Limitations Flashcards
1
Q
Max Takeoff 190/195
A
51,800 Kg / 50,790 Kg
2
Q
Max Landing
A
44,000 Kg / 45,000 Kg
3
Q
Max Takeoff E2
A
61,200 kg
4
Q
Max Landing E2
A
54,000 kg
5
Q
Max 90 degree crosswind (including gusts) for CAT II and LVO
A
15 Kt (AD)
6
Q
Max 90 degree crosswind component (STEADY) - Takeoff and Landing
A
25 Kt DRY RWY
7
Q
Max 90 degree crosswind component (STEADY) Takeoff wet
A
15 Kt WET RWY
8
Q
Max 90 degree crosswind component (STEADY) takeoff and Landing wet
A
15 Kt WET RWY
9
Q
Max 90 degree crosswind component (STEADY) Takeoff and Landing DRY RWY or TAXIWAYS (1700m X40m or less)
A
25 Kt DRY
10
Q
Max 90 degree crosswind component (STEADY) Takeoff and Landing WET RWY or TAXIWAYS (1700m X40m or less)
A
15 Kt WET
11
Q
Max takeoff and landing tailwind component
A
10 Kt (AD)
12
Q
XFEED Switch must be set to
A
OFF for takeoff and landing
13
Q
Max Turbulent airspeed at or above 10,000 ft
A
270 Kt/.76 M
14
Q
Max windshield wiper operation speed
A
250 Kt
15
Q
Max gear extension speed VLO
A
265 Kt
16
Q
Max gear retraction speed VLO
A
235 Kt
17
Q
Max gear extended speed VLE
A
265 Kt
18
Q
Max speed flap position 1
A
230 Kt
19
Q
Max speed flap position 2
A
215 Kt
20
Q
Max speed flap position 3
A
200 Kt
21
Q
Max speed flap position 4 and 5
A
180 Kt
22
Q
Max speed flap position FULL
A
165 Kt
23
Q
Design maneuvering speed
A
240 Kt
24
Q
E2 Max gear extension speed VLO
A
250 KIAS
25
E2 Max gear retraction speed VLO
220 KIAS
26
Auto pilot Precision approach
50 ft below DH/DA
27
E2 AP Precision approach
DH/DA (AD)
28
AP Nonprecision approach
MDA
29
AP Minimum Engagement Height on Takeoff
Acceleration Altitude1 (AD) Use of the autopilot in TO mode is prohibited. (AD)
30
AP Minimum Engagement Height on Go-Around
400 ft. AGL Applies only to a manually-flown go-around
31
AP Minimum Use Height - Enroute E1 / E2
500 ft AGL / 1000 ft AGL
32
AP Minimum Use Height - Visual Approach
500 ft AGL (AD) Applies to all visual approaches with no instrument backup. (AD)
33
ENGINE STARTER DUTY CYCLE (E1)
1st and 2nd attempt - 90 seconds ON (ground) / 10 seconds off
34
ENGINE STARTER DUTY CYCLE (E1) in flight
120 seconds ON (in flight)
35
ENGINE STARTER DUTY CYCLE (E2)
Maximum time - 240 seconds ON (ground/in flight) 30 min off-
36
Definition of Icing Conditions
Icing conditions exist when OAT (on the ground/takeoff) or TAT (in flight) is 10°C or less 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; or... — when operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines; or freeze on engines, nacelles, or engine sensor probes
37
Engine and Wing Anti-Ice System - On Ground - The T/O DATASET MENU on the MCDU must be set to ENG in the following cases:
when OAT is between 5ºC and 10ºC and;
• if there is any possibility of encountering visible moisture up to 1700 ft AFE
38
Engine and Wing Anti-Ice System - On Ground - The TO DATASET MENU on the MCDU must be set to ALL in the following cases
when OAT is below 5ºC and;
• if there is any possibility of encountering visible moisture up to 1700 ft AFE
39
The XFEED Selector must be set to
OFF during takeoff and landing
40
Do not takeoff with brake temperature indicators in
the amber range
41
Maximum altitude with flaps/slats extended is
20,000 ft
42
Takeoff with the Automatic Takeoff Thrust Control System (ATTCS) not in green is
not authorized
43
For aircraft equipped with Engine CF34-10E5-A1 when using TO-1 ATTCS will not be displayed. Takeoff is.
allowed
44
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.
45
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
46
For E2 airplanes, following high thrust operation the engine will be operated at or near idle for
three (3) minutes before shutdown to thermally stabilize the engine's hot section. Af ter landing, with thrust reversers stowed and idle thrust and Taxi time at or near idle can be included in this period.
47
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.
48
Max Taxi & Ramp E95
50,950 Kg
49
Max Taxi & Ramp E2
61,700 kg
50
Max Zero Fuel E95
42,500 Kg
51
Max Zero Fuel E2
51,850 kg
52
Max Headwind (for CAT II and LVO)
25 Kt
53
Max 90 degree crosswind component (STEADY) Takeoff and Landing STANDING WATER GROOVED RWY
10 Kt
54
Max 90 degree crosswind component (STEADY) Takeoff and Landing STANDING WATER NON-GROOVED RWY
05 Kt
55
Max takeoff tailwind component for LVO
5 Kt (AD)
56
Maximum wind for passenger door operation
40 Kt
57
Maximum wind for cargo door opening
40 Kt
58
RUNWAY SLOPE Max (up hill, down hill)
+2.0%, -2.0%
59
Min fuel temperature
- 37°C
60
Max fuel imbalance left/right
360 kg
61
ALTITUDES Max operating
41,000 ft
62
ALTITUDES Max takeoff and landing
10,000 ft
63
ALTITUDES Max flap extension
20,000 ft
64
TEMPERATURES Max ambient for takeoff and landing
52°C
65
TEMPERATURES Min ambient approved for takeoff
-54°C
66
Max altitude for single pack operation
31,000 ft
67
Max differential pressure
8.4 psi
68
Max negative differential pressure
-0.5 psi
69
Max differential pressure for takeoff & landing
0.2 psi
70
LIMIT MANEUVERING LOAD FACTORS Flaps up
-1.0 to +2.5 G
71
LIMIT MANEUVERING LOAD FACTORS Flaps down (1, 2, 3, 4, 5 and full)
0.0 to +2.0 G
72
Max N1 and N2
100%
73
Max ITT During engine start (on ground)
740°C
74
E2 Max ITT During engine start (on ground), in flight, Takeoff and Go-Around
1054ºC
75
Max ITT During engine start (in flight)
875ºC
76
Max ITT Takeoff and Go-Around
983°C - Time limited to 5 min
77
Max Continuous ITT
960°C
78
E2 Max Continuous ITT
1017ºC
79
Min Oil Pressure E1/E2
25 psi / 50 psi
80
Max Oil Temperature E1 / E2
155°C / 163ºC
81
E2 Min Oil Temperature Idle / takeoff
- 40°C / 24ºC
82
ENGINE STARTER DUTY CYCLE (E1) 3rd through 5th attempt- 90 seconds ON (ground) / 120 seconds ON (in flight)
5 minutes off
83
Dry-Motoring Cycle 1st / 2nd attempt
90 seconds ON / 30 seconds ON - 5 minutes off
84
ENGINE STARTER DUTY CYCLE (E2) Maximum time
240 seconds ON (ground/in flight) / 30 min off
85
APU Starter Duty Cycle (E1) 1st and 2nd attempt
60 seconds ON / 60 seconds off
86
APU Starter Duty Cycle (E1) 3rd and subsequent
30 seconds ON / 5 minutes off
87
E2 APU Cooling period after each starting attempt - 1st and 2nd attempt
60 seconds off / 3rd and subsequent: 5 minutes off
88
APU - Min/ Max temperature for operations
-54°C / ISA +35°C
89
APU Max altitude for Start E1/E2
30,000 ft / 39,000 ft
90
APU Max altitude for electrical supply E1 / E2
33,000 ft / 39,000 ft
91
APU Max altitude for bleed supply
15,000 ft
92
APU Max altitude to assist engine start E1 / E2
21,000 ft / 20,000 ft
93
APU Max rotor speed
108%
94
APU Max EGT start.
1032°C
95
APU Max EGT Continuous
717°C only E1
96
Maximum operating airspeed
VMO
97
Maximum operating mach number
.82 (MMO)
98
Maximum airspeed for RAT operation
VMO/MMO
99
Turbulent air penetration speed (below 10,000 ft.)
250 KIAS
100
Tire limit ground speed
195 Kt
101
Maximum indicated airspeed (if windshield wiper failed in the non-parked position)
320 KIAS
102
Maximum Speed to open side (Direct Vision) window 160 KIAS
160 KIAS
103
Low visibility: Max takeoff tailwind component for LVO
5Kt
104
Low visibility - — Max Headwind
25 Kt .
105
Low visibility - — Max 90 degress crosswind (including gusts)
15 Kt (AD)
— Takeoff with contaminated runways is not allowed
106
Para os E195 E2 o limite de LMC é de
270 kg - DIM Narrow Bodies
107
Maximum Xwind Standing water grooved RWY
10 kt
108
Maximum Xwind Standing water non grooved RWY
05 kt
109
Use of TCS is prohibited when:
- TO or GA are the active vertical modes; — Conducting an instrument approach when the weather is below 1000 ft./5 km; and, — Any operation where the autopilot and/or flight director are mandatory
