Limitations Flashcards
(234 cards)
1
Q
Flight Manoeuvring Load Acceleration Limits Clean:Slaps & flats extended:Slats extended ONLY:
A
Clean: -1g to +2.5g
Slaps & flats extended: 0g to +2g
Slats extended ONLY: 0g to +2g
FCOM - LIM - 10 - General
2
Q
Weight Limitations: !! A320 !!(highest available option)
Maximum taxi weight (highest option available):
Maximum take off weight (breaks release, highest)
Maximum landing weight:
Maximum zero fuel weight:
Minimum weight:
A
FOR A320!!
Highest available option
Maximum taxi weight: 77,400 / 73,900
Maximum take off weigh: 77,000 / 73,500
Maximum landing weight: 66,000
Maximum zero fuel weight: 62,500
Minimum weight: 37,230
FCOM - Lim - 11 - Weight & CG
3
Q
Weight Limitations: !! A319 !!(highest / lowest available )Maximum taxi weight: highest / lowestMaximum take off weight (breaks release) highest / lowestMaximum landing weight:Maximum zero fuel weight:Minimum weight:
A
4
Q
Coldest acceptable
OUTSIDE AIR TEMPERATURE at FL399
A
-70
FCOM - Lim 12
5
Q
Maximum allowable runway slope (mean)
A
6
Q
Max runway altitude
A
9,200ft
7
Q
Nominal runway width
A
8
Q
A
38kt (gusts included)
9
Q
Max tailwind
A
10kts
10
Q
Max wind for passenger door operation
A
65kts
11
Q
Max wind for cargo door operation
A
40kts OR 50kts if:
1) Nose into wind OR
2) Cargo door on LEEWARD side
Should be closed by 65
11
Q
What wind MUST the cargo doors be closed by?
A
65kts
12
Q
A
13
Q
Maximum crosswind for TAKEOFF or LANDING (gust included) for:
Slush / Dry Snow / Wet Snow (up to 3mm)
Frost / Compacted snow (temp
A
29kt
14
Q
Maximum crosswind for TAKEOFF or LANDING (gust included) for:
Dry Snow: >3mm
Wet snow: > 3mm
Compacted snow (OAT ABOVE 15)
Slippery When Wet
A
25kts
15
Q
Maximum crosswind for TAKEOFF or LANDING (gust included) for:
Water: >3mm up to 12.7mm (1/2”)
Slush: >3mm up to 12.7mm (1/2”)
A
20kts
16
Q
Maximum crosswind for TAKEOFF or LANDING (gust included) for:
ICE (cold & dry)
A
15kts
17
Q
Maximum crosswind for TAKEOFF or LANDING (gust included) for:
Damp Wet (up to 3mm)
A
38kts
18
Q
Take off is not recommended with what runway conditions?
A
19
Q
What is the MMO?
A
20
Q
What is VMO between 24,600 and 0ft?
A
350kts
21
Q
A319 VMCA at 0ft Altitude
A
22
Q
A319 VMCG at 0ft AltitudeConf 1+F: ?Conf 2: ?COnf 3: ?
A
At 0ft altitudeAll configs: 104.5
23
Q
A320 VMCA at 0ft altitude
A
110ts(-2000 = 112 and +2000= 108)** shark and no sharks have the same VMCA
24
25
26
Maximum Flap / Slats speeds:Conf 1: ? Conf 1 + F: ?Conf 2: ?COnf 3: ?Conf FULL: ?
27
How many slat positions are there?
(i.e when you move the lever, the slats move to a new position.)
3.
Conf 2 + 3 slats are the same.
28
29
What is VLE and What is the VLE speed?
VLE = Max speed with landing gear extended.
280ts / 0.67
30
What is 'VLO extension' and what is the speed?
VLO Extension: Max speed the landing gear can be extended 250kt
31
What is 'VLO retraction' and what is the speed?
VLO Extension:
Max speed the landing gear can be retracted is 220kts
32
Maximum altitude at which the gear may be extended?
25,000ft
33
Speed at which the gear is hydraulically active?
260kts
34
Max wind for cargo door operation
35
Maximum tire speed?
195kts
35
Windshield wiper max speed?
36
Cockpit window open max speed?
37
A320 -
What WEIGHT should you consider for taxiing?
What speed restriction?
Taxi weight about 76,000kg.
Do not exceed a taxi speed of 20kts in a turn.
38
Ram air inlet pressure limitation?
Only open if diff. pressure
39
Air conditioning with LP ground unit?
What max airflow?
What other limitations?
Max airflow from ground cart of 1.2kg/s
Do not use conditioned air simultaneously from the packs and th LP ground unit (avoid chattering of non return valve)
40
APU with HP ground unit - what restrictions?
Do not use HP ground unit when APU supplies bleed air, to avoid bleed system damage.
41
Cabin pressurisation:Maximum positive diff pressure
9.0 PSI
42
Cabin pressurisation:
Maximum negative diff pressure
-1psi
43
Cabin pressurisation:
What is the safety Relief Valve setting?
8.6 PSI
44
Cabin altitude warning - what height?
45
Maximum cab altitude selection?
Minimum cabin altitude selection?
14,000ft and -2000ft
46
Max diff pressure and safety valve tolerance?
+/- 7hpa or 0.1 PSI
47
Avionics ventilation:During ground operations, limit the aircraft power supply with avionics ventilation system in the normal configurations follows:OAT = 49 = ?OAT = 55 = ?OAT = 60 = ?OAT = 64 = ?
OAT = 49 = No limitOAT = 55 = 2 hoursOAT = 60 = 1 hourOAT = 64 = 1/2 hour
48
Minimum height for use of autopilot on takeoff with SRS mode?
49
Minimum height for use of the autopilot in:
\* Straight in , non precision approach = \*
Circling approach =
ILS approach (Cat 1 ) =
PAR approach =
Go around (AP / FD engagement) =
All other phases =
Use of AP / FD in OPEN DES / DES mode not permitted in approach, unless:??
\* Straight in , non precision approach = minima\*
Circling approach = minima - 100ft
ILS approach (Cat 1 ) = 160ft AGL
PAR approach = 250ft AGL
Go around (AP / FD engagement) = 100ft AGL
All other phases = 500ft AGL
Use of AP / FD in OPEN DES / DES mode not permitted in approach, unless: Altitude is set to / above MDA or 500ft whichever is highest
50
Non precision approaches with engine out:DOES THE FOLLWING APPLY TO:1) A319?2) A3203) BothIf one engine is INOP, it is not permitted to use the autopilot to perform NPAs in the following modes: FINAL APP, NAV / v/s and nav / fpa. Only FD use is permitted.
1) A319 only.It is no longer applicable to ANY A320.
51
ILS Cat II Minimum decision height:
100ft AGL
52
ILS Cat II
How many Autopilots required?
At least ONE must be engaged in approach mode and Cat 3 single / dual must be displayed on FMAs.
(A/THR must be used selected or managed mode)
53
ILS Cat III Fail Passive (single)Minimum decision height?
50ft
54
ILS Cat III Fail Passive (single)
How many autopilots required?
At least ONE must be engaged in approach mode and Cat 3 single / dual must be displayed on FMAs.
(A/THR must be used selected or managed mode)
55
ILS Cat III Fail Operational (Dual)
What is the ALERT height?
100ft
56
ILS Cat III Fail Operational (Dual)
Cat III with DH = what is the minimum decision height?
20ft
57
ILS Cat III Fail Operational (Dual)
How many autopilots required with DH and Without?
2 Autopilots must be engaged in APPR mode and CAT 3 DUAL must be displayed.
A/THR must be used in selected or managed mode.
58
Cat III without DH
What is the minimum RVR?
75m
59
Engine out AUTOMATIC landing.
What flap setting is allowable for
a) A319
b) A320?
a) A319 can be automatically landed, single engine, with Flaps 3 or Flaps Fullb) A320 can only be automatically landed, single engine, in flaps Full.
60
What are the automatic landing / rollout wind limits for A320 Sharklets?
Headwind:
Tailwind:
Crosswind:
Headwind: 30
Crosswind (without rollout): 20
Crosswind (with rollout): 15
Tailwind: 10
61
Automatic landing limitations:Slope angle = Maximum Airport elevation = Maximum weight = A319 exception = Minimum elevation? =Sharklet exception = Roll out RWY conditions =
62
ILS Auto Landing in CAT 1 or better Auto landing in CAT 1 or better weather is possible on cat 1 ground installations or when ILS sensitive areas are not protected under which precautions?
- Airline has checked that ILS beam quality and the effect of terrain profile before the runway has no adverse affect on AP / FD guidance. (in part. terrain within 300m must be evaluated)
- Crew is aware that LOC / GS beam fluctuations may occur. PF read to immediately disco. AP and take appropriate action.
- At least CAT 2 capability on FMA and Cat II / III procedures applied
- Visual references are obtained at an altitude appropriate to the performed cat 1 approach, otherwise a go around must be flown.
63
ELECTRICAL
What is the max continuous load per generator?
100% (90 kva)
64
ELECTRICAL
Max cont. load per TR
200A
65
FLAPS & SLATSMaximum altitude with F&S extended
20,000ft
66
FUEL (NON shark)
Maximum imbalance allowed
INNER when heavier tank fuel quantity is:
FULL = 4300kg= 2250kg = 1500kg = OUTER: =
Special notes & exceptions =
NON SHARK INNER when:
FULL = 1500kg 4300kg= 1600kg2250kg = 2250kg 1500kg = NO LIMIT BELOW 2250kg quantityOUTER: = 690kg
\*\*\*\*Special notes = \*\*\*\*
= Max imbalance (one fuel / one empty) allowed provided:1) Fuel content on one side (outer + inner) is equal to fuel content of other side (outer + inner)OR2) On the side of the lighter outer tank, the inner tank fuel quantity is higher than the opposite inner tank quantity. (up to a maximum of 3000kg higher)ANDIn exceptional circumstances (fuel system failures) the above-mentioned max fuel imbalance values may be exceed without sig. affecting aircraft handling qualities. The a/c remains fully controllable in all phases of flight?
67
FUEL (SHARKY AIRCRAFT)Maximum imbalance allowedTAKE OFF:INNER when heavier tank fuel quantity is:FULL = 3000kg= 1450kg = OUTER: = IN FLIGHT and LANDING:INNER when heavier tank fuel quantity is:FULL = 4300kg= 2250kg = 1500kg = OUTER: = Special notes & exceptions =
68
Is there a difference in FUEL IMBALANCE figures between SHARK and NON SHARK aircraft?
Yes. The shark let aircraft have a much more restrictive imbalance range for TAKEOFF.The rest remain the same.
69
Minimum FUEL temperature for JET A1
-43
70
Maximum fuel temperature for Jet A1
54
71
Minimum fuel quantity for take off
1500kg and wing low level warning must not be displayed on ECAM
72
Are there restrictions on centre tank fuel for take off?
73
For fuel, which tank must be emptied first?
The centre tank, followed by the wing tanks.
74
Can fuel types be mixed?
Yes, various types of fuel can be mixed in all proportions and the freezing point varies based on non-linear laws.
This is FCOM guidance only, maybe not OMA.
75
HYDRAULIC What is the normal operating pressure?
3000 PSI +/- 200
76
Maximum brake temperature for take off?
300
77
Is the brake system designed to hold the aircraft in a stationary position with a high thrust setting?
78
Taxi with deflated tiresWhat are the two limitations?
79
Nose Wheel Steering Handwheels MAX:
Towing and pus back max:
Towbarless towing max:
Handhweels: 75
Towing and push: 95
Towbarless: 85
80
Inertial Reference System:
1) Demonstrated between: ?
2) If all ADIRUs have the same magnetic variation table:
FLIGHTS USING NAV MODE PROHIBITED BETWEEN:
a) ?
B) ?
3) If ONE ADIRU has a different magnetic variation table:
FLIGHTS USE NAV MOVE PROHIBITED BETWEEN:a) b)c)
Inertial Reference System:1) Demonstrated between: 73N and 73S2) If all ADIRUs have the same magnetic variation table:FLIGHTS USING NAV MODE PROHIBITED BETWEEN:a) North of 73 NB) South of 60s3) If ONE ADIRU has a different magnetic variation table:FLIGHTS USE NAV MOVE PROHIBITED BETWEEN:a) North of 60N, between 30 W and 160 W ANDb) North of 73 N andc) South of 55 S
81
When should EGPWS enhanced function be inhibited ?
(TERR PB to OFF, on the GPWS panel)
When the aircraft is less than 15nm from the airfield AND1) Operations to / from runways not in the EGPWS database2) For specific approach procedures, which have previously been identified as pot. producing false terrain alerts
82
When must the ISIS bug functions NOT be used?
If both PFDs are lost
83
Minimum O2 bottle pressure takes in account:
84
APU: Low Oil level ecamWhat is the implication?
If no leak, APU may be started and maint. action required within next 10hr of APU operation
85
APU starter cycles - limit?
86
Maximum APU N speed (as shown on ecam)
What N does the APU auto shut down?
ECAM: 107% (actual = 106%)
(APU auto shuts down at 107% N, that appears on ecam)
(This corresponds to an actual N speed of 106%)
87
Maximum APU EGT?
Max EGT = 675Max for start
(35,000ft) = 1120
88
Within the APU start envelope, within how many attempts is the APU 'guaranteed' to start?
3 conservative start attempts
89
On BATTERY, what is the limit for APU start?
25.000ft. (emer elec config)
90
APU:
Below WHICH altitude and temperature can we expect full APU electrical output?
Below 25,000ft and below ISA + 35
91
Below which altitude can we use the APU to start an engine?
20.000ft.
92
Up to which altitude we use the APU to supply both packs?
15,000ft
93
Below which altitude, can we use one pack from the APU?
22.500ft.
94
Can we use WAI with the APU bleed?
No.
95
ENGINE:
Take off and go around MAX EGT and TIME?
Max EGT: 950
5 min dual engine
10 min single engine
96
ENGINE
Maximum time for MCT
Max EGT
No time limit
915 Celsius
97
Engine start MAX EGT?
725
98
Engine OIL:
Max continuous temperature?
Can we accept a transient temperature and if yes, how long?
Max continuous: 140
Max transient: 155
15 minutes
99
Minimum ENGINE oil temperature for:Start:Take off:
Start: -40Take off: -10
100
Minimum ENGINE oil quantity:
OMB
9.5qts + 0.5 / hour
101
Max ENGINE n1 and n2
N1 = 104%
N2 = 105%
102
Engine start cycle restrictions:
- 4 consec cycles (max 2 mins each)
- 20 second pause between attempts
- after 4 attempts, 15 min cooling
- No running engagement of the starter, when N2 \> 20%
103
What are the 5 restrictions for Reduced Thrust Takeoff?
- Only permitted if airplane meets all app. perf requirements at planned take off weight,
- Thrust reduced must not exceed 25% of full rated TO thrust. To meet this required, the flex temp must not be higher than ISA +53 (T MAX FLEX)
- Assumed temp, must not be lower than flat rating temperature (or current OAT)
- Not allowed on contaminated runways
- Take off at reduced thrust is permitted for any inop item affecting perf, ONLY if the associated perf shortfall has been applied.
104
Reduced Thrust Takeoff: A319What are the 5 restrictions?
105
What is the T MAX FLEX for A319 and A320?
A319: ISA +60 (T MAX FLEX)
A320: ISA + 53
106
Autoland limits for A319 (2 eng)
20 / 20 / 5
107
Autoland limits for A319 (1 eng)
15 / 10 / 5
108
Autoland limits for A320 (SH) with and without roll out
30/ 20 / 10 without rollout
30 / 15 / 10 with rollout
109
Autoland limits for A320 (NO SH)
110
Maximum levels of contamination for take off
- 12.7mm of standing water (20 kt)
- 12.7mm slush (20kt)
- 25mm wet snow (25k)
- 100m dry snow (25kt)
111
%N for amber font
102%
112
%N for auto shutdown
107% or greater
113
EGT for amber font
within 33C of current max EGT
114
EGT for auto shutdown
computer calculated
115
%N for AVAIL
99.5% or 95% for \> 2 seconds
116
Min batt voltage to start
25.5V, if less charge for 20 mins
117
When can you press APU START?
5 seconds after MASTER SW has been depressed and no LOW OIL LEVEL advisory
118
Max START EGT?
1000C
119
Max operating EGT?
700C
120
When can you NOT check for the LOW OIL LEVEL during APU start?
Battery starts
121
After turning batteries to AUTO how much time do you have to start the APU?
30 minutes
122
After the batteries have been on for 35 minutes how much batt capacity is remaining?
\<25%
123
Approx how long until APU available after start is engaged?
~1 minute
124
After AVAIL extinguishes during shutdown, how long do you leave batteries on for?
2 minutes
125
Max service ceiling
FL390
126
Max altitude to start on batteries only
FL250
127
Max altitude to power one AC pack
FL200
128
Max altitude to power two AC packs
FL150
129
APU starter limit
After 3 consec starts attempts allow 60 minutes for cool down
130
Max alt to start engines
8,000 ft
131
Max alt for APU anti-ice
TRICK, you can't use APU for anti-ice
132
What is the cooling period for emergency shutdown?
None
133
NAV mode may be used in the terminal area, provided:
- GPS PRIMARY
or
- The appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed
or
- FMS navigation is cross-checked with NAVAID raw data
134
Runway Slope (mean)
+/-2%
135
Max crosswind for start
35kts
136
Max operating altitude with slats and/or flaps extended is
20,000ft
137
Minimum Height For Use Of Autopilot
Take off with SRS
100 ft AGL.
Note: Takeoff with SRS mode - An internal FMGS logic prevents the autopilot from engaging during the 5 seconds after liftoff.
138
Minimum Height For Use Of Autopilot
ILS approach when CAT 2 or CAT 3 is not displayed on the FMA
160 ft AGL
139
Minimum Height For Use Of Autopilot
Straight-in non-precision approach
Applicable Minimum
140
Maximum wind for passenger door operation
65kts
141
Takeoff and GA (TOGA and FLEX)
Thrust Setting/EGT Limits
Takeoff and GA (TOGA and FLEX)
319 and 320 / 321 / NEO
635 °C / 650 °C / 1,083°C
5 min (10 min engine failure.)
142
Maximum brake temperature for takeoff (brake fans (if installed) off)
300 C
143
RunwayAltitude
9,200ft
144
NominalRunwayWidth
45m(148ft)
145
VLE
280kts (M .67)
146
Oil Temperature (CEO)
Starting
-40 °C
Above Idle
-10°C
147
APU Starter
After three consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt.
148
Minimum Height For Use Of Autopilot
UseoftheAPorFDinOPENDESor DES mode is not permitted in approach, unless the FCU altitude is set at or above:
Highest of:
Minimums or 500 ft (A319/A320) Minimum or 900 ft (A321)
149
Fuel Temp
For JET A only, if TAT reaches -34C , monitor on FUEL SD page that fuel temperature remains higher than -36C
150
Reverser Limits
Maximum reverse should not be used below 70 kt. Idle reverse is permitted down to aircraft stop.
151
VLO (extension)
250kts (M .60)
152
Cabin Pressure
• Maxpositivedifferentialpressure
• Maxnegativedifferentialpressure
9. 0psi
- 1.0psi
153
Max Landing (320)
145,505lb
154
Max Landing (657-687)
171,519lb
155
MCT
Thrust Setting/EGT Limits
MCT
CEO / NEO
610 °C / 1,043°C
156
Max Taxi speed (A320CEO)
When the taxi weight is higher than 67,550lbs (76,000kg): Caution: Do not exceed a taxi speed of 20 kt during a turn.
157
Non-Precision Approaches with Engine-Out (319 and 657-668, 670, 671)
If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes:
FINAL APP
NAV V/S
NAV/FPA.
Only FD use is permitted.
158
Minimum Height For Use Of Autopilot
Circling Approach
100 feet below Applicable Circling Minimums
159
Max Landing (502-536)
137,788 lb
160
Minimum Oil Pressure (901-905)
65 PSI
161
Max Alt for landing gear extended
25,000ft
162
VLO (retraction)
220kts (M .54)
163
Fuel Imbalance, Inner tanks when one is full
TO / Flight&Landing
319 and 320s: (At TO / Flight and Landing)
1,102 / 3306
321:
882 / 2910
164
Minimum Height For Use Of Autopilot
All other phases
500 ft AGL (A319/A320) 900 ft AGL (A321)
165
Maximum Certified Altitude
FL398
166
Max speed for Windshield Wipers
230kts
167
STARTING (On Ground and Inflight)
Thrust Setting/EGT Limits
STARTING
CEO / NEO
635 °C / 1,083°C
168
Wingspans
Non-Sharklet
111feet,10inches
Sharklet
117feet,5inches
169
Maximum demonstrated crosswind
38kts (gust included)
170
Reduced Thrust Takeoff Limits
FLEX takeoff is not permitted on contaminated runways
171
Max crosswind with CAT II and III
Crosswind: 15 kts
172
Max tire speed
195 kts
173
APU With HP Ground Unit
The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System.
174
Starter Limitations
ALL CEO / NEO:
One Cycle = 1 / 2 consecutive start attempts
(CEO)Man start, 2 mins max start / 5 mins crack
For Ground Starts (auto or man), between cycle pause: 15 s / 35 s
After 3 cycles or 5 / 15 min continuous cranking (or cumulated NEO)
Cooling Period = 30 min / 15 min
Do not start, when
N2 is above 10% GND, 18 % FLT / 20%
175
Tailstrike Pitch Attitudes
L/G Struts Compressed
319 - 13.9 degrees
320 - 11.7 degrees
321 - 9.7 degrees
176
Max tailwind for:
Takeoff
Landing
Takeoff - 15kts
Landing - 10kts
177
APU Bleed use with Air Start Unit
The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System.
178
Packs use with the LP Air Conditioning Unit
The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time, to prevent any adverse effect on the Air Conditioning system.
179
What is the reduced usable fuel capacity of the Center Tank on 697 and 698 (Invicta-FRS system)
reduced usable capacity of up to 42.9 gallons
180
ELAC Functions
Normal Elevators
Normal Ailerons
Normal Pitch and Roll
Alternate Pitch
Direct Pitch and Roll
Abnormal Attitude
Aileron Droop
Autopilot orders
181
SEC Functions
Normal Roll
Alternate Pitch
Direct Pitch and Roll
Abnormal Attitude
Speed Brakes
182
FAC Functions
Rudder Limitations
Turn Coordination
Rudder Dampening
Rudder Trim
Aircraft envelope
Windshear
Low Energy Warning
183
NAV mode may be used in the terminal area, provided:
- GPS PRIMARY
or
- The appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed
or
- FMS navigation is cross-checked with NAVAID raw data
184
Runway Slope (mean)
+/-2%
185
Max crosswind for start
35kts
186
Max operating altitude with slats and/or flaps extended is
20,000ft
187
Minimum Height For Use Of Autopilot
Take off with SRS
100 ft AGL.
Note: Takeoff with SRS mode - An internal FMGS logic prevents the autopilot from engaging during the 5 seconds after liftoff.
188
Minimum Height For Use Of Autopilot
ILS approach when CAT 2 or CAT 3 is not displayed on the FMA
160 ft AGL
189
Minimum Height For Use Of Autopilot
Straight-in non-precision approach
Applicable Minimum
190
Maximum wind for passenger door operation
65kts
191
Takeoff and GA (TOGA and FLEX)
Thrust Setting/EGT Limits
Takeoff and GA (TOGA and FLEX)
319 and 320 / 321 / NEO
635 °C / 650 °C / 1,083°C
5 min (10 min engine failure.)
192
Maximum brake temperature for takeoff (brake fans (if installed) off)
300 C
193
RunwayAltitude
9,200ft
194
NominalRunwayWidth
45m(148ft)
195
VLE
280kts (M .67)
196
Oil Temperature (CEO)
Starting
-40 °C
Above Idle
-10°C
197
APU Starter
After three consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt.
198
Minimum Height For Use Of Autopilot
UseoftheAPorFDinOPENDESor DES mode is not permitted in approach, unless the FCU altitude is set at or above:
Highest of:
Minimums or 500 ft (A319/A320) Minimum or 900 ft (A321)
199
Fuel Temp
For JET A only, if TAT reaches -34C , monitor on FUEL SD page that fuel temperature remains higher than -36C
200
Reverser Limits
Maximum reverse should not be used below 70 kt. Idle reverse is permitted down to aircraft stop.
201
VLO (extension)
250kts (M .60)
202
Cabin Pressure
• Maxpositivedifferentialpressure
• Maxnegativedifferentialpressure
9. 0psi
- 1.0psi
203
Max Landing (320)
145,505lb
204
Max Landing (657-687)
171,519lb
205
MCT
Thrust Setting/EGT Limits
MCT
CEO / NEO
610 °C / 1,043°C
206
Max Taxi speed (A320CEO)
When the taxi weight is higher than 67,550lbs (76,000kg): Caution: Do not exceed a taxi speed of 20 kt during a turn.
207
Non-Precision Approaches with Engine-Out (319 and 657-668, 670, 671)
If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes:
FINAL APP
NAV V/S
NAV/FPA.
Only FD use is permitted.
208
Minimum Height For Use Of Autopilot
Circling Approach
100 feet below Applicable Circling Minimums
209
Max Landing (502-536)
137,788 lb
210
Minimum Oil Pressure (901-905)
65 PSI
211
Max Alt for landing gear extended
25,000ft
212
VLO (retraction)
220kts (M .54)
213
Fuel Imbalance, Inner tanks when one is full
TO / Flight&Landing
319 and 320s: (At TO / Flight and Landing)
1,102 / 3306
321:
882 / 2910
214
Minimum Height For Use Of Autopilot
All other phases
500 ft AGL (A319/A320) 900 ft AGL (A321)
215
Maximum Certified Altitude
FL398
216
Max speed for Windshield Wipers
230kts
217
STARTING (On Ground and Inflight)
Thrust Setting/EGT Limits
STARTING
CEO / NEO
635 °C / 1,083°C
218
Wingspans
Non-Sharklet
111feet,10inches
Sharklet
117feet,5inches
219
Maximum demonstrated crosswind
38kts (gust included)
220
Reduced Thrust Takeoff Limits
FLEX takeoff is not permitted on contaminated runways
221
Max crosswind with CAT II and III
Crosswind: 15 kts
222
Max tire speed
195 kts
223
APU With HP Ground Unit
The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System.
224
Starter Limitations
ALL CEO / NEO:
One Cycle = 1 / 2 consecutive start attempts
(CEO)Man start, 2 mins max start / 5 mins crack
For Ground Starts (auto or man), between cycle pause: 15 s / 35 s
After 3 cycles or 5 / 15 min continuous cranking (or cumulated NEO)
Cooling Period = 30 min / 15 min
Do not start, when
N2 is above 10% GND, 18 % FLT / 20%
225
Tailstrike Pitch Attitudes
L/G Struts Compressed
319 - 13.9 degrees
320 - 11.7 degrees
321 - 9.7 degrees
226
Max tailwind for:
Takeoff
Landing
Takeoff - 15kts
Landing - 10kts
227
APU Bleed use with Air Start Unit
The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System.
228
Packs use with the LP Air Conditioning Unit
The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time, to prevent any adverse effect on the Air Conditioning system.
229
What is the reduced usable fuel capacity of the Center Tank on 697 and 698 (Invicta-FRS system)
reduced usable capacity of up to 42.9 gallons
230
ELAC Functions
Normal Elevators
Normal Ailerons
Normal Pitch and Roll
Alternate Pitch
Direct Pitch and Roll
Abnormal Attitude
Aileron Droop
Autopilot orders
231
SEC Functions
Normal Roll
Alternate Pitch
Direct Pitch and Roll
Abnormal Attitude
Speed Brakes
232
FAC Functions
Rudder Limitations
Turn Coordination
Rudder Dampening
Rudder Trim
Aircraft envelope
Windshear
Low Energy Warning
