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EC130 B4/T2 > Emergency Procedures > Flashcards

Emergency Procedures Flashcards

1
Q

Land Immediately

A

Self explanatory

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2
Q

Land As Soon As Possible

A

Emergency conditions are urgent and require landing at the nearest landing site at which a safe landing can be made

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3
Q

Land As Soon As Practicable

A

Emergency conditions are less urgent and in the pilots judgement, he may proceed to the nearest airfield where he can expect appropriate assistance.

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4
Q

Continue Flight

A

Continue flight as planned. Repair at the destination according to the maintenance manual.

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5
Q

What do bolded items mean?

A

Immediate actions that the pilot shall take

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6
Q

Gong sound

A

A gong sound is generated each time a red warning appears on the CWP

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7
Q

Continuous Tone

A

Nr is below 360 RPM OR max takeoff rating exceeded

  1. Collective - Reduce maintain Nr in norm op range
  2. Engine parameters - Check
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8
Q

Intermittent Tone

A

Nr is above 410 RPM
1. Collective - Increase to maintain Nr in norm op range

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9
Q

Auto - Cruise Flight over Land

A
  1. Collective - Reduce to maintain Nr in norm op range
  2. IAS - Vy
    - If relight impossible or loss of TR thrust
  3. Twist grip - IDLE Position
  4. Maneuver into wind
  5. 70ft: Cyclic - FLARE
    - 20/25ft
  6. Collective - GRADUALLY INCREASE
  7. Cyclic - FORWARD, slightly nose up <10degrees
  8. Pedals - ADJUST
  9. Collective - INCREASE
    - after touch-down
  10. Controls - ADJUST to control ground run
    - once stopped
  11. Collective - FULL DOWN
  12. Rotor Brake - APPLY <170 RPM
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10
Q

Auto - Cruise Flight over Water

A

1-9 Same as Land
- after touch-down
10. Collective - MAINTAIN
11. Forward door emergency handles - PULL UP
12. Doors - JETTISON OR OPEN
13. Rotor Brake - APPLY
Abandon aircraft when rotors stop

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11
Q

Hover Auto - IGE

A
  1. Collective - MAINTAIN
  2. Pedals - CONTROL YAW
  3. ** Collective - INCREASE** to cushion
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12
Q

Hover Auto - OGE

A
  1. ** Collective - FULL LOW PITCH**
    - when Nr stops decreasing
  2. Cyclic - FORWARD gain airspeed according to available height
  3. Auto procedure - APPLY
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13
Q

Relight in Flight

A
  1. Fuel Pump - ON
  2. Engine starting selector - OFF position
  3. Engine starting selector - ON position
    Relighting automatic as soon as Ng <17%
    After relighting procedure
  4. Fuel Pump - OFF
    Min of 1000ft necessary to complete procedure post flame-out
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14
Q

Loss of TR Thrust - Hover IGE
(or OGE within HV diagram)

A

Left yaw
LAND IMMEDIATELY
1. Twist Grip - IDLE position
2. Collective - INCREASE

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15
Q

Loss of TR Thrust - Hover OGE
(clear area, out of HV diagram)

A

Left yaw
Simultaneously:
1. Collective - REDUCE depending on available height
2. Cyclic - FORWARD to gain speed
3. Airspeed - Maintain Vy or highter
4. Collective - ADJUST obtain min sideslip angle
LAND AS SOON AS POSSIBLE
If a go-around has been performed, carry out an auto on a suitable area as landing procedure.

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16
Q

Loss of TR Thrust - In Cruise Flight

A

Left Yaw
1. Airspeed - Maintain Vy or highter
2. Collective - ADJUST obtain min sideslip angle
LAND AS SOON AS POSSIBLE
Approach and Landing on suitable are for Auto:
1. Twist grip - IDLE position
2. Carry out auto according to procedure

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17
Q

Loss of TR Control

A

Symptoms: jamming of pedals, loss of pedal effectiveness.
Landing is made easier with right wind component
Go around impossible <20kts due to loss of vertical fin effieciency
1. Cyclic and Collective - ADJUST for 70kts
On suitable area for running landing:
2. Shallow approach
3. Slight left sideslip - reduces airspeed as collective is applied
4. Running landing

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18
Q

Smoke in Cabin - Source not Ident
B4

A
  1. Heating, Demisting - OFF
    Smoke Clears - YES - CONTINUE FLIGHT

Smoke Clears - NO …
1. EMER SW - OFF
2. DCT BAT - OFF
3. EXT PWR BAT/EPU - OFF
4. GENE - OFF
5. MASTER AVIONIC - OFF
6. Vent Cabin
When smoke clears …
7. All consumers - OFF
8. EMER SW - ON
9. DCT BAT - ON
10. EXT PWR BAT/EPU - ON, check parameters
11. GENE - ON, check parameters
Smoke Clears - NO - LAND AS SOON AS POSSIBLE

Smoke Clears - YES …
If parameters NOT correct:
12. GENE - OFF
13. Apply case A og GENE DC generate off line procedure
LAND AS SOON AS PRACTICABLE

If parameters CORRECT:
12. AVIONICS - ON
13. Min req consumers - ON, one at a time
CONTINUE FLIGHT

CAUTION - with EMERG SW - OFF or BATT and GEN - OFF, the VEMD goes off. Apply proc for failure of both screens

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19
Q

Smoke in Cabin - Source Ident
B4/T2

A
  1. Corresponding system - OFF
  2. Vent cabin
    CONTINUE FLIGHT, depending on system failed

Note - after DC has been switched off and on in flight, GOV light will remain on until the next normal full engine shut down and battery switch off on the ground

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20
Q

Smoke in the Cabin - Source not Ident
T2

A
  1. Heating, Demisting, ECS - OFF
    Smoke Clears - YES - CONTINUE FLIGHT

Smoke Clears - NO …
1. BATT - EMER SHED
2. GENE - OFF
3. AVIONIC - OFF
4. Vent Cabin
When smoke clears …
5. All consumers - OFF
6. BATT - ON, Check DC parameters
7. GENE - ON, check DC parameters

Smoke Clears - NO
8. BATT - OFF
9. GENE - OFF
LAND AS SOON AS POSSIBLE

Smoke Clears - YES …
-If DC parameters NOT correct:
12. GENE - OFF
13. Case A GENE off line procedure
LAND AS SOON AS PRACTICABLE

-If DC parameters CORRECT:
12. AVIONICS - ON
13. Min req consumers - ON, one at a time
CONTINUE FLIGHT

CAUTION - with EMER SHED position, the VEMD goes off. Apply proc for failure of both screens

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21
Q

VEMD - Failure of one screen

A
  1. OFF1/OFF2 - OFF
    Read all available info on other screen by using the SCROLL pushbutton

Top screen failure - 3 parameters engine page will be automatically displayed on lower screen, TQ and delNg off line, only T4 and digital Ng available.

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22
Q

VEMD - Failure of Both Screens

A
  1. Power for level flight only
  2. 100kt (-2kt/1000ft)
  3. LAND AS SOON AS PRACTICABLE
  4. No hover landing
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23
Q

VEH PARAM or ENG PARAM

A

Abnormal vehicule or engine parameter

  1. SCROLL - PRESS, to reach relevant page and check the parameter
    CONTINUE FLIGHT
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24
Q

Nr Indication Failure

A
  1. Collective - MAINTAIN TQ > 10%
    Nr reading is given by Nf pointer.
    LAND AS SOON AS PRACTICABLE
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25
Q

Nf Indication Failure

A
  1. Nr Indication - CHECK in normal op range with TQ > 0
    CONTINUE FLIGHT

Note - in case Nf indication failure, the EBCAU may not be available

26
Q

Engine Oil Temp High

A

B4 > 115C
T2 > 117C

  1. Airspeed - 80 KIAS

Temp stays/increases - LAND AS SOON AS POSSIBLE
Temp reduces - LAND AS SOON AS PRACTICABLE

Check cooler fan operation

27
Q

Engine Oil Press Low
No (ENG P) red light associated

A

Oil press < 1.1bar

  1. Reduce power, begin descent
  2. CWP light test

(ENG P) Light - NOT WORKING - LAND IMMEDIATELY, Auto
OR
(ENG P) Light - WORKING - LAND AS SOON AS PRACTICABLE

28
Q

(ENG P) red light

A

Oil Press < 1.1 Bar

  1. Reduce power, begin descent
  2. Check gauge
    - normal: LAND AS SOON AS PRACTICABLE
    - low/nil: LAND IMMEDIATELY
29
Q

VEMD - Ng/N1 Indicator Failure

A

FLI is replaced by the 3 data symbology

  1. Comply with the max TQ value and T4/TOT limit of 810C
    LAND AS SOON AS PRACTICABLE
30
Q

VEMD - TQ Indicator Failure

A

FLI is replaced by the 3 data symbology

  1. Comply with the Ng/N1 given in the table
    LAND AS SOON AS PRACTICABLE
31
Q

VEMD - del Ng/del N1 and TQ Indication Failures

A
  • FLI is replaced by the 3 data symbology
  • (GOV) red light warning can also induce loss of del Ng/del N1 and TQ
  • Comply with Ng limit and respect T4/TOT limit of 810C
    LAND AS SOON AS PRACTICABLE
32
Q

VEMD - T4/TOT Indication Failure

A
  • FLI replaced by the 3 data symbology
  • Comply with Ng/N1 and TQ limits
  • On ground: do not start engine
    LAND AS SOON AS PRACTICABLE
33
Q

U/BUS >31.5 V
Red Line

A
  1. GENE - OFF
  2. Unnecessary equip - OFF
    LAND AS SOON AS PRACTICABLE
34
Q

29.0 V < U/BUS </= 31.5 V
Yellow Line

A
  1. U/BUS voltage - MONITOR
    CONTINUE FLIGHT
35
Q

U/BUS </= 26.0 V
Yellow line

A
  1. GENE - Reset, then ON
  2. U/BUS > 26.0 V - CONTINUE FLIGHT
    OR
  3. U/BUS < 26.0 V - Unnecessary equip - OFF
    LAND AS SOON AS PRACTICABLE
36
Q

I/GEN >200A
Red line flashing

A
  1. Unnecessary equip - OFF
    CONTINUE FLIGHT

Note - after engine start on batt, temporary high gen current is normal as batt is being recharged. Avoid high electrical load consumers

37
Q

(ENG FIRE) red light - On Start

A
  1. Engine starting selector - OFF position
  2. Emerg fuel shut-off handle - AFT
  3. Fuel P - OFF
  4. Crank - Press (10 sec.)
  5. Emerg SW - OFF
  6. Rotor Brake - APPLY, </= 170 RPM
  7. Evacuate
38
Q

(ENG FIRE) red light - Hover, Takeoff, Final

A

LAND IMMEDIATELY
No hover, low powered landing
On ground, same procedure as fire on start

39
Q

(ENG FIRE) red light - In Flight

A

One of the 3 detectors has exceeded limits

  1. Collective - LOWER
  2. CONFIRM FIRE
  3. AUTO - Vy
  4. Emerg fuel shut-off handle - AFT
  5. Fuel P - CHECK OFF
  6. Engine starting selector - OFF position
    After landing:
  7. Emer SW - OFF
  8. Rotor Brake - APPLY </= 170 RPM
  9. Evacuate
40
Q

(GOV) red light - In Flight
(GOV) yellow light will come on too

A

Major Governor failure, EBCAU engaged

  1. AVOID abrupt changes
  2. Ng/N1 > 80% below 20,000ft
    LAND AS SOON AS PRACTICABLE
  3. Shallow approach, No hover landing
  4. SLOW down collective on shutdown
  5. Engine starting selector - OFF
41
Q

(GOV) red light - During Start

A

Major Governor Failure
Emergency mode engaged (EBCAU)
1. Engine start selector - OFF position immediately

42
Q

(GOV) yellow light - Continuous

A

Minor FADEC Failure
Governing funtion degraded.

  1. AVOID abrupt changes
  2. IAS < Vne power off
    LAND AS SOON AS PRACTICABLE
43
Q

(GOV) yellow light - Flashing idle/start/shutdown

A

Minor FADEC Failure
Governor redundance failure, no impact on function
- Start up - abort
- Auto Training - cancel training

44
Q

(TWT GRIP) Red light

A
  1. Twist grip - TURN to FLIGHT position
    CONTINUE FLIGHT
45
Q

(ENG CHIP) Yellow light

A
  1. REDUCE power
    LAND AS SOON AS POSSIBLE
  2. Low-power approach/landing, prepare for power loss
46
Q

(MGB P) red light

A

Main Gear Box low oil pressure <1bar

  1. REDUCE power
    LAND AS SOON AS POSSIBLE

If safe landing not possible, contine to nearest site

47
Q

(MGB TEMP) yellow light

A

B4 > 115C
T2 > 117C

  1. IAS - Vy
    - Light OUT LAND AS SOON AS PRACTICABLE
    - Light ON LAND AS SOON AS POSSIBLE
48
Q

(MGB CHIP) Yellow light

A
  1. REDUCE power
  2. MONITOR lights: (MGB P) and (MGB TEMP)
    LAND AS SOON AS POSSIBLE
49
Q

(TGB CHIP) Yellow light

A

CONTINUE FLIGHT
Avoid prolonged hovering

50
Q

(HYDR) + (SERVO) Yellow lights

A

Hyd Press < 20 bar

  1. Avoid abrupt manuevers
    - Bank < 30deg
    - IAS < 110kts
    LAND AS SOON AS PRACTICABLE

Normal approach and landing
Note: (LIMIT) yellow light may be on if LH circuit failed

51
Q

(SERVO) yellow light

A

Jamming of a distributor valve

LAND AS SOON AS PRACTICABLE

52
Q

(BATT) Yellow light

A

Battery off line. (50min day, 20min night) advised to cut time in half

  1. Check BAT/EPU - ON
    - ON: Check voltage and LAND AS SOON AS PRACTICABLE
    - OFF: Turn it on … CONTINUE FLIGHT
53
Q

(GENE) yellow light

A

DC generator off line

  1. U bus on VEMD - CHECK
  2. GENE - Reset
  3. If still on - turn off unnecessary equip
    LAND AS SOON AS PRACTICABLE

Note: If battery fails, VEMD will go out

54
Q

(FUEL) yellow light

A

Fuel quantity < 106lb or 15min at MCP

LAND AS SOON AS POSSIBLE

Warning: Avoid large power changes - could lead to engine flame out

55
Q

(FUEL P) yellow light

A

Low Fuel Pressure

IN FLIGHT:
1. REDUCE POWER
2. Fuel pump - ON
3. LAND AS SOON AS POSSIBLE
4. Low power approach and landing

Warning: be prepared for engine flame out

56
Q

(FUEL FILT) yellow light

A

Fuel filter clogged

  1. REDUCE POWER
    - Light out: LAND AS SOON AS PRACTICABLE
    - Light on: LAND AS SOON AS POSSIBLE
  2. Ng/N1 oscillations occur - LAND IMMEDIATELY

T2 - Flashing at Idle - Level 1 clog

57
Q

(LIMIT) Yellow light

A

Main servo max load
Max rotor head stress
Extreme longitudinal control position

In Flight
1. REDUCE power
2. REDUCE speed
3. REDUCE load factor

Hovering:
1. REDUCE speed or tailwind component

CONTINUE FLIGHT

Note: (LIMIT) may appear associated with HYD 1 if failure

58
Q

(PITOT) yellow light

A

Pitot heat inop

  1. Pitot - Check on
    - ON: Monitor airspeed
    - OFF: turn it on

CONTINUE FLIGHT

59
Q

(HORN) Yellow light

A

Aural warning not operative

  1. HORN - Check on
    - ON: Aural warning failure
    - OFF: turn on

CONTINUE FLIGHT

60
Q

(DOOR) yellow light

A

On or both cargo hold doors unlocked

  1. Airspeed - 70kts
  2. Low ROD and shallow approach

LAND AS SOON AS PRACTICABLE

61
Q

(BATT TEMP) red light

A

Nicad Only
Battery temp >71C

  1. BATT - OFF
  2. Check U bus voltage
    - normal: LAND AS SOON AS PRACTICABLE
    - above max - BATT - OFF and GENE - OFF
62
Q

Bleed Valve Failure

A
  • Green/White stripped flag on FLI = bleed valve open
  • Will get (GOV) amber light as well
  1. Avoid abrupt power changes
    LAND AS SOON AS PRACTICABLE

EC130 B4/T2 (13 decks)

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