Limitations Flashcards
Max Takeoff Weight
85,517lbs
Max Landing weight
74,957lbs
Max Zero fuel weight
69,886lbs
Max Aft Cargo
2,535lbs
Max Forward Cargo
3,306lbs
Minimum runway width
100 Feet (SW)
Wing Span
93ft 11in
Aircraft length
103ft 11in
Tail Hieght
32ft 4in
Max Operation Altitude
41,000ft
Max Takeoff and landing altitude
8,000ft
Max temp takeoff and landing
ISA +35•C (52•C)
Min temp takeoff and landing
-40•C
Runway Slope
+/- 2%
Max Tailwind
15kt
Max single pack operation
31,000ft
VMO SL-8,000’
300
VMO SL-10,000’- Mach Transition
320
MMO
.82
VA
240
VLO EXT
250
VLE RET
250
VLE
250
V Tire
195
V RAT Deploy Max
VMO/MMO
Vmin (to provide electrical power)
130
Vb (below 10,000ft)
250
Vb (10,000ft and above)
270/.76m (whichever is lower)
Vwiper operation max
250 (SW)
Vwindow
160
VFE 1
230
VFE 2
215
VFE 3
200
VFE 4
180
VFE 5
180
Flaps Full
165
Dry Runway Croswind
38kt
Wet Runway Crosswind
31kt
Runway with compact snow crosswind
20kt
Runway with standing water, slush, wet snow, dry snow crosswind
18kt
Runway with ice crosswind
12kt
Max altitude flaps/ slats extended
20,000ft
Enroute operation slats/ flaps
Prohibited
Minimum spoiler speed
180kt
Cat II approach slats/ flaps
What setting?
Mandatory flaps 5
Go Around
Landing Flaps Full
Go around flaps 4
Go Around
Landing flaps 5
Go around flaps 2
Battery minimum voltage
22.5v
Engine start temp limit max
815c
Oil temp start temp minimum
-40c
Oil pressure start minimum
25psi
Engine start ground cranking limits
Starts 1-2
-90 sec on/ 10 sec off
Starts 3-5
-90 sec on/ 5 min off
Starter cranking limits engines (in flight)
Starts 1-2
-120 sec on/ 10 sec off
Starts 3-5
-120 sec on/ 5 min off
Dry motoring limits
Motor 1
-90 sec on/ 5 min off
Motor 2-5
-30 sec on/ 5 min off
After 5 cycles the process may be repeated after 15 minutes
No N1 % increase manual abort (ground start)
50% N2
Fuel capacity total
20,935lbs
Max fuel imbalance
794lbs
Minimum fuel tank temp
-37c
Wait 30 seconds after the EICAS is energized to start the APU
True
Simultaneous use of the APU bleed and the HP cart is prohibited
True
APU Starter duty cycles
Attempt 1-2
60 sec off
Attempt 3
5 min off
APU start temperature min/max
-54c/ ISA + 35
APU max start altitude
30,000 ft
APU continuous operation min/ max temps
-54c / ISA + 35 (52c)
APU operation Max altitude
33,000 ft
APU GEN use Max altitude
33,000 ft
APU Max altitude bleed use
15,000 ft
APU Max altitude engine start
21,000 ft
Max differential pressure up to FL370
7.8psi
Max differential pressure above FL370
8.34psi
Max differential over pressure
8.77psi
Max differential negative pressure
-0.5psi
Max differential pressure takeoff and landing
0.2 psi
Min reservoir temp for engine start (hydraulics)
-18c
Autopilot minimum engagement height
400ft
Autopilot minimum use height
50ft
Autopilot minimum use height on a non precision approach
MDA
Between 5-10c the MCDU dataset menu must be set to ENG when visible moisture will be encountered up to 1,700 ft or on the ground at all.
True
The MCDU data set menu must be set to ALL if the OAT is less than 5c. Moisture below 1,700ft or on the ground at all
True
Max Ramp Weight
85,870lbs
LL Max Ramp Weight
85,450
LL Max T/O Weight
85,098
LL Max Landing Weight
74,957
LL Max Zero Fuel Weight
69,467
