LIMITATIONS A319/320 Flashcards
1
Q
VOLOTEA Operative Weights 319
A
MTW: 66.400 kg MTOW*: 66.000 kg MLW*: 61.000 kg / 62.500 kg MZFW*: 57.000 kg / 58.500 kg Min Weight: 35.400 kg
2
Q
VOLOTEA Operative Weights 320
A
MTW: 77.400 kg / 78.400 kg MTOW*: 77.000 kg / 78.000 kg MLW*: 64.500 kg MZFW*: 61.000 kg Min Weight: 37.230 kg
3
Q
Vmo/Mmo
A
350 KIAS (<24.000´) / 0.82
4
Q
VMCL / VMCA- / VMCG- (319)
A
111kts* / 110kts-* / 108kts-*(RWY 35M:+1.5, 30M:+2.5)
5
Q
VMCL / VMCA- / VMCG- (320)
A
113kts* / 112kts-* / 112kts-*(RWY 35M:+1.5, 30M:+2.5)
6
Q
Max Speeds/ALT Flaps/Slats
A
1 -> 230 1+F -> 215 2 -> 200 3 -> 185 FULL -> 177 Max ALT -> 20.000 ft
7
Q
Max Speeds Landing Gear Extended
A
VLE - Extended -> 280 / M0.67
VLO - Extension -> 250 / M0.60
VLO - Retraction -> 220 / M0.54
8
Q
Max Spd Cockpit Window Open
A
200 kts
9
Q
Max Tire Speed
A
195 kts
10
Q
Max Wiper Operating Speed
A
230 kts
11
Q
Severe Turb Speed
A
> FL200/330: 275 KIAS/ .76 M
FL200 and below : 250 KIAS
12
Q
Max Pressure Altitude /
For Take-Off and Landing
A
- 800 ft
- 2000* / 9200 ft*
13
Q
Max Differential Pressure /
Max Safety Relief
A
- 1.0/9.0psi
8. 6 psi
14
Q
Maneuvering Load Limits /
Flaps/Slats extended
A
- 1.0/+2.5g
0. 0/+2.0g
15
Q
Temperature Limits TO/LDG
A
-40ºC*/+55ºC
Reducing to -52º/+38 ºC at 9200 ft
16
Q
Temperature Limits FL398
A
-70ºC/-29ºC
~ Linearly from 0 ft
17
Q
Max Runway Slope /
Min Runway Width
A
+/-2.0%
30m/ 45m (320)
18
Q
Max Cross-wind DRY Runway
A
38 kts (26kt <45m)
19
Q
Max Cross-wind Good - Medium - Poor
Rwy<45m
A
38 -(29)- 25 -(20)- 15
20 -(10)- 10 -(10)- N/A
20
Q
Max Tailwind Component
A
10 kts (15kts)*
21
Q
Max Wind Pax Door Operation /
Max Wind Cargo Doors
A
65 kts 40 kts (50 kts) 50 kts if the nose into the wind or cargo doors on the leeward side
22
Q
Required Fire Fighting Category
A
RFF 6
ALTN: RFF4
RFF 4/5 may be accepted in certain conditions ref OM-A.8.1.2.G
23
Q
Max Brake Temperature T/O
A
300º C
150º C (Brake fan ON)
24
Q
ENG LIMITS TO/GA
A
Time Limit (Max) -> 5 min (10min OEI) Max TGT -> 950 OIL PRESS (Min/Max) -> 13 – 90 (~N2) OIL TEMP (Min/Max) -> -10 / 155 Max N1 / N2 -> 104 / 105
25
ENG LIMITS MCT
```
Time Limit (Max) -> NONE
Max TGT -> 915
OIL PRESS (Min/Max) -> 13 – 90 (~N2)
OIL TEMP (Min/Max) -> 140
Max N1 / N2 -> 104 / 105
```
26
ENG LIMITS STARTING/ TRANSIENT
```
Time Limit (Max) -> N/A
Max TGT -> 725
OIL PRESS (Min/Max) -> -
OIL TEMP (Min/Max) -> -40 / 155
Max N1 / N2 -> N/A
```
27
ENG Starter Duty Cycle
: 1 Standard automatic start cycle, includes up to 3 attempts.
: For ground starts, a 20 sec pause is required between cycles.
: 15 minutes cooling time, subsequent to 4 failed cycles.
: The starter must not be run when N2 is above 20%.
28
Fuel Temp Limits (JET A1/JP8/No3)*
-43 ºC / + 54 ºC
29
Minimum Fuel QTY for T/O
1.500 kg
30
LO LVL Warning ECAM
<750 kg 1 wingtank
31
Advisory imbalance (phs 2/6)
>1500 kg difference
32
Total Fuel
18.729 kg* (Fuel density 0.785)
Outer Tanks : 691 kg x2
Inner Tanks : 5.435 kg x2*
Center Tank : 6.476 kg
33
Check OXYGEN PRESS tables*
< 800 PSI 2CM,
< 1100 PSI 2CM+OBS,
< 1400 PSI 2CM+2OBS
34
DO NOT PULL CB
SFCC, ECU/EEC, EIU
35
Max VOLOTEA Taxi Speed
30 kts / 50 kts on the RWY
| With TOM >76T -> 20 kts
36
Min Taxi Strip for 180º Turn
20.5/ 22.8 m
37
Max NWS angle
- Taxi: 75º (30º tires deflated)
- Towbarless: 85º
- Towbar: 95º
38
Wingspan
34.1 m
39
Lenght
33.84 / 37.57 m
40
Wheelbase
7,59 m
41
Tailspan
12.45 m
42
Height
11,75 m
43
APU Limitations
- NO APU BLEED together with HP ASU
- Use of APU Bleed air for Wing Anti-ice is NOT permitted
- During refueling/defuel allowed to start or shutdown, but not after start failure or auto shutdown.
- Starting 3 attempts, then 60 min.
- Max EGT running : 675 ºC*
- Max Rotor (N) Speed : 107%
- Max EGT for start
44
Autoland Limitations
- Headwind 20 kts/ 30kts (320)
- Crosswind 20 kts
- Tailwind 10 kts
OEI A319: 15/ 10/ 10 - 5kts with CONF3 or ELEV>5750ft
- A/THR must be used in selected or managed speed
- At least 1 AP in APPR mode for CAT2 and CAT3 SINGLE, both for CAT3 DUAL
- OEI CAT2/CAT3 SINGLE, if procedures completed before 1000 ft.
- Depending on situation, provided runway approved for automatic ldg, allowed up to 69 t.*
- Automatic roll-out using 1 thrust reverser, max winds 15/10/10(5)
- Elevation < 9200 ft MSL*
- Not allowed < -1000 ft pressure altitude
- Glide Slope 2.5º - 3.15º
- Runway Width minimum 45m
45
Autopilot Limitations
- > 100 ft AGL at T/O, and at least 5 sec after lift-off; or after manual Go-Around
- > 160 ft AGL with ILS CAT1 on FMA
- > 250 ft AGL in approach with FINAL APP, V/S or FPA mode
- > 500 ft AGL in Circling approach and in all other phases.
- With OEI, AP not permitted to perform NPA in: FINAL APP, NAV V/S, NAV/FPA. Only FD.
46
Instrument Altimeter Tolerance
PFD 1 and 2 -> 20 ft
PFDs and ISIS -> 100 ft
PFDs and Mech.SBY -> 300 ft
47
RVSM Altimeter Tolerance
PFD 1 or 2 -> 25 ft
PFDs and Apt ELEV -> 75 ft
In FLT PFD 1 and 2 -> 130 ft
General RVSM Requirement: Minimum of 2 Altimeters 200 ft
48
Center of Gravity Limits
12-40 % / 13-45 % (320)
49
Icing Conditions
OAT/TAT < 10 oC and Visible Moisture (clouds, fog <1sm, rain, snow, etc) or contamination on ramps, taxiways or runways.
50
Severe Ice Accretion
when accumulation on the airframe aprox > 5mm
51
Max Contamination
Runway is considered contaminated > 3 mm
- Dry Snow: 100 mm
- Wet Snow: 30mm
- Slush/Water: 12,7 mm
52
Maximum differential pressure to open ram air inlet
1 PSI
53
Max continuous load per generator
100% (90KVA)
54
Max TR load
200A
55
CAT II ILS min DH and autopilot disconnect height
Min DH = 100 feet AGL (RA)
| Min Autopilot disconnect height = 80 feet AGL
56
Taxi with deflated tires speeds for one, two deflated same gear and NWS limit
1 = 7 kts
2 = 3 kts
NWS angle limit = 30 degrees
57
Lo LVL OIL ECAM mesare for APU
APU can be started and run for 10 hours, maintenance action us required within this period
58
Max alt for APU start on batteries only
25.000 feet
59
APU one pack alt
22.500 feet
60
APU two pack alt
15.000 feet
61
Min engine oil qty
9.5 + 0.5 hour
62
FLEX limitations
Not reduced by more than 25% of max THR. Max FLEX = ISA+55, must not be lower than actual OAT.
Do not use one contaminated runways.
63
APU altitude limitations for
ground mode,
starts on bats only and
100% gen load
Ground mode = 14500ft
Starts on bats only = 25000ft
100% gen load = 30000ft
64
Max APU altitude
41000ft
65
Engine. No running engagement of starter
20% N1
66
Max taxi speed
30kts on taxiways
50kts on runways
20kts weight above 76T and in turns
67
Brakes temp limits requiring maintenance
- Tem on same gear differ by more than 150º and one is more than 600º or less than 60º
- The two gears differ by more than 200º
- Fuse plug melted
- Brake above 900º
68
Max airflow from ground carts
1.2 kg/s
69
Air from Packs and LP ground cart simultaneously
Forbidden to avoid chattering of non return valves
70
APU bleed with HP ground air
Do NOT use HP ground air with APU Bleed to avoid bleed air system damage
71
MAX cabin alt selection
14000ft
72
Cabin ALT warning
9550ft
73
MAX normal cabin ALT
8000ft
74
MAX fuel imbalance at takeoff for inner tanks (outer tanks balanced)
500kg
75
MAX fuel imbalance at takeoff for outer tanks (inner tanks balanced)
370kg
76
MAX fuel imbalance in flight and landing for outer tanks (inner tanks balanced)
690kg
77
ENG Vibration during flight
?
78
ENG Vibration during start
?
79
Hydraulics normal pressure
3000PSI +/- 200PSI
