LIM Flashcards
1
Q
Load limit
Clean config
Other config
A
-1 to +2.5g
0g to +2g
2
Q
Max landing weight
A
177-187
- 9
- 5
- 2
- 7
- 7
3
Q
Airport operational limit
Slope
Altitude and temp
A
2%
12500ft
-53*C
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
5
Q
Run way condition prohibit take off
A
Wet ice
Water on to of compacted snow
Any snow over ice
6
Q
VMO/MMO
A
330
.86
7
Q
VA
A
.78
8
Q
VMCL
A
126kts
9
Q
Flap 1 1+F 2 3 Full
A
240 215 196 186 180
10
Q
Landing gear extended
Extend/retract
GRAVITY extend
A
250
250
200
11
Q
Tire speed
A
204
12
Q
Wipers
A
230
13
Q
Window
A
230
Packs must be off
14
Q
RAM air
A
1PSI
15
Q
Ground air and APU
A
only one can be used at a time
16
Q
Max and Min differential pressure
safety valve pressure
A
+9.25 -1
+8.85 -0.26
17
Q
Max normal cabin altitude
max selectable cabin altitude
A
8000ft
14000ft
18
Q
Auto land minimum weight
A
123000kg
19
Q
Without GPS Primary what happens
A
FM updates via NAV aids or simply uses the NAV aid to determine position
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
21
Q
CAT 2 minimum DH
Required automatics
height to disconnect AP if manual landing
A
100ft and 80ft
1 AP
22
Q
CAT3A DH and required automatics
A
50ft
1AP and ATHR
23
Q
CAT3B
A
2AP and ATHR
24
Q
EO autoland requirement
A
CONFIG 3 and ECAM done by 1000ft
25
Auto land max wind
35,20,10
26
```
Auto land
Slope
Elevation
Weight
VApp max wind correction
Runway condition
```
-2.5 to -3.25
9200ft
Max landing weight
VLS+5-15kts
27
Depending situation, max auto land weight
229tones
28
Altitude phones prohibited
ON BOARD MOBILE TELEPHONY SYSTEM
Below FL100 AGL
29
When does IN SEAT POWER SUPPLY SYSTEM must be switched off
Take off and landing
30
Max flap slats operation altitude
20 000ft
31
Fuel JET B AND JP4 limitation
Trim tank empty and isolated during entire flight
32
Inner tank max fuel imbalance
Outer tank max fuel imbalance
2900kg
1480 kg
33
No limitation for fuel imbalance what weight
7500kg
34
Max fuel tempJET A and so on
JET B AND JET4
Min temperature
+55
+49
Freezing point or -44, below FL 300
-54 above FL300
35
Trim tank forward transfer pump failure
Do not transfer fuel unless less than 3* pitch, to avoid fuel flowing back.
Transfer in descent
36
Wing Tk LO LVL
No take off
37
Mixed fuel
Okay as long as known freezing point
38
Normal hydraulic pressure
3000+_200PSI
39
Max brake temperature for take off without brake fan
300
40
PFD BOTH LOST watch out of ISIS
Do not use the big
41
Oxygen time
Emergency decent
FL 100
SMOKE 100%
15min
105min
8000ft 15min
22min
98min
8000ft 15min
42
LOW OIL LEVEL ECAM
Max 15 hours APU operator
43
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
3 times
Max alt FL415
Battery start FL250
Bleed+power FL225
FL250
APU MASTER 3 min then start
115kVA
44
Takeoff EGT and time limit
920 20s
900 5minutes
900 10minutes EO
45
MCT EGT and time
850 unlimited
46
Starting EGT
GROUND
AIR START
700*C
850*C
47
Engine OIL temp
MAX
MIN for take off
190*C
20*C
48
Oil pressure MIN
Oil quantity MIN
25PSI
Min 15qt or 6qt + 0.7qt/hr
49
N1
N2
N3
99
103.3
100
50
Starter limit
Max continuous
Cycles
Max N1 for start
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
51
Max fuel in tanks
76. 2
76. 3
76. 5
52
Fuel burn per hour
2600kg for 30minutes
5.2 for one hour
700 per hold
53
Stabilization criteria
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
54
Reset time
CB
COMPUTER
5s
3s
55
Landing distance on
MP, flap 3, 10T over weight, ISA+20, 1000ft
3360 without 15%
56
FM reset period
ND map not available
MCDU please wait
2-3minutes
57
When will all data be lost in FM
Caution during reset
3 Dual FM reset within 2minutes
Don't do anything with MCDU for atleast 1 minute in case of causing another reset
58
Max temp for one brake to avoid park brake
500 or 350 with brake fans
59
Brake pressure check PSI
2200-2700
60
Rain repellent restriction
Don't use when dry
61
When complete IRS alignment
First flight of day
Crew change
GPS not avail + poor NAV aid coverage
GPS not avail with flight time more than 3 hours
62
Fast alignment
Less than 5 seconds
63
Pack flow low when
200 passengers or below 60% ECON px
64
180 degree turn minimum distance
42m for 200
46m for 300
65
When does trim tank transfer start and end
```
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
66
When are trim tank isolation valves closed
Take off and landing
67
Too far aft CG
FMGEC set 3% forward
68
FQI degradation or ZFW/ZFWCG not entered
Forward 1.5%
69
Amber box OXY
Below 1000PSI
Check LIM (640 at 50*C)
70
APU behavior below 10*C
12PSI with bleed fluctuation
71
Instrument tolerance
PFD ground check 25ft/300 STBY/
On ground cross check/20ft/none STBY/60isis
72
ECAM CG VS LOADSHEEY
2%
73
Change on INIT B comparing loadsheet final and prelim
300kg 0.5%
74
Ground crew aware push back max angle
65*
75
NWS memo not appear during push back
No engine start during push back.
Avoid damage on nose wheel during pressurization
Refer to limitation for dispatch
76
Time before take off after engine start
5 minutes
3 minutes less than 1.5 hour turn around
77
Ice shedding procedure
Below 1*C
N1 50% for 10s every hour
Every 45 if freezing fog taxi in and out
78
Rudder trim limit
0.6*
79
When brake fans off after engine start
Green arc
80
Take off thrust initially
1.1 EPR
HALF FORWARD
FULL FORWARD IF 20kts x wind or tail wind
81
MAX REC buffer
0. 3g
| 0. 2g accepted if entered
82
EO circle to land weight unable maintain level flap 3
30 degrees at 230 tones
83
How is IDG cooled
Through engine fan air
84
Reset computer time
1s
85
ENG2 fail caution of hydraulic
If flaps or slats out ELEC pump will keep running. Turn it off
86
NPA buffer
50ft
87
Engine out ceiling +20*C ISA
Atleast FL150
88
EO timing for relight when start
Starter to IGN
89
IOC alert phase
ATSU next page
90
Circling approach
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
Why take FLX out if TOGA take off
If forgot to put TOGA plane will warn with ECAM
92
Windshear flap setting
flap 3
93
ECAM status and down to INOP SYS last thing before REMOVE STATUS
GW above landing weight or not
94
Altitude for APU BLEED
1 PACK
ENG START
2 PACKS
FL225
FL200
FL175
95
item to include brief
PACKS for RTOW, DEPARTURE BRIEF, CTWO+
96
Failure management for partner
MAKE SUMMARY
CRZ APPR LANDING GA
97
When is predictive windshear inhibit
100kt to 50ft take off up to 2300
below 50ft for landing
98
When is REACTIVE windshear operational
3s after lift off up to 1300ft RA
1300ft down to 50ft
99
Why selected speed slat flap jam
because managed speed will lead to follow of GD S or F speed which are inacurate
100
if must head somewhere else, how to find out MAX speed with slat flap jam
speed out until hear bing
101
GA slat flap jam
go to max speed
102
Stoping with accumulator pressure
Stop on runway
103
When is it considered one application
when feet completely off
104
Landing PERF failure codes
COMP somehwere QRH
105
Hold sector entry
Max speed
Direct
Parallel
Offset
230kts
106
NPA what kind of approach
stablilized approach
107
Derated climb
Tends to burn more fuel but reduces maintenance costs
108
When pack flow low
Below 200 PX
AND
ECON below 60% 138
109
SID protection zone within 25nm MSA
900m left and right of track
+35ft. Clearance
50ft in turn
110
Beyond 25nm MSA protection on track
5nm left and right of track
2000ft clearance
111
EO fuel burn compared to both engine operative
+30%
112
EO ceiling with full anti ice
FL135
113
Minimum climb gradient
11.8%
114
RAT powering EMER GEN fuel pumps working
Left 2, or right 2 if left 2 inop
115
Fuel transfer sequence
4000kg trim tank to inner
3500kg outer to inner
116
V1
VR
V2
VR min 1.05 stall
V2 min 1.1 stall
117
Flex max thrust reduction
25% reduction
118
Runway line up allowance
Displac d thresh hold
25. 1m 90* turn TODA
55. 4m 180* turn TODA
50. 5m ASDA
80. 8m ASDA
Displaced thresh hold no allowance
119
Minimum ground roll
Shortest distance for take off. Add MR
Limits flex +31
Shorten runway 2000ft or 1000ft
120
APU fuel burn
130kg roughly 200kg
121
Auto brake not in IFL
Anything with delta VREF or failure code. Manual only
122
Wing span
60m
123
Contingency
Recommended extra
Mandatory fuel
total 1500kg
Contingency 300kg
124
SPEED SPEED SPEED aural warning
2000ft to 100ft RA
PRIM generated
Only in normal law
None of both RA failed
Flap 2,3,full
125
Pitch protection
30* 25* if low speed. 15* nose down
Green = sign
126
High speed protection
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
When does AP and FD disappear in turn
Above 45* reappear after 40*
128
Beta target generation
PRIM
129
Maneuver load alleviation
Trigger
8* +2g
Aileron and spoilers deflected to reduce load
Elevator compensates pitch moment
Trigger above 250kt
Clean
Normal or alternate law
130
Runway lighting
300m before threshold (red)and 900m into runway(red and white)
131
Taxi way lights on runway and when clear of ILS sensitive areas
Yellow green then full green
132
Gravity fuel feed limit
2T inner unusable per tank
Ceiling FL200 if airtime more than 30min
FL150 if less than
133
EMER elec go around
NO FD request simple procedure
134
EO go around attitude
10-12.5
135
NDB and VOR approach tolerance
NDB 5
VOR 2.5
136
Energy descent VS and mm
6000ft and 40nm
137
TORA
TODA
ASDA
ASDR
TODA=TORA+CLEARWAY
ASDA=TORA+STOPWAY
138
When is alpha floor lost
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
APU fuel burn source
ENG 1 collector cell(FWD APU PUMP)
Trim pipe(both uses AFT APU PUMP)
Trim tank
140
Auto flap retract
200
141
Buffer for CAT B
1~1.5ton due high level and tendency of short cut
142
Tendency of cancel flight to ZFW in ZSPD
Dramatic increase in ZFW
143
Technique to increase climb
Selected speed
Derate 1
FLX
Around 30-40nm
144
Reason check fuel distributions
Due possible non star dead fuel distribution
145
Fuel management for trim transfer on known unlikely arrival (shorter star)
Put a shorter arrival
FWD transfer earlier
146
Traffic speration
TAKE OFF
ARRIVAL
2min for super 6nm
| 4nm same type
147
Speed brake inhibit
MLA
ALPHA PROT
low speed stability
Above MCT
Spoiler angle reduced in 2,3,full
148
Fuel low consideration
Maybe fuel in trim pipe
149
Mach switch over
FL315 average
150
Raining brake consideration
Use max rev due no fan with ELEC
151
GRID mora ND
Use CSTR
152
Manage descent look out
May overspeed
153
PRIM function
All laws
Speed brake
Speed protection
Rudder travel limit
154
SEC
Direct law with yaw damper
Rudder trim and travel limiter
155
BCM
Comes up total elec failure
Loss of rudder control due PRIM AND SEC
Uses B OR Y
no turn coordination
156
Repair interval
| ABCD
A immediate
B 3
C 10
D 60
157
Repair extension
Maximum of days noted in original defect B3 C10 D60
158
Maintenance message
No need to care
| engineer will fix within 800flight hours
159
When is aircraft not longer bonded by MEL
After strart moving under own thrust
160
Bank limit before engine scrape with landing gear down
17
22 uncompressed
161
Tail strike angle
10.1
162
ALT 1
Pitch, roll and yaw normal
```
Protections
Load
Bank angle protection
Low speed(ADR2) stability
High speed(ADR3) stability
```
163
ALT2
Pitch normal
Roll direct
Yaw degraded
Load prot
Low speed stability
High speed stability
Maybe fly 4000 ft below REC
164
Level off power and attitude
N1 around 50-60% range
3-4*
165
Approach power and attitude
Approximately 45% N1 and 3 degrees on final
50-60% N1 for approach level off stabilized approach
166
Beta target
0 aileron input meaning minimum drag
167
How much fuel when trim tank has fuel
36.5 tone
168
When will outer tank have fuel
Above 9
169
Flap load relief system
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
ALpha lock
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
When does brake require maintenance action
Above 800*
150* difference with one above 600 same gear
150* difference with one below 60*
200* difference between average on the other
172
Brake cooling time without cooling fans at 400*
35 minutes to 300*
450 smoke appears
500 release park brake prevent hydraulic overheat
600 fire possible
173
75 msg how to activate and deactivate
After sending do not respond
Dealt by sending "KA XXX ops normal - H75 error"
174
Holding speed
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
Turb speed
240 FL200
260 FL350
0.78
176
Bank angle in normal law
Up to 33* remains constant
Above 33-67 constant input required, let go of stick and returns to 33
177
RFF for A330
DEP/ARR
ALT
ETOPS
Dep/ARR 9(7 if less than 72 hours)
ALT 7
ETOPS 4
May disregard if captain sees fit
178
load sheet requirement before departure
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
Where to carry live stock
Bulk cargo which has ventilation
180
Documents left behind departure station
Signed loadsheet
Trim loadsheet
DG sheet
Maintenance log
Dispatch message
181
APU use exception
Above 26
Below 14
15min before departure
5minutes after arrival
182
What temperature not to board passengers
28
183
Max fuel discrepancy
+1700
-1000
184
When to do water check during refuel
1000L
185
Engine ground run
Acceptable but prefer crew to run the test
186
Refusal of passenger
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
Drunk passengers
Do not board them
188
Pregnant woman boarding
1-36th week is okay
189
Shaky about boarding or not
Sign form of indemnity
Not allowed for medical condition or disability
190
Delay of boarding
When more than 30minutes expected
191
When required for ASR in RVSM in terms of altitude deviation
300ft
192
When does RVSM start
FL290 to FL410
193
Requirement for jump seat
Older than 12
Not pregnant more than 26weeks
No alcohol
194
Max bank angle allowed
25 manual
30 any other case
195
Max vs
2500ft/min 2500ft to 1000ft
1500ft/min below 1000ft
196
Volcanic ash within 60nm of track
DAY VMC
197
Alternate prediction altitude
FL220 within 200nm
| FL310 for anything more max range speed
198
Max approaches
3 unless significant weather improvement
199
Hydraulic fluid amount
Green: 38L - 15.1L
Blue: 29.5L - 13.8L
Yellow: 19L - 8.5L
200
ND GRID MORA range
40nm
201
Abnormal hydraulic pressure with RAT
2500 psi
