Perf. & Lim. Flashcards
Can a refuelling be performed on battery power?
YES
MRW?
70,307 kg
MLW?
57,833 kg
MTOW?
69,853 kg
Max. Tailwind Tkof & Lndg?
15 kt
Above 10 kt refer Special Procedure
Max. pressure diff. ?
-0.5 / +8.8
+1 max. at landing
Can you use PACKS when ext. air cart is connected?
NO
Min AP engagement height?
400 ft
Lowest AP use height?
80 ft
During APP & LDG with A/T, approach speed must be?
Increased by 5 kt
Max. AC Load?
75 kVA
Max. DC Load TRU 1 & 2?
350 amp
Max. DC Load TRU 3?
225 amp
Max. altitude with flaps?
FL200
Lowest height with spoilers manually extended?
500 ft AGL
Min. speed with spoilers manually extended?
Vref + 10 kt
When can MAX spoilers be used?
Emergency ONLY
Max. fuel imbalance?
454 kg
Max. fuel quantity L & R tanks?
3050 kg
Max. fuel quantity Center tank?
11,300 kg
Max. TOTAL FUEL quantity?
17,400 kg
Max. FL in icing conditions?
FL350
Max. APP path angle?
3.8
>3.5 refer to Performance section
MZFW?
55,111 kg
Minimum Flight Weight?
36,287 kg
VMO > 8,000 ft?
330 kt
MMO?
M 0.82
VMO < 8,000 ft?
300 kt
VFE FLAP 1?
230 kt
VFE FLAP 2?
210 kt
VFE FLAP 3?
210 kt
VFE FLAP 4?
190 kt
VFE FLAP 5?
170 kt
VLO EXTENSION?
250 kt
VLO RETRACTION?
220 kt
VLE?
250 kt
TURBULENCE SPEED < 10,000 ft?
265 kt
TURBULENCE SPEED >10,000 ft?
280 kt
WINDSHIELD WIPER SPEED?
250 kt
TIRE LIMIT SPEED?
195 kt
Max. AIRPORT ALTITUDE?
10,000 ft
Max. FL?
410
Max. TKOF TEMP?
52.5 c
Min. TKOF TEMP?
-54 c
Load Factor FLAPS UP?
-1.0 to +2.5 g
Load Factor FLAPS DOWN?
0.0 to +2.0 g
Min. Engine operation temp. in ground fog?
-18 c
Cowl anti-ice must be ON on the ground when?
+10 c or below with any visible moisture
+10 c or below if contam. on ground
Cowl anti ice must be on in flight when?
In icing conditions
When ICE is annunciated
Wing anti-ice must be ON on the ground when?
+5 c or below with any visible moisture
+5 c or below if contam. on ground
Wing anti-ice must be ON in flight when?
In icing conditions
When ICE is annunciated
Wing anti-ice should be OFF above what level?
FL350
Wing anti-ice is prohibited above what temp?
TAT > 15 c
Ice shedding procedure on ground?
OAT 3 c or below and visible moisture
Min. 60% N1 every 30 minutes
During an APP in icing conditions, Vref Vac and Vga must be increased by?
+ 5 kt
Min. fuel tank temp. for Tkof?
-37 c
Max. fuel tank temp. for start?
+ 52.5 c
Unattended APU use, fuel quantity limitations?
Max. 2830 kg in either wing tank
Transfer to center tank if necessary
Max. brake temp. (BTMS) for tkof?
6 units
Max. brake temp. (BTMS) for gear retract?
13 units
Min. oil temp. for APU start?
- 40 c
APU start limitations?
Max. 3 per hour
2 minute delay between starts
Max. altitude APU use?
FL230
ENG. warm-up with oil below -40 c?
Engine start prohibited.
ENG. warm-up with oil below -6 c?
Idle only
ENG. warm-up with oil between - 6 c and +21 c?
30% N1
ENG. warm-up with oil between 21 c and 49 c?
50% N1
ENG. warm-up with oil above 49 c?
No limit
Max. EGT Tkof?
1054 c
Max. EGT Continuous?
1016 c
Above 290, max. N1 is?
95.2%
ENG start limitations?
After 3 attempts or 4 min cranking, a 30 minute cooling period is required. Do not engage starter if N2 on ground > 20%
Max. X-wind for start and ice shedding?
43 kt
Max. tail-wind for start and ice shedding?
18 kt
Can an defuel be performed on battery power?
NO. AC power is needed.
Hydraulic system nominal pressure?
3,000 psi
What is the backup to Hyd. Engine Driven Pump 1A?
PTU
What is the backup to Hyd. Engine Driven Pump 2A?
AC Motor Pump ACMP 2B
What is the backup to Hyd. AC Motor Pump 3A?
AC Motor Pump ACMP 3B
The RAT hydraulic pump provides press. to what system?
System #3
What happens in case of a Hyd. overheat in a system?
Fluid is drained overboard
PTU pump is driven by fluid from which system?
By #2 system’s fluid
Hyd. ACMP 2B is driven by what type of current?
AC current 115 VAC from AC BUS 1
When does the backup ASMP 3B runs?
When ACMP 3A fails
For TKF & LDG
Hyd. ACMP 3A and 3B are driven by what type of current?
AC current 115 VAC from AC BUS 2
What systems are not powered by the RAT?
Nose Steering
Reverses
PTU
GND Spoilers
Gear
RAT operates at what nominal pressure?
2,850 psi
When would the PTU operate on AUTO?
QTY in system 1 is 5% & system 2 is running and when either:
TKF thrust is applied
SLAT/FLAP is in position 4 or 5
ALT FLAP is selected
EDP 1A fails or left engine inoperative
Parking brake is OFF during right single engine taxi
When would ACMP 2B operate on AUTO?
QTY in system 2 is 5% & AC power available and when either:
TKF thrust is applied
SLAT/FLAP is in position 4 or 5
ALT FLAP is selected
EDP 2A fails or right engine inoperative
Parking brake is OFF during left single engine taxi
EDP 1A fails or left engine inoperative
When would ACMP 3B operate on AUTO?
QTY in system 3 is 5% & AC power available and when either:
TKF thrust is applied
In flight SLAT/FLAP is out of zero
On ground during SLAT/FLAP deployment
One second after ACMP 3A fails
What are the two modes of the FlyByWire system?
NORMAL and DIRECT
Nose up pitch compensation is active until what bank angle?
33 deg. Beyond that aft sidestick must be applied
At what speed does the YD activates?
70 kt
What is the 1/2 bank mode max. bank angle?
15 degrees
At what altitude is 1/2 bank mode auto activated?
31,500 ft
What cabin altitude triggers the Emerg. Desc. Mode?
14,500 ft
OEI cruise speed?
310 KIAS
Max. diversion time and distance?
60 min / 390 nm
Max. cabin pressure differential?
8.8 psi / -0.5 psi
