Limitations Flashcards
(103 cards)
0
Q
Flight Maneuvering Load Acceleration Limits
Other configurations
A
0 g to +2 g
1
Q
Flight Maneuvering Load Acceleration Limits
Clean configuration
A
-1 g to +2.5 g
2
Q
Weight Limitations
Maximum taxi weight (-200/-300)
A
233 900 kg
3
Q
Weight Limitations
Maximum takeoff weight (-200)
30-03-2014 t/m 25-10-2014
A
PH-AOA t/m PH-AOC: 222.000 kg
PH-AOD t/m PH-AON: 230.000 kg
4
Q
Weight Limitations
Maximum landing weight (-200)
A
182 000 kg
5
Q
Weight Limitations
Maximum zero fuel weight (-200)
A
170 000 kg
6
Q
Weight Limitations
Minimum weight (-200)
A
116 000 kg
7
Q
Weight Limitations
Maximum takeoff weight (-300)
A
233 000 kg
8
Q
Weight Limitations
Maximum landing weight (-300)
A
187 000 kg
9
Q
Weight Limitations
Maximum zero fuel weight (-300)
A
175 000 kg
10
Q
Weight Limitations
Minimum weight (-300)
A
121 000 kg
11
Q
Environmental Envelope
Minimum TAT (-200/-300)
A
-53 ‘C
12
Q
Airport Operations and Wind Limitations
Runway slope (mean)
A
+/-2 %
13
Q
Airport Operations and Wind Limitations
Runway altitude
A
12 500 ft
14
Q
Airport Operations and Wind Limitations
Maximum demonstrated crosswind
A
40 kt
15
Q
Airport Operations and Wind Limitations
Maximum tailwind for takeoff
A
15 kt
16
Q
Airport Operations and Wind Limitations
Maximum tailwind for landing at or below 11 000 ft
A
15 kt
17
Q
Airport Operations and Wind Limitations
Maximum tailwind for landing above 11 000 ft
A
10 kt
18
Q
Airport Operations and Wind Limitations
Maximum wind for passenger door operation
A
40 kt (or 50, if the aircraft nose is oriented into the wind)
19
Q
Airport Operations and Wind Limitations
Maximum wind for cargo door operation
A
40 kt (or 50, if the aircraft nose is oriented into the wind, or the cargo door is on the leeward side)
20
Q
Airport Operations and Wind Limitations
The passenger/cargo door must be closed before the wind speed exceeds:
A
60 kt.
21
Q
Airport Operations and Wind Limitations
Maximum Crosswind for Takeoff/Landing (Gust included) - Damp
Wet (3mm or less water)
A
40 kt
22
Q
Airport Operations and Wind Limitations
Maximum Crosswind for Takeoff/Landing (Gust included) -
3mm or less of slush, dry snow, wet snow;
Frost
Compacted Snow (OAT at or below -15’C)
A
27 kt
23
Q
Airport Operations and Wind Limitations
Maximum Crosswind for Takeoff/Landing (Gust included) - Dry Snow - between 3 mm and 100 mm Wet Snow - between 3 mm and 30 mm Compacted Snow (OAT above -15'C) Slippery when wet
A
20 kt
24
Airport Operations and Wind Limitations
Maximum Crosswind for Takeoff/Landing (Gust included) -
Water - between 3 mm and 12.7 mm
Slush - between 3 mm and 12.7 mm
20 kt
25
Airport Operations and Wind Limitations
Maximum Crosswind for Takeoff/Landing (Gust included) -
Ice (cold & dry)
15 kt
26
Maximum Operating Speed VMO/MMO
VMO/MMO
330 kt / M.86
27
Minimum Control Speeds
VMCL (-200)
118 kt
28
Minimum Control Speeds
VMCL (-300)
123 kt
29
Gear Down Speeds
Maximum speed with landing gear extended (VLE)
250 kt/0.55
30
Gear Down Speeds
Maximum speed at which the landing gear may be operated (extension and retraction) (VLO)
250 kt/0.55
31
Gear Down Speeds
Maximum speed for gravity extension (VLE/VLO)
200 kt
32
Gear Down Speeds
Maximum altitude at which the landing gear may be extended
21 000 ft
33
Maximum Tire Speed
Ground speed
204 kt
34
Windshield Wipers In Use
Maximum speed
230 kt
35
Cockpit Window Open
Maximum speed
230 kt
36
Speedbrakes
No limitation.
37
Ram Air Inlet
Opens only if differential pressure is lower than:
1 PSI
38
Cabin Pressure
Maximum positive differential pressure
9.25 PSI
39
Cabin Pressure
Maximum negative differential pressure
-0.73 PSI
40
Cabin Pressure
Safety relief valve setting
8.85 PSI / -0.26 PSI
41
Cabin Pressure
Maximum normal cabin altitude
8000 ft
42
Cabin Pressure
Minimum/Maximum cabin altitude selection
-2000 ft / +14000 ft
43
Auto Pilot Function
Minimum weight for use of autoland
123 000 kg
44
Cabin Pressure
Outflow valve closure (altitude)
15000 ft
45
Auto Pilot Function
Minimum height for use of the autopilot on takeoff with SRS mode
100 ft AGL
46
Auto Pilot Function
Minimum height for use of the autopilot in:
Straight-in non precision approach
Applicable minimum
47
Auto Pilot Function
Minimum height for use of the autopilot in:
Straight-in LNAV/VNAV approach
Applicable minimum
48
Auto Pilot Function
Minimum height for use of the autopilot in:
Circling approach
Applicable circling minimum -100 ft
49
Auto Pilot Function
Minimum height for use of the autopilot in:
ILS approach when CAT2 or CAT3 is not displayed on the FMA
160 ft AGL
50
Auto Pilot Function
Minimum height for use of the autopilot in:
Go-around (AP or FD engagement)
100 ft AGL
51
Auto Pilot Function
Minimum height for use of the autopilot in:
All other phases
500 ft AGL
52
Use Of Nav And Final App Modes For Non-Precision Approach
NAV, or NAV and FINAL APP mode may be used for:
VOR, VOR/DME, NDB, NDB/DME or RNAV (including GPS) approach, but not for ILS, LOC, LOC-BC, LDA or SDF.
53
Use Of Nav And Final App Modes For Non-Precision Approach
FINAL APP mode guidance capability with GPS PRIMARY has been demonstrated down to:
MDH/DH (barometric) 250 ft.
54
Category II
Minimum decision height
100 ft AGL
55
Category III Fail Passive
Minimum decision height
50 ft
56
Category III Fail Operational
Alert height
Minimum RVR
200 ft
| 75 m
57
Maximum Wind Conditions For CAT II/CAT III Automatic Approach, or Automatic Landing and Automatic Rollout
Headwind
Tailwind
Crosswind
35 kt
10 kt
20 kt
58
Engine Out
CAT II and CAT III fail passive autoland are only approved:
In Configuration 3;
| If engine out procedures are completed before reaching 1000 ft in approach.
59
Threshold Crossing Height
Minimum threshold crossing height (TCH)
38 ft
If the TCH is below the minimum TCH, the ILS glideslope is too low to give sufficient main gear clearance at the runway threshold. It is allowed to fly the ILS, however at 200 ft HAT a gentle transition must be made from the ILS glideslope to a visual glideslope.
60
Automatic Landing
Depending on the situation (e.g. emergency or other) and provided that the runway is approved for automatic landing, the flight crew can decide to perform an autoland up to:
229 000 kg
61
Electronic Outlets
It is forbidden to use the electronic outlets during
Takeoff and landing
62
In Seat Power Supply System (ISPSS)
Maximum outlet load (except for momentary exceedance)
100 Watt
63
In Seat Power Supply System (ISPSS)
Maximum momentary outlet current
10 Ampere
64
Flaps And Slats
Maximum operating altitude with flaps and/or slats extended
20 000 ft
66
Maximum Allowed Wing Fuel Imbalance
Maximum allowed wing fuel imbalance in inner tanks at takeoff, landing and in flight (outer balanced)?
Tank content (heavier tank) - Authorized asymmetry
FULL - 2900 kg
17000 kg - 4800 kg
7500 kg - 7500 kg
66
Fuel Temperature
Maximum fuel temperature JET A, JET A1, JP 5, JP 8, N3 JET, RT, and TS-1
+55'C
67
Maximum Allowed Wing Fuel Imbalance
Maximum allowed wing fuel imbalance in outer tanks at takeoff, landing and in flight (inner balanced)?
Tank content (heavier tank) - Authorized asymmetry
FULL - 1480 kg
2400 kg - 1580 kg
1730 kg - 1730 kg
68
Fuel Temperature
Maximum fuel temperature JP 4, JET B
+49'C
69
Fuel Temperature
Fuel freezing point JET A
-40'C
70
Fuel Temperature
Fuel freezing point JET A1
-47'C
71
Fuel Management
In case of a trim tank forward transfer pump failure, do not select the trim tank forward when the pitch attitude is above ... to avoid inadvertent fuel aft transfer.
3 degrees
72
Minimum Fuel Quantity For Takeoff
5200 kg;
| WING TK LO LVL warning must not be displayed on ECAM for takeoff.
73
Fuel Mixability
If a freeze point measurement is not possible, how do we determine the fuel freezing point of a mixture of fuels?
Assuming that fuel type A has a higher freezing point than fuel type B:
- If the mixture of fuel type A and type B contains less than 10% of fuel type A, the freezing point of the mixture can be considered as that of fuel type B.
- If the mixture of fuel type A and type B contains more than 10% of fuel type A, the freezing point of the mixture can be considered as that of fuel type A.
74
Hydraulic
Normal operating pressure
3000 PSI +/-200
75
Brakes
Maximum brake temperature for takeoff
300'C
76
Nosewheel Steering (NWS)
Nosewheel steering angle limit
72 degrees
77
Nosewheel Steering (NWS)
Nosewheel steering angle limit for towing and pushback
65 degrees (markings on the nose landing gear door)
78
Inertial Reference System
The ground alignment of the IRS has been demonstrated to be acceptable between ...
82'N and 82'S.
79
Inertial Reference System
If all ADIRUs have the same magnetic variation table; in MAGNETIC reference, flight using the NAV mode are prohibited:
- North of 73'N between 90'W and 120'W;
- North of 82'N;
- South of 60'S.
(When flying at latitudes beyond these limits, TRUE reference must be selected)
80
Enhanced Ground Proximity Warning System (EGPWS)
The EGPWS enhanced functions should be inhibited when (TERR push button OFF, on the GPWS panel) when the aircraft is less than 15 nm from the airfield:
- For operations to/from runways not incorporated in the EGPWS database;
- For specific approach procedures, which have been previously been identified as potentially producing false terrain alerts.
81
Cockpit Fixed Oxygen System
Minimum flight crew oxygen must be checked when below ...
1000 PSI
82
APU - General
Maximum EGT
Maximum EGT for start
650'C
| 1250'C
83
APU - General
Maximum N (rotor speed)
107%
84
APU - general
After three consecutive start attempts without cooling down, a ... interval must be observed before the next start.
60-minute
85
APU - General
The APU may be started and operated even if the LOW OIL LEVEL ECAM advisory is displayed. Maintenance action is required within next ... Of APU operation.
15 h
86
APU - Envelope
APU operation and start limit (FL)
41 450 ft (entire envelope)
87
APU - Envelope
APU battery start limit (ELEC EMER CONFIG) (FL)
25 000 ft
88
APU - Envelope
Ground starting and operation limit (FL)
14 600 ft
89
APU - Envelope
Bleed air & elec power
-1 000 ft to 22 500 ft
90
APU - Envelope
Elec power only
22 500 ft to 41 450 ft
91
Power Plant - Thrust Setting / EGT Limits
Takeoff and go-around
Time limit / EGT limit
5 or 10 min / 975'C
92
Power Plant - Thrust Setting / EGT Limits
MCT
Time limit / EGT limit
Unlimited / 940'C
93
Power Plant - Thrust Setting / EGT Limits
Starting
EGT limit on ground / in flight
750'C / 975'C
94
Power Plant - Oil
Maximum continuous temperature
160'C
95
Power Plant - Oil
Maximum transient temperature (15 min)
175'C
96
Power Plant - Oil
Minimum starting temperature
-40'C
97
Power Plant - Oil
Minimum oil quantity
12 qt + estimated consumption (average estimated consumption = 0,56 qt/h)
98
Power Plant - Oil
Minimum oil pressure
10 PSI
99
Power Plant - RPM
N1 max
115.5 %
Note: the N1 limit depends upon ambient conditions and engine air bleed configuration. These may limit the N1 to a value lower than that given above.
100
Power Plant - RPM
N2 max
113 %
101
Power Plant - Starter
Starter limitations
- Starter maximum continuous operation is 5 min;
- Between each cycle, wait 30 s per minute of operation for stater cooling;
- After two consecutive 5 min duty cycles, wait 10 min to allow starter to cool before each subsequent 5 min duty cycle;
- No running engagement of the starter when the N2 is above 30%.
102
Power Plant - Reduced Thrust Takeoff
T MAX FLEX (-200)
T MAX FLEX (-300)
ISA+43'C
| ISA+72'C
