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EMB175 STUDY GUIDE ITEMS > E175 LIMITATIONS > Flashcards

E175 LIMITATIONS Flashcards

1
Q

AIRCRAFT DEMENSIONS

A

LENGTH: 103’ 11” (104’)
WIDTH: 93’ 11” (94’)
HEIGHT: 32’ 4” (33’)

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2
Q

CABIN LOADING

A

Max PAX 76
(12 First/64 Coach)

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3
Q

CARGO COMPARTMENT

A

FWD: 3,307lbs
AFT: 2,535lbs

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4
Q

AIRCRAFT WEIGHTS-MAXIMUM RAMP WEIGHT (MRW)

A

85,800lbs

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5
Q

AIRCRAFT WEIGHTS-MAXIMUM TAKEOFF WEIGHT (MTOW)

A

85,500lbs

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6
Q

AIRCRAFT WEIGHTS:MAXIMUM LANDING WEIGHT (MLW)

A

74,900lbs

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7
Q

AIRCRAFT WEIGHTS:MAXIMUM ZERO FUEL WEIGHT (MZFW)

A

69,800lbs

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8
Q

MINIMUM CREW

A

Left Seat Pilot & Right Seat Pilot
(Captain & First Officer)

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9
Q

AIRCRAFT OPERATIONS

A

Day & Night
VFR & IFR
Icing Conditions
CAT I & CAT II
RVSM

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10
Q

AIR: Max Cabin Differential Overpressure (Safety Valve)

A

8.8 PSI

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11
Q

AIR: Max Cabin Differential Pressure

A

Above FL370- 8.4 PSI
T/O & Landing- 0.2 PSI
Negative- 0.5 PSI

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12
Q

AIR: Maximum Altitude Depressurized

A

10,000’ or MEA
(Whichever is higher)

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13
Q

AIR: Maximum Altitude for Single Pack Operation

A

31,000’

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14
Q

AIRSPEEDS
(MMO Above FL280)

A

0.82M

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15
Q

AIRSPEEDS
(VMO Above 10,000 to FL280)

A

320 KIAS

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16
Q

AIRSPEEDS
(VMO Below 10,000)

A

250 KIAS (FAA Regulatory)
300 KIAS Structural Speed Limit

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17
Q

AIRSPEEDS
(VA)

A

240 KIAS

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18
Q

AIRSPEEDS
(VLE)

A

250 KIAS

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19
Q

AIRSPEEDS
(VLO)

A

250 KIAS

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20
Q

AIRSPEEDS
(VLR)

A

250 KIAS

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21
Q

AIRSPEEDS
(VFE1)

A

230 KIAS

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22
Q

AIRSPEEDS
(VFE2)

A

215 KIAS

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23
Q

AIRSPEEDS
(VFE3)

A

200 KIAS

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24
Q

AIRSPEEDS
(VFE4)

A

180 KIAS

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25
Q

AIRSPEEDS
(VFE5)

A

180 KIAS

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26
Q

AIRSPEEDS
(VFEFULL)

A

165 KIAS

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27
Q

AIRSPEEDS
(Max Turbulent Airspeed Below 10,000’)

A

250 KIAS

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28
Q

AIRSPEEDS
(Max Turbulent Airspeed 10,000’ & Above)

A

270 KIAS or .76M

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29
Q

AIRSPEEDS
(Max Crosswind for Takeoff)

A

Dry: 35 kts
Wet: 30 kts

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30
Q

AIRSPEEDS
(Max Crosswind for Landing)

A

See AOM 1 Limitations

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31
Q

AIRSPEEDS
(Max Tailwind)

A

10 KT

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32
Q

AIRSPEEDS
(Max Headwind for CAT II Operations)

A

25 KT

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33
Q

AIRSPEEDS
(Max Crosswind for Landing <RVR 4000 or 3/4)

A

15 KT

34
Q

AIRSPEEDS
(Max DV Window Operation)

A

160 KIAS

35
Q

AIRSPEEDS
(Max Tire Speed)

A

195 KIAS

36
Q

AIRSPEEDS
(Max Windshield Wiper Speed)

A

250 KIAS

37
Q

ALTITUDES
(Max Operating Altitude)

A

41,000’

38
Q

ALTITUDES
(Max Flaps Extended Altitude)

A

20,000’

39
Q

ALTITUDES
(Max Takeoff & Landing Altitude)

A

10,000’

40
Q

ALTITUDES
(Min Takeoff & Landing Altitude)

A

-1,000’

41
Q

When is takeoff not authorized without further maintenance inspection?

A

In the event of landing below -40°C.

42
Q

TEMPERATURES
(Min/Max Takeoff & Landing Temperature (SAT))

A

-40°/54°C

43
Q

ALTITUDES
(Max Altitude Display Difference in Flight for RVSM)

A

180 ft

44
Q

APU
(Name/Model)

A

Sundstrand APS 2300

45
Q

APU
(1st & 2nd Start Attempts)

A

START/ON then 60 Seconds OFF

46
Q

APU
(3rd Start Attempt)

A

START/ON then 5 Minutes OFF

47
Q

APU
(Minimum Starting Temperature)

A

-54°C

48
Q

APU
(Maximum Operation Temperature)

A

ISA +39°C
(Supplemental Information Applicable >ISA +35°C)

49
Q

APU
(EGT Start)

A

1032°C

50
Q

APU
(EGT Continuous)

A

717°C

NOTE: No time limit in amber on ground/inflight between 662-717°C.

51
Q

APU
(Maximum Rotor Speed)

A

108%

52
Q

APU
(Maximum Altitudes)

A

Electrical: 33,000’
Starting: 30,000’
Engine Start Assist: 21,000’
ECS Bleed: 15,000’

53
Q

AUTOPILOT
(Minimum Engagement Altitude for Takeoff/Go-Around)

A

Above 400’

54
Q

AUTOPILOT
(Minimum Engagement Altitude during Landing)

A

Above 50’

55
Q

ENGINE
(Make/Model)

A

GE CF34-8E5

56
Q

ENGINE
(N1 RPM Max)

A

99.5%

57
Q

ENGINE
(N2 RPM Max)

A

99.4%

58
Q

ENGINE
(Max Start ITT)

A

815°C

59
Q

ENGINE
(Max Normal T/O ITT)

A

965°C (2 Minutes)
949°C (3 Minutes)
[Total 5 Minutes]

60
Q

ENGINE
(Max T/O & G/A ITT)

A

1006°C (2 Minutes)
990°C (3 Minutes)
[5 Minutes Total]

61
Q

ENGINE
(Max Continuous ITT)

A

960°C

62
Q

ENGINE
(Min/Max Oil Pressure)

A

25 PSI / 95 PSI

63
Q

ENGINE
(Continuous Oil Temperature)

A

155°C

64
Q

ENGINE
(Transient Oil Temperature)

A

163°C
(15 Minute Limit)

65
Q

ENGINE THRUST
(T/O-1)

A

13,000 lbs / ATTCS = 14,200 lbs

66
Q

ENGINE THRUST
(T/O-2)

A

11,800 lbs / ATTCS = 13,000 lbs

67
Q

FUEL
(Brazilian)

A

QAV1

68
Q

FUEL
(ASTM)

A

Jet A or A1

69
Q

FUEL
(American)

A

JP8

70
Q

FUEL
(Maximum Capacity)

A

20,934 lbs
(10,467 lbs / Tank)

71
Q

FUEL
(Maximum Useable)

A

20,784 lbs
(10,392 lbs / Tank)

72
Q

FUEL
(Unusable)

A

150 lbs
(75 lbs / Tank)

73
Q

FUEL
(Maximum Imbalance)

A

794 lbs

74
Q

FUEL
(Weights determined based on what standard fuel density?)

A

6.767 lbs : US Gallon

75
Q

FUEL
(Minimum Fuel Tank Temperature)

A

-37°C

76
Q

FUEL
(Cross-feed Operation)

A

OFF for Takeoff and Landing

77
Q

STARTER
(Starting Engines: 1st & 2nd Start)

A

GND 90 sec START / 10 sec cool-down
FLT 120 sec START / 10 sec cool-down

78
Q

STARTER
(Starting Engines: 3rd - 5th Start)

A

GND 90 sec START / 5 sec cool-down
FLT 120 sec START / 5 sec cool-down

79
Q

STARTER
(Dry Motoring)

A

1st Dry Motor: Max 90 sec / 5 min cool-down

2nd-5th Dry Motor: Max 30 sec / 5 min cool-down

80
Q

STARTER
(When may the 5 sequential dry motoring cycles be repeated?)

A

Following a 15 min cool-down period.

EMB175 STUDY GUIDE ITEMS (2 decks)

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