Limitations Flashcards
0
Q
Max takeoff
A
21,500
1
Q
Max ramp
A
21,750
2
Q
Max zero fuel
A
16,500
3
Q
Min flight weight
A
14,000
4
Q
Max landing weight
A
19,200
5
Q
Max baggage compartment
A
500
6
Q
Vmo
A
330
7
Q
Mmo with mach trim operative and AP disengaged
A
.81
8
Q
Mmo with mach trim inop and AP engaged
A
.81
9
Q
Mmo with mach trim inop and AP disengaged
A
23,400-42,000 ft .76-.78
>42,000 .78
10
Q
Vmo/Mmo standby instruments
A
325/.75
11
Q
Turbulence penetration speed
A
250/.73
12
Q
Demonstrated crosswind
A
22
13
Q
Tire limit speed
A
165
14
Q
Vlo
A
200
15
Q
Vle
A
260
16
Q
Vfe 8
A
250
17
Q
Vfe 20
A
200
18
Q
Vfe 40
A
150
19
Q
Vmca flaps 8
A
103
20
Q
Vmca flaps 20
A
101
21
Q
Vmcg APR on
A
102
22
Q
Vmcg APR off
A
100
23
Q
Vmcl flaps 8
A
105
24
Vmcl flaps 40
98
25
Load factor flaps up
2.9 to -1.0
26
Load factor flaps down
2.0 to 0.0
27
No intentional stalls, gear or flap extension above
18,000
28
Max pressure altitude for takeoff
14,000
29
Tailwind component
10
0 above 12,000
30
Runway type
Paved
31
Water depth
3/4 inch or less ( refer to poh for lesser takeoff depths)
32
External power limit
1500
33
ADC/AHRS setting for takeoff
NORM
34
EICAS or MFD set to what for takeoff
SUMRY or FLT
35
Min turn around time
15 min between touchdown and takeoff thrust
36
APU altitude limit
10,000 ft
37
APU gen limit
300 amps
38
APU OFF when:
Gravity fueling, deice operations
39
Can you takeoff with APU FAIL CAS
No
40
APU starter limits
1 min, 2 min, 15 min
41
Rudder boost for takeoff
Must be ON
42
Max pressure altitude
51,000
43
Ground temperature limits for aircraft and components
- 23 or above for aircraft and components
| - 15 or above for cabin
44
Spoilers and flaps limitation
Never in flight unless specified by emergency or abnormal checklist
45
Auto spoilers armed for
Takeoff and landing
46
Engine sync limitations
Must be OFF for takeoff, landing, and SE operations
47
Generator limits
300 amps
48
Starter/Generator limits
1 min, 2 min, 30 min
49
APR/Takeoff power limit
5 min
50
Thrust reverser limits
max reverse usable down to 40 KIAS
limited to idle thrust with engine manual mode
51
Fuel capacity
Left 1678 Right 1676 Fuselage 2708 Total 6292 Usable 6062
52
Max fuel imbalance
200
53
Max differential
9.9 to -0.5 psi
54
HI FLOW limitations
OFF with takeoff power, landing, anti ice operations, and flight above FL300
55
Cabin 8,750
single chime, master caution, CABIN ALT CAS, CAB ALT flashes on pressurization panel, amber box around cabin alt on EICAS
56
Cabin 9,500
single chime, master caution, LR EMER PRESS ON CAS, EMER PRESS switch ON, CAB ALT flashes on pressurization panel
57
Cabin 10,000
Triple chime, master warning, CABIN ALTITUDE aural, CAB ALT flashes on pressurization panel, red box around cabin alt on EICAS
58
Cabin 13,700
Both outflow valves close
59
Cabin 14,500
Single chime, master caution, PAX OXY DEPLOY CAS, pax masks drop, emergency lights activate
60
Minimum in flight temperature
-73
61
Yaw damper
Off for takeoff and landing
62
Min autopilot engage height
500 AGL
63
Lowest autopilot use height VNAV, LNAV/VNAV, LPV
200 LPV
300 LNAV/VNAV or MDA whichever higher
400 LNAV or MDA whichever higher
64
Hydraulic fluid type
MIL-H-5606
65
Crew and pax masks
Not approved for use above 40,000 ft cabin altitude
