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T44BOLDFACE/OPSLIMITS

  1. EMERGENCY SHUT DOWN ON DECK
    • 1. CONDITION LEVERS - FUEL CUTOFF
    • 2. FIREWALL VALVES - CLOSED
    • 3. BOOST PUMPS - OFF
    • 4. FIRE EXTINGUISHER - AS REQUIRED
    • 5. GANG BAR - OFF
    • 6. EVACUATE AIRCRAFT
  2. EMERGENCY SHUTDOWN CHECKLIST
    • 1. (C) POWER LEVER - IDLE
    • 2. (C) PROP LEVER - FEATHER
    • 3. (C) CONDITION LEVER - FUEL CUTOFF
    • if fire or fuel leak?
    • 4. (C) FIREWALL VALVE - CLOSED
    • 5. (C) FIRE EXTINGUISHER - AS REQUIRED
    • 6. (C) BLEED AIR - CLOSED
  3. Aborted Takeoff
    Announce "ABORT, ABORT, ABORT"

    • Power levers- Idle
    • Reverse- As required
    • Brakes- As required
    • Condition Levers- Fuel Cutoff
    • **as soon as practicable
    • Firewall Valves- Closed
    • Boost Pumps- Off
    • Fire Extinguishers- As required
    • Gang Bar- Off
    • Evacuate Aircraft
  4. WINDMILLING AIRSTART
    • 1. (C) POWER LEVER (FAILED ENGINE) - IDLE
    • 2. (C) PROP LEVER (FAILED ENGINE) - FULL FORWARD
    • 3. (C) CONDITION LEVER (FAILED ENGINE) - FUEL CUTOFF
    • 4. FIREWALL VALVE - OPEN
    • 5. AUTOIGNITION - ARMED
    • 6. CONDITION LEVER - LOW IDLE
    • 7. POWER - AS REQUIRED
  5. Brake Fire
    • Stop Aircraft
    • Firefighting Assistance- Request
    • Emergency Shutdown on Deck checklist - Execute
  6. Low Altitude Windshear
    • Power- Max Allowable
    • Attitude- Set and Hold approx 15o nose up
    • Gear- Up
    • Flaps- Maintain current setting
  7. SMOKE/FIRE OF UNKNOWN ORIGIN
    • 1. CREW - ALERTED
    • 2. CABIN TEMPERATURE MODE - OFF
    • 3. VENT BLOWER - AUTO
    • 4. OXYGEN MASK/MIC SWITCH(100%) - AS REQUIRED
  8. FUEL LEAK
    Where is it coming from?

    • Condition lever- Fuel Cutoff
    • Emergency shutdown checklist- complete
  9. SMOKE AND FUME ELIMINATION
    • 1. OXYGEN MASK/MIC SWITCH (100%) - AS REQUIRED
    • 2. PRESSURIZATION - DUMP
  10. Jammed Power Lever
    • Condition Lever (affected engine) - Fuel Cutoff
    • Emergency Shutdown Checklist- Execute
  11. PROP FAILURE/MALFUNCTION
    • 1. PROP RPM - ADJUST TO NORMAL RPM
    • 2. (C) POWER LEVER- IDLE
    • 3. (C) PROP LEVER - FEATHER
    • 4. ALTERNATE PROP FEATHERING CHECKLIST- AS REQUIRED
  12. DUAL INVERTER FAILURE you will lose what?
    GCANT

    • GPS
    • Compass
    • Attitude Gyro
    • Nav Needles
    • Torque gauge
  13. EXPLOSIVE DECOMPRESSION
    • 1. OXYGEN MASK/MIC SWITH (100%) - AS REQUIRED
    • 2. DESCEND - AS REQUIRED
  14. TORQUE:

    NORMAL RANGE
    Max @ 2200 RPM
    Max @ 1900 RPM
    Normal: 400-1315ft/lbs

    Max @ 2200RPM: 1315ft/lb

    Max @ 1900RPM: 1520ft/lb
  15. TURBINE TACHOMETER (N1)

    Normal Range & Max
    Normal: 50-101.5%

    Max: 101.5%
  16. Interstage Turbine Temp. (ITT)

    Normal
    Max Continuous
    Max Starting
    400o- 790o C NORMAL

    790o C Max Continuous

    1090o C Max Starting
  17. Propeller Tachometer (N2)

    Normal and Max
    1800-2200 RPM Normal

    2200 Max
  18. Oil Temp and Pressure

    Normal and Max
    Oil Temp: Normal 10-99o C Max 99o C

    Oil Pressure: 40PSI Minimum, 85-100PSI Norm, 100PSI Max
  19. Pneumatic Pressure

    Normal and Max
    12-20 PSI Normal

    20 PSI Max
  20. GYRO SUCTION

    Below 15,000' MSL

    15 - 31,000' MSL
    HG 4.3 -5.9 (5.1 +- 0.8) Below 15K'

    HG 3.0 - 5.9 15K' - 31K'
  21. Cablin altimeter and Pressure differential

    Normal and Max
    0-4.7 PSI NORMAL

    4.7 PSI MAX
  22. Fuel Quantity

    yellow arc range
    0-265 lbs
  23. Propeller Deicer Ammeter

    Normal
    14-18 Amps normal Operation
  24. Airspeed Indicator

    Normal Range
    88-227 KIAS
  25. VMCG (min controllable speed on ground)
    63 kts
  26. VMCA (Min controllable airspeed)
    86 KIAS
  27. VMO (max dive/ max level flight)
    227 KIAS

    decreases 4 KIAS for every 1000' above 15,500'MSL
  28. VLE (max gear extension)
    155 KIAS
  29. VLO (max gear retraction speed)
    145 KIAS
  30. VFE @ 35% approach flaps

    VFE @ 100% Down flaps
    174 KIAS (35%)

    140 KIAS (100%)
  31. VSSE (Min safe one engine inoperative)
    91 KIAS
  32. VYSE (one engine inop best RATE of climb)
    110 KIAS
  33. VXSE (one engine inop best ANGLE of climb)
    102 KIAS
  34. Max sink rate at ground contact
    600 FPM
  35. Max Crosswind
    20 Knots
  36. Max Ramp weight
    9710 lbs
  37. Max T/O weight
    9650lbs
  38. Max Landing weight
    9168 lbs
  39. define Max Allowable Power
    Max power available from the engines for takeoff. Time is limited to 5 minutes
  40. define Max Continuous Power
    Maximum power available from the engines not limited by time. Intended for emergency use and at pilots discretion
  41. define Cruise Climb
    Max power approved for normal climb
  42. Define Cruise
    Power required from the engines to maintain level flight at a desired altitude while traveling at an airspeed within the normal operating range approved for the aircraft. Will vary with altitude and airspeed
  43. OPS LIMITS:

    Max allowable ITT
    790o C
  44. OPS LIMITS:

    Max Continuous ITT
    790o C
  45. OPS LIMITS:

    CRUISE CLIMB ITT
    765o C
  46. OPS LIMITS:

    CRUISE ITT
    740o C
  47. OPS LIMITS:

    LO-IDLE ITT
    685o C
  48. OPS LIMITS:

    Starting ITT
    1090o C for 2 seconds
  49. OPS LIMITS:

    Acceleration ITT
    850o C
  50. OPS LIMITS:

    Max Reverse ITT
    790o C
  51. OPS LIMITS:

    Max Reverse:

    N1%
    N2 RPM
    86%

    2,100 RPM
  52. VA (maneuvering speed)
    153 KIAS
  53. OPS LIMITS:

    Max Reverse Time limit
    1 minute
  54. OPS LIMITS:

    Acceleration:
    Time limit
    Torque and
    N1%
    N2 RPM
    2 seconds Max time

    2,100 Ft/Lb Torque

    102.6% N1

    2,420RPM N2
  55. Oil Px below 85PSI is _______
    below 40PSI is _______
    • undesirable
    • unsafe
  56. Ambient Temp Limitations:

    Aircraft shall not be operated when T/O ambient temp is____or greater above standard temperature for the airport
    37o C
  57. C.G. Limitations @ 9650lbs
    19.4% THRU 31.8% M.A.C. @ 9650lbs
  58. C.G. Limitations @ 9168lbs
    17.3% THRU 31.8% M.A.C. @ 9168lbs
  59. C.G. limitations @ 7850lbs
    11.6% THRU 31.8% M.A.C. @ 7850lbs
  60. Acceleration G-Limits

    Clean level flight
    Clean Max Bank
    FULL FLAPS
    Clean level: +3.0 To -1.0g

    Clean Max Bank: +3.0 To -1.0g

    Full Flaps: +2.0 To 0g
  61. Max Altitude
    31,000'
  62. Dual powered items on hot battery bus
    • 2 boost pumps
    • 2 Firewall Shutoff valves
    • 1 crossfeed valve
  63. Single powered items off hot battery bus?
    TBACCE

    • Threshold lights
    • Baggage door light
    • Aft compartment light
    • Cabin observation light
    • Cross feed light
    • Engine fire extinguishers
  64. Min Volts for APU charge? APU start? Battery Start?
    • APU Charge: 18V
    • APU Start: 20V
    • Battery Start: 22V
  65. Items you have remaining with TOTAL DC FAILURE?
    • ITT gauge
    • PROP RPM gauge (N2)
    • N1 Gauge
    • Pitot static instruments
    • Standby compass
    • Co-pilots turn and slip ind
    • Clock
  66. Auto Ignition activates when?
    • - the system is ARMED
    • - Torque below 410+-50ft/lbs
  67. PROP GOVERNORS:
    Primary Governor?
    Overspeed Governor?
    Fuel Topping Governor?
    Normal Range?
    • Primary Governor: 2200rpm
    • Overspeed Governor: 2288rpm +-40
    • Fuel topping Governor: 2332rpm
    • Normal: 1800-2200rpm

    At 2420rp: reduction gearbox failure
  68. Oil to fuel heater begins to bypass oil at ____deg F and completely bypasses oil at ___deg F
    • 70deg F
    • 90def F
  69. Beta Blade Angle
    15o to -5o
  70. Boost Pumps provide ____psi fuel to engine driven fuel pump and for cross feeding
    30psi
  71. suction lift for how many hours before overhaul?

    altitude limitation because of cavitation?
    10 hrs

    stay below 13K' on suction lift bc of pump cavitation
  72. 3 items that disable electric heat
    • Windshield heat
    • Prop de-ice
    • Lip Boot de-ice
  73. 5 things that interfere with MAGNETIC COMPASS
    • Windshield anti-ice
    • Windshield Wipers
    • Air conditioning
    • Electric heat
    • Vent Blower
  74. Right Squat Switch
    GFISH

    • G- makes ldg Gear circuit inop
    • F- Flight hour meter is INOP
    • I- deactivates AOA indexer lights
    • S- deactivates Stall warning
    • H- deactivates right engine lip heat
  75. Left Squat Switch
    HHHAP

    • H- left engine inlet lip heat inop
    • H- electric heater to remain in GRD MAX (8elements)
    • H- reduces AOA heat from 28VDC to 14 VDC
    • A- closes Ambient air solenoid
    • P- Pressurization controls
  76. DC Generator Voltages
    28.25 +- 0.8V
  77. AC Inverter Frequency
    400 +- 6 Hz
  78. AC Inverter Voltage
    114 +- 7 V
  79. Max Endurance Glide
    102 Kias
  80. Max Glide Range
    130 KIAS
  81. Min Oxygen required for Local/Cross country FLight
    1000 (1500 for cross country)
Author
Aflax12
ID
74076
Card Set
T44BOLDFACE/OPSLIMITS
Description
Boldface and Ops Limits for the T44A
Updated

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