Limitations 200

Question 0

Why 2 minute delay observed between APU cranking attempts

Answer 0

Allow for the starter and starter contactor cooling and fuel drainage

Question 1

Min fuel for go-around

Basic fueling policy

Answer 1

450lbs per side (900lbs)

Question 2

If both engines are to be started using the APU bleed air

Answer 2

The operating engines thrust must not exceed 70% N2

Question 3

When must the wing anti-ice be turned on (200 only)

Answer 3

2 minutes prior to T/O during all ground ops 5c OAT or below unless type III or type IV anti-icing fluid has been applied

Question 4

APU Start cycle (DC Ground Power)

Answer 4

15 seconds…..2 minutes off
15 seconds…..20 minutes off
15 seconds…..2 minutes off
15 seconds…..40 minutes off

Question 5

AC Generator loading values

Answer 5

Main GEN - 30kVA up to FL 350
25 kVA from FL 350-360
APU GEN - 30 kVA all altitudes

Question 6

Oil Pressure Limits

Answer 6

Idle          25psi
Takeoff     45psi
Max continuous 115psi
Transient        - (200) 
Max transient after cold start (10 min)
156psi,  130 psi at idle (200)

Question 7

Max altitude for engine start with APU bleed air

Answer 7

13,000’

Question 8

N2 split at ground idle power

Answer 8

Not greater than 2% N2

Question 9

Starter cranking limits (200)

Answer 9

1 min……..10 secs off
1 min……..10 secs off
1 min……..5 minutes off
The starter must not be engaged if indicated N2 RPM exceeds 55%:

Question 10

Flaps Vfe

Answer 10

8 - 230 KIAS
20 - 230 KIAS
30 -185 KIAS
45 -170 KIAS

Question 11

Flaps Vfo

Answer 11

8 - 200 KIAS
20 - 200 KIAS
30 - 185 KIAS
45 - 170 KIAS

Question 12

Hydraulic 3b pump

Answer 12

Must be on instead of Auto from the before start checklist until the shutdown checklist

Question 13

Min fuel for T/O when with a T/O alternate

What configuration was used to compute the fuel?

Answer 13

4,600 lbs
• A/C weight - 52,000 lbs
• Altitude - 10,000 feet
• Speed - 200 kts IAS
• Flaps - 20 degrees
• Single Engine
fuel burn of 3,510 lbs/hr. rounding up and adding 1,000 per the AD 2007-17-07

Question 14

Max cruise in RVSM

Answer 14

.83M

Question 15

T/O with fuel load in excess of_____in the center tank is not permitted unless each wing tank is above______

Answer 15

500lbs

4,400lbs

Question 16

APU Door not closed or position unknown

Answer 16

300 KIAS

And APU must remain in operation

Question 17

Cargo in cargo compartment

Answer 17

Flight must be within 45 min of suitable airport

300 nautical miles

Question 18

APU Start cycles (Battery)

Answer 18

30 seconds…..2 minutes off
30 seconds…..20 minutes off
30 seconds…..2 minutes off
30 seconds…..40 minutes off

Question 19

Oil Temp Limitations

Answer 19

Min Start -40c
Max Continuos +155c
Max Permissible +163c ( for 15 min)

Question 20

Max Ramp Weight

Answer 20

53,250 lbs.

Question 21

Max T/O Weight

Answer 21

53,00 lbs.

Question 22

Max Landing Weight

Answer 22

47,00 lbs.

Question 23

Max Zero Fuel Weight

Answer 23

44,000 lbs.

Question 24

Minimum operating weight

Answer 24

25,480 lbs.

Question 25

Max weight in cargo compartment

Answer 25

3,500 lbs.

Question 26

Maximum airspeed for windshield wiper operation failed in the non-parked position

Answer 26

220 KIAS

Question 27

Landing on contaminated runways is prohibited when (200)

Answer 27

• Standing water >0.75
• Slush >0.88
• Wet snow >1.5
• Dry snow >3.75
• Crosswind or tailwind component exceeds the guidelines for braking action in 3.7 Braking Action Takeoff & Landing
Wind Component Guidelines

Question 28

Takeoff on Contaminated Runways 
prohibited when (200)

Answer 28

• Standing water >0.5
• Slush >0.5
• Wet snow >1.0
• Dry snow >3.0
• Crosswind or tailwind component exceeds the guidelines for braking action in 3.7 Braking Action Takeoff & Landing WindComponent Guidelines

Question 29

Engine Type

Answer 29

GE CF34-3B1

Question 31

Airplane Cold Soak

Answer 31

• -30 for more than 8 hrs before first flight
• The engines must be motored for 60 seconds and fan rotation must be verified before an engine start is initiated
• Thrust reversers must be actuated until the deploy and stow cycles are less than 5 seconds

Question 32

Automatic Performance Reserve (APR)

Answer 32

If takeoff performance is predicated upon the use of APR, the APR system must be verified operative prior to takeoff.
The APR system must be selected OFF if an APR INOP Amber Caution message is displayed on EICAS.
APR OFF performance must be used if an APR INOP Amber Caution message is displayed.

Question 33

Engine start during flight Using APU Bleed Air

Answer 33

During single-engine operations, APU bleed air extraction for an engine start is not permitted.
During double-engine failure conditions, APU bleed air extraction for engine starts is permitted.
However, APU bleed air extraction is limited to 13,000 ft. and below.

Question 34

Maximum operating altitude

Answer 34

36,000 ft

Question 35

Maximum Starting Altitude for APU

Max Operating Altitude for APU

Answer 35

• 30,000 ft

* 36,000 ft

Question 36

When can the flaps not be extended (200)

Answer 36

• The visibility will remain above the visibility required for the approach in use (precision)
• The visibility and ceiling will remain above that required for the approach in use (non-precision)
• An emergency condition exists

Question 37

Minimum Operating Weight Empty

Answer 37

25,480 lbs.

Question 38

Fuel imbalance

Answer 38

Takeoff 800 lbs

All other Phases of flight 800lbs

Question 39

Max N1

Answer 39

98.6%