Ec-130 T2 Emergency Procedures

Front 1

EP: Engine Flame-out

-Cruise Flight

-Over Land

Back 1

-Reduce Collective

-IAS 70 (Vy)

-(Relight if altitude/time allows)

-Twist Grip Idle

-Maneuver into wind

-At 70 ft: Flare

-At 20-25 ft: Gradually Increase Collective, slightly nose-up attitude, adjust pedal, Increase Collective to cushion.
-At touchdown: Cyclic, collective, pedal: Adjust to control ground run

-Collective: Full down

-Rotor brake: Apply below 170 Nr

Front 2

EP: Engine Flame-out

-Cruise Flight

-Over Water

Back 2

Same as Over Land except:

-After touchdown:

-Maintain collective

-Pull Emergency door handles

-Apply rotor brake

Abandon once rotor has stopped.

Front 3

EP Engine Flame-out

-Hover IGE

Back 3

-Maintain Collective

-Pedals control yaw

-Increase collective to cushion

Front 4

EP Engine Flame-out

-Hover OGE

Back 4

-Collective Full Down to stop NR decrease

-Cyclic forward

-Autorotation procedure: Apply

Front 5

EP: In-Flight Relighting Procedure

Back 5

Engine Starting Selector: OFF

-[GENE] OFF

-[FUEL PUMP] ON

-Engine Starting Selector: ON

After relight:
-[GENE] ON

-[FUEL PUMP] OFF

REQUIRES AT LEAST 1000 ft AGL to perform relight.

Front 6

EP: Complete Loss of Tail Rotor Thrust

-Hover IGE

Back 6

LAND IMMEDIATELY

-Twist Grip: Idle

-Collective: Increase to Cushion

Front 7

EP: Complete Loss of Tail Rotor Thrust

-Hover OGE

Back 7

Simultaneously:

-Collective: Reduce (depending on height)

-Cyclic: Forward to gain airspeed

-Airspeed: Vy or greater

-Collective: Adjust to maintain min. sideslip

LAND AS SOON AS POSSIBLE

Carry out autorotative landing at suitable area.

Front 8

EP: Complete Loss of Tail Rotor Thrust

-In Cruise Flight

Back 8

Airspeed: Vy or higher

Collective: Adjust to obtain minimum sideslip

LAND AS SOON AS POSSIBLE

Approach and Landing:

Twist Grip: Idle

Carry out Autorotative landing at suitable area

Front 9

EP: Loss of Tail Rotor Control

Back 9

-Cyclic and Collective: Adjust to set 70 kt IAS

Approach with left sideslip. Running landing

Front 10

EP: Smoke in Cockpit/Cargo

-Source Not Identified

Back 10

-[Batt] EMER SHED

-[GENE] OFF

-[AVIONICS] OFF

-Ventillate Cabin to clear smoke

-All consumers: OFF

-[BATT] ON (check DC parameters)

-[GENE] ON (check DC parameters)

smoke clears?

NO? - LAND AS SOON AS POSSIBLE

YES? - DC PARAMETERS CORRECT?

.

NO? - [GENE] OFF; Apply Case A

of Gen offline procedure; LAND

AS SOON AS PRACTICABLE

YES? - [AVIONICS] ON;

Minimum required consumers:

ON (turn on one-by-one);

CONTINUE FLIGHT

Front 11

EP: Smoke in Cockpit/Cargo

-Source Identified

Back 11

Corresponding System: OFF

Ventilate Cabin

CONTINUE FLIGHT

Front 12

EP: VEMD Screen Failure

-One Screen

Back 12

[OFF 1] or [OFF 2] OFF

Use [SCROLL] to see information

Front 13

EP: VEMD Screen Failure

-Both Screens

Back 13

-IAS: 100kt (-2kt / 1000ft)

LAND AS SOON AS PRACTICABLE

-Landing procedure: No Hover landing

NR constant at 394 RPM

Front 14

ANY Caution Messages on VEMD

Back 14

CONTINUE FLIGHT

Front 15

Abnormal NR/N2 indication

-NR Indication Failure

Back 15

Collective: Maintain Torque > 10%

NR Reading given by N2 indication

LAND AS SOON AS PRACTICABLE

Front 16

Abnormal NR/N2 indication

-N2 Indication Failure

Back 16

NR Indication: Check in the green with TRQ > 0%

CONTINUE FLIGHT

Note: N2 Value can be read off VEMD Screen

Note: EBCAU Might not be available

Front 17

Abnormal Engine Parameter Indication

-Engine Oil Temperature

Back 17

Airspeed: Set >80 KIAS

-Temperature Reduces?

-Yes: LAND AS SOON AS PRACTICABLE; check oil cooler fan for operation

-No: LAND AS SOON AS POSSIBLE

Front 18

Abnormal Engine Parameter Indication

-Engine Oil Pressure

Back 18

CWP: Check ENG P

ENG P on?

No: CWP Light Test

ENG P on?

No: LAND IMMEDIATELY

Yes: LAND AS SOON AS PRACTICABLE

Yes: LAND IMMEDIATELY

Front 19

Abnormal Engine Parameter Indication

-Loss of N1, TOT, or TRQ parameters

Back 19

N1/Delta N1 ind. failure:

-Comply with TRQ limits and TOT limit of 836. Note: TOT limits displayed are starting limits

Torquemeter Failure:

-Comply with N1 Table

Delta N1 AND Torquemeter Failure:

-Note: red GOV can cause Delta N1 and Torquemeter failure

-VEMD reverts to 3-data page. Comply with TOT limit of 836

TOT Indication Failure:

-Respect N1 and TRQ limitations

-Switch off Heating and Demisting or ECS

-On Ground, do not try to start engine.

For all failures: LAND AS SOON AS PRACTICABLE

Front 20

EP: ENG FIRE light

-Start up

Back 20

Engine Starting Selector: OFF

Emergency Fuel Shutoff Handle: AFT

[FUEL PUMP]: OFF

[CRANK]: PRESS (10 secs)

[BATT]: OFF

Rotor Brake: Apply (<170 NR)

Evacuate aircraft and fight fire from outside

Front 21

EP: ENG FIRE light

-Hover, TO, or Final

Back 21

LAND IMMEDIATELY

Once on ground, apply procedure in Start Up

Front 22

EP: ENG FIRE light

-In Flight

Back 22

LAND IMMEDIATELY

Collective Pitch: LOWER

IAS: Vy

Autorotation Procedure: APPLY

Emergency Fuel Shut-Off Handle: AFT

[FUEL PUMP]: CHECK OFF

Engine Starting Selector: OFF

After Landing

[BATT] OFF

Rotor Brake: APPLY (<170 NR)

Evacuate Aircraft and fight fire from outside

Front 23

EP: Red GOV Light

-In Flight

Back 23

Flight Parameters: Check

EBCAU Automatically engages (yellow) GOV light illuminates

Collective Pitch: Avoid Abrupt Changes

Maintain: >80% N1 < 20,000 ft PA

: >85% N1 >= 20,000 ft PA

LAND AS SOON AS PRACTICABLE

Approach and Landing:

Powered approach

Avoid steep angle

After touchdown:

Collective Pitch: Slowly down to low pitch

Engine Starting Selector: OFF

Note: this failure may result in loss of Delta N1 and torque parameters

Front 24

EP: Red GOV Light

-During Engine Starting

Back 24

Engine Starting Selector: OFF Immediately

Front 25

EP: Yellow GOV light

-Permanently Lighted

Back 25

Collective: Avoid abrupt changes

IAS: Maintain below power off VNE

LAND AS SOON AS PRACTICABLE

Note: May result in fixed NR 394. If this happens, tail rotor authority is reduced.

Front 26

EP: Yellow GOV light

-Flashing

Back 26

Only happens at idle.

Autorotation training: Return to base

Startup: Abort

Front 27

EP: ENG P Light

Back 27

Oil Pressure: CHECK Gauge

Low or NIL?

LAND IMMEDIATELY

AUTOROTATION PROCEDURE: APPLY

Shutdown engine time permitting

NORMAL?
LAND AS SOON AS PRACTICABLE

Front 28

EP: TWT GRIP Light

Back 28

Twist Grip: TURN to FLIGHT Position

CONTINUE FLIGHT

Front 29

EP: ENG CHIP light

Back 29

Collective Pitch: REDUCE Power

LAND AS SOON AS POSSIBLE

Low power approach and landing.

Be prepared for engine failure.

Note: Takeoff prohibited until specific checks performed.

Front 30

EP: MGB P light

Back 30

Collective: REDUCE power

LAND AS SOON AS POSSIBLE

If safe landing site not available, reduce power and fly at Vy to nearest landing site.

Front 31

EP: MGB TEMP Light

Back 31

IAS: SET to Vy

CWP: MONITOR

MGB P light?

NO?
LAND SOON AS PRACTICABLE

YES?

LAND AS SOON AS POSSIBLE

Front 32

EP: MGB CHIP light

Back 32

Collective: REDUCE Power

MGB P and MGB TEMP lights: Monitor

Front 33

EP: TGB CHIP light

Back 33

Avoid prolonged hovering

CONTINUE FLIGHT

Front 34

EP: HYDR + SERVO lights

Back 34

-Keep aircraft in more or less level attitude

-Avoid Abrupt Maneuvers

-Maintain angle of bank less than 30 deg.

-Maintain IAS less than 110kt or VNE

Note: LIMIT light will be on when load factor exceeded or LH circuit failure.

LAND AS SOON AS PRACTICABLE

Normal approach and landing.

Front 35

EP: SERVO light

Back 35

LAND AS SOON AS PRACTICABLE

Front 36

EP: BATT TEMP light

Back 36

[BATT]: OFF

U Bus Voltage: CHECK

NORMAL?

LAND AS SOON AS PRACTICABLE

ABOVE Umax?

[BATT]: ON

[GENE]: OFF

Unnecessary Equipments: OFF

LAND AS SOON AS PRACTICABLE

Front 37

EP: BATT light

Back 37

[BATT]: CHECK ON

YES?

CHECK Voltage on VEMD

LAND AS SOON AS PRACTICABLE

NO?

[BATT]: ON

BATT light off?

CONTINUE FLIGHT

Front 38

EP: GENE light

Back 38

U bus on VEMD: CHECK

[GENE]: CHECK ON

Yes?

GENE Reset Circuit breaker: Check not popped

[GENE]: RESET

[GENE]: ON

GENE light: Check

ON?

Unnecessary Equipment: OFF

U bus on VEMD: MONITOR

LAND AS SOON AS PRACTICABLE

OFF?

CONTINUE FLIGHT

Front 39

EP: FUEL light

Back 39

LAND AS SOON AS POSSIBLE

15 minutes of flight time remain

note: Avoid large attitude changes

Front 40

EP: FUEL P light

Back 40

IN FLIGHT:

COLLECTIVE PITCH: REDUCE POWER

[FUEL PUMP]: ON

LAND AS SOON AS POSSIBLE

low power approach and landing

Note: Be prepared for engine flameout

Front 41

EP: FUEL FILT light

Back 41

Continuously on: Fuel Filter pre-clogging level 2 reached

LAND AS SOON AS PRACTICABLE

VEMD: MONITOR N1

N1 Oscillations?

LAND IMMEDIATELY

Flashing at Idle or during Startup or Shutdown: Preclogging level 1 reached

One-time 3 hour flight permitted to an area where maintenance can be performed.

Front 42

EP: LIMIT light

Back 42

In High-speed cruise flight or steep maneuvers:

Collective: REDUCE power

Cyclic: REDUCE speed or load factor

At rearward speed or hovering in high tailwinds:

Cyclic: REDUCE rearward speed

REDUCE tailwind component.

CONTINUE FLIGHT

Front 43

EP: PITOT light

Back 43

Monitor airspeed indicator.

CONTINUE FLIGHT

Front 44

EP: HORN light

Back 44

[HORN]: CHECK ON.

YES?

Audible horn failure

NO?

[HORN]: ON

CONTINUE FLIGHT

Front 45

EP: DOOR light

Back 45

Airspeed: REDUCE to 70 KIAS

LAND AS SOON AS PRACTICABLE

Front 46

EP: INST LIGHT light

Back 46

CONTINUE FLIGHT

Note: Dome light can be used for additional instrument panel lighting

Front 47

EP: P2 OVHT light

Back 47

TEMP BUTTON on ECS PANEL: OFF

ON VEMD: CHECK P2 unlit

After 1 Minute: Check P2 OVHT

ON?

P2 Manual Valve: CLOSE

CONTINUE FLIGHT

Note: Demisting function is degraded when P2 bleed is cut off

If external visibility becomes degraded:
LAND AS SOON AS POSSIBLE

OFF?

CONTINUE FLIGHT

Front 48

EP: Rotor Brake Inoperative

Back 48

Rotor Stopping with wind blowing:

Aircraft: INTO THE WIND

Cyclic Stick: slightly INTO WIND

Front 49

EP: Bleed Valve Failure

Back 49

The bleed valve is normally open during startup, shutdown, and at low power settings.

If flag does not disappear at high power settings (near MCP), engine power is reduced, especially in cold weather.

If flag does not reappear at low power settings, engine may surge. Avoid abrupt changes in power settings.

Bleed valve failure results in yellow GOV light.

LAND AS SOON AS PRACTICABLE

Front 50

EP: ICS Inoperative

Back 50

ICS: OFF

COM 1: Check ON; Adjust volume

NOTE: VHF and Audio warnings available for LH Pilot only

Front 51

EP: AVCS Failure

Back 51

[AVCS]: OFF

After 30 seconds

[AVCS]: ON

AVCS fail light?

ON?

CONTINUE FLIGHT

FAIL?

[AVCS] OFF

CONTINUE FLIGHT