Limitaciones Flashcards
Practice and Learn Avianca A330-200 limitations.
Maximum Altitude
41.450 Ft.
Flight Maneuvering Load Acceleration
Clean: -1 to + 2,5 g
Other: 0 to 2 g
Maximum Taxi Weight A330-200
233.900 Kg.
Maximum Takeoff Weight A330-200
233.000 Kg.
Maximum Landing Weight A330-200
182.000 Kg.
Maximum Zero Fuel Weight A330-200
170.000 Kg.
Minimum Weight A330-200
116.000 Kg.
Runway Slope (Mean)
+/- 2 %
Maximum Depth for Contaminated Runway (AV POLICY)
1/4 Inch
6,3 mm
Maximum Runway Altitude
12.500 Ft.
Winds (XW & TW) for Takeoff And Landing A330-200
XW T/O: 32 Kt.
XW Landing: 45 Kt.
TW T/O & Landing: 15 Kt.
TW Landing Above 11.000 Ft: 10 Kt.
Maximum Wind for Pax and Cargo door Operations
40 Kt.
50 Kt. If aircraft nose is oriented into the wind.
Cargo door must be closed before _______ Kt.
+ 60 Kt.
Maximum Wind Conditions For Autoland.
HW: 35 Kt.
XW: 20 Kt.
TW: 10 Kt.
Maximum Wind Consitions For CAT 2/3 Operations (AV POLICY)
HW: 35 Kt.
XW: 15 Kt.
TW: 10 Kt.
Autoland Altitude Limitation
9.200 Ft.
Glideslope Range
-2,5°/ -3,25°
VMO (Up to 30.000 Ft.)
330 Kt.
MMO (Over 30.000 Ft.)
M 0,86
Green Dot Formula
0,6 X Weight + 107*
*Over FL200 +1 Kt/1.000 Ft
Maximum Flaps Speed
1: 240 Kt. 1+F: 215 Kt. 2*: 205 Kt. 2: 196 Kt. 3: 186 Kt. FULL: 180 Kt.
This Slats/flaps position corresponds to CONF 1
VLE & VLO
250 Kt./M 0,55
VLE/VLO by gravity
200 Kt.
The gear extension is inhibited at ______ Kt.
280 Kt.
Anti Skid is operative at ______ Kt.
10 Kt.
Autobrake is operative at _______ Kt.
72 Kt.
Maximum Tire Ground Speed
204 Kt.
Max Speed for Windshield Wipers
Also for Cockpit Window Opening
230 Kt.
Maximum Taxi Speed
30 Kt.
Max Taxi Speed for turns 90 or more
Less than 10 Kt.
Taxi Speed for a 180 Turn
5-10 Kt.
Max Taxi Speed with one deflated tire
7 Kt.
Max Taxi Speed with two deflated tires (Same Gear)
3 Kt. also NWS Limited to 30°
Maximum positive differential pressure
9,25 PSI
Max. Negative differential pressure
-0,73 PSI
Safety Relief Valve Opening
8,85 PSI
RAM Air Open
Less than + 1,0 PSI
Minimum Battery Voltage
25,5 V
Minimum Autopilot Height for Use
100 Ft. AGL
Minimum Autopilot Height Disconnection when using FINAL APP, v/s or FPA
250 Ft. AGL
Minimum Autopilot Height Disconnection when Circling or other Phases
500 Ft. AGL
Minimum Autopilot Height Disconnection when CAT 1 displayed on FMA
160 Ft. AGL
Engine out autoland only allowed with Flaps _____.
FLAPS 3
Maximum Altitude for Flaps Extension
20.000 Ft.
Maximum Allowable Fuel Inbalance (Inner Tanks)
If:
FULL: 2.900 Kg.
- 000 Kg: 4.800 Kg.
- 500 Kg: 7.500 Kg.
Maximum Allowable Fuel Inbalance (Outer Tanks)
If:
FULL: 1.480 Kg.
- 400 Kg: 1.580 Kg.
- 730 Kg: 1.730 Kg.
Minimum Fuel For Takeoff
5.200 Kg.
WING TK LO LVL must not be displayed on ECAM
Hydraulic Normal Operating Pressure
3.000 PSI +/- 200
Max brake temperature for Takeoff
300° C
Avoid Using Parking Brake If Temperature is Mora than
500° C
Maximum Nosewheel Steering Deflection
72° (65° During Towing)
Maximum APU time usage if ECAM advisory LO LVL Is show
15 h
APU start cycles
3 cycles then 60 min wait.
APU max N speed
107 %
APU Battery Start Altitude Limit
25.000 Ft.
APU Electrical limit operation altitude
41.450 Ft.
APU Max Altitude for Assist Engine Start
20.000 Ft.
APU bleed limit operation altitude (Single Pack)
22.500 Ft.
APU Bleed limit Operarion Altitude (Dual Pack)
17.500 Ft.
APU Max EGT for Starting
1250° C
APU Max EGT for Running
650° C
Engine TOGA Time and EGT Limits
Time: 5 min (10 min engine out)
EGT: 900° C
Note: TOGA EGT limit 920° C limited to 20 s
Engine MCT EGT Limit
850° C
Engine Starting on Ground EGT Limit
700° C
Engine Starting on Air EGT Limit
850° C
Max N1 %
99 %
Max N2 %
103,3 %
Max N3 %
100 %
Maximum and Minimum Oil Temperatures
190° C/20° C
Minimum Oil Pressure
25 PSI
Takeoff is prohibited when _______ of slush and XW of ________
(AV POLICY)
1/4 inch or 6,3 mm
15 XW
Landing prohibited when RCAM codes ________ and XW ________
AV POLICY
0 or 1
15 XW
ADVERTENCIA: La información contenida en la siguientes flashcards esta basada en los manuales FCOM, FCTM y AFM.
El propósito de estas cartas es proporcionar una forma amigable y didactica de aprender y estudiar las limitaciones del Airbus A330.
Al no ser un documento oficial, siempre verifique los manuales vigentes.
Cualquier error encontrado informarlo a senick91@outlook.com