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1977 Piper Cherokee Arrow III Turbo

  • Serial #: 28R-7703335
  • Registration Tail #: N44862
  • Piper Model: PA-28R-201T
  • ICAO Code: P28S
  • WEIGHTS
    • Maximum Take-off Weight: 2,900 lbs
    • Maximum Ramp Weight: 2,900 lbs
    • Standard Empty Weight: 1,824 lbs (as currently equiped
    • Maximum Useful Load: 1,076 lbs
  • DIMENSIONS
    • Wing Span 35.5 ft 
    • Length 25.0
    • Height 7.9 ft / 2.4 m
  • Fuel Capacity Useable 72 US gal / 273 liters
  • Cruising Speed TAS 137 kts / 254 km/h
    • 75% Power, Best Power Mixture  Includes 45 minute fuel reserve plus allowance for fuel used during taxi, take-off, climb and descent.
  • SPEEDS
    • Rotation  (Vr)                                   = 77 KIAS (at maximum weight of 2,900 pounds & 0 degrees flaps)
    • Rotation  (Vr)                                   = 64 KIAS (at maximum weight of 2,900 pounds & 25 degrees flaps)
    • Best Rate (Vy)
      • 2750 lbs, gear down, flaps up   = 78 KIAS 
      • 2750 lbs, gear up, flaps up        = 90 KIAS
    • Best Angle (Vx)
      • 2750 lbs, geardown, flaps up   = 71KIAS
      • 2750 lbs, gearup,flaps up         = 78 KIAS
    • Stall Clean (Vs)                               = 63 KIAS
    • Stall Landing Configuration  (Vso) = 56 KIAS
    • Best Glide - Clean (V glide)            = 97 KIAS
    • Climb                                              = 104 KIAS
      • 2900 pounds, sea level = 940 fpm
      • 2300 pounds, sea level = 1300 fpm
    • Cruise Climb                                   = 104 KTS
      • Mixture: Rich / Propeller 2450 RPM / Throttle 33 inches Manifold Pressure / 14 gallons per hour
    • Turbulent Air Operating Speed (Vno)      = 146 KIAS (see POH Subsection 2.3)
    • Maneuvering Speed (Va)  2900 lbs          = 119 KIAS
    • Never Exceed                                          = 183 KIAS
    • Gear down (Vge)                                     = 129 KIAS
    • Maximum Flap Speed (Vfe)                     = 103 KIAS
    • Landing Final Approach (Flaps40°)         = 75 KIAS
    • Maximum Demonstrated Crosswind      = 17 KTS
  • Cruising Range 880 NM / 1,630 KM / 1,012 SM
    • 45 min. reserves @ 55% Power @ 9,000 ft, peak EGT mixture (11 gallons per hour)
  • Flight above 20,000 feet is not approved.
    Service Ceiling (100 fpm) 16,200 ft / 4,983 m
  • Take-off Ground Roll 1,110 feet (Sea level, standard pressude, standard tempature, takeoff weight 2,200, no wind)
    • Take-off Distance Total over 50 ft Obstacle 1,600 ft / 487 m
  • Landing Ground Roll 645 feet  (Sea level, standard pressude, standard tempature, maximum weight 2,900, no wind, full braking)
    • Landing Distance Total over 50 ft Obstacle 1,520 ft / 463 m

ENGINE

AVIONICS / EQUIPMENT