CRJ2014

Card Set Information

Author:
SteveCRJ
ID:
280349
Filename:
CRJ2014
Updated:
2015-08-04 23:06:41
Tags:
CRJ
Folders:

Description:
CRJ limitations
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  1. Hot start
    Interrupted Start
    N2 Stagnation 200
    • Affected thrust lever..... shut off
    • Ignition...............................off
    • Dry motor................... until ITT reduced below 120 respecting start time limit
  2. No light off CRJ200
    • Affected thrust lever........ shutoff
    • Ignition............................. off
    • Dry motor... until start time limit
  3. Start abort message hot start 700, 900
    • Affected thrust lever.... shut off
    • Dry motor.................. until ITT reduced below 120 respecting starter time limit
    • Affected engine stop
  4. Configuration warnings
    Take off... discontinue immediately
  5. Rejected takeoff
    • Simultaneously thrust lever....idle
    • wheel brakes....... maximum
    • .......................... til safe stop
    • Thrust reversers
    • operating engine....... maximum
    • ........................ consistent with
    • .................... directional control
  6. Excessive asymmetry or loss of braking
    • Wheel brakes........... release
    • ...............................momentarily
    • Anti-skid................... off
    • Wheel brakes........... reapply as
    • ................................... required
  7. Stab trim runaway CRJ200
    • Control column ............. Assume manual control and override runaway
    • Both stab trim disc......... press and hold and release
    • Airplane control.......... transfer to pilot left hand side
    • Stab CH1 and Stab CH2 hstcu cbs 2F5 and 4A1.................... open
  8. Stab trim runaway CRJ700, 900
    • Control wheel...............Assume manual control and override runaway
    • Stab trim disc................. select
  9. High altitude stall recovery (PF)
    • Auto-pilot disengage if required
    • Pitch attitude
    • Lower nose to reduce angle of attack
    • Thrust levers advance to max power and call max thrust
    • Roll attitude wings level
    • Flight spoiler lever select to retract
    • Pitch attitude maintain nose down pitch until airplane is effectively out of stall condition   -5 to -10 degrees
    • Pitch attitude smoothly pitch to normal flight thrust lever set to appropriate setting within limits
  10. High altitude stall recovery (PM)
    • Auto pilot disengagement confirmed
    • ATC declare an emergency
    • Notify of immediate need for lower altitude
    • Thrust lever set max thrust on command
    • Pitch attitude and airspeed monitor
    • Call out any limitation exceedances
    • Call out aircraft state
    • Call out terrain
  11. Max aft cargo
    • 3500
    • 3740
    • Wifi
    • 3650
  12. Max forward cargo
    • ----
    • 1000
    • 1700 total 850/850
  13. Flight time to suitable airport
    • 45 minutes
    • 60 minutes
    • 60 minutes
  14. Minimum runway width
    100'
  15. Max ops altitude
    • 37000
    • 39000
    • 39000
  16. Max takeoff and landing
    • 10000
    • 9600
    • 9600
  17. Max temperature takeoff and land
    ISA +35C
  18. Min temperature takeoff
    -40C
  19. VMO
    335k
  20. MMO
    • .85 M
    • .85 M .83 RVSM
    • .84 M .82 RVSM
  21. Flaps 1
    230 kt
  22. VFO 8
    • 200 kt
    • 230 kt
    • 230 kt
  23. VFO 20
    • 200 kt
    • 230 kt
    • 230 kt
  24. VFE 8
    • 215 kt
    • 230 kt
    • 230 kt
  25. VFE 20
    • 215 kts
    • 230 kts
    • 220 kts
  26. VFE 30
    185 kts
  27. VFE 45
    170 kts
  28. VLO EXT
    220 kts
  29. VLO RET
    200 kt
  30. VLE
    220 kts
  31. VTIRE
    • 182 k gs
    • 182 k gs
    • 195 k gs
  32. VADG deploy max
    • 250 kts wet
    • VMO/MMO
    • VMO/MMO
  33. VB
    280 kts
  34. MB
    .75 M
  35. VWIPER Ops max
    • 220 kts
    • 250 kts
    • 250 kts
  36. Brakes normal PSI
    • 1000-3200 PSI green
    • 1800-3200 PSI green
    • 1800-3200 PSI green
  37. Anti-skid
    >35 kts or WOW +5 seconds
  38. Minimum spoiler speed
    • approach speed +20
    • approach speed +10
    • approach speed +10
  39. Engine
    • CF 34-3A1/3B1
    • CF 34-8C1/8C5B1
    • CF 34-8C5
  40. Max continuous thrust ITT
    • 3A1-860C
    • 3B1-874C
    • 927C
    • 960C
  41. Max start ITT
    • 900C
    • 815C
    • 815C
  42. N1 idle
    • ----
    • 20-25%
  43. N1 max continuous
    • 89.6%
    • 99.5%
    • 99.5%
  44. N1 normal takeoff
    • 96.2%
    • 97.9%
    • 99.5%
  45. N1 minimum reduced thrust
    • 3A1-85%
    • 3B1-83.5%
  46. N2 idle
    • 56.5-68%
    • 55-65%
    • 55-65%
  47. N2 max continuous
    • 99.2%
    • 97.9%
    • 98%
  48. N2 normal takeoff
    • 98.3%
    • 98.3%
    • 99.4%
  49. engine start ground 200
    • 60 seconds on 10 seconds off
    • 60 seconds on 10 seconds off
    • 60 seconds on 5 minutes off
    • 60 seconds on 5 minutes off
  50. engine start ground 700/900
    • 90 seconds on 10 seconds off
    • 90 seconds on 10 seconds off
    • 90 seconds on 5 minutes off
    • 90 seconds on 5 minutes off
    • 90 seconds on 5 minutes off
  51. dry motoring ground 200
    • 90 seconds on 5 minutes off
    • 30 seconds on 5 minutes off
  52. dry motoring ground 700/900
    • 90 seconds on 5 minutes off
    • 30 seconds on 5 minutes off
    • 30 seconds on 5 minutes off
    • 30 seconds on 5 minutes off
    • 30 seconds on 5 minutes off
    • 30 seconds on 5 minutes off
  53. useable fuel pressure refueling
    • Main 4760
    • Main 7492
    • Main 7492
  54. fuel total pressure refueling
    • 14518
    • 19594
    • 19594
  55. total fuel gravity refueling
    • 13960
    • 14580
    • 14810
  56. fuel maximum imbalance
    800
  57. max imbalance for takeoff
    • 800
    • 300
    • 300
  58. fuel minimum GA per wing
    • 450
    • 600
    • 600
  59. fuel min temperature takeoff
    +5 C
  60. main generator
    • 35000' 30 KVA >35000' 25 KVA
    • 40 KVA
    • 40 KVA 
  61. APU generator
    • 30 KVA
    • 40 KVA
    • 40 KVA
  62. max continuous DC TRU
    • 100 amp
    • 120 amp
    • 120 amp
  63. APU min temperature start
    -40C
  64. APU max operating alt
    • 37000
    • 41000
    • 41000
  65. APU max start alt
    • 30000
    • 37000
    • 37000
  66. APU max alt bleed use
    • 15000
    • 25000
    • 25000
  67. APU max alt engine start
    • 13000
    • 21000
    • 21000
  68. APU max door open with APU not running
    • 300 kts
    • 220 kts
    • 220 kts
  69. APU start aircraft battery
    • 2 x 30 sec on  20 min off
    • 2 x 30 sec on  40 min off
  70. max pressure diff
    8.7 psi
  71. max pressure negative diff
    -.5psi
  72. single pack ops
    • 25000
    • 31000
    • 25000
  73. pack overheat
    88C
  74. pack overpressure
    >50 psi
  75. cabin alt caution
    8500-10000
  76. cabin alt warning
    10000
  77. CPAM packs O2
    • 14000 +/- 500'
    • 14000'
    • 14000'
  78. emergency depr
    • 14250 +/- 750
    • 14500 +/- 500
    • 14500 +/- 500
  79. 200 dimensions
    • length 87' 10"
    • width  69' 8"
    • height 20' 8"
  80. 700 dimensions
    • length 106' 8"
    • width    76' 3"
    • height   24' 10"
  81. 900 dimensions
    • length 119' 4"
    • width    76' 3"
    • height   24' 7"
  82. minimum fuel
    • 1500 lbs
    • 2100 lbs
    • 2150 lbs

    • provides 1 GA and 1 approach from 10 mile final
    • and 30 minutes of fuel at 1500 AFE 225 kts
  83. emergency fuel
    • 1050 lbs
    • 1500 lbs
    • 1550 lbs

    • provides 30 minutes of fuel 1500' AFE at 225 kts
    • or fuel for 1 GA and 1 approach from 10 mile final
  84. minimum O2 for dispatch
    • 200 1410 psi
    • 7/9   960 psi

    International 1650 psi
  85. deice communication elements
    • A type
    • B percentage
    • C time
    • D
    • E check
  86. continuous ignition
    • contaminated
    • cross wind 10 kts 200
    • rain
    • turbulence
    • thunderstorms
  87. reduced thrust takeoff
    • anti-ice
    • contaminated
    • tailwind 5 kts
    • windshear
    • anti-skid inop
    • takeoff behind heavy
    • flaps 8
  88. battery
    • main 24 volts 17 amps
    • APU  24 volts 43 amps
  89. air driven generator wet
    • 200 kts
    • 330 kts 12 minutes
    • 335 kts   4 minutes
  90. hold speed
    • <6000       200 kts
    • 6-14,000   230 kts
    • >14,000    265 kts
  91. turn radius
    • 200  75'
    • 700  75'
    • 900  80'
  92. 200 weights
    • 53250
    • 53000
    • 47000
    • 44000
  93. 700 weights
    • 75250
    • 75000
    • 67000
    • 62300
  94. 900 weights
    • 85000
    • 84500
    • 70750
    • 70100
  95. thrust increase apr
    • 500
    • 1100
    • 700

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