Limitations Flashcards
1
Q
Max Takeoff 175
A
37,500 Kg
2
Q
Max Landing
A
34,000 Kg
3
Q
Max Ramp Weight MRW
A
37,660 kg
4
Q
Max Zero Fuel Weight MZFW
A
31,700 kg
5
Q
Max 90 degree crosswind for CAT II
A
12 Kt
6
Q
Max 90 degree crosswind component (STEADY) - Takeoff RCC 6
A
38 Kt DRY RWY
7
Q
Max 90 degree crosswind component (STEADY) Takeoff wet RCC 3
A
15 Kt WET RWY
8
Q
Max takeoff and landing tailwind component including CAT II
A
10 Kt
9
Q
XFEED Switch must be set to
A
OFF for takeoff and landing
10
Q
Max Turbulent airspeed at or above 10,000 ft
A
270 Kt/.76 M
11
Q
Max windshield wiper operation speed
A
253 Kt
12
Q
Max gear extension speed VLO
A
250 Kt
13
Q
Max gear retraction speed VLO
A
250 Kt
14
Q
Max gear extended speed VLE
A
250 Kt
15
Q
Max speed flap position 1
A
230 Kt
16
Q
Max speed flap position 2
A
215 Kt
17
Q
Max speed flap position 3
A
200 Kt
18
Q
Max speed flap position 4 and 5
A
180 Kt
19
Q
Max speed flap position FULL
A
165 Kt
20
Q
AP Precision approach CAT II
A
50 ft
21
Q
AP Minimum Engagement Height
A
400 ft
22
Q
AP Minimum Engagement Height cruise and descent
A
1000 ft AGL
23
Q
AP Minimum Use Height Approach
A
50 ft
24
Q
ENGINE STARTER DUTY CYCLE (E1)
A
1st and 2nd attempt - 90 seconds ON (ground) / 10 seconds off
25
ENGINE STARTER DUTY CYCLE (E1) in flight
120 seconds ON (in flight)
26
Definition of Icing Conditions
Icing conditions may exist whenever the Outside Air Temperature
(OAT) on the ground or for takeoff, or Total Air Temperature (TAT)
inflight, is 10°C or below and visible moisture in any form is present
(such as clouds, fog with visibility of one mile or less, rain, snow, sleet,
and ice crystals).
27
The XFEED Selector must be set to
OFF during takeoff and landing
28
Do not takeoff with brake temperature indicators in
the amber range
29
Maximum altitude with flaps/slats extended is
20,000 ft
30
For E1 / E2 airplanes, after the engine has started, operate at or near idle for at least
two (2) minutes before selecting high thrust. Taxi time at or near idle can be included in the warm-up period.
31
For E1 airplanes, following high thrust operation the engine will be operated at or near idle for
two (2) minutes before shutdown to thermally stabilize the engine's hot section. Taxi time at or near idle can be included in this period
32
In the event that a limitation in this manual disagrees with the AFM limitation, the AFM will prevail. In the event that a placard or instrument marking disagrees with the limitations shown in this manual,
the more restrictive limitation will prevail.
33
Max Headwind (for CAT II and LVO)
25 Kt
34
RUNWAY SLOPE Max (up hill, down hill)
+2.0%, -2.0%
35
Min fuel temperature
- 37°C
36
Max fuel imbalance left/right
360 kg
37
ALTITUDES Max operating
41,000 ft
38
ALTITUDES Max takeoff and landing
10,000 ft
39
ALTITUDES Max flap extension
20,000 ft
40
TEMPERATURES Max ambient for takeoff and landing
52°C
41
TEMPERATURES Min ambient approved for takeoff
-54°C
42
Max altitude for single pack operation
31,000 ft
43
Max differential pressure
8.4 psi
44
Max negative differential pressure
-0.5 psi
45
Max differential pressure for takeoff & landing
0.2 psi
46
LIMIT MANEUVERING LOAD FACTORS Flaps up
-1.0 to +2.5 G
47
LIMIT MANEUVERING LOAD FACTORS Flaps down (1, 2, 3, 4, 5 and full)
0.0 to +2.0 G
48
Max N1 and N2
99,5% 99,4%
49
Max ITT During engine start
815°C
50
Max ITT normal Takeoff and Go-Around
965ºC First 2 minutes of the total 5 minutes
limit
51
Max ITT Normal Takeoff and Go Around emaining 3 minutes of the total
5 minutes limit
949ºC
52
Max ITT Takeoff and Go-Around first 2 min / remaining 3 min of total 5 min
1006°C / 990 °C - Time limited to 5 min
53
Max Continuous ITT
960°C
54
Min Oil Pressure
25 psi
55
Max Oil Temperature
95°C
56
ENGINE STARTER DUTY CYCLE (E1) 3rd through 5th attempt- 90 seconds ON (ground) / 120 seconds ON (in flight)
5 minutes off
57
Dry-Motoring Cycle 1st attempt / 2 through to 5
90 seconds ON / 30 seconds ON / 5 minutes off (After five sequential motorings, cycle may be repeated
following a 15-minute cool-down period)
58
ENGINE STARTER DUTY CYCLE Maximum time
90/ 120 seconds ON (ground/in flight) / 10 sec off
59
APU Starter Duty Cycle 1st and 2nd attempt
60 seconds off
60
APU Starter Duty Cycle 3rd
5 minutes off
61
APU - Min/ Max temperature for operations
-54°C / 52°C
62
APU Max altitude for Start
30,000 ft
63
APU Max altitude for electrical supply E1
33,000 ft
64
APU Max altitude for bleed supply
15,000 ft
65
APU Max altitude to assist engine start E1
21,000 ft
66
APU Max rotor speed
108%
67
APU Max EGT start.
1032°C
68
APU Max EGT Continuous
717°C
69
Maximum operating airspeed
VMO
70
Maximum operating mach number
.82 (MMO)
71
Maximum airspeed for RAT operation
VMO/MMO
72
Turbulent air penetration speed (below 10,000 ft.)
250 KIAS
73
Tire limit ground speed
195 Kt
74
Low visibility - — Max Headwind
25 Kt .
75
The takeoff weight (weight at brake release or at start of takeoff run) is
the lowest between MTOW and the following weights:
− Maximum takeoff weight as calculated using the approved
software, and as limited by field length, climb and brake energy.
− Maximum takeoff weight, as limited by enroute, and landing
operating requirements
76
The landing weight is the lowest among MLW and the following
weights calculated using the approved software:
− Maximum approach and landing weight as limited by altitude,
temperature and climb gradient.
77
Maximum fuel capacity is
11709 l (9496 kg).
78
Maximum usable quantity per tank
5812.5 l (4714 kg)
79
Unusable quantity per tank
42 l (34 kg)
80
Max oil temperature continuous
155°C
81
Max oil temperature transient
163°C
82
Engine max STARTING DUTY CYCLE time 3rd to 5th
90 Seconds (On ground)
120 seconds (In-flight) / 5 min off
83
For ground starts, the maximum cumulative starter run time
per start attempt is
90 seconds (motoring plus start time)
84
For in-flight starts, the maximum cumulative starter run time
per start attempt is
120 seconds (motoring plus start time)
85
Maximum differential overpressure
8.8 psi
86
Due to engine compressor stall possibility, static takeoff is not
recommended with crosswind component greater than
25 kt
87
Max headwind CAT II
25kt
88
FMS - pilots must compare any procedures/route retrieved from the
FMS database with those published on the charts. Differences
between the charts and the FMS information up to
3 degrees are
acceptable.
