Emergency procedures

Question 1

BAT on Warning Unit
OVHT and audio tone
and

BAT OVERHEAT on ML
and voice Message
“BATTERY OVERHEAT”

Answer 1

ON GROUND:
1 “BAT MSTR” sw - OFF
- BAT DISCON appear
2 Engines - Shut down

IN FLIGHT:
1 “BAT MSTR” sw - OFF
- BAT DISCON appear
2 “LAND ASAP”
3 Engine shutdown
4 Visual inspection No overheat sign VMC
5 Start-up
6 BAT MSTR sw - OFF
- BAT DISCON appear
7 LAND ASAPRACTICABLE

Question 2

GEN1 OVERHEAT

                   and/or   

                OVERHEAT         GEN2                 

             and audio tone

Answer 2

1. Affected GEN sw - OFF
   If caution disappears within one minute:
   
   2. Electrical load - Reduce
   3. Continue flight

If caution remains on for more than 1 minute:
2 “OEI flight condition - Establish”
3 “Affected engine - Identify”
4 “Single engine emergency shutdown “
5 LAND ASA PRACTICABLE

Question 3

Electrical fire/short circuit

                     ON GROUND  Odor of burning insulation and/or acrid smoke

Answer 3

1. “Double engine emergency shutdown
2. “Passengers -Alertevacuate”
3. “EPU, if connected -Disconnect”
4. “Fire -Extinguish ifpossible”

Question 4

Electrical fire/short circuit

                     IN FLIGHT

Odor of burning insulation and/or acrid smoke

Answer 4

1. “Both BUS TIE sw’s - OFF”
   ( BUS TIE OPEN)
   2.”GEN 1 and GEN 2 sw’s - OFF”
   (GEN DISCONECTED
   3.”Electrical consumers - Reduce ama possible”
   4.”Passengers - Alert”
2. Follow flow chart procedure

Question 5

ENG 1 and ENG 2
FAIL FAIL
and
ENG1 FAIL ENG2
and audio tone

Answer 5

“Autorotation”
1.”Collective lever - Reduce to maintainNr0”
2.”Airspeed - Vy / 90 Max rang / 60 Rod”
3.”Double engine emergency shutdown”
at approx. 100 ft
4.Flare attitude -15 20*
at approx. 8 - 12 ft
5.Flare attitude - reduce to approx. 10*
6. Heading -Maintain
7.Collective lever -Raise to stop desc and cushion
8.”BAT MSTR sw -OFF”

Question 6

ENG1 CHIP
or
CHIP ENG2
and audio tone

Answer 6

1. FUZZ BURN sw - 1s
2. Chip pulse event - record
3. Eng parameter - Monitor
   if ENG CHIP goes off:
4. Continue flight
   if ENG CHIP remain ON
5. “OEI flight condition -Establish”
6. “Affected engine - Identify”
   Alternative 1 : single eng emergency shutdown
   2 : ENG MAIN sw IDLE, check indications
7. LASA Practicable

Question 7

ENG1 FUEL FILTER
or
FUEL FILTER ENG2
and audio tone

Answer 7

ONE Land ASAPracticable

“Both Land ASAP”

Question 8

ENG1 OIL LOW PRESSURE
or
OIL LOW PRESSURE ENG2
and audio tone

Answer 8

1. “OEI flight condition -Establish”
2. VMD page -Select
3. Engine oil pressure indicator -Check
4. Affected engine -Identify
5. Single engine emergency shutdown
6. Land ASAPracticable

Question 9

ENG1 OVERSPEED N2 >120%
or
OVERSPEED ENG2
and audio tone

Answer 9

1. “OEI flight condition -Establish”
2. Affected engine -Identify
3. Single engine emergency shutdown
4. Land ASAPracticable

Question 10

ENG1                     FIRE
                                or
                              FIRE           ENG2
                              and 
              "FIRE ENG ONE FIRE"

Answer 10

1.”OEI flight condition -Establish”
2.”FIRE sw affected eng Raise guard, press
eng shutdown, ACTIVE, BOT1, FUEL VALVE CLSD
3.”BOT1/BOT2 pb - Press; bottle1 activated
- EXT indicator light on
(EMER OFF SW panel)
4. Clock stop watch - Start, after BOT1 and
EXT light extinguish
5. VMS page selected
6. Affected ENG - Ident
7. Single eng emergency shutdown
8. Passengers -Alert
If FIRE warning disappears:
9. LASAP
If FIRE warning is still on after 1 min
9. BOT1/BOT 2 pb - Press; Bottle 2 activated
- EXT indicator light on
(EMER OFF SW panel)
If FIRE warning remains on:
10. Land immediately

Question 11

CABIN FIRE

Answer 11

1.”Airspeed -Vy recommended”
2.”Passengers - Alert”
3.”Heating - OFF”
4.”Fire -Extinguish bif possible”
5.”Fumes, smoke - Eliminate, sliding door
windows and vents”
6.”LAND ASAP”
7.”After lending Double eng emergency shutdown”

Question 12

LOW and/or LOW on
FUEL1 FUEL2 WU

                           and FUEL1                     LOW                                      on ML "fuel one , low"

Answer 12

1.Fuel qty - Check
fuel qty positive
2.FUEL XFER PUMP A and F sw’s -Check on
3.FUEL XPMP A and F cb’s -Check in

if both LOW FUEL remain on
4.”Land within 8 min

if one LOW FUEL remain on
4.”Expect single eng failure after approx 10min

Question 13

TAIL ROTOR DRIVE FAILLURE

Landing surface hard enough (concrete asphalt ) and flat
Should permit running landing
Left crosswind is advantage

Answer 13

1.”Collective lever - Reduce to obtain min slideslip
2.”Airspeed - Maintain 70 or higher”
3.Select suitable landing area
4.”Shallow approach with nose left”
if airspeed can be reduced below appropriate low speed
5.”Airspeed reduced close to the ground until nose
aligned with landing direction”
6.”Landing”

if nose change from left to right

5. “Airspeed increase”
6. “Approach abort, climb for autorotation”
7. “Autorotation glide establish”
8. “Double eng emergency shutdown”
9. “Autorotation landing”

Question 14

MGB OIL P

Answer 14

1.”Power - reduce”
2.”Airspeed - set to Vy
3.”Land Immediately 15 min max”
dry run 30 min

Question 15

MGB HIGH TEMP

Answer 15

1.VMD page
2.”MGB oil temp and press - Check
in limit
3.Land ASAPracticable
Out of limit
3.”Power - Reduce amapossible
If indication remain out of limit
4.” Land ASAP

Question 16

ROTOR BRAKE

Answer 16

1. Rotor brake lever - Check
   if remain on
   2.”Land ASAP”

Question 17

AP on WU for 10s
and
AUTOPILOT
and audio tone + “hands on”

Answer 17

1. Flying controls - Hands-on
2. AP1 + AP2 - Re-engage (cyclic grip)
   if unsuccessful:
   3- Airspeed - Reduce to VNE AP OFF
   110 kt
   4- LASA Practicable

Question 18

AFT FUEL PUMP

and audio tone

Answer 18

1. fuel level in the main tank - Check
2. FUEL XFER PUMP A sw - Check ON
3. FUEL XPMP-A cb - Check in

in the event of aft fuel transfer pump failure the main tank unusable fuel increase to 33l / 26 kg
FWD 16 L / 13 kg

Question 19

JET FUEL PUMP

and audio tone

Answer 19

1. FUEL XFER PUMP A sw - Check ON

If caution remains on, the main tank unsuable 72l / 58kg

Question 20

FUEL QTY DEG

and audio tone

Answer 20

the degraded fuel qty indication represents the minimum fuel level within pitch attitude ranges of -3 to +6
aircraft weight calculation will be incorrect
1. Level flight - Establish, 100kt if feasible
2. Fuel qty - Check
3. Remaining flight time - Verify dest can be reached with remainingfuel
4. Alternative destination - Select if required

Question 21

AFT + FWD FUEL PUMP

and audio tone

Answer 21

1. Fuel level in the main tank - Check
2. FUEL XFER PUMP A and F sw - Check ON
3. FUEL XPMP-A and F cb - Check in
   when FUEL RESERVE appears:
4. LAND WITHIN 20 MIN