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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
AP A.TRIM + P/R SAS + TRIM
1. Flight controls... hands on
26
Second AHRS failure AP A.TRIM + GYRO + AHRSi
1. Flight controls... hands on If operating IMC: 2. LAND ASAP
27
AP A.TRIM + TRIM
1. Flight controls... hands on
28
AUTOROTATION
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 10. BAT MSTER sw... OFF
29
Double engine failure flight
Autorotation... perform
30
Double engine failure - HIGE
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
Engine oil - Temp high
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
Engine overspend - drive shaft failure
1. OEI flight condition... establish 2. Affected engine... identify 3. Single engine emergency shutdown... perform
33
Engine overspeed - governing failure
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: 9. TWIST GRIP (affected engine)... reduce before lowering the collective lever to full down position (to keep N2/N(Ro) within limits)
34
Single engine failure - flight
1. OEI flight condition... establish 2. Affected engine... identify 3. Single engine emergency shutdown... perform
35
Single engine failure - HIGE
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
Single engine failure - HOGE
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
Single engine failure - takeoff
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
AHRS 1 and AHRS 2
If operating IMC: 2. LAND ASAP
39
Cabin Fire
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
Electrical fire/ short circuit (ground)
1. Double engine emergency shutdown... perform 2. Passengers... alert/evacuate 3. EPU, if connected... disconnect 4. Fire... extinguish if possible
41
Electrical fire / short circuit (in flight)
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
Abnormal vibration
LAND ASAP
43
Total electrical power loss
LAND ASAP
44
Tail Rotor Failure - Hover
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
Tail rotor failure / fixed pitch tail rotor control failure - FWD Flight
1. Collective lever... reduce to obtain minimum 2. Airspeed... maintain 70 KIAS or higher Test 6. Auto rotation... perform

EC135 (J) (5 decks)

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