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ATR42/72 320 > Speed, W&B and Loading Limitations > Flashcards

Speed, W&B and Loading Limitations Flashcards

1
Q

What is the MRW Maximum Ramp or Taxi weight?

A

37,632lb (17,070kg)

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2
Q

What is the TOW Maximum Takeoff weight?

A

37,258lb (16,900kg)

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3
Q

What is the MLW Maximum Landing weight?

A

36,155lb (16,400kg)

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4
Q

What is the MZFW Maximum Zero Fuel weight?

A

34,259lb (15,540kg)

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5
Q

How is the Center of Gravity measured? What are the considerations?

A

The limits of the center of gravity are given in percentage of the mean aerodynamic chord (MAC), taking into consideration the landing gear extended.

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6
Q

What is the distance from the reference point DATUM to the reference chord leading edge?

A

The distance from the reference point DATUM to the reference chord leading edge is 11.425 meters (449.8 inches).

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7
Q

What is the MAC distance on the ATR42-320?

A

In the ATR42-320 the MAC is 2.285m long (89.96 inches).

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8
Q

Standard Mass for Crew Members Weight according to ATR

A

For the ATR 42-320 the standard mass for each flight crewmember is 85 kg (187.4 lb) and for each cabin crewmember 75 kg (165.3 lb).

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9
Q

Standard Mass for Pax Weight according to ATR

A
  • 84 kg (185.2 lb) for all flights, except holiday charters
  • 76 (167.6 lb) kg for holiday charters
    and
  • 35 kg (77.2 lb) for children.
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10
Q

What is the Fuel Capacity for ATR42-320?

A

4,960lb per tank being
9,920lb Total

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11
Q

There are 2 forward cargo compartments. How much weight can each one hold?

A

1058lbs each (2116lbs total)

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12
Q

There are 2 sections on the aft compartment. The forward-aft compartment has a maximum capacity of?

A

560Lbs

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13
Q

There are 2 sections on the aft compartment. The aft-aft compartment has a maximum capacity of?

A

983Lbs

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14
Q

VMO and MMO for 320?

A

250 KIAS 0.55M

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15
Q

Va Manouvering Speed?

A

160 KIAS

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16
Q

Flaps 15 Speed Limitation?

A

170 KIAS

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17
Q

Flaps 30 Speed Limitation?

A

150 KIAS

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18
Q

Flaps 45 Speed Limitation?

A

130 KIAS (Emergency Only)

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19
Q

VLE and VLO

A

VLE 170 KIAS and VLO 160 KIAS

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20
Q

Max “Rough Air Speed” Turbulence Penetration speed “Vra”?

A

180 KIAS

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21
Q

Max Wipers Operation Speed?

22
Q

Max Tire Speed?

A

165 KIAS (Ground Only)

23
Q

Max G Force load in general, flaps and gear extended too?

A

+2.5G and -1G “ Flaps Extended or Landing Gear Extended 2.0G both”

24
Q

VMCL Speed? “Lower speed in Landing Config”

A

Flaps 15 = 91 KIAS Flaps 30 = 89 KIAS

25
Q

Takeoff and Landing Tail Wind limitation?

26
Q

Maximum Cross-wind in takeoff and landing?

A

Takeoff 45kt Landing 38kt

27
Q

Refueling Max Pressure in PSI?

28
Q

Max Fuel Imbalance on both tanks?

29
Q

Minimum Height for AP engagement?

30
Q

Minimum Height for using AP and YD except for Takeoff, Go-around and Approach?

31
Q

VS and IAS use Altitude Limitation during approach?

32
Q

CAT 1 Approach mode Altitude Limitation during approach?

33
Q

Which engine on the ATR42-320 is the critical engine?

A

Left Engine

34
Q

What is the VMCG and VMCA?

A

It’s not a fixed speed. Must be calculated

35
Q

What is VMCL? What is the procedure? What is the speed for Flaps 15 and 30?

A

VMCL is the Minimum Control Speed During Approach and Landing. On VMCL to start a turn into the good engine you need at least 20° bank angle and it takes approximately 5 seconds to start turning. VMCL Flaps 15 = 91kt VMCL Flaps 30 = 89Kts

36
Q

What is the VMLB Minimum Maneuvering Speed Low Bank? What is the bug colour on the ASI?

A

Limited Bank Angle of 15° for a certain speed according to the current aircraft weight.
This one is set on the White Bug

37
Q

What is VGA speed?

A

Minimum speed to perform maneuvering during a go-around maneuvering
VGA = VmHB + 5kt or 1.1 x VMCA whichever is higher

38
Q

What is the Vapp?

A

Final Approach speed in landing configuration + Winds correction speed

39
Q

What is Vref?

A

Referencia Landing Speed
Consider Landing Configuration, Gear Down + Flaps 30° at Final Approach.

40
Q

What is the appropriate NP Propeller setting during the Climb phase?

A

Set 86.3NP initially. When TQR reduces below 75%, set 77.3NP

41
Q

About Max Torque calculation, which phases are mandatory to calculate max torque?

A

Takeoff and Go-around. The other phases we just calculate to cross-check if FDAU is working properly.

42
Q

Which are the temperatures considered Atmospheric Icing Conditions?

A

On Ground = OAT +5 or below with visible moisture
In-flight = TAT +7 or below with visible moisture

43
Q

Which are the temperatures and conditions considered Ground Icing Conditions?

A

OAT +5 or below with Standing water, Snow, Rain, or Slush when operating on TWY, RWY, or Ramp.

44
Q

What is Decelerating Height? How is the calculation?

A

Altitude to start decelerating from 240Kts to VAPP
86NP = IAS x 10
77NP = IAS x 10 + 500
Ex: If I`m at 240kt and 86NP:
240 x 10 = 2400ft (This is the altitude to start decelerating to the VAPP.

45
Q

What is the Max Demonstrated Xwind for Take Off, and for Landing using Flaps 30 and 45?

A

Takeoff = 45kt Landing Flaps 30 = 38kt Landing Flaps 45 = 20kt

46
Q

For Go-around bleeds must be?

47
Q

Max slope allowed for ATR operations?

48
Q

What is the Dispatch Considerations for operation limitation with Landing Gear down the whole flight?

A

86%NP FL160 160KIAS

49
Q

Can the airplane be dispatched to operate with flaps up?

A

Yes, unless the airplane will encounter Ice on the route. However, it causes a huge loss in performance

50
Q

What is the PL angle where we can`t reduce more before feathering the bad engine in case of engine failure?

A

48 degrees on the PL

51
Q

Holding speed?

A

160Kts Clean

ATR42/72 320 (5 decks)

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