embLimitation

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Author:
Anonymous
ID:
6635
Filename:
embLimitation
Updated:
2010-02-10 23:13:58
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emb145 limitations
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Limitations
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  1. Minimum flight crew:
    2 Pilots
  2. TheEMB-145 is certified in the transport category in the following conditions:
    Day, Night, VFR, IFR, Icing conditions
  3. Max runway slope:
    ± 2% of runway length.
  4. Runway surface:
    paved
  5. Max temperature for aircraft:
    ISA+35°C
  6. Min/Max takeoff & landing pressure altitude:
    -1000',8000'(ER/LR) 10,000' (XR)
  7. Min/Max SAT at FL370:
    -65/-21.5°C
  8. Min/Max SAT for takeoff:
    -40/52°C
  9. Min TAT above FL250:
    -45°C
  10. Min SAT below FL250:
    -54°C
  11. Mx inspection needed when landing below:
    -40°C
  12. VLO for gear retraction/extension:
    200/250 KIAS
  13. VLE:
    250 KIAS
  14. VA:
    200 KIAS
  15. Max flap ext. speed for flaps 9:
    250 KIAS
  16. Max flap ext. speed for flaps 18:
    200 KIAS
  17. Max flap ext. speed for flaps 22:
    200 KIAS
  18. Max flap ext. speed for flaps 45:
    145 KIAS
  19. Max flap ext. speed for flaps 45 (XR):
    160 KIAS
  20. Above 10,000' with YD disengaged, max speed for flaps 22(XR):
    180 KIAS
  21. Above 10,000' with YD disengaged, max speed for flaps 45(XR):
    145 KIAS
  22. For non-XR, when flaps are extended to/retracted from 45,momentary airspeed deviations between 145 and _______will not require a Mx inspection.
    160 KIAS
  23. For non-XR, when flaps are extended to/retracted from 22,momentary airspeed deviations between 200 and _________ will not require a Mx inspection.
    210 KIAS
  24. Max airspeed after T/O without retrimming:
    160 KIAS
  25. Max airspeed for turbulent air penetration below 10,000': _____ and above 10,000': _________.
    200KIAS, 250 KIAS or .63M whichever is lower
  26. Min/Max fuel tank temperature is:
    -40/52°C
  27. Max N1:
    100%
  28. For all models, min/max oil pressure < 88% N2:
    34/110 psi
  29. On ER/LR, min/max oil pressure >= 88% N2:
    50/110 psi
  30. On XR, min/max oil pressure >= 88% N2:
    48/110 psi
  31. On XR, operation between 34 and 48 psi is permitted for:
    T/O and go-around phases
  32. Max oil pressure may be exceeded during start if the oil tempis below: ____ . The engine must remain at IDLE until oilpresure is less than: _____
    21°C, 110 psi
  33. All aircraft will display oil pressure <= ____ psi in green.
    110
  34. All aircraft will display oil pressure in range ____ in amber and permitted in all operation modes. Limited to ____. Operation in the oil pressure amber range between ____ in amber and permitted in all operationmodes Limited to ____. However, total over-pressuretime may not exceed ____
    111 and 115 psi, 5 minutes, 116 and 155 psi, 2 minutes, 5 minutes
  35. Min oil temp for start:
    -40°C
  36. To increase N2 above ____ , the engine oil temp must be ____. Or, run the engine for at least ____ OR complete a staticrunup to ____ , allow the engines to stabilize and ensurethat the oil pressure is ____
    83%, 40°C, 8 minutes, 88% N2, <= 83 psi
  37. LP and HP spool vibration limits maybe exceeded up to ____for ____ during takeoffs and go-arounds. Else ____
    2.5 IPS, 5 minutes, 10seconds
  38. Max ITT for start on all engines:
    800°C
  39. All ER/LR takeoff thrust ratings/ITT limits (948°) are timelimited to ____
    5 minutes
  40. All XR, takeoff thrust ratings/ITT between ____ are timelimited to ____. Takeoff thrust ratings/ITT up to ____are permitted up to max of ____
    971°-992°, 90 seconds, 970°, 5 minutes
  41. Any engine exceedance or peak must be monitored and loggedby the crew.
    Any engine exceedance or peak must be monitored and loggedby the crew.
  42. Dry motoring continuous operation:
    5 minutes ON & 5minutes OFF
  43. Engine starting cycle, 1-4: ____. For 5th cycle: ____.
    1 minute ON & 1 minute OFF, 1 minute ON & 5 minutes OFF
  44. After start, the engines must run at idle or taxi thrust for ____ for cold engines. or ____ for warm engines.
    4 minutes, 2 minutes
  45. Engine is considered cold, if it's been shut down for at least:
    90minutes
  46. Engines must run for at least ____ at idle or taxi thrustbefore shutdown.
    2 minutes
  47. Max altitude for starting APU:
    FL300
  48. Max operational altitude for APU:
    FL370
  49. The APU will automatically shutdown at ____ rotor speed.
    104%
  50. EGT may exceed ____ for maximum of ____
    680 up to 717°C, 5 minutes
  51. Min battery temp for APU start:
    -20°C
  52. Start cycle for the APU: After 1-2 attempts: ____ .After 3rd attempt: ____
    1 minute off, 30 minutes off
  53. Max APU generator load above FL300:
    300A
  54. Min AP engagement height:
    500 AGL
  55. AP disengagement height is: ____ for visual approaches, ____ for CAT I, ____ for CAT II and ____ for non-precision.
    200', 200', 85', before leaving MDA
  56. Max ISIS duration when operating only on batteries is ____ . Maybe exceeded to ____ if pitot #3 is turned OFF in non-icing conditions.
    40 minutes, 45 minutes
  57. The airplane must not be moved during power-up initialization. Do not cage attitude in turning flight.
    The airplane must not be moved during power-up initialization. Do not cage attitude in turning flight.
  58. Max altitude for flap extension:
    FL200
  59. Max differential pressure:
    7.8 psi
  60. Max differential over-pressure:
    8.1 psi
  61. Max differential negative-pressure:
    -0.3 psi
  62. Min temp for manual anti-ice operation: ____ SAT on groundand TAT in-flight.
    -40°C
  63. Max temp for anti-ice operation:
    10°C
  64. Holding configuration in icing:
    Landing-gear UP, flaps 0 and min airspeed of 200 KIAS
  65. Max windshield wiper operating speed:
    170 KIAS
  66. Do not operate windshield wiper:
    on a dry windshield
  67. Max imbalance allowed between tanks:
    800 lb

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