(ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (e) Approval requirements. (18) Replacing wheels and skis where no weight and balance computation is involved. ); (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. 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. shall, before that inspection, remove or open all necessary (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. For the purposes of this section the following definitions apply. Where is the throttle typically located on a helicopter? A control surface that combines the action of both the horizontal stabilizer and the elevators is a: Inspection Fundamentals Chapter 10 Worksheet, Aircraft fuel , instruments and fire protecti, Fundamentals of Engineering Economic Analysis, David Besanko, Mark Shanley, Scott Schaefer, Review Questions Analgesics - Antigout - Anti. The application form, to become a certified mechanic is FAA Form ______. (where practicable) improper operation. 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. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). (2) Shock absorbing devices - for improper oleo fluid level. Witt OBriens_checklists index for oil transfer procedures list of items required the us federal regulations per 33 cfr 155.750 and california code of (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. Highest customer reviews on one of the most highly-trusted product review platforms. How are main rotors of helicopters classified? (b) Each person performing an annual or 100-hour inspection 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. 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. Where should you find this entry? (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. The part may be mutilated to deter its installation in a type certificated product. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. Collapse to view only 43.13 - Performance rules (general). 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. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? fittings. installation and improper operation. A 100 hour inspection is required on ______________. (6) Engine controls - for defects, improper travel, and improper safetying. ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. By an identification letter stamped on one of the hexes of the nozzle body (3) Bonding and shielding - for improper installation and poor condition. H,Ht001300Ff l; Forms, Real Estate breakage. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. 2115 0 obj <>stream (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. Roll, pitch, yaw. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. condition, apparent and obvious defects, and insecurity of ); (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. (ix) Hydraulic and electrical actuating system of components. (ii) Monocoque or semimonocoque wings or control surfaces. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. What classification of turbulence would require an over "G" inspection? The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. When the angle of attack of an airfoil is increased so it reaches maximum lift the: Ribs can be ___________ by stamping holes in the assembly. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (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. 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) Seats and safety belts - for poor condition and apparent Experience a faster way to fill out and sign forms on the web. (9) Accessories - for apparent defects in security of mounting. 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. (iv) Friction. Title 14 was last amended 2/02/2023. If Pertinent details of the repair are on file at this repair station under Order No. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. What is an attitude, and what are some common positive and negative attitudes about physical activity? (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (5) Flight and engine controls - for improper installation and improper operation. Business. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. (2) Studs and nuts - for improper torquing and obvious Refer to FAR, Part. shall inspect (where applicable) all components of the wing and (xiv) Members of the side truss, horizontal truss, or bulkheads. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . Cables that travel completely through bulkheads require the use of a _______ and should not be deflected more than ________ from a straight line. (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. foul the controls. 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. (2) Shock absorbing devices - for improper oleo fluid level. (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. (4) Appliance major repairs. (9) Accessories - for apparent defects in security of mounting. May 21/2007. 43, App. 23, 1964, unless otherwise noted. (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. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (b) The tests required by paragraph (a) . (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. 1993, 29 FR 5451, Apr. (v) Installation of structural parts other than the type of parts approved for the installation. (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. "Removed right wing from aircraft and removed skin from outer 6 feet. Airspeed limitations for a specific aircraft are found in the __________. (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. 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