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EC 135 Procedures > Caution > Flashcards

Caution Flashcards

0
Q

BUSTIE OPN

A
  1. GEN AMPS. - Verify normal value
    Normal value:
  2. LAND ASA PRACTICABLE

if one GEN AMPS value shows XXX

  1. Failed system. - GEN sw OFF
  2. LAND ASA PRACTICABLE

if both GEN AMPS show XXX
2. Double GEN DISCON procedure
30min on battery

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1
Q

BAT DISCON

A
  1. BAT MSTR sw. - Reset, then ON
    If caution remain ON
  2. LAND ASA PRACTICABLE
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2
Q

CAD DEGR

A
  • Failure of CAD lane
    Or
  • Failure of both VEMD lanes
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3
Q

CAD FAN

A

Do not start

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4
Q

CPDS OVHT

A
  1. Pull for heating/defog knob. - Push
  2. Pull for AIR knob. - Pull
  3. VENT SYST rheostat - Turn to MAX

if caution remain ON
4. land within 30 min

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5
Q

DEGRADE

system I and/or II

A

Caution:

  • Avoid using Max pwr and perform pwr variation slowly
  • Maintain TQ>20% on each engine
  • In case of eng main sw failure for shutdown, use twist grip
  1. Engine parameter. - Monitor ( compare with normal engine)
  2. LAND ASA PRACTICABLE

After landing

  1. Normal eng shutdown
  2. CAD (SYS 1/2). - Check for FADEC FAIL
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6
Q

ENG CHIP

A

” ON GROUND”
“1. Eng ident”
“2. Single eng emer shutdown”

“ON FLIGHT”
“1. OEI flight condition”
2. ENG CHIP sw. - BURN 1”
3. Chip pulse event record

If ENG CHIP remain ON

“4. Eng ident”
Alternative 1: “Single eng emer shutdown”
Alternative 2: “ ENG main sw. - IDLE”. If needed for landing
6. LASA PRACTICABLE

If ENG CHIP extinguish a second activation will be authorised

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7
Q

ENG CHP CT

A

ENG CHIP CAUTION IS NOT AVAILABLE

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8
Q

ENG FAIL

A

1 “ OEI flight conditions”
2 “ affected eng Ident”
3 “ Single eng emer shutdown perform”
4 LASA PRACTICABLE

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9
Q

ENG O FILT

A

1- eng Oil t&p Monitor

2- LASA PRACTICABLE

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10
Q

ENG OF CT

A

Eng O Filt caution is not available

Do not start

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11
Q

FIRE EXT

A

Fire extinguishing system is active

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12
Q

FADEC FAIL

A

1-“Collective lever Adjust to maintain NRo within normal range”

2-“Affected eng Ident by small chge”
3-“Respective TWIST GRIP Adjust slowly to set
80% (+-2%) N1 on the affected eng
Simultaneously adjust collective to maintain
eng within limits.
(When the OAT is below –10_C, adjust N1 to 77% ($ 2%) instead of 80%.)

AND AVOID QUICK TWIST GRIP ROTATIONS. HOLD MIN. 10% TORQUE ON THE NORMAL ENGINE TO MAINTAIN AUTOMATIC CONTROL OF VARIABLE NRO IN ACCORDANCE WITH SECTION 7, FLM EC 135 T2 (CPDS).

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13
Q

FLI DEGR

A

1- do not try to match the needles when different parameters are designated as first limit
Avoid using max Pwr. Use the needle of the other engine for limit indication
2-LASA PRACTICABLE

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14
Q

FLI FAIL

A
  1. Do not try to trim engines

2. LASA PRACTICABLE

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15
Q

F PUMP AFT and FWD

A
  1. Fuel qty. check
  2. FUEL PUMP XFER-A and XFER-F sw+ cb. Check on
    Remaining flight 30min Vy / 20min at max range
16
Q

F PUMP AFT

A

1- Fuel level main tank Chck

Qty ok

2- FUEL PUMP XFER-A sw ON
3- XFER-A pump cb Chck in
If remain on

4- FUEL PUMP XFER-A sw OFF

QTY LOW

2- FUEL PUMP XFER-A sw OFF

in hover condition the unusable fuel can be up to 71 kg
Qty unusable can be reduce to 7.5 kg when flying with 80 kias or more

17
Q

F PUMP FWD

A

1- Fuel level main tank Chck

Qty ok

2- FUEL PUMP XFER-F sw ON
3- XFER-F pump cb Chck in

If remain on
4- FUEL PUMP XFER-F sw OFF

QTY LOW

2- FUEL PUMP XFER-F sw OFF

in forward flight condition the unusable fuel can be up to 59 kg
Qty unusable can be reduce to 3.6 kg when flying with 80 kIAS or less

18
Q

F QTY DEGR

A

The degraded fuel qty indication represent the minimum fuel level within pitch attitude range -3 +6

Set pitch between 0 +/-1 before reding fuel qty, the calculate remaining flight endurance

19
Q

F QTY FAIL

A

The fuel qty has failed

DO NOT calculate flight endurance according the fuel qty indication
Fuel qty information only by LOW FUEL warning

LASA PRACTICABLE

20
Q

FUEL

A

1- fuel qty chck

If fuel in the main
2- FUEL PULP XFER-A-F Chck on

If 0 in the main
2- FUEL PULP XFER-A-F Chck oFF

3- LASA PRACTICABLE

21
Q

FUEL FILT

A

“One caution”
LASA PRACTICABLE

“Both caution”
“LASAP”

22
Q

FUEL PRESS

A

1- FUEL PRIME PUMP sw ON
2- LASA PRACTICABLE

be prepared for eng failure

23
Q

FUEL VALVE

A

LASA PRACTICABLE

24
Q

GEN DISCON

I or II

A

1- Affected GEN sw OFF
2- DC V, GEN AMPS and BAT AMPS chck

If battery is discharged
3- Electrical consumers Reduce
4- LASA PRACTICABLE

25
Q

GEN DISCON

I and II

A

Only ESS BUS I+ II are available

1- Both GEN sw     OFF
2- Electrical consumers Reduce
3- SHED BUS sw   EMER ON
4- DC VOLT and BAT AMPS CHCK
   below 62A during landing
              51A during cruise 
5- Land within 30mn

During IFR
“5- LASAP”

26
Q

GEN OVHT

A

“1- Affected GEN sw OFF”

1mn caption still ON

2- OEI conditions
3- affected eng Ident
4- Single eng emer shutdown
5- LASA PRACTICABLE

27
Q

HYD PRESS

A

Warning: do not operate Hyd test in flight
Extended flight with failed Hyd should be avoided

In case of HYD PRESS II failure YAW servo boost will be lost. Pedal forces will increase

LASA PRACTICABLE

28
Q

OVSP

A

On ground
Do not start

On flight
LASA PRACTICABLE
affected eng is no longer protected against pwr turbine overspend

29
Q

REDUND

I and or II

A

LASA PRACTICABLE

30
Q

ROTOR BRK

A

1- chck lever

“2- LASAP”

31
Q

XMSN OIL P
System 1 OR 2

Oil pressure in respective pump below minimum

A

“1- XMSN OIL P chck normal range

2- LASA PRACTICABLE

32
Q

XMSN CHIP

A

1- XMSN oil P chck

2- LASA PRACTICABLE

33
Q

XMSN OIL T

115*c light trigger

A

“1- XMSN oil T&p chck”

Within limits
2- LASA PRACTICABLE

Out of limits
2- pwr reduced as much as possible

If oil T remains out of limits
“3- LASAP”

34
Q

ENG OIL P

A 
************
Mini       1.3 bar
Cont       1.3 - 5 bar
Caution     5 - 10 bar
Max          10 bar

For eng start 10 - 15 bar max 2 min

1: Check OIL P

Normal range: LASA Practicable

Out of range:

    - OEI condition
    - Ident / Idle. / Off
    - LASA Practicable

EC 135 Procedures (4 decks)

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