Limitations Flashcards
Max runway slow
+/- 2%
Max operating Altitude
43,100 feet
Max takeoff and landing altitude
8,400 feet
Turbulent penetration airspeed
290 kts/ .78 Mack
Whichever is lower
Max takeoff and landing tail wind
10 kts
Ground wind limits for doors
40 kts while opening or closing
65 kts while open
Max crosswind for takeoff braking action good
40 KTS
True or false
Crosswind guidelines are considered limitation
False
Max taxi weight (MTW)
409,000 lbs
Max takeoff weight
408,000 lbs
Max landing weight (MLW)
320,000 lbs
Max zero fuel weight
295,000 lbs
MIN oxygen ETOPS
1350 PSI
MIN oxygen non ETOPS
1250 PS
MAX cabin pressure difference
9.10 Psi (Red tick on cabin DIFF indicator)
MAX Cabin difference for T/O and landing
0.125 psi (236 feet below airport Px Alt.)
APU starter duty cycle
Max 3 attempts in 60 mins
1 min cooling between attempts.
Max Altitude to use APU Bleed Air
17,000 feet
Min Altitude for Autopilot engagement for TOGA
250 feet
Min. Altitude for Autopilot engagement for ILS Approach
50 feet below MDA(H)/DA(H)
Min. Altitude for Autopilot engagement for single channel ILS Approaches
100 feet AGL
Minimum altitude for auto pilot engagement for Autoland (2 or 3 Autopilots)
Touchdown/roll out
Flaps setting for Autoland
Flaps 25/30
Max crosswind or headwind for Autoland
25 kts
Max crosswind for Autoland cat II/III
15 kts
Max tailwind for Autoland
10 kts
What type of radios does not operated while refueling
HF radios
How many times you can reset a circuit breaker and after how long is the cooling period
Once, two minutes
Which circuit breaker you can reset after it tripped
Fuel pump or fuel valve
Trust rating for capital CF6-80C2B6F Engine
60,200 pounds
N1 and N2 limits for 2B6F Engines
N1 117.5%
N2 112.5%
Max EGT for a start
Ground/in-flight
Ground 750 Unlimited time
In flight 870 40 seconds transient
Max EGT for takeoff
960
Max EGT for Max continues
925
Max time at takeoff trust for aircraft N651GT
Five minutes (641GT 10 minutes)
Normal engine starter duty cycle
One minute on
One minute off indefinitely
Extended engine starter duty cycle
0 to 5 minutes on,Then off until 0% N2
5 to 10 Minutes on, then 20 minutes off
10 to 15 Minutes on, then 30 minutes off
Starter re-engagement N2
0% recommended
0-20% permissible
21-30% only if on fire
>30% may cause damage to starter
Min. engine oil pressure
10
Max oil temp
160°C continues
175°C 15 minutes max
Minimum oil quantity for dispatch
17
Continue ignition on
Moderate to heavy rain Moderate to severe turbulence Volcanic ash Icing conditions Standing water or slush
When is continuing ignition turned on automatically
When Engine Anti-ice is on
When leading edge flaps are extended (Because require for takeoff and landings)
Max altitude to extend flaps
20,000 feet
Use of speed breaks in flight with flaps beyond_______Is not recommended
20
Do not use speedbrakes below
800 feet AGL
From engine start to engine shut down_______
Messages are the primary means of alerting crew to non-normal conditions or improper configuration
EICAS
Max Allowable fuel weighed in center tank
85,200 pounds
38,647 kg
Maximum allowable fuel weight in left or right tanks
43,097 pounds
19,549 kg
True or false
Fuel tanks have to be filled in a specific order
False
Max fuel weight in center tank with wing tanks less than full
22,050 pounds
10,000 kg
Max allowable fuel in balance between left and right main thanks
2500 pounds when main tank fuel is 48,000 pounds or less
1500 pounds when main tank fuel is greater than 79,800 pounds
Engine Anti-ice must be on
Below 22,000 feet in icing conditions
Prior to thrust reduction for descent and icing conditions
Max allowable in-flight difference between captain And FO how to display in RVSM
200 feet
Max difference on ground between captain and FO altitude displays
SL
5K
10K
40
45
50
Max difference on ground between captain or FO Altitude and field elevation
SL
5K
10K
75
75
75
MMO
.86 Mack
Glide slope Angle for outoland
Max min
- 25
2. 5
How many hydraulics do you need to autoland
3
