Limitations Flashcards
What are the Dimensions:
Wingspan?
Tail Height?
Length?
Wingspan: 50.88 m
Tail Height: 15.85 m
Length: 54.94 m
Min Pavement Width
44.6 m
Eye Height at Touchdown
8.25 m
Max Altitude
43,100 ‘
Turbulence Penetration Speed
290 KIAS / 0.78 M
Max Runway Slope
+/- 2%
Max Take Off and Land Altitude
8,400 ‘
Autoland:
Max Headwind
Max Crosswind
Max Tailwind
Max Headwind: 25 kts
Max Crosswind: 25 kts
Max Tailwind: 15 kts
Max Take Off and Land Tailwind
15 kts
Min autopilot engage height
200 ‘ AGL
What is trim is prohibited with autopilot engaged?
Aileron trim
Max Altitude for flap extension?
20,000 ‘
Min Alt for Speedbrake extension?
800 ‘
Speedbrake must not be used with what configuration?
Landing flaps 25 or 30
APU Starter Cycle
3 x start attempts in 60 mins
APU Bleed Air
17,000 ‘
APU Electrical
43,100 ‘
When is ENG CONT IGNITION used?
- Must be selected ON in severe turbulence
- Automatic ON when ENG Anti-Ice ON in icing conditions
- Flap lever out of the UP position
Engine Starter Duty Cycle?
Continuous for 5 mins
Cool for 30 sec per min of operation
Max Fuel Tank Temperature
49 °C
Min in flight Fuel Tank Temp (*JET A1)
-44 °C
(3 °C above the Fuel Freezing temp for specified fuel)
HF Radios
Do not use HF radios while refuelling
APU use while fuelling
Not allowed for start or shutdown
WX Radar use on ground
Do not use while in hangar, or 50 ft near a fuel spill or fuelling.
Do not use near ground personnel
Max Taxi Weight
187,333 kgs
Max Take Off Weight
186,880 kgs
Max Landing Weight
147,871 kgs
Max Zero Fuel Weight
140,160 kgs (Tasman 141,656 kgs)
What should flight crew NOT blank during take off?
ENG Vibratation display
Use of Centre Tank Fuel
Centre tank may contain up to 10,000 kgs of fuel with less than full main tanks, provided centre tank fuel weight plus actual zero fuel weight does not exceed MZFW and CofG limits observed
Fuel Imbalance
1,134 kgs (21,772 kgs or less)
linear reduction to 680 kgs (36,197 kgs)
Centre Fuel Tank Pumps
Intentional Dry run of Centre tank fuel pumps prohibited
Time limit for use of TO/GA thrust
5 mins
Use of Wing Anti-Ice
The wing anti-ice system may be used as a de-icer or anti-icer in flight only.
Wing anti-ice must not be used with TAT above 10 °C
Icing conditions exist when
OAT is 10° C or below during ground operations, takeoff, initial climb or go-around or
TAT is 10° C or below in-flight and
visible moisture (clouds, fog with visibility less than one mile, rain, snow, sleet, ice crystals, and so on) is present or
standing water, ice, or snow is present on the ramps, taxiways or runways.
Use of Engine Anti-Ice
Engine anti-ice must be ON during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temperature is below -40° C SAT.
Max Cabin Diff Press
8.6 psi
Pax Oxy auto deploy
14,000 ‘
The emergency lighting system is powered by ? and for how many minutes?
Remote batteries for 15 mins
Flight Deck Temp selectors set temps between
18-30 °C
In the automatic mode, the outflow valve will close if cabin altitude exceeds?
11,000 ‘
The CABIN ALT light illuminates if cabin altitude exceeds?
10,000’
Flap limit speeds:
Flaps 1
Flaps 5
Flaps 15
Flaps 20
Flaps 25
Flaps 30
Flaps 1: 250 KIAS
Flaps 5: 230 KIAS
Flaps 15: 210 KIAS
Flaps 20: 210 KIAS
Flaps 25: 180 KIAS
Flaps 30: 170 KIAS
RAT provides adequate hydraulic power above what speed
130 KIAS
Nose wheel steering angle with tiller
65°
Nose wheel steering angle with rudder
7°
Max speed with geer extended
270 KIAS / 0.82 M
Max speed to retract gear
270 KIAS
Fuel Quantities
Tasman:
L or R Main Tank: 19,355 kgs
Centre Tank: 38,517 kgs
Total: 77,227 kgs
General:
L or R Main Tank: 18,267 kgs
Centre Tank: 36,349 kgs
Total: 72,882 kgs
Taxi Speeds…
Straight
Lo-Vis/slippery spd
Turn
Turn 90°
Straight: 30 kts
Lo-Vis / Slippery: 10 kts
Turn: 15 kts
Turn 90°: 10 kts
