BE30 - Malfonctions (SOP Drills) Flashcards

1
Q

Abnormal & Emergency situation -
Sequence

A

1) Fly

2) Vital actions
- Identifiy situaton
- Silence & cancel warnings
- Complete vital actions

3) Navigate
- Climb to FRA
- Fly ASAP

4) Complete vital actions, if required

5) Standby ATC & PAX

6) 1500’ AAE
- Set MCP

7) Decide WHERE TO?
- MSA
- Direction (Hold, continue, etc.)

8) Advise ATC
- Navigation intentions
- Declare Emergency

9) Emergency Checklist

10) Normal Checklists

11) TESTRA

12) Consider advice from Dispatch / MEL

13) Plan return
- Weather?
- Radio/Nav setup
- Approach briefing
- Landing considerations

14) Revise sequence
- Have you missed anything?

15) Descent & In-Range checklists

16) Request approach

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2
Q

Engine FAILURE after V1 -
With Autofeather (or) unscheduled feather

A

FCM = ‘‘Malfonction’’

PF = ‘’ CONFIRM MAX POWER & FAIL / FEATHER / FIRE ‘’
* PM = ‘’ POWER SET ‘’
* PM = ‘’ X ENGINE FAILED & FEATHERED’’

PF = Confirm postive rate, then ‘‘GEAR UP’’
* PM = ‘‘GEAR UP’’

PF = ‘’ CALL FRA ‘’
* PM = ‘‘FRA’’

PF = Accelerate Vtarger, then ‘‘FLAPS UP’’
* PM = ‘‘Flaps up’’

PF = Accelerate Vyse (125), then ‘’ IAS’’
* PM = ‘‘IAS’’

PF = ‘’ STANDBY ATC & PAX ‘’
* PM = to ATC, ‘’ INUIT 555, PANPAN (x3), Emergency in progress, standby’’
* PM = to PAX, ‘‘Remain seated (x3)’’

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3
Q

Engine FAILURE after V1 -
WITHOUT Autofeather

A

FCM = ‘‘Malfonction’’

PF = ‘’ CONFIRM MAX POWER & FAIL / FEATHER / FIRE ‘’
* PM = ‘’ POWER SET ‘’
* PM = ‘’ X ENGINE FAILED & NOT FEATHER’’

PF = Confirm postive rate, then ‘‘GEAR UP’’
* PM = ‘‘GEAR UP’’

PF = ‘’ X ENGINE MANUAL FEATHER DRILL’’
* PM = ‘’ X PROP LEVER’’
* PF = ‘’ CONFIRMED, FEATHER ‘’
* PM = ‘’ FEATHERED ‘’

PF = ‘’ CALL FRA ‘’
* PM = ‘‘FRA’’

PF = Accelerate Vtarger, then ‘‘FLAPS UP’’
* PM = ‘‘Flaps up’’

PF = Accelerate Vyse (125), then ‘’ IAS’’
* PM = ‘‘IAS’’

PF = ‘’ STANDBY ATC & PAX ‘’
* PM = to ATC, ‘’ INUIT 555, PANPAN (x3), Emergency in progress, standby’’
* PM = to PAX, ‘‘Remain seated (x3)’’

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4
Q

Engine FAILURE - In flight

A

FCM = ‘‘Malfonction’’

PF = ‘’ MAX POWER & FLAPS UP, GEAR UP ‘’
* PM = ‘’ MAX POWER & FLAPS UP, GEAR UP ‘’

PF = Maintain Vyse (125)
* If at high altitude, monitor speed for drift down

PF = ‘’ CONFIRM FAIL / FEATHER / FIRE ‘’
* PM = ‘’ X ENGINE FAILED & NOT FEATHER’’
* PF = ‘’ X SHUTDOWN DRILL’’

PM = ‘’ X CONDITION LEVER ‘’
* PF = ‘’ CONFIRMED, CUT OFF’’
* PM = ‘‘CUT OFF’’

PM = ‘’ X PROP LEVER’’
* PF = ‘’ CONFIRMED, FEATHER ‘’
* PM = ‘’ FEATHERED ‘’

PM = ‘’ X FIREWALL VALVE ‘’
* PF = ‘’ CONFIRMED, CLOSE ‘’
* PM = ‘’ CLOSED ‘’

PM = ‘’ SHUTDOWN DRILL COMPLETE ‘’

FCM = Continue emergency sequence

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5
Q

Engine FIRE - In flight

A

FCM = ‘‘Malfonction’’

PF = ‘’ MAX POWER & FLAPS UP, GEAR UP ‘’
* PM = ‘’ MAX POWER & FLAPS UP, GEAR UP ‘’

PF = Maintain Vyse (125)
* If at high altitude, monitor speed for drift down

PF = ‘’ CONFIRM FAIL / FEATHER / FIRE ‘’
* PM = ‘’ X ENGINE FIRE ‘’
* PF = ‘’ X FIRE DRILL ‘’

PM = ‘’ X CONDITION LEVER ‘’
* PF = ‘’ CONFIRMED, CUT OFF’’
* PM = ‘‘CUT OFF’’

PM = ‘’ X PROP LEVER’’
* PF = ‘’ CONFIRMED, FEATHER ‘’
* PM = ‘’ FEATHERED ‘’

PM = ‘’ X FIREWALL VALVE ‘’
* PF = ‘’ CONFIRMED, CLOSE ‘’
* PM = ‘’ CLOSED ‘’

PM = ‘’ X FIRE EXTINGUISHER ‘’
* PF = ‘’ CONFIRMED, PUSH ‘’
* PM = ‘’ PUSHED ‘’

PM = ‘’ FIRE DRILL COMPLETE ‘’

FCM = Continue emergency sequence

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6
Q

Engine FIRE - After V1
(takeoff continued)

A

FCM = ‘‘Malfonction’’

PF = ‘’ CONFIRM MAX POWER & FAIL / FEATHER / FIRE ‘’
* PM = ‘’ POWER SET ‘’
* PM = ‘’ X ENGINE FIRE ‘’

PF = Confirm postive rate, then ‘‘GEAR UP’’
* PM = ‘‘GEAR UP’’

PF = ‘’ CALL FRA ‘’
* PM = ‘‘FRA’’

PF = Accelerate Vtarger, then ‘‘FLAPS UP’’
* PM = ‘‘Flaps up’’

PF = Accelerate Vyse (125), then ‘’ IAS’’
* PM = ‘‘IAS’’

PF = ‘’ X ENGINE FIRE DRILL ‘’

PM = ‘’ X CONDITION LEVER ‘’
* PF = ‘’ CONFIRMED, CUT OFF’’
* PM = ‘‘CUT OFF’’

PM = ‘’ X PROP LEVER’’
* PF = ‘’ CONFIRMED, FEATHER ‘’
* PM = ‘’ FEATHERED ‘’

PM = ‘’ X FIREWALL VALVE ‘’
* PF = ‘’ CONFIRMED, CLOSE ‘’
* PM = ‘’ CLOSED ‘’

PM = ‘’ X FIRE EXTINGUISHER ‘’
* PF = ‘’ CONFIRMED, PUSH ‘’
* PM = ‘’ PUSHED ‘’

PF = ‘’ STANDBY ATC & PAX ‘’
* PM = to ATC, ‘’ INUIT 555, MAYDAY (x3), Emergency in progress, standby’’
* PM = to PAX, ‘‘Remain seated (x3)’’

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7
Q

Single Engine Missed Approach

A

PF = ‘’ GO AROUND, MAX POWER, FLAPS APPROACH ‘’
* PM = POWER SET, FLAPS APPROACH’’

PM = ‘’ POSITIVE RATE ‘’
* PF = ‘’ GEAR UP ‘’

PM = ‘’ FRA ‘’

PF = Accelerate Vtarger, then ‘‘FLAPS UP, HDG/NAV’’
* PM = ‘‘HDG/NAV’’

PF = Accelerate Vyse (125), then ‘’ IAS’’
* PM = ‘‘IAS’’

PM = ‘‘1500 FEET ‘’ (AAE)
* PM = ‘’ AFTER TAKEOFF CHECKLIST’’

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8
Q

Rejected Takeoff

A

CPT = ‘’ REJECT ‘’

FO = Standby ATC
* ‘’ INUIT 555, RAJECTING TAKEOFF ON RWY XX, STANDBY ‘’

FCM =
* Determine nature of emergency
* Determine if an evacution is required

CPT = Completes [x] DRILL by flow

CPT = ‘’ ADVISE ATC & PAX ‘’
* FO (to pax) = ‘‘REMAIN SEATED (x3) ‘’
* FO (to ATC) = ‘’ ………….’’

CPT = “Confirm ATC advised?”
* FO = ‘’ Confirmed ‘’

If evacuation required….

CPT =
* Pressurization switch = DUMP
* Cabin lights = ON (at night)
* Seat belt signs = OFF

CPT (announce to passenger) =
* ‘’ EVACUATE (x3)’’ [or] ‘‘RAPID DEPLANE (x3)’’ - as per the situation
* ‘’ Captain’s [or] First Officer side ‘’

CPT =
* Commands FO to evacuate wt. pax

FO =
* Grabs cockpit fire extinguisher & evacuates pax

CPT =
* Gang bar = DOWN (if daylight)
* Bat Bus switch = EMER OFF
* CVR CB = PULL

CPT =
* Grabs door fire extinguisher & assists evacuation from inside

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9
Q

STALL

  • Signs
  • Drill
A

SIGNS
* Buffet
* Buzzer
* 90 kts (clean)
* 105 kts (dirty)]

DRILL

FCM = ‘‘STALL’’

PF = ‘’ Stall. Max Power’’
* Disconnects AP
* Releases back pressure & advances power levers

PM = ‘‘Power set’’

PF = Once airspeed builds up, executes a smooth recover

PM = ‘’ Positive rate’’
* PF = ‘‘Flaps up. Gear up’’

PM = ‘‘125 kts’’
* PF = ‘‘Yaw Damp ON. Climb Power’’

PM = ‘‘Climb power set. Your levers’’
* PF = ‘‘After takeoff checklist’’

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10
Q

Windshear

A

FCM = ‘’ WINDSHEAR ‘’

PF : ‘’ Windshear. Max Power ‘’
* Advances power levers
* Rotates 10deg nose up, up to Vx (125)

PM : ‘‘Max Power Set’’
* Props FULL FORWARD
* Sets Max Power

Note = Do not change the configuration if the vertical path is NOT under control.

If the AC is still descending :

PF : ‘’ Firewall power’’’
* Pitch up, until the AC stops descending
* Never below Vx (125)

FCM : Resume with missed approach procedure & drill

Do not change the configuration if the vertical path is NOT under contro

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11
Q

Rapid Decompression

A

1a) Oxygen masks = ON
1b) Mic Selector Switch = MASK

2) Passenger Manual Drop-Out = PULL ON

3) Consider if descent is requied

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12
Q

Emergency Descent

A

1) Oxygen masks = As required

2) Power levers = IDLE
3) Prop levers = FULL FWD
4) Flaps & Gear = UP & UP
5) Airspeed = Vmo

PM = Set highest of MOCA (or) 10,000’ in the altitude box

PM = Seatbelt signs ON

PM = Advises ATC, ‘‘MAYDAY (3x)…’’
PM = Standby Pax, ‘‘Emergency Descent, (3x) Remain Seated’’

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13
Q

Which situation may lead to an evacuation ?

A

1) Fire, smoke or fumes
2) Forced landing / Ditching

If required
3) Rejected Take-off
4) Emergency Shutdown

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14
Q

Post-Evacuation tasks

A

1) Count PAX

2) Locate PAX at a safe distance

3) Ensure medical attention is provided to PAX who requires it

4) Ensure PAX protected from environmental conditions

5) Ensure PAX do not return to the aircraft

6) Ensure AC is protected from further damage

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15
Q

Which (3x) situations require a MAYDAY?
[as per FOM]

A

Serious / Imminent danger

  • Engine fire
  • Electrical fire & smoke
  • Emergency Descent
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16
Q

Which (3x) situations require a PANPAN?
[as per FOM]

A

Safety is a concern, but no immediate assistance required

  • Engine failure
  • Flaps UP landing
  • Onboard medical emergency
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17
Q

Pilot incapacitation - Order of authority

A

1) Check pilot (if on board)
2) Deadheading captain on type (if on board)
3) First officer

18
Q

Approach - ENGINE OUT

A

[prior to inbound track]
PF : Reduce speed to 170 kts

[2 dot below]
PF : ‘‘Flaps Approach’’
* PM : ‘‘Flaps Approach’’

[1 dot below]
PF : ‘‘Gear down. Pre-landing checks’’
* Reduce speed to 125 kts

PM : Selects Gear down + Props full fine
* Complete Pre-Landing checks

[2nm prior FAF]
PF : ‘’ Final checks. Flaps to go’’
* PM = ‘‘Final checklist completed, Flaps to go’’

[FAF]
PM : ‘’ Stabilized / Unstable, Goaround’’

[Approaching minimums]
PM : ‘’ 300 / 200 / 100 feet above’’

[minimums]
PM : ‘’ Minimums. Runway _ o’clock’’

PF : ‘‘Landing. FULL FLAPS’’
* Disconnects AP & YD.
* Reduces speed to Vref
* PM : Selects FULL FLAPS

Only difference vs. a normal approach is that FULL FLAPS are held until DA/MDA, instead of having full flaps at the FAF

19
Q

Partial / Flapless approach
- DRILL
- VREF (Fapp/Fup)

A

[prior to inbound track]
PF : Reduce speed to 170 kts

[2 dot below]
PF : ‘‘Flaps Approach’’
PM : ‘‘Flaps Approach’’

[1 dot below]
PF : ‘‘Gear down. Pre-landing checks’’
* Reduce speed to 125 kts

PM : Selects Gear down + Props full fine
* Complete Pre-Landing checks

[2nm prior FAF]
PF : ‘’ Final checks’’
* PM = ‘‘Final checklist completed, Yaw Damp to go’’

[FAF]
PM : ‘’ Stabilized / Unstable, Goaround’’

[Approaching minimums]
PM : ‘’ 300 / 200 / 100 feet above’’

[minimums]
PM : ‘’ Minimums. Runway _ o’clock’’

PF : ‘‘Landing’’
* Disconnects AP & YD
* Reduces speed to Vref

*** Vref increased by :
Flaps APPR : Vref +10
Flaps UP : Vref +20

20
Q

NO LIGHT UP START
(within 10 seconds)

A
  1. Condition Lever = CUTOFF
  2. Ignition / Engine Start = OFF
21
Q

HOT START or HUNG START

A

If ITT appears likely to exceed 1,000°C:

  1. Condition Lever = CUTOFF
  2. Ignition / Engine Start = STARTER ONLY

Once ITT below 400°C:

  1. Ignition / Engine Start = OFF
22
Q

ENGINE FIRE ON START

A

Affected engine :

  1. Condition Lever = CUTOFF
  2. Firewall Valve = CLOSE
    * annunc. illuminated : [EXTINGUISHER PUSH] & FW Valve [CLOSED]
  3. Starter Switch = STARTER ONLY

If fire warning persists :

  1. Fire Extinguisher = ACTIVATE
    * annunc. illuminated : [DISCHARGED] – ILLUMINATED
23
Q

EMERGENCY ENGINE SHUTDOWN
(On Ground)

A
  1. Condition Levers = CUTOFF
  2. Prop Levers = FEATHER
  3. Firewall Valves = CLOSE
    * annunc. illuminated : [EXTINGUISHER PUSH] & FW Valve [CLOSED]
  4. Gang Bar = DOWN
  5. Battery Bus Switch = EMER OFF
24
Q

ENGINE FAILURE IN FLIGHT BELOW VMCA

A
  1. Power = REDUCE ON OPERATING ENGINE TO MAINTAIN DIRECTIONAL CONTROL
  2. Nose = LOWER TO ACCELERATE ABOVE VMCA
25
Q

GLIDE
(BOTH ENGINES INOPERATIVE)

A
  1. Landing Gear & Flaps = UP
  2. Propeller(s) = *If no airstart is planned, *FEATHERED
    !! WARNING !!
    Do not feather engine propeller if a windmilling airstart is planned.
    Airstart with a windmilling propeller will result in lower starting temperatures
    .
  3. Airspeed = 135 KIAS
26
Q

[CAB ALT HI] & [CABIN ALTITUDE] annunciator
(PRESSURIZATION LOSS)

A
  1. Oxygen:
    a. Oxygen Masks/Headsets = DON
    b. Mic Switches = OXYGEN MASK
  2. Passenger Manual Drop-out = PULL ON

If required :

  1. Descend
27
Q

AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE

[CABIN ALT HI] without [PASS OXYGEN ON]

A
  1. Passenger Manual Drop-out = PULL ON
28
Q

[CABIN DIFF HI] annunciator

A
  1. Bleed Air Valve Switches = ENVIR OFF

If required (if results in a [CAB ALT HI] illum…) :

  1. Oxygen (Crew & Passengers)
  2. Descend

[Sugg.] At first, try ENVIRO = LOW (50% of air inflow)

29
Q

SMOKE AND FUME ELIMINATION

A
  1. Oxygen:
    a. Oxygen Masks/Headsets = DON
    b. Mic Switches = OXYGEN MASK
  2. Mask Selector Switch = EMERG
  3. Smoke Googles = ON
30
Q

[L/R BLEED FAIL] annunciator

A
  1. Bleed Air Valve Switch (affected eng.) = PNEU/ENVIR OFF
31
Q

DUAL GENERATOR FAILURE

A

If at NIGHT :
1. Instrument Emergency Lights = ON

THEN :
2. Generator Switches = RESET / ON

If EITHER resets :
3. Loadmeter = DO NOT EXCEED 100% ON OPERATING GENERATOR (95% FL340 & ABV)

If NONE resets :
3. Non-Essential Equipment = OFF

32
Q

SINGLE INVERTER FAILURE

A
  1. AC Bus C/B’s = CHECK

If C/B TRIPPED :
2. C/B = RESET

If C/B NOT tripped :
3. Failed Inverter = SELECT BUS TRANSFER

33
Q

DUAL INVERTER FAILURE

A
  1. Attitude/Heading Control = USE BACKUP INSTRUMENTS

If AC power necessary for completion of flight :
2. AC Bus C/B’s = RESET (If tripped)

PFD will still fonction (on VDC)
AP/YD inop.

34
Q

PITCH TRIM RUNAWAY

A
  1. Aircraft Attitude = MAINTAIN USING ELEVATOR CONTROL
  2. A/P / Trim Disconnect = DEPRESS FULLY
    * [PITCH TRIM OFF] – ILLUMINATED
35
Q

UNSCHEDULED RUDDER BOOST ACTIVATION

A
  1. A/P / Trim disconnect = DEPRESS & HOLD (FIRST LEVEL)
  2. Rudder boost = OFF

If condition persists :
3. Rudder Boost C/B = PULL

36
Q

SPINS

A

Simultaneously :
1. Control Column = FULL FORWARD
2. Ailerons = NEUTRAL
3. Rudder = APPLY FULL OPPOSITE SPIN DIRECTION
4. Power Levers = REDUCE TO IDLE ON BOTH ENGINES

Then :
4. Rudder = NEUTRALIZE–HOLD UNTIL ROTATION STOP
5. Execute smooth pullout.

37
Q

[DOOR UNLOCKED] annunciator

A
  1. All Occupants = SEATED / SEAT BELTS FASTENED
38
Q

EMERGENCY DESCENT

A

IF REQUIRED (ex.: rapid decompression) =
1. Oxygen masks = ON

Then :
2. Power Levers = IDLE
3. Prop Levers = FULL FORWARD
4. Flaps = UP
5. Landing Gear = UP
6. Airspeed = MMO / VMO

39
Q

Which (2x) emergencies require the PASS MANUAL DROP-OUT to be pulled?

A

[CAB ALT HI]
&
Auto-deployment malfunction
* [CAB ALT HI] without [PASS OXY ON]

40
Q

Which (2x) emergencies require the OXYGEN MASKS?

A

[CAB ALT HI]
&
Smoke & Fumes evacuation

41
Q

Which (2x) emergencies considers the OXYGEN MASKS, if required?

A

[CAB DIF HI]
&
Emergency descent

42
Q

Which (2x) emergencies considers to DESCEND, if required?

A

[CAB ALT HI]
&
[CAB DIF HI]