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EC130 B4/T2 > Emergency Procedures > Flashcards

Emergency Procedures Flashcards

(62 cards)

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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
Nf Indication Failure
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
Engine Oil Temp High
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
Engine Oil Press Low No (ENG P) red light associated
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
(ENG P) red light
Oil Press < 1.1 Bar 1. **Reduce power, begin descent** 2. Check gauge - normal: **LAND AS SOON AS PRACTICABLE** - low/nil: **LAND IMMEDIATELY**
29
VEMD - Ng/N1 Indicator Failure
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
VEMD - TQ Indicator Failure
FLI is replaced by the 3 data symbology 1. Comply with the Ng/N1 given in the table **LAND AS SOON AS PRACTICABLE**
31
VEMD - del Ng/del N1 and TQ Indication Failures
- 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
VEMD - T4/TOT Indication Failure
- 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
U/BUS >31.5 V Red Line
1. GENE - OFF 2. Unnecessary equip - OFF **LAND AS SOON AS PRACTICABLE**
34
29.0 V < U/BUS
1. U/BUS voltage - MONITOR **CONTINUE FLIGHT**
35
U/BUS
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
I/GEN >200A Red line flashing
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
(ENG FIRE) red light - On Start
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,
38
(ENG FIRE) red light - Hover, Takeoff, Final
**LAND IMMEDIATELY** No hover, low powered landing On ground, same procedure as fire on start
39
(ENG FIRE) red light - In Flight
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
40
(GOV) red light - In Flight (GOV) yellow light will come on too
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
(GOV) red light - During Start
Major Governor Failure Emergency mode engaged (EBCAU) 1. **Engine start selector - OFF position immediately**
42
(GOV) yellow light - Continuous
Minor FADEC Failure Governing funtion degraded. 1. AVOID abrupt changes 2. IAS < Vne power off **LAND AS SOON AS PRACTICABLE**
43
(GOV) yellow light - Flashing idle/start/shutdown
Minor FADEC Failure Governor redundance failure, no impact on function - Start up - abort - Auto Training - cancel training
44
(TWT GRIP) Red light
1. **Twist grip - TURN to FLIGHT position** **CONTINUE FLIGHT**
45
(ENG CHIP) Yellow light
1. **REDUCE power** **LAND AS SOON AS POSSIBLE** 2. Low-power approach/landing, prepare for power loss
46
(MGB P) red light
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
(MGB TEMP) yellow light
B4 > 115C T2 > 117C 1. **IAS - Vy** - Light OUT **LAND AS SOON AS PRACTICABLE** - Light ON **LAND AS SOON AS POSSIBLE**
48
(MGB CHIP) Yellow light
1. **REDUCE power** 2. MONITOR lights: (MGB P) and (MGB TEMP) **LAND AS SOON AS POSSIBLE**
49
(TGB CHIP) Yellow light
**CONTINUE FLIGHT** Avoid prolonged hovering
50
(HYDR) + (SERVO) Yellow lights
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
(SERVO) yellow light
Jamming of a distributor valve **LAND AS SOON AS PRACTICABLE**
52
(BATT) Yellow light
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
(GENE) yellow light
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
(FUEL) yellow light
Fuel quantity < 106lb or 15min at MCP **LAND AS SOON AS POSSIBLE** Warning: Avoid large power changes - could lead to engine flame out
55
(FUEL P) yellow light
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
(FUEL FILT) yellow light
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
LIMIT light
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
(PITOT) yellow light
Pitot heat inop 1. **Pitot - Check on** - ON: Monitor airspeed - OFF: turn it on **CONTINUE FLIGHT**
59
(HORN) Yellow light
Aural warning not operative 1. HORN - Check on - ON: Aural warning failure - OFF: turn on **CONTINUE FLIGHT**
60
(DOOR) yellow light
On or both cargo hold doors unlocked 1. **Airspeed - 70kts** 2. Low ROD and shallow approach **LAND AS SOON AS PRACTICABLE**
61
(BATT TEMP) red light
**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
Bleed Valve Failure
- 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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