LIMITATIONS Flashcards
1
Q
Max. T/O Wt.
A
85,517 lb
2
Q
Max. Lnd. Wt.
A
74,957 lb
3
Q
Max. Zero Fuel Wt.
A
69,886 lb
4
Q
Max. AFT Cargo
A
2,535 lb
5
Q
Max. FWD Cargo
A
3,306 lb
6
Q
Min. Runway Width
A
100’ (SW)
7
Q
Wing Span
A
93 ft 11 in.
8
Q
Aircraft Length
A
103 ft 11 in
9
Q
Tail Height
A
32 ft 4 in.
10
Q
Max. Ops. Alt.
A
41,000 ft
11
Q
Max. T/O & Lnd
A
8,000 ft
12
Q
Max. Temp. T/O Lnd
A
ISA + 35°C (52˚C)
13
Q
Min. Temp. T/O Lnd
A
-40°C
14
Q
RWY Slope
A
+/- 2%
15
Q
Max. Tailwind
A
15kts
16
Q
Max. Single Pack Operations
A
FL310
17
Q
VMO SL- 8,000’
A
300
18
Q
VMO 10,000- Mach Transition
A
320
19
Q
MMO
A
0.82M
20
Q
VA
A
240
21
Q
VLO EXT
A
250
22
Q
VLE RET
A
250
23
Q
VLE
A
250
24
Q
V Tire
A
195
25
V RAT DEPLOY MAX
VMO/MMO
26
VMIN (to provide electrical power)
130
27
VB (below 10,000 ft)
250
28
VB (10,000 ft and above)
270/.76M (whichever is lower)
29
V wiper ops max
250 (SW)
30
Vwindow
160
31
VFE 1
230
32
VFE2
215
33
VFE3
200
34
VFE4
180
35
VFE5
180
36
VFE6
165
37
MAXIMUM RECOMMENDED CROSSWIND
| DryRunway
38kts
38
MAXIMUM RECOMMENDED CROSSWIND
| WetRunway
31kts
39
MAXIMUM RECOMMENDED CROSSWIND
| Runway with Compacted Snow
20kts
40
MAXIMUM RECOMMENDED CROSSWIND
| Runway with Standing Water/Slush/WetSnow/DrySnow.
18kts
41
MAXIMUM RECOMMENDED CROSSWIND
| Runway with Ice
12kts
42
SLATS / FLAPS
| Max. Alt. Flaps/SlatsExtended
FL200
43
SLATS / FLAPS
| Enroute Ops
Prohibited
44
SLATS / FLAPS
| Min. Spoiler Speed
180kts
45
SLATS / FLAPS
| CATII Approach
Mandatory Flaps 5
46
SLATS / FLAPS
| Landing Flaps Full Go Around
Flaps 4
47
SLATS / FLAPS
| Landing Flaps 5 Go Around
Flaps 2
48
Max. Ramp Wt.
85,870 lb
49
Due to engine compressor stall possibility, static takeoff is not recommended with crosswind component greater than
30kts
50
BATTERY LIMITATIONS
| Min. voltage
22.5V
51
MAX ENGINE ITT Start
815C
52
OIL TEMP. MIN START
-40C
53
OIL PRESSURE MIN Start
25psi
54
STARTER CRANKING LIMITS
Engine Start (Ground)
1 & 2
90 Seconds ON 10 Seconds OFF
55
STARTER CRANKING LIMITS
Engine Start (Ground)
3&4
90 Seconds ON 5 Minutes OFF
56
STARTER CRANKING LIMITS
Engine Start (In Flight)
1 & 2
120 Seconds ON 10 Seconds OFF
57
STARTER CRANKING LIMITS
Engine Start (In Flight)
3&5
120 Seconds ON 5 Minutes OFF
58
DRY MOTORING DUTY CYCLE LIMITS
Motoring #
1
90 Seconds ON 5 Minutes OFF
59
DRY MOTORING DUTY CYCLE LIMITS
Motoring #
2-5
30 Seconds ON 5 Minutes OFF
60
Max. Fuel Capacity
20,935 lb
61
Max. Imbalance
794lbs
62
Min. Fuel Tank Temp.
-40C
63
ItispermissibletotakeoffandlandwithaFUELIMBALANCEmessage as long as the actual imbalance does not exceed
794lbs
64
Fuel crossfeed must be selected OFF during
takeoff and landing
65
APU OPERATIONAL LIMITS
| Max Operation Altitude
FL330
66
APU OPERATIONAL LIMITS
| START Altitude
FL300
67
APU OPERATIONAL LIMITS
| Electrical Generator Use
FL330
68
APU OPERATIONAL LIMITS
| Altitude Bleed Use
15000
69
APU OPERATIONAL LIMITS
| Altitude Engine Start
FL210
70
Maximum Differential Pressure
| Up to 37,000 ft
7.8 psi
71
Maximum Differential Pressure
| Above 37,000 ft
8.34 psi
72
Maximum Differential Pressure
| Max. Diff. Over Pressure
8.77 psi
73
Maximum Differential Pressure
| Max. Diff. Neg. Press
-0.5 psi
74
Maximum Differential Pressure
| Max. Diff. Press T/O Lnd
0.2 psi
75
HYDRAULIC TEMPERATURE
| Min. Reservoir Temp. for ENG Start
-18°C
76
Use of the autopilot below the altitudes listed is prohibited.
Min. Engagement Height
400 ft AGL
77
Use of the autopilot below the altitudes listed is prohibited.
Min. Use Height
50ft AGL
78
Use of the autopilot below the altitudes listed is prohibited.
Min. Use Height - Non-precision Approach
MDA
79
TAS, TAT, and SAT information are only valid above
60kts
80
FMS LIMITATION
| RNP instrument approaches are
not authorized (SW
81
FMS LIMITATION
| The use of FMS Speed Mode is
prohibited in the event of an engine failure.
