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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 on 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 slightly 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
Torquemeter Failure
Comply with NG table Usually NG ~93/94 LAND AS SOON AS PRACTICABLE
26
Delta NG AND Torquemeter failure
Use T4 and numeric NG and comply with NG table (usually ~93 NG) LAND AS SOON AS PRACTICABLE
27
T4 Indication Failure
Comply with NG and TQ limitations. LAND AS SOON AS PRACTICABLE Do not start engine without T4 indications
28
Over Voltage of the Generator >31.5V
[GENE] - OFF Apply GENE procedure case A LAND AS SOON AS PRACTICABLE
29
Over Voltage of the Generator 29V to 31.5V
Monitor voltage CONTINUE FLIGHT
30
Under Voltage of the Generator
<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
Over Current of the Generator
Unnecessary equipment - OFF CONTINUE FLIGHT
32
ENG FIRE at start up
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
ENG FIRE Hover, Takeoff, Final
LAND IMMEDIATELY No-hover landing Then apply ENG FIRE start up procedure
34
ENG FIRE In Flight
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
Red GOV light
Major FADEC Failure 1. Check flight parameter (EBCAU will automatically engage with amber 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
Solid Amber GOV Light
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
Flashing Amber GOV Light During Idle, Startup, Shutdown
Governor redundancy failure: No impact on governing function During startup: Abort startup Autorotation training: Cancel training and return to base
38
ENG P
Check Gauge Normal: LAND AS SOON AS PRACTICABLE Low or nil: LAND IMMEDIATELY -Apply autorotation procedure -Shut down engine if time permits
39
TWT GRIP
Return to flight position CONTINUE FLIGHT
40
ENG CHIP
Collective - REDUCE POWER LAND AS SOON AS POSSIBLE Low power approach and landing Be prepared for loss of engine power
41
MGB P
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
MGB TEMP
Set speed to Vy Light goes off: LAND AS SOON AS PRACTICABLE Light stays on: LAND AS SOON AS POSSIBLE
43
MGB CHIP
Collective - REDUCE POWER LAND AS SOON AS POSSIBLE
44
TGB CHIP
Avoid prolonged hovering CONTINUE FLIGHT
45
HYDR + SERVO
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
SERVO
Jamming of a distributor valve on main servo unit LAND AS SOON AS PRACTICABLE
47
BATT TEMP
Sensor disabled. Not applicable for lead-acid batteries
48
BATT
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
GENE
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
FUEL
18 minutes of flight time remain at MCP LAND AS SOON AS POSSIBLE Avoid abrupt maneuvers (don't slosh fuel around)
51
FUEL P
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
FUEL FILT
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
LIMIT
High load factor or extreme longitudinal control position Cruise flight: Reduce speed and collective Hovering: Reduce rearward speed or tailwind component CONTINUE FLIGHT
54
PITOT
PITOT - Check on Off? - TURN ON On? - Monitor airspeed indicator CONTINUE FLIGHT
55
DOOR
Airspeed - REDUCE to 70Kt LAND AS SOON AS PRACTICABLE Descent and approach at low rate of descent
56
Rotor Brake Inop
Land into the wind Cyclic slightly into wind Wait for rotor to stop completely
57
Bleed valve failure
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 amber GOV light
58
Abnormal Nf Governing
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
Generally, what does a red warning light mean?
Immediate action
60
61
Vy
70kt at 0Hp (-1kt/1000’)
62
[FILTER]
Pressure differential met or exceeded. If significant rise in TOT or any fluctuations of engine parameters, press button to open bypass. [bypass] will illuminate.
63
[GENE]
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
64
GENE
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
65
Cranking Procedure
SHALL be performed after an aborted start. Starting selector - OFF Fuel shutoff - Forward Ng under under 10 percent FUEL P - ON CRANK - 20 sec max FUEL P - OFF

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