Doss IFS Limits (Black)

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Author:
cdavies87
ID:
265222
Filename:
Doss IFS Limits (Black)
Updated:
2014-03-05 19:49:35
Tags:
boldface limits doss ifs
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Description:
Black Limits for Doss IFS
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  1. VS0 (Stall speed in LDG configuration, kts)
    34
  2. VS1 (Stall speed in CRUISE configuration, kts)
    42
  3. VG (Rotate Speed, kts)
    44
  4. Lift-off airspeed (kts)
    52
  5. Normal landing final approach airspeed (kts)
    60
  6. No-Flap landing final approach airspeed (kts)
    65
  7. VX (flaps T/O, kts)      (Best angle of climb)
    60
  8. VX (flaps CRUISE, kts)      (Best angle of climb)
    65
  9. Vy (flaps T/O, kts)      (Best rate of climb)
    66
  10. Vy (flaps CRUISE, kts)      (Best rate of climb)
    70
  11. Positive limit load factor (flaps CRUISE)
    +4.4
  12. Negative limit load factor (flaps CRUISE)
    -2.2
  13. Positive limit load factor (flaps T/O or LDG)
    +2.0
  14. Negative limit load factor (flaps T/O or LDG)
    0
  15. Voltmeter lower limit red arc (volts)
    8-11
  16. Voltmeter caution range yellow arc (volts)
    11-12.5
  17. Voltmeter upper limit red line (volts)
    16.1
  18. Approved fuel grade
    100LL
  19. Fuel tank capacity (US gal.)
    24.5
  20. Max. ramp weight (lbs)
    1770
  21. Max. landing weight (lbs)
    1764
  22. Forward CG limit (at or below 1653 lbs)
    7.95
  23. Forward CG limit (1764 lbs)
    8.07
  24. Aft CG limit (1764 lbs)
    12.16
  25. Aft CG limit (at or below 1653 lbs)
    12.48
  26. Max weight in baggage compartment (lbs)
    44
  27. Min. rpm during engine runup idle check
    975
  28. Min. permissible static rpm (full throttle runup)
    2000
  29. Tachometer normal operating range (rpm)
    700-2800
  30. Min. rpm drop during magneto check
    25
  31. Max. rpm drop during magneto check
    150
  32. Max. rpm drop difference between magnetos
    50
  33. Max. permissible continuous bhp
    125
  34. Min. oil pressure (psi)
    10
  35. Max. oil pressure for full power operation if OAT <0°C (psi)
    70
  36. Min. oil temperature (°F)
    75
  37. Min. oil temp for full power operation if oil pressure norm (°F)
    100
  38. Max. oil temperature (°F)
    240
  39. Fuel pressure lower limit red line (psi)
    3.5
  40. Fuel pressure upper limit red line (psi)
    16.5
  41. Max. time for CHT below 300°F in descent (minutes)
    5
  42. Min. CHT (°F) takeoff & descent
    240
  43. CHT normal operating range (°F)
    300-420
  44. CHT caution range (°F)
    420-460
  45. Max. CHT (°F)
    460
  46. Max. OAT (°C) operation w/ full winterization kit
    0
  47. Max. OAT (°C) operation w/ partial winterization kit
    12.5
  48. Max. crosswind component student dual (kts)
    15
  49. Maximum airplane structural temperature (°C)
    55
  50. Propeller approx. minimum ground clearance (inches)
    10
  51. Main landing gear tire pressure (psi)
    33
  52. Nose gear tire pressure (psi)
    26
  53. Min. OAT (°C) cabin heat not req for 10 min. before T/O
    -20

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