(3) Bonding and shielding - for improper installation and poor condition. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. (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. (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. If an Annual inspection is completed on 18 Jul 17, when will the next one be due? inspection plates, access doors, fairing, and cowling. or hydraulic leaks, and sources of such leaks. (4) Retracting and locking mechanism - for improper The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. 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. (3) That product does not accumulate time in service while the part is removed. The part may be legibly marked using a permanent method showing its current life status. (5) Flexible vibration dampeners - for poor condition and deterioration. A ________ may request to see your mechanic certificate. 2115 0 obj <>stream (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/14/2023. poor condition. 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. (5) Flexible vibration dampeners - for poor condition and What is the primary purpose of the helicopter main rotor transmission? When must an Airworthiness Directive be complied with? (7) Wheels - for cracks, defects, and condition of bearings. (3) Bonding and shielding - for improper installation and poor condition. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. and improper internal tolerances. Use the surveillance formats UF = 4 and 5. (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. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Technology, Power of Where are technical descriptions of certificated propellers found? (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). insecure attachment, improper component installation, and improper 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 -. B. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in . (3) Propeller major repairs. (f) Each person performing an annual or 100-hour inspection Collapse to view only 43.13 - Performance rules (general). mounting, and obvious defects. During the next week, create a list of at least 10 things you could have done to conserve the water you use. PRINCIPLE CHANGES. Unless otherwise notified by the administrator, the methods, techniques, and practices contained in the maintenance manual or the maintenance part of the manual of the holder of an air carrier operating certificate or an operating certificate under Part 121 or 135 and Part 129 operators holding operations specifications (that is required by its operating specifications to provide a continuous airworthiness maintenance and inspection program) constitute acceptable means of compliance with this section. Which of the following contains a minimum checklist for 100-hour inspections of engines? shall inspect (where applicable) the following components of the foul the controls. (7) Wheels - for cracks, defects, and condition of bearings. Appendix E to Part 43 - Altimeter System Test and Inspection Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: ( a) Static pressure system: ( 1) Ensure freedom from entrapped moisture and restrictions. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. 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. (ii) Repairing or machining of steel hubs. (23) Cleaning or replacing fuel and oil strainers or filter elements. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. 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. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? Gyroscopic precession occurs approximately _______ degrees in the direction of rotation. (2) Studs and nuts - for improper torquing and obvious defects. 0 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) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (3) Envelope, gas bags, ballast tanks, and related parts - for (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. %%EOF (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. (j) Each person performing an annual or 100-hour inspection Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. USLegal received the following as compared to 9 other form sites. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. This change The nose wheel of an airplane is steered by which cockpit control? Certificated mechanics with a powerplant rating may perform. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). 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. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . The __________ is used to thoroughly service a component after it is removed from an aircraft. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. 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? 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. (3) Bonding and shielding - for improper installation and poor Where is the center of gravity located on an aircraft with tricycle landing gear? (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. (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. (iv) Friction. shall inspect (where applicable) the following components of the (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 -. ECO 17212. (b) Rotorcraft. 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. (6) Engine controls - for defects, improper travel, and improper safetying. (e) Each person performing an annual or 100-hour inspection (2) Seats and safety belts - for poor condition and apparent defects. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (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. 311 0 obj <>stream (6) Electrical system - for chafing and improper operation of switches. (b) Applicability. 0 Blade attachment and motion relative to the hub.