Limitations 200 Flashcards
This flashcard deck was created using Flashcardlet's card creator
Why 2 minute delay observed between APU cranking attempts
Allow for the starter and starter contactor cooling and fuel drainage
Min fuel for go-around
Basic fueling policy
450lbs per side (900lbs)
If both engines are to be started using the APU bleed air
The operating engines thrust must not exceed 70% N2
When must the wing anti-ice be turned on (200 only)
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
APU Start cycle (DC Ground Power)
15 seconds…..2 minutes off
15 seconds…..20 minutes off
15 seconds…..2 minutes off
15 seconds…..40 minutes off
AC Generator loading values
Main GEN - 30kVA up to FL 350
25 kVA from FL 350-360
APU GEN - 30 kVA all altitudes
Oil Pressure Limits
Idle 25psi Takeoff 45psi Max continuous 115psi Transient - (200) Max transient after cold start (10 min) 156psi, 130 psi at idle (200)
Max altitude for engine start with APU bleed air
13,000’
N2 split at ground idle power
Not greater than 2% N2
Starter cranking limits (200)
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%:
Flaps Vfe
8 - 230 KIAS
20 - 230 KIAS
30 -185 KIAS
45 -170 KIAS
Flaps Vfo
8 - 200 KIAS
20 - 200 KIAS
30 - 185 KIAS
45 - 170 KIAS
Hydraulic 3b pump
Must be on instead of Auto from the before start checklist until the shutdown checklist
Min fuel for T/O when with a T/O alternate
What configuration was used to compute the fuel?
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
Max cruise in RVSM
.83M
T/O with fuel load in excess of_____in the center tank is not permitted unless each wing tank is above______
500lbs
4,400lbs
APU Door not closed or position unknown
300 KIAS
And APU must remain in operation
Cargo in cargo compartment
Flight must be within 45 min of suitable airport
300 nautical miles
APU Start cycles (Battery)
30 seconds…..2 minutes off
30 seconds…..20 minutes off
30 seconds…..2 minutes off
30 seconds…..40 minutes off
Oil Temp Limitations
Min Start -40c
Max Continuos +155c
Max Permissible +163c ( for 15 min)
Max Ramp Weight
53,250 lbs.
Max T/O Weight
53,00 lbs.
Max Landing Weight
47,00 lbs.
Max Zero Fuel Weight
44,000 lbs.
Minimum operating weight
25,480 lbs.
Max weight in cargo compartment
3,500 lbs.
Maximum airspeed for windshield wiper operation failed in the non-parked position
220 KIAS
Landing on contaminated runways is prohibited when (200)
• 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
Takeoff on Contaminated Runways prohibited when (200)
- 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
Engine Type
GE CF34-3B1
Airplane Cold Soak
- -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
Automatic Performance Reserve (APR)
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.
Engine start during flight Using APU Bleed Air
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.
Maximum operating altitude
36,000 ft
Maximum Starting Altitude for APU
Max Operating Altitude for APU
- 30,000 ft
* 36,000 ft
When can the flaps not be extended (200)
- 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
Minimum Operating Weight Empty
25,480 lbs.
Fuel imbalance
Takeoff 800 lbs
All other Phases of flight 800lbs
Max N1
98.6%
