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330 Flashcards

1
Q

Flight maneuvering load acceleration limit - clean configuration.

A

-1g to +2.5g

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2
Q

Flight maneuvering load acceleration limit - other configurations

A

0g to +2g

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3
Q

Environmental Envelope - Maximum Pressure Altitude

A

41,450 ft

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4
Q

Environmental Envelope - Maximum Elevation for takeoff and Landing

A

12,500 ft

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5
Q

Environmental Envelope - Minimum elevation for TO and LDG

A

-2,000 ft

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6
Q

Runway slope

A

-+2%

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7
Q

Nominal runway width

A

45m

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8
Q

Maximum certified Cross wind for
TO

A

32 kts gust included. An engine limitation

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9
Q

Max demonstrated crosswind for landing

A

40 kts gust included

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10
Q

Max tailwind TO

A

15 kts

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11
Q

Max tailwind LDG

A

15 kts at or Below 11,000 ft
10 kts above 11,000ft

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12
Q

Max wind conditions for ILS CAT II and CAT III

A

Headwind 35 kts
Tailwind 10 kts
Crosswind 20 kts

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13
Q

Cockpit window open Max speed

A

230 kts

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14
Q

Max Flaps/Slats Speed Config 1

A

240 kts

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15
Q

Max Flaps/Slats Speed Config 1+F

A

215 kts

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16
Q

Max Flaps/Slats Speed Config 2 (CONF 1*)

A

205 kts

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17
Q

Max Flaps/Slats Speed Config 2

A

196 kts

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18
Q

Max Flaps/Slats Speed Config 3

A

186 kts

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19
Q

Max Flaps/Slats Speed Config FULL

A

180 kts

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20
Q

Max operating speed VMO/MMO

A

330 kts/Mach 0.86

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21
Q

Max speed with landing gear extended VLE

A

250 kts/0.55 mach

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22
Q

Max speed with landing gear operating - extending

A

250 kts/0.55 mach

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23
Q

Max speed with landing gear gravity extension

A

200 kts

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24
Q

Max tire speed

A

204 kts

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25
Min control speed for LDG (VMCL)
126 kts
26
Wipers Max operating speed
230 kts
27
With pax on board, it is not recommended to exceed this time without air conditioning supply.
20 minutes
28
Cabin pressure - Max positive differential pressure
9.25 psi
29
Cabin pressure - Max negative differential pressure
-0.73 psi
30
Auto pilot can be used with the following minimum values:
At takeoff 100 ft AGL and at least 5s after lift off In approach with FINAL APP, V/S or FPA mode 250 ft AGL In circling approach 500 ft AGL ILS approach when CAT I on FMA 160 ft AGL ILS approach when CAT 2 or CAT 3 (single or dual) on FMA 0 ft AGL if autoland
31
Autoland landing glideslope limitation
-2.5 deg to -3.25 deg Airfied below 9.5
32
Minimum weight for autoland
116,000 kgs
33
APU start: after 3 consecutive start attempts, flight crew must wait for how many minutes before a new start attempt.
60 minutes
34
Max EGT for APU start
1250 deg C
35
Max EGT for APU running
650 deg C
36
APU Max N speed
107 %
37
APU Operation and Normal Start Envelope - maximum Pressure Altitude
41,450 ft
38
APU Operation - electrical power only
22,500 ft and above
39
APU Operation - bleed air and electrical power only
22,500 ft and below
40
APU Battery restart limit
25,000 ft
41
APU ground operation max and min altitude
14,600 ft and -1,000 ft
42
Engine Max EGT for TO and GA - all engines operative
900 deg C for 5 min includes TOGA, FLEX, DERATE thrust modes
43
Engine Max EGT for TO and GA - one engine inoperative
900 deg C for 10 min includes TOGA, FLEX, DERATE thrust modes
44
Engine Max EGT for TO and GA max MCT
850 deg C no time limit
45
Engine Max EGT for starting on ground
700 deg C
46
Engine Max EGT for starting in flight
850 deg C
47
Shaft Speed Max N1 Low Pressure Rotor Speed (in %)
99% depends on ambient conditions and on the configuration of the engine air bleed.
48
Shaft Speed Max N2
103.3%
49
Engine Shaft Speed Max N3
100%
50
Max Oil Temperature continuous
190 deg C
51
Min Oil Temperature before TO
20 deg C
52
Min Oil quantity
Above 6 qt + estimated consumption average 0.7 qt/hr but no lower than 15 qt
53
Min Oil pressure
25 psi
54
Eng Starter MAX continuous operation
5 min
55
Max engine starter operation
Two 3 min duty cycles and a consecutive 1 min cycle is permitted with run down to Zero N3 between each cycle. No running engagement of the starter when N3 is above 10% on ground or 30% in flight.
56
After one continuous operation, or the three cycles, how long to wait to allow the starter to cool.
30 minutes
57
Limitation of Reverse Thrust
Selection of Reverse Thrust is prohibited in flight. Backing the aircraft with Reverse Thrust is not permitted. Max reverse should not be used below 70 kts. Idle reverse is permitted down to aircraft stop.
58
FLEX TO limitations
not permitted in contaminated runway TFLEX cannot be: - higher than TMAXFLEX, equal to ISA+60 deg C - lower than the flat rating temp (TREF) - lower than the actual OAT
59
Max operating Altitude with Flaps/Slats extended
20,000 ft
60
Max fuel temp
Jet A1 +49 deg C
61
Min fuel temperature
Jet A1 -47 deg C
62
Max allowed Fuel Imbalance
Inner Tanks (Outer Balanced) Heavier Tk. Max Asymmetry Full. 2,900 kg 17,000. 4,800 kg 7,500 kg. 7,500 kg
63
Min fuel quantity for TO
5,200 kg ECAM alerts related to fuel low in the wing tanks must not appear for TO
64
Severe Ice accretion
Ice accumulation on the airframe reaches 5mm or 0.2in thick or more
65
Rain repellent
Use in case of heavy and moderate rain
66
Wipers Max operating speed
230 knots
67
Max break temp for TO
300 deg C
68
Nosewheel Syeering angle limit
72%
69
Taxi speed during a turn with deflated or damaged tire, maximum one tire per gear
7 kts
70
Taxi speed during turn with two deflated or damaged tire on the same gear.
3 kts
71
Max NWS angle with deflated or damaged tire
30 deg
72
APU Max Alt for aircon and pressurization - dual pack operation.
17,500 ft
73
APU Max Alt for aircon and pressurization - single pack operation.
22,500 ft
74
Use of APU bleed for wing anti-ice.
Not permitted

Limits (1 decks)

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