Limitations Flashcards

(79 cards)

1
Q

MAX Ramp Weight

A

85,870 lb

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2
Q

MAX T/O Weight

A

85,517 lb

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3
Q

MAX Landing Weight

A

74,957 lbs

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4
Q

MAX Zero Fuel Weight

A

69,886 lb

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5
Q

MAX AFT Cargo

A

2,535 lb

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6
Q

MAX FWD Cargo

A

3,306 lb

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7
Q

MIN Runway Width

A

100’ (SkyWest)

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8
Q

Wing Span

A

93ft 11in

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9
Q

Aircraft Length

A

103ft 11in

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10
Q

Tail Height

A

32ft 4in

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11
Q

MAX Operational Altitude

A

41,000 ft

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12
Q

MAX T/O & Land Altitude

A

8,000 ft

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13
Q

MAX Temp T/O & LAND

A

ISA +35C

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14
Q

MIN Temp T/O & Land

A

-40C

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15
Q

Runway Slope

A

+/- 2%

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16
Q

Max Tailwind

A

15 kts

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17
Q

Max Single Pack Altitude

A

31,000 ft

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18
Q

VMO (SL - 8,000ft)

A

300 KIAS

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19
Q

VMO > 8,000 ft

A

320 KIAS

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20
Q

MMO

A

0.82

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21
Q

VA

A

240 KIAS

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22
Q

VLO/LE

A

250 KIAS

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23
Q

VTire

A

195 KIAS

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24
Q

V RAT DEPLOY MAX

A

VMO/MMO

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25
V MIN RAT
130 KIAS
26
VB \< 10,000 ft | (Turbulence Penetration Speed)
250 KIAS
27
VB \> 10,000 ft | (Turbulence Penetration Speed)
270 KIAS / 0.76M | (whichever is lower)
28
VWIPER OPS MAX
250 KIAS (SkyWest)
29
VWINDOW
160 KIAS
30
VFE 1
230 KIAS
31
VFE 2
215 KIAS
32
VFE 3
200 KIAS
33
VFE 4
180 KIAS
34
VFE 5
180 KIAS
35
VFE FULL
165 KIAS
36
MAX Crosswind Dry Runway
38 kts
37
MAX Crosswind Wet Runway
31 kts
38
MAX Crosswind Runway with Compacted Snow
20 kts
39
MAX Crosswind Runway with Standing Water/Slush/Snow
18 kts
40
MAX Crosswind Runway with Ice
12 kts
41
MAX Altitude Flaps/Slats Extended
20,000 ft
42
Minimum Spoiler Speed
180 kts
43
CAT II Approach Flaps
FLAPS 5 MANDETORY
44
Go-Around Flaps when Landing Flaps FULL
Go-Around Flaps 4
45
Go-Around Flaps when Landing Flaps 5
Go-Around Flaps 2
46
Minimum Battery Voltage
22.5 V
47
MAX Engine Start ITT
815C
48
MIN OIL TEMP START
-40C
49
MIN OIL PRESSURE START
25 psi
50
Starter Cranking Limits (Ground) Start 1 & 2 Start 3 - 5
_1 & 2_ - 90 sec ON / 10 sec OFF _3 - 5_ - 90 sec ON / 5 min OFF
51
Starter Cranking Limits (Flight) Start 1 & 2 Start 3 - 5
1 & 2 - 120 sec ON / 10 sec OFF 3 - 5 - 120 sec ON / 5 min OFF
52
Dry Motoring Duty Cycle Limits Motoring 1 Motoring 2 - 5
_1_ - 90 sec ON / 5 min OFF _2 - 5_ - 30 sec ON / 5 min OFF
53
N1 Requirement on Start
Must have N1 indication before starter cuttout (50%N2)
54
MAX Fuel Capacity
20,935 lbs
55
MAX Fuel Imbalance
794 lbs
56
MIN Fuel Tank Temp.
-40C
57
Fuel Crossfeed Must Be:
OFF during takeoffand landing
58
Wait ____ after the _____ is energized to start the APU
30 sec / EICAS
59
Unattended APU
5 min (SkyWest)
60
APU Starter Duty Cycle Start Attempt 1 & 2 Start Attept 3
60 sec OFF 5 min OFF
61
APU Min/Max Start Temp
-54C / ISA+35
62
MAX APU Start Altutude
30,000 ft
63
MAX APU Altitude
33,000 ft
64
MAX APU Generator Use
33,000 ft
65
MAX APU Bleed Use
15,000 ft
66
Max APU Engine Start Altitude
21,000 ft
67
Maximum Differential Pressure
7. 8 PSID \< 37,000 ft 8. 34 PSID \> 37,000 ft
68
OVER PRESS Relief Valve
8.77 PSID
69
NEG PRESS Relief Valve
-0.5 PSID
70
MAX DIFF PRESS T/O + LAND
0.2 PSID
71
MIN Hydraulic Resevoir Temp for ENG Start
-18 C
72
Anti-Icing MCDU - ENG
5C to 10C Visible Moisture \< 1,700 ft AFE Contaminated Ramps/Runway
73
Anti-Icing MCDU - ALL
\< 5C Visible Moisture \< 1,700 ft AFE Contaminated Ramps/Runway
74
Ice Detector Failure
Must be ON \< 10C TAT in Visible Moisture
75
Min AP Engagement Height
400 ft AGL
76
Min AP Use Height Precision/Non-Precison App
77
TAS, TAT, and SAT Valid
Above 60 kts
78
CAT 1 Appraoches Require
Baro Alt Minimums
79
IESS Prohibited
Back Course Approaches