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A330 > LIM > Flashcards

LIM Flashcards

1
Q

Load limit

Clean config
Other config

A

-1 to +2.5g

0g to +2g

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2
Q

Max landing weight

A

177-187

  1. 9
  2. 5
  3. 2
  4. 7
  5. 7
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3
Q

Airport operational limit

Slope

Altitude and temp

A

2%

12500ft

-53*C

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4
Q

Max TAKE OFF X wind

Max landing x wind

Max tail wind

Max cargo door

A

32kts

40kts

15kts below 11000ft

10kts above 11000ft

40kts for cargo and passenger door

Or 50 if into wind.

Cargo door muSt close before 60

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5
Q

Run way condition prohibit take off

A

Wet ice

Water on to of compacted snow
Any snow over ice

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6
Q

VMO/MMO

A

330

.86

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7
Q

VA

A

.78

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8
Q

VMCL

A

126kts

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9
Q 
Flap 
1
1+F
2
3
Full
A 
240
215
196
186
180
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10
Q

Landing gear extended

Extend/retract

GRAVITY extend

A

250

250

200

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11
Q

Tire speed

A

204

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12
Q

Wipers

A

230

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13
Q

Window

A

230

Packs must be off

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14
Q

RAM air

A

1PSI

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15
Q

Ground air and APU

A

only one can be used at a time

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16
Q

Max and Min differential pressure

safety valve pressure

A

+9.25 -1

+8.85 -0.26

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17
Q

Max normal cabin altitude

max selectable cabin altitude

A

8000ft

14000ft

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18
Q

Auto land minimum weight

A

123000kg

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19
Q

Without GPS Primary what happens

A

FM updates via NAV aids or simply uses the NAV aid to determine position

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20
Q

Time limitation for RNP 10nm without GPS primary

A

No time limitation if NAV aids are around(auto update position)

5.7 hours after the last update position

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21
Q

CAT 2 minimum DH

Required automatics

height to disconnect AP if manual landing

A

100ft and 80ft

1 AP

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22
Q

CAT3A DH and required automatics

A

50ft

1AP and ATHR

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23
Q

CAT3B

A

2AP and ATHR

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24
Q

EO autoland requirement

A

CONFIG 3 and ECAM done by 1000ft

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25
Q

Auto land max wind

A

35,20,10

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26
Q 
Auto land
Slope
Elevation
Weight
VApp max wind correction
Runway condition
A

-2.5 to -3.25

9200ft

Max landing weight

VLS+5-15kts

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27
Q

Depending situation, max auto land weight

A

229tones

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28
Q

Altitude phones prohibited

ON BOARD MOBILE TELEPHONY SYSTEM

A

Below FL100 AGL

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29
Q

When does IN SEAT POWER SUPPLY SYSTEM must be switched off

A

Take off and landing

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30
Q

Max flap slats operation altitude

A

20 000ft

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31
Q

Fuel JET B AND JP4 limitation

A

Trim tank empty and isolated during entire flight

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32
Q

Inner tank max fuel imbalance

Outer tank max fuel imbalance

A

2900kg

1480 kg

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33
Q

No limitation for fuel imbalance what weight

A

7500kg

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34
Q

Max fuel tempJET A and so on

JET B AND JET4

Min temperature

A

+55

+49

Freezing point or -44, below FL 300

-54 above FL300

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35
Q

Trim tank forward transfer pump failure

A

Do not transfer fuel unless less than 3* pitch, to avoid fuel flowing back.

Transfer in descent

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36
Q

Wing Tk LO LVL

A

No take off

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37
Q

Mixed fuel

A

Okay as long as known freezing point

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38
Q

Normal hydraulic pressure

A

3000+_200PSI

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39
Q

Max brake temperature for take off without brake fan

A

300

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40
Q

PFD BOTH LOST watch out of ISIS

A

Do not use the big

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41
Q

Oxygen time
Emergency decent
FL 100

SMOKE 100%

A

15min
105min

8000ft 15min

22min
98min

8000ft 15min

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42
Q

LOW OIL LEVEL ECAM

A

Max 15 hours APU operator

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43
Q

APU start limit

ALT with ELEC

ALT with batteries only (EMER ELECTRIC CONFIG)

ALT with power and bleed

ALT with JETB OR JP4

if first start fail how attempt second

ELEC only power output

A

3 times

Max alt FL415

Battery start FL250

Bleed+power FL225

FL250

APU MASTER 3 min then start

115kVA

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44
Q

Takeoff EGT and time limit

A

920 20s
900 5minutes
900 10minutes EO

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45
Q

MCT EGT and time

A

850 unlimited

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46
Q

Starting EGT

GROUND

AIR START

A

700*C

850*C

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47
Q

Engine OIL temp

MAX

MIN for take off

A

190*C

20*C

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48
Q

Oil pressure MIN

Oil quantity MIN

A

25PSI

Min 15qt or 6qt + 0.7qt/hr

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49
Q

N1
N2
N3

A

99

103.3

100

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50
Q

Starter limit
Max continuous
Cycles
Max N1 for start

A

5minutes

3minutes x 2, 1minute. N3 0 in between

After 3 cycle or 5minutes continuous 30min cooldown

No start when N1 10% on ground or 30% in air

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51
Q

Max fuel in tanks

A
  1. 2
  2. 3
  3. 5
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52
Q

Fuel burn per hour

A

2600kg for 30minutes

5.2 for one hour

700 per hold

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53
Q

Stabilization criteria

A

1000 or 500ft

Lateral/vertical correct flight path

Landing config

Stabilized speed and thrust(if due restriction by 500ft)

No excess parameters

Unless only require small adjustment, then must go around

Prevailing condition okay

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54
Q

Reset time
CB
COMPUTER

A

5s

3s

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55
Q

Landing distance on

MP, flap 3, 10T over weight, ISA+20, 1000ft

A

3360 without 15%

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56
Q

FM reset period

A

ND map not available

MCDU please wait

2-3minutes

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57
Q

When will all data be lost in FM

Caution during reset

A

3 Dual FM reset within 2minutes

Don’t do anything with MCDU for atleast 1 minute in case of causing another reset

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58
Q

Max temp for one brake to avoid park brake

A

500 or 350 with brake fans

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59
Q

Brake pressure check PSI

A

2200-2700

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60
Q

Rain repellent restriction

A

Don’t use when dry

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61
Q

When complete IRS alignment

A

First flight of day

Crew change

GPS not avail + poor NAV aid coverage

GPS not avail with flight time more than 3 hours

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62
Q

Fast alignment

A

Less than 5 seconds

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63
Q

Pack flow low when

A

200 passengers or below 60% ECON px

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64
Q

180 degree turn minimum distance

A

42m for 200

46m for 300

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65
Q

When does trim tank transfer start and end

A 
FL255 climb
6250kg inner tank
CG not on target
Trim tank not full
Slats and gear retracted

FL245 descent or 35 min to destination or 75 if trim tank forward pump failure

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66
Q

When are trim tank isolation valves closed

A

Take off and landing

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67
Q

Too far aft CG

A

FMGEC set 3% forward

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68
Q

FQI degradation or ZFW/ZFWCG not entered

A

Forward 1.5%

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69
Q

Amber box OXY

A

Below 1000PSI

Check LIM (640 at 50*C)

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70
Q

APU behavior below 10*C

A

12PSI with bleed fluctuation

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71
Q

Instrument tolerance

A

PFD ground check 25ft/300 STBY/

On ground cross check/20ft/none STBY/60isis

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72
Q

ECAM CG VS LOADSHEEY

A

2%

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73
Q

Change on INIT B comparing loadsheet final and prelim

A

300kg 0.5%

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74
Q

Ground crew aware push back max angle

A

65*

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75
Q

NWS memo not appear during push back

A

No engine start during push back.

Avoid damage on nose wheel during pressurization

Refer to limitation for dispatch

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76
Q

Time before take off after engine start

A

5 minutes

3 minutes less than 1.5 hour turn around

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77
Q

Ice shedding procedure

A

Below 1*C

N1 50% for 10s every hour

Every 45 if freezing fog taxi in and out

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78
Q

Rudder trim limit

A

0.6*

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79
Q

When brake fans off after engine start

A

Green arc

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80
Q

Take off thrust initially

A

1.1 EPR

HALF FORWARD

FULL FORWARD IF 20kts x wind or tail wind

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81
Q

MAX REC buffer

A
  1. 3g

0. 2g accepted if entered

82
Q

EO circle to land weight unable maintain level flap 3

A

30 degrees at 230 tones

83
Q

How is IDG cooled

A

Through engine fan air

84
Q

Reset computer time

85
Q

ENG2 fail caution of hydraulic

A

If flaps or slats out ELEC pump will keep running. Turn it off

86
Q

NPA buffer

87
Q

Engine out ceiling +20*C ISA

A

Atleast FL150

88
Q

EO timing for relight when start

A

Starter to IGN

89
Q

IOC alert phase

A

ATSU next page

90
Q

Circling approach

A

Disconnect early
AP off FD off RW TRK

30s extend if possible but within circling area

around 700ft/min

turn in final more early

atleast 1nm start final turn

91
Q

Why take FLX out if TOGA take off

A

If forgot to put TOGA plane will warn with ECAM

92
Q

Windshear flap setting

93
Q

ECAM status and down to INOP SYS last thing before REMOVE STATUS

A

GW above landing weight or not

94
Q

Altitude for APU BLEED

1 PACK

ENG START

2 PACKS

A

FL225

FL200

FL175

95
Q

item to include brief

A

PACKS for RTOW, DEPARTURE BRIEF, CTWO+

96
Q

Failure management for partner

A

MAKE SUMMARY

CRZ APPR LANDING GA

97
Q

When is predictive windshear inhibit

A

100kt to 50ft take off up to 2300

below 50ft for landing

98
Q

When is REACTIVE windshear operational

A

3s after lift off up to 1300ft RA

1300ft down to 50ft

99
Q

Why selected speed slat flap jam

A

because managed speed will lead to follow of GD S or F speed which are inacurate

100
Q

if must head somewhere else, how to find out MAX speed with slat flap jam

A

speed out until hear bing

101
Q

GA slat flap jam

A

go to max speed

102
Q

Stoping with accumulator pressure

A

Stop on runway

103
Q

When is it considered one application

A

when feet completely off

104
Q

Landing PERF failure codes

A

COMP somehwere QRH

105
Q

Hold sector entry

Max speed

A

Direct

Parallel

Offset

230kts

106
Q

NPA what kind of approach

A

stablilized approach

107
Q

Derated climb

A

Tends to burn more fuel but reduces maintenance costs

108
Q

When pack flow low

A

Below 200 PX

AND

ECON below 60% 138

109
Q

SID protection zone within 25nm MSA

A

900m left and right of track

+35ft. Clearance

50ft in turn

110
Q

Beyond 25nm MSA protection on track

A

5nm left and right of track

2000ft clearance

111
Q

EO fuel burn compared to both engine operative

112
Q

EO ceiling with full anti ice

113
Q

Minimum climb gradient

114
Q

RAT powering EMER GEN fuel pumps working

A

Left 2, or right 2 if left 2 inop

115
Q

Fuel transfer sequence

A

4000kg trim tank to inner

3500kg outer to inner

116
Q

V1

VR
V2

A

VR min 1.05 stall

V2 min 1.1 stall

117
Q

Flex max thrust reduction

A

25% reduction

118
Q

Runway line up allowance

Displac d thresh hold

A
  1. 1m 90* turn TODA
  2. 4m 180* turn TODA
  3. 5m ASDA
  4. 8m ASDA

Displaced thresh hold no allowance

119
Q

Minimum ground roll

A

Shortest distance for take off. Add MR

Limits flex +31

Shorten runway 2000ft or 1000ft

120
Q

APU fuel burn

A

130kg roughly 200kg

121
Q

Auto brake not in IFL

A

Anything with delta VREF or failure code. Manual only

122
Q

Wing span

123
Q

Contingency
Recommended extra
Mandatory fuel

A

total 1500kg

Contingency 300kg

124
Q

SPEED SPEED SPEED aural warning

A

2000ft to 100ft RA

PRIM generated

Only in normal law

None of both RA failed

Flap 2,3,full

125
Q

Pitch protection

A

30* 25* if low speed. 15* nose down

Green = sign

126
Q

High speed protection

A

Bank to 0 if stick let go.

Limit bank angle to 45*

Trim frozen

Continuous pitch up ordered

OVERSPEED ECAM +4kts or +0.006M

127
Q

When does AP and FD disappear in turn

A

Above 45* reappear after 40*

128
Q

Beta target generation

129
Q

Maneuver load alleviation

Trigger

A

8* +2g

Aileron and spoilers deflected to reduce load

Elevator compensates pitch moment

Trigger above 250kt
Clean
Normal or alternate law

130
Q

Runway lighting

A

300m before threshold (red)and 900m into runway(red and white)

131
Q

Taxi way lights on runway and when clear of ILS sensitive areas

A

Yellow green then full green

132
Q

Gravity fuel feed limit

A

2T inner unusable per tank

Ceiling FL200 if airtime more than 30min

FL150 if less than

133
Q

EMER elec go around

A

NO FD request simple procedure

134
Q

EO go around attitude

135
Q

NDB and VOR approach tolerance

A

NDB 5

VOR 2.5

136
Q

Energy descent VS and mm

A

6000ft and 40nm

137
Q

TORA
TODA
ASDA
ASDR

A

TODA=TORA+CLEARWAY

ASDA=TORA+STOPWAY

138
Q

When is alpha floor lost

A

When auto thrust on AND

EO with slag flaps out

EO with derated thrust

Above 100RA

Above 0.53M

TLA below 5* considered EO

139
Q

APU fuel burn source

A

ENG 1 collector cell(FWD APU PUMP)

Trim pipe(both uses AFT APU PUMP)

Trim tank

140
Q

Auto flap retract

141
Q

Buffer for CAT B

A

1~1.5ton due high level and tendency of short cut

142
Q

Tendency of cancel flight to ZFW in ZSPD

A

Dramatic increase in ZFW

143
Q

Technique to increase climb

A

Selected speed

Derate 1

FLX

Around 30-40nm

144
Q

Reason check fuel distributions

A

Due possible non star dead fuel distribution

145
Q

Fuel management for trim transfer on known unlikely arrival (shorter star)

A

Put a shorter arrival

FWD transfer earlier

146
Q

Traffic speration

TAKE OFF

ARRIVAL

A

2min for super 6nm

4nm same type

147
Q

Speed brake inhibit

A

MLA

ALPHA PROT

low speed stability

Above MCT

Spoiler angle reduced in 2,3,full

148
Q

Fuel low consideration

A

Maybe fuel in trim pipe

149
Q

Mach switch over

A

FL315 average

150
Q

Raining brake consideration

A

Use max rev due no fan with ELEC

151
Q

GRID mora ND

152
Q

Manage descent look out

A

May overspeed

153
Q

PRIM function

A

All laws

Speed brake

Speed protection

Rudder travel limit

154
Q

SEC

A

Direct law with yaw damper

Rudder trim and travel limiter

155
Q

BCM

A

Comes up total elec failure

Loss of rudder control due PRIM AND SEC

Uses B OR Y
no turn coordination

156
Q

Repair interval

ABCD

A

A immediate
B 3
C 10
D 60

157
Q

Repair extension

A

Maximum of days noted in original defect B3 C10 D60

158
Q

Maintenance message

A

No need to care

engineer will fix within 800flight hours

159
Q

When is aircraft not longer bonded by MEL

A

After strart moving under own thrust

160
Q

Bank limit before engine scrape with landing gear down

A

17

22 uncompressed

161
Q

Tail strike angle

162
Q

ALT 1

A

Pitch, roll and yaw normal

Protections
Load
Bank angle protection
Low speed(ADR2) stability
High speed(ADR3) stability
163
Q

ALT2

A

Pitch normal
Roll direct
Yaw degraded

Load prot
Low speed stability
High speed stability
Maybe fly 4000 ft below REC

164
Q

Level off power and attitude

A

N1 around 50-60% range

3-4*

165
Q

Approach power and attitude

A

Approximately 45% N1 and 3 degrees on final

50-60% N1 for approach level off stabilized approach

166
Q

Beta target

A

0 aileron input meaning minimum drag

167
Q

How much fuel when trim tank has fuel

168
Q

When will outer tank have fuel

169
Q

Flap load relief system

A

Occurs passing 2.5kts VFE in config 2,3 or full

Returns to normal 2.5kts below VFE

Over speed warning at 4kts above actual slat flap position

170
Q

ALpha lock

A

Stops slat retraction when

AOA above 8.5 or below 148kts

Returns to normal when above 154 kts or below 8.2 or 7.6 AOA depending on aircraft

Only flap 1 to 0

Not active on ground below 60ktx

171
Q

When does brake require maintenance action

A

Above 800*

150* difference with one above 600 same gear

150* difference with one below 60*

200* difference between average on the other

172
Q

Brake cooling time without cooling fans at 400*

A

35 minutes to 300*

450 smoke appears

500 release park brake prevent hydraulic overheat

600 fire possible

173
Q

75 msg how to activate and deactivate

A

After sending do not respond

Dealt by sending “KA XXX ops normal - H75 error”

174
Q

Holding speed

A

230 below FL140
240 above FL140-200
265 above FL200

JAPAN or KOREA
200 SEA LEVEL to 6000
230 6000 to FL140
265 anything above

175
Q

Turb speed

A

240 FL200

260 FL350

0.78

176
Q

Bank angle in normal law

A

Up to 33* remains constant

Above 33-67 constant input required, let go of stick and returns to 33

177
Q

RFF for A330
DEP/ARR
ALT
ETOPS

A

Dep/ARR 9(7 if less than 72 hours)
ALT 7
ETOPS 4

May disregard if captain sees fit

178
Q

load sheet requirement before departure

A

Final load sheet onboard and ACK

or

Final signed at station and one in AC

or

Received but not acknowledged call IOC and confirm acknowledged

179
Q

Where to carry live stock

A

Bulk cargo which has ventilation

180
Q

Documents left behind departure station

A

Signed loadsheet

Trim loadsheet

DG sheet

Maintenance log

Dispatch message

181
Q

APU use exception

A

Above 26

Below 14

15min before departure

5minutes after arrival

182
Q

What temperature not to board passengers

183
Q

Max fuel discrepancy

A

+1700

-1000

184
Q

When to do water check during refuel

185
Q

Engine ground run

A

Acceptable but prefer crew to run the test

186
Q

Refusal of passenger

A

Any grounds in terms of safety. Initially by ASM or MOD

Even if passenger is sick and requires extra care.

Consider if required to evacuate

187
Q

Drunk passengers

A

Do not board them

188
Q

Pregnant woman boarding

A

1-36th week is okay

189
Q

Shaky about boarding or not

A

Sign form of indemnity

Not allowed for medical condition or disability

190
Q

Delay of boarding

A

When more than 30minutes expected

191
Q

When required for ASR in RVSM in terms of altitude deviation

192
Q

When does RVSM start

A

FL290 to FL410

193
Q

Requirement for jump seat

A

Older than 12

Not pregnant more than 26weeks

No alcohol

194
Q

Max bank angle allowed

A

25 manual

30 any other case

195
Q

Max vs

A

2500ft/min 2500ft to 1000ft

1500ft/min below 1000ft

196
Q

Volcanic ash within 60nm of track

197
Q

Alternate prediction altitude

A

FL220 within 200nm

FL310 for anything more max range speed

198
Q

Max approaches

A

3 unless significant weather improvement

199
Q

Hydraulic fluid amount

A

Green: 38L - 15.1L
Blue: 29.5L - 13.8L
Yellow: 19L - 8.5L

200
Q

ND GRID MORA range

201
Q

Abnormal hydraulic pressure with RAT

A330 (7 decks)

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