FM Ops Limits Flashcards

1
Q

Maximum Operating Pressure Altitude 787-8/9

A

43,100

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

Maximum Operating Pressure Altitude 787-10

A

41,100

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

Maximum Takeoff and Landing Pressure Altitude

A

14,000

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

MAXIMUM TAKEOFF AND LANDING TAILWIND COMPONENT

A

15 kts

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

Maximum Landing Gear Speed

A

270 kts/.82M

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

Maximum Landing Gear Extended Speed

A

270 kts/.82M

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

Severe turbulence at and above 25,000 feet

A

310 knots/.84 Mach (whichever is lower)

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

Severe turbulence below 25,000 feet

A

290 KIAS

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

Takeoff Crosswind Guidelines (787-8)

A

40 Kts

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

Takeoff Crosswind Guidelines (787-9)

A

40 Kts

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

Takeoff Crosswind Guidelines (787-10)

A

40 kts

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

Landing Crosswind Guidelines

A
40 Kts  
Sideslip only (zero crab) landings are not recommended with crosswind components in excess of 25 knots. This recommendation ensures adequate ground clearance and is based on maintaining adequate control margin.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

ICING CONDITIONS DEFINITION

A

Icing conditions exist when OAT (ground) or TAT (flight) is 10°C or below.

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

Do not engage the autopilot below a minimum engagement altitude of

A

200 feet AGL after takeoff.

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

Autoland capability may only be used for operations to runways at or below

A

8400 feet airport field elevation.

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

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below

A

135 feet AGL

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

With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25°, the autopilot must be disengaged below

A

100 feet AGL.

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

If the glidepath angle for approach is greater than 3.77°, the autopilot must be disengaged no later than

A

50 feet below DH/MDA.

19
Q

Do not use FLCH on final approach below

A

1000 feet AFE.

20
Q

Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations:
Headwind

A

25 knots

21
Q

Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations:
Tailwind

A

15 knots

22
Q

Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations:
Crosswind

A

15 knots

23
Q

ILS AUTOMATIC LANDING Maximum wind component speeds:

Headwind

A

25 knots

24
Q

ILS AUTOMATIC LANDING Maximum wind component speeds:

Tailwind

A

15 knots

10 knots for CAT II/III

25
Q

ILS AUTOMATIC LANDING Maximum wind component speeds:

Crosswind

A

25 knots

15 knots for CAT II/III

26
Q

The maximum glideslope angle

A

3.25°.

27
Q

The minimum glideslope angle is

A

2.50°.

28
Q

Do not operate HF radio during

A

fueling operations.

29
Q

Oil Quantity

Minimum prior to start

A

18 quarts

30
Q

Oil Temperature

Oil temperature must be greater than_______for engine start.

A

-40°C

31
Q

Intentional selection of reverse thrust in flight is_______________

A

prohibited.

32
Q

Backing the aircraft with use of reverse thrust is____________________

A

prohibited.

33
Q

Do not use speed brakes in flight below____________

A

1000 feet AGL.

34
Q

AIRSPEED UNRELIABLE

A
  1. Autopilot disconnect switch . . . . . . . . . . . . .Push

2 A/T ARM switches (both) . . . . . . . . . . . . . . . . OFF

3 F/D switches (both) . . . . . . . . . . . . . . . . . . . . . OFF

4 Set the following gear up pitch attitude and thrust: Flaps extended . . . . . . . . . 10° and 85% N1
Flaps up…………………………… 4° and 70% N1

35
Q

CABIN ALTITUDE

A

1 Don oxygen masks.

2 Establish pilot communications.

36
Q

Dual Eng Fail/Stall u

A

1 FUEL CONTROL switches (both) …. CUTOFF, then RUN Attempts to clear stall condition and allow engines to be put into start mode.

2 RAM AIR TURBINE switch ….Push and hold for 1 second

37
Q

Loss of All Displays

A

1 See the EFB, Documents, LOSS OF ALL DISPLAYS.

38
Q

Smoke, Fire or Fumes

A

1 Don oxygen masks, if needed.

2 Establish pilot and cabin communications.

39
Q

FD DOOR AUTO UNLOCK

A

1 FD DOOR ACCESS selector. . . . . Rotate to DENY and hold for 1 second

40
Q

STABILIZER

A

1 STAB cutout switches (both) . . . . . . . . . CUTOUT

2 Do not exceed the current airspeed.

41
Q

Do not attempt to make a turn away from an obstacle within _______ feet of the wing tip or __________feet of the nose

A

15 feet
55 feet

42
Q

Minimum pavement required for a 180 degree turn

A

787-9: 138’4”
787-9: 154
787-10: 176’7”

180 degree turn on a 150 ft runway requires differential braking

787-10

43
Q

Max crosswind for SA CAT 1 approaches

A

15 kts

44
Q

Restriction on control inputs

A

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or yaw (e.g. large side slip angles) as they may result in structural failure. At any speed, including below VAT.