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EJET ELEVACAO > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

(66 cards)

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1
Q

MAX T/O and LANDING

A

T/O E1 50,790 E2 61,200

LDG E1 44,000 E2 54,000

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2
Q

X WIND COMPONENTS FOR T/O & LDG DRY

A

T/O LDG DRY 25KT
T/O LDG DRY NARROW 15 KT

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3
Q

X WIND COMPONENT WET

A

T/O 20KT WET
LDG 15 KT WET
T/O LDG 05 WET NARROW

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4
Q

MAX TAILWIND COMPONENT

A

10 KT T/O AND LDG

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5
Q

MAX TAILWIND LVO

A

05 KT

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6
Q

MAX WIND PASSENGER DOOR OPERATION

A

40 KT

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7
Q

MAX WIND FOR CARGO DOOR OPENING

A

40 KT

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8
Q

RUNWAY SLOPE

A

-2% - +2%

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9
Q

MIN FUEL TEMPERATURE

A

-37 CELCIUS

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10
Q

MAX FUEL IMBALANCE

A

360KG
(XBLEED must be set to OFF for T/O and LDG

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11
Q

MAX OPERATING SPEED

A

Vmo

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12
Q

MAX OPERATING MACH NUMBER

A

.82 Mmo

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13
Q

MAX TURBULENT AIRSPEED BELOW 10,000FT

A

250 KT

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14
Q

MAX TURBULENT AIRSPEED AT OR ABOVE 10,000 FT

A

270 KT/ .76 M

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15
Q

TIRE LIMIT GROUND SPEED

A

195 KT

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16
Q

MAX WINDSHIELD WIPER SPEED

A

320 KT ( failed in non-parked position)
250 kt normal conditions

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17
Q

GEAR SPEEDS

A

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

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18
Q

FLAP SPEEDS

A

(SAME FOR E1 AND E2)
1 - 230 Kt
2 - 215 Kt
3 - 200 Kt
4 & 5 - 180 Kt
FULL - 165 Kt

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19
Q

MANEUVERING SPEED

A

240 Kt

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20
Q

MAX OPERATING ALTITUDE

A

41,000 FT

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21
Q

MAX T/O LDG ALTITUDE

A

10,000 FT

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22
Q

MAX FLAP EXTENSION Altitude

A

20,000 FT

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23
Q

MAX AMBIENT TEMPERATURE FOR T/O & LDG

A

52 CELCIUS

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24
Q

MIN AMBIENT TEMPERATURE APPROVED FOR T/O

A

-54 CELCIUS

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25
MAX ALTITUDE FOR SINGLE PACK OPERATION
31,000 FT
26
MAX POSITIVE AND NEGATIVE DIFFERENTIAL PRESSURE
-0.5 psi - +8.4 psi
27
MAX DIFFERENTIAL PRESSURE FOR T/O & LDG
0.2 psi
28
MIN ALT FOR AP USE
PRECISION E1 50FT BELOW DH/DA E2 DH/DA NON PRECISION E1MDA E2 MDA
29
MIN ALT FOR AP USE
EN ROUTE - E1 500 FT AGL E2 1000 FT
30
MIN ENGAGEMENT HEIGHT FOR AP
T/O - Acceleration ALT ALL Other - 400 ft AGL (both)
31
MANEUVERING LOAD FACTOR LIMITS
Flaps Up: -1.0 to +2.5 G Flaps Down: 0.0 to +2.0 G
32
MAX N1
100% (BOTH)
33
MAX N2
100% (BOTH)
34
MAX ITT DURING ENGINE START GROUND AND FLIGHT
E1 Ground 740 C Flight 875 C E2 Ground 1054 C Flight 1054 C
35
MAX ITT T/O & GO-AROUND
E1 983 C E2 1054 C
36
MAX CONTINUOUS ITT
E1 960 C E2 1054 C
37
MIN OIL PRESSURE
E1 25 PSI E2 50 PSI
38
MIN OIL TEMP IDLE (E2)
-40 C
39
MIN OIL TEMP T/O (E2)
24 C
40
MAX OIL TEMPERATURE
E1 155 C E2 163 C
41
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)
42
DRY-MOTORING CYCLE (E1)
1st attempt 90 seconds ON 5 minutes off 2nd attempt 30 seconds ON 5 minutes off
43
ENGINE STARTER DUTY CYCLE (E2)
MAX TIME 240 Seconds ON (ground & flight) 30 min off
44
APU STARTER CYCLE (E1)
1st & 2nd 60 Seconds ON 60 Seconds OFF 3rd and subsequent 30 seconds ON 5 min OFF
45
APU STARTER CYCLE (E2)
1st and 2nd attempt cooling period 60 secs off 3rd + cooling period 5 min off
46
MIN & MAX TEMP FOR OPERATIONS
-54 CELCIUS ISA +35 CELCIUS (BOTH)
47
MAX ALT FOR START
E1- 30,000 FT E2 - 39,000 FT
48
MAX ALT FOR ELECTRICAL SUPPLY
E1 - 33,000 FT E2 - 39,000 FT
49
MAX ALT FOR BLEED SUPPLY
15,000 FT (BOTH)
50
MAX ALT TO ASSIST ENGINE START
E1- 21,000 FT E2- 20,000 FT
51
MAX ROTOR SPEED
108% (BOTH)
52
MAX EGT START
1032 CELCIUS (BOTH)
53
MAX EGT CONTINUOUS
E1- 717 CELCIUS E2 -------------
54
USE OF ANTI ICE
On Ground ​ The T/O DATASET MENU on the MCDU​ must be set to **EN​G** 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 en​countering 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
55
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
56
FUEL CAPACITY E1
MAX usable p/ tank 6550 kg UNUSABLE p/ tank 46kg MAX FUEL CAPACITY 13,192KG/ 13,690 KG
57
MIN FUEL TEMPERATURE
-37 Celcius
58
MAX FUEL IMBALANCE
360 kg
59
XFEED LIMITATION
Must be set to OFF during takeoff and landing.
60
RNP RANGE for MANDATORY GPS and FD
operations using RNP 0.3 to less than 1.
61
Vmo
0-8,000 300kt 10,000 - 290 320 290+ ate .82M
62
T/O GO AROUND POWER TIME LIMIT
AEO- 5 MINUTES OEI- 5 MINUTES
63
ENGINE WARMUP TIME
E1 - 2 MINUTES E2 - 2 MINUTES
64
ENGINE COOLDOWN TIME
E1 - 2 MINUTES E2 - 3 MINUTES
65
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.
66
LMC
225 kg

EJET ELEVACAO (17 decks)

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