LIMITATIONS Flashcards
MAX T/O and LANDING
T/O E1 50,790 E2 61,200
LDG E1 44,000 E2 54,000
X WIND COMPONENTS FOR T/O & LDG DRY
T/O LDG DRY 25KT
T/O LDG DRY NARROW 15 KT
X WIND COMPONENT WET
T/O 20KT WET
LDG 15 KT WET
T/O LDG 05 WET NARROW
MAX TAILWIND COMPONENT
10 KT T/O AND LDG
MAX TAILWIND LVO
05 KT
MAX WIND PASSENGER DOOR OPERATION
40 KT
MAX WIND FOR CARGO DOOR OPENING
40 KT
RUNWAY SLOPE
-2% - +2%
MIN FUEL TEMPERATURE
-37 CELCIUS
MAX FUEL IMBALANCE
360KG
(XBLEED must be set to OFF for T/O and LDG
MAX OPERATING SPEED
Vmo
MAX OPERATING MACH NUMBER
.82 Mmo
MAX TURBULENT AIRSPEED BELOW 10,000FT
250 KT
MAX TURBULENT AIRSPEED AT OR ABOVE 10,000 FT
270 KT/ .76 M
TIRE LIMIT GROUND SPEED
195 KT
MAX WINDSHIELD WIPER SPEED
320 KT ( failed in non-parked position)
250 kt normal conditions
GEAR SPEEDS
E1 E2
Max gear extension Vlo 265 Kt 250 Kt
Max gear retraction Vlo 235 Kt 220 Kt
Max gear extended Vle 265 Kt 265 Kt
FLAP SPEEDS
(SAME FOR E1 AND E2)
1 - 230 Kt
2 - 215 Kt
3 - 200 Kt
4 & 5 - 180 Kt
FULL - 165 Kt
MANEUVERING SPEED
240 Kt
MAX OPERATING ALTITUDE
41,000 FT
MAX T/O LDG ALTITUDE
10,000 FT
MAX FLAP EXTENSION Altitude
20,000 FT
MAX AMBIENT TEMPERATURE FOR T/O & LDG
52 CELCIUS
MIN AMBIENT TEMPERATURE APPROVED FOR T/O
-54 CELCIUS
MAX ALTITUDE FOR SINGLE PACK OPERATION
31,000 FT
MAX POSITIVE AND NEGATIVE DIFFERENTIAL PRESSURE
-0.5 psi - +8.4 psi
MAX DIFFERENTIAL PRESSURE FOR T/O & LDG
0.2 psi
MIN ALT FOR AP USE
PRECISION E1 50FT BELOW DH/DA
E2 DH/DA
NON PRECISION E1MDA
E2 MDA
MIN ALT FOR AP USE
EN ROUTE - E1 500 FT AGL
E2 1000 FT
MIN ENGAGEMENT HEIGHT FOR AP
T/O - Acceleration ALT
ALL Other - 400 ft AGL (both)
MANEUVERING LOAD FACTOR LIMITS
Flaps Up: -1.0 to +2.5 G
Flaps Down: 0.0 to +2.0 G
MAX N1
100% (BOTH)
MAX N2
100% (BOTH)
MAX ITT DURING ENGINE START GROUND AND FLIGHT
E1 Ground 740 C
Flight 875 C
E2 Ground 1054 C
Flight 1054 C
MAX ITT T/O & GO-AROUND
E1 983 C
E2 1054 C
MAX CONTINUOUS ITT
E1 960 C
E2 1054 C
MIN OIL PRESSURE
E1 25 PSI
E2 50 PSI
MIN OIL TEMP IDLE (E2)
-40 C
MIN OIL TEMP T/O (E2)
24 C
MAX OIL TEMPERATURE
E1 155 C
E2 163 C
ENGINE STARTER CYCLE (E1)
1st and 2nd attempt 90 seconds ON ( ground ) 10 s off
120 seconds ON (flight)
3rd-5th attempt 90 seconds On (ground) 5 minutos off
120 seconds ON ( flight)
DRY-MOTORING CYCLE (E1)
1st attempt 90 seconds ON 5 minutes off
2nd attempt 30 seconds ON 5 minutes off
ENGINE STARTER DUTY CYCLE (E2)
MAX TIME 240 Seconds ON (ground & flight) 30 min off
APU STARTER CYCLE (E1)
1st & 2nd 60 Seconds ON 60 Seconds OFF
3rd and subsequent 30 seconds ON 5 min OFF
APU STARTER CYCLE (E2)
1st and 2nd attempt cooling period 60 secs off
3rd + cooling period 5 min off
MIN & MAX TEMP FOR OPERATIONS
-54 CELCIUS
ISA +35 CELCIUS
(BOTH)
MAX ALT FOR START
E1- 30,000 FT
E2 - 39,000 FT
MAX ALT FOR ELECTRICAL SUPPLY
E1 - 33,000 FT
E2 - 39,000 FT
MAX ALT FOR BLEED SUPPLY
15,000 FT (BOTH)
MAX ALT TO ASSIST ENGINE START
E1- 21,000 FT
E2- 20,000 FT
MAX ROTOR SPEED
108% (BOTH)
MAX EGT START
1032 CELCIUS (BOTH)
MAX EGT CONTINUOUS
E1- 717 CELCIUS
E2 ————-
USE OF ANTI ICE
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.
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 AF
In Flight - The engine and wing anti-ice systems operate automatically in case of ice encounter when the ICE PROTECTION Mode selector is in AUTO
ANTI ICE PROCEDURE FOR E2
Takeoffs using engine anti-ice system – Prior to initiation a takeoff with engine anti-ice a static run-up to a minimum of 60% N1 must be performed.
During this run-up all engines parameters must be checked to guarantee engine normal operation
FUEL CAPACITY E1
MAX usable p/ tank 6550 kg
UNUSABLE p/ tank 46kg
MAX FUEL CAPACITY 13,192KG/ 13,690 KG
MIN FUEL TEMPERATURE
-37 Celcius
MAX FUEL IMBALANCE
360 kg
XFEED LIMITATION
Must be set to OFF during takeoff and landing.
RNP RANGE for MANDATORY GPS and FD
operations using RNP 0.3 to less than 1.
Vmo
0-8,000 300kt
10,000 - 290 320
290+ ate .82M
T/O GO AROUND POWER TIME LIMIT
AEO- 5 MINUTES
OEI- 5 MINUTES
ENGINE WARMUP TIME
E1 - 2 MINUTES
E2 - 2 MINUTES
ENGINE COOLDOWN TIME
E1 - 2 MINUTES
E2 - 3 MINUTES
AUTOMATIC SHUTDOWN DURING FLIGHT
In flight, there is no automatic shutdown if EGT exceeds the limits. In this case, the APU must be shutdown if it is not essential for the flight.
LMC
225 kg
