Engine Fire or Engine Severe damage or Seperation at V1

Question 1

When can “FAILURE” be called?

Answer 1

After Gear is retracted

Question 2

When should the PF instruct the PM to “Indentify the failure?”

Answer 2

At approximately 400 feet AGL

Question 3

What is the rotation rate with OEI and to what pitch attitude?

Answer 3

1.5-2º per sec (Half of the normal rate)
12-13º Nose UP

Aiming for 2º per second to 13º should aid in rotating at a slower rotation rate.

This should take approximately 7 seconds unlike normal rotation rate which is 5 seconds

Question 4

If an engine fails at V1, what will the F/D command?

Answer 4

V2 or airspeed at lift-off, whichever is greater.

Note: It is possible to be below V2 at v1. It is critical, that rotation is performed correct. A sustained flight below v2 will result in a failed RTP attempt.

Question 5

Which direction should the rudder be trimmed with OEI?

Answer 5

Towards the live engine.

SLIP/SPIN indication gives a clue as to which engine is dead: “STEP ON THE SAIL BOAT”.

Dead leag = Dead Engine

Question 6

Explain the steps to follow after an engine failure AT V1

Answer 6

Parrallel RUNWAY centreline and HOLD pressure on rudder

2. Rotate at 2º per second up to 13º Nose up (V2+20 kts)…. Atleast 6 seconds.
3. Follow Flight Directors

Keep Wings S+L with rudder.

4. Wait for the “Positive Rate” call from PM.
5. Call “Gear Up”
6. Call “FAILURE”
7. At 400ft AGL, check and confirm (or call for) “HDG SEL” & “Indetify the failure”
8. ENAGAGE A/P
9. Fly SPECIAL PROCEDURE
10. Execute Memory items:

PF: place hand on the EFFECTED thrust lever and call ‘NUMBER ONE/TWO THRUST LEVER”

wait for PM call: “CONFIRMED”
PF: close the thrust lever.

PM: Places their hand on the respective start lever
and awaits the call

PF: calls “NUMBER ONE or TWO
START LEVER” …. confirm correct and call “CONFIRMED CUTOFF”

PF: calls “NUMBER ONE or TWO
FIRE SWITCH” …. confirm correct and call “CONFRIMED PULL”

11. @ Acceleration altitude, call “ bug up”
12. Clean up flaps

Check all actions are correct and still flying correct SPECIAL PROCEDURE.

13. Select or request : LVL CHNG & Max continuous thurst.
14. Call “after take off checklist”
15. Call “NON NORMAL CHECKLIST”

1. If an engine failure occurs on the ground, the pitch command target speed V2 or greater, up to V2+20 kts.
2. If the Memory Items are commenced prior to acceleration height, acceleration should be delayed until the Memory Items are completed.

Question 7

When going through the NNC how should the PF respond to the PM’s calls for executing items?

Answer 7

PM _____________________________ PF
Autothrottle: “Disengage” …………. “Disengaged”

Thrust lever: “Close” …………………. “Number one/two closed”

Start lever: “CUTOFF” …………………. “Number one/two CUTOFF”

Engine fire switch: “Pull” ………………“Number one/two pulled”

Question 8

What are the 7 critical items to better handle an engine failure during take off?

Answer 8

1. Apply rudder to “parallel centreline”
2. Rotate @ approximately 2º p/s to 12º Nose up.
3. Wings level
4. Check IAS
5. Centre Slip/skid indicator
6. Trim if necessary
7. Engage A/P

Question 9

If an engine fails after LIFT OFF, what will the F/D command?

Answer 9

• If IAS< V2 : PITCH DOWN to increase speed to V2
• If IAS>V2 : Maintain IAS
• If IAS > (V2 + 20): Pitch UP to reduce speed to V2+20

Slow rotation will result in scenario TWO. Fast rotation will result in scenario ONE. Normal Rotation rate with OEI is 2º p/sec up to 13º Nose up (7 seconds)