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EC135 (J) > Boldface > Flashcards

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1
Q

AP A.TRIM (W)

A

Flight Controls…. Hands on

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2
Q

BAT TEMP (W)

A

On Ground:
1. BAT MSTR sw… OFF

In Flight:
1. BAT MSTR sw… OFF
2. LAND ASAP

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3
Q

FIRE (ENGINE 1) or FIRE (ENGINE 2) (W)

A

On Ground:
1. Respective EMER OFF sw… Open switch guard, press and release
2. Both FUEL PRIME PUMPS… OFF
3. Both ENG MAIN sw…. OFF

In Flight
1. OEI Flight Condition… Establish
2. Respective EMER OFF sw… Open switch guard, press and release
3. Affected engine… Identify
4. Single engine emergency shutdown… Perform (E-120)
IF FIRE WARNING light is off:
5. LAND ASAP
IF FIRE WARNING light remains on:
5. LAND IMMEDIATLEY

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4
Q

LOW FUEL (SYSTEM 1) or LOW FUEL (SYSTEM 2) (W)

A
  1. Clock… start stopwatch
    If both LOW FUEL warning lights are on:
  2. LAND WITHIN 10 MINUTES
    OR
    If LOW FUEL Warning light is on:
  3. FUEL quantity indication… check
    If both LOW FUEL Warning lights remain on:
  4. LAND WITHIN 10 MINUTES
    If one LOW FUEL warning light remains on:
  5. Expect single engine failure after approx. 10 minutes
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5
Q

ROTOR RPM (W)

A
  1. Rotor RPM Indicator… Check
  2. Collective Lever… Adjust as necessary to maintain N(RO) [Rotor speed] within normal range.
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6
Q

XMSN OIL P (W)

A

LAND ASAP

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7
Q

ENG CHIP (SYSTEM 1) or ENG CHIP (SYSTEM 2)

A

On Ground:
1. Affected engine… Identify
If ENG CHIP caution indication remains on:
5. Single engine emergency shutdown… Perform

In Flight:
1. OEI Flight condition… Establish
If ENG CHIP caution indication remains on:
5. Affected engine… Identify
OPTION 1:
6. Single engine emergency shutdown… Perform (E-120)
OR
OPTION2:
6. ENG main switch… Idle

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8
Q

ENG FAIL (SYSTEM 1) or ENG FAIL (SYSTEM 2)

A
  1. OEI Flight condition… Establish
  2. Affected engine… Identify
  3. Single engine emergency shutdown… Perform (E-120)
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9
Q

ENG OIL P (SYSTEM 1) or ENG OIL P (SYSTEM 2)

A

If Indication is out of limit:
2. OEI Flight condition… Establish
3. Affected engine… Identify
4. Single engine emergency shutdown… Perform (E-120)

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10
Q

FADEC FAIL (SYSTEM 1) or FADEC FAIL (SYSTEM 2)

A
  1. Collective Lever… Adjust as necessary to maintain N(RO) within normal range
  2. Affected engine… Identify by small collective changes
  3. Respective TWIST GRIP… Adjust slowly to set 80% (+ or - 2%) N(1) [Gas generator] on the affected engine (TWIST GRIP caution my come on). Simultaneously adjust collective to maintain engine within limits
    After Landing:
  4. Respective TWIST GRIP… Reduce, before lowering the collective pitch lever to full down position (to keep N(2) [power turbine speed] /N(RO) [rotor speed] within limits
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11
Q

FUEL FILT (SYSTEM 1) or FUEL FILT (SYSTEM 2)

A

If both caution indications:
LAND ASAP

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12
Q

GEN DISCON (SYSTEM 1) and GEN DISCON (SYSTEM 2)

A

If operating IMC:
6. LAND ASAP

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13
Q

GEN OVHT (SYSTEM 1) or GEN OVHT (SYSTEM 2)

A
  1. Affected GEN switch… OFF
    If GEN OVHT caution remains on for more than 1 minute:
  2. OEI Flight condition… Establish
  3. Affected engine… Identify
  4. Single engine emergency shutdown… Perform (E-120)
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14
Q

ROTOR BRK

A

If the ROTOR BRK caution remains on:
2. LAND ASAP

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15
Q

SHED EMER

A

If operating IMC:
3. LAND ASAP

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16
Q

XMSN OIL P (SYSTEM 1) or XMSN OIL P (SYSTEM 2)

A
  1. XMSN oil pressure indicator… Check in normal range
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17
Q

XMSN OIL T

A
  1. XMSN oil temperature and oil… Check pressure indication
    If Indications are out of limits:
  2. Power… Reduce as much as possible
    If oil temperature indication remains out of limits:
  3. LAND ASAP
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18
Q

Single Engine Emergency Shutdown

A
  1. ENG MAIN sw (Affected engine)… IDLE, check indications, then OFF
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19
Q

Double Engine Emergency Shutdown

A

On Ground:
1. Both ENG MAIN sw… OFF
2. Both FADEC sw… OFF
3. Both fuel PRIME PUMP sw… OFF
4. BAT MSTR sw… OFF
If there is an indication that the engines are still running:
5. Both TWIST GRIPS… Turn to shut off

In Flight
1. Both ENG MAIN sw… OFF
2. Both FADEC sw… OFF
If there is an indication that the engines are still running:
3. Both TWIST GRIPS… Turn to shut off

20
Q

AP A.TRIM (W) + ACTUATION + TRIM

A
  1. Flight controls… hands on
21
Q

AP A.TRIM + GYRO + TRIM

A
  1. Flight controls… hands on
22
Q

GYRO + AHRSi + ATT

A
  1. Flight controls… hands on
  2. RCU… Reconfigure to valid AHRS
23
Q

AP A.TRIM + AUTOPILOT

A
  1. Flight controls… hands on
24
Q

Reconfigured AHRS
AP A.TRIM + GYRO + AHRS (1 or 2)

A
  1. Flight controls… hands on
    If operating IMC:
  2. LAND ASAP
    OR
25
Q

AP A.TRIM + P/R SAS + TRIM

A
  1. Flight controls… hands on
26
Q

Second AHRS failure
AP A.TRIM + GYRO + AHRSi

A
  1. Flight controls… hands on
    If operating IMC:
  2. LAND ASAP
27
Q

AP A.TRIM + TRIM

A
  1. Flight controls… hands on
28
Q

AUTOROTATION

A
  1. Collective lever… reduce to maintain N(Ro) within limits
  2. Airspeed… 75 KIAS recommended
  3. Double eng emer shutdown… perform (page E-110)
    After touchdown
  4. BAT MSTER sw… OFF
29
Q

Double engine failure flight

A

Autorotation… perform

30
Q

Double engine failure - HIGE

A
  1. Right pedal… apply as necessary to stop yaw
  2. Landing attitude… establish
  3. Collective lever… raise as necessary to cushion landing
    After steady ground contact:
  4. Collective lever… lower rapidly
31
Q

Engine oil - Temp high

A
  1. Airspeed… increase if possible
    If engine oil remains above limit:
  2. OEI flight condition… establish
  3. Affected engine…. identify
  4. Engine main sw… ground idle
  5. Oil temp indicator… monitor
    If engine oil temperature remains above limit:
  6. Single engine emergency… perform
32
Q

Engine overspend - drive shaft failure

A
  1. OEI flight condition… establish
  2. Affected engine… identify
  3. Single engine emergency shutdown… perform
33
Q

Engine overspeed - governing failure

A
  1. Collective lever… Raise to maintain N2 and N(RO) within limits
  2. Affected engine… identify
  3. TWIST GRIP (affected engine)… reduce torque until the normal engine takes the load (TWIST GRIP and DEGRADE caution comes on)
  4. Collective lever… readjust as required to stay within limits
  5. ENG MODE SEL sw (affected engine)… MAN
  6. TWIST GRIP (affected engine)… adjust torque manually to 20-30% according to weight and ambient conditions
  7. Collective lever… readjust as necessary without changing TWIST GRIP position
    After landing:
  8. TWIST GRIP (affected engine)… reduce before lowering the collective lever to full down position (to keep N2/N(Ro) within limits)
34
Q

Single engine failure - flight

A
  1. OEI flight condition… establish
  2. Affected engine… identify
  3. Single engine emergency shutdown… perform
35
Q

Single engine failure - HIGE

A
  1. Collective lever… adjust to maintain rotor RPM
  2. Landing attitude… establish
  3. Collective lever… raise as necessary to stop descent and cushion landing
    After landing:
  4. Affected engine… identify
  5. Single engine emergency shutdown… perform
36
Q

Single engine failure - HOGE

A
  1. Airspeed… increase if possible
  2. Collective lever… adjust to maintain rotor RPM
    If forced landing required:
  3. Landing attitude… establish
  4. Collective lever… raise as necessary to stop descent and cushion landing
    After landing:
  5. Affected engine… identify
  6. Single engine emergency shutdown… perform

Or

If transitioning to OEI flight:
3. Airspeed… gain 65KIAS
4. Collective lever… adjust to OEI-limits or below
After reaching safe altitude:
5. Collective lever… reduce to OEI MCP or below
6. Affected engine… identify
7. Single engine emergency shutdown… perform

37
Q

Single engine failure - takeoff

A
  1. Collective lever… adjust to maintain rotor RPM
    If performing a rejected takeoff:
  2. Landing attitude… establish
  3. Collective lever… raise as necessary to stop descent and cushion landing
    After landing:
  4. Affected engine… identify
  5. Single engine emergency shutdown… perform

If transitiong to OEI - flight:
2. Collective lever.. adjust to OEI-limits or below
3. Airspeed… gain, 65KIAS (VY)
After reaching safe altitude:
4. Collective lever… reduce to OEI MCP or below
5. Affected engine… identify
6. Single engine emergency shutdown… perform

38
Q

AHRS 1 and AHRS 2

A

If operating IMC:
2. LAND ASAP

39
Q

Cabin Fire

A

On ground:
1. Double engine emergency shutdown… perfrom
2. Passengers… alert/evaluate
3. Fire… extinguish if possible
In flight:
1. Airspeed… reduce, if necessary (65 KIAS recommend)
2. Passengers… alert
3. Heating/air conditioning… OFF
4. Fire… extinguish if possible
5. Fumes, smoke… eliminate, open sliding doors, windows and vents
6. LAND ASAP
After landing:
7. Double engine emergency shutdown… perform

40
Q

Electrical fire/ short circuit (ground)

A
  1. Double engine emergency shutdown… perform
  2. Passengers… alert/evacuate
  3. EPU, if connected… disconnect
  4. Fire… extinguish if possible
41
Q

Electrical fire / short circuit (in flight)

A

In flight:
1. Both BUS TIE sw’s… OFF
2. Both BUSTIE OPN cautions… ON
3. DC volts, GEN amps and BAT amps… compare, note higher load
4. BAT MSTR sw… OFF
If fire/smoke eliminated:
5. LAND ASAP
OR
If fire/ smoke continues:
5. Respective GEN sw (higher load)… OFF
If fire/smoke elminated:
7. LAND ASAP
OR
If fire/smoke continues:
7. Both GEN sw’s… NORM
9. Other GEN sw… OFF
If fire/smoke eliminated :
11. LAND ASAP
OR
11. Both GEN sw’s… OFF
12. LAND ASAP

42
Q

Abnormal vibration

43
Q

Total electrical power loss

44
Q

Tail Rotor Failure - Hover

A

HIGE
1. Both TWIST GRIPS…. turn to minimum
2. Landing attitude… establish
3. Collective lever… apply as necessary
After landing:
4. Double engine emergency shutdown… perform

HOGE
1. Collective lever… reduce immediately
2. Both TWIST GRIPS… turn to minimum
If height permits:
3. Airspeed… gain
4. Collective lever… raise to stop descent and cushion
After landing:
5. Double engine emergency shutdown… perform

45
Q

Tail rotor failure / fixed pitch tail rotor control failure - FWD Flight

A
  1. Collective lever… reduce to obtain minimum
  2. Airspeed… maintain 70 KIAS or higher

Test

  1. Auto rotation… perform

EC135 (J) (5 decks)

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