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SOCATA-DAHER TBM 900

667 Rhubarb1263  3.8 years ago
185 downloads

The design of the TBM family originates from the Mooney 301, a comparatively low-powered and smaller prototype Mooney developed in the early 1980s. Following Mooney's acquisition by French owners, Mooney and SOCATA started of a joint venture for the purpose of developing and manufacturing a new, enlarged turboprop design, which was designated as the TBM 700. Emphasis was placed upon the design's speed, altitude, and reliability. Upon its entry onto the market in 1990, it was the first high-performance single-engine passenger/cargo aircraft to enter production.

Spotlights

General Characteristics

  • Created On Windows
  • Wingspan 60.7ft (18.5m)
  • Length 48.9ft (14.9m)
  • Height 21.5ft (6.5m)
  • Empty Weight 11,966lbs (5,427kg)
  • Loaded Weight 13,702lbs (6,215kg)

Performance

  • Horse Power/Weight Ratio 0.437
  • Wing Loading 24.6lbs/ft2 (120.1kg/m2)
  • Wing Area 556.9ft2 (51.7m2)
  • Drag Points 4185

Parts

  • Number of Parts 140
  • Control Surfaces 7
  • Performance Cost 553