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1
Q

Autopilot minimum Engagment Height

A

400 ft

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2
Q

Minimum Use Height (MUH) Autopilot
Cruise and Descent

A

1000 ft

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3
Q

Minimum Use Height (MUH)
Approach

A

50ft

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4
Q

Maximum differential pressure

A

8.4 psi

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5
Q

Maximum differential negative pressure

A

-0.5 psi

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6
Q

Maximum differential overpressure

A

8.8psi

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7
Q

Maximum differential pressure Take-off and Landing

A

0.2 psi

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8
Q

Engine Starter Limits
(GROUND and IN FLIGHT)

A

1) GROUND START- (90s 10s) (90s 10s)
(90s 5min) (90s 5min) (90s 5min)

2) IN FLIGHT START- (120s 10s)
(120s 10s) (120s 5min) (120s 5min) (120s 5min)

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9
Q

Engine Starter
DRY MOTORING DUTY CYCLE LIMITS

A

(90s 5min) (30s 5 min) (30s 5min) (30s 5min) (30s 5min) (30s 5min)
After 5 sequential motoring 15min

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10
Q

ENGINE
MAX GROUND START ITT

A

740 C

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11
Q

ENGINE
MAX IN-FLIGHT START ITT

A

875 C

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12
Q

ENGINE
MAX CONTINUOUS ITT

A

960 C

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13
Q

ENG MAX OIL TEMPERATURE

A

155 C

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14
Q

Max Cabin Diff. Press up to 37000 ft

A

7.8 psi

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15
Q

Max Cabin Diff. Pressure above 37000 ft

A

8.4 psi

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16
Q

Max Tire Speed

A

195 KTS

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17
Q

APU ALTITUDE START LIMIT

A

30000 ft

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18
Q

APU ELECTRICAL GEN MAX ALTITUDE LIMIT

A

33000 ft

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19
Q

APU BLEED MAX OPERATIONAL ALTITUDE

A

15000 ft

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20
Q

APU MAX ALTITUDE ENGINE START

A

21000ft

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21
Q

APU MAX ROTOR SPEED

A

108%

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22
Q

APU EGT START LIMIT

A

1032 C

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23
Q

APU EGT CONTINUOUS LIMIT

A

717 C

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24
Q

ENG MIN OIL PRESSURE

A

25psi (During starts with oil temperature below -22C the minimum oil pressure is 5 psi, time limited to 2 min.)

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25
Q

VMO below 8000ft

A

300KT

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26
Q

10000ft <VMO< 29000ft

A

320KTS

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27
Q

Mmo

A

0.82 mach

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28
Q

Flaps 1

A

230 Kts

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29
Q

Flaps 2

A

215 KTS

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30
Q

FLAPS 3

A

200 KTS

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31
Q

FLAP 4

A

180KTS

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32
Q

FLAP 5

A

180 KTS

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33
Q

FLAP FULL

A

165 KTS

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34
Q

FLAPS UP LOAD FACTOR LIMIT

A

-1.0 g 2.5g

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35
Q

FLAPS DOWN LOAD FACTOR LIMIT

A

0.0 g / 2.0 g

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36
Q

Max Operating Altitude

A

41000 ft

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37
Q

VLO EXTENSION

A

265 KTS

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38
Q

VLE

39
Q

VLO Retraction

40
Q

Maximum Fuel (both Wings)

41
Q

Unusable Fuel (per wing tank )

42
Q

Maximum Flap Extended Altitude

43
Q

MZFW (Maximum Zero Fuel Weight)

A

42500kg. EMB 195
40800kg. EMB 190

44
Q

MLW (Maximum Landing Weight)

A

45000kg E195
43000kg E190

45
Q

Max Speed Direct Vision Window

46
Q

Runway Limits

A

Runway
Slope from -2% to +2%
Surface PAVED

47
Q

Windshield Wiper Speed Limitation

48
Q

ENG MAX N1 and N2 indication

49
Q

ENG Minimum N2

50
Q

Max Permitted Fuel Imbalance Tanks

51
Q

APU STARTER LIMITS (cooling period)

A

Cooling period after each starting attempt

(1st and 2nd) 60s OFF
(3rd attempt) 5 min OFF

52
Q

MAX CONTAMINANT DEPTH TAKE-OFF

53
Q

MRW (Max Ramp Weight)

A

50950 kg E195
50460 kg E190

54
Q

MTOW (Max. Take-off Weight)

A

50790 kg EMB 195
50300 kg EMB 190

55
Q

Temperature Limitation ANTI-ICE System

A

NO TEMPERATURE LIMITATION FOR ANTI-ICE SYSTEM

56
Q

ON GROUND

The TO DATASET MENU ON MCDU must be set to ENG when?

(ICE AND RAIN PROTECTION)

A

1) OAT is within 5-10 C. ( 5 compreso )

2)If there is any possibility of encountering visible moisture up to 1700ft AFE

3)When operating on ramp,taxiways,or runways where surface snow, ice, standing water, or slush may be ingested by the engine, nacelles, or engine sensor probes

57
Q

ON GROUND

The TO DATASET MENU on the MCDU must be set to ALL when?

(ICE AND RAIN PROTECTION)

A

1)OAT is below 5 C

2) If there is any possibility of encountering visible moisture up to 1700 ft AFE

3) 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, nacelle, or engine sensor probes.

58
Q

ICE AND RAIN PROTECTION
IN FLIGHT

A

The engine and wing anti-ice systems operate automatically, in case of ice encounter when the Ice Protection Mode Knob is in the AUTO position.

If either one or both ice detectors are failed, the Crew must set the Mode Selector to ON when icing conditions exists or are anticipated below 10 C TAT with visible moisture.

59
Q

CROSSFEED OPERATION

A

CROSSFEED Selector Knob must be set OFF during take-off and landings

60
Q

MINIMUM CREW

61
Q

Minimum Equipments Required for CAT II APPROACHES
(Demonstrated to meet airworthiness requirements)

A
  • 2 IRS (Inertial Reference Systems)
  • 2 FDs (Flight Director Systems)
  • 2 PFDs (Primary flight Displays)
  • 1 Windshield Wiper
  • 2 VOR/ILS NAV System
  • 1 VHF/COMM System
  • 1 RA (Radio Altimeter)
  • 1 EGPWS (Ground Proximity Warning System)
  • 2 ADS (Air Data Systems)
  • 1 Autopilot System Channel

NOTE: Manual FD (Flight Director) CAT II ILS Approaches are prohibited.

62
Q

CAT II APPROACH AND LANDINGS FLAPS LIMITATION

A

CAT II approach and landing must be performed with flaps 5.

63
Q

FLIGHT CONTROLS CAT II LIMITATION

A

CAT II is prohibited with the SPOILER FAULT EICAS message displayed.

64
Q

DEMONSTRATED WIND COMPONENTS CAT II

A

Headwind 37 KTS
Tailwind 15 KTS
Crosswind 16KTS
( values not to be considered limiting)

65
Q

RVSM MINIMUM EQUIPMENT REQUIRED

A

During RVSM operation it is necessary that the following equipment and instruments be in proper operating condition.

  • 2 RVSM Compliant ADs (Air Data Systems)
  • 1 Autopilot with Altitude Hold Mode operative
  • 1 Altitude Alerter
  • 1 Transponder
66
Q

Max take-off and landing tailwind component

67
Q

FUEL TEMPERATURE LIMIT

A

JET A / F35= -37 C

JET A1 / JP-8 / QAV-1 / F-34 / F-35= -44

68
Q

Maximum latitude for stationary Alignment

A

78.25 gradi

69
Q

MAX XWIND DRY

(Take-off)

70
Q

MAX XWIND WET
(Take-off)

71
Q

MAX XWIND SNOW
(Take-off)

72
Q

MAX XWIND SLUSH/WET SNOW
(Take-off)

73
Q

MAX XWIND WITH ICE
(Take-off)

74
Q

MAX TAILWIND (take-off and landing)

75
Q

AUTOLAND MAX TAILWIND & XWIND

A

15 KTS & 15KTS

76
Q

Max Airport Altitude for the AUTOLAND

77
Q

AIRPLANE SERVICE CEALING

78
Q

TAKE-OFF,LANDING AND GROUND OPERATION ENVELOPE LIMIT

A

-1000<x< 10000

79
Q

MAX TEMP FL 410

80
Q

Lenght EMB 195

81
Q

Height Embraer 195

82
Q

Wingspan EMB 195

83
Q

TAILSPAN EMBRAER 195

84
Q

WHEELBASE width

85
Q

AUTOLAND MAX HEADWIND

86
Q

MAX TAKE-OFF AND LANDING TEMPERATURE AND GROUND TEMP
( 0 FT )

87
Q

MIN TAKE-OFF AND LANDING TEMPERATURE
( 0 ft )

A

-40 C
(In the event of a landing below -40,the airplane may not take-off without further maintenence inspection)

88
Q

Operational envelope limit MAX TEMP

FROM 0 to 36000 (more or less)

89
Q

ANTI-ICE AUTOMATIC NORMAL OPERATION ENGAGEMENT HEIGHT

A

1700 FT AFE

90
Q

ENGINE MAX TAKE-OFF AND GO AROUND ITT

A

983 C. (Above 5.5 C for 2 sec, 4.4 C for 5 sec, 3.6 C for 15 sec, 2.4 C 30 sec)

91
Q

MAGNETIC CUT-OUT REGIONS (IRS)

A

North 73.125 < X < 82
West 80 < X < 130

North > 82
West/East 0 < x < 180

South 60 < x < 82
East 120 < x < 160

South > 82
East/West 0 < x < 180

92
Q

Runway slope for AUTOLAND

A

Min -1%
Max +1%

93
Q

Min BATT 2 APU temperature for engine start

94
Q

Minimum OIL temperature engine for cold Ops

A

-22 C and minimum oil pressure of 25 psi can be lowered to 5 psi

LIM TYPE (1 decks)

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