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EMB120 Limitations > Limitations > Flashcards

Limitations Flashcards

1
Q

Acft wingspan

A

19.78m

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2
Q

Acft length

A

20.00m

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3
Q

Acft tail height

A

6.35m

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4
Q

Max rwy slope

A

±2%

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5
Q

Max tw (to/ldg)

A

10 kts

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6
Q

Max xwind

A

30 kts

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7
Q

Max altitude - engine bleeds open/EEC on

A

32,000’

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8
Q

Max altitude – engine bleeds open/EEC off

A

25,000’

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9
Q

Max altitude – engine bleeds closed/EEC on

A

25,000’

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10
Q

Max altitude – engine bleeds closed/EEC off

A

20,000’

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11
Q

Max altitude – RH front aisle seat (1B) occupied

A

25,000’

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12
Q

VA

A

200 KIAS

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13
Q

VFE 10

A

200 KIAS

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14
Q

VFE 25

A

150 KIAS

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15
Q

VFE 45

A

135 KIAS

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16
Q

VLE

A

200 KIAS

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17
Q

VLO

A

200 KIAS

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18
Q

MMO

A

0.52

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19
Q

VMO >8000’

A

272 KIAS

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20
Q

VMO ≤8000’

A

250 KIAS

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21
Q

Turbulence penetration speed

A

175 KIAS

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22
Q

Max G flap retracted

A

-1.0 to +2.8

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23
Q

Max G flap extended

A

0 to +2.0

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24
Q

Max zero fuel weight

A

10,900 kg

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25
Q

Max ramp weight

A

12,070 kg

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26
Q

Max takeoff weight

A

11,990 kg

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27
Q

Max landing weight

A

11,700kg

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28
Q

Max baggage compartment weight - standard

A

550 kg

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29
Q

Max baggage compartment weight – dual net

A

700 kg

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30
Q

Minimum operational temp

A

-54°C

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31
Q

Maximum operational temp – Air Con operating

A

ISA +35°C

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32
Q

Maximum operational temp – Air conditioning inop

A

ISA +20°C Alt alert deenergised
ISA +15°C Alt alert energised

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33
Q

Maximum cabin differential

A

7.2 psi

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34
Q

Starter duty cycle

A

30 seconds on, 3 minutes off
30 seconds on, 3 minutes off
30 seconds on, 30 minutes off

35
Q

Max usable fuel qty per side

A

2866 lbs

36
Q

Max fuel imbalance

A

600 lbs

37
Q

Add __ lbs to unusable fuel when main ejector boost pump is inoperative

A

80 lbs

38
Q

APU max start EGT

A

732°C to 974°C for 10 seconds

39
Q

APU Max start alt

A

20,000’

40
Q

Max wiper speed

A

160 kts

41
Q

Min NH for pneumatic deicing systems

A

80%

42
Q

Main generator max load - on ground

A

380A (400A < ISA +27°C)

43
Q

Main generator max load – in flight

A

400A (380A > 27,000’)

44
Q

Aux generator max load

A

150A (140A > 18,000’)

45
Q

APU generator max load

A

400A (290A >16,000’)

46
Q

Max battery temp

A

70°C

47
Q

Min icing speed – flap up/gear up

A

165 KIAS

48
Q

Min icing speed – flap 15/gear up

A

140 KIAS

49
Q

Min battery voltage – engine start (no APU)

A

24v

50
Q

Min battery voltage – APU start

A

22v

51
Q

Max NH for positive oil px during engine start

A

45%

52
Q

Main landing gear track

A

6.58 m

53
Q

Min pavement width for 180° turn

A

18.85 m

54
Q

Min taxi turning radius

A

15.76 m (wingtip)

55
Q

Rwy considered wet

A

a. Surface water not more than 3mm deep
b. Slush or loose snow equivalent to surface water not more than 3mm deep
c. Sufficient moisture to appear reflective but without significant areas of standing water

56
Q

Rwy considered contaminated

A

More than 25% of the runway surface area within the required length and width being used covered by:
a. water, or slush more than 3 mm deep
b. loose snow more than 20 mm deep
c. compacted snow or ice, including wet ice

57
Q

T6 – takeoff

A

816°C for 5 mins

58
Q

T6 – max continuous

A

800°C

59
Q

T6 – starting

A

816-850°C for 20 seconds
850-950°C for 5 seconds

60
Q

T6 – transient

A

816-850°C for 20 seconds

61
Q

Torque – takeoff

A

110% for 5 mins

62
Q

Torque – max continuous

A

100%

63
Q

Torque – max climb/cruise

A

84%

64
Q

Torque – transient

A

120% for 20 seconds

65
Q

NP – takeoff/climb/cruise

A

100.0-101.0

66
Q

NP – transient

A

110% for 20 seconds

67
Q

NP- reverse

A

80.5%

68
Q

NH – takeoff/max continuous

A

102%

69
Q

NH – ground idle

A

62% min

70
Q

NH – climb/cruise

A

100%

71
Q

Oil temp – all airborne ops

A

45-115°C

72
Q

Oil temp – ground idle

A

-40 to 115°C

73
Q

Oil temp – starting

A

-40°C

74
Q

Oil temp – transient

A

115-125°C for 15 minutes

75
Q

Oil press – all airborne ops

A

55-65psi

76
Q

Oil press – ground idle

A

40 psi min

77
Q

Oil press – starting

A

70 psi max

78
Q

Oil press – transient

A

40-70psi

79
Q

Icing conditions exist in flight or on the ground in visible moisture with IOAT of __ C or below

A

+10℃

80
Q

Leading edge deicers must be activated only after reaching __________ speed

A

Final segment speed (VFS)

81
Q

In icing conditions, use of flaps is restricted to ____________.
When flaps have been extended for approach and landing, they may not be retracted unless ________ or unless _______

A

In icing conditions, use of flaps is restricted to takeoff, approach and landing.
When flaps have been extended for approach and landing, they may not be retracted unless upper surface of wing is clear of ice or unless flap retraction is required for go-around.

82
Q

OEI Max Bank Angle - V2

A

15°

83
Q

OEI Max Bank Angle - V2 + 5

A

20°

84
Q

OEI Max Bank Angle - V2 + 10

A

25°

EMB120 Limitations (6 decks)

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