Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

175 > 175 2020 Limits Memory > Flashcards

175 2020 Limits Memory Flashcards

1
Q

CABIN ALTITUDE HI

A

OXYGEN MASKS&raquo_space;> DON, 100%

CREW COMMUNICATION&raquo_space;> ESTABLISH

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

ENGINE ABNORMAL START

A

AFFECTED ENGINE&raquo_space;> START/STOP SELECTOR = STOP

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

SMOKE EVACUATION

A

OXYGEN MASKS»> DON, EMERG
CREW COMMUNICATION&raquo_space;> ESTABLISH
PRESSURIZATION DUMP&raquo_space;> PUSH IN

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

SMOKE/FIRE/FUMES

A

OXYGEN MASKS&raquo_space;> DON, 100%

CREW COMMUNICATION&raquo_space;> ESTABLISH

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

BATT 1 (2) OVERTEMP

A

ASSOCIATED BATTERY&raquo_space;> OFF

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

JAMMED CONTROL COLUMN - PITCH

A

ELEVATOR DISCONNECT HANDLE&raquo_space;> PULL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

JAMMED CONTROL WHEEL - ROLL

A

AILERON DISCONNECT HANDLE&raquo_space;> PULL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

PITCH TRIM RUNAWAY

A

A/P DISCONNECT BUTTON&raquo_space;> PRESS AND HOLD

PITCH TRIM SYS 1and2 CUTOUT BUTTONS&raquo_space;> PUSH IN

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

ROLL (YAW) TRIM RUNAWAY

A

A/P DISCONNECT BUTTON&raquo_space;> PRESS AND HOLD

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

STEERING RUNAWAY

A

STEER DISC SWITCH&raquo_space;> PRESS

Steer airplane using differential braking and rudder.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

MTW (LR)

A

85,870 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

MTOW (LR)

A

85,517 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

MLW (LR and LL)

A

74,957 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

MZFW (LR)

A

69,886 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

MTW (LL)

A

LR-420 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

MTOW (LL)

A

LR-419 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

MZFW (LL)

A

LR-419 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Wing Span

A

93 ft 11 in

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Aircraft Length

A

103 ft 11 in

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Tail Height

A

32 ft 4 in

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Max. Ops. Alt.

A

41,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Max. T/O & Lnd Alt.

A

10,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Max. Temp. T/O Lnd

A

ISA + 35°C (52°C)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

Min. Temp. T/O Lnd

A

-40°C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

RWY Slope

A

+/- 2%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

Max. Tailwind

A

15 kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
27
Q

Max. Single Pack Operations

A

31,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
28
Q

VMO SL- 8,000’

A

300

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
29
Q

VMO 10,000- Mach Transition

A

320

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
30
Q

MMO

A

0.82

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
31
Q

VA

A

240

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
32
Q

VLO EXT, VLE RET, VLE

A

250

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
33
Q

V Tire

A

195

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
34
Q

V RAT DEPLOY MAX

A

VMO/MMO

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
35
Q

VMIN (to provide electrical power)

A

130

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
36
Q

VB (below 10,000 ft)

A

250

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
37
Q

VB (10,000 ft and above)

A

270/.76M (whichever is lower)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
38
Q

V wiper ops max

A

250 (SW)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
39
Q

Vwindow

A

160

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
40
Q

VFE 1

A

230

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
41
Q

VFE 2

A

215

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
42
Q

VFE 3

A

200

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
43
Q

VFE 4

A

180

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
44
Q

VFE 5

A

180

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
45
Q

VFE FLAPS FULL

A

165

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
46
Q

Max Rec’d Xwind Landing?

Dry/Wet/Sn/Slush/Icy

A

See QRH Perfomance PD35-24. (38/31/20/18/12)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
47
Q

Due to engine compressor stall possibility, static takeoff is not recommended with
crosswind component greater than…

A

25 kt.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
48
Q

Max. Alt. Flaps/Slats Extended

A

20,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
49
Q

Flap/Slat Enroute Ops

A

Prohibited

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
50
Q

Min. Spoiler Speed

A

180 kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
51
Q

CAT II Approach Flap Setting

A

Mandatory Flaps 5

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
52
Q

Landing Flaps Full, GA Flaps =

A

Go-Around Flaps 4

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
53
Q

Landing Flaps 5, GA Flaps =

A

Go-Around Flaps 2

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
54
Q

Battery Min. Voltage

A

22.5V

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
55
Q

Engine Max ITT

A

815°C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
56
Q

Oil Pressure Min

A

25 psi

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
57
Q

Engine Ground Start Attempts 1 and 2 Cranking Time Limits

A

90 Seconds ON, 10 Seconds OFF

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
58
Q

Engine Ground Start Attempts 3,4 and 5 Cranking Time Limits

A

90 Seconds ON, 5 Minutes OFF

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
59
Q

Engine Flight Start Attempts 1 and 2 Cranking Time Limits

A

120 Seconds ON, 10 Seconds OFF

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
60
Q

Engine Flight Start Attempts 3,4 and 5 Cranking Time Limits

A

120 Seconds ON, 5 Minutes OFF

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
61
Q

For ground starts, the maximum cumulative starter run time per start attempt (motoring plus start time) is =

A

90 seconds

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
62
Q

For flight starts, the maximum cumulative starter run time per start attempt (motoring plus start time) is =

A

120 seconds

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
63
Q

Dry Motor #1 start limit

A

90 Seconds ON

5 Minutes OFF

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
64
Q

Dry Motor #2-5 start limit

A

30 Seconds ON
5 Minutes OFF
After five sequential motoring cycles, the process may be repeated following a 15
minute cool down period.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
65
Q

When it is necessary to perform an engine start with tailwind, monitor N1 indication. When
there is no positive increase of N1 indication before starter cutout (50% N2), the engine start
must be…

A

…manually aborted.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
66
Q

Takeoff with the Automatic Takeoff Thrust Control System (ATTCS) OFF is…

A

…not authorized.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
67
Q

Max. Fuel (JET A, JET A1) Capacity

A

20,935 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
68
Q

Max. Imbalance

A

794 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
69
Q

Min. Fuel Tank Temp.

A

-37°C

70
Q

Can you takeoff and land with a FUEL IMBALANCE message?

A

Yes, as long as the

actual imbalance does not exceed 794 lb.

71
Q

Fuel crossfeed must be selected ___ during takeoff and landing.

A

OFF.

72
Q

Wait ____ seconds after the EICAS is energized to start the APU.

A

30 seconds

73
Q

Do not leave the aircraft unattended more than ___ minutes with the APU running (SW).

A

5 minutes

74
Q

Simultaneous use of the APU bleed and the HP cart is…

A

…prohibited.

75
Q

APU Starter Duty Cycle Attempts 1 and 2 =

A

60 Seconds OFF

76
Q

APU Starter Duty Cycle Attempt 3 =

A

5 Minutes OFF

77
Q

APU Min Start Temp

A

-54°C

78
Q

APU Max Start Temp

A

ISA +35

79
Q

APU Max Start Altitude

A

30,000 ft

80
Q

APU Min Operating Temp

A

-54°C

81
Q

APU Max Operating Temp

A

ISA +35 (52°C)

82
Q

APU Max Operating Altitude

A

33,000 ft

83
Q

APU Max Electrical Gen Altitude

A

33,000 ft

84
Q

APU Bleed Use Altitude

A

15,000 ft

85
Q

APU Engine Start Altitude

A

21,000 ft

86
Q

Max DeltaP >37,000’

A

8.4 psi

87
Q

Max DeltaP <37,000’

A

7.8 psi

88
Q

Max. DeltaP Over Pressure

A

8.8 psi

89
Q

Max DeltaP Negative Pressure

A

-0.5 psi

90
Q

Max DeltaP T/O Lndg

A

0.2 psi

91
Q

Min. Hydraulic Reservoir Temp. for ENG Start

A

-18°C

92
Q

Brake temperature indication must be in the ____ range for takeoff.

A

Green

93
Q

Go-around after deployment of the thrust reversers?

A

Do not attempt a go-around maneuver.

94
Q

After selecting reverse thrust, do not move the thrust levers into the forward thrust range until…

A

…REV icon on the EICAS is shown in amber or green.

95
Q

The use of thrust reversers during normal taxi operations is…

A

…prohibited.

96
Q

The use of thrust reversers for power back operations is…

A

…prohibited.

97
Q

The TO DATASET MENU on the MCDU must be set to ENG in the following cases when
OAT is from 5°C to 10°C and:

A

When there is any possibility of encountering visible moisture up to 1,700 ft AFE.
– When operating on ramps, taxiways, or runways where surface snow, ice, standing
water, or slush may be ingested by the engines, or freeze on engines, nacelles, or
engine sensor probes.

98
Q

The TO DATASET MENU on the MCDU must be set to ALL in the following cases when
OAT is less than 5°C and:

A

– When there is any possibility of encountering visible moisture up to 1,700 ft AFE.
– When operating on ramps, taxiways, or runways where surface snow, ice, standing
water, or slush may be ingested by the engines, or freeze on engines, nacelles, or
engine sensor probes.

99
Q

When either one or both ice

detectors are failed, the crew must set the mode selector to ON when…

A

…icing conditions exist or are anticipated below 10°C TAT with visible moisture.

100
Q

A/P Min. Engagement Height

A

400 ft

101
Q

A/P Min. Use Height

A

50 ft

102
Q

A/P Min. Use Height - Non-precision Approach

A

MDA

103
Q

TAS, TAT, and SAT information are only valid above…

A

…60 kt.

104
Q

While transmitting in VHF1, the standby magnetic compass indication is…

A

…not valid.

105
Q

Barometric altimeter minimums must be used for all…

A

…CAT I approaches.

106
Q

T/F

Navigation is not to be predicated on the use of the Terrain Awareness System.

A

True. Don’t use predicitve EGPWS if airport not in database. Press in the GRD PROX TERR INHIB button to
inhibit predictive EGPWS functions.

107
Q

T/F

RNAV (GPS) LP minima are not authorized.

A

True.

108
Q

ICE Briefing

A

Introduction (docs/fit)
Communication (emergency notification, suspicous activity the FA uses plain english using their full name when notifying flight deck)
Entry Protocol.

109
Q

Additional Normally Briefed by Capt Items

A

*Emergency/Abnormal procedures management.
• *Rejected takeoff plan. This includes reasons for rejecting the takeoff and crew duties.
NOTE: * The captain normally conducts these briefing items. These items need only be
briefed on the FFOD for the crew.

110
Q

On power up, what if the battery is below 22.5V but equal to or above 21.0V?

A

You can recharge battery - see SOPM. Below 21.0V call maintenance.

111
Q

The APU is started approximately ___ minutes prior to pushback, unless required for passenger
comfort.

A

10 minutes

112
Q

Packs should be ____ when a ground air source is being utilized.

A

OFF

113
Q

H-PBIT runs automatically when…

A

…all 3 hyd systems are pressurized for at least 1 minute and reservoir temp greater than +10C.
(1 min, 1 way to interrupt)

114
Q

H-PBIT is interrupted when…

A

…any flight control surface is moving during the test. (1 min, 1 way to interrupt)

115
Q

E-PBIT runs automatically when…

A

…an initial AC source is introduced. (3 min, 3 ways to interrupt)

116
Q

E-PBIT is interrupted when…

A

…any hydraulic pump is running, flight control mode panel switches cycled, AC power interrupted. (3 min, 3 ways to interrupt)

117
Q

How do you force a E-PBIT to run?

A
  1. Power down using Leaving the Airplane Checklist.
  2. Wait 1 minute.
  3. Perform power up using Safety and Power Up Checklist.
  4. Wait 3 minutes for E-PBIT to run.
  5. Perform H-PBIT when required.
118
Q

How do you force a H-PBIT to run?

A
  1. Don’t move any flight control surface.
  2. STEER OFF EICAS displayed.
  3. Confirm all 3 hydraulic systems are below 250 psi and temps above 10C.
  4. Load 27.2 = 3A, 1, 2 turn the electrical pumps on in that order.
  5. Wait 1 minute.
  6. Turn off the pumps.
119
Q

When do you need to do the SOPM hydraulic system warm up?

A

Reservoir temp below -18C.

120
Q

When the smart probes are contaminated with ice or snow…

A

…turn ON ADSP Heater Switch. Make sure the PBITs run…see SOPM.

121
Q

Conditions conducive to icing exist on the ground and for takeoff when…

A

…the OAT is 10°C or below, when operating on ramps, taxiways, or runways where surface snow, ice, standing water, or
slush may be ingested by the engines or freeze on engines, nacelles, or engine sensor probes.

122
Q

A Cold Weather Preflight inspection must be performed…when:

A
  1. The OAT is 5°C or less, or
  2. The wing fuel temperature is 0°C or less, or
  3. Atmospheric conditions conducive to icing exist, or
  4. The aircraft has remained overnight and may have frozen contaminants due to exposure to
    frost or precipitation, which could involve the entire airframe, or
  5. On any through flight where residual ice from the inbound flight may have accumulated on
    airframe surfaces or components, or
  6. Cold soak ice is suspected in the fuel tank area.
123
Q

Thin layer of frost underneath wing ok?

A

Yes…A 3 mm (1/8 in) frost layer is permitted on the underwing surfaces. A thin layer of
hoarfrost is permitted on the fuselage provided the layer is thin enough to distinguish surface
features underneath, such as painting and markings.

124
Q

Engine 1 is normally started first and utilized for single engine taxi. When the crew elects to
taxi single engine on engine 2, electric hydraulic pump 1 selector knob must be…

A

…turned ON.

Once engine 1 is running, turn electric hydraulic pump 1 to AUTO.

125
Q

After second engine start, verify the EICAS N1 target value is…

A

…+0.5% to -0.1% of the
ACARS or release N1 value. For example, if the ACARS / release N1 value is 90.0, then the N1 target on the EICAS must be 89.9 to 90.5.

126
Q

When it is necessary to perform an engine start with a tailwind, monitor N1. When there is no
positive increase of N1, before starter cutout (50% N2), the start must be…

A

…manually aborted.

127
Q

When oil pressure is not indicated by the time idle rpm is achieved…

A

…conduct an

immediate shutdown of the engine.

128
Q

Although FADEC provides automatic over-temperature protection and automatically aborts the
start in the event of a hot start, hung start, or no light off, the engine start must be manually
aborted when:

A

NNoTM*/HHN ( Seven!)

  1. No positive oil press w/in 10 sec after N2 increase.
  2. No N1 increase at starter cutout (~50%N2) when starting with TW.
  3. No ITT indication within 30 seconds of fuel flow (no light off).
  4. ITT exceeds 815C (hot start).
  5. Oil Pressure stabilizes outside of green range.
  6. N1 or N2 fail to accelerate to stable (hung start).
  7. Intermittent elec or pneu start malfunction occurs before starter cutout.
129
Q

When an automatic abort occurs or engine start is manually aborted due to abnormal
engine indications, its cause…

A

…must be investigated and corrected before further attempts
to start the engines.

130
Q

In case of an automatic abort due to an engine hot start and with no ENGINE
EXCEEDANCE EICAS message….

A

…two additional engine starts are allowed. (but you should probably call maintenance…unless your FO f’ed up cross bleed is a good example).

131
Q

Max Taxi Speed, Straight / DRY

A

30 kt

132
Q

Max Taxi Speed, Straight / WET or CONTAMINATED

A

10 kt

133
Q

Max Taxi Speed, Turns / DRY

A

10 kt

134
Q

Max Taxi Speed, Turns / WET or CONTAMINATED

A

5 kt

135
Q

For FOD prevention and damage to other aircraft and equipment in close proximity, limit the
thrust to…

A

…40% N1, as much as possible, and avoid rapid accelerations and decelerations.

136
Q

Capt, when would you NOT SE taxi?

A
  1. Contamination.
  2. Maneuvering room marginal.
  3. <5 min taxi time.
  4. Airport forbids SE taxi.
  5. Risk personnel injury or equip damage.
  6. Capt’s call.
    Also consider: slope, weight, 2 min warm up.
137
Q

During ground operations of more than 30 minutes in icing conditions, or when increased fan
vibration due to fan ice accumulation is present, the engine thrust may be increased at 30 minute
intervals to approximately…

A

..54% N1 and held at that thrust level for 30 seconds, or until the fan
vibration level returns to normal. When airport surface conditions and the concentration of other
aircraft do not permit the engine thrust to be increased to 54%, set an acceptable thrust level
and time interval that is safe and practical.

138
Q

Normal Takeoff Procedure (up to 10 kt tailwind):

A

40% N1 (with or without brakes), stable. Advance to TO/GA.

139
Q

Normal Takeoff Procedure (up to 11-15 kt tailwind):

A

A/T disarmed. Apply brakes and advance thrust to 60% N1. Stable. Release brakes, Arm A/T / TO/GA detent before 60 kt.

140
Q

Static Takeoff (SNA):

A

Apply brakes. 40% N1, stable. TO/GA detent. Release brakes at takeoff N1 target.

141
Q

The use of Flex Thrust Takeoff is prohibited given the following operational constraints:

A
  1. Takeoff on contaminated runways.
  2. Reported or forecast windshear.
  3. When a special departure procedure specifies full thrust for takeoff.
142
Q

New Capt RTO Callouts:

A 
"REJECT" or "REJECT MY CONTROLS"
later
“THIS IS THE CAPTAIN REMAIN
SEATED WITH YOUR SEAT BELT
FASTENED.”
143
Q

For SEO, limit bank angle to

A
  • 15° at V2
  • 20° at V2 + 5 kt
  • 25° at V2 + 10 kt
144
Q

Max Angle Climb Speed?

A

VFS (use for obstacle clearance)

145
Q

Max Rate of Climb Speed?

A

~VFS+50 (use for weather conditions)

146
Q

Hold Leg Lengths Times?

A

Below 14k 1min

Above 14k 1.5min.

147
Q

SkyWest Min Holding Speeds?

A

6000andbelow: 200
6001andabove: 210

148
Q

FAA Max Holding Speeds?

A

<=6000 200 KIAS
6001-14k 230 KIAS
>=14,001 265 KIAS

149
Q

Intentional flight in severe icing conditions is…

A

…prohibited.

150
Q

2020 SOPM Climb Speed Schedule?

A

270 kt to M 0.73 or APG

151
Q

2020 SOPM Descent Speed Schedule?

A

280 kt to M 0.74 or APG

152
Q

CAT II crosswind limit?

A

15 kt (Ops Spec C060)

153
Q

CAT II Lowest authorized published RA setting?

A

80 ft.

154
Q

CAT II DH is limited to ___ ft above TDZ.

A

100

155
Q

Planed missed approach fuel burn?

A

700 lbs

156
Q

Planned missed approach fuel burn is derived using FOQA data and based on:

A

Executing 1 missed approach. Completing a subsequent approach using average actual distances. Note: FOQA shows average miles flown while conducting a missed and subsequent approach is 39.6 nm. Distances will vary.

157
Q

Minimum Fuel amount?

A

2,250 lbs

158
Q

Emergency Fuel amount?

A

1,500 lbs

159
Q

Minimum Fuel provides…

A

…45 minutes of fuel endurance based upon 1,500 ft AFE / Green Dot /
Clean.

160
Q

Emergency Fuel provides…

A

…30 minutes of fuel endurance based upon 1,500 ft AFE / Green Dot /
Clean.

161
Q

Which checklist do you do first?

A 
Unless the situation dictates otherwise, the priority for handling an emergency/abnormal situation
is:
M - Memory / QRC items
E - Emergency items
A - Abnormal items
N - Normal checklists
162
Q

Defacto Emergency Descent Memory Items (think SOPM).

A

When the cabin reaches 14,500 ft or above, set MASKS DEPLOY selector knob to OVRD
immediately.

The flight profile must be monitored and TERRAIN set on MFD.

163
Q

Dry (6) Xwind TO/Lndg

A

38 kts

164
Q

Wet (5) Xwind TO/Lndg

A

31 kts

165
Q

Dry/Compact Snow (4) Xwind TO/Lndg

A

20 kts

166
Q

Slush Xwind TO

A

18 kts

167
Q

Wet Snow (3) Xwind Lndg

A

15 kts

168
Q

Ice/Slush/Wet Ice TO

A

12 kts

169
Q

Slush (2) Xwind Lndg

A

12 kts

170
Q

Ice Xwind Lndg

A

8 kts

171
Q

New November 2020 CAT II Xwind Limit

A

12 kts…I guess that was the AOM limit?

175 (9 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions