FM Ops Limits Flashcards

(48 cards)

1
Q

Maximum Operating Pressure Altitude 787-8/9

A

43,100

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2
Q

Maximum Operating Pressure Altitude 787-10

A

41,100

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3
Q

Maximum Takeoff and Landing Pressure Altitude

A

14,000

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4
Q

MAXIMUM TAKEOFF AND LANDING TAILWIND COMPONENT

A

15 kts

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5
Q

Maximum Landing Gear Speed

A

270 kts/.82M

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6
Q

Maximum Landing Gear Extended Speed

A

270 kts/.82M

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7
Q

Severe turbulence at and above 25,000 feet

A

310 knots/.84 Mach (whichever is lower)

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8
Q

Severe turbulence below 25,000 feet

A

290 KIAS

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9
Q

Takeoff Crosswind Guidelines (787-8)

A

40 Kts

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10
Q

Takeoff Crosswind Guidelines (787-9)

A

40 Kts

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11
Q

Takeoff Crosswind Guidelines (787-10)

A

40 kts

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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.
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13
Q

ICING CONDITIONS DEFINITION

A

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

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14
Q

Do not engage the autopilot below a minimum engagement altitude of

A

200 feet AGL after takeoff.

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15
Q

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

A

8400 feet airport field elevation.

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16
Q

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

A

135 feet AGL

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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.

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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.

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19
Q

Do not use FLCH on final approach below

A

1000 feet AFE.

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20
Q

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

21
Q

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

22
Q

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

23
Q

ILS AUTOMATIC LANDING Maximum wind component speeds:

Headwind

24
Q

ILS AUTOMATIC LANDING Maximum wind component speeds:

Tailwind

A

15 knots

10 knots for CAT II/III

25
ILS AUTOMATIC LANDING Maximum wind component speeds: | Crosswind
25 knots | 15 knots for CAT II/III
26
The maximum glideslope angle
3.25°.
27
The minimum glideslope angle is
2.50°.
28
Do not operate HF radio during
fueling operations.
29
Oil Quantity | Minimum prior to start
18 quarts
30
Oil Temperature | Oil temperature must be greater than_______for engine start.
-40°C
31
Intentional selection of reverse thrust in flight is_______________
prohibited.
32
Backing the aircraft with use of reverse thrust is____________________
prohibited.
33
Do not use speed brakes in flight below____________
1000 feet AGL.
34
AIRSPEED UNRELIABLE
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
CABIN ALTITUDE
1 Don oxygen masks. 2 Establish pilot communications.
36
Dual Eng Fail/Stall u
1 FUEL CONTROL switches (both) …. CUTOFF, then RUN 2 RAM AIR TURBINE switch ….Push and hold for 1 second
37
Smoke, Fire or Fumes
1 Don oxygen masks, if needed. 2 Establish pilot and cabin communications.
38
FD DOOR AUTO UNLOCK
1 FD DOOR ACCESS selector. . . . . Rotate to DENY and hold for 1 second
39
STABILIZER
1 STAB cutout switches (both) . . . . . . . . . CUTOUT 2 Do not exceed the current airspeed.
40
Do not attempt to make a turn away from an obstacle within _______ feet of the wing tip or __________feet of the nose
15 feet 55 feet
41
Minimum pavement required for a 180 degree turn
787-9: 138’4” 787-9: 154 787-10: 176’7” 180 degree turn on a 150 ft runway requires differential braking 787-10
42
Max crosswind for SA CAT 1 approaches
15 kts
43
Restriction on control inputs
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.
44
GLS Autoland
Do not autoland from a GLS approach even if Land 2 or Land 3 are displayed
45
ABORTED ENGINE START L,R
1. FUEL CONTROL SWITCH (affected side)……………CUTOFF
46
Do not align IRS at North/South latitudes
Greater that 78.14.75
47
Demonstrated RNP Flight Operations Values in NM for mode of flight
48
Checklists on QRC (8)
Aborted Engine Start Drift down Dual Eng Fail/Stall Engine Svr Damage/Sep Fire Engine Tailpipe Loss of All Displays Smoke, Fire, Fumes Evacuation