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FM > BA EP's > Flashcards

BA EP's Flashcards

1
Q 
Two or more of the following symptoms:
● Loss of MGB lubrication indicated on the EICAS page by
– MGB OIL P
– MGB PMP MAIN
– MGB PMP AUX
– MGB oil pressure at zero
– Possible rise in MGB oil temperature
● MGB CHIP
● Yaw kicks, abnormal MGB noises, or unusually high power
requirements.
A

MGB FAILURE IMMINENT

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2
Q

MGB FAILURE IMMINENT

A
  1. LAND/DITCH IMMEDIATELY
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3
Q 
One of the following symptoms:
● Drop in MGB oil pressure indicated on the EICAS page by:
– MGB OIL P
– Low MGB oil pressure.
– Possible rise in MGB oil temperature
● Loss of MGB lubrication indicated on the EICAS page by:
– MGB OIL P
– MGB PMP MAIN
– MGB PMP AUX
– MGB oil pressure at zero
– Possible rise in MGB oil temperature
● MGB CHIP
● MGB oil pressure greater than 80 psi
● Abnormal MGB noises
A

MGB MALFUNCTION

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4
Q 
Symptom:
● MGB FIRE light illuminated
Possible symptoms:
● Illumination of associated MGB related warnings and cautions
- MGB OIL P
- MGB OIL TEMP
- MGB PMP MAIN
- MGB PMP AUX
● Loss of MGB oil pressure and/or rise in temperature
● Drop in fuel and/or hydraulic pressure
● AC electrical system malfunctions
A

MGB FIRE

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5
Q

MGB FIRE

A
  1. CONFIRM FIRE

If fire confirmed:
2. LAND/DITCH IMMEDIATELY

If fire not confirmed:
3. LAND AS SOON AS POSSIBLE

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6
Q 
Symptoms:
● Engine FIRE light illuminated
● Red warning light illuminated on the corresponding EFSL
● Flames and/or smoke coming from engine compartment
Possible symptoms:
● ENG1 FUEL P , ENG2 FUEL P
● ENG1 OIL P , ENG2 OIL P
● ENG1 OIL TEMP, ENG2 OIL TEMP
● ENG1 CHIP, ENG2 CHIP
● Electrical system malfunctions
A

ENGINE COMPARTMENT FIRE INFLIGHT

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7
Q

ENGINE COMPARTMENT FIRE INFLIGHT

A
  1. CONFIRM FIRE
  2. SINGLE-ENGINE PROFILE - ESTABLISH

If fire confirmed (affected engine):

  1. FCS - CONFIRM; IDLE, CONFIRM; OFF
  2. EFSL - CONFIRM; OFF
  3. BOOST PUMPS - CONFIRM; OFF
  4. PRI FIRE EXTINGUISHER BUTTON - CONFIRM; PUSH
  5. SEC FIRE EXTINGUISHER BUTTON - CONFIRM; PUSH

If fire still persists:

  1. LAND/DITCH IMMEDIATELY
  2. LAND AS SOON AS POSSIBLE
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8
Q

Symptoms:
● Engine FIRE light illuminated
● Hand or voice signals from ground crew
● Red warning light illuminated on the corresponding EFSL

A

ENGINE COMPARTMENT FIRE ONDECK

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9
Q

ENGINE COMPARTMENT FIRE ONDECK

A
  1. CONFIRM FIRE
  2. FCSs - OFF
  3. EFSLs - OFF
  4. BOOST PUMPS - OFF
    If fire confirmed (affected engine):
  5. PRI FIRE EXTINGUISHER BUTTON - CONFIRM; PUSH
  6. SEC FIRE EXTINGUISHER BUTTON - CONFIRM; PUSH
  7. EMERGENCY ELECTRICAL CUTOFF
  8. ROTOR BRAKE
  9. EVACUATE
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10
Q

INTERNAL FIRE (CABIN, ELECTRICAL, AND/OR AVIONICS)

A

Symptoms:

● Smoke/fumes/sparks originating from a single component inside the cabin

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11
Q

INTERNAL FIRE (CABIN, ELECTRICAL, AND/OR AVIONICS) - EP

A
  1. CONFIRM/SUPRESS FIRE
  2. AFFECTED EQUIPMENT - OFF
  3. AFFECTED CIRCUIT BREAKERS - PULL
  4. HEAT/COOL SWITCHES - OFF
  5. RAM AIR, DOOR, WINDOW - CLOSED
  6. WHEELS/FLOATS - AS REQUIRED

If electrical or avionics fire persists:
7. EMERGENCY ELECTRICAL CUTOFF

If electrical or avionics fire persists:

  1. LAND/DITCH IMMEDIATELY
  2. LAND AS SOON AS POSSIBLE
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12
Q

SMOKE AND FUME ELIMINATION

A
  1. HEAT/COOL SWITCHES - OFF

2. RAM AIR, DOOR, WINDOW - OPEN

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13
Q

Symptoms:
● TOT rises rapidly after FCS has been placed in the OFF position
● TOT does not decrease after FCS has been placed in the OFF position

A

ENGINE POST-SHUTDOWN FIRE

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14
Q

ENGINE POST-SHUTDOWN FIRE

A
  1. EFSL - CONFIRM: OFF

If high TOT still evident after 10 seconds:
2. CRANK BUTTON - DEPRESS
If TOT continues to rise or does not decrease:
3. EMERGENCY ELECTRICAL CUTOFF
4. ROTOR BRAKE
5. EVACUATE

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15
Q

Symptoms:
● Known or suspected aircraft damage
● Abnormal vibrations

A

KNOWN OR SUSPECTED AIRCRAFT DAMAGE/ABNORMAL VIBRATIONS

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16
Q

KNOWN OR SUSPECTED AIRCRAFT DAMAGE/ABNORMAL VIBRATIONS

A

If severe vibrations and/or drastically altered flight characteristics:
1. LAND/DITCH IMMEDIATELY
If moderate vibrations:
2. LAND AS SOON AS POSSIBLE

17
Q

Symptom:
● Any uncommanded left yaw not attributable to mechanical failure of the tail
rotor drive system

A

UNCOMMANDED LEFT YAW

18
Q

UNCOMMANDED LEFT YAW

A
  1. PEDALS - FULL RIGHT DEFLECTION
  2. CYCLIC - FORWARD
  3. COLLECTIVE - REDUCE
  4. NR - HI
19
Q

Symptom:

● TGB CHIP

A

TGB CHIP

20
Q

TGB CHIP

A
  1. LAND AS SOON AS POSSIBLE
21
Q

THE BIG 4

A
  1. NR
  2. AIRSPEED/ALTITUDE
  3. WHEELS/FLOATS
  4. ANALYZE
22
Q

Symptoms:
● FADEC 1 FAIL or FADEC 2 FAIL
● Engine status light on overhead quadrant
● PFD TRQ display switches to OEI GOV mode
● Affected engine will not respond to collective movement due to fuel flow metering
being frozen at the rate present when the FADEC failed

A

FADEC FAIL

23
Q

FADEC FAIL

A
  1. TRNG SWITCH - FLT

2. FADEC BACKUP SWITCH (affected engine) - CONFIRM; BACKUP

24
Q

Symptom:

● Aircraft ondeck in unsafe condition

A

EMERGENCY SHUTDOWN PROCEDURE ONDECK

25
Q

EMERGENCY SHUTDOWN PROCEDURE ONDECK

A
  1. EFSLs - OFF
  2. EMERGENCY ELECTRICAL CUTOFF
  3. ROTOR BRAKE
  4. EVACUATE
26
Q 
Possible symptoms:
● BATT TEMP
● SFI Battery FAULT light
● Smoke and/or fumes from radome or vent
● Noises from radome
A

BATTERY OVERTEMPERATURE (AIRCRAFT OR SFI)

27
Q

BATTERY OVERTEMPERATURE (AIRCRAFT OR SFI)

A 
If the BATT TEMP is present:
1. BATT RELAY SWITCHES - BOTH OFF
2. SFI ACFT - OFF
If BATT TEMP is not present and the SFI FAULT light is illuminated with smoke
from radome:
3. SFI BATT and ACFT - OFF
If symptoms persist (smoke/fumes from radome or electrical malfunctions):
4. LAND AS SOON AS POSSIBLE

FM (4 decks)

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