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Ual > Limitations > Flashcards

Limitations Flashcards

1
Q

Operating Pressure Altitude

A

41,000 feet

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2
Q

Takeoff/Landing Pressure Altitude

A

10,000 feet

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3
Q

Minimum runway width

A

100 feet (30 meters)

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4
Q

MAXIMUM TAKEOFF/LANDING TAILWIND COMPONENT

A

★15 knots

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5
Q

Maximum gear extension speed

A

270 knots/.82 Mach

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6
Q

SEVERE TURBULENCE PENETRATION SPEED

A

Climb and Descent ★280 knots/.76 Mach
Cruise TURB N1 setting from cruise page

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7
Q

Takeoff Crosswind Component Guidelines
6 dry
5 wet
dry or wet Landing

A

33
25
37

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8
Q

Maximum cabin pressure differential

A

9.10 psi

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9
Q

Limit on pack takeoff

A

When engine bleeds are on (either one or both), do not operate air conditioning
packs in high for takeoff, approach, and landing.

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10
Q

Duct pressure

A

A duct pressure difference of more than 8 PSI may indicate a mechanical
malfunction. If a duct pressure split is observed after bleeds are configured for
flight, and the lowest indication is approximately 18 PSI or less, contact
Maintenance

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11
Q

Engine anti ice ground

A

OAT 10c or below
Visible moisture in any form is present (i.e., clouds, fog with visibility of 1 mile
or less, rain, snow, sleet, or ice crystals), or
While operating on ramps, taxiways, or runways where snow, standing water,
or slush may be ingested by the engines or freeze on the engines, nacelles,
or engine sensor probes.

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12
Q

Engine anti ice flight

A

10 c TAT

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13
Q

Engine ignition regarding anti ice

A

Must be turned on before anti ice

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14
Q

Window heat on prior to takeoff time

A

10 min

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15
Q

Minimum Altitude for Use of Autopilot on Approach

A

ILS/GLS coupled approaches (no autoland) ★50 feet AGL
Non-precision approaches ★50 feet below MDA/DA

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16
Q

Level change

A

Do not use LVL CHG on final approach below 1000 feet AFE.

17
Q

Normal starter duty cycle:

A

Multiple consecutive start attempts are permitted. Each start attempt is limited to
2 minutes (700/800/900/9ER)/3 minutes (MAX) of starter usage.

18
Q

Reduced thrust in ALTN mode

A

Operation with assumed temperature reduced for takeoff thrust is not permitted
with the Electronic Engine Control (EEC) in ALTN mode.

19
Q

APU MAXIMUM ALTITUDE
Bleed / electrical

A

APU bleed and electrical 10,000 feet
APU bleed 17,000 feet
APU electrical load 41,000 feet

20
Q

Holding in icing conditions

A

Holding with flaps extended prohibited

21
Q

Speed brake lever in flight operation greater flaps 10

A

In flight, the speed brake lever SHOULD not be extended beyond the ARMED
detent with greater than flaps 10 selected.

22
Q

Max fuel imbalance

A

Not exceeding 1000 pounds

23
Q

Minimum accumulator brake pressure

A

1200 psi

24
Q

Engine cool down time

A

3 minutes or at the gate

25
Q

Runway slope

A

+-2%

26
Q

Boeing flight deck door needs to be checked when

A

Operational check each day

27
Q

Wing anti ice and de ice fluid limitation

A

Unless protected by type 2 or type 5 use wing anti ice

28
Q

Landing operations on runways with condition code 1 or 0

A

takeoff prohibited

29
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS any configuration

A

Max 2.5g /-1.0g

30
Q

During takeoff do not use wing anti-ice.

A

until after the first thrust reduction

31
Q

Use of aileron trim with the autopilot engaged

A

is prohibited.

32
Q

APU WARMUP Time for bleed air

A

1 min NG 2 min MAX

33
Q

FLAP EXTENSION ALTITUDE

A

20,000

34
Q

The maximum allowable in-flight difference between Captain and First Officer
altitude displays for RVSM operations is

A

200 feet.

35
Q

Minimum fuel for stationary ground operation Of electric hyd pumps

A

1675 pounds related tank

36
Q

TIRE GROUNDSPEED

A

195 NG
204 MAX

37
Q
A

Ual (2 decks)

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