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EC130 B4/T2 > Emergency Procedures > Flashcards

Emergency Procedures Flashcards

1
Q

Engine Flame out

A

Autorotation Procedure:
Collective — Reduce NR green
IAS — Vy

If relighting impossible/after tail rotor:
Twist grip — idle detent

At height ~ 70’
Cyclic flare

20/25 ft
Collective pitch — Gradually increase
Cyclic — Forward to slightly nose up landing
Pedal — Adjust for trim
Collective pitch — increase to cushion landing

After touch-down
Cyclic, collective, pedal — Adjust to control ground run

On aircraft stopped
Collective — Down
Rotor brake — apply

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2
Q

In Flight Relighting

A

Starting selector — Off
Fuel pump — On
Starting selector — On

After relighting
Fuel P — Off

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3
Q

Engine Flame Out — IGE

A

Collective — Maintain
Pedals — Yaw
Collective — Increase to cushion landing

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4
Q

Engine Flame Out — OGE

A

Collective pitch — Full down
Cyclic — forward to regain airspeed
Autorotation

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5
Q

Tail rotor failure — IGE

A

Land immediately
Twist Grip — Idle
Collective — increase to cushion landing

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6
Q

Tail Rotor Failure — OGE

A

Collective — Reduce
Cyclic — Forward to gain speed
Cyclic — Adjust IAS to Vy

Land as soon as possible

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7
Q

Tail Rotor Failure — Cruise

A

Cyclic — Adjust IAS TO Vy
Collective — Reduce to control sideslip
Land as soon as possible

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8
Q

Smoke in cockpit — source not IDd

A

Hearing/Demisting — Off

Smoke clears:
Continue Flight

Smoke does not clear:
  Master Sw / Emer SW — Shut off
  Direct Batt — Off
  Ext Pwr — Off
  Gene — Off
  Avionics — Off
  Ventilate the Cabin
  All consumers — Off
  Master Sw — On
  Ext Pwr — On
  Dir Bat — On
  Gene — On

If DC parameter correct / no smoke detected
Avionics — On
All consumers — On

If DC parameters is not correct
Gene — Off
Unnecessary equip — Off
Land as soon as practicable

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9
Q

Smoke in cockpit — source identified

A

Corresponding system — Off
Ventilate the cabin

Continue flight depending on system failed

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10
Q

VEMD Screen Failure — 1 screen

A

Failed screen — Off

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11
Q

VEMD Screen Failure — both screen

A

Avoid power overlimit, maximum power to establish level flight

IAS = 100 kts - (2 KTS / 1000 ft)

Land as soon as practicable / no hover landing

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12
Q

Abnormal NR indication

A

Collective — maintain TRQ > 10%

NR reading is given by Nf pointer

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13
Q

Abnormal Nf indication

A

NR Guage — CHECK in green /w

TRQ > 0

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14
Q

Engine Oil Temp > 115°C

A

Airspeed — 80 KTS

TEMP Reduces
Land as soon as practicable

TEMP does not reduce
Land as soon as possible
Check cooler fan operation

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15
Q

Low Engine Oil Press

A

Check ENG P

If lit
Land Immediately

If not lit
CWP Test
If working,
LAND AS SOON AS PRACTICABLE

If not working,
  LAND IMMEDIATELY
    Auto rotation / Shutdown engine
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16
Q

Loss of NG Indicator

A

Respect
maximum TRQ
T4 < 810°C

LAND AS SOON AS PRACTICABLE

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17
Q

Loss of TRQ Indicator

A

Respect the Ng on Table

LAND AS SOON AS PRACTICABLE

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18
Q

Loss of NG and TRQ indications

A

GOV warning can also cause loss of NG/TRQ

Comply with Ng Limit Table
Substitute Delta -4 with 810*C

LAND AS SOON AS PRACTICABLE

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19
Q

Loss of T4 Indicator

A

Respect Ng / TRQ

ON GROUND - Don’t start

LAND AS SOON AS PRACTICABLE

20
Q

Engine Fire — Startup

A 
Start selector — Off
Emergency Fuel Shutoff — AFT
Booster Pump — Off
Crank — 10 Secs
Master SW — Off
Rotor Brake — Apply
Evacuate aircraft
21
Q

Engine Fire — Hover/Takeoff/Final

A 
No Hover, powered landing
Start selector — Off
Emergency Fuel Shutoff — AFT
Booster Pump — Off
Crank — 10 Secs
Master SW — Off
Rotor Brake — Apply
Evacuate aircraft
22
Q

Engine Fire — In Flight

A 
Collective — Reduce Pitch
IAS — Vy
Autorotation — Apply
Emerg Fuel Shutoff — Aft
Start selector — Off

After landing
Master Sw — OFF
Rotor brake — Apply
Evacuate Aircraft

23
Q

Red Gov Light — In Flight

A 
Ensure — EBCAU engaged (Amber Gov)
Collective pitch — avoid abrupt 
  changes
  Maintain Ng > 80% below 20000’
  Maintain Ng > 85% above 20000’

LAND AS SOON AS PRACTICABLE

Powered approach / Avoid steep
Slowly lower collective
Start selector Off

24
Q

Red Gov Light — Startup

A

Start selector — Off

25
Q

Permanent Amber Gov — In Flight

A

Collective — avoid abrupt power
changes
IAS — maintain below power off Vne

LAND AS SOON AS PRACTICABLE

26
Q

Permanent Amber Gov — Ground

A

Ground: Do not start

Start up: abort

27
Q

Eng P

A

Oil Pres Guage — check

Low or nil
Land immediately
Autorotate
Shutdown engine

Normal
Land as soon as practicable

28
Q

TWT GRIP

A

Twist Grip — increase to Flight gate

29
Q

Engine Chip

A

Collective — Reduce Power

Land as soon as possible

Low power approach / be prepared for eng loss

30
Q

MGB P

A

Collective — Reduce Power

Land as soon as possible

31
Q

MGB Temp

A

IAS — Vy
CWP — check MGP P

IF MGB TEMP
LAND AS SOON AS POSSIBLE

IF NO MGB TEMP
LAND AS SOON AS PRACTICABLE

32
Q

MGB chip

A

Collective — reduce power
MGB P / MGB Temp — Monitor

Land as soon as possible.

33
Q

TGB CHIP

A

Avoid prolonged hovering

CONTINUE FLIGHT

34
Q

HYDR + SERVO

A

Keep aircraft more or less level
IAS — < 110 KTS / VNE
Normal Approach / Landing

LAND AS SOON AS PRACTICABLE

35
Q

SERVO

A

Land as soon as practicable

36
Q

BATT

A

Ext Pwr — check on

If on,
VEMD — check voltage
Land as soon as practicable

If off,
Ext Pwr — On
Continue Flight

37
Q

GENE

A

U bus on VEMD — Check
GENE — Check On

If on,
GENE RST — press
If fixed, Continue Flight

If off,
Unnecessary Equip — Off
Land as soon as practicable

38
Q

Fuel

A

Land as soon as possible

15 mins at MCP

39
Q

Fuel P

A

Collective pitch — Reduce Power
Booster pump — On

Land as soon as possible

Low power approach and landing
Prepare for engine flame out

40
Q

Fuel Filt

A

Collective — Reduce Power

If light goes out,
Continue flight at reduced power
Land as soon as practicable

If light does not go out,
Land as soon as possible

Monitor Ng
If Ng oscillates
Land Immediately
Apply Autorotation

41
Q

Pitot

A

Pitot — check on

If yes,
Monitor airspeed Indicator

If no,
Turn on

Continue Flight

42
Q

HORN

A

Horn — Check On

If yes,
Aural warning failure

If no,
Turn it on

CONTINUE FLIGHT

43
Q

Door

A

IAS — 70 KTS

LAND AS SOON AS PRACTICABLE

Descent/Approach at low sink rate

44
Q

Limit

A

In high speed cruise
Collective — reduce power
Cyclic — reduce speed

In rearward Flight / Hover in tailwind
Cyclic — reduce rear speed / tailwind

CONTINUE FLIGHT

45
Q

Bleed valve

A

Land as soon as practicable

Should open at shutdown
Check GOV fuse on 30A — Do not start

If flag doesn’t appear at low power setting,
Engine surge
Avoid abrupt changes in power

LAND AS SOON AS PRACTICABLE

EC130 B4/T2 (3 decks)

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