Limits Flashcards
1
Q
G limits
A
Clean +2.5/-1
Configured +2/-0
2
Q
Max taxi weight
A
233.9T
3
Q
Max takeoff weight
A
233.0T
4
Q
Max landing weight
A
182T
5
Q
Max zero fuel weight
A
170.0 T
6
Q
Minimum weight
A
116.0 T
7
Q
Minimum TAT
A
-53 deg
8
Q
Max and min Takeoff and landing pressure altitude
A
-2000 ft to 12’500 ft
9
Q
Maximum temp
A
+55 deg (decreases with altitude)
10
Q
Max runway slope
A
+- 2%
11
Q
Max demonstrated crosswind
A
45kts
12
Q
Max tailwind for takeoff
A
15kts
13
Q
Max tailwind for landing
A
15kts up to 11’000ft
10kts above 11’000ft
14
Q
Max wind for passenger or cargo door operation
A
40kts (50kts if nose is pointed into wind, or for cargo door on the lee wind side)
15
Q
Max speed at which doors must be shut
A
60kts
16
Q
VMO/MMO
A
330kts / 0.86 M
17
Q
Max flap speed - Conf 1
A
240kts
18
Q
Max flaps speed - Conf 2
A
205/196 kts
19
Q
Max flap speed -conf 3
A
186kts
20
Q
Max flaps speed - Conf full
A
180 kts
21
Q
Max speed for landing gear operation and use
A
250 kts
22
Q
Max altitude for landing gear operation and use
A
21’000ft
23
Q
Max tire speed
A
204 kts
24
Q
Max wiper speed
A
230 kts
25
Max speed with windows open
230 Kts
26
Air conditioning and external pack usage
Do not use conditioned air simultaneously from packs and low pressure ground units (to avoid chattering of the non return valves)
27
APU and ground HP cart restrictions
Do not use both at the same time in order to prevent damage to the overall system
28
Maximum normal cabin altitude
8'000 ft
29
Maximum manual cabin pressure
14'000ft
30
Minimum altitude for AP engagement
100ft
31
Minimum height for AP in non precision approach
Applicable minima
32
Minimum altitude for AP in ILS approach without CAT 2
160 ft
33
Minimum altitude for AP in a go around
100 ft
34
Auto Thrust restrictions
No receiving AAR or boom AAR
35
Airspace the FMGS is certified to operate in
BRNAV, PRNAV, RNP 4, RNP 10
36
Minimum DH for cat 2 approach
100ft
37
Minimum altitude for AP use during CAT2 approach
80ft
38
CAT 2 wind restrictions
Tailwind 10 kts
Crosswind 20 kts
Headwind 35 kts
39
Max wind speed for air stairs operation
35kts
40
Max weight for each step on air stairs
114 kg, 1 person every 2 steps
41
Max altitude for flaps and slats
20'000 ft
42
Approved fuel types
Jet A, Jet A1, Jet B, JP4, JP5, JP8
43
Inter tank asymmetry limits
Full tanks - 2.9 T
Half tanks - 4.8 T
7.5T - no restriction
44
Outer tank asymmetry maximum
Full tanks 1.48T
2. 4 T - 1.58 T
1. 73 T - no restrictions
45
Max fuel temperatures
Jet A, Jet A1, JP8, JP5 - +55•c
| JP 4, Jet B - +49•c
46
Minimum fuel quantity for take off ( associated warning)
5.2T
| Wing tank low level ECAM
48
Min speed for RCVR AAR operations
225kts or VPROT +10kts of config 0; whatever is greater
49
Maximum speed for RCVR AAR
300 KCAS or M.8
50
Operating altitude for RCVR AAR
5'000ft to 30'000ft
51
Limitations for AAR below 20'000ft
Do not refuel the trim tank more than 2.5 T. If you cannot, do in flight as soon as possible.
If last AAR operation planned below 20'000ft, ensure TT below 2.5 T prior to
There is no independent monitoring of the COG
52
If trim pump failure, at what pitch attitude can you not preform a manual transfer
3deg NU
53
Max brake temperature for take off
300 Deg C with brake fans off.
| 150 deg c with fans on
54
Max NWS angle
72 Deg.
| Limited to 65 deg for pushback and tow
56
Taxi with deflated tyres
7kts during the turn if only 1 tire is blown on any or all of the sets
3kts if 2 tyres are blown on the same gear, and NWS limited to 30 deg
57
Minimum flight crew oxygen pressure (worse case scenario)
910 psi
58
Boom Altitude limits
1'500 ft up to either 30'000 ft (heavy) or 35'000 ft (light) or 41'000 (no RCVR's within contact or pre contact)
59
G limits for Boom ops
Lowering or raising: > 0.8g
RCVR in contact: 0.5-1.5 g
Boom lowered: 0-2g
60
Max airspeed for boom operations
325kts or 0.86 M whichever is lower
61
Minimum airspeed for Boom ops
Whichever is greater of
1. VPROT +10 kts or
2. 180 CAS at or below 22'500ft
3. 200 CAS above 22'500ft
62
Altitude limits for Hose AAR
1'500ft to 35'000 ft
| Up to 41'000ft if no aircraft inside contact or precontact
63
Hose Deployed G limits
0 to +2 g
64
Max speed hoses deployed
325 KCAS or 0.86M
65
Hose temperature envelope
Do not deploy below -54 deg
| Cannot be extended for longer than 15 min between -50 to -54 deg without fuel transfer
66
What does the APU Low oil level ECAM mean
Maint. Action required in the next 15 hrs of operation, can be started and used as normal
67
APU starter duty cycle
3 consecutive starts required 60 min cool before starting attempted again
68
APU EGT limits (starting and normal operation)
Starting : 1250 deg
| Normal: 650 deg
69
APU altitude start and operation limit
41'450 ft
70
Max altitude for APU bleed supply
22'500 ft
71
MAX altitude that the APU can start from the APU battery
25'000 ft
72
Max OAT for APU operations
ISA +40 up to 16'600 ft
| ISA +35 above 16'600 ft
73
Normal hydraulic pressure
3000 PSI +/-200
77
Minimum fuel temperature
Inner tanks: -54•c or +3•c on the freezing point whatever is higher
Outer or trim tank: freezing point
78
TOGA EGT LIMITS
OEI 10 min 975 deg
| AEO 5 min 975 deg
79
MCT EGT limit
940 deg
80
Engine starting EGT limits
750 deg on ground
| 975 deg airborne
81
Max oil temperature
160 deg
82
Max transient oil temperature
For 15 min up to 175 deg
83
Engine N1 max
115.5%
84
Engine N2 max
113%
85
Max time for engine starter motor
5 min
86
Engine starting Duty cycle
```
5 min on
30sec off
5 min on
10 min off
5 min on ...
```
87
Flex max
ISA+72
88
FCOM definition of stormy areas
Within 3nm laterally
Below a thunderstorm
Within 5000ft above
