Limitations Flashcards
Aircraft dimensions
Length
103’ 11” (104’)
Aircraft dimensions
Width
93’ 11” (94’) (Wingspan)
Aircraft Dimensions
Height
32’ 4” (33’)
Cabin Loading
Max Pax
76
Cabin loading
First
12
Cabin Loading
Coach
64
Cargo Compartment Max Weight
FWD
3307 lbs
Cargo Compartment Max Weight Limits
AFT
2535 lbs
Aircraft Weights
MRW
85,800 lbs
Aircraft weights
MTOW
85,500 lbs
Aircraft weights
MLW
74,900 lbs
Aircraft Weights
MZFW
69,800 lbs
Minimum Crew
Left seat pilot and Right seat pilot (Captain & First Officer)
Aircraft Operations (5)
- Day & Night
- VFR & IFR
- Icing Conditions
- CAT I & CAT II
- RVSM
Max Cabin Differential Overpressure (Safety Valve)
8.8 PSI
Max Cabin Differential Pressure
Above FL370
8.4 PSI
Max Cabin Differential Pressure
T/O & Landing
0.2 PSI
Max negative Cabin Differential Pressure
-0.5 PSI
Max Altitude Depressurized
10,000’ or MEA whichever is Higher
Max Altitude for Single Pack Operation
31,000
Airspeed
MMO Above FL280
0.82M
Airspeed
VMO 10,000’ to FL280
320 KIAS
Airspeed
VMO Below 10,000’
250 KIAS*
- *FAA Regulatory Speed
- Structural Speed Limit 300 KIAS
Airspeed
VA
240 KIAS
Airspeed
VLE
250 KIAS
Airspeed
VLO
250 KIAS
Airspeed
VLR
250 KIAS
Airspeed
VFE1
230 KIAS
Airspeed
FE2
215 KIAS
Airspeed
VFE3
200 KIAS
Airspeed
VFE4
180 KIAS
Airspeed
VFE5
180 KIAS
Airspeed
VFEFULL
165 KIAS
Max Turbulent Airspeed
Below 10,000’
250 KIAS
Max Turbulent Airspeed
10,000’ and Above
270 KIAS or .76M
Max Crosswind for Takeoff
(Dry)
35 kts
Max Crosswind for Takeoff
(Wet)
30 kts
Max Crosswinds for landing
See AOM 1 Limitations
Max Tailwind
10 KT
Max Headwind for CAT II Operations
25 KT
Max Crosswind for Landing
< RVR 4000 or 3/4
15 KT
Max DV (Direct View)Window Operation
160 KIAS
Max Tire Speed
195 KIAS
Max Windshield Wiper Speed
250 KIAS
Max Operating Altitude
41,000’
Max Flaps Extended Altitude
20,000’
Max Takeoff & Landing Altitude
10,000’
Min Takeoff & Landing Altitude
-1,000’
Minimum and Maximum Takeoff & Landing Temperature (SAT)
— 40 degrees C to 54 degrees C
Note: in the event of a landing below - 40 degrees C, takeoff not authorized without further maintenance inspection
Max Altitude Display Difference in flight for RVSM
180 ft
APU
First & Second Start Attempts
START/ON then 60 sec OFF
APU
Third Start Attempt
START/ON then 5 min OFF
APU Brand Name
Sunstrand APS 2300
APU
Minimum Starting Temperature
-54 degrees C
APU
Maximum Operation Temperature
ISA + 39 degrees C
Supplemental information applicable > ISA + 35 degrees C
APU
EGT (Start) temperature
1032 degrees C
APU EGT (Continuous) temperature
717 degrees C
No time limit in Amber on ground/inflight between 662-717 degrees C
APU
Max Rotor Speed
108%
APU
Max starting altitude ___________ ft
Max Electrical Altitude __________ ft
30,000’
33,000’
APU
Max ENG Start Assist Altitude
21,000’
APU
Max ECS Bleed Altitude
15,000’
Autopilot
Min Engagement Altitude on Takeoff or Go Around
Above 400’
Autopilot
Min Engaged Altitude during Landing
Above 50’
Engine Type
GE CF34-8E5
Engine Max N1 RPM
99.5%
Engine Max N2 RPM
99.4%
Engine Max Start ITT
815 degrees C
Engine max normal T/O ITT
2 minutes at 965 degrees
3 minutes at 949 degrees [Total 5 min]
Engine max T/O ITT
Engine max G/A ITT
2 minutes at 1006 degrees C
3 minutes at 990 degrees C [Total 5 min]
Engine Max Continuous ITT
960 degrees C
Engine Min/Max Oil Pressure
25 PSI - 95 PSI
Engine Continuous Oil Temperature
155 degrees C
Engine Transient Oil Temperature
163 degrees C (15 min limit)
Engine Thrust
T/O-1
13,000 lbs / OEI ATTCS = 14,200 lbs
Engine Thrust
T/O-2
11,800 lbs / OEI ATTCS = 13,000 lbs
Brazilian Fuel type
QAV1
ASTM fuel type
Jet A or A1
American military Fuel Type
JP8
Fuel Capacity
20,934 lbs (10,467 lbs / tank)
Useable fuel
20,784 lbs (10,392 lbs/tank)
Unusable Fuel
150 lbs (75 lbs/tank)
Imbalance fuel
794 lbs
Min fuel tank temp
-37 degrees C
Fuel Crossfeed Operation must be ______ for takeoff and landing
OFF
Engine 1st & 2nd Starter Time GND
90 sec START / 10 Sec cool down
Engine 1st & 2nd Starter time FLT
120 sec START / 10 sec cool down
Engine 3rd-5th Starter time GND
90 sec START / 5 min cool down
Engine 3rd-5th Starter time FLT
120 sec START / 5 min cool down
1st Dry Motor Starter Time
Max 90 sec followed by 5 min cool down
2nd-5th Dry Motor Starter Time
Max 30 sec followed by 5 min cool down
Note: after 5 sequential Dry Motoring Cycles, the sequence may be repeated following a 15 min cool down period
