operating under 21.191 (d) and (e) However, this paragraph does not authorize the performance of any inspection required by Part 91 or Part 125 of this chapter or any inspection performed after a major repair or alteration. An aircraft Type Certificate Data Sheet contains. 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. Summary of Proposed Rule. Sign off for an annual inspection can be done by who? How is the pitch of the rotor blades changed in a rigid rotor system? apparent defects. Learn more ME406 Series Emergency Locator Transmitter - ACR. What is the usual final step of an annual inspection before the maintenance entry is made? 1.5. (x) Wing main ribs and compression members. (2) Systems and components - for improper installation, apparent %%EOF (a) Maintenance record entries. shall inspect (where applicable) components of the engine and What is an attitude, and what are some common positive and negative attitudes about physical activity? 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. (3) Bonding and shielding - for improper installation and poor condition. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. (vi) Installation of parts not approved for the propeller. 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. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. 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