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ERJ7 > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

1
Q

Max. T/O Wt.

A

85,517 lb

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2
Q

Max. Lnd. Wt.

A

74,957 lb

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3
Q

Max. Zero Fuel Wt.

A

69,886 lb

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4
Q

Max. AFT Cargo

A

2,535 lb

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5
Q

Max. FWD Cargo

A

3,306 lb

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6
Q

Min. Runway Width

A

100’ (SW)

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7
Q

Wing Span

A

93 ft 11 in.

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8
Q

Aircraft Length

A

103 ft 11 in

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9
Q

Tail Height

A

32 ft 4 in.

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10
Q

Max. Ops. Alt.

A

41,000 ft

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11
Q

Max. T/O & Lnd

A

8,000 ft

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12
Q

Max. Temp. T/O Lnd

A

ISA + 35°C (52˚C)

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13
Q

Min. Temp. T/O Lnd

A

-40°C

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14
Q

RWY Slope

A

+/- 2%

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15
Q

Max. Tailwind

A

15kts

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16
Q

Max. Single Pack Operations

A

FL310

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17
Q

VMO SL- 8,000’

A

300

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18
Q

VMO 10,000- Mach Transition

A

320

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19
Q

MMO

A

0.82M

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20
Q

VA

A

240

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21
Q

VLO EXT

A

250

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22
Q

VLE RET

A

250

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23
Q

VLE

A

250

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24
Q

V Tire

A

195

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25
Q

V RAT DEPLOY MAX

A

VMO/MMO

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26
Q

VMIN (to provide electrical power)

A

130

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27
Q

VB (below 10,000 ft)

A

250

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28
Q

VB (10,000 ft and above)

A

270/.76M (whichever is lower)

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29
Q

V wiper ops max

A

250 (SW)

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30
Q

Vwindow

A

160

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31
Q

VFE 1

A

230

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32
Q

VFE2

A

215

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33
Q

VFE3

A

200

34
Q

VFE4

A

180

35
Q

VFE5

A

180

36
Q

VFE6

A

165

37
Q

MAXIMUM RECOMMENDED CROSSWIND

DryRunway

A

38kts

38
Q

MAXIMUM RECOMMENDED CROSSWIND

WetRunway

A

31kts

39
Q

MAXIMUM RECOMMENDED CROSSWIND

Runway with Compacted Snow

A

20kts

40
Q

MAXIMUM RECOMMENDED CROSSWIND

Runway with Standing Water/Slush/WetSnow/DrySnow.

A

18kts

41
Q

MAXIMUM RECOMMENDED CROSSWIND

Runway with Ice

A

12kts

42
Q

SLATS / FLAPS

Max. Alt. Flaps/SlatsExtended

A

FL200

43
Q

SLATS / FLAPS

Enroute Ops

A

Prohibited

44
Q

SLATS / FLAPS

Min. Spoiler Speed

A

180kts

45
Q

SLATS / FLAPS

CATII Approach

A

Mandatory Flaps 5

46
Q

SLATS / FLAPS

Landing Flaps Full Go Around

A

Flaps 4

47
Q

SLATS / FLAPS

Landing Flaps 5 Go Around

A

Flaps 2

48
Q

Max. Ramp Wt.

A

85,870 lb

49
Q

Due to engine compressor stall possibility, static takeoff is not recommended with crosswind component greater than

A

30kts

50
Q

BATTERY LIMITATIONS

Min. voltage

A

22.5V

51
Q

MAX ENGINE ITT Start

A

815C

52
Q

OIL TEMP. MIN START

A

-40C

53
Q

OIL PRESSURE MIN Start

A

25psi

54
Q

STARTER CRANKING LIMITS
Engine Start (Ground)
1 & 2

A

90 Seconds ON 10 Seconds OFF

55
Q

STARTER CRANKING LIMITS
Engine Start (Ground)
3&4

A

90 Seconds ON 5 Minutes OFF

56
Q

STARTER CRANKING LIMITS
Engine Start (In Flight)
1 & 2

A

120 Seconds ON 10 Seconds OFF

57
Q

STARTER CRANKING LIMITS
Engine Start (In Flight)
3&5

A

120 Seconds ON 5 Minutes OFF

58
Q

DRY MOTORING DUTY CYCLE LIMITS
Motoring #
1

A

90 Seconds ON 5 Minutes OFF

59
Q

DRY MOTORING DUTY CYCLE LIMITS
Motoring #
2-5

A

30 Seconds ON 5 Minutes OFF

60
Q

Max. Fuel Capacity

A

20,935 lb

61
Q

Max. Imbalance

A

794lbs

62
Q

Min. Fuel Tank Temp.

A

-40C

63
Q

ItispermissibletotakeoffandlandwithaFUELIMBALANCEmessage as long as the actual imbalance does not exceed

A

794lbs

64
Q

Fuel crossfeed must be selected OFF during

A

takeoff and landing

65
Q

APU OPERATIONAL LIMITS

Max Operation Altitude

A

FL330

66
Q

APU OPERATIONAL LIMITS

START Altitude

A

FL300

67
Q

APU OPERATIONAL LIMITS

Electrical Generator Use

A

FL330

68
Q

APU OPERATIONAL LIMITS

Altitude Bleed Use

A

15000

69
Q

APU OPERATIONAL LIMITS

Altitude Engine Start

A

FL210

70
Q

Maximum Differential Pressure

Up to 37,000 ft

A

7.8 psi

71
Q

Maximum Differential Pressure

Above 37,000 ft

A

8.34 psi

72
Q

Maximum Differential Pressure

Max. Diff. Over Pressure

A

8.77 psi

73
Q

Maximum Differential Pressure

Max. Diff. Neg. Press

A

-0.5 psi

74
Q

Maximum Differential Pressure

Max. Diff. Press T/O Lnd

A

0.2 psi

75
Q

HYDRAULIC TEMPERATURE

Min. Reservoir Temp. for ENG Start

A

-18°C

76
Q

Use of the autopilot below the altitudes listed is prohibited.
Min. Engagement Height

A

400 ft AGL

77
Q

Use of the autopilot below the altitudes listed is prohibited.
Min. Use Height

A

50ft AGL

78
Q

Use of the autopilot below the altitudes listed is prohibited.
Min. Use Height - Non-precision Approach

A

MDA

79
Q

TAS, TAT, and SAT information are only valid above

A

60kts

80
Q

FMS LIMITATION

RNP instrument approaches are

A

not authorized (SW

81
Q

FMS LIMITATION

The use of FMS Speed Mode is

A

prohibited in the event of an engine failure.

ERJ7 (14 decks)

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