Q300 Limitations

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Author:
tojones89
ID:
265576
Filename:
Q300 Limitations
Updated:
2014-03-08 17:54:22
Tags:
limits Q300
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Q300 Limitations
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  1. MAUW
    19505
  2. MLW
    19051
  3. MZFW
    17917
  4. Max total baggage compartment weight
    1134
  5. Centre of gravity limits
    21.5% to 40% at MAUW and 15% down to 13608kg
  6. Flap g limits
    • Flaps retracted: 2.5 & -1.0
    • Flaps extended: 2.0 and 0.0
  7. Max fuel imbalance
    272kg
  8. Max operating attitude
    25000'
  9. Max operating altitude for takeoff and landing
    10000
  10. Max altitude for extending landing gear or wing flap
    15000'
  11. Max tailwind component
    20kts - Air Nelson limit
  12. Max crosswind
    36kts
  13. VMO
    • 243 up to 17000'
    • Thence a linear decrease to¬†
    • 214 at 25000'
  14. VA
    177
  15. VLO
    163
  16. VLE
    173
  17. VRA (rough air)
    190
  18. Alternate gear extension speed
    140
  19. Max tire speed (ground speed)
    165
  20. MTOP
    • 105.6 for up to 5 mins
    • 800 - ITT
    • 102.7 - Nh
    • 1212 - Np
    • 55 to 65 - Oil press
    • 45 to 115 - Oil temp
  21. NTOP
    • 92 - torque (on ground)
    • 765 - ITT (may be exceeded by 5 for 5 mins)
    • 101 - Nh
    • 1212 - Np
  22. Max continuous
    • 90 (96 below 1125 Np)
    • 800 - ITT
    • 102.7 - Nh
    • 1212 - Np
  23. Starting limits
    • 900 to 950 - 5 seconds
    • 840 to 900 - 12 seconds
    • 800 to 840 - 20 seconds
  24. Transient limits
    • 115 - Tq
    • 840 - ITT
    • 103.7 - Nh
    • 1320 - Np
    • 125 - Oil temp
  25. Max reverse
    Same as NTOP
  26. Minimum Nh during flight
    66%
  27. Prohibited range for Np
    500 to 780
  28. DC Gen load limits
    Ground/Air
    0.7/1.0
  29. TRU Limits
    Ground/Air
    1.0/1.0
  30. AC Generators limits
    Ground/Flight
    • Below +10 OAT = 1.0
    • +10 OAT and above = 0.33
    • In flight = 1.0
  31. Presurisation limits:
    normal cabin diff
    max cabin diff
    max differential limit for T/O and LDG
    max cabin alt
    • 5.5 +/- 0.3
    • 5.95
    • 0.5
    • 8000'
  32. What is considered icing conditions
    SAT on ground is 10 or below, or SAT in flight is 5 or below, and visible moisture in any form is present.

    On the ground, any signs of standing water, slush or snow below 10 is considered icing conditions
  33. Minimum height for autopilot engagement
    1000'
  34. Engine start tailwind limits
    GPU assisted
    APU or cross gen start
    Battery start
    • 35kts
    • 20kts
    • No tailwind allowed

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