DA20-C1 Ops Limits

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Author:
JGrizz84
ID:
259312
Filename:
DA20-C1 Ops Limits
Updated:
2014-07-19 16:29:01
Tags:
IFS
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Description:
23 JULY
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  1. Forced landing final approach airspeed (flaps, LDG, kts)
    55
  2. Min. engine-out airspeed to sustain windmilling prop (kts)
    60
  3. Forced landing final approach airspeed (flaps T/O, kts)
    60
  4. Forced landing final approach airspeed (flaps CRUISE, kts)
    64
  5. Best glide airspeed (1764 lbs) (L/D Max)
    73
  6. VVE (flaps LDG, kts) (Max. Airspeed with flaps extended)
    78
  7. VVE (flaps T/O, kts) (Max Airspeed with flaps extended)
    100
  8. VA (kts, 1764 lbs) (No full or abrupt control inputs above VA or overstress conditions will occur.)
    106
  9. VNO (Max. structural curising speed, kts)
    118
  10. Force propeller to windmill if stopped, starter inop (kts)
    137
  11. VNE (Never exceed airspeed, kts)
    164
  12. Max. permissible bank angle for steep turns (in degrees)
    60
  13. Voltmeter green arc (volts)
    12.5-16.1
  14. Usable fuel (US gal.)
    24
  15. Max takeoff weight (lbs)
    1764
  16. Max. tailwind component (kts)
    5
  17. Max. crosswind component student solo (kts)
    10
  18. DA20 max. demonstrated crosswind component (kts)
    20
  19. Max. total wind student solo (kts)
    20
  20. Max. total wind student dual (kts)
    25
  21. Max. cumulative starter op. before cooling 3-5min. (secs.)
    30
  22. Max. continuous starter operation (secs.)
    10
  23. Max. oil quantity (US qts)
    6
  24. Min. oil quantity (US qts)
    4
  25. Min oil temp. to begin an area SFL at area idle (°F)
    170
  26. Oil temperature normal operating range (°F)
    170-220
  27. Max. rpm after start until oil temp indication registers
    1000
  28. Max. oil pressure (psi)
    100
  29. Max. time for oil pressure to reach 10 psi after start (secs.)
    30
  30. Oil pressure normal operating range (psi)
    30-60
  31. Max. permissible continuous rpm (redline)
    2800
  32. Min. rpm operations with fuel pump off
    1400
  33. Min. rpm during flight if beyond gliding range of a runway (area idle)
    1400

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