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91 Cards in this Set

  • Front
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Maximum ramp weight

12,500 pounds
Maximum take-off weight
12,375 pounds
Maximum landing weight
11,500 pounds
Maximum zero fuel weight
9,300 pounds
Mmo
.72 Mach
Vmo
((8,000 to 29,300 feet)
275 knots
Vmo
(below 8,000 feet)
260 knots
Turbulent air penetration
180 knots
Vfe flaps 15
200 knots
Vfe flaps 35
161 knots
Vfe ground flaps 60
Prohibited in flight
Max speed with flaps failed to ground 60
140
Max gear extended Vle
200 knots
Max gear operating
(extending or retracting)
200 knots
Vsb maximum speedbrake operating speed
No limit
Vx 2 engine flaps 15
124 knots
Vy 2 engine flaps 15
191 knots
Vmca flaps 0
89 knots
Vmca flaps 15
81 knots
Vmcg
89 knots
Maximum tire speed
165 knots
Maximum autopilot speed
275 knots or .72 mach
Maximum altitude for take off or landing
14,000 feet
Maximum tailwind for take off and landing
10 knots
Maximum crosswind for take off and landing
26 knots (not a limit)
Minimum temperature for take off and landing
minus 33 Celsius
Maximum operating altitude
45,000 feet
Generator load
300 amps to 41,000
250 amps above 41,000
Load factor
-1.52 to +3.6 at 12,375 pounds flaps up

Flaps 15 or 35
0 to +2 at 12,375 pounds
Minimum battery voltage for start
24 volts
Minimum/maximum external power current for start
800/1,000 amps
Start cycle limitation
3 starts in 30 minutes
3 cycles of operation with a 60 second rest between cycles
Battery cycle limitations
3 starts per hour
Approved oil
Mobile Jet II
Engine type
Williams FJ44-2C
Maximum ITT take-off
820 degrees Celsius
Maximum Continuous ITT
805 degrees Celsius
Maximum N1 take off
105.2
Maximum N1 continuous
105.2
Maximum N2 take off
98.8
Maximum N2 Continuous
98.8
Maximum tailwind for start
16 knots
Maximum crosswind for start
16 knots
Maximum time to light off
10 seconds
Maximum current for ground operation
250 amps
Maximum time for pitot heat on ground
2 minutes
Maximum time for anti-ice on ground with high RPM
1 minute
Fuel boost pumps on when.....
Fuel Low Level lights illuminate
Maximum asymmetric fuel differential
200 pounds (600 has been demonstrated)
Minimum N2 for anti ice equipment
75%
Minimum temperature for tail de-ice boots
-35 Celsius
Hydraulic Fluid
MIL-H-83282
Cabin Pressurization Max Differential
9 psi
Minimum altitude for autopilot to engage after takeoff
240 AGL
Minimum altitude for autopilot engage in cruise
1,000 AGL
Minimum altitude for autopilot on an ILS
70 AGL
Minimum altitude for autopilot on a nonprecision
240 AGL
Things required for single pilot operation
Autopilot
Headset
Checklist
Charts
N1 redline
105.3%
ITT Engine Start red triangle
1002 C
Minimum temperature for tail de-ice boots
-35 Celsius
Hydraulic Fluid
MIL-H-83282
Cabin Pressurization Max Differential
9 psi
Minimum altitude for autopilot to engage after takeoff
240 AGL
Minimum altitude for autopilot engage in cruise
1,000 AGL
Minimum altitude for autopilot on an ILS
70 AGL
Minimum altitude for autopilot on a nonprecision
240 AGL
Things required for single pilot operation
Autopilot
Headset
Checklist
Charts
N1 redline
105.3%
ITT Engine Start red triangle
1002 C
Engine running red line ITT
822 degrees Celsius
Oil temperature red line
136 degrees Celsius
Oil pressure red line
22 psi
Engine failure below V1
Brakes
Throttles
Speedbrakes
Engine failure above V1
Maintain directional control
Accelerate to Vr
Rotate at Vr
Climb at V2
Landing gear up
If necessary, Wing X Flow switch
At 1,500 feet, V2+10, retract flaps, accelerate to Venr
Engine failure during approach
Increase power
Vapp
Flaps at approach
Engine fire
Throttle: idle
Engine firewall shutoff, push
Fire bottle
Engine restart
Ignition both on
Fuel boost both on
Throttles idle
200 knots if altitude allows
Electrical fire or smoke
Oxygen mask
Mic switch
Environmental smoke
Oxygen mask
Mic switch
Smoke removal
Oxygen masks
Mic switch
Cabin Altitude Light
Oxygen mask
Mic switch
Emergency descent
Passenger oxygen
Emergency descent
AP/Trim button-push
Throttles idle
Speedbrakes
20 degrees nose down
Battery Overtemp
Note volts/amps
Battery emer
Note volts/amps
Autopilot malfunction
Disengage
Electric Elevator Trim Runaway
Autopilot disconnect
Throttles as required
Speed brakes as required
Manual trim as required
Pitch Trim CB-pull
Emergency Evacuation
Parking brake set
Throttles off
Firewall buttons
Fire bottles
Battery off
ELT activate
Escape route
Things on the Hot Battery Bus
Lights
Voltmeter
Emergency Bus
ELT
What is powered by the EMER battery position?
Hot and EMER busses

EMER Bus includes:
Comm 1
Nav 1
Standby HSI
AHRS2
Standby airspeed/altimter
Audio 1
Floodlight rheostat
Standby N1 display
Right pitot/static heat
Landing gear warnign CB
Gear Control CB
Hydraulic Control CB
Flap control CB
Scenario: Airborne, dual GEN failure and the Battery Switch in BATT. How long will things run?
10 minutes.
Scenario: Airborne with dual GEN failure and the Battery Switch in EMER. How long will things run?
30 minutes