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B767 > B767 > Flashcards

B767 Flashcards

1
Q

Aborted Engine Start Drill

A

Fuel Control Switch-Cutoff

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2
Q

Engine Failure in Cruise

A

-A/T arm switch off
-MCT
-Trim adjust
-E/O CRZ select on FMC
-Set drift down alt in window
-E/O CRZ D/D: execute (ensure VNAV)
-Lights on
-ATC advise
PF- turn if required
-call “checklist, engine failure in cruise”
-at altitude capture determine optimum cruise altitude
-adjust thrust as required
proceed to land

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3
Q

Engine Failure on Final (Flaps 20 or less)

A

“Checklist, engine failure”
continue landing

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4
Q

Engine Failure on Final (Flaps more than 20 or past FAF)

A

Go-Around
-or-
adjust thrust to maintain speed and continue

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5
Q

Stall

A

Call “Stall”
Hold control column firmly
A/P off
A/T off
Gently lower nose to stop shaker/buffet (may need trim, may need to reduced thrust)
when out of stall:
wings level
increase thrust
speedbrakes retracted
maintain configuration (call “flaps 1 if clean during t/o)
when recovered:
adjust thrust as needed
adjust pitch
recover flight path
reengage A/P and A/T if desired

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6
Q

GPWS Caution

A

Correct the flight path or the aircraft configuration

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7
Q

GPWS Warning

A

“Firewall”
A/P off
A/T off
Aggressively apply maximum thrust
wings level
pitch to 20 degrees
retract speed brakes
(if you’re going to hit something pitch to shaker/buffet)
maintain configuration
Monitor RA
Slowly decrese pitch and accelerate when clear
PM-verify max thrust
-monitor V/S and altitude

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8
Q

T/A

A

look for traffic
maneuver as needed

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9
Q

TCAS R/A

A

A/P off
A/T off
Smoothly adjust pitch to satisfy RA command
Follow lateral path
Pm “tcas RA”
(if in landing config and a climb is required: max thrust, call for flaps 20 & gear up with “positive rate”)
when clear of traffic return to assigned altitude using a vs of no more than 500fpm
PM advises ATC

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10
Q

Nose High Recovery

A

A/P off
A/T off
lower nose
Nose down trim
reduce thrust
bank to lower nose if required
when recovered approaching the horizon:
roll level
Check airspeed and adjust thrust
adjust pitch

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11
Q

Nose Low Recovery

A

A/P off
A/T off
recover from stall
roll wings level
pitch up (trim if required)
adjust thrust and drag as required

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12
Q

Windshear ahead during T/O

A

Reject T/O

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13
Q

Windshear Escape Maneuver (Manual Flight)

A

A/P off
“windshear, TOGA”
push GA switch
Aggressively apply maximum thrust
A/T off
wings level
pitch 15 degrees
Retract speedbrakes
follow GA guidance
maintain config
monitor VS and altitude
accelerate when clear

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14
Q

Windshear Escape Maneuver (AutoFlight)

A

“windshear, TOGA”
push G/A switch
Verify GA mode
Verify GA thrust
retract speedbrakes
monitor performance
maintain config
monitor VS and altitude
accelerate when clear

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15
Q

Airspeed Unreliable

A

A/P off
A/T off
F/D’s off (both)
Flaps extended: pitch 10, thrust 80% N1
Flaps Up: pitch 4, thrust 75% N1

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16
Q

Dual Engine Failure

A

Both Engine Start selectors: FLT
Both Thrust: Idle
Both Fuel Control: Cutoff then run
(if engine appears stalled or EGT approaches the standby engine indicator placard limit: fuel control cutoff switch (affected engine): cutoff then run) repeat as needed

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17
Q

Cabin Altitude

A

Oxygen - on
Communication- establish
Main deck alert- use oxy
RTS/FSB signs- on
If occupants in main cargo- main cargo alert switch push (fin specific)
Non explosive - check cabin alt & rate
Explosive-emergency descent (atc advise, xpdr 7700, 10000’, idle, speed brakes, Vmo)

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18
Q

Engine Limit/Surge/Stall

A

A/T arm switch -off
thrust lever-confirm and retard
(retard until engine indications stay within limits or thrust lever at idle)

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19
Q

Smoke/fire from a Lithium Battery

A

Transfer control if required
“Backup to the flight deck, backup to the flight deck” (if passenger flight)

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20
Q

Smoke/Fire/Fumes

A

O2 masks- don
communications- establish

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21
Q

Three Green Lights Not On For Landing

A

If: no “gear disagree” message and “gear” light not illuminated

-accomplish normal landing

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22
Q

Oceanic Diversion - All Engine

A

Initiate applicable drills and time critical checklists
declare emergency and request clearance
either: proceed as per clearance
-or-
Turn 30 degrees right and offset 5NM
When establsihed offset +/-500ft

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23
Q

Oceanic Diversion - Single Engine

A

Initiate applicable drills and time critical checklists
declare emergency and request clearance
Either: proceed as per clearance
-or-
turn 30 degrees right and offset 5NM
(when established on offset descent to below FL290 and maintain +/-500ft)

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24
Q

Crew Incapacitation

A

Assume Control
A/P on
Tilt him back
Slide him back
Secure him (seat belts, away from flight controls)
Remove and replace if able

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25
Q

ETOPS (Minutes and NM)

A

180 minutes
1293 NM

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26
Q

No reduced thrust when (3):

A

Windshear
contaminated
prohibited by route or MEL

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27
Q

Max diff

A

9.1psi

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28
Q

minimum altitiude for A/P engagement

A

200’

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29
Q

Max wind for autoland

A

headwind: 25kts
Xwind: 25kts (15kts company limitation)
tailwind: 10kts

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30
Q

max altitude with flaps extended

A

20,000’

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31
Q

Vfe 1

A

250

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32
Q

Vfe 5

A

230

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33
Q

Vfe 15/20

A

210

34
Q

Vfe 25

A

180

35
Q

Vfe 30

A

170

36
Q

fuel freeze temp

A

Jet A :-40
Jet A1: -47

37
Q

Fuel capacity wings/centre

A

~19000kgs wings
~38000kgs centre

38
Q

max ASI differences ground/air

A

6kts ground
8kts air

39
Q

max barber pole difference

A

6kts (ground or air)

40
Q

max heading differences
HSI-HSI
HSI-RMI
HSI-STBY

A

HSI-HSI = 1deg
HSI-RMI = 2 deg
HSI-STBY = 10 deg

41
Q

Max altimeter differences on ground

A

50’
75’ from published field elevation

42
Q

Vlo (alternate system)

A

250kts

43
Q

Vlo (normal system)

A

270kts

44
Q

Vle

A

270kts

45
Q

Minimum O2

A

1550psi for 4 people for 180 minutes

46
Q

maximum wind for main deck cargo door

A

40kts to open
60kts once opened

47
Q

minimum oil pressure

A

10psi

48
Q

maximum oil temperature

A

175 deg C (15 min b/w 160 and 175 C)
(oil temp must be indicating b/f t/o)

49
Q

maximum altitude

A

43,100’

50
Q

max t/o and landing altitude

A

8400’

51
Q

max tail wind

A

10kts (15kts for fin 675)

52
Q

max dry snow for t/o

A

4 inches

53
Q

max packed snow for t/o

A

2 inches

54
Q

max slush/wet snow/water for t/o

A

1/2 inch

55
Q

max engine temp

A

870 deg C

56
Q

max engine temp continuous

A

750 deg C

57
Q

Reject before 80kts for…(11)

A

• Activation of the master caution
• System failure(s)
• Unusual noise or vibration
• Tire failure
• Abnormally slow acceleration
• Unsafe take-off configuration warning
• Fire or fire warning
• Engine failure
• A side window opens
• The airplane is unsafe or unable to fly
-windshear

58
Q

Reject after 80kts for…(4)

A

• Fire or fire warning
• Engine failure
• The airplane is unsafe or unable to fly
-wind shear

59
Q

“Glide slope, Glide slope” may be canceled when…(4)

A

• localizer approach
• visual maneuvering from an ILS
• when conditions require a deliberate approach below glideslope
• unreliable glideslope signal

60
Q

Turbulence penetration speed

A

290/.78

61
Q

Nosewheel steering angle tiller/rudder pedals

A

65/7 degrees

62
Q

Max altitude for Apu bleed

A

17000’

63
Q

Height

A

52’

64
Q

Wingspan

A

167’

65
Q

Autobrake speed activation

A

85kts

66
Q

Minimum oil for dispatch

A

14

67
Q

Fuel config means….(3)

A

Imbalance of 2000lbs
C tank has 1200+ lbs of fuel & c tank pumps are off
Low fuel

68
Q

T/o not authorized in …(4)

A

Hail
Heavy ice pellets
Moderate or heavy freezing rain

69
Q

Landings not authorized in…(2)

A

Moderate or heavy freezing rain

70
Q

Max x-wind

A

33kts

71
Q

Altimeters must agree within ft while in rvsm airspace

A

200ft

72
Q

Max number of apu starts

A

3/hour

73
Q

Wind shear indications in flight (7)

A

Stall
Below 1000’: 15kt deviation
+/-500’ vs deviation
5 degrees of pitch
1 dot glide slope deviation
Unusual thrust
Wind shear alert

74
Q

T/o alternate required when….(2)

A

Below 2600 rvr or 1/2sm
Below landing minimum

75
Q

Max angle of climb

A

Vref 30+80/M0.77

76
Q

Max rate of climb

A

Minimum clean speed (Vref 30+80) + 50/M0.78

77
Q

Total passenger count tolerance

A

+/-16

78
Q

X-wind takeoff technique

A

Thrust levers 70%
Thrust levers to t/o target
N1 engage

79
Q

Run up required when…(2)

A

Engine anti-ice is used (visible moisture 1sm or less)
+3C or less

80
Q

Run up technique

A

60% for 30 seconds every 30 minutes

B767 (1 decks)

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