-1 numbers chp 1

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Author:
C17FLYR
ID:
62471
Filename:
-1 numbers chp 1
Updated:
2011-02-09 19:47:54
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numbers chp
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-1 numbers chp 1
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  1. Empty weight
    4900lbs
  2. Max takeoff weight
    6500 lbs
  3. Max Shaft Horsepower
    1100
  4. oil capacity
    18.5
  5. red OIL PX annunciator with PCL at idle
    <15 psi
  6. amber OIL PX annunciator with PCL at idle
    15-40 psi
  7. amber & red OIL PX annunciator with PCL at idle
    15-40 psi(5 sec+)
  8. red OIL PX annunciator with PCL above idle
    <40 psi
  9. amber OIL PX annunciator with PCL above idle
    40-90psi(10 sec+)
  10. turbine output shaft speed
    30,000 RPM
  11. prop operating speed
    2000 RPM
  12. prop diameter (4 blade, const-speed, variable pitch, non-reversing, feathering)
    97 in.
  13. – torque available from sea level to approx. 12K to 16K ft
    100%
  14. torque @ prop shaft when 100% torque
    2900 ft/lbs
  15. thrust @ sea level, zero airspeed when 100% torque
    2750 lbs
  16. blade angle when prop in low pitch
    15°
  17. voltage supplied by PMA to PMU (PMU converts it to DC)
    32 VAC
  18. PMU switches to 28 VDC battery bus
    40-50% Np
  19. PMU managed minimum above 10K
    80% N1
  20. IOAT reads as 121°
    96-121°C (IOAT)
  21. PMU goes offline
    +121°C (IOAT)
  22. ignition and boost pump deactivated during auto start
    50% N1
  23. fuel pressure switch limit, turns on BP
    10 psi
  24. manual motor after aborted start/inverted flight limit
    20 seconds
  25. – normal wing tank capacity
    527 lbs
  26. – collector tank capacity
    47 lbs
  27. usable fuel (through single point refueling system)
    1100 lbs
  28. over wing refueled full fuel load (manually filled)
    1200 lbs
  29. imbalance where FUEL BAL annunciator illuminated & auto balance turns off
    30 lbs (for 2 minutes)
  30. auto fuel balance
    20 lbs (30 sec+)
  31. middle fuel probe
    445 (± 50) lbs
  32. inner fuel probe
    308 (± 50) lbs
  33. collector tank pressurized by transfer jet pumps
    1 to 1.5 psi
  34. pressure in supply line where FUEL PX annunciator illuminated
    <10psi
  35. L or R FUEL LO annunciator illuminated
    110 lbs
  36. starter/generator output
    28 VDC (300 amp)
  37. main (lead-acid) battery output
    24 VDC (42A/HR
  38. aux battery output (30 minutes of emergency power)
    24 VDC (5 A/HR)
  39. minimum generator voltage to charge the battery
    25VDC
  40. minimum battery voltage to connect external power
    22 VDC
  41. normal hydraulic pressure
    3000±120 psi
  42. hydraulic system total capacity (below 1Qt - HYDRO FL LO annunciator)
    5 Qt
  43. hydraulic reservoir capacity
    0.6 gal
  44. min hydraulic pressure to operate NW steering, gear&doors, flaps, speed brake
    1800 psi
  45. – hydro pressure display goes from white to amber
    <1800 psi
  46. – emergency accumulator pressure where EHYD PX LO annunciator illum.
    <2400±150
  47. – fuel pressure supplied by engine driven low pressure fuel pump
    40 psi
  48. – fuel pressure supplied by engine driven high pressure fuel pump
    700 psi
  49. – max hydraulic volume allowed past the hydraulic fuse
    45 cubic inches
  50. – hydraulic pressure relief valve opens
    3250 to 3500 psi
  51. – EHYD PX LO annunciator illuminates
    2400 (± 150) psi
  52. – hydro system fluid level where HYDR FL LO annunciator illuminates
    1 qt
  53. – normal gear extension/retraction time
    6 seconds
  54. gear warning horn sounds if A/S is below 120
    87% N1
  55. NWS range of castor
    160°
  56. flap deflection in TO
    23°
  57. – flap deflection in LDG
    50°
  58. speed brake deflection when deployed
    70°
  59. TAD active with no weight on wheels
    80 knots
  60. Below this Mach is blanked on A/S ind
    0.40 Mach
  61. stall
    18 units
  62. – on speed AOA
    10 to 11 AOA
  63. max endurance
    8.8 AOA
  64. – max range
    4.9 AOA
  65. Optimum approach speed decrease rate
    1 knot/100 lbs
  66. – Optimum max range AOA altitude
    25,000’ MSL
  67. Pre-stall stick shaker
    5 - 10 kts (15.5 units)
  68. windscreen designed for bird strike of
    4 lbs @ 270 KIAS
  69. – CFS handle lanyard length
    10 ft
  70. Ejection seat limits
    0’/0 KIAS to 35,000’/370 KIAS
  71. Automatic seat/pilot separation
    14,000’ to 16,000’ MSL
  72. ISS BOTH rear seat ejection delay
    0.37 seconds
  73. – emergency oxygen supply lasts
    10 min
  74. Bleed air inflow prevented with A/C clutch engaged
    <7500’ MSL
  75. automatically maintained until 18,069’ MSL (3.6 + 0.1 psid)
    8000’ cockpit P/A
  76. – CKPT ALT annunciator illuminated
    19,000’ cockpit P/A
  77. – CKPT PX annunciator illuminated
    3.9 + 0.1 psid
  78. – DUCT TEMP annunciator illuminated
    300° F
  79. – UHF/VHF memory
    20 frequencies
  80. – RMU cursor automatically reverts to UHF field
    20 seconds
  81. – NAV memory
    10 frequencies
  82. ELT transmission limit (battery limited)
    50 hours
  83. – EADI declutters
    > +30°/-20° pitch or 65° roll
  84. – Full EADI presentation reappears after unusual attitude
    < +25°/-15° pitch and 60° roll
  85. – NACWS display time limit after trigger is released
    7 seconds
  86. – NACWS landing mode
    1.5 NM range
  87. NACWS vertical separation alert (enroute mode)
    ± 2700’
  88. – NACWS vertical separation alert (landing mode)
    ± 500’
  89. NACWS rectangle with digits
    Less than or equal to ±300’
  90. NACWS upward/downward pointing triangle with digits
    Less than or equal to ± 400’ to 900’
  91. – NACWS upward/downward pointing triangle with no digits
    Less than or equal to ± 1000’ to 2700’
  92. – GPS self test indications
    34.5 NM, 315 DTK, 130° bearing
  93. – GPS user defined waypoints
    250
  94. GPS stored flightplans
    25
  95. max waypoints per flight plan
    30
  96. flash prior to turn to next waypoint
    20 seconds
  97. CDI full scale deflection, enroute mode
    ± 5 NM
  98. CDI full scale deflection, approach arm
    ± 1 NM
  99. CDI full scale deflection, approach active
    ± 0.3 NM
  100. – Approach arm
    30 NM
  101. Approach active
    2 NM
  102. FDR annunciator illuminates
    80% full
  103. AUX BAT test light will not illuminate
    <50% capacity
  104. OBOGS TEMP annunciator illuminates
    200° F
  105. NORMAL O2 concentration, sea level to 15,000’ MSL
    25% to 70%
  106. NORMAL O2 concentration, 15,000’ to 31,000’ MSL
    45% to 95%
  107. O2 concentration, MAX selected
    95%
  108. OBOGS warm-up time (after engine start)
    3 minutes
  109. OBOGS FAIL annunciator extinguishes during BIT test
    < or = 2 minutes
  110. – baggage compartment weight limit
    80 lbs
  111. icing inhibitor mix
    .5 pint/ 50 gal fuel
  112. external power requirements
    28 to 28.5 VDC/1000 to 1500 Amps
  113. main gear tire pressure
    225 ± 5 psi
  114. nose wheel tire pressure
    120 ± 5 psi

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