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174 Cards in this Set
- Front
- Back
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Max Torque
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19,600 in lbs
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NTS Torque
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1,260 +/- 600 in lbs
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Torque w/ oil temp below 0C
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Minimum
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Torque w/ oil temp between 0-40c
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4,500 in lbs Maximum
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Torque w/ oil temp 40c and rising
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19,600 in lbs
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Safety coupling torque
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-6,000 in lbs
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Maximum reverse torque difference
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1,000 in lbs
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Run up torque
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8,000 - 9,000 in lbs
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Maximum positive torque flux during NTS check
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500 in lbs
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Minimum torque rise at flight idle
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200 - 2,000 in lbs
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Low speed ground idle RPM
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69 - 75.5%
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Normal ground idle RPM
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94 - 102%
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Reverse RPM
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96 - 106%
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Flight idle RPM
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92.5 - 100.5%
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Normal in flight RPM
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98 - 102%
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RPM Fluctuation
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+/- 0.5%
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Starter disengage RPM
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60%
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Prop brake disengage RPM
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23%
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Pitchlock RPM (engaged)
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103%
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Fuel topping RPM
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103.5%
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Start circuit energized RPM
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16%
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Start circuit de-energized RPM
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65%
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TD switch from start limiting to normal litmiting RPM
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94%
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Maximum RPM for light off
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35%
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Oil pressure indication by RPM
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35%
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Maximum Turbine Inlet Temperature?
For how many mins? |
1083 for 5 mins
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Military Turbine Inlet Temperature?
For how many mins? |
1049 for 30 mins
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NATOPS maximum continuous Turbine Inlet Temperature?
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1010
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CFLSW maximum continuous Turbine Inlet Temperature?
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932
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NATOPS climb Turbine Inlet Temperature?
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1010
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CFLSW climb Turbine Inlet Temperature?
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970
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Procedure if Turbine Inlet Temperature exceeds 1083 over 5 seconds or 1175 momentarily
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Reduce power to hold temperature within limits / record discrepancy / overtemp inspection required
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Turbine Inlet Temperature for temp controlling check
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910
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Turbine Inlet Temperature temp limiting range
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0 - 65 degrees throttle movement
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Maximum Turbine Inlet Temperature for enrichment start in flight
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200
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Maximum Turbine Inlet Temperature for enrichment start on ground
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100
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Maximum Turbine Inlet Temperature during start
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830
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Procedure for adnormal torch during starts?
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Overtemp inspection
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Procedure for start Turbine Inlet Temperature of 830 - 850?
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Record discrepancy
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Procedures for start Turbine Inlet Temperature of 850 - 965?
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Discontinue start / record discrepancy / one restart is permitted after cooling below 200C
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Procedure for start Turbine Inlet Temperature exceeds 965?
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Discontinue start / record discrepancy / overtemp inspection is required
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Normal start Turbine Inlet Temperature range
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750 - 830
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Enginge starter switch released at what RPM?
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60%
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Start light out within how many seconds after release of start switch?
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15 seconds
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Starter duty cycle
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1 min on 1 min off
1 min on 5 min off 1 min on 30 min off |
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Maximum RGB oil pressure during start and warmup?
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250 psi
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Maximum RGB oil pressure during start and warmup may be exceeded below what OAT?
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15C
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Minimum RGB Oil pressure at LSGI
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50 psi
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RGB oil pressure at normal
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150 - 250 psi
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RGB allowable oil pressure flux
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+/- 20 psi
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Maximum power section oil pressure during start and warmup?
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100 psi
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Minimum power section oil pressure at LSGI
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50 psi, may be below if witihin limits at 100% RPM
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Power section oil pressure at normal
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50 - 60 psi
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Power section allowable oil pressure flux
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+/- 5 psi
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Maximum oil temp on ground?
For how many mins? Then reduced to what temp? |
100C / 30 mins / 85C
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Maximum oil temp in flight?
For how many mins? Then reduced to what temp? |
100C / 5 mins / 85C
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Normal oil temp
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60 - 85C
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Minimum oil temp for maximum torque
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40C and rising
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Minimum oil temp for starting
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-40C
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Normal oil quantity
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4 - 12 gallons
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Minimum oil quantity
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4 gallons
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Oil MIL-SPEC
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MIL-L-23699
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Utility/Booster hydraulic system normal pressure
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2,900 - 3,200 psi
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Utility/Booster hydraulic system maximum pressure
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3,500 psi
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RPM for normal hydraulic pressure
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100%
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Minimum hydraulic pressure at LSGI
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2,550 psi
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Aileron boost hydraulic pressure
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2,050 psi
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Rudder boost maximum hydraulic pressure w/ flaps set at 15-100%
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3,500 psi
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Rudder boost maximum hydraulic pressure w/ flaps set at 0-15%
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1,600 psi
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Rudder boost hydraulic pressure w/ flaps set at 15-100%
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2,900 - 3,200 psi
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Rudder boost hydraulic pressure w/ flaps set at 0-15%
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1,100 - 1,400 psi
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Rudder boost caution hydraulic pressure w/ flaps set at 0-15%
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1,400 - 1,600 psi
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Auxiliary hydraulic system pressure
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2,900 - 3,300 psi
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Auxiliary hydraulic system maximum pressure
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3,500 psi
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Utility/Booster accumulator pressure
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1,500 +/- 100 psi
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Normal brake accumulator pressure
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1,500 +/- 100 psi
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Emergency brake accumulator pressure
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1,000 +/- 100 psi
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Normal brake pressure
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2,900 - 3,200 psi
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Maximum normal brake pressure
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3,500 psi
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At what psi will there be one application of normal brakes remaining?
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2,250 psi
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Emergency brake pressure
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2,900 - 3,300 psi
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Emergency maximum brake pressure
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3,500 psi
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At what psi will there be one application of emergency brakes remaining?
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2,900 psi
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Electrical system generator rating
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40 KVA
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What is the power source if the Copilot inverter power switch is in the standby position?
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Isolated DC
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What happens when the Copilot inverter power switch is in the normal position?
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Inverter is off
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DC power sources
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Battery, transformer rectifiers, external
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How many generators to power all buses?
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two
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Normal power source for L/H AC BUS
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#1 engine
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Normal power source for R/H AC BUS
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#4 engine
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Normal power source for ESS AC BUS
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#2 engine
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Normal power source for Main AC BUS
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#3 engine
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Normal power source for ESS Avionics BUS
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#1 BSU
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Normal power source for Main Avionics BUS
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#2 BSU
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Standby power source for Copilot Inverter BUS
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Isolated DC BUS
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Primary power source for #1 BSU
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Essential AC BUS
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Alternate power source for #1 BSU
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Main AC BUS
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External power source for #1 BSU
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L/H AC BUS
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Primary power source for #2 BSU
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Main AC BUS
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Alternate power source for #2 BSU
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Essential AC BUS
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External power source for #2 BSU
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R/H AC BUS
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DC electrical voltage
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25-30 vdc
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Max DC electrical load
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0-1.03
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Battery voltage
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24 vdc
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Minimum battery voltage
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21 vdc
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AC electrical voltage
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110-125 vac
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AC electrical frequency
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380-420 hz
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Max AC load
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0-1.05
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Prop blade de-icing amps
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60-90
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Spinner anti/de-icing amps
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65-90
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Max # of cycles of Prop Anti-Icing/De-Icing during ground ops
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two
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Wing empennage anti-ice overheat light illuminates at what temp?
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200F
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Maximum OAT for ground operation of the windshield anti-ice?
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27C/81F
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Windshield anti-ice cold start temp
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-45F
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Fuel unbalance limit inboard to outboard tanks
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500-1,000 lbs, more to outboard
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Fuel unbalance limit of symmetrical tanks
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1,000 lbs
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Fuel unbalance limit of wing to wing
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1,500 lbs
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External tanks fuel unbalance limit
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1,000 lbs
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Aux tanks fuel unbalance limit
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one empty one full providing all other tanks are symmetrically fueled
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Main tank fuel pumps system pressure
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15-24 psi
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Aux tank fuel pumps system pressure
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28-40 psi
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External tank fuel pumps system pressure
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28-40 psi
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Fuel dump pump system pressure
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28-40 psi
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Fuel LOW PRESS light illuminates
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8.5 psi
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Fuel system TANK EMPTY light
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23 psi
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Pressure of fuel surge suppressor
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40 +\- 5 psi
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Maximum re-fueling pressure
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60 psi
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Oxygen system capacity
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25 liters
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Oxygen system LOW Warning light
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2.5 liters
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Oxygen system operational pressure in no flow condition
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270-455 psi
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Oxygen system operational pressure in a continuous condition
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270-340 psi
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Minimum temp for static feather check
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OAT of 32F or 0C
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Maximum pressurization for crew door jetison
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3.1 in hg
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Pressure control maximum differential
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15.8 in hg
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Pressurization gage limits
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-1.2 to 15.8 in hg
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Limitation for pressurization if an inner or outer pane of windshield is cracked
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10 in hg
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Limitation for pressurization if an inner or outer pane cargo compartment window is cracked
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10 in hg
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Limitation for pressurization if both panes of cargo compartment window is cracked
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0 in hg
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Max speed of w/ 10% flaps
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220 knots
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Max speed of w/ 20% flaps
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210 knots
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Max speed of w/ 30% flaps
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200 knots
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Max speed of w/ 40% flaps
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190 knots
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Max speed of w/ 50% flaps
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180 knots
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Max speed of w/ 60% flaps
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165 knots
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Max speed of w/ 70% flaps
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155 knots
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Max speed of w/ 80% flaps
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150 knots
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Max speed of w/ 90% flaps
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145 knots
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Max speed of w/ 100% flaps
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145 knots
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Max speed gear down
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170 knots
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Max speed w/ landing lights extended
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170 knots
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Max angle of bank w/ flaps up
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60 degrees
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Max angle of bank w/ flaps down
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45 degrees
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Max taxi speed w/ A/C weight <155K
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20 knots
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Max taxi speed w/ A/C weight >155K
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10 knots
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Recommended max takeoff weight
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155K
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Overload max takeoff weight
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175K
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Normal landing weight
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130K
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Max speed for windmill taxi start
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100 knots
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Fire extinguisher system pressure
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575-660 psi at 70F
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APU RPM
-Normal? -Max? -Overspeed? |
Normal 95-105
Max 106 Overspeed 110 |
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APU EGT
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260-650
Max 650 |
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APU Generator
-Frequency? -Volts? -Load? |
380-420 hz
110-125 vac 0-1.05 |
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APU warm up/cool down time
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1 min
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Minimum bleed air pressure on ground
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35 psi
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APU bleed air checks
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30-15 not less than 16 seconds
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Engine bleed air checks
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65-35 not less than 30 seconds
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What is the power source if the Copilot inverter power switch is in the NORM position?
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Inverter is off, power is supplied by the Phase A of the essential Avionics AC BUS
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What is the power source if the AC EI & FC inverter power switch is in the NORM position?
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Phase C Essential Avionics AC BUS
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What is the power source if the AC EI & FC inverter power switch is in the STBY position?
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Essential DC BUS
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At what Fuel System Pressure does the BY-PASS LIGHT illuminate
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4 PSID
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Safety Valve Opens above and below what in hg
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-0.76/15.9 in hg
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Crossover Turbine Inlet Temperature
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800 to 840
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Procedure for peak Turbine Inlet Temperature between 720 and 750
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Continue start and record discrepancy.
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Procedure for peak Turbine Inlet Temperature below 720
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Discontinue start, record discrepancy, 1 attempt to restart w/ TD in null.
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