• 2022-05-29 问题

    检查机身下蒙皮是否有裂纹。 A: Examine the bottom skin panels of the fuselage for cracks. B: Inspect fuselage lowermost skin panels for cracks. C: Inspect fuselage underside skin panels for cracks.

    检查机身下蒙皮是否有裂纹。 A: Examine the bottom skin panels of the fuselage for cracks. B: Inspect fuselage lowermost skin panels for cracks. C: Inspect fuselage underside skin panels for cracks.

  • 2021-04-14 问题

    LessononeTextA课本课后练习-口语词意解析5 fuselage

    LessononeTextA课本课后练习-口语词意解析5 fuselage

  • 2021-04-14 问题

    词汇与结构All exhaust air is _____to atmosphere via a valve, usually at the rear of the fuselage.

    词汇与结构All exhaust air is _____to atmosphere via a valve, usually at the rear of the fuselage.

  • 2022-06-05 问题

    ‌The center engine is mounted aft of the fuselage structure below the vertical fin.​

    ‌The center engine is mounted aft of the fuselage structure below the vertical fin.​

  • 2022-06-05 问题

    The center engine is mounted aft of the fuselage structure below the vertical fin.

    The center engine is mounted aft of the fuselage structure below the vertical fin.

  • 2022-06-14 问题

    Body of the aircraft A: fuselage B: wing C: tail skid D: engine

    Body of the aircraft A: fuselage B: wing C: tail skid D: engine

  • 2022-06-14 问题

    ‏Body of the aircraft ‌ A: fuselage B: wing C: tail skid D: engine

    ‏Body of the aircraft ‌ A: fuselage B: wing C: tail skid D: engine

  • 2022-06-05 问题

    The center engine is mounted aft of the fuselage structure below the vertical fin. A: 正确 B: 错误

    The center engine is mounted aft of the fuselage structure below the vertical fin. A: 正确 B: 错误

  • 2022-06-09 问题

    wheel well fire A: Landing gear bay B: Avionics bay C: Cargo hold D: Rear fuselage

    wheel well fire A: Landing gear bay B: Avionics bay C: Cargo hold D: Rear fuselage

  • 2021-04-14 问题

    词汇与结构 If the cabin were ______ at sea level pressure while flown above 35,000 feet the pressure differential would exceed 9 psi limiting the structural life of the fuselage.

    词汇与结构 If the cabin were ______ at sea level pressure while flown above 35,000 feet the pressure differential would exceed 9 psi limiting the structural life of the fuselage.

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