B763, Manchester UK, 2008

B763, Manchester UK, 2008

Summary

On 13 December 2008, a Thomsonfly Boeing 767-300 departing from Manchester for Montego Bay Jamaica was considered to be accelerating at an abnormally slow rate during the take off roll on Runway 23L. The aircraft commander, who was the pilot not flying, consequently delayed the V1 call by about 10 - 15 because he thought the aircraft might be heavier than had been calculated. During the rotation the TAILSKID message illuminated momentarily, indicating that the aircraft had suffered a tail strike during the takeoff. The commander applied full power and shortly afterwards the stick shaker activated briefly. The aircraft continued to climb away and accelerate before the flaps were retracted and the after-takeoff check list completed. The appropriate drills in the Quick Reference Handbook (QRH) were subsequently actioned, fuel was dumped and the aircraft returned to Manchester for an overweight landing without further incident.

Event Details
When
13/12/2008
Event Type
HF, RE
Day/Night
Day
Flight Conditions
On Ground - Normal Visibility
Flight Details
Operator
Type of Flight
Public Transport (Passenger)
Take-off Commenced
Yes
Flight Airborne
Yes
Flight Completed
Yes
Phase of Flight
Take Off
Location
Location - Airport
Airport
General
Tag(s)
Inadequate Aircraft Operator Procedures
HF
Tag(s)
Data use error, Distraction, Pre Flight Data Input Error, Procedural non compliance
RE
Tag(s)
Overrun on Take Off, Unable to rotate at VR, Intentional Premature Rotation
Outcome
Damage or injury
Yes
Aircraft damage
Minor
Non-aircraft damage
Yes
Non-occupant Casualties
No
Off Airport Landing
Yes
Ditching
Yes
Causal Factor Group(s)
Group(s)
Aircraft Operation
Safety Recommendation(s)
Group(s)
None Made
Investigation Type
Type
Independent

Description

On 13 December 2008, a Thomsonfly Boeing 767-300 departing from Manchester for Montego Bay Jamaica was considered to be accelerating at an abnormally slow rate during the take off roll on Runway 23L. The aircraft commander, who was the pilot not flying, consequently delayed the V1 call by about 10 - 15 kts because he thought the aircraft might be heavier than had been calculated. During the rotation the TAILSKID message illuminated momentarily, indicating that the aircraft had suffered a tail strike during the takeoff. The commander applied full power and shortly afterwards the stick shaker activated briefly. The aircraft continued to climb away and accelerate before the flaps were retracted and the after-takeoff check list completed. The appropriate drills in the Quick Reference Handbook (QRH) were subsequently actioned, fuel was dumped and the aircraft returned to Manchester for an overweight landing without further incident.

Investigation

An Investigation into the occurrence was carried out by the UK AAIB. It was found that the Zero Fuel Weight (ZFW) had been incorrectly entered into the Aircraft Operator’s CTOP or ‘Computer Take Off Programme’ (which is used by the crew to calculate the correct take off speeds) instead of the takeoff weight (TOW). This error generated significantly slower takeoff speeds than were required for the actual weight of the aircraft and the crew did not recognise this upon seeing and using them prior to beginning the take off. It was found that the data entry error had the effect of reducing the V1, Vr and V2 to about 20 knots below their true values.

As a result of this occurrence, the Operator introduced into their Operations Manual a more explicit procedure for cross checking of data entry prior to departure:

Both pilots should independently extract the ATOM[1] from the load sheet and perform the C-TOP calculation. PF should call out any further assumptions made e.g. surface wind, runway conditions, use of anti-ice etc."

The Investigation noted that the commander reported having flown about six empty sectors in a Boeing 767 prior to this flight such that the slow takeoff speeds set did not trigger an alert to him.

The UK AAIB Report was issued on 9 July 2009 and made no Safety Recommendations.

Further Reading

Notes

  1. ^ Actual Takeoff Mass

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