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Flashcards in QRH Memory Items Deck (17)
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1
Q

RAPID DEPRESSURISATION/ EMERGENCY DESCENT

A

RAPID DEPRESSURISATION/ EMERGENCY DESCENT
• Oxygen Masks …………………………………On
• Mic Switch …………………….Mask
• Passenger Signs……………………………..On
EMERGENCY DESCENT, accomplish as req’d:
PF:
-Select IAS for descent
-Power levers…………….Flight Idle
• Condition Levers……………………Max
• Airspeed ……………………………..VMO
Note: If structural integrity is in doubt, limit airspeed as much as possible and avoid high manoeuvring loads.
• “Emergency descent” PA

PM:
-Advise ATC
-Set Alt Pre-Select & Arm ALT SEL
“10,000 Set, ALT SEL”
-Set transponder as required

2
Q

ENGINE FAILURE/FIRE INFLIGHT SHUTDOWN

A

Affected Engine:
• Power Lever ………………Flight Idle
• Condition Lever ………………….Fuel Off
• Alternate Feather …………Feather
• Pull Fuel Off Handle …………………Pull
• Tank Aux Pump……………Off
IF Fire:
• Extg switch (affected engine) ……………….. Fwd Btl IF fire persists, wait up to 30 seconds:
• Extg Switch (affected engine)…………Aft Btl

3
Q

APU FIRE

A

Confirm apu auto shutdown: APU RUN lgt out and APU BTL discharges

If either remain illuminated:
1. Ext switch - extg
———————-
2. APU BLEED- off
3. APu Gen - off
4. APU PWR - off

4
Q

Windshear Recovery

A

PM:
“Windshear Set Max Power”
-Apply MTOP, Rotate to 9 Degrees

PM:
-Condition Levers to max
-Trims Power to MTOP

Do Not Change Configuration Until Flight Path Is Under Control

IF THE AIRCRAFT IS STILL DESCENDING

PF:
- “Firewall the Power Levers”
-Increase Pitch to Stop descent but not below V2 / VGA
-Maintain V2 / VGA

PM:
-Firewall Power Levers

Should the Stick Shaker activate in turbulence, immediately reduce the Pitch Attitude sufficiently to silence the Shaker. In the event this should occur close to the ground, maintain the pitch attitude, which silences the Shaker, until terrain contact is no longer a factor, then allow the aircraft to accelerate back to V2/ VGA.

CLIMB UNTIL CLEAR OF OBSTACLES OR TERRAIN Reduce Power and Pitch Attitude appropriate to the phase of flight

Reconfigure aircraft as necessary

5
Q

EGPWS TERRAIN,
OBSTACLE CAUTION / WARNING
MSAW WARNING

A

PF:
-Selects GA (disengage the auto-pilot)
-Power Levers towards MTOP
- “Going Around Set max Power”
-Roll Wings Level
-Climb aggressively respecting the Stick Shaker
-Target VGA speed
-Call for Go Around Drills

PM:
-Condition Levers to max
-MTOP set
-Carries out Standard Go Around Drills

ONCE WARNING HAS CEASED AND CLEAR OF OBSTACLES OR TERRAIN:

-Establish level flight

Check airspeed and adjust power

6
Q

Pitch Jam

A

PF:
-“Pitch Jam Assist”
-Disengage Auto-pilot (if required)
-Flap and Airspeed maintain at time of Jam.
(Or 150kts whichever greater)

Both pilots attempt to dislodge jam.

IF UNABLE TO CONTROL AIRCRAFT

Both Pilots: -Relax Force

PF: “Pitch Disconnect”
PM: -Pulls Pitch Disconnect handle and rotates 90 degrees

-Both Pilots will now attempt to control aircraft.
-Pilot with free control will call “I have control”
-Pilot with Jammed control will respond “You have control”

7
Q

Roll Jam

A

PF: -“Roll Jam”
- Disengage Auto-pilot (if required)

PM:
-“Roll Disconnect”
-Pull Roll Disconnect handle and rotates 90 degrees

Both Pilots will now attempt to control aircraft.

Pilot with free control will call “I have control”.

Pilot with Jammed control will respond “You have control”.

8
Q

Single Engine Missed Approach

A

PF:
- “Going Around”
-GA button
-Advance towards MTOP
-Pitch up to 9º
- “Go Around Drill”

PM:
-Condition Lever to Max
-Power Levers to MTOP
- “Max Power Set”
-Retract Flap to 15°. If less than 15°, leave at current position
“Flap ___ (0°/5°/10°/15°)”
Observe Positive Climb on Altimeter
-Select Gear UP, call “Positive Climb, Gear Up”
-Select Lateral Mode (see notes).
-Select ALTSEL, confirm correct altitude selected
- “HDG/NAV & ALTSEL selected”

Above Acceleration Alt:

PM: - “Acceleration Altitude”
PF: - “Select ALT”
PM: -Select ALT
-Call “ALT Selected, VFRI is…”
PF: -Verify airspeed greater than VFRI
- “Flap Zero”
PM: -Select Flap 0º
-Call “Flap 0º Selected, VCLIMB is___”
PF: Call “Select IAS, Set VCLIMB”
PM: -Select IAS, set VCLIMB
-Select ALT SEL
-Call “VCLIMB Set, ALT SEL”

Prior to reaching the Engine MTOP Limit:
PF: -“Max Continuous Power”
PM: -Set MCP
-Call “Power Set”

9
Q

Prop Overspeed

A

Above 400ft AGL
PM: “PROP OVERSPEED #1 (or #2)”

F/O: -Select Synchrophase OFF

PF: -“#1 (or #2) Confirmed”
-“Memory Items, Propeller Overspeed”
-Reduce airspeed to minimum appropriate for flap configuration and flight conditions
PM: -“Power Lever #1 (or #2)” PF: -“Confirmed”
-Affected Power Lever to FLT IDLE

PM: -“Condition Lever #1 (or #2)”. PF: “Confirmed, Start Feather”
-Select Condition Lever to Start/Feather
-“Start/Feather”

PM: -“Alternate Feather #1 or #2” PF: -“Confirmed”
-Select Alt FX Switch to “Feather”
-State: “Propeller Feathered or Negative Feather”

IF PROPELLER DOES NOT FEATHER, DO NOT SHUT DOWN ENGINE

PM: -“Alternate Feather, Norm” check alternate advisory light goes out
-“Condition Levers Max”

PF: -Power Lever (affected engine) Advance.
Do not exceed 1212 RPM.
-Power Lever (Non affected engine) as req’d to maintain desired flight profile.

Land immediately at nearest suitable airport.

IF PROPELLER FEATHERS

PF: -“Memory Items Shutdown Engine #1 (OR #2)”
PM: -Complete appropriate memory Items

10
Q

Engine Malfunction/Fire
At or after V1

A

PM: -“V1”
- “Rotate”

PF:
-Rotate to 9º nose up.
-Check wings level, ball centred, correct heading.
-Trim as required.

PM: -observe positive climb on Altimeter
-“Positive Climb”
PF: -Confirm Positive Climb, Call “Gear Up”

PM: -Select Gear Up
-“Gear Up Selected”

PF: -Establish Climb V2 (V2 + 10 max)

PM: -Monitor Flight Path by reference to flight instruments.
-Call “Engine Malfunction” OR “Engine Fire”
-Cancel all caution and warning lights

above accel Alt
PM: -“Acceleration Alt”

When ready to LAcc

PF: - “Select ALT”
PM: -Select ALT
-Call “ALT Selected, VFRI is…”
PF: -Verify airspeed > VFRI
- “Flap Zero”
PM: -Select Flap 0º
-“Flap 0º Selected”
PF: -“Select IAS, Set VCLIMB”
PM: -Select IAS, set VCLIMB
-Select ALT SEL
-“VCLIMB Set, ALT SEL”

ASSESS THE PROBLEM

PM: -Identify the malfunction
PF: -Confirm malfunction, Call for Memory Item.
“Memory Items, Shutdown Engine #1 or #2” or
“Propeller Overspeed #1 or #2”
PM: Complete Memory Item

Single engine climb shall be at VCLIMB after flap retraction (or VCLIMB +15kt in icing conditions). MTOP may be used for up to five minutes, after which MCP will be set.

11
Q

RTO

A

Either pilot state, “Stop Stop”,
Aborted Takeoff Procedure is initiated

PF: Simultaneously
-Power Levers……..Disc
-Braking…………Max

PIC: -“I Have Control”
F/O: -“You Have Control”
-Advises ATC of the ABORT
-Cancels all flashing Master Caution and/or Master Warning Lights

Once the aircraft has stopped the crew will assess the problem

12
Q

Impact Drill

A

PIC: -I Have Control”
F/O -“You Have Control”

WHEN IMPACT IMMINENT

PIC: -“Impact Drill”
F/O: -Cycle the Seatbelt Sign
-Emergency Lights on

As the aircraft departs the runway or engine power is no longer effective

F/O: -Condition Levers……Fuel Off

13
Q

“SMOKE” AND/OR FUSELAGE FIRE OR SMOKE / FUMES

A
  1. Oxygen Masks ……. On / 100% (Emerg As Req’d)
  2. Smoke Goggles (If applicable)……………………. On
  3. Mic Switch ……………………………………………. Mask
  4. Recirc Fans …………………………………………….. Off
14
Q

ABORTED ENGINE START

A

IMMINENT OVER TEMPERATURE, HUNG START or FAILURE TO LIGHT UP (WITHIN 10 SECONDS):

  1. Condition Lever …………………………………. Fuel Off
  2. IF ITT does not decrease immediately

Pull Fuel Off Handle …………………………………. Pull

  1. Ignition (affected engine) ……………………………. Off
  2. Motor engine for a minimum of 15 seconds
  3. Start Select………………………………………………. Off
15
Q

PROPELLER OVERSPEED
(Abbreviated memory drills)

A

Above 400ft AGL:

  1. Synchrophase …………………………………………. Off
  2. Airspeed …………… reduce toward minimum speed appropriate to flap configuration and flight conditions

Affected Engine:

  1. Power Lever ………………………………….. Flight Idle
  2. Condition Lever ………………………. Start / Feather
  3. Alternate Feather ………………………………. Feather

IF Propeller Does NOT Feather:

DO NOT SHUT DOWN ENGINE.

  1. Alternate Feather Switch (affected engine) .. Norm
    (check Alternate advisory light out).
  2. Condition Levers ……………………………………. Max
  3. Power Lever (affected engine) …. Advance. Do not exceed 1212rpm
  4. Power Lever (non affected engine) . As required to maintain desired flight profile.
  5. Land immediately at nearest suitable airport.

IF Propeller Feathers:

  1. ENGINE FAIL / FIRE / SHUTDOWN ………………………………… Accomplish
16
Q

PROPELLER GROUND RANGE ADVISORY LIGHT CYCLING

A
  1. Power Levers ………….. Advance above Flight Idle
17
Q

ROLL CONTROL MALFUNCTION

A

(Aeroplane Rolls With No Control-Wheel Input)

  1. Roll Control ……………….. Apply to hold wings level

If continuous illumination of SPLR 1 or SPLR 2 PUSH OFF switch-lights in wings level flight:

  1. Illuminated switch-light …………………… PUSH OFF

If SPLR 1 or SPLR 2 PUSH OFF switch-lights do not illuminate in wings level flight:

  1. Power …………………………………………………. Apply
  2. Airspeed………………………………………….. Increase