Limits Flashcards

(36 cards)

1
Q

maximum takeoff crosswind (all flaps, dry)

A

28 knots

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2
Q

max wet t/o crosswind

A

20 knots

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3
Q

max ldg xw dry

A

35

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4
Q

max ldg xw wet

A

30

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5
Q

rvsm with eo/ir

A

not allowed, needs to be retracted

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6
Q

on the ground display difference between p and cp

A

50 ft from sea level to 5000, 60 feet from 5001 to 10000

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7
Q

generators

A

if a generator load exceeds 41% while on deck, advance thrust to a min of 32%

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8
Q

oil quantity

A

overland ops: 60% full (12 qts)
overwater ops: 60% full (12 qts) or 7 qts plus 1 qt per total flight hour. whichever is higher. Flights should plan to arrive with 7 qts or more for possible toga operation

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9
Q

engine starter duty cycle

A

2 minutes

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10
Q

N2

A

do not try to engage the starter if n2 is more than 55%

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11
Q

max to egt

A

950-965 c 3 minutes
950 c for 5 minutes
if exceeds 950 but is less than 965 for less than 3 minutes, flight may be continued. thrust should be reduced below 950c as soon a flight conditions permit it

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12
Q

engine failure after takeoff

A

max time for operating at 950c goes from 5 to 10 minutes

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13
Q

max cont egt

A

925c

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14
Q

max start egt

A

725c

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15
Q

max n1

A
  1. 7% 20 seconds

104. 0% continuous

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16
Q

max n2

17
Q

min oil px

A

13psi

during negative g you can operate below 13 psi for 10 secs before shutdown is required

18
Q

max oil temp

A

155c
140-155c 45 minutes
140c continuous

19
Q

engine idle prior to shutdown

20
Q

engine ignition

A

shall be set to continuous if flying thru heavy rain, hail or sleet. shall be set to FLT is heavy turb is encounterd

21
Q

windshear takeoffs

A

reduced thrust takeoffs not recommended if winshear conditions exist.

22
Q

eec in alternate

A

no reduced thrust or atm takeoffs, no autothrottle, no fmc n1, and both eecs have to be in alternate

23
Q

reverse thrust

A

not to be used in flight or for backing

24
Q

unsymmetrical maneuver

A

a maneuver that includes a simultaneous combination of lateral control and elevator inputs such that high roll rate (greater than 10 deg/sec) is coincident with a/c load factor greater than 1.0gs.

25
symmetric flight g limit
min for stores loaded flaps 1-40 0.3. min for gear down or in transition 0.5. min for weapon bay door transition 1.0. max for clean wings with or w/o pylons flaps up-40 is 1.8. max for flaps 30-30 with no stores and greater than 149.8K 1.4. stores loaded flaps up max 1.4. stores loaded 25-40 1.3 max. gear down max 1.8. weapn bay door max 1.4.
26
weights
max taxi/tow-189.7 max t/o weight-189.2 max landing weight-149.8 max zfw-141.8
27
min altitude on station
200 feet. 1000 feet for pilot seat swaps
28
fuel temperature
tank feeding engine-59c tank feeding apu-59c tanks not feeding engine or apu-62c min is 3c above freezing point of fuel being used or -43c, whichever is higher
29
max lateral fuel imbalance
1000lbs for ground and flight
30
hydraulics min fuel
min fuel for ground operation of electric pumps is 1675lbs in related tank
31
apu limits
in flight- apu bleed plus electric load maximum 10000ft on deck-apu bleed plus electrical load 14000ft apu bleed only 17000ft apu electrical load only 41000ft
32
max flap extension altitude
21000ft
33
speedbrakes
do not deploy unless radio altitude is less than 1000ft
34
speedbrake
will stay in flt detent. deployment above 1.5gs is prohibited
35
landing lights
limit landing light illumination to less than 5 minutes when not in flight. does not apply to led landing lights
36
look ahead terrain alerting
do not use within 15 nm of takeoff, approach, or landing at an airport not contained in the system.