Max design ramp weight

30,550 lbs

Max design takeoff weight

30,300 Lbs

Max design landing weight

27,100 Lbs

 Max design zero fuel weight

20,800 Lbs

MMO

Mach .80

VMO above 8,000 feet

305 Kts

VMO below 8,000 feet

270 Kts

VFE 7 degrees

250 Kts

VFE 15 degrees

200 Kts

VFE 35 degrees

175 Kts

VLE/VLO

210 Kts

Max turbulent air penetration

225 Kts/ .80M

Max speedbrakes extension

No limit

Minimum airspeed

speedbrakes extension

Vref + 15 Kts

Minimum SE enroute climb

180 Kts

Max tire groundspeed

165 Kts

Minimum speed in icing

180 Kts

Max altitude limit for

takeoff and landing

14,000 feet

Max tailwing component

10 Kts

Max X-wind component

25 Kts

Altitude where the speedbrakes

must be retracted

500 feet

Max altitude limit

47,000 feet

Max altitude with flaps extended

18,000 feet

What position must the pressure source knob be above FL 410?

Norm

Maximum baggage weight

1,000 lbs

The engine didn't start.

How long must you wait

to rest the starter?

2 minutes

The engine didn't start for the

second time now. How long

must you wait before using

the starter again?

5 minutes

The engine didn't start for the

third time now. how long

must you wait before using

the starter again?

30 minutes

How long can you motor

the engine using the

batteries only?

20 seconds

How long can you motor the engine using the batteries with generator assist?

15 seconds

How long can you motor

the engine using a GPU?

1000 amps: 15 seconds

1500 amps: 7 seconds

What is the APU starter

limitation?

3 start cycles per 30 minutes

with a 90 seconds rest between cycles

What is the battery

start limitation?

3 engine starts/hr

Max current GPU

1500 amps

Max voltage GPU

28 V

Max engine generator limit

300 amps

275 amps if above FL350

Max engine generator limit

above FL 350

275 amps

Max APU amps limit

275 amps

Max battery temperature

63 C

Max start ITT

950 C

Max ITT other than start

920 C

Max tailwind for engine start

10 Kts

How long can you keep the engines at T/O thrust on the ground?

2 minutes

How long can you keep

the throttles at T/O power

in flight?

5 minutes

How long can you keep the throttle to T/O power in single engine?

10 minutes

Max oil consumption

1 quart in 8 hrs

During start, when should oil pressure increase steadily?

Within 20 seconds of ITT rise

Max altitude for APU start?

FL 200

Max airspeed for APU start

250 Kts

Max altitude APU operation

FL 300

How long do you have to

wait to restart the APU,

following its shutdown?

30 seconds after RPM reads 0%

What should you do

following an automatic

shutdown of the APU?

Inspect the APU compartment

Minimum temperature for

using the auxiliary pump

- 40 C

When is checking the thrust reversers required?

a) first flight of the day

b) First flight after maintenance action

c) If performance is predicated on their use

At what speed should the thrust reversers

be idle at?

65 Kts

How long can you extend

the TR's with the APU running?

30 seconds

How much thrust can you

use when the TR's are deployed in ground static operation?

Idle

What is the nose tire inflation?

120 PSI (+-5)

What is the main tire inflation?

160 PSI (+-5)

When should the engine

anti-ice selected?

in visible moisture

between +10C to -35C

When do we use SAT or RAT?

Ground: SAT

Flight: RAT

Except for preflight, what is

the max temperature for

use of the bleed air anti-ice?

+ 20C

Can you use flaps 15 in icing condition?

Other than flaps 0 is prohibited

Except takeoff, approach and landing

Max altitude to use

the wing anti-ice?

FL 410

What is a limitation

with the message

FUEL LEVEL LOW L-R?

Affected fuel boost pump must be turned ON

Max assymetrical fuel differential

Normal operation: 400 Lbs

Emergency return: 800 Lbs

What is the normal

cabin pressure limit?

9.3 PSI

What is the max PSI for the

pressure relief valve?

9.6 PSI

What is the max pressure

gauge redline?

9.7 PSI

How is Vref indicated?

a) 0.6 AOA on the gauge

b) Green caret on the airspeed indicator

What are the load factors

with the flaps up?

-1.2 to +3 G

What are the load factors

with the flaps down?

0 to + 2g

The load factors limit the aircraft

to how many FPM on landing?

600 FPM

How many BLE's and how many

can be missing?

9. None

How many static wicks

can be missing?

Two

When is it prohibited

to use the autopilot?

a) Any comparison monitor is activated

b) Either PFD is in ATT or HDG reversion

c) Either AHRS has failed

 Minimum altitude to use

the autopilot on takeoff?

400 Feet

Minimum altitude to use

the autopilot during a

precision approach?

80 feet

Minimum altitude to use

the autopilot during a

non-precision approach?

200 Ft

Autopilot minimum height

during a visual app?

1000 FT

True or false: the fuel tank temperature

indication on EICAS does monitor

for fuel temp out of limits

False

                                                  AFM, operating limitations section 2

How many static wicks can be

missing on the flight controls?

1- Never more than one (out of the 3 or 4 installed)

2- Never more than 2 total for the whole aircraft

                                              AFM, operating limitations section 2