Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
91 Cards in this Set
- Front
- Back
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
|