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EC130 135 Checkride Study > EC130 B4 Emergency Procedures > Flashcards

EC130 B4 Emergency Procedures Flashcards

1
Q

Land immediately

A

Self explanatory. Land even if not completely safe to do so.

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2
Q

Land as soon as possible

A

Urgent. Land at nearest landing site at which a safe landing can be made.

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3
Q

Land as soon as practicable

A

Less urgent. At pilot’s judgement, proceed to nearest airfield where he can expect appropriate assistance.

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4
Q

Continue flight

A

Continue flight as planned. Repair at destination.

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5
Q

Continuous tone

A

310hz tone when NR below 360 rpm
285hz tone when max takeoff is exceeded or about to be exceeded

Collective - REDUCE
Engine parameters - CHECK

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6
Q

Intermittent Tone

A

310hz intermittent tone when NR above 410 rpm

Collective - INCREASE to maintain normal operating NR

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7
Q

Engine Flame Out in Cruise Flight (over land)

A
  1. Collective - REDUCE to maintain normal NR
  2. IAS - Vy

If relighting impossible or after loss of TR thrust:
3. Twist grip - IDLE
4. Maneuver aircraft into the wind in final approach

At 70 feet AGL:
5. Cyclic - FLARE

At 20-25 feet and at constant attitude:
5. COLLECTIVE - GRADUALLY INCREASE to reduce rate of descent and forward speed
7. CYCLIC - FORWARD for lightly nose up landing attitude (under 10 deg)
8. PEDALS - ADJUST to counter sideslip tendency
9. COLLECTIVE - INCREASE to cushion touchdown

After touchdown:
10. CYCLIC COLLECTIVE PEDALS - ADJUST to control ground run

Once aircraft has stopped:
11. COLLECTIVE - FULL DOWN
12. ROTOR BRAKE - APPLY below 170 Nr

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8
Q

Autorotation Over Water

A

Apply same procedure as over land, except items 10, 11 and 12, but maneuver to head the aircraft equally between the wind and wave direction on final approach. Ditch with minimum forward speed (IAS < 30 kt (56 km/h)) and rate of descent. Then apply
following check- list for items 10, 11, 12.

After touch-down
10. Collective - MAINTAIN
11. Forward doors emergency
handles - PULL-UP
12. Doors - JETTISON or OPEN
13. Rotor brake - APPLY
Abandon aircraft once the rotor has stopped.

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9
Q

Engine Flame Out in a Hover

A
  1. Collective - MAINTAIN
  2. Pedals - CONTROL YAW
  3. Collective - INCREASE as needed to cushion touch-down
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10
Q

Engine Flame-out Hover OGE

A
  1. Collective - FULL LOW PITCH
  • When NR stops decreasing
    2. Cyclic - FORWARD to gain airspeed according to available height
    3. Autorotation procedure - APPLY
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11
Q

In-Flight Relighting

A

According to available height and cause of flame-out:

  1. FUEL PUMP or FUEL P - ON
  2. Engine starting selector - OFF position
  3. Engine starting selector -ON position
    The relighting sequence will therefore be automatically carried out as soon as Ng < 17 %.
  • After relighting procedure
  1. FUEL PUMP or FUEL P - OFF

At least 1000 ft (300 m) are necessary to complete relighting procedure after flame-out.

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12
Q

Loss of Tail Rotor Thrust - Hover IGE (or OGE within H/V diagram)

A

LAND IMMEDIATELY

  1. Twist Grip - IDLE position
  2. Collective - INCREASE to cushion touch-down
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13
Q

Loss of Tail Rotor Thrust - Hover OGE (Clear area out of H/V diagram)

A

Simultaneously,

  1. Collective - REDUCE depending on available
    height
  2. Cyclic - FORWARD to gain speed
  3. Airspeed - MAINTAIN Vy or higher
  4. Collective - ADJUST to obtain minimum
    sideslip angle

LAND AS SOON AS POSSIBLE

If a go-around has been performed, carry out an autorotative landing on a suitable area as landing procedure.

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14
Q

Loss of Tail Rotor Thrust in Cruise Flight

A
  1. Airspeed - MAINTAIN Vy or higher
  2. Collective - ADJUST to obtain minimum sideslip angle

LAND AS SOON AS POSSIBLE

APPROACH AND LANDING
On a suitable area for autorotative landing:

  1. Twist grip - IDLE position
  2. Carry out an autorotative landing according to the autorotation procedure
    (Refer to SECTION 3.2 § 1).
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15
Q

Loss of Tail Rotor Control (jammed pedals)

A

Symptom: Jamming of pedals or loss of pedal effectiveness. These conditions make it impossible to change tail rotor thrust with the pedals.

WARNING:

LANDING IS MADE EASIER WITH A RH WIND COMPONENT.
WHEN AIRSPEED IS LESS THAN 20 KT (37 KM/H), GO-AROUND IS IMPOSSIBLE DUE TO LOSS OF VERTICAL FIN EFFICIENCY.

  1. Cyclic and collective - ADJUST to set IAS to 70 kt
    (130 km/h) in level flight

On a suitable area for a running landing procedure:
Make a shallow approach with a slight left sideslip. Perform a running landing. The sideslip will be reduced progressively as airspeed is reduced and collective is applied to
cushion the landing.

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16
Q

Smoke in the Cabin

A

SOURCE NOT IDENTIFIED:

Heating, Demisting - OFF

Smoke clears?

Yes - CONTINUE FLIGHT

No:
1. Master/Emer sw - OFF
2. DCT Batt - OFF
3. EXTPWR BATT/BATT EPU - OFF
4. GENE - OFF
5. Master Avionic - OFF
6. Ventilate cabin
WHEN SMOKE CLEARS
7. All consumers - OFF
8. Master - ON
9. DCT Batt - ON
10. EXT PWR Batt - ON
11. Gene - ON (Check DC parameters)

Smoke clears?

Yes?
(DC parameters correct)
12. Master Avionic - ON
13. Minimum required consumers - ON (one by one)
CONTINUE FLIGHT

(DC parameters not correct)
12. Gene - OFF
13. Apply case A of Gene DC generator off line procedure

NO?
LAND AS SOON AS POSSIBLE

(Apply VEMD dual screen failure procedure if necessary)
(GOV light will remain on after cycling power)

SOURCE IDENTIFIED:

Corresponding system - OFF
CONTINUE FLIGHT

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17
Q

VEMD Screen Failures

A

FAILURE OF ONE SCREEN:

Off1 or Off2 - OFF
Read available information on other screen
(TQ AND NG will be offline)

FAILURE OF BOTH SCREENS:

Establish maximum authorized power for level flight at:
100 KIAS (-2kt/1000’)

LAND AS SOON AS PRACTICABLE

Carry out a no-hover landing

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18
Q

[OVERLIMIT DETECTED]

A

CONTINUE FLIGHT

Address the overlimit at destination

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19
Q

NR Indication Failure

A

Collective - Maintain TQ over 10%

NR reading is given by NF pointer

LAND AS SOON AS PRACTICABLE

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20
Q

NF Indication Failure

A

NR indication: Check in normal operating range with TQ>0

CONTINUE FLIGHT

(NF can be read on VEMD: [select] the [+] multiple times to view)

(EBCAU may not be available after NF failure)

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21
Q

High Engine Oil Temperature

A

Engine Oil Temperature over 115 C:

Airspeed - SET to 80 KIAS

Temperature reduces?

Yes - LAND AS SOON AS PRACTICABLE (check cooler fan operation)

No - LAND AS SOON AS POSSIBLE

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22
Q

Low Engine Oil Pressure

A

[ENG P] light on?

YES - LAND IMMEDIATELY
Apply autorotation procedure and shut down engine if time permits

NO:

CWP light test to verify [ENG P] light working

If light is NOT burnt out then LAND AS SOON AS PRACTICABLE

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23
Q

Loss of NG, TQ, or T4 parameters

A

FLI disables
3 data page displayed along with a failure message

LAND AS SOON AS PRACTICABLE

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24
Q

NG/Delta NG Failure

A

Comply with maximum TQ and T4 limits.

T4 limitations displayed are starting limitations. Ignore overlimit if T4 remains within flight limitations

LAND AS SOON AS PRACTICABLE

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25
Q

Torquemeter Failure

A

Comply with NG table

Usually NG ~93/94

LAND AS SOON AS PRACTICABLE

26
Q

Delta NG AND Torquemeter failure

A

Use T4 and numeric NG and comply with NG table (usually ~93 NG)

LAND AS SOON AS PRACTICABLE

27
Q

T4 Indication Failure

A

Comply with NG and TQ limitations.

LAND AS SOON AS PRACTICABLE

Do not start engine without T4 indications

28
Q

Over Voltage of the Generator >31.5V

A

[GENE] - OFF
Apply GENE procedure case A

LAND AS SOON AS PRACTICABLE

29
Q

Over Voltage of the Generator 29V to 31.5V

A

Monitor voltage

CONTINUE FLIGHT

30
Q

Under Voltage of the Generator

A

<26V

GENE procedure - APPLY

Voltage over 26V?

Yes - CONTINUE FLIGHT

No - APPLY GENE procedure case A
(probable cause is a fault that doesn’t make GENE light come on)

31
Q

Over Current of the Generator

A

Unnecessary equipment - OFF

CONTINUE FLIGHT

32
Q

ENG FIRE
at start up

A
  1. Starter - OFF
  2. Fuel shutoff - ENGAGE
  3. [FUEL P] - OFF
  4. Crank - PRESS 10 seconds
  5. Rotor brake - APPLY under 170rpm
  6. [Master sw] - OFF
  7. Evacuate aircraft and fight fire from outside
33
Q

ENG FIRE
Hover, Takeoff, Final

A

LAND IMMEDIATELY

No-hover landing

Then apply ENG FIRE start up procedure

34
Q

ENG FIRE
In Flight

A

LAND IMMEDIATELY

  1. Collective - LOWER
  2. IAS - Vy
  3. Autorotation Procedure - APPLY
  4. Emergency Fuel Shutoff - AFT
  5. FUEL P - Check OFF
  6. Engine Starting Selector - OFF

After Landing
7. Rotor Brake - APPLY (under 170rpm)
8. Master SW - OFF
9. Evacuate aircraft and fight fire from outside

35
Q

Red GOV light

A

Major FADEC Failure

  1. Check flight parameter (EBCAU will automatically engage with yellow GOV light)
  2. Collective -AVOID abrupt changes (Maintain NG >80%)

LAND AS SOON AS PRACTICABLE

Make a powered approach
Avoid steep angle

After touchdown:
Collective - Lower SLOWLY
Starting selector - OFF

(Red GOV light during start: Abort start immediately)

36
Q

Solid Yellow GOV Light

A

Minor FADEC Failure
(Governing function degraded)

  1. Collective - Avoid abrupt power changes
  2. IAS - Maintain below power off Vne

LAND AS SOON AS PRACTICABLE

On ground: Do not start engine

37
Q

Flashing Yellow GOV Light During Idle, Startup, Shutdown

A

Governor redundancy failure: No impact on governing function

During startup: Abort startup

Autorotation training: Cancel training and return to base

38
Q

ENG P

A

Check Gauge

Normal:
LAND AS SOON AS PRACTICABLE

Low or nil:
LAND IMMEDIATELY
-Apply autorotation procedure
-Shut down engine if time permits

39
Q

TWT GRIP

A

Return to flight position
CONTINUE FLIGHT

40
Q

ENG CHIP

A

Collective - REDUCE POWER

LAND AS SOON AS POSSIBLE

Low power approach and landing
Be prepared for loss of engine power

41
Q

MGB P

A

Collective - REDUCE POWER

LAND AS SOON AS POSSIBLE

(Fly at Vy to safe landing site if needed)
(At low power, max 55min until gearbox failure)

May turn on at idle - OK

42
Q

MGB TEMP

A

Set speed to Vy

Light goes off:
LAND AS SOON AS PRACTICABLE

Light stays on:
LAND AS SOON AS POSSIBLE

43
Q

MGB CHIP

A

Collective - REDUCE POWER

LAND AS SOON AS POSSIBLE

44
Q

TGB CHIP

A

Avoid prolonged hovering

CONTINUE FLIGHT

45
Q

HYDR + SERVO

A

Loss of hydraulic pressure

  • Keep aircraft at close to level attitude
  • Avoid abrupt maneuvers
  • AOB less than 30 deg
  • IAS below 110 KT (or Vne if less)

LIMIT light indicates LH circuit failed or high load factor maneuvers

LAND AS SOON AS PRACTICABLE

Make normal approach and landing

46
Q

SERVO

A

Jamming of a distributor valve on main servo unit

LAND AS SOON AS PRACTICABLE

47
Q

BATT TEMP

A

Sensor disabled. Not applicable for lead-acid batteries

48
Q

BATT

A

EXT PWR BATT/BATT EPU - CHECK ON

Off?
- Turn on
CONTINUE FLIGHT

On?
- Check voltage on VEMD
LAND AS SOON AS PRACTICABLE

(BATT light will come on whenever connected to EPU)

49
Q

GENE

A

U/BUS on VEMD - CHECK
GENE - CHECK ON

OFF?
- Turn on
CONTINUE FLIGHT
__________________________

ON?
- Check GENE CB not popped
- GENE RESET - PRESS
(If GENE light goes off then CONTINUE FLIGHT)

Light still on:
GENE CASE A:
- Unnecessary equipment -OFF
- U/BUS - MONITOR
LAND AS SOON AS PRACTICABLE
____________________________
Max flight time on battery:
50 minutes day
20 minutes night

50
Q

FUEL

A

18 minutes of flight time remain at MCP

LAND AS SOON AS POSSIBLE

Avoid abrupt maneuvers (don’t slosh fuel around)

51
Q

FUEL P

A

Low fuel pressure

(In flight)

Collective - REDUCE POWER
FUEL P - TURN ON
LAND AS SOON AS POSSIBLE

(Low power approach and landing)
(Be prepared for engine flameout)

52
Q

FUEL FILT

A

Collective - REDUCE POWER

Light goes out:
LAND AS SOON AS PRACTICABLE at reduced power setting

Light stays on:
LAND AS SOON AS POSSIBLE

If Ng oscillations occur:
LAND IMMEDIATELY
Apply autorotation procedure

53
Q

LIMIT

A

High load factor or extreme longitudinal control position

Cruise flight:
Reduce speed and collective

Hovering:
Reduce rearward speed or tailwind component

CONTINUE FLIGHT

54
Q

PITOT

A

PITOT - Check on

Off? - TURN ON

On? - Monitor airspeed indicator

CONTINUE FLIGHT

55
Q

DOOR

A

Airspeed - REDUCE to 70Kt

Descent and approach at low rate of descent

56
Q

Rotor Brake Inop

A

Land into the wind

Cyclic slightly into wind

Wait for rotor to stop completely

57
Q

Bleed valve failure

A

Do not start without green flag visible

Doesn’t disappear at high power settings - Power available will be reduced

Doesn’t appear at low power settings - Compressor stall possible, avoid abrupt power changes

LAND AS SOON AS PRACTICABLE

Bleed valve failure results in yellow GOV light

58
Q

Abnormal Nf Governing

A

Nr/Nf drops below 375 rpm in flight:
Engine parameters - CHECK
NR/NF - CHECK ALIGNED

LAND AS SOON AS PRACTICABLE

Collective anticipator issues will not be remedied until Nr/Nf decreases below 360rpm (GOV light will come on)

59
Q

Generally, what does a red warning light mean?

A

Immediate action

60
Q
A

EC130 135 Checkride Study (6 decks)

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