Limitations Flashcards
Max Ramp Weight
6040lbs
Max Takeoff Weight
6000 lbs
Max Landing Weight
5550 lbs
Max Zero Fuel Weight
4900 lbs
Max Aft Baggage Compartment
300 lbs
Max Cargo X-Tend Compartment
40lbs
Min Oil Temp
-40F/-40C
Min temp for battery 1 start
0F/-18C
Min voltage for battery 1 start
23.5 Volts
Min temp for EPU Start
-40F/C
EPU Voltage and Amperage requirements
28V and 800-1000 amps
Max tailwind for start
15 knots
Max crosswind for start
25 knots
Inflight air start and less than 18,000ft Speed
120-200 knots
Starter Limits
30 seconds on per attempt
1st Attempt - 30 seconds Off
2nd Attempt - 5 minutes Off
3rd Attempt - 30 minutes Off
Approved fuel types
Jet-A, Jet A-1, JP-8
Maximum Fuel
296 gallons
Maximum allowable fuel imbalance
15 gallons
Min fuel temp
-40F/C
Max fuel temp
122F/50C
Gallons increments when refueling
75 gallons
Type of engine and capable thrust
Williams FJ33-5A
1846lbs thrust, uninstalled, sea level, temp of 60F
Approved oil
Mobile Jet II / Mobile 254
Max oil quantity
3 quarts
Amount of oil to full line
2.2 quarts
Maximum tailwind
10 knots
Maximum demonstrated crosswind
18 knots - Flaps 50%
16 knots - Flaps 100%
Maximum airport elevation
10,000ft
Minimum airport elevation
-1,000 ft
Minimum Takeoff temperature
-40C/F
Maximum Takeoff temperature
50C/122F
Vmo/Mmo
250knots/.53 Mach
Vo
150 knots
Maximum time in T/O Thrust
5 minutes
Maximum operating altitude
FL280
Min operating temp at FL280
-61C/-77F
Min operating temp at FL200
-54C/-65F
Cool down after high energy event
30 minute
Flight Load Limits
\+3.6g, -1.5g Flaps Up, any Weight \+1.9g, 0g Flaps 50%, any weight \+1.9g, 0g Flaps 100%, any weight \+3.6g, -1.5g Vle \+2g, 0g Vlo
Vfe - 50%, 100%
190 knots - Flaps 50%
150 knots - Flaps 100%
Vlo- Extend
210 knots
Vlo - Retract
150 knots
Vle
210 knots
Maximum cabin pressure differential
6.4 psi
Min landing gear operating temp
-40C/F
Maximum gear cycles
Rest period between cycles
8 gear cycles per 30 minutes
10 seconds
Generator 1 voltage and Current
27.8V, 270A
Generator 2 Voltage and Amp
28.7V, 72A
CABIN ALTITUDE Warning Altitude
10,000ft
Minimum Autopilot engagement speeds
85 knots - Flaps 100%
95 knots - Flaps 50%
105 knots - Flaps Up
Minimum autopilot engagement altitude
400’ AGL
Minimum altitude for autopilot use
1,000ft AGL - visual approaches
DA/MDA - Instrument approaches
Usable IPS fluid
3.0 gal
Minimum IPS fluid dispatch quantity into icing conditions
1.0 gal
Minimum windshield IPS temp
-30F/-34C
Minimum wing/stab IPS Temp
-40C/F
Minimum airspeed in icing conditions
160 knots
Maximum flap deflection with ice accretion
50% Flaps
Max duty cycle for windshield IPS
10 seconds on, 10 seconds off
How long before departure is tactile inspection required?
5 minutes
Maximum time for probe heat on ground
5 minutes