LIM Flashcards
Load limit
Clean config
Other config
-1 to +2.5g
0g to +2g
Max landing weight
177-187
- 9
- 5
- 2
- 7
- 7
Airport operational limit
Slope
Altitude and temp
2%
12500ft
-53*C
Max TAKE OFF X wind
Max landing x wind
Max tail wind
Max cargo door
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
Run way condition prohibit take off
Wet ice
Water on to of compacted snow
Any snow over ice
VMO/MMO
330
.86
VA
.78
VMCL
126kts
Flap 1 1+F 2 3 Full
240 215 196 186 180
Landing gear extended
Extend/retract
GRAVITY extend
250
250
200
Tire speed
204
Wipers
230
Window
230
Packs must be off
RAM air
1PSI
Ground air and APU
only one can be used at a time
Max and Min differential pressure
safety valve pressure
+9.25 -1
+8.85 -0.26
Max normal cabin altitude
max selectable cabin altitude
8000ft
14000ft
Auto land minimum weight
123000kg
Without GPS Primary what happens
FM updates via NAV aids or simply uses the NAV aid to determine position
Time limitation for RNP 10nm without GPS primary
No time limitation if NAV aids are around(auto update position)
5.7 hours after the last update position
CAT 2 minimum DH
Required automatics
height to disconnect AP if manual landing
100ft and 80ft
1 AP
CAT3A DH and required automatics
50ft
1AP and ATHR
CAT3B
2AP and ATHR
EO autoland requirement
CONFIG 3 and ECAM done by 1000ft
Auto land max wind
35,20,10
Auto land Slope Elevation Weight VApp max wind correction Runway condition
-2.5 to -3.25
9200ft
Max landing weight
VLS+5-15kts
Depending situation, max auto land weight
229tones
Altitude phones prohibited
ON BOARD MOBILE TELEPHONY SYSTEM
Below FL100 AGL
When does IN SEAT POWER SUPPLY SYSTEM must be switched off
Take off and landing
Max flap slats operation altitude
20 000ft
Fuel JET B AND JP4 limitation
Trim tank empty and isolated during entire flight
Inner tank max fuel imbalance
Outer tank max fuel imbalance
2900kg
1480 kg
No limitation for fuel imbalance what weight
7500kg
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
Trim tank forward transfer pump failure
Do not transfer fuel unless less than 3* pitch, to avoid fuel flowing back.
Transfer in descent
Wing Tk LO LVL
No take off
Mixed fuel
Okay as long as known freezing point
Normal hydraulic pressure
3000+_200PSI
Max brake temperature for take off without brake fan
300
PFD BOTH LOST watch out of ISIS
Do not use the big
Oxygen time
Emergency decent
FL 100
SMOKE 100%
15min
105min
8000ft 15min
22min
98min
8000ft 15min
LOW OIL LEVEL ECAM
Max 15 hours APU operator
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
Takeoff EGT and time limit
920 20s
900 5minutes
900 10minutes EO
MCT EGT and time
850 unlimited
Starting EGT
GROUND
AIR START
700*C
850*C
Engine OIL temp
MAX
MIN for take off
190*C
20*C
Oil pressure MIN
Oil quantity MIN
25PSI
Min 15qt or 6qt + 0.7qt/hr
N1
N2
N3
99
103.3
100
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
Max fuel in tanks
- 2
- 3
- 5
Fuel burn per hour
2600kg for 30minutes
5.2 for one hour
700 per hold
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
Reset time
CB
COMPUTER
5s
3s
Landing distance on
MP, flap 3, 10T over weight, ISA+20, 1000ft
3360 without 15%
FM reset period
ND map not available
MCDU please wait
2-3minutes
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
Max temp for one brake to avoid park brake
500 or 350 with brake fans
Brake pressure check PSI
2200-2700
Rain repellent restriction
Don’t use when dry
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
Fast alignment
Less than 5 seconds
Pack flow low when
200 passengers or below 60% ECON px
180 degree turn minimum distance
42m for 200
46m for 300
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
When are trim tank isolation valves closed
Take off and landing
Too far aft CG
FMGEC set 3% forward
FQI degradation or ZFW/ZFWCG not entered
Forward 1.5%
Amber box OXY
Below 1000PSI
Check LIM (640 at 50*C)
APU behavior below 10*C
12PSI with bleed fluctuation
Instrument tolerance
PFD ground check 25ft/300 STBY/
On ground cross check/20ft/none STBY/60isis
ECAM CG VS LOADSHEEY
2%
Change on INIT B comparing loadsheet final and prelim
300kg 0.5%
Ground crew aware push back max angle
65*
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
Time before take off after engine start
5 minutes
3 minutes less than 1.5 hour turn around
Ice shedding procedure
Below 1*C
N1 50% for 10s every hour
Every 45 if freezing fog taxi in and out
Rudder trim limit
0.6*
When brake fans off after engine start
Green arc
Take off thrust initially
1.1 EPR
HALF FORWARD
FULL FORWARD IF 20kts x wind or tail wind