Brainscape's Knowledge GenomeTM

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


See full index

Emergencies > Memory Items > Flashcards

Memory Items Flashcards

1
Q

Turbulence Penetration Speed

A
  • FL250 = 290KTS
    +FL250 = 310/.84M lower of the speeds
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Flap Extension Altitude

A

FL200

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

Max gear speed VLE/MLE,VLO/MLO

A

270/.82

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

Waypoints BMW tolerance

A

+-1 degree
+- 2 NM
N/S Tracks may be 3NM

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

AIRSPEED UNRELIABLE

A

Autopilot disconnect switch PUSH
Autothrottle ARM switches (both) OFF
F/D switches (both) OFF
Set the following
Flaps extended 10˚ and 85% N1
Flaps retracted 4˚ and 70% N1

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

STABILIZER

A

STAB cutout switches (both) CUTOUT
Do not exceed current airspeed

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

SMOKE, FIRE or FUMES

A

OXYGEN MASKS, REGULATORS ON, 100%
CREW COMMUNICATIONS ESTABLISH

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

SMOKE OR FIRE FROM LITHIUM BATTERY

A

If necessary transfer control to the flight crew member seated on the opposite side of the fire.
PA “BACKUP TO THE FLIGHT DECK” x 2

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

FIRE ENG

A

A/T ARM switch (confirm) OFF
Thrust Lever (confirm) IDLE
FUEL CONTROL switch (confirm) CUTOFF
Engine Fire Switch (confirm) PULL

➢ If the FIRE ENG message stays shown Engine fire switch Rotate to the stop and hold for 1 second

➢ If after 30 seconds, the FIRE ENG message stays shown Engine fire switch Rotate to the other stop and hold for 1 second

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

ENGINE SEVERE DAMAGE OR SEPARATION

A

A/T ARM switch (confirm) OFF
Thrust Lever (confirm) IDLE
FUEL CONTROL switch (confirm) CUTOFF
Engine Fire Switch (confirm) PULL

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

Min alt for speed brakes

A

800ft

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

Speed brakes with alt gear ext?
True or false ?

A

True no speed brakes when doing extension you can use again after complete

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

No Flch or vs below

A

1000agl

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

Ap disengage 8/9

A

100/135

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

Max spd

A

.90/360kts

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

Max t/w

A

10

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

Max demo xwind
To/ld
8/9

A

To/ld
-8 40/37
-9 33/40

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

ENGINE LIMIT OR SURGE OR STALL

A

A/T ARM switch (confirm) OFF
Thrust Lever (confirm) Retard until message blanks or idle

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

DUAL ENG FAIL/STALL

A

FUEL CONTROL switched (both) CUTOFF, then RUN
RAM AIR TURBINE switch Push and hold for 1 second

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

ABORTED ENGINE START / ENGINE AUTOSTART

A

FUEL CONTROL switch CUTOFF

21
Q

ABCO TTTBAD (FOM 12 p.14)

A

ATC-ADVISE
BRIEF F/A’s
COMPANY ADVISE (DIVERSION QRH Normal)
OVERWEIGHT (QRH Normal & ECL)

Type of emergency & Landing classification
Touchdown surface / Emergency exits / Landing attitude
Time available
Bracing signals
Advise to passengers
Displace passengers

22
Q

ENGINE INOPERATIVE IN CRUISE / DRIFTDOWN “EASTER” (1.02.10 p.13)

A

ENG Call for “ENG OUT” on VNAV pg, confirm MOD CRZ
ALTITUDE Set ENG OUT altitude in MCP altitude window
SPEED Ensure “VNAV SPD” - confirm / “EXECUTE” Engine out drift down – Confirm MCT (CON)
TALK ATC / 121.5 / All Exterior LIGHTS ON
EXECUTE TURN Execute turn if required in HDG/TRK SEL – consider ETOPS diversion
RECALL Recall items, “Checklist ENGINE FAIL” / ETOPS DIVERSION / ABCO

23
Q

OCEANIC DIVERSION (QRH 0.01-0.03)

A

Engine-Out [TURN / OFFSET as required]
DRILLS / Time Critical Checklists
ATC – Declare Emergency & Request Clearance
If unable to obtain clearance;
TURN 30° R (China/ Russia) or 30° L/R (OCA)
OFFSET (5 NM OCA/China, 16.2 NM Russia)
@ OFFSET; DESCEND below FL 290 and maintain +/- 500 ft

All-Engine DRILLS / Time Critical Checklists

ATC – Declare Emergency & Request Clearance
If unable to obtain clearance;
TURN 30° R (China/ Russia) or 30° L/R (OCA)
OFFSET (5 NM OCA/China, 16.2 NM Russia)
@ OFFSET; CLIMB or DESCEND +/- 500 ft

24
Q

PILOT INCAPACITATION (FOM 12.5.8)

A

Does not respond to:
• Two communications;
• A single verbal challenge;
• Or there is significant deviation to flight profile.

Crew Actions:
• Assume control
• Autopilot ON
• Request assistance using Urgent Communications Procedure

• Tilt the incapacitated flight crew member’s seat back; and
• Move the seat full aft and move the rudder pedals full forward; and
• Move the incapacitated flight crew member’s head back; and
• Use shoulder harness as a restraint; and
• When practicable, remove the incapacitated flight crew member from the seat and replace, if possible, with another crew
member.
When a flight crew member requires the continuous use of medical oxygen the flight shall land at the nearest suitable
airport.

25
Q

“RECOVERY” RECOVERY

A

Technique to return the aircraft to a normal state after a TCAS RA/UPSET/GPWS/STALL/WINDSHEAR ESCAPE
AUTOPILOT ON
FLCH Engage
BUG UP Set Flaps Up Maneuvering speed
CLEAN UP Retract Flaps on Schedule

26
Q

R/A

A

◦ Disengage A/P
◦ Disconnect A/T
If Req’d

◦ Smoothly adjust pitch to
satisfy TA
◦ Fly planned lateral
path

27
Q

R/A in
Landing
Config

A

◦ Thrust - Maximum
◦ Disengage A/P
◦ Disconnect A/T If Req’d

Flaps 20
◦ Positive Rate: Gear Up

◦ Pitch Smoothly adjust to satisfy TA
◦ Fly planned lateral path

28
Q

GPWS

A

“FIREWALL”

◦ Disengage A/P
◦ Disconnect A/T
◦ Maximum Thrust aggressively
◦ Roll Wings level &
◦ Pitch up to 20 NU
◦ Pitch limit if
necessary
◦ Retract Speedbrakes

29
Q

STALL

A

“STALL”

AP AT DISC

◦ Pitch nose down to
exit stall

◦ May need to
decrease Thrust

◦ Roll wings level

◦ Increase
Thrust smoothly

◦ Check/Retract
Speekbrakes

◦ Maintain existing
Gear/Flaps

◦ If clean during T/O; Flaps 1

30
Q

Windshear
Manual

A

“WINDSHEAR
TOGA”

◦ Disconnect A/P
◦ Push TOGA
◦ Disconnect A/T
◦ Maximum Thrust
aggressively

◦ Rolls Wings level &
Pitch to 15*NU
◦ Follow TO/GA
◦ Retract Speedbrakes

31
Q

Windshear
Automatic

A

“WINDSHEAR
TOGA”

◦ Push TOGA
◦ Verify TOGA

◦ Verify Thrust
advances GA

◦ Monitor system
performance

◦ Retract Speedbrakes

32
Q

Upset
Nose High
Recovery

A

Disengage A/P and disconnect A/T
Nose down as much as full – TRIM
Reduce Thrust
Roll for nose down
Recover: Roll wings level at horizon
Check airspeed and adjust thrust
Establish pitch attitude

33
Q

Upset - Nose low

A

Disengage A/P and disconnect A/T
Recover from stall if necessary
Roll in shortest direction to wings level
Recover: Adjust pitch – TRIM
Adjust thrust and drag

34
Q

Severe Engine Damage indications

A

N1-0
N2-0
High vibe

35
Q

FLT CONTROL MODES

A

NORMAL
SECONDARY
DIRECT

36
Q

FLAP AND SLAT CONTROL MODES

A

PRIMARY
SECONDARY
ALTERNATE

37
Q

CATASTROPHIC PA

A

2 MINS EMERGENCY STATIONS X2
30 SEC BRACE FOR LANDING X2
REMAIN SEATED X2

38
Q

RAPID DEPLANEMENT

A

Deplane immediately and leave your personal belongings.

39
Q

NADP 1

A

THRUST REDUCTION 1500
ACC HEIGHT 3000

40
Q

NADP2

A

THRUST REDUCTION 1000
ACC HEIGHT 1000

41
Q

ENGINE RUNUP

A

3’ OR COLDER
40%
5 SECONDS
60 MINS EVERY

50-55% with high vibes bring vines to 4 units or less

42
Q

ICE DETECT FAIL WHEN TO TURN ANTI ICE ON

A

When the primary ice detection system is not being used or is inoperative, icing conditions
may exist in flight when displayed TAT is less than or equal to 15°C. In flight, when displayed
TAT is greater than 10°C but less than or equal to 15°C and visible moisture is present, engine
and wing anti-ice must be selected ON except activation may be delayed until 2500 ft AGL for
take-off.

43
Q

ICING CONDITIONS ON THE GROUND

A

Icing conditions also exist when the OAT on the ground and for take-off 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 and
visible moisture in any form is present (such as clouds, fog with visibility of one mile or less,
rain, snow, sleet and ice crystals).

44
Q

ENG ANTI-ICE

A

Ground Operation in Icing Conditions
During ground operations (including taxi-in and taxi-out) in icing conditions when the OAT is 3°C or
below, the engine must be run up to a minimum of 40% N1 for at least 5 sec duration at intervals no
greater than 60 min. If high engine vibration indications occur, a run-up to 50% N1 may be done.

Engine anti-ice must be selected ON during all ground operations when icing conditions exist or are
anticipated, except when the temperature is below -40°C OAT. Do not use engine anti-ice if OAT (on
the ground) exceeds 10°C.

45
Q

400’

A

LNAV/HDG
ALTITUDE
DRILL?

46
Q

Reject reasons <80

A

• activation of the master caution system • system failure(s) • unusual noise or vibration • tire failure • abnormally slow acceleration • take-off configuration warning • fire or fire warning • engine failure • predictive windshear warning • the airplane is unsafe or unable to

47
Q

Above 80 knots and before V1, reject the takeoff for any of the following:

A

• fire or fire warning
• engine failure
• predictive windshear warning
• the airplane is unsafe or unable to fly

48
Q

Run up in icing

A

When both of the following exist, do an engine run-up to minimize ice build-up:
• OAT is 3°C or below
• visible moisture present (fog with visibility of one statute mile [1600 m] or less, rain,
snow, sleet, ice crystals, and so on)

Run-up to a minimum of 40% N1 for at least 5 sec duration at intervals no greater than
60 min. If high engine vibration indications occur, a run-up to 50% N1 may be done.
If take-off is not completed within 120 min total taxi time, manually de-ice the engines before take-off

49
Q

Fan Ice Removal

A

CAUTION: Avoid prolonged operation in moderate to severe icing conditions.
If moderate to severe icing conditions are encountered:
Note: Operation in icing conditions may result in engine vibration indications above the normal
operating range during ice shedding.
During flight in moderate to severe icing conditions for prolonged periods with N1 settings at or
below 70%, or when fan icing is suspected due to high engine vibration, the fan blades must be
cleared of any ice. Do the following procedure every 15 min on both engines, one engine at a time:
Reduce thrust toward idle then increase to a minimum of 70% N1 for 10 to 30 sec.

Emergencies (1 decks)

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