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BV-107 > 107 EP’s > Flashcards

107 EP’s Flashcards

1
Q

EMERGENCY AIRCRAFT SHUTDOWN

A

ECL’s: stop
Fire T-handle: pull
Rotor brake: armed / engage
Master switch: off
“Emergency evacuation” A/R

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2
Q

EMERGENCY DESCENT

A

Lower collective to maintain NR
Airspeed: 120 kts or Vne
Back angle: Up to 30 degrees
Caution: At 500 AGL, Reconfigure for power on landing

“EMERGENCY AIRCRAFT SHUTDOWN” A/R

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3
Q

EMERGENCY EVACUATION

A

“EMERGENCY A/C SHUTDOWN” perform

Open emergency exits
Evacuate through nearest safe exit

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4
Q

EMERGENCY EVACUATION (WATER)

A

“EMERGENCY A/C SHUTDOWN” complete

Evacuation decision - notify crew/ pax to remain inside, with exits closed until directed otherwise

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5
Q

POST SHUTDOWN FIRE

(indicated by a RAPID rise in PTIT advice 250 C)

A

ECL’s (both) confirm/stop
Ignition switch OFF
Start button - motor

If fire persists: pull fire T-handle

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6
Q

ILLUMINATED ENGINE FIRE T-HANDLE

A

Confirm fire
ECL: confirm / STOP
Fire T-handle: confirm / PULL
Discharge bottle 1 and/or 2 A/R

If fire persists:
“EMERGENCY DESCENT”
Land as soon as POSSIBLE

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7
Q

CABIN AREA / COCKPIT FIRE ON GROUND

A

“EMERGENCY AIRCRAFT SHUTDOWN” perform
Fire extinguisher A/R
“EMERGENCY EVACUATION” A/R

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8
Q

CABIN AREA / COCKPIT FIRE IN FLIGHT

A

Land as soon as POSSIBLE

Checklist

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9
Q

ILLUMINATES HEATER FIRE T- HANDLE

A

Heater switch OFF
Heater Fire T-handle: confirm / PULL

If fire persists: discharge BOT 1

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10
Q

EMERGENCY ENGINE SHUTDOWN

A

ECL confirm / STOP
Fire T-handle confirm / PULL
Fuel boost pump confirm / OFF

Single engine flight

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11
Q

DUAL ENGINE FAILURE - HOVER

A

Adjust collective to cushion

(30 kts best cushion speed)

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12
Q

DUAL ENGINE FAILURE IN FLIGHT

A

Perform Autorotation

Best glide:
85 KIAS above 2600 DA
65 KIAS below 2600 DA

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13
Q

SINGLE ENGINE FAILURE

A

Collective - adjust to maintain NR
Adjust airspeed
Engine beeps - both max

Checklist

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14
Q

LOTS OF NF SIGNAL
(FLEX SHAFT FAILURE)

A

Ground:
ECL’s (both) STOP

Flight:
Collective - adjust to maintain NR (usually RAISE)

Checklist

(Fuel control senses NF @ 0 so sends all the fuel and affected engine goes to topping. Other engine reduces power since its load id reduced. Easy to mistake this as an engine failure initially since good engine is reducing power. Recognize ZERO NF on triple tach. Don’t shut down the good engine!)

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15
Q

ALL ABNORMAL ENGINE INSTRUMENT INDICATIONS OR WARNING LIGHTS

A

Check for secondary indications

Checklist

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16
Q

FOR EVERY EMERGENCY / ABNORMAL CONDITION:

A

Fly the aircraft
Contain RRPM

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17
Q

LAND IMMEDIATELY (definition)

A

Land without delay.

Pilots are to bear in mind that the consequences of continued flight are likely to be more hazardous than, for example, ditching, or landing in trees.

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18
Q

LAND AS SOON AS POSSIBLE (definition)

A

Land at the nearest suitable landing area (i.e. open field) without delay.

The consideration is the survival of occupants.

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19
Q

LAND AS SOON AS PRACTICABLE ( definition )

A

Land at the nearest suitable airfield/heliport.

Extended flight is not recommended.

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20
Q

EMERGENCY ENGINE SHUTDOWN (definition)

A

Shut down engine(s) without delay. Engine shutdown in flight is usually not an immediate action unless a fire exists.

Before shutting down an engine, identify the affected
engine by checking indications of RRPM, T5, engine oil
and fuel pressure.

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21
Q

OEI WATER LANDING / DITCHING

A

Checklist

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22
Q

ELECTRICAL FIRE - KNOWN SOURCE

A

System switch or breaker: OFF / PULL

If fire persists:
“CABIN / COCKPIT FIRE - FLIGHT” perform

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23
Q

ELECTRICAL FIRE - UNKNOWN SOURCE

A

Checklist

24
Q

HEATER OVERHEAT CAUTION LIGHT

A

Checklist

25
Q

SMOKE AND FUME ELIMINATION

A

Checklist

26
Q

ENGINE RESTART DURING FLIGHT

A

Checklist

27
Q

SINGLE ENGINE FLIGHT

A

Checklist

28
Q

ENG 1 or ENG 2 CHIP DET CAUTION LIGHT

A

Checklist

29
Q

NO. 1 or 2 ENG OIL PRESS LIGHT

A

Checklist

30
Q

NO. 1 or 2 ENGINE LOW OIL QTY LIGHT

A

Checklist

31
Q

ENGINE OIL TEMPERATURE HIGH (+121C)

A

Checklist

32
Q

NO. 1 or 2 LOW FUEL PRESSURE LIGHT

A

Checklist

33
Q

UNMATCHED ENGINES

A

Checklist

34
Q

EMERGENCY ENGINE TRIM CAUTION LIGHT
(FREEZE FAIL)

A

Checklist

35
Q

ENGINE OVERSPEED CAUTION LIGHT

A

Checklist

36
Q

XMSN OIL PRESS
caution light

A

Check for secondary indications
- pressure or temp gauges
- CHIP DETECTOR
- XMSN OIL TEMP caution
- zero NR
- abnormal noise / vibration

If secondary indication confirmed:
“IMMINENT XMSN FAILURE” perform

If no secondary indications:
Checklist

37
Q

XMSN OIL TEMP
CAUTION LIGHT
115 C

A

Check for secondary indications
- pressure or temp gauges
- CHIP DETECTOR
- XMSN OIL PRESSURE caution
- zero NR
- abnormal noise / vibration

If secondary indication confirmed:
“IMMINENT XMSN FAILURE” perform

If no secondary indications:
Checklist

38
Q

CHIP DETECTOR
CAUTION LIGHT

A

Check for secondary indications
- pressure or temp gauges
- XMSN OIL PRESSURE caution
- XMSN OIL TEMP caution
- zero NR
- abnormal noise / vibration

If secondary indication confirmed:
“IMMINENT XMSN FAILURE” perform

If no secondary indications:
Checklist

39
Q

IMMINENT TRANSMISSION FAILURE

A

Collective MIN power (do not autorotate)
Airspeed 65 KIAS
Minimize control inputs
Land IMMEDIATELY

40
Q

Nf OVERRUNNING Nr
(SPRAG CLUTCH NOT ENGAGED)

A

ECL (affected engine) confirm / STOP

Ground operations when Ng reaches 0:
ECL (engaged engine) confirm / STOP

41
Q

MAIN FUEL QUANTITY INDICATOR FAILURE

A

Checklist

42
Q

NO. 1 or 2 BOOST FAIL LIGHTS

A

Checklist

43
Q

FUEL CROSSFEED
(procedure)

A

Checklist

WARNING: Avoid nose low attitudes. Unless
necessary, crossfeed should be terminated
when quantity reaches 400 lbs in either tank.
Fuel starvation will result in a dual engine
flameout.

44
Q

NO. 1 or 2 TANK 25% FUEL LIGHT

A

Checklist

45
Q

NO. 1 or 2 AUX FUEL OVERFLOW LIGHT

A

Checklist

(close valve, turn off transfer pump)

46
Q

NO. 1 OR 2 GEN FAIL CAUTION LIGHT

A

Checklist

47
Q

NO. 1 AND 2 GEN FAIL CAUTION LIGHTS
(Dual Failure)

A

Checklist

48
Q

NO. 1 OR 2 RECT FAIL CAUTION LIGHT

A

Checklist

49
Q

NO. 1 AND 2 RECT FAIL CAUTION LIGHTS
(Dual Failure)

A

Checklist

50
Q

AC FEEDER FAIL LIGHT

A

Checklist

51
Q

AUX AC BUS FAIL LIGHT

A

Checklist

52
Q

TOTAL AC AND DC ELECTRICAL FAILURE -
ENGINE SHUT DOWN

A

Checklist

53
Q

NO. 1 OR 2 SAS FAIL LIGHT
(single & dual)

A

Checklist

Slow to 80 KIAS or Vne - 10
SAS Selector - select operable system or off if dual failure
Airspeed
- Max 110 KIAS VFR single SAS failure
- Max100 KIAS VFR dual SAS failure
- Max 80 KIAS IFR
Land as soon as PRACTICABLE

54
Q

AIRCRAFT CONTROL ERRATIC

A

Minimize control inputs
Reduces collective pitch

If control remains erratic:
SAS Selector OFF

If control remains erratic:
Land as soon as POSSIBLE

55
Q

GROUND RESONANCE

A

Become airborne

Or
Collective full down
“EMERGENCY SHUTDOWN” perform

56
Q

HYD BOOST FAIL LIGHT

A

Check cockpit and companionway gauges

If pressure(s) are normal:
Land as soon as PRACTICABLE

Any abnormal pressure indication:
“HYD BOOST FAIL LIGHT” perform

57
Q

NG indication and Engine Oil Pressure are lost simultaneously

A

Engine oil pump failure

(NG tach gen is driven by Engine Oil Pump)

Shut down engine

STM 7-16

BV-107 (2 decks)

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