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H130T2 > Emergencies > Flashcards

Emergencies Flashcards

1
Q

Engine Flame Out in Cruise Flight

A 
Lower collective to mtn Nr in green arc
airspeed 70 KIASautorotate	
if relight impossible or loss of t/r thrust	
Twist Grip to idle	
Into Wind landing, flare at 70'	
once on ground, collective full down	
rotor brake apply below 170 Nr
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2
Q

Engine Flame Out in Hover - IGE

A

maintain collective
control yaw with pedals
use collective tocushion landing

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3
Q

Engine Flame Out in Hover OGE safe autorotative landing cannot be ensured if inside HV diagram or in confined area

A

collective full down
when Nr stops decreasing:
cyclic forward to gain airspeed if height allows
apply autorotative procedure

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4
Q

In Flight Relight

auto relight will occur after N1 Less than 10%

A 
Engine start selector - OFF	
GENE - OFF	
Fuel Pump - ON	
Engine start selector - ON		
After Start: GENE ON,	
Fuel Pump OFF
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5
Q

Engine Oil Temp Over Limit

A

Airspeed 80 KIAS
If temp reduces, land ASAPL check fan operation
If temp not reducing, land ASAP

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6
Q

Hot Start

A

Engine Start Selector - OFF

Crank - press for 10 seconds

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7
Q

Engine oil Pressure LOW on VEMD

A

CWP - Check Eng P light on or off
ENG P light ON -autorotate & shutdown
ENG P light OFF -press CWP light test
ENG P light ON - land ASAPL
Eng P light OFF - autorotate & shutdown

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8
Q

Drive Shaft Failure

low Nr and low Rpm Hornwith high Np

A

enter autorotation

do not shut down engine to maintain t/r

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9
Q

GEN Over Voltage >31.5 V

A 
GENE OFF	
monitor for BATT Temp	
Unnecessary equipment OFF	
monitor Ubus on VEMD	
Land ASAPL
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10
Q

GEN Under Voltage

Probable cause of such a failureis a generator defect that doesnot make GENE light come on.

A

check U bus on VEMD
if > 26vcontinue flight
if

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11
Q

GEN Current Overlimit
(flashing red underline)
After engine starting on battery, a temporary high generatorcurrent is normal because the battery is being recharged.During this phase, avoid using high electrical loadconsumers.

A

Unnecessary equipment OFF

Continue Flight

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12
Q

Smoke in Cabin/Cargo - Source Not Identified

When [BATT] is set to “EMER SHED” position,the VEMD goes off.
After DC had been switched-off and on in flight,GOV light will remain on until the next normal full engine and battery switch-off on the ground.
NR is constant at 394 rpm.

A 
SOURCE NOT IDENTIFIED	
Heating, Demisting, ECS off
If smoke clears continue flight
If smoke does not clear	
BATT in Emergency SHED	
GENE OFF	
AVIONICS OFF	
Vent Cabin

When smoke clears all consumers OFF
BATT ON - check DC Parameters
GEN ON - check DC Parameters

If smoke persists - LAND ASAP
If smoke clearscheck DC parameters

DC Parameters not correct
GENE OFF
​LAND ASAPL

DC Parameters correct	
Avionics ON	
min consumers ON one by one	
if smoke returns, switch off consumer	
Continue flight
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13
Q

Tail Rotor Failure In HOVER IGE or OGE in HV Diagram (LH Yaw)

A

Twist Grip - IDLE

Cushion Landing with collective

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14
Q

Tail Rotor Failure In HOVER (out of HV Diagram) (LH Yaw)

A

Lower Collective if altitude permits
Cyclic FWD to gain airspeed 70 KIAS or higher
adjust collective for min sideslip angle
Land ASAPautorotate

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15
Q

Tail Rotor Failure In FLIGHT

A 
Maintain airspeed 70 KIAS or higher	
adjust collective for min sideslip angle	
LAND ASAP	
twist grip idle 
autorotate
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16
Q

Loss of Tail Rotor Control
loss of pedal effectiveness
go around impossible with IAS

A 
Airspeed to 70 KIAS in level flight
Find suitable run on landing area
Land with RH wind component	
shallow approach with left sideslip	
run on landing
sideslip willreduce with reduced airspeed	
apply collective to cushion landing
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17
Q

NR Indication Failure

A

Collective MAINTAIN TRQ > 10 %.
NR reading is given by N2 pointer.
LAND ASAPL

18
Q

N2 indication Failure
The N2 value can be read on the VEMD screen.
Press [SELECT],then [+] as many times as required to display the parameter in the rectangular window at the bottom of the FLI or 3-data screen.
EBCAU may not be available

A

NR indication CHECK in green range with TRQ > 0.

CONTINUE FLIGHT

19
Q

N1 indicator failure
When a parameter is off line, the parameter value is not displayed onthe VEMD upper screen and the parameter scale symbology isdisplayed in yellow.The First Limitation Indicator (FLI) is replaced by the 3 datasymbology (N1/􀀧N1, TOT and TRQ) and a failure message isdisplayed.

A

Comply with max TRQ value and TOT limit of 836°C.
Land ASAPL

20
Q

TOT Indicator Failure
When a parameter is off line, the parameter value is not displayed onthe VEMD upper screen and the parameter scale symbology isdisplayed in yellow.The First Limitation Indicator (FLI) is replaced by the 3 datasymbology (N1/􀀧N1, TOT and TRQ) and a failure message isdisplayed.

A

Respect N1 & TRQ limitations
heating, demisting, ECS OFF
Land ASAPL
on grounddo not try restart

21
Q

VEMD both screen failure

Nr constant at 394 rpm

A

to avoid power overlimit
max 100 KIAS (-2/1000’)
Land ASAPL no hover landing

22
Q

Bleed Valve Failure
flag appears when bleed valve is open
flag disappears when bleed valve is closed
The bleed valve is normally open when then the engine is shut down, during starting and at low power settings.

A

If the flag does not disappear at high power settings (i.e. near MCP or above), the maximum available engine power is reduced, specifically in cold weather.
If the flag does not reappear at low power settings, the engine may surge.
Avoid abrupt changes in power settings.
Bleed valve failure results in YELLOW GOV
LAND ASAPL

23
Q

Smoke in Cabin/Cargo - Source Identified
When [BATT] is set to “EMER SHED” position, the VEMD goes off.
After DC had been switched-off and on in flight, GOV light will remain on until the next normal full engine and battery switch-off on the ground.
NR is constant at 394 rpm.

A

Source Identified
Corresponding system off
vent cabin
continue flight

24
Q

VEMD failure of one screen

A

OFF1 or OFF2 - off
read available info on other screen
use scroll on VEMD or collif top screen fails
3 eng parameters will display on lower screen

25
Q

VEMD caution messages

A

when parameter offline, value not displayed and parameter scale in yellow
comply with caution message (no light - no action)

26
Q

Overlimit Detected

A

This message appears as soon as a parameter overlimit is recorded in theVEMD and will be displayed on the FLI or engine page until 40 % N1 during the next engine start.After the flight, check the recorded overlimit data and perform theassociated maintenance actions.

27
Q

GEN OverVoltage 29.0V

A

monitor Ubus Voltage

continue flight

28
Q

Engine Fire in Hover, Takeoff, Final

A 
Land Immediately	
no-hover powered landing
	
eng start selector OFF	
emergency fuel shutoff handle AFT	
Fuel Pump OFF	
Crank for 10 sec	
Batt OFF	
Rotor brake apply 	
evacuate and fight fire
29
Q

eng fail on start

A

return start selector to OFF
wait 30 sec
eng crank prior to next start

30
Q

To abort start

A

turn starting selector off

fuel pump off

31
Q

Engine Crank Procedure
(max 20 sec)
crank with EFSO valve closed could damage engine high pressure fuel pump

A

Start OFF
Emerg Fuel Shut off Lever FORWARD
FUELPumps ON
N1

32
Q

Loss of N1 andTrq
When a parameter is off line, the parameter value is not displayed onthe VEMD upper screen and the parameter scale symbology isdisplayed in yellow.The First Limitation Indicator (FLI) is replaced by the 3 datasymbology (N1/􀀧N1, TOT and TRQ) and a failure message isdisplayed.

A

GOVcan induce loss of N1 & Tq

comply with N1 limitations and TOT limit of 836C

33
Q

Audio Gong

A

Red Warning appears on CWP

34
Q

Audio Continuous Tone @ 310 HzNr below 360 rpm

A

reduce collective to maintain NR or power within limits

check engine parameters

35
Q

Audio Intermittent Tone @ 310 HzNr above 410 rpm

A

increase collective to maintain Nr in green arc

36
Q

Audio Continuous Tone @ 285 Hz

  • after 1.5 sec if power remains in transient range
  • immediately when transient power limits are exceeded
  • immediately when max transient rating is or will be exceeded during fast power increase
A

reduce collective to maintain NR or power within limits

check engine parameters

37
Q

ROTOR BRAKE INOP

A

WAIT UNTIL ROTOR COMES TO A STANDSTILL BEFORE LEAVING THE AIRCRAFT
Rotor stopping with wind blowing:
Park aircraft INTO WIND
Cyclic stick slightly INTO WIND.

38
Q

ICS inop
VHF communications remain available for the pilot only via COM 1 transceiver.
Audio warnings remain available only for the pilot.

A

check ICS ON

checkCOM 1 on & volume up

39
Q

AVCS fail or on continuously

3/rev vibration level increases significantly at high airspeeds when AVCS is off.

A

turn avcs OFF
after 30 sec avcs ON
fail light off - continue flt
fail light on - avcs OFF - continue flight

40
Q

Stuck Left Pedal
Decrease Collective or Increased Speed - nose right
Increase Collective or Decreased Speed - nose left

A

shallow approach - keep speed up - land strait with speed
or autorotate
or quickstop - as nose swings left throttle to idle

41
Q

Stuck Right Pedal
Decrease Collective or Increased Speed - nose right
Increase Collective or Decreased Speed - nose left

A

shallow approach to 6 ft @ 40-50 knots

approach to land with RH wind component

H130T2 (4 decks)

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