FCOM LIM Flashcards
1
Q
Maximum pax LIM
A
318 / 319 / 320 Airbus 180 / 145 / 136 Avianca 162 / 132 / 120
2
Q
Kind of operations LIM
A
VFR / IFR Extended overwater Icing conditions
3
Q
Weights LIM
A
318 / 318 / 319 / 320 / 320s Mtxw +400 = = = = Mtow 63.0 / 68.0 / 75.5 / 77.0 / 78.0 Mlw 57.5 / 57.5 / 62.5 / 66.0 / 66.0 Mzfw = / -3 / -4 / -3,5 / = MinW = / 34.5 / 35.4 / 37.2 / =
4
Q
Runway slope LIM
A
+- 2 %
5
Q
RUNWAY ALTITUDE LIM
A
MAX
9200 ft
_______________
MIN
CEO/321 -1000 ft
NEO -2000 ft
6
Q
NOMINAL RUNWAY WIDTH LIM
A
NEO/321 ……………………………………………45 m
________________________________
CEO 320 Nominal Width………………….45 m
Minimal runway width……..30 m
7
Q
WIND FOR TAKEOFF AND LANDING DRY LIM
A
A321NEO ………………………… 35kt (JUST TAKE OFF)
CEO/NEO…………………………..38kt
8
Q
Maximum X wind for TO and LNDG damp LIM
A
20kt
9
Q
Maximum X wind for TO and LNDG ice LIM
A
15Kt
10
Q
MAXIMUN TAIL WIND for AUTOMATIC LANDING LIM
A
10Kt
11
Q
Maximum wind to operate pax door LIM
A
65kt
12
Q
Maximum wind to operate cargo door LIM
A
40kt or 50kt if nose is into the wind ( and should be closed before 65Kt)
13
Q
TO is FORBIDDEN if LIM
A
Wet ice Water over compacted snow Dry snow
14
Q
MAXIMUM OPERATING SPEED VMO/MMO
A
350kt / 0.82 mach
15
Q
MAXIMUM FLAPS/SLATS SPEEDS A320
A
1 230kt 1+f 215kt 2 200kt 3 185kt Full 177kt
16
Q
MAXIMUM OPERATING SPEED VMO/MMO
A
Mvle 280kt / 0.67 mach Mvlo ext 250kt / 0.60 mach Mvlo ret 220kt / 0.54 mach
17
Q
MAXIMUM TIRE SPEED
A
195 G/S
18
Q
WIPERS MAXIMUM OPERATING SPEED
A
230kt
19
Q
COCKPIT WINDOW OPEN MAXIMUM SPEED
A
200kt
20
Q
MAXIMUN SPEED WHEN ABOVE 76000 kg
A
320 CEO……….20kt
21
Q
RAM Air inlet min pressure LIM
A
1 psi
22
Q
PACKS USE WITH LOW PRESSURE AIR CONDITIONING UNIT
A
DO NOT USE LP with / PACKS (Max p 1,2kg/s)
23
Q
APU BLEED USE WITH HIGH PRESSURE AIR START UNIT
A
DO NOT USE ( avoid system damage)
24
Q
CABIN PRESSURE MAX positive delta pressure LIM
A
9.0 psi
25
CABIN PRESSURE Max negative delta pressure LIM
-1.0 psi
26
CABIN PRESSURE Safety relief delta pressure LIM
8.6 psi (0.1psi tolerance)
27
AVIONICS VENTILATION LIM
**49°c No limit**
55°c T\< 2h
60°c T\< 1h
64°c T\< 1/2h
28
Minnimum AP engagement HEIGHT LIM
100ft or 5s ( system logic )
29
Minimum Height WITH AP In approach with FINAL APP, V/S or FPA mode
250ft
30
Minimum Height WITH AP In **CIRCLING** approach
**500** ft AGL for aircraft category **C**
**600** ft AGL for aircraft category **D**
31
Minimum Height WITH AP ILS/MLS approach when **CAT1** is displayed on the FMA
**160ft**
32
Minimum Height WITH AP **ILS**/MLS approach when **CAT2** OR **CAT 3** is displayed on the FMA
0 FT AGL if autoland
33
Minimum Height WITH AP After a manual go-around
100ft
34
Minimum Height WITH AP ( ALL OTHER PHASES ) LIM A320
500ft
35
Minimum Height SET WITH AP in OPEN DES LIM
500ft or MDA / MDH ( whichever is higher)
36
RNP ACCURACY
ENR 1.0nm TER 0.5nm APP 0.3nm
37
TO WITH OUT "GPS PRIMARY" LIM
GPS DESELECT until a safe altitude
38
TO WITH GLS LIM
FORBIDDEN
39
FOR RNAV(GNSS)
At least 1 "GPS PRIMARY"
40
USE OF NAV MODE IN RNAV APPROACH
An RNAV(RNP) approach may be performed, with GPS PRIMARY not available, only if the radio navaid coverage supports the RNP value and HIGH accuracy is displayed on the MCDU with the specified RNP, and an operational approval is obtained. An RNAV(GNSS) approach may be performed provided that GPS PRIMARY is available
41
ILS CAT2 minimum decision height LIM
100ft If manual landing disconnect ap bfr 80ft
42
ILS CAT 3 FAIL PASSIVE (single) minimum decision height LIM
50ft A/THR
43
ILS CAT 3 FAIL OPERATIONAL (dual) minimum decision height and alert height LIM
A320 NEO........ NONE
A320................... 25ft
A321.................... 22ft
AH 100ft
MIN RVR 75m
44
**ENGINE OUT** CAT**2/3** **FLAP** CONFIG LIM
A320N/21/21N........... 3+FULL
A320CEO.....................FULL
45
MINIMUM FUEL QUANTITY FOR TAKE OFF
![]() ![]() ![]() ![]() ![]() ![]() ![]()
1500kg
![]() ![]() ![]()
46
MAXIMUM TAILWIND for TAKEOFF and LANDING
A320/1 NEO.............................. 15kt
CEO...............................................10kt
**10kt......COMPANY OMA POLICY**
***\* if landing with MORE than 10kt TL use CONF FULL***
47
MAXIMUM FLAPS/SLATS SPEEDS A321
1 235kt 1+f 225kt 2 215kt 3 195kt Full 190kt
48
MINIMUM CONTROL SPEED FOR LANDING (VMCL) A320 NEO
116kts
49
MINIMUM CONTROL SPEED FOR LANDING (VMCL) A320
114kts
50
Minimum Height WITH AP ILS/MLS approach when CAT2 or CAT3 (single or dual) is displayed on the FMA
0 ft AGL if autoland
51
Minimum Height WITH AP ( ALL OTHER PHASES ) LIM A321
900ft
52
DEGRADED SITUATION If GPS PRIMARY LOST is displayed on the ND and MCDU
the navigation accuracy remains sufficient for RNP operations provided that, the RNP value is checked or entered on the MCDU and HIGH ACCURACY is displayed.
53
USE OF NAV MODE AFTER TAKEOFF
NAV mode may be used after takeoff provided that: ‐ GPS PRIMARY is available, or ‐ The flight crew checked the FMGS takeoff updating.
54
USE OF NAV MODE IN TERMINAL AREA
NAV mode may be used in terminal area provided that: ‐ GPS PRIMARY is available, or ‐ the appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed, or ‐ FMS navigation is crosschecked with navaid raw data.
55
USE OF NAV MODE IN APPROACH BASED ON RADIO NAVAIDS
A navaids approach may be performed in NAV, APP NAV or FINAL APP, with AP or FD engaged, provided that: ‐ If GPS PRIMARY is available, the reference navaid may be unserviceable, or the airborne radio equipment may be inoperative, or not installed, provided that an operational approval is obtained ‐ If GPS PRIMARY is not available, the reference navaid and the corresponding airborne radio equipment must be serviceable, tuned and monitored during the approach.
56
MAXIMUM WIND CONDITIONS FOR ILS/MLS **CAT II** OR **CAT III** AND FOR **CAT I**
Headwind : 40 kt for CAT II / 30 kt for CAT III
Tailwind : 10 kt
Crosswind: 25 kt for CAT II / 20 kt for CAT III
57
**AUTOMATIC** LANDING Alt LIMIT
A320 CEO................................. 6500ft / -1000ft
A320 NEO................................. 9200ft / -2000ft
A321 .............................................5750ft / -1000ft
58
APU START ATTEMPTS
**X3 then 60 min**
59
APU MAX ROTOR SPEED
Maximum N speed .................... 107%
60
Maximum EGT for APU start (below 35 000 ft)
1 090 °C
61
Maximum EGT for APU start (above 35 000 ft)
1 120 °C
62
Maximum EGT for APU running
675 °C
63
APU START/SHUTDOWN DURING REFUELING/DEFUELING
‐ If the APU failed to start or following an automatic APU shutdown, do not start the APU ‐ If a fuel spill occurs, perform a normal APU shutdown.
64
**APU BLEED** Max altitude to **assist engine start**
20 000 ft
65
**APU BLEED** Max altitude for **air conditioning and pressurization (_single_ pack operation) ..and elec power supply**
22 500 ft
66
**APU BLEED** Max altitude for **air conditioning and pressurization (_dual_ pack operation) ..and elec power supply**
15 000 ft
67
Use of **APU bleed** air for **wing anti-ice** is......
not permitted.
68
APU START CEILING LIMIT
41 000ft
69
APU ELEC POWER ONLY
Above 22 500ft
70
APU Battery restart limit (ELEC Emer CONFIG)
25 000 ft
71
GSM ONBOARD
The use of mobile phones is prohibited in the toilets and the cockpit. It is prohibited to use the GSM Onboard System: ‐ Below 3 000 m AGL (approximately 10 000 ft) ‐ In some geographical areas (refer to the “Regional Operation Data for the Onboard Mobile Telephony System” document for the identification of these geographical areas).
72
THRUST SETTING/EGT LIMITS
A320 NEO
73
THRUST SETTING/EGT LIMITS
A320 IAE
74
THRUST SETTING/EGT LIMITS
A321 PW
75
SHAFT SPEEDS ( N )
A320 NEO
Maximum N1 in normal operation..............................................................100 %
Maximum N1 permitted.................................................................................105 %
\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Maximum N2 in normal operation.............................................................100 %
Maximum N2 permitted.......................................................................................................... 105 %
76
SHAFT SPEEDS (N)
A320 CEO
A321
Maximum N1......................................................................................................100 %
\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_
Maximum N2 ...................................................................................................100 %
77
OIL TEMPERATURE
A320 CEO
A321
78
OIL TEMPERATURE
A320 NEO
79
MINIMUM OIL PRESSURE
A320 CEO
A321
80
MINIMUM and MAXIMUM OIL PRESSURE
A320 NEO
81
MINIMUM OIL QUANTITY
A320 NEO - 14 quarts
A320 CEO and A321 - 11 quarts (0.3 qt/h)
82
START attempts
A320 NEO ........ 3x /35s/ then 15 min
(The starter must not be run when N2 is above 20 %)
A320 CEO / A321 ...... 3x /15s/ then 30 min or 5 min crank
(The starter must not be run when N2 is above 10 % on-ground and 18 % in-flight.
83
REVERSE THRUST
Maximum reverse should not be used below 70 kt.
Idle reverse is permitted down to aircraft stop.
84
REDUCED THRUST TAKEOFF
TFLEX cannot be:
‐ Higher than TMAXFLEX, equal to ISA + 50 °C.(NEO)
ISA + 55 °C.(CEO)
ISA + 42 °C.(A321)
ISA + 72 °C.(LCH,LCI)
‐ Lower than the flat temperature (TREF).
‐ Lower than the actual OAT.
85
CROSSWIND OPERATION ON GROUND
NEO.............. The engine is able to start in crosswind up to 35 kt.
CEO.................The engine is able to start in crosswind up to 35 kt. **(GUST)**
321N...............The engine is able to start in crosswind up to **45** kt.
86
MAXIMUM ALTITUDE FLAPS/SLATS EXTENDED
Maximum operating altitude with slats and/or flaps extended.....................20 000 ft
87
FUEL TEMPERATURE LIMITS WHEN JP4 AND JET B FUELS ARE USED
If the wing fuel temperature exceeds 30 °C at engine start, the altitude must be limited to 35 000 ft until the center tank is empty.
If the wing fuel temperature exceeds 40 °C at engine start, the altitude must be limited to 30 000 ft until the center tank is empty.
If the wing fuel temperature exceeds 49 °C at engine start, the altitude must be limited to 25 000 ft until the center tank is empty.
88
FUEL TEMPERATURE
A320 CEO
89
FUEL TEMPERATURE
A320 NEO
90
FUEL TEMPERATURE
A321
91
MAXIMUM ALLOWED FUEL IMBALANCE
500 kgs .... inner tank. CHECK TABLE
92
DEFINITION OF SEVERE ICE ACCRETION
Ice accretion is considered severe when the ice accumulation on the **airframe** reaches approximately
**5 mm** (0.2 in) thick or more.
93
DEFINITION OF ICING CONDITIONS
‐ Icing conditions exist when the OAT (on ground or after takeoff) or the TAT (in flight) is at or
below 10 °C and visible moisture in any form is present (such as clouds, fog with visibility of 1 sm (1 600 m) or less, rain, snow, sleet or ice crystals).
‐ Icing conditions also exist when the OAT on the ground and for takeoff is at or below 10 °C and operating on ramps, taxiways or runways where surface snow, standing water or slush may be ingested by the engines, or freeze on engines, nacelles or engine sensor probes.
94
DEFINITION OF THIN HOARFROST
Thin hoarfrost is typically a white crystalline deposit which usually develops uniformly on exposed surfaces on cold and cloudless nights.
It is so thin that surface features (lines or markings) can be distinguished beneath it.
95
RAIN REPELLENT usage
The flight crew should only use the rain repellent in the case of **moderate to heavy rain.**
96
BRAKE TEMPERATURE
Maximum brake temperature for takeoff (brake fans off).....................................................300 °C
97
MINIMUM FLIGHT CREW OXYGEN PRESSURE
check table
98
NOSEWHEEL STEERING (NWS)
Towbarless operation on the nose landing gear (towing and pushback) is approved when using the accepted towbarless towing vehicles listed in the Airbus WISE ISI 09.11.00001, with the following
information:
Maximum NWS angle...................................................................................... ±85 °
99
INERTIAL REFERENCE SYSTEM (IRS)
IR GROUND ALIGNMENT
Ground alignment of the IRS is possible in latitudes between 73 ° North and 73 ° South.
100
TAXI WITH DEFLATED OR DAMAGED TIRES
‐ If maximum one tire per gear is deflated (consider three gears)
Maximum taxi speed during turn................................................................................................. 7 kt
‐ If two tires are deflated on the same main gear (maximum one main gear)
Maximum taxi speed................................................................................................................... 3 kt
‐ For the nosewheel steering (NWS) angle
Maximum NWS angle................................................................................................................. 30 °
101
GPWS / PREDICTIVE GPWS
The predictive GPWS functions should be inhibited (TERR pushbutton to OFF, on the GPWS panel) when the aircraft position is less than 15 NM from the airfield:
‐ For operations from/to runways not incorporated in the predictive GPWS database.
‐ For specific approach or departure procedures, which have previously been identified as potentially causing expected or spurious terrain alerts.
102
FLIGHT MANEUVERING LOAD ACCELERATION LIM
Clean configuration .........-1 g to +2.5 g Other configurations.........0 g to +2 g
103
MINIMUM CONTROL SPEED FOR LANDING (VMCL) OLD A320
109kts
104
CAN YOU MAKE AN **AUTOLAND** IF **CAT 2** ON FMA?
**YES - *"At least CAT2 capability is displayed on the FMA and the crew uses CATII / III procedures"***
105
**GSM ONBOARD**
FORBIDDEN in the toilets and cockpit
