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HS-121 Trident BEA(G-AWZT)

525 FlightClipper  3 days ago

Hawker-Siddeley HS121 Trident airliner

The HS121 Trident (English name: Hawker Siddeley HS121 Trident) is a three-engine short-haul civil airliner developed by the British company de Havilland Company (later merged into Hawker Siddeley Company) in the 60s of the 20th century, mainly serving British European airlines, with a total of 117 aircraft produced. The model was used as a leader's plane in Chinese mainland and was retired in the early 90s. It adopts three independent full hydraulic control systems and S-shaped air intake design, and was originally planned to be equipped with an RB141 engine, but later changed to a lower thrust RB163 Spey engine. The aircraft has derived five models: 1C, 1E, 2E, 3B and Super 3B, of which 23 2E aircraft have been delivered to China's civil aviation. The Type 3B is equipped with an RB142 engine at the tail to form a four-engine layout, and the Super 3B is specially developed for China's civil aviation, with a maximum passenger capacity of 180 people. With a cruising speed of 573-604 mph and a range of 1,800-2,400 miles, it was one of the early passenger aircraft to achieve autonomous driving

AG1:LANDING GEAR LIGHT(You must extend landing gear)

AG2:WING LIGHT

AG3:NAV LIGHT

AG4&BREAK:Reverse thrust

The landing speed is usually less than 130 knots, and the takeoff speed is usually less than 125 knots.

The Hawke Siddeley Trident airliner, registered G-AWZI, was destroyed in a Zagreb air crash in Yugoslavia due to a mistake by air traffic controllers, killing 176 people and not surviving

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COCKPIT

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All systems are turned on by default, and the warning light on the flight engineer panel turns on when turned off

REAL IMAGE

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USE MOD

WEATHER

Washington&B.C

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General Characteristics

  • Created On Windows
  • Wingspan 132.0ft (40.2m)
  • Length 165.9ft (50.6m)
  • Height 42.3ft (12.9m)
  • Empty Weight N/A
  • Loaded Weight 166,213lbs (75,393kg)

Performance

  • Power/Weight Ratio 0.527
  • Wing Loading 28.7lbs/ft2 (140.2kg/m2)
  • Wing Area 5,788.4ft2 (537.8m2)
  • Drag Points 48130

Parts

  • Number of Parts 393
  • Control Surfaces 9
  • Performance Cost 2,002