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E175 > Aircraft Limitations > Flashcards

Aircraft Limitations Flashcards

1
Q

Max Ramp Weight

A

85,870

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2
Q

Max Takeoff Weight

A

85,517

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3
Q

Max Landing Weight

A

74,957

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4
Q

Max Zero Fuel Weight

A

69,886

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5
Q

Max Tailwind Component

A

10 kits

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6
Q

Max runway slope

A

+/-2%

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7
Q

Max Operating Altitude

A

41,000 feet

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8
Q

Max T/O and Landing Altitude

A

8,000 Feet

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9
Q

Min T/O and Landing Altitude

A

-1,000 feet

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10
Q

Max Ambient Air Temp for t/o and landing

A

52 degrees C

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11
Q

Max Flap extension Altitude

A

20,000 feet

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12
Q

Min ambient temp for takeoff

A

-40 degrees C (SAT)

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13
Q

Min temp for operation

A

-54 degrees C

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14
Q

Max operating speed (VMO)

A

Up to 8000’……300 KIAS
8000’ to 10,000’…..300-320 KIAS (increases linearly)
10,000 to FL290….. 320 KIAS (VMO)
FL290 to FL410…… .82M (MMO)

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15
Q

Max Operating Mach Number

A

.82M (MMO)

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16
Q

Max RAT operating Speed

A

VMO/MMO

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17
Q

Turbulent Airspeed

A

Below 10,000’ …..250 KIAS

At or Above 10,000’ …….270 KIAS/.76M

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18
Q

Max Tire Limit Ground Speed

A

195 Kts

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19
Q

Max Wiper Operation Speed

A

253 KIAS

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20
Q

Max Gear speed

A

Extension(VLOE)….250 KIAS
Extended (VLE)…..250 KIAS
Retraction (VLOR)…..250 KIAS

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21
Q

Flap Operating Speed (1,2,3,4,5,Full)

A

1…….230 KIAS
2…….215 KIAS
3…….200 KIAS
4…….180 KIAS
5…….180 KIAS
FULL…..165 KAIS

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22
Q

Max Fuel Capacity

A

20,935# (10392.5# or 1535.5 U.S. gal per tank)

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23
Q

Unusable Quantity per Tank

A

75 lbs/tank

24
Q

Max Fuel imbalance

A

794 lbs

25
Q

Min Fuel Temp

A

-40 degrees C

26
Q

Max Pressure differential Pressure

A

Up to 37,000’…….7.80 psi

Above 37,000’…….8.34 psi

27
Q

Max Differential Overpressure

A

8.77 psi

28
Q

Max Differential Negative Pressure

A

-0.5 psi

29
Q

Max Differential Pressure for T/O. and Landing

A

0.2 psi

30
Q

Max Single PACK operation

A

FL310

31
Q

Max N1

A

99.5%

32
Q

Max N2

A

99.4%

33
Q

Min N2

A

58.5%

34
Q

ITT Parameters (temps)

A

Start….815 degrees C
Max TOGA……990 degrees C
Max Cont……960 degrees C

35
Q

Max Oil Pressure

A

95 psi

36
Q

Min Oil pressure

A

25 psi

37
Q

Max Continuous Oil Temp

A

155 degrees C

38
Q

Max Transient Oil Temp

A

163 degrees C

39
Q

Engine Cycle Limitations

A

1-2 attempts…..90 sec ON/10 sec OFF
3-5 attempts….. 90 sec ON/5 min OFF

120 sec ON in flight

40
Q

Dry motoring duty cycle limits

A

1 attempt…….90 sec ON/5 min OFF
2-5 attempts…..30 sec ON/ 5 min OFF *

  • After 5 sequential motorings, cycle may be repeated after a 15 min cool down
41
Q

APU starter Duty Cycle

A

1-2 attempts……1 min ON/1 min OFF

3 attempts……1 min ON/5 min OFF

42
Q

Min APU Start temp

A

-54 degrees C

43
Q

Max APU start Altitude

A

30,000’

44
Q

Max APU operating altitude

A

33,000’

45
Q

Max APU electrical gen altitude

A

33,000’

46
Q

Max APU bleed air altitude

A

15,000’

47
Q

Max APU engine start assist altitude

A

21,000’

48
Q

Max APU rotor speed

A

108%

49
Q

Max APU EGT

A

Start…..1032 degrees C

Continuous…..717 degrees C

50
Q

Types of Operations

A

Visual (VFR)
Instrument (IFR)
Icing Conditions
Cat I and II

51
Q

Max forward cargo weight?

A

3306 lbs

Heated and Ventilated

52
Q

Aft Cargo limit?

A

2535 lbs

53
Q

Max thrust?

A

14,200 lbs of thrust

54
Q

Nose wheel steering limit? (In degrees)

A

76 degrees each way

55
Q

Crosswind recommended speeds?

A 
38 kts - Dry
31 kts - Wet
20 kts - dry snow
18 kts - Slush
12 kts - Ice

E175 (17 decks)

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