Limitations Flashcards

(40 cards)

1
Q

787 Approach Category

A

Straight In Approach CAT D
Circling Approach CAT D

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2
Q

787 Maximum Operating Altitude

A

787-8 43,100’
787-9 43,100’
787-10 41,100’

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3
Q

Maximum Takeoff and Landing Pressure Altitude

A

14,000’

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4
Q

Maximum Runway Slope

A

+/- 2%

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5
Q

Maximum Tailwind for Takeoff and Landing

A

15 Knots

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6
Q

Maximum Landing Gear Speeds

A

Operation 270/.82
Extended 270/.82

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7
Q

Sever Turbulence Penetration Speed

A

At or above 25,000’ 310/.84
Below 25,000’ 290

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8
Q

When is a rolling takeoff advised

A

Crosswind greater than 20 Knots
Tailwind greater than 5 Knots

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9
Q

Maximum N1 for a static engine run:

A

55% N1

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10
Q

Maximum crosswind all types, dry runway, with percent MAC less than or equal to 20%

A

40 Knots

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11
Q

Maximum Landing Weight 787-8

A

380.0

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12
Q

Maximum Landing Weight 787-9

A

425.0

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13
Q

Maximum Landing Weight 787-10

A

445.0

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14
Q

Maximum Pressurization

A

Cruise 9.9 psi
Takeoff and Landing .11 psi

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15
Q

When do icing conditions exist

A

Ground 10c OAT
In-Flight 10c TAT

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16
Q

Do not operate Engine or Wing Anti-Ice when

A

Ground Greater than 10c
In Flight Greater than 15c

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17
Q

Minimum Autopilot Engagement Altitude

18
Q

AutoLand capability may only be used for operations at airports at or below:

19
Q

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

20
Q

With LAND 2 and LAND 3 annunciated and glide slope angle greater than 3.25 degrees, the autopilot must be disengaged below:

21
Q

If the glide path angle is greater than 3.77 degrees the autopilot must be disengaged no later than:

A

50’ below DH or MDA

22
Q

Do not use FLCH below:

23
Q

Maximum wind component speeds when takeoff weather calls for HUD Takeoff Operations

A

Headwind 25 Knots
Crosswind 15 Knots
Tailwind 15 Knots

24
Q

Maximum crosswind for a Special Authorization CAT 1 Approach:

25
Maximum Autoland Wind Components
Headwind 25 Knots Crosswind 15 Knots Tailwind 10 Knots
26
APU Start attempts and cooling
2 attempts then 5 min cooling before a 3rd attempt.
27
HF Radio Restriction
Do not operate HF radios during fueling operations.
28
Maximum Engine EGTs
Ground Start 750 Flight Start 875 Maximum Continuous 1030 Takeoff and Go Around 1065 for 5 minutes
29
Minimum oil quantity prior to engine start
18 Quarts
30
Minimum oil temperature prior to engine start
-40c
31
Reverse Thrust Restrictions
Do not use reverse thrust in flight Do not attempt to back up using reverse thrust Do not attempt to go around once reverse thrust is deployed.
32
Maximum Engine RPM
N1 108.5 N2 117.5
33
Maximum Flap Operation Altitude
20,000'
34
Speed Brake Restriction
Do not use below 1,000'
35
Prior to takeoff, the maximum allowable altimeter difference
75' between Captain and FO's altimeter and 75' between altimeters and field elevation. 200' between Captain and FO's altimeter before entering RVSM airspace.
36
EICAS Messages that prohibit entry into RVSM airspace.
NAV AIR DATA SYS ALTITUDE ALERT
37
Maximum fuel imbalance for taxi, takeoff, and landing
1500-2500 lbs depending on main tank fuel
38
Fuel Jettison Restriction
Do not jettison fuel while at flaps 30
39
Minimum Hydraulic Quantity
RF
40
Maximum Tire Speed
Takeoff 204 Knots Landing 226 Knots