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PC12

  1. APP speed with boot failure
    Flaps 00 speed 134 kts.
  2. Va at the following weights:
    9921
    9480
    9039
    6610
    • 9921 = 158 kts.
    • 9480 = 155 kts.
    • 9039 = 151 kts.
    • 6610 = 129 kts.
  3. Power settings
    • speed - torque - gear - flap
    • Terminal area   120    32psi      Up      00
    • App vector        150    24psi      Up     150
    • Non-Pre / FAF   120    24psi      Dwn   150
    • Non-Pre-In FAF 120     5 psi      Dwn   150
    • Circle/MDA       120    24psi      Dwn    150
    • Prec app          120     12psi      Dwn   150
  4. Vref
    • 0 flaps = 118 kts
    • 15 flaps = 98 kts
    • 30 flaps = 89 kts
    • 40 flaps = 84 kts
  5. Vfe
    • 15 flaps = 163 kts
    • > 15 flaps = 130kts
  6. Vref for Holding in Icicng no flaps
    • Holding in Icing
    • 00 flaps = 140 - 170 kts
  7. Max emergency gear extension speed
    110 kts
  8. Vy @ Sl
    Vy @ 20,000
    • Vy @ SL = 120 kts
    • Vy @ 15k = 115 kts
    • Vy @ 20k = 110 kts
  9. App speed
    Flaps 15
    Pusher Ice Mode
    108 kts
  10. Vx
    Vx = 110 kts
  11. EIS caution for Ng
    Ng <= 60%
  12. Temp that EIS caution will blink w probes de-ice off?
    <+40 c
  13. EIS warning for Ng
    Ng > 104%
  14. EIS warning for Np
    Np > 1870 with Ng > 90%
  15. EIS warning for oil temp
    Oil temp > 1100 C
  16. Gen 2 amp rating
    • Belt driven
    • Max 130 amps continuous
  17. Gen 1 max amp rating
    • Max amp is 300
    • 450 for 2/min hour
  18. Type of Battery
    24 vdc NiCad 40 amp

    • 20 min upto 60 amp
    • 30 min below 50 amp
  19. Type of wing
    1. wet wing

    2. 2 spars

    3. 1 fuel tank
  20. Cabin pressurization failure
    1. Pressure indicator - Check

    If cabin altitude> 10,700'

    • 2. O2 mask all occupants - ON
    • 3. Pax O2 - AUTO/ON
    • 4. Pax - DON Msk
  21. PCL Controls What?
    PCL movement control FCU directly
  22. Demonstrated X-wind 400 Flaps
    With 400 Flaps X-wind is 15 kts.
  23. Demonstrated X-wind 150 Flaps
    X-wind w 150 flaps = 25 kts.
  24. Max torque in reverse
    Max torque in reverse is 34 psi
  25. Max reverse prop RPM
    Max reverse prop RPM = 1650
  26. OAT Limits
    • OAT limits =
    • -550 C to +500 C
  27. Max flap cycle with OAT <= 250 C
    Max flap cycles = 8
  28. Max Transient prop RPM
    Max transient prop RPM = 1870
  29. PC12 has what type of flaps
    single piece Fowler type flap on each wing
  30. How much will AOA be reduced when in "Pusher Ice Mode"?
    AOA reduced 8 degrees
  31. Control surface De-ice sequence
    • 1. Horizontal stablizer
    • 2. Wings bottom inboard
    • 3. Wings top inboard
    • 4. Wings bottom outboard
    • 5. Wings top outboard
  32. What comprises Stall Warn/Stick Pusher system?
    • External AOA sensor on each wing
    • 2 - Computers
    • 1 - Stick shaker
    • 1 - Stick pusher
  33. Max landing weight?
    Max landing weight = 9921
  34. When does "CAB PRESS" annunciator illuminate?
    Cabin pressure exceeds 10,500'

    Max cabin differential of 6.5 psi
  35. What is climb speed with
    00 flaps 'Pusher Ice Mode' on
    130 kts
  36. When is the PCL lever aft of Idle Detent Prohibited?
    1. Engine not running

    2. During flight

    3. MOR is being used
  37. Which BUS supplies Boots Power?
    GEN 2 BUS supplies power to timer and control valves
  38. What happens if Boot De-ice pressure falls below <10 psi or there is a sequence failure?
    CAWS - Green DE ICE BOOTS flash

    CAWS - Red DE ICE illuminates
  39. Control surface De-Ice system pressure is ?
    Nominal pressure is 14 psi

    Over pressure relief @ 18 psi
  40. ITT Starting limits
    • 8000 - 8700 C = 20 sec
    • 8700 - 9990 C = 12 sec
    • 10000 C = 2 sec
  41. What is the Auto Engine start sequence?
    60 sec OFF

    60 sec OFF

    30 min OFF
  42. What is Vr when departing into known icing with flaps 150?
    Known Icing Vr = 88 kts
  43. What is landing distance increase with flaps 150?
    Landing distance distance increase = 1.31
  44. What is landing distance increase with flaps 00?
    Landing distance increase = 1.83
  45. What is Max Zero fuel weight?
    Max Zero Fuel Wgt = 9039
  46. An amber HYDR CAWS light indicates?
    1. In flight - Pressure in hydraulic system < 1800psi

    2. On ground - Pwr Pack cycled at least 6X in 1 hour and needs servicing
  47. Hydraulic Power Pack will not have electrical power under what conditions?
    Loss of GEN 1 which isolates NON ESS BUS

    Power Pack over heat - Thermal Protection CB
  48. EIS Torque caution range is?
    EIS torque caution range = 44.4 - 61.0 psi
  49. What is EIS Torque Warning?
    >61 psi
  50. EIS Caution Range for ITT?
    EIS caution range = 8700 - 10000 C
  51. EIS Warning for ITT?
    EIS Warning = >10000 C.
  52. Procedure for NO COMBUSTION w/in 10 secs?
    • Condition lever - CutOff
    • Starter Switch - Reset
    • 30 Sec - Dry Motoring Run
  53. PUSHER ICE MODE CAWS light illuminates when?
    • PROP Heat - ON
    • INERT SEP - OPEN

    Shaker/Pusher automatically switches to Ice Mode
  54. GEN 1 OFF or GEN 2 OFF annunciator lights illuminate when?
    • 1. Over voltage
    • 2. Under voltage
    • 3. Overload
    • 4. Reverse Current
  55. White Arc limits
    54 - 130 kts.
  56. Green Arc limits?
    91 - 236 kts
  57. Vlo speed?
    • Vlo = 177 kts.
    • Do not extend or retract gear above this speed
  58. Minimum Battery Voltage for External Start?
    Minimum Battery Volatge for External Start = 28 VDC
  59. Minimum Battery Voltage for battery start?
    Minimum Battery Voltage for Battery start = 24 VDC
  60. When is A/P and yaw Damper OFF?
    A/P and Yaw Damper are off for TakeOff and Landing
  61. Not feathered stabilized prop operation is prohibited at
    350 - 950 RPM
  62. Turbine Oil Quantity?
    Turbine Oil Qty = 14.5 gts.
  63. Total Usable Fuel?
    Total Usable Fuel = 402 gal. approximately 2725 lbs.
  64. Icing limitations during flight?
    • Operational DeIce Boots
    • Flaps 150
    • 108 KIAS

    • Boot Failure
    • Flaps 00
    • 134 KIAS
  65. When will CAWS illuminate "PUSHER"?
    • Built in test fail
    • Push signal from 1 computer lasing <3 sec
    • No torque output during push
    • Either Disconnect switch pushed
    • A/C is below .5Gs for <3 sec
  66. Aircraft Dimensions are?
    • Lenght = 53' 3"
    • Width = 47' 3"
    • Height = 14' 0"
    • Landing gear width = 14" 3"
  67. AV BUS Warning light comes on when?
    AV BUS voltage is < 18 VDC
  68. How many Flap position sensors are there?
    5 flap position sensors

    • 4 on wings
    • 1 flap handle
  69. Ignition system components
    • Exciter
    • High Tension Cables
    • Two Spark igniters
    • Cockpit control switch
  70. EIS Caution light when?
    Battery Voltage =< 22 VDC
  71. ECS consists of what components?
    Air cycle system

    Distribution system

    Control system
  72. How many switches are used for landing gear indication and warning?
    6 Proximity switches

    2 Micro switches
  73. Windshield heating elements & controller are powered by?
    LH 28 VDC GEN 2 BUS

    RH 28 VDC NON-ESS BUS
  74. PROBE HEAT switch provides how much VDC to which items?
    28 VDC from GEN 2 BUS to

    • Pitot heads
    • Static ports
    • AOA probes
  75. Describe what happens with Boost Pumps in AUTO POSITION?
    Low pressure switch turns on pump if <2 psi and CAWS illuminates FUEL PRESS

    3.48 psi pumps and annunciators are off
  76. PROP DEICE power is supplied from which busses at what VDC?
    28VDC

    BATT BUS & GEN 1 BUS
  77. PAX O2 switch in auto permits flow of O2 when
    Cabin pressure exceeds 13,500'
  78. Cabin Pressuration Control System (CPCS) does what?
    • Regulates cabin pressure via outflow valves
    • Entirely pneumatic except:
    • Switching ground & flight modes
    • In flight depressurization
  79. VCCS may be operated
    • During ground operations
    • Up to an altitude of 25'000'
  80. ECS Emergency Shutoff Valve performs
    Isolates cabin during emergencies such as engine fire

    Opens ram air scoop on right side of fuselage letting fresh air into cabin
  81. Maximum Cabin pressure differential is
    Red line = 6.5 psi
  82. Cabin Differential dial markings are
    • Green arc = 5.75 psi 
    • Yellow arc = 5.75 - 6.5 psi
    • Red line = 6.5 psi
  83. Maximum fuel imbalance is
    26.4 gals or 178 lbs.
  84. Holding non-icing fuel flow increase?
    Fuel flow increase = 25-50%
  85. Maximum cabin weight?
    Max cabin weight = 3300 lbs.
  86. Maximum baggage weight?
    Max baggage wgt. = 400lbs.
  87. R/H air/ground signal is sent to which systems?
    • R/H stick pusher computer
    • Landing gear indication
    • Altitude & Heading reference system
    • (AHRS)
    • Transponder
  88. L/H air/ground signal is sent to which systems?
    • L/H stick pusher computer
    • Cabin pressure control system (CPCS)
    • CAWS
    • EIS
    • Hydraulic system control
  89. Main tire pressure
    Main tire pressure = 60 psi
  90. When is oil checked?
    Oil level is checked 10 minutes after shut down.
  91. How many fuel check points?
    • 2 - wing tanks
    • 1 - aft and left of nose wheel
    • 1 - fuel filter
  92. When should parking brake be left off?
    Do not use parking brake when A/C will be idle for long periods and at FBOs.
  93. When shutting down let ITT stabilize for?
    Stabilize ITT for 2 minutes.
  94. Take-off maximum DC Amps?
    Take-Off max amps =< 15 amps
  95. Maximum Mach?
    Max Mach = .48
  96. OAT 250 C to 500  C What is the maximum flap cycles?
    Max flap cycles = 6
  97. GPU must provide?
    27-30 VDC at 500 Amps for A/C power supply.

    1000 Amps for engine start
  98. Name 7 DC Power BUSes
    • BATT DIRECT BUS
    • BATT BUS
    • GEN 1 BUS
    • GEN 2 BUS
    • NON ESS BUS
    • AV BUS 1
    • AV BUS 2
  99. Items on BATT DIRECT BUS are?
    • Cargo door motor
    • Clock
    • Dome light @ 50%
    • Stand-by Power (if applicable)
  100. Fuel vent pressure?
    Fuel vent pressure is .2 - 2.0 psi
  101. When is the Oil/Fuel Heat Exchanger by passed?
    If fuel temp > 210 C exchanger is by passed.
  102. High pressure fuel pump provides what pressure at 13% Ng
    At 13% Ng high pressure pump provides 210 pph @ 75 psi
  103. High pressure fuel pump provides what pressure at 100% Ng
    At 100% Ng high pressure pump provides 1591 pph @ 800 psi.
  104. L/R FUEL LOW CAWS annunciator illuminates when?
    Tank is =< 20 gals or 135 lbs of fuel
  105. What comprises the hydraulic power pack?
    • Electric driven hydraulic pump
    • Reservoir
    • System pressure accumulator
    • Filter w by-pass valve
  106. If hydraulic pump motor fails, how long will system pressure accumulator keep gear in retracted position?
    =< 200 minutes
  107. Hydraulic power pack is connected to which BUS?
    NON ESS BUS
  108. When is altitude select capture prohibited?
    Altitude select prohibited below 1000'
  109. Propeller diameter?
    104 -105"
  110. Lowest temperature for Boot Operation?
    Lowest temp for boot operation is -400 C.
  111. Vmo is?
    Vmo is 236 KIAS
  112. TCV attempts to maintain a selected temperature between?
    180 C - 300 C
  113. CPCS maintains a cabin differential of
    5.75 psi = 10,000' equivalent max service ceiling of 30,000'
  114. O2 over pressurization green rupture disk ruptures at?
    Green disk ruptures at 2775 psi
  115. Systems on NON ESS BUS are?
    • Power control circuits for:
    • VCCS
    • Hydraulic system
    • Electrical Heating
    • R/H Landing Light
  116. When charging BATT with External Power source what are the switch configurations?
    • EXT PWR - ON
    • BATT - ON
  117. Nose wheel tire pressure?
    60 psi
  118. Use Flight Idle when temp is?
    Temp is =< +50 C use Flight Idle
  119. If you get a ESNTL BUS warning what are your actions?
    Continue flight
  120. What is the FCWU?
    Flap Control Warning Unit
  121. Major components of Ng governor?
    • Fly weights
    • Feedback spring
    • Pilot valve
  122. Major components of FCU
    • 3-D cam
    • Ng governor
    • Fuel valve - makes up fuel metering system
  123. Fuel Control Unit (FCU) is driven by?
    High pressure engine driven fuel pump via internal splined coupling shaft
  124. Useful load is?
    Useful load is 4454 lbs.
  125. Which aileron has electrically operated trim tab?
    Left aileron
  126. How can stick pusher be over-ridden?
    • By pressing 'PUSHER INTR' button to disengage stick pusher actuator
    • Manually overriding by pulling on yoke (appox. 60-65 lbs.)
  127. Maximum airspeed pointer at 30,000'?
    At 30,000 Max A/S pointer is aligned with 173 KIAS
  128. Vr @ SL, Std Day
    Vr = 79 KIAS
  129. Vso
    Vso - 64 KIAS
  130. Voltage regulators are set to maintain what output?
    28 VDC +/- .5 VDC
  131. Normal descent speed?

    High speed descent?
    Normal = 2000 fpm

    High speed = 3000 fpm
  132. Best glide @ 9039 lbs. Prop feathered
    Best glide = 114
  133. Hydraulic System requires what pressure?
    Hydraulic pressure = 2450 - 2800 psi.

    Pwr pack cycles w pressure < 2450 psi
  134. Engine starting system is comprised of?
    • Starter/Generator
    • Ignition system
    • Relays controlling electrical power thru system
  135. Ng at Ground Idle is?
    Ng @ GI = 50.7%
  136. Max O2 pressure
    Max O2 pressure is 1850 - 2000 psi
  137. Lamps test is used to test?
    • CAWS lights
    • Master Caution/Warning
    • Triple trim indicators
    • All LEDS on EPMP
    • Red A/S warning light
  138. EIS caution light is on when GEN 2 DC amps are?
    EIS caution lights when GEN @ DC amps > 140 Amps
  139. Max Propeller RPM?
    Max Prop RPM = 1700 RPM
  140. Inverter Warning indication?
    RMI flag
  141. Primary ACU provides indication of?
    • Torque
    • ITT
    • Ng
    • Fuel Qty data
  142. Inverters Convert VDC to ?
    28 VDC to

    • 26VAC &
    • 115VAC @ 400 Hz
  143. Inverters are on which BUS
    INV 1 - BATT BUS

    INV 2 - GEN 1 BUS
  144. Passenger door is secured by?
    6 locking pins or shoot bolts
  145. Cabin rate selector can be adjusted to
    100 fpm to 2000 fpm
  146. ECS is primary?
    ECS is primary system to condition air
  147. Fuel system
    • Vents are not connected
    • Balancing at 5% of current fuel
    • High side boost pump activated so it uses more fuel from that side
  148. Heating system consists of?
    • 2 - 28VDC heating units
    • 2000 C shutoff limit
  149. Components of shaker/pusher system are?
    • 2 AOA
    • 2 computers
    • 1 computer to shake
    • 2 computers to push
  150. At what speed does shaker activate?
    10 Kts above stall speed
  151. Ng Governor operation?
    • Ng governor controls engine speed thru axial positioning of 3-D cam, flyweights, feedback spring and pilot valve
    • Pilot valve regulates bleeding of Pt pressure from lower chamber of 3-D cam
    • P1/P2 differentials function of pilot valve vs flyweights & feedback spring position
  152. Pressure Relief Valve operation
    • Prevents engine fuel system over-pressure
    • Dumps un-metered fuel >1350 psi to by-pass line back to engine driven fuel pump
  153. EIS WARNING range digits blink at?
    80/minute
  154. EIS CAUTION range digits blink at?
    40/min
  155. Oil pressure system:

    1st valve pressure

    2nd valve pressure
    1st valve pressure 90-135 psi

    2nd valve pressure <160 psi
  156. Major components of Engine Fuel System?
    • Low pressure engine driven fuel pump
    • Oil to fuel heat exchanger
    • Hi pressure engine driven fuel pump
    • Fuel Control Unit (FCU)
    • Fuel Flow Transducer
    • Flow Divider
    • Fuel Manifold
    • Fuel Nozzles
  157. By-Pass Valve
    • By-Pass valve maintains constant delta pressure (P1/P2)
    • 53 psid
    • During acceleration demand for metered fuel (P2) is greater so less P1 is dumped
  158. Minimum Flow Valve
    • Adjusted to provide 90 PPH during start
    • Prevent flame out during rapid deceleration
  159. Torque Limiter
    • Torque limiter works with FCU to prevent torque from exceeding 46+/- .5 psi
    • Unit is a:
    • sealed bellows w torque meter oil pressure
    • limit springs
    • valve seals Py air orifice plumed to FCU
  160. Pusher Ice Mode illuminates when?
    • Prop switch - ON
    • Inert Sep - OPEN
    • Shaker/Pusher automatically switches to "Ice Mode"
  161. Procedure for NO COMBUSTION w/I 10 sec.
    • Condition Lever - Idle/Cutoff
    • Starter Switch - Reset
    • Dry Motoring Run - 30 sec.
  162. EIS Warning for ITT
    Warning when temp >10000
  163. EIS Caution range for ITT
    Caution range for ITT temp 8700 - 10000
  164. EIS Torque Warning
    Torque Warning when torque is > 61 PSI
  165. Hydraulic Power Pack will not have Electrical Power under what conditions?
    • Loss of GEN 1 which isolates NON-ESS BUS
    • Power Pack overheat via Thermal Protection
  166. An amber HYDR CAWS light indicates:
    • In flight pressure < 1800 PSI
    • On Ground - Power Pack cycled at least 6 times in 1 hr. & needs servicing
  167. Max Zero Fuel Weight?
    Max Zero Fuel Weight = 9039
  168. Landing distance increase with zero flaps
    Landing distance increase with 0 flaps is 1.83
  169. Landing distance increase with 150 flaps
    Landing distance increase with 150 = 1.31
  170. Auto Engine Start Sequence ie: Sec - Off
    • 60 sec - OFF
    • 60 sec - OFF
    • 30 min - OFF
  171. Surface De-Ice system pressure is
    • Nominal 14 PSi
    • Over Pressure Relief at 18 PSI
  172. If BOOT De-Ice pressure falls Below _____. What happens?
    • < 10 PSI or
    • Error in Sequence

    • Green DE ICE BOOTS light flashes
    • Red DE ICE light illuminates
  173. Which BUSS supplies Boots Power?
    GEN 2 BUS supplies power to Timer and control valves
  174. PCL Aft of IDLE detent prohibited
    • Engine not running
    • During flight
    • Using MOR
  175. What is the IAS in the climb when Zero
    flaps & PUSHER ICE MODE
    IAS is 130 kts.
  176. When does CAB PRESS annunciator illuminate?
    • Cabin altitude exceeds 10,700'
    • Max cabin differential of 6.5 PSI
  177. Max Landing Weight?
    Max Landing Weight = 9921 lbs.
  178. Surface De-Ice sequence is?
    • Horizontal Stabilizer
    • Wings - Bottom Inboard
    • Wings - Top Inboard
    • Wings - Bottom Outboard
    • Wings - Top Outboard
    • 8 sec per section
  179. How much will AOA be reduced when in PUSHER ICE MODE?
    Stall AOA is reduced 80
  180. What type of flaps on PC 12?
    Single piece Fowler type flap on each wing.
  181. Transient Prop RPM is
    Transient Prop RPM = 1870
  182. OAT up to 250 C. What is the maximum flap cycles?
    Up to 250 C maximum flap cycles = 8
  183. OAT limits for PC 12
    -550 C to +500 C
  184. What is the maximum Reverse Prop RPM?
    Max Reverse Prop RPM = 1650 RPM
  185. What is maximum Torque in Reverse?
    34 PSI is maximum Torque in Reverse
  186. What is the demonstrated X-wind at 150 flaps
    Demonstrated X-wind at 150 flaps = 25 KIAS
  187. PCL controls what?
    PCL movement directly controls FCU.
  188. Holding Speed for Icing & Normal conditions?
    • Icing Holding Speed is 170 KIAS
    • Normal Holding Speed is 150 KIAS
  189. What type of wing is on PC 12?
    • Wet wing
    • 2 spars
    • 1 fuel tank
  190. What type of battery?
    • 24 VDC NiCad 40 amp
    • 20 min. up to 60 amp draw
    • 30 min. below 50 amp draw
  191. GEN 1 maximum AMP
    • Max = 300 AMP
    • 450 for 2 min./hr.
  192. GEN 2 Max AMP?
    • Max 130 AMP continuous.
    • Belt driven 28 VDC
  193. EIS Caution illuminates when ITT is?
    EIS Caution light when ITT = 8000 - 8700 C.
  194. EIS - Caution Range digits blink at what rate?
    Caution range digits blink at 40/min.
  195. EIS Warning range digit blink at what rate?
    EIS Warning digits blink at 80/min.
  196. What is the function of the Pressure Relief Valve in the fuel system?
    • Prevents engine fuel system over pressurization
    • Dumps unmetered fuel >1350 PSI to bypass line back to fuel tans
  197. If Gear fails to retract what do you do?
    • CAWS NON ESSNTL BUS light - refer to electrical
    • CAWS HYDR light - refer to Emergency Extension
  198. Gear Warning horn sounds when?
    • Gear is UP & Flap Lever is past 150
    • Airspeed is <130 KIAS & Power < 10% of Max Torque
  199. CAWS AIR/GRD light illuminates when
    • One AIR/GRD switch fails
    • No light comes on when both switches fail at same time.
  200. Right Hand Gear AIR/GRD switch fails
    1. in the air position
    2. in the ground position
    • Fails in the air position
    •     Possible to Retract Gear on the ground
    • Fails in ground position
    •     Normal gear extension
    •     If engine fails then Emergency Ext.
  201. What are the values for High & Low hydraulic pressure?
    • High HYD pressure is 2800
    • Low HYD pressure is 2450
  202. CAWS HYDR light illuminated means
    • Hydr fluid is low
    • Main system pressure is < 1800 PSI - not enough pressure
    • On the ground - The pump motor has been activated more than 6 times in an hour indicating an excessive leak rate in the system
  203. If the CAWS HYDR light is continuously illuminated: What actions are taken?
    • On ground - System requires maintenance
    • In Flight - HYDR CTL CB Pull
    •             - KIAS < 177 kts.
    •             - Emergency Extension
  204. Accessory Gearbox Drives?
    • FCU
    • Engine driven fuel pump
    • Pressure & Scavenge oil pump
    • N1 Tach generator
    • Starter/Generator
  205. CAWS ESNTL BUS light is illuminated. What conditions exist?
    • Voltage is <  18 VDC
    • Check GEN 1, GEN 2 or BATT BUS
  206. CAWS FUEL PRESS light is illuminated. What actions are taken?
    • Reduce power to minimal to sustain flight
    • Fuel pumps on
    • If FUEL PRESS light stays on Land As Soon as Possible. Prepare for of field landing.
  207. CAWS
    Yellow DE-ICE & Green PROP DE-ICE flashing.
    What are your actions?
    • Prop switch OFF
    • Prop Switch ON
    • Check CB - Do not reset unless tripped
    • If light goes out after 5 seconds continue
  208. CAWS
    Yellow DE-ICE light & Green De-ICE BOOTS illuminated. What actions are taken?
    • Boots Switch OFF
    • PCL Increase power
    • Boots switch ON
  209. CAWS 
    Yellow AOA DE-ICE & Green PROBES DE-ICE illuminated. What are the actions taken?
    • Check CB
    • Probe switch OFF wait 3 min.
    • Probes switch ON
  210. CAWS
    Green PROBES DE-ICE light does not come on?
    Indicates failure of Pitot/Static Probe de-ice system.
  211. CAWS:
    Yellow PUSHER & Green INERT SEP & PROP DE-ICE illuminated.
    PUSHER ICE Mode is OFF are indications of what condition?
    Stall Warning/Stick Pusher system failure
  212. Propeller De-ice modes are
    • OAT > 00 C - Standby
    • OAT 00 =< 160 C
    •      Blades 1-3 heated 45 sec.
    •      Blades 2-3 heated 45 sec.
    •      System off 90 Sec.
    • OAT >-160 C 
    •       Blades 1-3 heated 90 sec. 
    •       Blades 2-4 heated 90 sec.
  213. EIS Torque Caution Range is 
    EIS Caution Range is 44.4 - 61.0 PSI
  214. Departing into Known Icing Conditions. Vr w 150 flaps is
    Vr = 9 kts.

    79 + 9 = 88 kts.
  215. ITT Starting limits are
    • 8000 - 8700 C - 20 sec.
    • 8700 - 9990 C - 12 sec.
    • 10000 C - 5 sec
  216. EIS warning when oil temperature is >
    EIS warning when oil temperature is > 1100 C.
  217. GEN 1 OFF or GEN 2 OFF annunciators illuminate when there is
    • Over voltage
    • Under voltage
    • Overload
    • Reverse current
  218. White arc on airspeed indicator
    64 - 130 KIAS
  219. Green arc on airspeed indicator
    91 - 236 KIAS
  220. Ramp weight is ?
    Takeoff weight is ?
    • Ramp = 9965
    • Takeoff = 9921
    • Landing = 9921
    • Zero Fuel = 9039
  221. GPU must provide
    • 27 - 30 VDC of 500 amps to supply power to aircraft and
    • 1000 amps for engine start
  222. L/R FUEL LOW CAWS annunciator illuminates when
    < 20 gals in respective tank
  223. Temperature Control Valve attempts to maintain a selected temperature between
    180 C to 300 C
  224. CPCS maintains a max cabin differential of
    5.75 PSI = 10k' equivalent at a max service ceiling of 30k'
  225. Ground idle is what %
    Ground idle 50.7% Ng
  226. Maximum O2 pressure range is
    Max O2 pressure is between 1850 - 2000 PSI
  227. EIS caution illuminates when GEN 2 DC amps are
    EIS caution illuminates when GEN 2 DC amps > 140 amps
  228. Primary ACU provides indication of the following
    • Torque
    • ITT
    • Ng
    • Fuel Quantity data
  229. Maximum speed for Emergency Gear extension
    Maximum speed for Emergency Gear extension is 110 KIAS
  230. Engine operating limits are
    • Torque:
    • 44.3 PSI max TO limited to 5 min.
    • 36.9 PSI max climb/cruise - continuous
    • ITT:
    • 7200 C max ITT - continuous
    • 8000 C max ITT for TO limited to 5 min
    • 8700 C max ITT limited to 20 sec.
    • 10000 C MAX ITT start limited to 3 sec.
  231. Iceing limitations during flight
    • Operational De-Ice Boots
    •      150 Flaps
    •      108 KIAS
    • Boot Failure
    •       00 Flaps
    •       130 KIAS minimum
  232. Maximum fuel imbalance
    26.4 gal or 178 lbs.
  233. Maximum Cabin differential is:
    • Green Arc = 5.75 psi
    • Yellow Arc = 6.50 psi
    • Red Line = 6.50 psi
  234. Cabin Pressurization Control System  differential dial markings are
    • Green arc = 5.75 PSI
    • Yellow arc = 6.50 PSI
    • Red line = 6.50 PSI
  235. When deploying ECS Emergency Shutoff Valve what happens?
    • Firewall SHUTOFF isolates the system during emergencies such as engine fire
    • Opens Ram Air Scoop on right side under fuselage letting fresh air into the cabin
  236. VCCS maybe operated under what conditions?
    • During ground operations
    • Up to an altitude of 25k'
  237. Cabin Pressurization Control system (CPCS) does what?
    • Regulates cabin pressure via outflow valves
    • Entirely pneumatic except for
    •    Switching Ground & Flight modes
    •    In flight depressurization
Author
jaford047
ID
55513
Card Set
PC12
Description
Training
Updated

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