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Flashcards in Limitations 787 Deck (29)
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1
Q

Do not engage the autopilot below a minimum engagement altitude of ———— feet after takeoff

A

200

2
Q

Autoland capability may only be used for operations to runways at or below————feet airport field elevation.

A

8,400

3
Q

Without Land 2 or Land 3 annunciated, the autopilot must be disengaged below ————-feet AGL

A

135

4
Q

Do not use FLCH on final approach below ———-feet AFE

A

1000

5
Q

Maximum wind component speeds when takeoff weather minima are predicated on HIUD takeoff operations

Headwind

A

25 KNOTS

6
Q

Maximum wind component speeds when takeoff weather minima are predicated on HIUD takeoff operations

Tailwind

A

15 KNOTS

7
Q

Maximum wind component speeds when takeoff weather minima are predicated on HIUD takeoff operations

Crosswind

A

15 Knots

8
Q

Maximum wind component speeds when using autopilot ILS Automatic Landing

Headwind

A

25 Knots

9
Q

Maximum wind component speeds when using autopilot ILS Automatic Landing

Tailwind

A

15 Knots

10!Knots for CAT II/III

10
Q

Maximum wind component speeds when using autopilot ILS Automatic Landing

Crosswind

A

25 Knots

15 Knots for CAT II/III

11
Q

The maximum glideslope angle is ———-

A

3.25 degrees

12
Q

The minimum glideslope angle is ————-degrees for AP Autoland Ops.

A

2.50

13
Q

Maximum operating pressure altitude

  • 8 and -9
  • 10
A

43,100

41,100

14
Q

Maximum Takeoff and Landing Tailwind Component

A

15 Knots

15
Q

Turbulent Air Penetration Speed

At and above 25,000 feet

Below 25,000 feet

A

310 Kts or .84 Mach whichever is Lower

289 KIAS

16
Q

Takeoff and Landing Crosswind Guidelines -8, -9, -10

All weights Dry Braking Action

A

40 Knots Maxim

Anything less than Dry runway with a runway code of less than. 6 use table

17
Q

Icing conditions exist when OAT (ground) or TAT (flight) is ——- or below

A

10 degrees C

18
Q

Minimum Oil Quantity prior to start

A

18 Quarts

19
Q

Minimum Oil Temperature prior to engine start

A

-40 degrees C

20
Q

RECALL URPT

A
UPSET
PUSH
ROLL
THRUST
STABILIZE
21
Q

4 Characteristics of a stall

A

BUFFETING
LACK OF PITCH
LACK OF ROLL
INABILITY TO ARREST DESCENT

22
Q

Airspeed Unreliable

flaps extended

A
  1. Autopilot…..Off
  2. A/T armband both …off
  3. Set the gear up pitch … 10° / 85% N1
23
Q

Airspeed Unreliable

Flaps up

A
  1. Autopilot…..Off
  2. A/T armband both …off
  3. Set the gear up pitch … 4°/ 70% N1
24
Q

CABIN ALT

A
  1. Don O2 Masks

2. Establish pilot and cabin communications

25
Q

SMOKE. FIRE. FUMES.

A
  1. Don O2 Masks

2. Establish pilot and cabin communications

26
Q

DUAL ENGINE FAILURE

A
  1. Fuel control switches (both) …… CUTOFF, then RUN

Attempt to clear stall condition and allow engines to be put in start mode

  1. RAM AIR TURBINE ……..Push and hold 1 second
27
Q

FD DOOR AUTO UNLOCK

A
  1. FD DOOR ACCESS selector ………rotate to DENY and hold for 1 second
28
Q

LOSS OF ALL DISPLAYS

A
  1. See EFB documents, LOSS OF ALL DISPLAYS
29
Q

STABILIZER

A
  1. STAB CUTOUT SWITCHES …..CUTOUT

2. DO NOT EXCEED the current airspeed