相关题目
Airplane certification conditions include one engine becoming inoperative and windmilling (or, in airplanes with autofeathering devices, feathered), not more than a 5° bank toward the operative engine, takeoff power on the operative engine, landing gear up, flaps in the takeoff position, and the most critical C.G.
Flight Controls System refers to those units and components which furnish a means of manually controlling the flight attitude characteristics of the aircraft, including items such as hydraulic boost system, rudder pedals, control column linkages, control cables, tab controls, mounting brackets, etc.
This Section of the Pilot＇s Operating Handbook shall contain the appropriate Supplements (operating information) necessary to safely and efficiently operate the airplane when equipped with the various optional system and equipment not provided with the standard airplane.
The procedure shall specify that intentionally rendering one engine inoperative for the purpose of demonstrating, or training in, the recognition of VMCA will be done by starting at or above VSSE, then gradually reducing the speed (at approximately one knot per second) until either VMCA or stall warning, whichever occurs first, is obtained.
Range values should include an allowance for fuel to start, taxi, takeoff, climb and reserve. For start, taxi and takeoff, allow 5 minutes of fuel flow at takeoff power. Reserve shall be computed as 45 minutes at the cruise power to be used for the flight.
Polyurethane is used for producing the fuselage, wing tips, and other curved parts of small aircraft; relatively inexpensive, fuel resistant, and compatible with most adhesives; do not use a hot wire to cut polyurethane foam; easily contoured with a large knife and sanding equipment.
Distribution of air conditioning system is used to induct and distribute air. Includes equipment rack cooling systems and items such as blowers, scoops, ducting, inlets, check valves, etc. Does not include valves which are part of pressurization and temperature control.
Doors refer to those removable units used for entrance or exit, and for enclosing other structure contained within the fuselage, including passenger and crew doors, cargo doors, emergence exits, etc. Electrical and hydraulic systems associated with door control are included as appropriate.
In the description of the airplane＇s Engine, give the following information as deemed necessary: 1.Manufacturer and model number 2.Type of engine, number of cylinders, type of compressor, etc. 3.Rated power 4.Rated engine speed 5.Gear reduction if applicable 6.Accessories normally installed 7.Turbocharging or other augmentation 8.Restrictions, warnings, tips
In the description of the airplane＇s Engine, abnormal operations should be discussed briefly. This should be held to the minimum that will help a pilot to correct a situation or enable him to describe it to a mechanic. It should not be a maintenance procedure.
