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Embraer > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Takeoff 190/195

A

51,800 Kg / 50,790 Kg

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2
Q

Max Landing

A

44,000 Kg / 45,000 Kg

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3
Q

Max Takeoff E2

A

61,200 kg

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4
Q

Max Landing E2

A

54,000 kg

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5
Q

Max 90 degree crosswind (including gusts) for CAT II and LVO

A

15 Kt (AD)

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6
Q

Max 90 degree crosswind component (STEADY) - Takeoff and Landing

A

25 Kt DRY RWY

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7
Q

Max 90 degree crosswind component (STEADY) Takeoff wet

A

15 Kt WET RWY

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8
Q

Max 90 degree crosswind component (STEADY) takeoff and Landing wet

A

15 Kt WET RWY

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9
Q

Max 90 degree crosswind component (STEADY) Takeoff and Landing DRY RWY or TAXIWAYS (1700m X40m or less)

A

25 Kt DRY

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10
Q

Max 90 degree crosswind component (STEADY) Takeoff and Landing WET RWY or TAXIWAYS (1700m X40m or less)

A

15 Kt WET

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11
Q

Max takeoff and landing tailwind component

A

10 Kt (AD)

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12
Q

XFEED Switch must be set to

A

OFF for takeoff and landing

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13
Q

Max Turbulent airspeed at or above 10,000 ft

A

270 Kt/.76 M

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14
Q

Max windshield wiper operation speed

A

250 Kt

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15
Q

Max gear extension speed VLO

A

265 Kt

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16
Q

Max gear retraction speed VLO

A

235 Kt

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17
Q

Max gear extended speed VLE

A

265 Kt

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18
Q

Max speed flap position 1

A

230 Kt

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19
Q

Max speed flap position 2

A

215 Kt

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20
Q

Max speed flap position 3

A

200 Kt

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21
Q

Max speed flap position 4 and 5

A

180 Kt

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22
Q

Max speed flap position FULL

A

165 Kt

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23
Q

Design maneuvering speed

A

240 Kt

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24
Q

E2 Max gear extension speed VLO

A

250 KIAS

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25
Q

E2 Max gear retraction speed VLO

A

220 KIAS

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26
Q

Auto pilot Precision approach

A

50 ft below DH/DA

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27
Q

E2 AP Precision approach

A

DH/DA (AD)

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28
Q

AP Nonprecision approach

A

MDA

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29
Q

AP Minimum Engagement Height on Takeoff

A

Acceleration Altitude1 (AD) Use of the autopilot in TO mode is prohibited. (AD)

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30
Q

AP Minimum Engagement Height on Go-Around

A

400 ft. AGL Applies only to a manually-flown go-around

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31
Q

AP Minimum Use Height - Enroute E1 / E2

A

500 ft AGL / 1000 ft AGL

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32
Q

AP Minimum Use Height - Visual Approach

A

500 ft AGL (AD) Applies to all visual approaches with no instrument backup. (AD)

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33
Q

ENGINE STARTER DUTY CYCLE (E1)

A

1st and 2nd attempt - 90 seconds ON (ground) / 10 seconds off

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34
Q

ENGINE STARTER DUTY CYCLE (E1) in flight

A

120 seconds ON (in flight)

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35
Q

ENGINE STARTER DUTY CYCLE (E2)

A

Maximum time - 240 seconds ON (ground/in flight) 30 min off-

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36
Q

Definition of Icing Conditions

A

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

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37
Q

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:

A

when OAT is between 5ºC and 10ºC and;

• if there is any possibility of encountering visible moisture up to 1700 ft AFE

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38
Q

Engine and Wing Anti-Ice System - On Ground - The TO DATASET MENU on the MCDU must be set to ALL in the following cases

A

when OAT is below 5ºC and;

• if there is any possibility of encountering visible moisture up to 1700 ft AFE

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39
Q

The XFEED Selector must be set to

A

OFF during takeoff and landing

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40
Q

Do not takeoff with brake temperature indicators in

A

the amber range

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41
Q

Maximum altitude with flaps/slats extended is

A

20,000 ft

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42
Q

Takeoff with the Automatic Takeoff Thrust Control System (ATTCS) not in green is

A

not authorized

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43
Q

For aircraft equipped with Engine CF34-10E5-A1 when using TO-1 ATTCS will not be displayed. Takeoff is.

A

allowed

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44
Q

For E1 / E2 airplanes, after the engine has started, operate at or near idle for at least

A

two (2) minutes before selecting high thrust. Taxi time at or near idle can be included in the warm-up period.

45
Q

For E1 airplanes, following high thrust operation the engine will be operated at or near idle for

A

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

46
Q

For E2 airplanes, following high thrust operation the engine will be operated at or near idle for

A

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.

47
Q

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,

A

the more restrictive limitation will prevail.

48
Q

Max Taxi & Ramp E95

A

50,950 Kg

49
Q

Max Taxi & Ramp E2

A

61,700 kg

50
Q

Max Zero Fuel E95

A

42,500 Kg

51
Q

Max Zero Fuel E2

A

51,850 kg

52
Q

Max Headwind (for CAT II and LVO)

A

25 Kt

53
Q

Max 90 degree crosswind component (STEADY) Takeoff and Landing STANDING WATER GROOVED RWY

A

10 Kt

54
Q

Max 90 degree crosswind component (STEADY) Takeoff and Landing STANDING WATER NON-GROOVED RWY

A

05 Kt

55
Q

Max takeoff tailwind component for LVO

A

5 Kt (AD)

56
Q

Maximum wind for passenger door operation

A

40 Kt

57
Q

Maximum wind for cargo door opening

A

40 Kt

58
Q

RUNWAY SLOPE Max (up hill, down hill)

A

+2.0%, -2.0%

59
Q

Min fuel temperature

A
  • 37°C
60
Q

Max fuel imbalance left/right

A

360 kg

61
Q

ALTITUDES Max operating

A

41,000 ft

62
Q

ALTITUDES Max takeoff and landing

A

10,000 ft

63
Q

ALTITUDES Max flap extension

A

20,000 ft

64
Q

TEMPERATURES Max ambient for takeoff and landing

A

52°C

65
Q

TEMPERATURES Min ambient approved for takeoff

A

-54°C

66
Q

Max altitude for single pack operation

A

31,000 ft

67
Q

Max differential pressure

A

8.4 psi

68
Q

Max negative differential pressure

A

-0.5 psi

69
Q

Max differential pressure for takeoff & landing

A

0.2 psi

70
Q

LIMIT MANEUVERING LOAD FACTORS Flaps up

A

-1.0 to +2.5 G

71
Q

LIMIT MANEUVERING LOAD FACTORS Flaps down (1, 2, 3, 4, 5 and full)

A

0.0 to +2.0 G

72
Q

Max N1 and N2

A

100%

73
Q

Max ITT During engine start (on ground)

A

740°C

74
Q

E2 Max ITT During engine start (on ground), in flight, Takeoff and Go-Around

A

1054ºC

75
Q

Max ITT During engine start (in flight)

A

875ºC

76
Q

Max ITT Takeoff and Go-Around

A

983°C - Time limited to 5 min

77
Q

Max Continuous ITT

A

960°C

78
Q

E2 Max Continuous ITT

A

1017ºC

79
Q

Min Oil Pressure E1/E2

A

25 psi / 50 psi

80
Q

Max Oil Temperature E1 / E2

A

155°C / 163ºC

81
Q

E2 Min Oil Temperature Idle / takeoff

A
  • 40°C / 24ºC
82
Q

ENGINE STARTER DUTY CYCLE (E1) 3rd through 5th attempt- 90 seconds ON (ground) / 120 seconds ON (in flight)

A

5 minutes off

83
Q

Dry-Motoring Cycle 1st / 2nd attempt

A

90 seconds ON / 30 seconds ON - 5 minutes off

84
Q

ENGINE STARTER DUTY CYCLE (E2) Maximum time

A

240 seconds ON (ground/in flight) / 30 min off

85
Q

APU Starter Duty Cycle (E1) 1st and 2nd attempt

A

60 seconds ON / 60 seconds off

86
Q

APU Starter Duty Cycle (E1) 3rd and subsequent

A

30 seconds ON / 5 minutes off

87
Q

E2 APU Cooling period after each starting attempt - 1st and 2nd attempt

A

60 seconds off / 3rd and subsequent: 5 minutes off

88
Q

APU - Min/ Max temperature for operations

A

-54°C / ISA +35°C

89
Q

APU Max altitude for Start E1/E2

A

30,000 ft / 39,000 ft

90
Q

APU Max altitude for electrical supply E1 / E2

A

33,000 ft / 39,000 ft

91
Q

APU Max altitude for bleed supply

A

15,000 ft

92
Q

APU Max altitude to assist engine start E1 / E2

A

21,000 ft / 20,000 ft

93
Q

APU Max rotor speed

A

108%

94
Q

APU Max EGT start.

A

1032°C

95
Q

APU Max EGT Continuous

A

717°C only E1

96
Q

Maximum operating airspeed

A

VMO

97
Q

Maximum operating mach number

A

.82 (MMO)

98
Q

Maximum airspeed for RAT operation

A

VMO/MMO

99
Q

Turbulent air penetration speed (below 10,000 ft.)

A

250 KIAS

100
Q

Tire limit ground speed

A

195 Kt

101
Q

Maximum indicated airspeed (if windshield wiper failed in the non-parked position)

A

320 KIAS

102
Q

Maximum Speed to open side (Direct Vision) window 160 KIAS

A

160 KIAS

103
Q

Low visibility: Max takeoff tailwind component for LVO

A

5Kt

104
Q

Low visibility - — Max Headwind

A

25 Kt .

105
Q

Low visibility - — Max 90 degress crosswind (including gusts)

A

15 Kt (AD)

— Takeoff with contaminated runways is not allowed

106
Q

Para os E195 E2 o limite de LMC é de

A

270 kg - DIM Narrow Bodies

107
Q

Maximum Xwind Standing water grooved RWY

A

10 kt

108
Q

Maximum Xwind Standing water non grooved RWY

A

05 kt

109
Q

Use of TCS is prohibited when:

A
  • 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

Embraer (15 decks)

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