Limitations Flashcards
1
Q
Flight Maneuvering Load Acceleration (Clean)
A
-1G to +2.5G
2
Q
Flight Maneuvering Load Acceleration (Slats+Flaps/Slats Only)
A
0G to 2G
3
Q
Environmental Envelope (Maximum Operating Altitude)
A
Slats/flaps retracted: 39 800 ft
Slats and/or flaps extended: 20 000 ft
Takeoff and Landing: 9 200 ft
4
Q
Environmental Envelope (Minimum Temperature)
A
- 70 ºC
5
Q
Environmental Envelope (Maximum Temperature)
A
+55 ºC
6
Q
Runway Slope
A
+/- 2%
7
Q
Runway Altitude
A
9200 ft
8
Q
Nominal/Minimum Runway Width
A
Nominal: 45 m
Min: 30 m
9
Q
Max. Crosswing Takeoff/Landing
A
38 knots demonstrated (gust included)
SFO/FO/SO<500h:
15 knots
10 knots if Ceiling < MDA+200/ RVR +400m
10
Q
Max. Tailwind Takeoff/Landing
A
10 knots
SFO/FO/SO<500h:
5 knots (dry rwy)
11
Q
Max. Wind Pax Door Operation
A
65 knots
12
Q
Max. Wind Cargo Door Opening
A
40 knots (50knots if aircraft nose is into the wind or if the door is on the leeward side)
13
Q
Max Operating Speed (VMO)
A
350 knots
14
Q
Max Operating Mach Number (MMO)
A
Mach 0.82
15
Q
Severe Turbulence Recommended Speed Below FL200
A
250 knots
16
Q
Severe Turbulence Recommended Speed At or Above FL200
A
275 knots/ Mach.76
17
Q
Flaps/Slats Configurations and Speeds ( Conf 1)
A
Slats 18º, Flaps 0º, ECAM 1, MAXIMUM SPEED 230 knots
18
Q
Flaps/Slats Configurations and Speeds ( Conf 1+F)
A
Slats 18º, Flaps 10º, ECAM 1+F, MAXIMUM SPEED 215 knots
19
Q
Flaps/Slats Configurations and Speeds ( Conf 2)
A
Slats 22º, Flaps 15º, ECAM 2, MAXIMUM SPEED 200 knots
20
Q
Flaps/Slats Configurations and Speeds ( Conf 3)
A
Slats 22º, Flaps 20º, ECAM 3, MAXIMUM SPEED 185 knots
21
Q
Flaps/Slats Configurations and Speeds ( Conf FULL)
A
Slats 27º, Flaps 40º(319)/35º(320), ECAM FULL, MAXIMUM SPEED 177 knots
22
Q
Max Altitude Flaps/Slats Extended
A
20 000 feet
23
Q
VLE - Max Speed Gear Extended
A
280 knots / M.67
24
Q
VLOe - Max Speed Gear may be extended
A
250 knots
25
VLOr - Max Speed Gear may be retracted
220 knots
26
Max speeds L/G doors not closed
250 knots
27
Max Altitude L/G may be extended
25 000 feet
28
Max Tire Speed
195 knots
29
Max Speed Windshield Wipers in use
230 knots
30
Max Speed Cockpit Window Open
200 knots
31
Max Altitude With Cockpit window/windshield cracked
FL230
32
Max Taxi speed (GW \> 76T)
20 knots in a turn
33
Max Taxi Speed with 1 tire per gear deflated
Turning: 7 knots
| (Max 3 tires)
34
Max Taxi Speed with 2 deflated tires on the same main gear
3 knots + Max 30º NWS
35
Max Taxi Speed with ECAM: "WHELL N/W STRG FAULT"
10 knots
36
Cabin Pressure Maximum Positive Diff. Press.
9 PSI
37
Cabin Pressure Maximum Negative Diff. Press.
-1 PSI
38
Cabin Pressure Maximum Positive Diff. Press. (Safety Relief Valve)
+8.6 PSI
39
Elec: Max Load per Generator
100 % (90 kVA)
40
Elec: Max Continuous Load per TRU
200A
41
Minimum Height to engage AP after TO with SRS mode
100 feet AGL (+5 seconds after liftoff)
42
Minimum Height AP use on ILS CAT 1
160 feet AGL
43
Maximum Fuel Imbalance allowed with full tanks
1500 kg
44
JET A-1 Freezing Temperature
-47ºC
45
JET A-1 Minimum Temperature
-43ºC
46
JET A-1 Maximum Temperature
+54ºC
47
Minimum Fuel for Takeoff
1500 kg
| (+ no "WING TK LO LVL" ECAM)
48
Normal Operating Hydraulic Pressure
3000 PSI +/- 200
RAT 2500 PSI
49
Max Takeoff brake temperature with Brake fans ON
150ºC
50
Max Takeoff brake temperature with Brake fans OFF
300ºC
51
APU "LOW OIL LEVEL"
another 10 hours of operation
52
APU Starter (waiting time after 3 attempts)
60 minutes
53
APU Maximum Rotor Speed
107%
54
APU Start Up and Electrical Power use
Max FL 390
55
APU Battery Restart limit up to (Elec Emerg)
FL 250
56
APU Max altitude to assist engine start
20 000 feet
57
APU Max altitude for air conditioning and pressurization with 2 packs
FL150
58
TOGA
5 minutes (10 if OEI)
59
TOGA EGT LIMIT
950ºC
60
MCT EGT LIMIT
915ºC
61
Engine: OIL Minimum Starting Temperature
-40ºC
62
Engine: OIL Minimum Takeoff Temperature
-10ºC
63
Minimum Engine Oil Quantity
9,5 Qts + 0,5 Qts/h + 15 minutes
64
Engine Start pause between start cycles
20 seconds
1 cycle = 3 attempts
65
Engine Start cooling after 4 attempts
15 minutes
66
IRS
73ºN - 60º S
67
Vmca
110 knots IAS at Sea Level, decreasing with increase in altitude
68
Vmcg
111 knots IAS at sea level with CONF 1+F, decreasing with increase in altitude and flap setting
69
MAX time without Air Cond Supply with PAX onboard
20 minutes
70
Max. APU EGT for START
1090°C below 35 000 ft
1120 ºC at or above 35 000 ft
or (MSN):
900°C below 25 000 ft
982 ºC at or above 25 000 ft
71
Max EGT for Engine start
635°C
72
Maximum taxi speed to backtrack
50 knots
73
ROLLING TAKEOFF MIN. RWY LENGTH
2300 m
74
MTOW (319/320)
Voe fleet:
66 000 kg/ 71 500 kg
75
MLW (319/320)
61 000 kg or 62 500 kg/ 66 000 kg (NNZ, MBK, NOL: 64500KG)
76
Maximum nosewheel travel during towing
85 º (Mechanical stop at 95º)
77
Maximum safety relief differential pressure
8.6 PSI
78
Maximum negative differential pressure
-1 PSI
79
RNP Accuracy with GPS PRIMARY
With AP ON in NAV:
* En Route: 1 NM
* In Terminal Area: 0.5 NM
* In Approach: 0.3 NM
With AP OFF and FD ON in NAV:
* En Route: 1 NM
* In Terminal Area: 0.51 NM
* In Approach: 0.3 NM
With AP OFF and FD OFF:
* En Route: 1.1 NM
* In Terminal Area: 0.51 NM
* Not Authorized
80
*_NON PRECISION APPROACHES WITH OEI_*
If OEI, use of AP is not allowed for NPA in the following flight modes:
‐ FINAL APP
‐ NAV/VS
‐ NAV/FPA.
Note: The use of FD in NAV mode remains authorized.
81
*_SPEED BRAKES LIMITATION_*
For approach, the use of speed brakes at or below 240 kt is **not permitted if**:
‐ GWCG is above 35 % or
‐ In overweight landing conditions.
82
*_AUTOLAND_*
Autoland has been demonstrated:
‐ With **CAT II** and **CAT III** ILS beam, with ILS slope angle inside a range of **-2.5 ° and -3.15 °**
‐ For an airport that has an elevation between -1 000 ft and 9 200 ft.
Performance of ROLL OUT mode has been demonstrated on dry and wet runways.
**One** autopilot at least must be engaged in APPR mode and **CAT 2** or CAT 3 SINGLE or CAT 3 DUAL capability must be displayed on **FMA**.
83
Minimum Height AP use on FINAL APP, V/S or FPA
250 ft AGL
84
Minimum Height AP use on CIRCLING
500 ft AGL
85
Minimum Height AP use after manual GO-Around
100 ft AGL
86
Use of AP or FD in OPEN DES or DES mode
The use of AP or FD in OPEN DES or DES mode is not permitted if FCU altitude is set below MDA/MDH or 500 ft AGL, whichever is higher.
87
Minimum Height AP use on CAT II Approach (No Autoland)
80 ft AGL
88
Minimum Decision height CAT II APPROACH AUTOLAND
100 ft AGL
## Footnote
One autopilot at least must be engaged in APPR mode and CAT 2 or CAT 3 SINGLE or CAT 3 DUAL capability must be displayed on FMA
89
MAX WIND - CAT II OR CAT III APPROACH OR AUTOMATIC LANDING AND AUTOMATIC ROLLOUT
With all engines operative (AEO):
CONF FULL with airport elevation at or below 5 750 ft:
* *Headwind: 20 kt (30 kt for A320)**
* *Tailwind: 10 kt**
**Crosswind: 20 kt**
With one engine inoperative (OEI):
CONF FULL with airport elevation at or below 5 750 ft:
**Headwind: 15 kt**
**Tailwind: 10 kt**
**Crosswind: 10 kt**
90
IRS accuracy compliance ( max light time)
16 h
91
IRS Ground Alignment latitude limitations
* If all ADIRUs have the same magnetic variation table:
Flights using the NAV mode are prohibited:
‐ North of 73 ° North, and
‐ South of 60 ° South.
* If one ADIRU has a different magnetic variation table:
Flights using the NAV mode are prohibited:
‐ North of 60 ° North, between 30 ° West and 160 ° West, and
‐ North of 73 ° North, and
‐ South of 55 ° South.
92
Max APU EGT
742 ºC/675ºC (MSN)
93
MAX EGT FOR ENGINE START
725 ºC
94
ENG MAX ROTOR SPEEDS (N1/N2)
N1: 104% / N2: 105%
95
OIL MINIMUM PRESSURE
13 PSI
96
OIL MAXIMUM TEMPERATURE
140ºC for continuous operations
97
Maximum/Min FLEX TEMP
The flex temperature must not be:
‐ Higher than **ISA + 70**
‐ Lower than the flat rating temperature or actual OAT.
98
Engine anti-ice must be ON
During all ground and flight operations when icing conditions exist or are anticipated, except during **climb and cruise** when the temperature is below **-40 °C SAT**.
The engine anti-ice must be **ON** prior to and during **descent** in icing conditions, **including** temperatures below **-40 °C SAT**.
99
Air Cond: Max time without AC
With pax on board, it is not recommended to exceed **20** min without air conditioning supply.
100
APU BLEED USE WITH HP 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.
101
Avionics Ventilation: Time limit without electrical power depending on OAT
49ºC55ºC - 2 h
55ºC60ºC - 1 h
60ºC64ºC - 0.5 h
102
PACKS USE WITH 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.
103
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.
104
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.
105
APU Max altitude for air conditioning and pressurization with 1 pack
20 000 feet
106
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.
107
RAIN REPELLENT
The flight crew should only use the rain repellent in the case of moderate to heavy rain
108
TAXI WITH DEFLATED OR DAMAGED TIRES
-Maximum taxi speed during turn: 7 kt (max one tire per gear)
‐ If two tires are deflated on the same main gear (maximum one main gear): Maximum taxi speed: 3 kt
‐ Maximum NWS angle: 30 °
In addition, if tire damage is suspected, the flight crew must ask for an aircraft inspection prior to vacate the runway or taxi. If the ground crew suspects that a tire burst may damage the landing gear, maintenance action is due.
109
Flights over water limitation
In order to comply with CAT.IDE.A.285 and since Volotea does not carry life rafts on board, the maximum distance to an adequate aerodrome will be limited to **1h** flight time in still air conditions or **400** nm, taking the lower one.
110
Navigation limitations due to SSR navigation performance requirements
All A320F fleet has anticolision system (ACAS)
ACAS II type, Mode S EHS (Enhanced Surveillance) ATC Transponders, and ADS-B system. Refer to FCOM DSC-34-SURV
111
Definition of Wet runway
A runway whose surface is covered by any visible dampness or water up to and including 3 mm deep within the area intended to be used (OM - B)
112
EFB Battery level
1st flight: 50% (90% mount inop)
consecutive flights: 25% (40% mount inop)
During descent the charging must be stopped and the charger and cables stowed before passing FL 100
113
A320F MAXIMUM DEVIATION FROM THE ILS GLIDE PATH AND/OR LOCALISER
In accordance with FCOM PRO-NOR-SRP-01-70 the warning of excessive beam deviation is a flashing of the LOC and G/S scales on the PFD and ND ROSE ILS. It shall occur whenever:
* G/S deviation is greater than 1 dot (above 100 ft RA).
* LOC deviation is greater than 1/4 dot(above 15 ft RA).
114
REQUIRED VISUAL REFERENCE FOR CAT II APPROACH
The visual references must contain:
• a segment of at least **3 consecutive lights** being:
• the centre of the approach lights, or
• touchdown zone lights, or
• runway centre line lights, or
• runway edge lights, or
• a combination of these
• a lateral element of the ground pattern:
• an approach lighting crossbar, or
• the landing threshold, or
• a barrette of the touchdown zone lighting
115
Max vertical speed during last 2000ft of climb/descent
1500 ft/min (FCOM)
116
What brake temp. Requires maintenance action?
-Temp difference between two brakes \> 150°C; + 1 brake over 600°C / below 60°C -ONE BRAKE EXCEEDS 900°C
117
G or Y HYD RESERVOIR value turns Amber?
When below LOW LEVEL WARNING: 3.5 L
118
Required equipment for RVSM
-1 XPDR -1 AP -1 FCU CHANNEL -1 FWC -2 ADRs -2 DMCs -2 PFDs
119
Max EXTRA FUEL (due weather)
805kg - 320 775kg - 319 ( Sufficient to 20' holding at 1500')
120
When is OETD not allowed?
- cold engine (\>6h) -Icing conditions - LVO - Slippery or contaminated rwy -self maneuvering to left - failure affecting HYD, ELEC; APU GEN; STEERING/BRAKING CAPABILITY; BLEED
121
When is OETD not allowed?
- cold engine (\>6h) -Icing conditions - LVO - Slippery or contaminated rwy -self maneuvering to left - failure affecting HYD, ELEC; APU GEN; STEERING/BRAKING CAPABILITY; BLEED
122
Max. Taxi speed on contaminated taxiways
10 knots
