IFS DA20 Boldface/Ops Limits

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Author:
Anonymous
ID:
8051
Filename:
IFS DA20 Boldface/Ops Limits
Updated:
2010-02-24 22:31:28
Tags:
IFS Boldface Ops Limits
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Description:
To help prepare those that will be attending IFS (Initial Flight Screening)
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  1. Forced landing final approach airspeed (flaps LDG)
    55
  2. Min. engine-out airspeed to sustain windmilling prop
    60
  3. Forced landing final approach airspeed (flaps T/O)
    60
  4. Forced landing final approach airspeed (flaps CRUISE)
    64
  5. Best glide airspeed (1764 lbs) (L/D Max)
    73
  6. VFE (flaps LDG) (Max. Airspeed with flaps extended)
    78
  7. VFE (flaps T/O) (Max. Airspeed with flaps extended)
    100
  8. VA (1764 lbs) (No full or abrupt control inputs aboveVA or overstress conditions will occur.)
    106
  9. VNO (Max. structural cruising speed)
    118
  10. Force propeller to windmill if stopped and starter is inop
    137
  11. VNE (Never exceed airspeed)
    164
  12. Maximum permissible bank angle for steep turns
    60°
  13. Voltmeter green arc (volts)
    12.5-16
  14. Usable fuel (US gal.)
    24.0
  15. Max. takeoff weight (lbs)
    1764
  16. Min. rpm for in-flight (area) idle beyond gliding rangeof a runway
    1400
  17. Min. rpm operations with fuel pump off
    1400
  18. Max. permissible continuous rpm
    2800
  19. Oil pressure normal operating range (psi)
    30-60
  20. Max. time for oil pressure to reach 10 psi after start
    30 sec.
  21. Max. oil pressure (psi)
    100
  22. Max. rpm after start until oil temp indication registers
    1000
  23. Oil temperature normal operating range (°F)
    170-220
  24. Min oil temp. to begin an area SFL at Area Idle (°F)
    170
  25. Min. oil quantity (US qts)
    4
  26. Max. oil quantity (US qts)
    6
  27. Max. continuous starter operation
    10 sec.
  28. Max. cumulative starter op. before cooling 3-5min.
    30 sec.
  29. Max. total wind student dual (kts)
    25
  30. Max. total wind student solo (kts)
    20
  31. DA20 max. demonstrated crosswind component (kts)
    20
  32. Max. crosswind component student solo (kts)
    10
  33. Max. tailwind component (kts)
    5
  34. ENGINE FIRE ON THE GROUND
    • FUEL SHUTOFF VALVE — OFF
    • CABIN HEAT — OFF
  35. ELECTRICAL FIRE ON THE GROUND
    GEN/BAT MASTER SWITCH — OFF
  36. ABORT
    • THROTTLE — IDLE
    • BRAKES — AS REQUIRED
    • FLAPS — CRUISE
  37. ENGINE MALFUNCTION IN FLIGHT (SUFFICIENT RUNWAY REMAINING TO LAND)
    • AIRSPEED — 60 KIAS
    • FLAPS — LDG
  38. ENGINE MALFUNCTION IN FLIGHT (FUEL PRESSURE LOSS)
    FUEL PUMP — ON
  39. ENGINE FIRE DURING FLIGHT
    • FUEL SHUTOFF VALVE — OFF
    • CABIN HEAT — OFF
  40. ELECTRICAL FIRE DURING FLIGHT
    • GEN/BAT MASTER SWITCH — OFF
    • AIR VENTS AND WINDOWS — OPEN
  41. CABIN FIRE IN FLIGHT
    • GEN/BAT MASTER SWITCH — OFF
    • AIR VENTS AND WINDOWS — OPEN
    • CABIN HEAT — OFF

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