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E-175 > Limitations > Flashcards

Limitations Flashcards

1
Q

Takeoff Weight Limiting Factors

A

Weight at brake release or start of T/O roll is limited by the most restrictive of the following:

  • Maximum certificates takeoff weight
  • Maximum runway limited takeoff weight
  • Tire speed and break energy limits weights
  • Maximum takeoff weight (climb limited)
  • Obstacle clearance, enroute, and landing weight limitations
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2
Q

Landing Weight Limiting Factors

A

The most restrictive of the following, incl. limitations for INOP EQP:

  • Maximum certificated landing weight
  • Maximum landing weight (runway length plus obstacle)
  • Maximum landing weight (climb limited)
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3
Q

Maximum Taxi & Ramp Weight

A

85,800

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4
Q

Maximum Takeoff (MTOW) Weight

A

85,500

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5
Q

Maximum Landing (MLW) Weight

A

74,900

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6
Q

Maximum Zero Fuel (MZFW) Weight

A

69,800

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7
Q

Maximum Forward Cargo (F1) Weight

A

3,306

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8
Q

Maximum Aft Cargo (R1) Weight

A

2,535

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9
Q

Note Overweight landing

A

Perform an “overweight landing” when a condition causes it to be safer to land overweight than to continue flight until at or below maximum certificated landing weight. QRH for procedure

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10
Q

Winds and altitudes are predicated on what?

A

Peak gust value & pressure altitude

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11
Q

Minimum Flight Crew

A

Pilot and Copilot

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12
Q

Max crosswind for takeoff and landing (Dry)

A

35knot

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13
Q

Max crosswind for takeoff and landing (Wet)

A

30knots

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14
Q

Maximum headwind for CatII approaches

A

25knots

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15
Q

Max crosswind for landing Vis

A

15kts

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16
Q

Max tailwind for takeoff and landing

A

10kts

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17
Q

Max runway slope

A

+2% , -2%

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18
Q

Flap maneuvering load acceleration limit

A

Up -1 to +2.5

Down 0 to +2.0. (Flap 1 - Full)

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19
Q

Max Operating Alt.

A

41,000

20
Q

Max takeoff and landing altitude

A

8,000

21
Q

Max SAT for takeoff, landing and ground start

A

52C

22
Q

Max altitude with flap extended

A

20,000

23
Q

Max flight operating altitude

A

78 North

78 South

24
Q

Min SAT for takeoff, landing and ground start

A

-40C

Note* In the event of landing below -40C, the airplane may not takeoff without further maintenance inspection.

25
Q

Minimum Operating Limit Speed.

A

Intentional speed reduction below the onset of stall warning, as defined by stick shaker operation, is prohibited unless a lower speed is specifically authorized for flight test or training operations.

26
Q

Operational Envelope

A

In the event of a landing below -40C, the airplane may not takeoff without further maintenance inspection.

27
Q

Speed Limits WARNING

A

Maximum operating limits speeds(Vmo/Mmo) shall NOT be deliberately exceeded in any regime of flight.

28
Q

Vmo

A

320

29
Q

Mmo

A

.82

30
Q

Maximum airspeed for RAT ops.

A

Vmo/Mmo

31
Q

Turbulent airspeed below 10,000 feet

A

250kts

32
Q

Turbulent airspeed at or above 10,000feet

A

270kts/.76M

33
Q

Tire limit ground speed

A

195kts

34
Q

Max airspeed for windshield ops.

A

250kts.

35
Q

Max airspeed for windshield wiper ops failed in non-parked

A

320kts

36
Q

Max airspeed to open flight deck window

A

160kts

37
Q

Max gear extension speed Vlo

A

250kts

38
Q

Max gear extended speed Vle

A

250kts

39
Q

Max gear retraction speed Vlo

A

250kts

40
Q

Max flap 1

A

230kts

41
Q

Max flap 2

A

215kts

42
Q

Max flap 3

A

200kts

43
Q

Max flap 4

A

180kts

44
Q

Max flap 5

A

180kts

45
Q

Max flap Full

A

165kts

46
Q

Minimum Control Speed

A

Refer to QRH

47
Q

Designed Maneuvering Speed

A

Full application of rudder and aileron controls, as well as maneuvers that involve angles of attack near the stall, must be confined to speeds at or below 240kts

E-175 (1 decks)

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