Perf. & Lim. Flashcards

1
Q

Can a refuelling be performed on battery power?

A

YES

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2
Q

MRW?

A

70,307 kg

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3
Q

MLW?

A

57,833 kg

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4
Q

MTOW?

A

69,853 kg

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5
Q

Max. Tailwind Tkof & Lndg?

A

15 kt
Above 10 kt refer Special Procedure

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6
Q

Max. pressure diff. ?

A

-0.5 / +8.8
+1 max. at landing

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7
Q

Can you use PACKS when ext. air cart is connected?

A

NO

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8
Q

Min AP engagement height?

A

400 ft

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9
Q

Lowest AP use height?

A

80 ft

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10
Q

During APP & LDG with A/T, approach speed must be?

A

Increased by 5 kt

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11
Q

Max. AC Load?

A

75 kVA

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12
Q

Max. DC Load TRU 1 & 2?

A

350 amp

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13
Q

Max. DC Load TRU 3?

A

225 amp

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14
Q

Max. altitude with flaps?

A

FL200

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15
Q

Lowest height with spoilers manually extended?

A

500 ft AGL

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16
Q

Min. speed with spoilers manually extended?

A

Vref + 10 kt

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17
Q

When can MAX spoilers be used?

A

Emergency ONLY

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18
Q

Max. fuel imbalance?

A

454 kg

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19
Q

Max. fuel quantity L & R tanks?

A

3050 kg

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20
Q

Max. fuel quantity Center tank?

A

11,300 kg

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21
Q

Max. TOTAL FUEL quantity?

A

17,400 kg

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22
Q

Max. FL in icing conditions?

A

FL350

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23
Q

Max. APP path angle?

A

3.8
>3.5 refer to Performance section

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24
Q

MZFW?

A

55,111 kg

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25
Minimum Flight Weight?
36,287 kg
26
VMO > 8,000 ft?
330 kt
27
MMO?
M 0.82
28
VMO < 8,000 ft?
300 kt
29
VFE FLAP 1?
230 kt
30
VFE FLAP 2?
210 kt
31
VFE FLAP 3?
210 kt
32
VFE FLAP 4?
190 kt
33
VFE FLAP 5?
170 kt
34
VLO EXTENSION?
250 kt
35
VLO RETRACTION?
220 kt
36
VLE?
250 kt
37
TURBULENCE SPEED < 10,000 ft?
265 kt
38
TURBULENCE SPEED >10,000 ft?
280 kt
39
WINDSHIELD WIPER SPEED?
250 kt
40
TIRE LIMIT SPEED?
195 kt
41
Max. AIRPORT ALTITUDE?
10,000 ft
42
Max. FL?
410
43
Max. TKOF TEMP?
52.5 c
44
Min. TKOF TEMP?
-54 c
45
Load Factor FLAPS UP?
-1.0 to +2.5 g
46
Load Factor FLAPS DOWN?
0.0 to +2.0 g
47
Min. Engine operation temp. in ground fog?
-18 c
48
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
49
Cowl anti ice must be on in flight when?
In icing conditions When ICE is annunciated
50
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
51
Wing anti-ice must be ON in flight when?
In icing conditions When ICE is annunciated
52
Wing anti-ice should be OFF above what level?
FL350
53
Wing anti-ice is prohibited above what temp?
TAT > 15 c
54
Ice shedding procedure on ground?
OAT 3 c or below and visible moisture Min. 60% N1 every 30 minutes
55
During an APP in icing conditions, Vref Vac and Vga must be increased by?
+ 5 kt
56
Min. fuel tank temp. for Tkof?
-37 c
57
Max. fuel tank temp. for start?
+ 52.5 c
58
Unattended APU use, fuel quantity limitations?
Max. 2830 kg in either wing tank Transfer to center tank if necessary
59
Max. brake temp. (BTMS) for tkof?
6 units
60
Max. brake temp. (BTMS) for gear retract?
13 units
61
Min. oil temp. for APU start?
- 40 c
62
APU start limitations?
Max. 3 per hour 2 minute delay between starts
63
Max. altitude APU use?
FL230
64
ENG. warm-up with oil below -40 c?
Engine start prohibited.
65
ENG. warm-up with oil below -6 c?
Idle only
66
ENG. warm-up with oil between - 6 c and +21 c?
30% N1
67
ENG. warm-up with oil between 21 c and 49 c?
50% N1
68
ENG. warm-up with oil above 49 c?
No limit
69
Max. EGT Tkof?
1054 c
70
Max. EGT Continuous?
1016 c
71
Above 290, max. N1 is?
95.2%
72
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%
73
Max. X-wind for start and ice shedding?
43 kt
74
Max. tail-wind for start and ice shedding?
18 kt
75
Can an defuel be performed on battery power?
NO. AC power is needed.
76
Hydraulic system nominal pressure?
3,000 psi
77
What is the backup to Hyd. Engine Driven Pump 1A?
PTU
78
What is the backup to Hyd. Engine Driven Pump 2A?
AC Motor Pump ACMP 2B
79
What is the backup to Hyd. AC Motor Pump 3A?
AC Motor Pump ACMP 3B
80
The RAT hydraulic pump provides press. to what system?
System #3
81
What happens in case of a Hyd. overheat in a system?
Fluid is drained overboard
82
PTU pump is driven by fluid from which system?
By #2 system's fluid
83
Hyd. ACMP 2B is driven by what type of current?
AC current 115 VAC from AC BUS 1
84
When does the backup ASMP 3B runs?
When ACMP 3A fails For TKF & LDG
85
Hyd. ACMP 3A and 3B are driven by what type of current?
AC current 115 VAC from AC BUS 2
86
What systems are not powered by the RAT?
Nose Steering Reverses PTU GND Spoilers Gear
87
RAT operates at what nominal pressure?
2,850 psi
88
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
89
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
90
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
91
What are the two modes of the FlyByWire system?
NORMAL and DIRECT
92
Nose up pitch compensation is active until what bank angle?
33 deg. Beyond that aft sidestick must be applied
93
At what speed does the YD activates?
70 kt
94
What is the 1/2 bank mode max. bank angle?
15 degrees
95
At what altitude is 1/2 bank mode auto activated?
31,500 ft
96
What cabin altitude triggers the Emerg. Desc. Mode?
14,500 ft
97
OEI cruise speed?
310 KIAS
98
Max. diversion time and distance?
60 min / 390 nm
99
Max. cabin pressure differential?
8.8 psi / -0.5 psi