H125 Emergencies Flashcards

1
Q

Which warnings are shown in case of an engine failure?

A

ENG P, GEN, Fuel P

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2
Q

ENG FIRE

Indication?

Actions?

A

Indications:

GONG

ENG FIRE => red

Actions:

AR / Check RPM / 65 KIAS

Engine shut-down

Fuel valve => off

GEN off

Master SW off

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3
Q

AR speed?

A

65 KIAS

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4
Q

Main rotor speed => power off?

A

320-430 RPM

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5
Q

How do you recognize a complete loss of tailrotor thrust?

A

Left yaw

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6
Q

Loss of tailrotor control

How do you recognize a loss of tailrotor control?

A

Pedals jammed, loss of pedal effectiveness.

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7
Q

What are two factors to consider while having a loss of tailrotor control?

(clockwise turning helicopter)

A
  • RH wind is favourable
  • Below 20 KIAS => no go-around possible due to loss of tailrotor fin effect
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8
Q

Procedure for loss of tailrotor control?

A
  1. Reduce speed to 70 KIAS
  2. Accu TEST: ON
  3. Accu TEST: OFF (after 5 seconds)
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9
Q

Tail Rotor Failures

Complete loss of tailrotor thrust

Hover IGE => Procedure?

A
  • Land immediately
    1. Twist grip => IDLE
    2. Collective => Increase to cushion landing
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10
Q

VNE power-off?

A

125 KIAS

(-3KIAS / 1000ft)

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11
Q

VEMD failure => both screens => procedure?

A

Failure of both screens To avoid any power overlimit, the maximum authorized power will be the power needed to establish level flight with the following law:

IAS kt = 100 kt at 0 Hp - (2 kt /1000 ft).

IAS km/h = 185 km/h at 0 Hp - (4 km/h per 300 m).

LAND AS SOON AS PRACTICABLE

Landing procedure: carry out a no hover landing. NR is constant at 394 rpm.

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