Limitations Flashcards
Max Ramp Weight
30,550
Max T/O Weight
30,300
Min Runway Length / Width
Min. Dry Length 4000’
Min. Width 70’
Ops review:
Dry < 4500’
Wet/Contam. < 5000’
DAAP < 4500’
Max Crosswind
Dry or Wet:
Contaminated:
Dry or Wet (T/O or Landing):
25 kts
Contaminated:
150ft wide or greater
15kts
149ft or less
10kts
Max Tailwind
10 kts
Max operating Altitude
FL470
Min Speedbrake Extension Alt.
500’ AGL
Vmo
8000’ or above:
Below 8000’:
8000’ or above
305 kts
Below 8000’
270 kts
Mmo
.80M
Vra
225 / .73M
Vlo (EXT or RET)
210 kts
Vfe
7*
15*
35*
7* 250 kts
15* 200 kts
35* 175 kts
Min Holding Airpseed in Icing
180 kts
APU Starter Limits
3 start attempts in a 30min period
90sec cooling between attempts
1 APU start following dual Gen failure
Do not restart APU until 30sec after APU RPM is at 0%
Max airspeed for APU Start
250 kts
Max Altitude for APU start
FL200
Max Airpseed with APU Operating
305 kts / .80M
Max Altitude with APU Operating
FL300
Autopilot Min Altitude
T/O, Climb, or Missed Approach
400’ AGL
Autopilot Min Altitude
Enroute or Descent
1000’ AGL
Autopilot Min Altitude
Precision Approach
80’ AGL
Autopilot Min Altitude
Non-Precision Approach
200’ AGL
Min Voltage for Engine Battery Start
24V
Max GPU Voltage for Battery Charging
28V
Max Fuel Quantity
11,200 lbs
Max Fuel Imbalance
Normal:
Above FL300:
Single Engine:
Normal: 400 lbs
Above FL300: 200 lbs
Single Engine: 200lbs
Aircraft Approach Category
Cat. B (120kts or less)
If approach speed is faster than 120kts use Cat. C
Max time for Engines at TO thrust
Normal:
Single Engine:
Normal: 5 min.
Single Engine: 10min.
Max Continuous Thrust (MCT) limited to
10min. when in Level Flight
CRU must be set 10min after Level Off
Time limit for Reverse Thrust
5min
30sec with APU operating
Transient Engine limitations
N1:
N2:
ITT:
N1: 106
N2: 106
ITT: 950
Time limit for each is 20sec.
Transient Oil pressure Limitation
0-20psi for 20sec
Engine Starter Limitations
1st start attempt 2min cooling
2nd attempt 5min cooling
3rd attempt 30min cooling
Limitations are independent of power source and applies to Dry or Wet motoring
Engine Motoring Limitations
Batteries Only:
Batt. with GEN assist:
GPU 1000A:
GPU 1500A:
Batteries Only: 20sec.
Batteries with GEN assist: 15sec.
GPU 1000A: 15sec.
GPU 1500A: 7sec.
MAX Baggage Compartment Weight
1,000 LBS
MAX Landing Weight
27,100
Ground Ops >47*C and No A/C, EICAS and Avionics Limited To
30min
WING ANTI-ICE Must be OFF for Operations Above:
FL410
ENGINE/STAB ANTI-ICE Must Be ON When In Visible Moisture and Temperatures Between
10C to -35C
WING ANTI-ICE Must Be ON When In Visible Moisture and Temperatures Between
5C to -35C
MIN Oil Temp For Start
-40*C
MIN Oil Temp For T/O
16*C
On the Ground PITOT HEAT Limited to
2min
L and R AVN - OFF
for Engine Start When
Battery Power Only
or
OAT below 0*C
Battery AMP Limit for Engine Start
100A
Battery AMP Limit for T/O
20A
With a cold soaked cabin, warm cabin to:
15*C before flight above FL250
Reserve Fuel
1464
AUX Hydraulic pump prohibited
Inflight
Or
-40*C or below on the ground
MIN fuel for dispatch
2564
MIN speed for Speed Brakes
Vref +15
TRs must be IDLE by
65kts
With APU MAX COOL ON
CABIN and CKPT TEMP SEL must be in AUTO
After MAX COOL is selected OFF, do not select Manual Temp for
30sec
Batteries Only Engine Start limits
3 Battery Starts per hour
A start with any GEN, or GPU 1000A or greater, 1 start only counts 1/3 towards your 3 per hour.
TR checks required
First flight of the day
Any maintenance is performed
Performance is predicated on their use
LAV pocket door must be Open for
T/O and Landing
Will get LAV DOOR CAS if door is not open with flaps or gear down
