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Dash 1 chapter 2.csv

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  1. Number of static wicks and placement
    • 17 total
    • 4 on each wing
    • 9 on elevator
  2. Battery voltage for start
    23.5 VDC
  3. Minimum main gear strut extension
    2.0 inches
  4. Minimum nose gear strut extension
    2.5 inches
  5. Delay between ejections w/ISS in both
    0.37 second
  6. Do not connect external power with battery voltage below
    22.0 V
  7. Connect external power for battery voltage below
    23.5 V
  8. LOW AOA (amber donut)
    10.5 units
  9. HIGH AOA (green chevron)
    18 units
  10. Best cockpit cooling at altitudes below 7500 MSL
    Set RAM AIR FLOW switch to OFF
  11. PMU IOAT limit for start
    121 C
  12. Indications for IOAT above PMU limit
    • IOAT and ITT indicated by amber dashes
    • PMU FAIL annunciator illuminated
  13. Use HIGH IOAT START procedure
    80 C
  14. Max ITT for auto start
    130 C
  15. Time for STARTER SWITCH MANUAL to cool IOAT or clear residual fuel
    20 sec
  16. Aural tones inaudible during engine start until
    50% N1
  17. Stay clear area from aircraft with engine running
    3 feet
  18. Time between GEN switch ON and AVIONICS MASTER switch ON
    10 sec
  19. Minimum idle on ground
    60% N1
  20. Prohibited range of stabilized prop speed on the ground
    62-80% Np
  21. Idle with PMU off during overspeed gov check
    N1 stable between 60 and 70%
  22. Approximate torque setting for overspeed gov check
    30%
  23. Np limit with PMU off during overspeed gov check
    100 + 2%
  24. Max amps limit for takeoff
    +50 amps
  25. Radius for inside gear w/NWS
    • 15.5 feet
    • 0.0 feet w/differential braking
  26. Radius for nose wheel w/NWS
    • 18.0 feet
    • 8.3 feet w/differential braking
  27. Radius for outside gear w/NWS
    • 19.6 feet
    • 8.6 feet w/differential braking
  28. Radius for wingtip w/NWS
    • 33.2 feet
    • 21.0 feet w/differential braking
  29. Minimum separation behind large A/C for wake turbulence avoidance
    2 minutes
  30. Setting to check engine instruments for T/O check
    25-30% torque
  31. Rotation attitude
    7-10 degrees NH
  32. Rotation speed with gusty winds
    Half gust factor (up to 10 knots)
  33. Best rate of climb (Vy)
    140 KIAS
  34. Increased visibility during climg
    160-180 KIAS
  35. Pitch and speed for obstacle clearance climb
    15 degrees NH and 140 KIAS
  36. Climb check altitude
    10,000 feet
  37. Increase in ITT w/defog on at any PCL setting
    40 C
  38. ITT limit as controlled by PMU
    820 C
  39. Required pressure differential above 18069 feet MSL
    3.6 +/- 0.2 psi
  40. Max fuel imbalance for pre-stall spinning and aerobatic checks
    50 lbs
  41. Power and descent rate desired for enroute descent
    200-250 KIAS and 4000 fpm
  42. Descent rate with speed brake extended and idle power
    8000-11000 fpm
  43. Airspeed to break up rudder icing
    170 KIAS
  44. Recommended holding speed
    120-150 KIAS
  45. Time to allow for correction of attitude errors
    1-2 min
  46. Pressurization DUMP before landing at fields above
    7500 MSL
  47. Gusty wind threshold and touchdown speeds
    Add half gust factor (up to 10 knots)
  48. Normal touchdown speed (depending on flap setting)
    75-105 KIAS
  49. Lower nosegear to runway below __ KIAS unless needed to affect stopping distance
    80 KIAS
  50. Brake with great caution above this speed
    80 KIAS
  51. Time for ITT to stabilize before shutdown
    1 min
  52. Max time to apply power to pitot/AOA heating elements on ground
    10 seconds
  53. Min volume of MIL 85470 ice inhibitor to be added to fuel
    0.5 pint/50 gal
  54. Max slope approved for fueling
    3 degrees
  55. Time limit for LH and RH single point refueling precheck valves to shut
    10 seconds
  56. Ground power required
    • 28-28.5 VDC
    • 1000 amps for 5 sec
    • 500 amps for 2 min
    • 300 amps continuous
    • 24.0-29.5 V for off-station
  57. Main gear tire pressure (norm)
    185 +/- 5 psi
  58. Main gear tire pressure (max)
    225+5 psi
  59. Nose gear pressure
    120+5 psi
  60. Wind speed to consider hangaring A/C
    80 knots
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Author
elitylski
ID
218686
Card Set
Dash 1 chapter 2.csv
Description
Dash 1 ch 2
Updated

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