Ye Ole Limits and Mems (Updated '19CQ) Flashcards
(119 cards)
1
Q
ENGINE ABNORMAL START
A
AFFECTED ENGINE»_space;> START/STOP SELECTOR = STOP
2
Q
CABIN ALTITUDE HI
or
SMOKE/FIRE/FUMES
A
OXYGEN MASKS»_space;> DON, 100%
CREW COMMUNICATION»_space;> ESTABLISH
3
Q
SMOKE EVACUATION
A
OXYGEN MASKS»> DON, EMERG
CREW COMMUNICATION»_space;> ESTABLISH
PRESSURIZATION DUMP»_space;> PUSH IN
4
Q
BATT 1 (2) OVERTEMP
A
ASSOCIATED BATTERY»_space;> OFF
5
Q
JAMMED CONTROL COLUMN - PITCH
A
ELEVATOR DISCONNECT HANDLE»_space;> PULL
6
Q
JAMMED CONTROL COLUMN - ROLL
A
AILERON DISCONNECT HANDLE»_space;> PULL
7
Q
PITCH TRIM RUNAWAY
A
A/P DISCONNECT BUTTON»_space;> PRESS AND HOLD
PITCH TRIM SYS 1and2 CUTOUT BUTTONS»_space;> PUSH IN
8
Q
ROLL (YAW) TRIM RUNAWAY
A
A/P DISCONNECT BUTTON»_space;> PRESS AND HOLD
9
Q
STEERING RUNAWAY
A
STEER DISC SWITCH»_space;> PRESS
Steer airplane using differential braking and rudder.
10
Q
MTW (LR)
A
85,870 lb.
11
Q
MTOW (LR)
A
85,517 lb.
12
Q
MLW (LR and LL)
A
74,957 lb.
13
Q
MZFW (LR)
A
69,886 lb.
14
Q
Minimum Runway Width
A
100 ft (SW)
15
Q
Wing Span
A
93 ft 11 in
16
Q
Length
A
103 ft 11 in
17
Q
Tail Height
A
32 ft 4 in
18
Q
Max Ops Altitude
A
41,000 ft
19
Q
Max Takeoff/Landing Altitude
A
8,000 ft
20
Q
Max Temp Takeoff/Landing
A
ISA + 35C (52C)
21
Q
Min Temp Takeoff/Landing
A
-40C
22
Q
Runway Slope
A
+/- 2%
23
Q
Max Tailwind
A
15 kt
24
Q
Max Single Pack Ops
A
31,000 ft
25
MMO
0.82
26
VMO SL to 8,000'
300
27
VMO 10,000' to Mach Transition
320
28
VA
240
29
VLOext / VLEret / VLE
250
30
VTIRE
195
31
VRAT Deploy Max
VMO/MMO
32
VMIN (to supply electrical power)
130
33
VB (<10,000')
250
34
VB (>10,000')
270 / .76M (whichever is lower)
35
V wiper ops max
250 (SW)
36
Vwindow
160
37
VFE 1
230
38
VFE 2
215
39
VFE 3
200
40
VFE 4
180
41
VFE 5
180
42
FULL flaps
165
43
Dry Runway Max Crosswind (Rec'd)
38 kt
44
Wet Runway Max Crosswind (Rec'd)
31 kt
45
Compact Snow Runway Max Crosswind (Rec'd)
20 kt
46
Standing Water/Slush/WetSnow/DrySnow Runway Max Crosswind (Rec'd)
18 kt
47
Icy Runway Max Crosswind (Rec'd)
12 kt
48
Due to engine compressor stall possibility, static takeoff is not recommended with crosswind component greater than...
30 kt
49
Max Altitude Flaps/Slats Extended
20,000 ft
50
Flaps/Slats Enroute Operations
Prohibited
51
Minimum Spoiler Speed
180
52
CAT II Approach Flap Setting
Mandatory Flaps 5
53
Landing Flaps Full, G/A Flaps =
Flaps 4
54
Landing Flaps 5, G/A Flaps =
Flaps 2
55
Battery Min Voltage
22.5 V
56
Engine Start Max Temp Max
815C
57
Engine Start Oil Temp Min
-40C
58
Engine Start Oil Pressure Min
25 psi
59
Engine Start Ground, First and Second Attempt
90 seconds ON, 10 seconds OFF
60
Engine Start Ground, Third, Fourth, Fifth Attempts
90 seconds ON, 5 minutes OFF
61
Engine Start Flight, First and Second Attempt
120 seconds ON, 10 seconds OFF
62
Engine Start Flight, Third, Fourth, Fifth Attempts
120 seconds ON, 5 minutes OFF
63
Ground start max cumulative starter run time (motoring plus start time)
90 seconds
64
Flight start max cumulative starter run time (motoring plus start time)
120 seconds
65
Dry motor first attempt
90 seconds ON, 5 minutes OFF
66
Dry motor attempts 2 thru 5
30 seconds ON, 5 minutes OFF
67
Dry motor after 5th attempt?
You can try #6 after you wait 15 minutes.
68
Tailwind start
No positive increase in N1 before starter cutout (50% N2) then the engine start must be manually aborted.
69
Can you takeoff with Automatic Takeoff Thrust Control System OFF?
No.
70
Max Fuel Capacity (JET A / A1)
20,935 lb
71
Max Fuel Imbalance
794 lb
72
Mun Fuel Tank Temp
-40C
73
Fuel crossfeed must be selected _____ during takeoff and landing.
OFF
74
Wait _____ seconds after EICAS is energized to start the APU.
30 seconds
75
Do not leave the airplane unattended more than ____ minutes with the APU running. (SW)
5 minutes
76
Simultaneous use of the APU bleed and HP cart is _____ .
PROHIBITED
77
APU Start Attempt 1 & 2.
60 seconds
78
APU Start Attempt #3...
5 minutes OFF
79
APU Min Start Temp
-54C
80
APU Max Start Temp / Continuous Ops
ISA +35C (52C)
81
APU Max Start Altitude / Continuous Ops
30,000 ft
82
APU Max Altitude Use / Electrical Gen Use
33,000 ft
83
APU Max Altitude Engine Start
21,000 ft
84
APU Max Bleed Altitude Use
15,000 ft
85
Max DeltaP <37,000 ft
7.8 psi
86
Max DeltaP >37,000 ft
8.4 psi
87
Max DeltaP Over Pressure
8.8 psi
88
Max DeltaP Negative Pressure
-0.5 psi
89
Max Pressure Differential Takeoff/Landing
0.2 psi
90
Min Hydraulic Reservoir Temp for Engine Start
-18C
91
Brake temp indication must in the ____ range for takeoff.
GREEN
92
After selecting reverse thrust, do not move thrust levers into the forward thrust range until...
...REV icon on EICAS is shown in amber or green.
93
TO DATASET MENU on MCDU must be set to ENG when OAT is...
5C-10C, when there is any possibility of contacting visble moisture up to 1,700' AFE. When operating on ramps, taxiways, runways, etc where snow, ice, standing water, slush, may be ingested by the engines, or freeze on the engines, nacelles, or engine sensor probes.
94
TO DATASET MENU on MCDU must be set to ALL when OAT is...
<5C, when there is any possibility of contacting visble moisture up to 1,700' AFE. When operating on ramps, taxiways, runways, etc where snow, ice, standing water, slush, may be ingested by the engines, or freeze on the engines, nacelles, or engine sensor probes.
95
When either or both ice detectors are failed, the crew must set the mode selector to ON when...
...icing conditions exist or below 10C TAT with visible moisture.
96
A/P min engagement height
400 ft
97
A/P min use height
50 ft
98
A/P min use height non-precision approach
MDA
99
TAS, TAT, and SAT information are only valid above...
60 kt
100
While transmitting in VHF1, the standby mag compass indication is...
...not valid.
101
RNAV LP minima are...
Not Authorized.
102
Manual engine start abort:
NNoTM*/HHN
1. No +Oil press w/in 10 sec after N2 increase.*
2. No N1 increase at starter cutout (~50% N2) when starting with Tailwind.*
3. No ITT w/in 30 sec of start. (no light off).
4. ITT exceeds 815C (hot start).
5. Oil press stabilizes not in green range.*
6. N1 or N2 fail to accelerate to stable (hung start).
7. Intermittent elec or pneu or starter Malfunction before starter cutout.*
103
Cold WX Preflt
1. OAT 5C or less.
2. Wing fuel temp 0C or less.
3. Atmospheric conds conducive to icing exist.
4. Overnight contamination.
5. Through flight residual.
6. Cold Soak ice.
104
Is underwing frost allowed?
Up to 1/8" frost layer underwing surfaces.
105
Defacto Emergency Descent Memory Items (think SOPM).
At least one MFD with terrain.
| Once Cabin Altitude reaches 14,500, PASSENGER OXYGEN to OVRD.
106
Engine Dry Motoring Duty Cycle Limits
```
#1 = 90 seconds ON, 5 minutes OFF.
#2-5 = 30 seconds ON, 5 minutes OFF.
```
After five sequential motoring cycles, the process may be repeated following a 15 min cool down period.
107
APU Starter Duty Cycle
Start Attempt #1 & 2 = 60 seconds OFF.
| Start Attempt #3 = 5 minutes OFF.
108
MTW (LL)
LR MTW - 420#
109
MTOW (LL)
LR MTOW - 419#
110
MZFW (LL)
LR MZFW - 419#
111
When an auto abort occurs or engine start is manually aborted due to abnormal indications... can you try again?
...its cause must be investigated and corrected before further attempts to start the engines.
112
In case of an automatic abort due to an engine hot start and with no ENGINE EXCEEDANCE EICAS message...
...two additional engine starts are allowed. (but you should probably investigate why / call mx).
113
No Flex Thrust Takeoffs?
1. Contaminated Runway.
2. Reported or forecasted Windshear.
3. Special departure (ex: Reno).
114
Max Angle Climb Speed?
VFS.
115
Max Rate of Climb Speed?
~VFS+50
116
SkyWest min hold speed?
<=6000 ft = 200 KIAS (FAA...)
| >6000 ft = 210 KIAS
117
Minimum Fuel?
2,250 lbs, 45 min, 1,500 ft AFE green dot clean.
118
Emergency Fuel?
1,500 lbs, 30 min, 1,500 ft AFE green dot clean.
119
Which checklist do you do first?
```
MEAN
Memory/QRC
Emergency
Abnormal
Normal
```
