(第3部分)执照英语官方题库参考答案解析v2.2r无水印版

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Troubleshooting information describing probable malfunctions, how to recognize those malfunctions, and the remedial action for those malfunctions shall be provided.

Communication system include the units and components which furnish a means of communicating from one part of the aircraft to another and between the aircraft and other aircraft or ground stations.

Data Transmission or Auto Calling, e.g. SELCAL, presents information derived from pulse-coded transmissions.

Cargo compartments have floor panels and linings. The linings keep smoke in the compartments and prevent damage to the lines and electrical wires.

Precautions and limitations such as use of landing gear and control surface locks, minimum turning radius, maximum towing and pushing loads on nose landing gear, etc.

The mach trim actuator also causes the elevator to be in a more nose down position during takeoff which allows the pilots to move the stabilizer to a more nose up position.

A wire code consists of a circuit function code, wire number, wire segment letter and wire size. Frequently a suffix indicating ground (N), phase (A, B, etc.) or thermocouple material (alumel, etc.) is added.

When there are several words in English for the same thing (synonyms), STE permits one of these synonyms to the exclusion of the others.

Suggestions for inclusion of emergency procedures for supercharger/turbocharger failure

Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position.

Best Angle-of-Climb Speed is the airspeed which delivers the greatest gain of altitude in the shortest possible horizontal distance.

TIT Gauge is a temperature measuring system that senses gas temperature in the turbine section of the engine.

Reference Datum is an imaginary vertical plane from which all horizontal distances are measured for balance purposes.

Arm is the horizontal distance from the reference datum to the center of gravity (C.G.) of an item.

Station refers to a location along the airplane fuselage usually given in terms of distance from the reference datum.

Limitations associated with optional systems or equipment may be included in this Section or in Section 9, Supplements.

Airspeed limitations and the operational significance of such limitations shall be provided.

Do not exceed this speed or Mach Number except in smooth air and then only with caution.

For turbopropeller powered airplanes only, the established temperatures and corresponding altitude limits of powerplant components and engine fluids shall be stated.

The wording given in the approved examples is not mandatory. It shows only one method to write the same information with approved words. You can frequently use different constructions with other approved words to say the same thing.

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