Dash 1 chapter 1.csv

Card Set Information

Author:
elitylski
ID:
218201
Filename:
Dash 1 chapter 1.csv
Updated:
2013-05-08 17:00:51
Tags:
T6
Folders:

Description:
T6 dash 1 chapter 1
Show Answers:

Home > Flashcards > Print Preview

The flashcards below were created by user elitylski on FreezingBlue Flashcards. What would you like to do?


  1. Engine Model
    Pratt & Whitney PT6A-68 free-turbine turboprop
  2. Propeller model
    Hartzell 97-inch, four-blade, constant-speed, variable-pitch, non-reversing, feathering propeller
  3. Basic empty weight
    4900 lbs
  4. Max gross takeoff weight
    6500 lbs
  5. Shaft horsepower
    1100 SHP
  6. Gas generator layout
    • four-stage axial-flow
    • compressor
    • single-stage centrifugal flow compressor
    • combustion chamber
    • single-stage compressor turbine
  7. Engine power section layout
    • Two-stage axial-flow power turbine
    • exhaust case
    • reduction gearbox
  8. Oil capacity
    18.5 quarts
  9. Power turbine output shaft speed
    30,000 RPM
  10. Propeller operating speed
    2,000 RPM
  11. 100% Torque (ft-lbs and lbs thrust)
    • 2900 foot-pounds
    • 2750 lbs thrust (sea level, zero airspeed)
  12. Max torque available at which altitudes
    Sea level to 12,000-16,000 MSL
  13. Two methods for propeller feather
    • 1. PCL off with PMU NORM - prop servo valve drains prop oil px
    • 2. PCL off activates feather dump solenoid, powered by PROP SYS circuit breaker
  14. PMU power supply
    • Permanent Magnet Alternator on RGB - 32 V
    • Or 28V from battery bus if Np below 40-50% or PMA fail
  15. N1 idle with PMU in Ground mode
    60-61%
  16. N1 idle with PMU in Flight Mode
    67% at idle
  17. N1 idle above 10,000 feet PA
    Raised to maintain Np above 80%
  18. PMU auto-abort for hot start
    • ITT > 940C for 2 sec
    • ITT > 870C for 4 sec
    • ITT > 840C for 19 sec
  19. PMU auto-abort for hung start
    N1 acceleration to idle is less than 50% of normal or light-off doesn't occur within 10 sec
  20. PMU defaults to high IOAT
    From 96 C to 121 C, PMU defaults to 121C
  21. Engine start: starters and igniters deenergized
    50% N1
  22. Engine start: boost pump deactivated
    50% N1 and fuel px > 10 PSI
  23. Engine start: PCL advance to idle
    above 60% N1
  24. Two ways to manually abort start
    PCL - off, starter switch - auto/reset
  25. PMU Manual mode annunciators
    Red PMU FAIL and Amber PMU STATUS
  26. Normal wing fuel tank capacity
    527 lb
  27. Collector fuel tank capacity
    47 lb
  28. Total normal fuel capacity
    1100 lb
  29. Gravity refuel full load
    1200 lb
  30. Auto fuel balance trigger
    20 lb imbalance >30 sec
  31. Outer fuel probe limit
    445 +/- 50 lbs
  32. Middle fuel probe limit
    308 +/- 50 lbs
  33. Inner fuel probe limit
    20 lbs
  34. Inverted flight fuel pickup
    15 sec of fuel
  35. Fuel px supplied by engine driven low px fuel pump
    40 psi
  36. Fuel px supplied by engine driven high px fuel pump
    700 psi
  37. Generator/starter
    • 28 VDC
    • 300 amp
  38. Battery
    • 24 VDC
    • 24 amp-hr
  39. Aux battery
    • 24 VDC
    • 5 amp-hr
    • 30 min supply
  40. Min battery voltage for external power
    22.0 V
  41. Hydraulic system capacity
    5 qt
  42. Hydraulic system pressure
    3000 +/- 120 psi
  43. Hydraulic system pressure relief valve
    3250 to 3500 psi
  44. Min hydraulic px for ldg gr, main gr doors, flaps, speed brake, and NWS
    1800 PSI
  45. Max hydraulic fluid past hydraulic fuse
    20-30 cubic inches (0.5 qt)
  46. Time for gear extension/retraction
    6 seconds
  47. Landing gear warning conditions
    • Gear not DOWN with PCL below mid-range (87% N1)
    • Airspeed below 120 KIAS with flaps UP or T/O
    • Gear not DOWN with Flaps LDG
    • Weight on wheels with gear not down
  48. Nose wheel castor
    160 degrees (80 degrees each side from center)
  49. TO Flap deflection angle
    23 degrees
  50. LDG Flap deflection angle
    50 degrees
  51. Speed brake deflection angle
    70 degrees
  52. 3 ways to retract speed brake
    • Move speed brake switch
    • extend flaps
    • move PCL to MAX
  53. Aileron deflection angle
    • 20 degrees up
    • 11 degrees nose down
  54. Aileron trim angle
    6 degrees up/down
  55. Aileron trim tab angle
    • 20 degrees tab up
    • 8 degrees tab down
  56. Elevator deflection angle
    • 18 degrees up
    • 16 degrees down
  57. Elevator trim angle
    • 5.5 degrees up
    • 22 degrees down
  58. Rudder deflection angle
    24 degrees left/right
  59. Rudder trim angle
    9 degrees left/right
  60. TAD active with no weight on wheels
    80 KIAS
  61. Primary pitot static system
    • Right wing pitot probe
    • Upper right and lower left static ports
  62. Standby pitot static system
    • Left wing pitot probe
    • Lower right and upper left static ports
  63. Mach information below ___ blanked
    0.40 Mach
  64. Standby attitude indicator accurate to 6 deg for ___ minutes with no electrical power
    9 min
  65. ___ or higher difference between accelerometers indicates fault
    1G
  66. AOA for stall
    18 units
  67. AOA activates stick shaker
    15-16 units
  68. AOA green arc (normal approach)
    10-11 units (1.3x stall speed)
  69. AOA white diamond (max endurance)
    8.8 units
  70. AOA White triangle (max range)
    4.9 units
  71. Optimum approach speed weight correction
    -1 knot/100 lbs fuel used
  72. Canopy strike limits
    4-pound birdstrike at 270 knots
  73. External CFS handle length (safe range)
    10 feet
  74. Ejection seat parameters
    0/0 to 35,000 at 370 KIAS
  75. Ejection seat auto seat-man separation altitude
    14,000-16,000 MSL
  76. Emergency oxygen supply time
    10 minutes
  77. Emergency oxygen tank black range
    1800-2500 psi
  78. Emergency oxygen tank temperature correction
    3.5 psi for each degree above or below 70F
  79. ISS BOTH front ejection seat delay
    0.37 sec
  80. SSK lowers __ seconds after man-seat separation
    4-6 sec
  81. Left side P3 port bleed air supplies __ system(s)
    OBOGS
  82. Right side P3 port bleed air supplies __ system(s)
    • canopy seal
    • anti-G
    • heat/defog
    • pressurization
  83. Below ___ bleed air inflow prevented with A/C clutch engaged
    7500 MSL
  84. Cockpit altitude maintained until 18,069 MSL
    8,000' PA
  85. Anti-G and canopy seal safety valve relieves pressure above __ psi
    7 psi
  86. Cockpit temp automatically controlled between __
    60F and 90F
  87. Temp in excess of __ directs heat exchanger bypass full closed
    165F
  88. Evap Blower HI setting output
    350 cu-ft/min
  89. UHF comm frequency range
    • 225.00 to 399.975 MHz in 25 kHz increments
    • (7,000 channels)
  90. UHF GUARD Frequency
    243.00 MHz
  91. VHF comm frequency range
    • 118.00 to 151.975 MHz in 25 kHz increments
    • (1,358 channels)
  92. VHF emergency frequency
    121.5 MHz
  93. RMU cursor defaults to UHF
    20 seconds
  94. UHF/VHF comm frequency storage
    20 presets
  95. VHF NAV frequency storage
    10 presets
  96. VHF NAV frequency range
    • 108.00 to 117.95 MHz
    • (200 VOR/LOC channels)
    • 329.15 to 335.00 MHz
    • (40 GS channels)
  97. VHF NAV Marker beacon frequency
    75.00 MHZ
  98. Backup UHF unit frequency storage
    20 presets
  99. ELT broadcast frequencies
    121.5 MHz and 406 MHz
  100. ELT battery life
    50 hours
  101. EHSI ARC mode width
    85 degrees
  102. EADI declutters
    • More than 30 nose up or 20 nose down
    • More than 65 bank
  103. EADI returns to normal after unusual attitude
    • Less than 25 nose up or 15 nose down
    • Less than 60 bank
  104. TAS Normal mode
    2700' above to 2700' below
  105. TAS Above mode
    8700' above to 2700' below
  106. TAS Below mode
    2700' above to 8700' below
  107. TAS Range
    40 NM radius
  108. TAS Sensitivity A (gear down)
    • Vertical separation <600' in 20 sec
    • Vertical separation <600' and horizontal separation <0.2 NM
    • Horizontal separation from non-altitude reporting A/C within 15 sec or 0.2 NM
  109. TAS Sensitivity B (gear up)
    • Vertical separation <800' in 30 sec
    • Vertical separation <800' and horizontal separation <0.55 NM
    • Horizontal separation from non-altitude reporting A/C within 20 sec or 0.55 NM
  110. TAS open white diamond
    Non-threat traffic: relative altitude greater than +/- 1200' or distance beyond 5 NM
  111. TAS filled white diamond
    Proximity traffic: within 1200' relative altitude and within 5 NM range but not a threat
  112. TAS filled yellow circle
    Traffic advisory/potential hazard: Time to closest point of approach is 15-30 sec
  113. GPS Receiver
    TSO C-129 Class A1
  114. GPS self test indications
    • 34.5 NM
    • 315 DTK
    • 130 bearing
  115. GPS user waypoints
    250
  116. GPS flight plans
    25
  117. GPS max waypoints per flight plan
    30
  118. GPS flash prior to turn to next WPT
    20 seconds
  119. GPS approach arm mode range
    30 NM from APT
  120. GPS approach arm CDI scale
    1 NM
  121. GPS enroute mode CDI Scale
    5 NM
  122. GPS approach active mode range
    2 NM from FAF
  123. GPS approach active CDI scale
    0.3 NM
  124. AUX BAT light fails to illuminate
    Less than 50% capacity
  125. Landing Gear Position warning
    • 250 Hz tone
    • 5 times per second
  126. Overspeed Warning
    • 1600 Hz tone
    • 5 times per second
  127. Master Warn, Master Caution, Fire tone
    Decaying tone
  128. OBOGS Oxygen NORMAL concentration: SL to 15,000 MSL
    25-70%
  129. OBOGS Oxygen NORMAL concentration: 15,000 - 31,000 MSL
    45-95%
  130. OBOGS Oxygen concentration in MAX
    95%
  131. OBOGS warm-up time after engine start
    3 minutes
  132. Baggage compartment max weight
    80 lbs
  133. Icing inhibitor mix
    • 0.5 pint per 50 gal fuel
    • (0.13% by volume)
  134. Service oil level within __ minutes of engine shutdown
    30 min
  135. For accurate oil level, check __ to __ minutes after shutdown
    15-20
  136. External ground power requirements
    • 28-28.5 VDC
    • 1,000 amp for 5 sec
    • 500 amp for 2 min
    • 300 amp continuous
    • 24.0 to 29.5 VDC for off station starts
  137. Brake fluid capacity
    0.5 pint
  138. Air conditioning refrigerant capacity
    3.1 lbs
  139. Main gear tire pressure
    225 +/- 5 psi
  140. Nose wheel tire pressure
    120 +/- 5 psi

What would you like to do?

Home > Flashcards > Print Preview