Limitations Flashcards
MAX TAXI WEIGHT
144,000 lb
N311GT
MAX TAXI WEIGHT
150,355 lb
Max Takeoff Weight
143,500 lb
N311GT
MAX TAKEOFF WEIGHT
149,914 lb
MAX LANDING WEIGHT
121,000 lb
N311GT
MAX LANDING WEIGHT
123,899 lb
MAX ZERO FUEL WEIGHT
113,000 lb
N311GT
MAX ZERO FUEL WEIGHT
116,844 lb
MIN OPERATING WEIGHT
78,000 lb
N311GT
MIN OPERATING WEIGHT
78,000 lb
Use of aileron trim with__________ ___________ is prohibited.
Autopilot Engaged
Do not engage auto pilot on takeoff below ________ _________ AGL
Below 1000 feet
For single channel ops during approach, the autopilot shall not remain engaged below ________ _________ AGL
50 feet AGL
Auto-land capability can only be used with flaps _____or_______ with both ___________ ___________
30 or 40. Engines Operative
MAX ENGINE START EGT
725 C
Intentional selection of reverse thrust in flight is __________________
Prohibited
APU
BLEED PLUS ELECTRICAL MAX ALT
10,000 feet
APU
BLEED AIR ONLY MAX ALT
17,000 feet
APU
ELECTRICAL MAX ALT
35,000 feet
APU
MAX OPERATING ALT
37,000 feet
APU
If there are multiple aborted start attempts, ___________minutes cooling is required between second and third start attempt. A wait of _________ ___________ after third start attempt.
Five
One hour
Max flap extension altitude is ___________ feet pressure altitude
20,000
Avoid _______ and _____________ _______________ ______________ ______________, especially in combination with large changes in pitch, roll, or yaw. As they may result in structural failure at any speed ___________ ____________ _____
Rapid and Large Alternating control inputs
Including below Va
When extending and retracting flaps with the ALTERNATE FLAPS position switch, allow _______ ______________ after releasing the ALTERNATE FLAPS switch before moving the switch again to avoid damage to the alternate flaps motor clutch.
15 seconds
Regarding Alternate Flaps
After a completed extend/retract cycle, ie ____ to _____ and ________ to _______ allow ________ __________ cooling before attempting another extension.
0 to 15 and back to 0
5 minutes
Do not operate weather radar in the _______________ or within _________ __________ of any personnel Or fuel spill
Hanger,
50 feet
Lateral imbalance between main tank 1 and 2 must be scheduled to ___________
Zero
Random fuel imbalance must not exceed _____________ lbs for taxi, takeoff, flight or landing.
1000 lbs
Main tanks must be scheduled to be full if center tank contains more than _____________lbs fuel
1000 lbs
Do not open main deck cargo door in actual or anticipated winds exceeding ____________ knots
45
Max glideslope angle __________degrees
3.25 degrees
Minimum Glideslope angle is ____________ degrees
2.5 degrees
Max takeoff and landing altitude_______________ ________________ ____________Altitude
With “Cabin Altitude” and “Takeoff Config” installed and operative
_____________ ___________ ______________ Altitude
8,400 feet pressure altitude
9,000 feet pressure altitude
Max aircraft operating altitude ____________ feet
37,000
Max Takeoff and landing tailwind component
10 knots
Demonstrated takeoff and landing crosswind component
35 knots
Do not operate HF radios during __________________
Refueling
Turbulent Airspeed
264 KIAS / .65M
Max allowable in-flight difference between Altimeters Captain and FO for RVSM
200 feet
Max allowable On-Ground difference between Altimeters Captain or FO and Feild Elevation for RVSM
75 feet
Max cabin differential
8.65 psi
The use off frequency _____.000 and 120._____ is prohibited on which comm radio?
120.000
120.005
VHF #2
Max Generator drive temp
157C
Max Engine N1
106%
Max Engine Takeoff EGT
930C
Max Engine Continuous EGT
895C
Min Engine Oil Pressure
13 psi
Cont Ignition must be used during _________, ___________ ,and ______-_______ Operations
Takeoff
Landing
Anti-Ice
Max APU EGT
760C
Max APU Continuous EGT
710C
Min fuel temp
Freeze point +3C or -45C whichever is higher
Max fuel temp
49C
For use of Electric Hydraulic Pump the respective side fuel main tank must contain a minimum of_________LBS
1675 lbs
The Main wing tanks hold ___,________lbs each
10,043 lbs
The Center Tank holds ____,__________ lbs
15,497 lbs
Total Fuel load is ______,______________ lbs
35,583 lbs
