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EJET ELEVACAO > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

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
Q

MAX ALTITUDE FOR SINGLE PACK OPERATION

A

31,000 FT

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26
Q

MAX POSITIVE AND NEGATIVE DIFFERENTIAL PRESSURE

A

-0.5 psi - +8.4 psi

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27
Q

MAX DIFFERENTIAL PRESSURE FOR T/O & LDG

A

0.2 psi

28
Q

MIN ALT FOR AP USE

A

PRECISION E1 50FT BELOW DH/DA
E2 DH/DA

NON PRECISION E1MDA
E2 MDA

29
Q

MIN ALT FOR AP USE

A

EN ROUTE - E1 500 FT AGL
E2 1000 FT

30
Q

MIN ENGAGEMENT HEIGHT FOR AP

A

T/O - Acceleration ALT
ALL Other - 400 ft AGL (both)

31
Q

MANEUVERING LOAD FACTOR LIMITS

A

Flaps Up: -1.0 to +2.5 G

Flaps Down: 0.0 to +2.0 G

32
Q

MAX N1

A

100% (BOTH)

33
Q

MAX N2

A

100% (BOTH)

34
Q

MAX ITT DURING ENGINE START GROUND AND FLIGHT

A

E1 Ground 740 C
Flight 875 C

E2 Ground 1054 C
Flight 1054 C

35
Q

MAX ITT T/O & GO-AROUND

A

E1 983 C

E2 1054 C

36
Q

MAX CONTINUOUS ITT

A

E1 960 C

E2 1054 C

37
Q

MIN OIL PRESSURE

A

E1 25 PSI

E2 50 PSI

38
Q

MIN OIL TEMP IDLE (E2)

A

-40 C

39
Q

MIN OIL TEMP T/O (E2)

A

24 C

40
Q

MAX OIL TEMPERATURE

A

E1 155 C

E2 163 C

41
Q

ENGINE STARTER CYCLE (E1)

A

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
Q

DRY-MOTORING CYCLE (E1)

A

1st attempt 90 seconds ON 5 minutes off

2nd attempt 30 seconds ON 5 minutes off

43
Q

ENGINE STARTER DUTY CYCLE (E2)

A

MAX TIME 240 Seconds ON (ground & flight) 30 min off

44
Q

APU STARTER CYCLE (E1)

A

1st & 2nd 60 Seconds ON 60 Seconds OFF

3rd and subsequent 30 seconds ON 5 min OFF

45
Q

APU STARTER CYCLE (E2)

A

1st and 2nd attempt cooling period 60 secs off

3rd + cooling period 5 min off

46
Q

MIN & MAX TEMP FOR OPERATIONS

A

-54 CELCIUS

ISA +35 CELCIUS

(BOTH)

47
Q

MAX ALT FOR START

A

E1- 30,000 FT

E2 - 39,000 FT

48
Q

MAX ALT FOR ELECTRICAL SUPPLY

A

E1 - 33,000 FT

E2 - 39,000 FT

49
Q

MAX ALT FOR BLEED SUPPLY

A

15,000 FT (BOTH)

50
Q

MAX ALT TO ASSIST ENGINE START

A

E1- 21,000 FT

E2- 20,000 FT

51
Q

MAX ROTOR SPEED

A

108% (BOTH)

52
Q

MAX EGT START

A

1032 CELCIUS (BOTH)

53
Q

MAX EGT CONTINUOUS

A

E1- 717 CELCIUS

E2 ————-

54
Q

USE OF ANTI ICE

A

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
Q

ANTI ICE PROCEDURE FOR E2

A

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
Q

FUEL CAPACITY E1

A

MAX usable p/ tank 6550 kg
UNUSABLE p/ tank 46kg

MAX FUEL CAPACITY 13,192KG/ 13,690 KG

57
Q

MIN FUEL TEMPERATURE

A

-37 Celcius

58
Q

MAX FUEL IMBALANCE

A

360 kg

59
Q

XFEED LIMITATION

A

Must be set to OFF during takeoff and landing.

60
Q

RNP RANGE for MANDATORY GPS and FD

A

operations using RNP 0.3 to less than 1.

61
Q

Vmo

A

0-8,000 300kt

10,000 - 290 320

290+ ate .82M

62
Q

T/O GO AROUND POWER TIME LIMIT

A

AEO- 5 MINUTES
OEI- 5 MINUTES

63
Q

ENGINE WARMUP TIME

A

E1 - 2 MINUTES

E2 - 2 MINUTES

64
Q

ENGINE COOLDOWN TIME

A

E1 - 2 MINUTES

E2 - 3 MINUTES

65
Q

AUTOMATIC SHUTDOWN DURING FLIGHT

A

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
Q

LMC

A

225 kg

EJET ELEVACAO (17 decks)

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