A330 Freighter Limitations Summary (Bold Qs should be memorized) Flashcards

1
Q

Length

A

208’ 11”

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2
Q

Wingspan

A

197’ 10”

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3
Q

Tail Height

A

55’ 3”

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4
Q

Minimum Turning width for 180-degree turn

A

157’

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5
Q

Max Taxi Weight (MTW)

A

515.6 Klbs

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6
Q

Max Takeoff Weight (MTOW)

A

513.6 Klbs

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7
Q

Max Landing Weight (MLW)

A

412.2 Klbs

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8
Q

Max Zero Fuel Weight (MZFW)

A

385.8 Klbs

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9
Q

Minimum Weight

A

266.7 Klbs

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10
Q

Flight Maneuvering Load Acceleration Limit: Clean configuration

A

-1.0g to +2.5g

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11
Q

Flight Maneuvering Load Acceleration Limit: Other than clean configuration

A

0g to +2.0g

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12
Q

Max. Altitude

A

41,450’

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13
Q

Max. Runway Altitude

A

12,500

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14
Q

Max. Runway Slope

A

±2%

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15
Q

Max. Takeoff Crosswind

A

32 kts (gusts included)

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16
Q

Max. Takeoff Tailwind

A

15 kts

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17
Q

Max. Landing Crosswind

A

40 kts (gusts included)

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18
Q

Max. Landing Tailwind

A

10 kts

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19
Q

Max wind to operate passenger/cargo doors

A

40 kts (50 nose into wind)

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20
Q

Max wind for passenger/cargo doors open

A

60 kts

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21
Q

Max wind for Main Deck Cargo Door operation

A

40 kts
*Main Deck Cargo Door must be closed before wind speed exceeds 60 kts

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22
Q

VMO/MMO

A

330 kts / M.86

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23
Q

VFE Flap 1 (1+F)

A

240 kts (215 kts)

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24
Q

VFE Flap 2 (1*)

A

196 kts (205 kts)

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25
VFE Flap 3
186 kts
26
VFE Flap FULL
180 kts
27
Min. Control Speed for Landing (VMCL)
126 kts
28
**Max. Altitude with flaps/slats extended**
**FL200**
29
VLE/VLO
250 kts / M.55
30
Max. Tire Speed
204 GS
31
**VLE for gravity gear extension**
**200 kts**
32
**Max. Windshield wiper speed**
**230 kts**
33
Max Cockpit window open speed
230 kts
34
Speedbrakes
No Limitation
35
Max. Positive Differential
9.25 psi
36
Max. Negative Differential
-0.73 psi
37
Safety Relief Valve Setting
8.85 psi to -0.26 psi
38
**Air Conditioning with LP Ground Unit**
**Do not use packs**
39
**Air Conditioning with HP Ground Unit**
**Do not use APU bleed**
40
**Autopilot minimum height for use: Takeoff**
**100’ AGL**
41
**Autopilot minimum height for use: Non ILS approach**
**250’ AGL (MDA OpSpec C071)**
42
**Autopilot minimum height for use: ILS when CAT 2 or CAT 3 not displayed**
**160’ AGL (DA-40 OpSpec C071)**
43
**Autopilot minimum height for use: Go-around**
**100’ AGL**
44
**Autopilot minimum height for use: All other phases**
**500’ AGL**
45
**Max. Autoland Wind Limits: Headwind**
**25 kts (20 kts in OEI)**
46
**Max. Autoland Wind Limits: Tailwind**
**10 kts**
47
**Max. Autoland Wind Limits: Crosswind**
**15 kts (10 kts in OEI)**
48
**Autoland Configuration Allowed**
**CONF 3 or CONF FULL**
49
**HAL A330 Aircraft Approach Category [FOM 4.3]**
**Category “C”**
50
Smallest Outer Tank fuel imbalance limit
3260 lbs
51
Max. fuel imbalance limits may be exceeded when
in “exceptional conditions”
52
Max. fuel temperature for JET A/A1
+55°C
53
Min. fuel temperature (inner tank)
-44°C ~ -54°C
54
Min. fuel quantity for takeoff
11,461 lbs
55
**Hydraulics normal operating pressure**
**3000 psi +/- 200 psi**
56
**Max. brakes temperature for takeoff**
**300°C**
57
Nosewheel steering angle limit
72°
58
Rudder steering angle limit
59
Braked pivot turns (one main gear fully stopped)
Not Allowed
60
Max. taxi speed with one/two tires deflated per gear
7 kts / 3 kts
61
Max. NWS angle if two tires deflated on the same main gear
30°
62
**IRS Nav max. RNP-10 triple-IRS time without GPS update**
**6.2 hours from alignment**
63
**Min. Courier Oxygen pressure (2 bottles)**
**1500 psi or higher for each bottle *Refer to table 1 in FCOM-LIM-OXY**
64
LOW OIL LEVEL ECAM advisory
May start/operate for 15 hrs
65
**APU Starter Limits**
**After 3 starts need 60 minutes to cool**
66
**APU Max. altitude for start and operation**
**41,450’ (aircraft ceiling)**
67
**APU Max. altitude for battery-only start**
**25,000’**
68
APU Max. altitude for one pack bleed and electrics
22,500’
69
APU Max. altitude for bleed engine start
20,000’
70
APU Max. altitude for two pack bleed and electrics
17,500’
71
APU Bleed for wing anti-ice
Not Permitted
72
ENG EGT limits: Takeoff and Go-around
20s at 920°C 5m or (10m with engine failure) at 900°C
73
ENG EGT limits: MCT
850°C
74
ENG EGT limits: Starting Normal / In Flight
700°C / 850°C
74
ENG Min. oil quantity (highest of)
15qts (6qts + est. consumption) *Average estimated consumption = 0.7qt/hr
75
ENG Starter Max. continuous operation
5m
76
ENG Cooling period after 5m continuous operation or 3 cycles
30m
77
ENG Starter Max starter engagement on Ground and In Flight
10% and 30% N3
78
Reverse Thrust Selection in flight
Prohibited
79
Backing aircraft using reverse thrust
Prohibited
80
Max. reverse should not be used below
70 kts
81
Max. temp. FLEX
ISA +60°C
82
Min. temp. FLEX
Flat rating temp or OAT
83
Reduced Thrust Takeoff use on contaminated runways
Not Permitted