Limitations Flashcards
Max Altitude Flaps/Slats Extended
20,000ft
Manoeuvre Limit Load Factors
Slats and Flaps Retracted -1g to + 2.5g
Slats and Flaps Extebded 0g to + 2.0g
Icing Conditions Definition
TAT +10 degrees C or below with visible moisture in flight.
Same on the ground but in addition vis less than 1.6km.
Max Take Off Weight
330-200 = 230,000kg /233,000kg
330-300 = 233,000kg /242,000kg
Max Landing Weight
330-200 = 180,000kg / 182,000kg
330-300 = 186,000kg /187,000kg
Max Zero Fuel Weight
330-200 = 160,000kg / 170,000kg
330-300 = 171,000kg/175,000kg
C of G limits for take off
(Check if outside) 18-33% MAC
VMO/MMO
330kts IAS
0.86M
Maximum design manoeuvring speed
If alternate or direct law are active then full aileron or rudder application or manoeuvres close to stalling angle of attack should be confined to speeds below VA
VA =M.78 above 27000ft 252-304kts SFC-27000ft
VFE speeds
Flap1 = 240kts (Intermediate APP)
Flap 1+F =215kts (Take off)
Flap 2 = 196kts
Flap 3 = 186kts
Flap Full = 180kts
VLO/VLE
IAS 250kts/M0.55
Alternate extension = Max 200kts IAS
Maximum Runway Slope
+/- 2%
During Towing Nose Wheel Angle to not be exceeded
65 degrees
NB mechanical stop is 95 degrees
High Engine Vibration
N1>=5.7
N2>=5.6
High Oil Temp
Between 165-175 degrees for more than 15 mins or >175 degrees
Procedure involves reducing thrust and shutting down engine if problem persists.