Limitations Flashcards
Max Takeoff 190/195
51,800 Kg / 50,790 Kg
Max Landing
44,000 Kg / 45,000 Kg
Max Takeoff E2
61,200 kg
Max Landing E2
54,000 kg
Max 90 degree crosswind (including gusts) for CAT II and LVO
15 Kt (AD)
Max 90 degree crosswind component (STEADY) - Takeoff and Landing
25 Kt DRY RWY
Max 90 degree crosswind component (STEADY) Takeoff wet
15 Kt WET RWY
Max 90 degree crosswind component (STEADY) takeoff and Landing wet
15 Kt WET RWY
Max 90 degree crosswind component (STEADY) Takeoff and Landing DRY RWY or TAXIWAYS (1700m X40m or less)
25 Kt DRY
Max 90 degree crosswind component (STEADY) Takeoff and Landing WET RWY or TAXIWAYS (1700m X40m or less)
15 Kt WET
Max takeoff and landing tailwind component
10 Kt (AD)
XFEED Switch must be set to
OFF for takeoff and landing
Max Turbulent airspeed at or above 10,000 ft
270 Kt/.76 M
Max windshield wiper operation speed
250 Kt
Max gear extension speed VLO
265 Kt
Max gear retraction speed VLO
235 Kt
Max gear extended speed VLE
265 Kt
Max speed flap position 1
230 Kt
Max speed flap position 2
215 Kt
Max speed flap position 3
200 Kt
Max speed flap position 4 and 5
180 Kt
Max speed flap position FULL
165 Kt
Design maneuvering speed
240 Kt
E2 Max gear extension speed VLO
250 KIAS
E2 Max gear retraction speed VLO
220 KIAS
Auto pilot Precision approach
50 ft below DH/DA
E2 AP Precision approach
DH/DA (AD)
AP Nonprecision approach
MDA
AP Minimum Engagement Height on Takeoff
Acceleration Altitude1 (AD) Use of the autopilot in TO mode is prohibited. (AD)
AP Minimum Engagement Height on Go-Around
400 ft. AGL Applies only to a manually-flown go-around
AP Minimum Use Height - Enroute E1 / E2
500 ft AGL / 1000 ft AGL
AP Minimum Use Height - Visual Approach
500 ft AGL (AD) Applies to all visual approaches with no instrument backup. (AD)
ENGINE STARTER DUTY CYCLE (E1)
1st and 2nd attempt - 90 seconds ON (ground) / 10 seconds off
ENGINE STARTER DUTY CYCLE (E1) in flight
120 seconds ON (in flight)
ENGINE STARTER DUTY CYCLE (E2)
Maximum time - 240 seconds ON (ground/in flight) 30 min off-
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
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
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
The XFEED Selector must be set to
OFF during takeoff and landing
Do not takeoff with brake temperature indicators in
the amber range
Maximum altitude with flaps/slats extended is
20,000 ft
Takeoff with the Automatic Takeoff Thrust Control System (ATTCS) not in green is
not authorized
For aircraft equipped with Engine CF34-10E5-A1 when using TO-1 ATTCS will not be displayed. Takeoff is.
allowed
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.
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
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.
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.
Max Taxi & Ramp E95
50,950 Kg
Max Taxi & Ramp E2
61,700 kg
Max Zero Fuel E95
42,500 Kg
Max Zero Fuel E2
51,850 kg
Max Headwind (for CAT II and LVO)
25 Kt
Max 90 degree crosswind component (STEADY) Takeoff and Landing STANDING WATER GROOVED RWY
10 Kt
Max 90 degree crosswind component (STEADY) Takeoff and Landing STANDING WATER NON-GROOVED RWY
05 Kt
Max takeoff tailwind component for LVO
5 Kt (AD)
Maximum wind for passenger door operation
40 Kt
Maximum wind for cargo door opening
40 Kt
RUNWAY SLOPE Max (up hill, down hill)
+2.0%, -2.0%
Min fuel temperature
- 37°C
Max fuel imbalance left/right
360 kg
ALTITUDES Max operating
41,000 ft
ALTITUDES Max takeoff and landing
10,000 ft
ALTITUDES Max flap extension
20,000 ft
TEMPERATURES Max ambient for takeoff and landing
52°C
TEMPERATURES Min ambient approved for takeoff
-54°C
Max altitude for single pack operation
31,000 ft
Max differential pressure
8.4 psi
Max negative differential pressure
-0.5 psi
Max differential pressure for takeoff & landing
0.2 psi
LIMIT MANEUVERING LOAD FACTORS Flaps up
-1.0 to +2.5 G
LIMIT MANEUVERING LOAD FACTORS Flaps down (1, 2, 3, 4, 5 and full)
0.0 to +2.0 G
Max N1 and N2
100%
Max ITT During engine start (on ground)
740°C
E2 Max ITT During engine start (on ground), in flight, Takeoff and Go-Around
1054ºC
Max ITT During engine start (in flight)
875ºC
Max ITT Takeoff and Go-Around
983°C - Time limited to 5 min
Max Continuous ITT
960°C
E2 Max Continuous ITT
1017ºC
Min Oil Pressure E1/E2
25 psi / 50 psi
Max Oil Temperature E1 / E2
155°C / 163ºC
E2 Min Oil Temperature Idle / takeoff
- 40°C / 24ºC
ENGINE STARTER DUTY CYCLE (E1) 3rd through 5th attempt- 90 seconds ON (ground) / 120 seconds ON (in flight)
5 minutes off
Dry-Motoring Cycle 1st / 2nd attempt
90 seconds ON / 30 seconds ON - 5 minutes off
ENGINE STARTER DUTY CYCLE (E2) Maximum time
240 seconds ON (ground/in flight) / 30 min off
APU Starter Duty Cycle (E1) 1st and 2nd attempt
60 seconds ON / 60 seconds off
APU Starter Duty Cycle (E1) 3rd and subsequent
30 seconds ON / 5 minutes off
E2 APU Cooling period after each starting attempt - 1st and 2nd attempt
60 seconds off / 3rd and subsequent: 5 minutes off
APU - Min/ Max temperature for operations
-54°C / ISA +35°C
APU Max altitude for Start E1/E2
30,000 ft / 39,000 ft
APU Max altitude for electrical supply E1 / E2
33,000 ft / 39,000 ft
APU Max altitude for bleed supply
15,000 ft
APU Max altitude to assist engine start E1 / E2
21,000 ft / 20,000 ft
APU Max rotor speed
108%
APU Max EGT start.
1032°C
APU Max EGT Continuous
717°C only E1
Maximum operating airspeed
VMO
Maximum operating mach number
.82 (MMO)
Maximum airspeed for RAT operation
VMO/MMO
Turbulent air penetration speed (below 10,000 ft.)
250 KIAS
Tire limit ground speed
195 Kt
Maximum indicated airspeed (if windshield wiper failed in the non-parked position)
320 KIAS
Maximum Speed to open side (Direct Vision) window 160 KIAS
160 KIAS
Low visibility: Max takeoff tailwind component for LVO
5Kt
Low visibility - — Max Headwind
25 Kt .
Low visibility - — Max 90 degress crosswind (including gusts)
15 Kt (AD)
— Takeoff with contaminated runways is not allowed
Para os E195 E2 o limite de LMC é de
270 kg - DIM Narrow Bodies
Maximum Xwind Standing water grooved RWY
10 kt
Maximum Xwind Standing water non grooved RWY
05 kt
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
