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yupi-s-TiSiTi. > Nice to know > Flashcards

Nice to know Flashcards

1
Q

When is a reduced thrust takeoff not authorized?

A

-Runway contaminated by standing water, ice, slush, snow
-Windshear conditions are suspected
Prohibited by MEL/CDL

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2
Q

Stabilized approach criteria (1000’)

A

Landing configuration & checklist complete
Airspeed +20/-5 kts of Vapp
Sink rate is 1000’fpm or less and stable*
Aircraft is on a vertical path that will result in landing within the TDZ

*Vert speed up to 1200’ per minute may be acceptable under approach conditions that require higher airspeeds/ground speeds due to non-normal aircraft system configuration. This will be discussed during the approach briefing.

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3
Q

Stabilized approach criteria (500’)

A

Airspeed within 5kts of Vapp
Engine thrust is stabilized at a level that results in target speed

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4
Q

Stabilized approach criteria (200’)

A

Aircraft is aligned with the lateral confines of the runway

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5
Q

US holding airspeeds

A

SL-6000’:200kts (1min)
6001-14000’:230kts (1 min)
14001-above:265kts (1.5 min)

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6
Q

ICAO holding airspeeds

A

SL-6000’:200kts (1min)
6001-14000’:230kts (1min)
14001’-FL200: 240kts (1.5min)
20001-FL340: 265kts (1.5 min)

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7
Q

Emergency fuel (-400/-800)

A

-400:10K
-800: 11K

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8
Q

Minimum fuel (-400/-800)

A

-400: 14K
-800: 15K

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9
Q

When should you use autobrakes MAX?

A

Should be used when minimum stopping distance is required. Deceleration rate is less that that produced by full manual braking on a dry runway

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10
Q

When should you use autobrakes 3 or 4?

A

Should be used for wet or slippery runways or when landing rollout distance is limited

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11
Q

When should you use autobrakes 1 or 2?

A

These settings provide a moderate deceleration suitable for all routine operations

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12
Q

The selected autobrake setting should provide at least _____ feet less landing distance than runway length.

A

1,000

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13
Q

Conditions required for LAHSO?

A

RW must be dry
Weather minimum 1000’ and 3SM vis
Tailwind max of 3 kts
Winshear not reported

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14
Q

Minimum width for 180 turn (-400/-800)

A

-400: 153’
-800: 172’

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15
Q

Do not attempt to turn away from an obstacle within ____ ft of wingtip.

A

15’

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16
Q

Do not attempt to turn away from an obstacle within ____ ft of the nose (-400/-800)

A

-400: 56 ft
-800: 58 ft

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17
Q

Under what conditions would you abort an autostart (-400)?

A

No N1 rotation by idle N2
Fuel control switch is in RUN, the engine RPM is low, and the autostart switch is OFF
Oil pressure indication is not normal by the time the engine is stabilized at idle

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18
Q

When does the PF call for the After Takeoff checklist?

A

When flaps are called to be retracted up

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19
Q

What is Vapp with autothrottles disengaged?

A

Vref+1/2 HW+full gust not to exceed 20 kts

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20
Q

What is the minimum Vapp?

A

Vref+5kts

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21
Q

Maximum landing weight (MLDW) is the most restrictive of:

A

AFM
Brake energy
Climb weight
Field (landing distance)
Structural
Tire speed

22
Q

Maximum runway takeoff weight (MRTW) is the most restrictive of:

A

Brake energy
Climb
Field (Accel stop/go)
Obstacle
Tire speed
Vmcg

23
Q

What will trigger take off warning horn

A

Stab trim not in takeoff range
Speedbrake lever not in DN detent
Flaps not in takeoff position
Body gear not centered
Parking brake set

24
Q

Regarding early and late departures, when is an ARTR required?

A

More than 15 minutes early or

6 hours late (int)
1 hr late (dom)

25
Q

(-400) Flaps up maneuvering speed

A

Vref30+80, Above 680 thousand pounds full maneuvering capability is not attained until reaching Vref30+100

26
Q

(-400 & -800) Flaps 1 maneuvering speed

A

Vref30+60

27
Q

(-400 & -800) Flaps 5 maneuvering speed

A

Vref30+40

28
Q

(-400 & -800) Flaps 10 maneuvering speed

A

Vref30+20

29
Q

(-400 & -800) Flaps 20 maneuvering speed

A

Vref30+10

30
Q

How many degrees AOB does maneuvering speed guarantee?

A

40 degrees

31
Q

(-800) Flaps up maneuvering speed

A

Vref30+100

32
Q

At gross weights greater than 680,000 lbs, limit bank angle to ___ until 20 knots above the flaps up speed

A

15 degrees

33
Q

PF takeoff briefing

A

We will plan on a flaps ______takeoff

using TO ______,

with an assumed temperature of ____°

From RWY ______.

It will be an NADP2 departure flown in _______and VNAV.

We are cleared via the _______ departure up to _______ft.

Initial heading is ________

and we’ll expect radar vectors to ______

Transition altitude is ______

I’ll have weather radar displayed on my ND and you display terrain.

In the event of an engine failure after V1, we will accomplish the Engine Failure Procedure for RWY ___ which is a ___ (Standard, special, complex) and requires ____. We’ll accelerate for clean up at 1000’ then continue the climb to 3000’ and plan on a visual approach to runway 35L and back it up with the ILS. Any questions?

34
Q

Minimum items for takeoff brief

A

Flap setting, thrust setting, runway, ATC clearance with altitude, lateral and vertical modes, transition altitude, EFP, any update to CRM/safety brief

35
Q

Approach and landing brief parts

A

Approach, Missed approach, landing conditions

36
Q

Advance thrust levers to approximately ___ % N1 prior to engaging throttles for takeoff.

A

70% (-400)
45% (-800)

37
Q

Desired pitch attitude for rotation

A

15° (-400)
11-14 (-800)

38
Q

Pilot monitoring calls on takeoff roll

A

Thrust set (by 80 knots)
80 knots
V1
Rotate
V2
Positive rate (on altimeter and VSI)

39
Q

What is an NADP1 and when is it used

A

Thrust reduction at 1500 and clean up at 3000 use is listed in ABG when required

40
Q

What is an NADP2 and when is it used

A

Standard maneuver 1000 feet for clean up and acceleration

41
Q

When shall PF have hands on the yoke and throttles and feet on rudder pedals?

A

Takeoff- from gear up until completion of After Takeoff Checklist

Approach- from initial slat/flap extension until a safe taxi speed is achieved

Go around- from initiation of go around until completion of the after takeoff checklist

42
Q

Max weight for 3 engine taxi

A

725K

43
Q

Max weight for 2 engine (symmetrical) taxi

A

660K

44
Q

Call outs visual approach

A

PM: 1000ft stable
PF: RW in sight

PM: 500 ft stable
PF: Landing

45
Q

Autoland callouts

A

PM: 1000 FT Stable
PF: Mins _ LAND _

PM: 500 FT stable
PF: Continuing

PM: Approaching Minimums
PM: Minimums
PF: Landing

46
Q

Best angle (-400)

A

Vref30+100

47
Q

Best angle (-800)

A

Vref30+(104-114)

48
Q

Max rate (-400)

A

Vref30+140 to 0.82 or UP+60

49
Q

Max rate (-800)

A

Vref30+120 to 0.83

50
Q

Why is the initial cruise altitude used on the FMC

A

3 packs remain in high flow until FMC cruise altitude

yupi-s-TiSiTi. (24 decks)

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