F50, vicinity Luxembourg, 2002

F50, vicinity Luxembourg, 2002

Summary

On 6 November 2002, a Fokker 50 operated by Luxair, crashed on approach to Luxembourg Airport following loss of control attributed to intentional operation of power levers in the ground range, contrary to SOPs.

Event Details
When
06/11/2002
Event Type
AW, FIRE, HF, LOC
Day/Night
Day
Flight Conditions
On Ground - Low Visibility
Flight Details
Aircraft
Operator
Type of Flight
Public Transport (Passenger)
Flight Origin
Intended Destination
Take-off Commenced
Yes
Flight Airborne
Yes
Flight Completed
No
Phase of Flight
Descent
Location
Location - Airport
Airport
General
Tag(s)
Approach not stabilised
FIRE
Tag(s)
Post Crash Fire
HF
Tag(s)
Flight / Cabin Crew Co-operation, Inappropriate crew response (automatics), Ineffective Monitoring, Manual Handling, Procedural non compliance, Violation
LOC
Tag(s)
Loss of Engine Power, Flight Management Error, Incorrect Thrust Computed, Aircraft Flight Path Control Error
EPR
Tag(s)
RFFS Procedures
AW
System(s)
Engine Fuel and Control
Contributor(s)
OEM Design fault
Outcome
Damage or injury
Yes
Aircraft damage
Hull loss
Non-aircraft damage
No
Non-occupant Casualties
No
Occupant Fatalities
Most or all occupants
Off Airport Landing
No
Ditching
No
Causal Factor Group(s)
Group(s)
Aircraft Operation
Aircraft Technical
Safety Recommendation(s)
Group(s)
Aircraft Operation
Aircraft Airworthiness
Investigation Type
Type
Independent

Description

On 6 November 2002, a Fokker 50 operated by Luxair, crashed on approach to Luxembourg Airport following loss of control attributed to intentional operation of power levers in the ground range, contrary to SOPs.

Synopsis

The following are extracts from the Accident report published by the Luxembourg Ministry of Transport:

Conclusions

…7. RVR was below approved company minima during the initial and the intermediate approach,

8. During the approach, the crew did not comply with the operator’s procedures,

9. Despite the fact that the meteorological conditions for a CAT II approach prevailed, none of the required prerequisites, to perform a CAT II approach, were taken by the crew.

10. The captain resumed the final approach after having announced a go-around, without co-pilot’s reaction,

11. In order to achieve this goal, the crew performed several non-standard actions, amongst which the prohibited positioning of the power levers beyond flight idle. The AFM contained a limitation that prohibits the selection of ground idle in flight.

12. The selection of the landing gear down, triggered the deactivation of the second safety device (solenoid secondary stops) which was a possible malfunction identified by the manufacturer.

Causes

The initial cause of the accident was the acceptance by the crew of the approach clearance although they were not prepared to it, namely the absence of preparation of a go-around. It led the crew to perform a series of improvised actions that ended in the prohibited override of the primary stop on the power levers.

Contributory factors can be listed as follows

1. A lack of preparation for the landing, initiated by unnecessary occupations resulting from an obtained RVR value, which was below their company approved minima, created a disorganisation in the cockpit, leading to uncoordinated actions by each crewmember.

2. All applicable procedures as laid down in the operations manual were violated at some stage of the approach. All this did not directly cause the accident, but created an environment whereby privately designed actions were initiated to make a landing possible.

3. Routine and the will to arrive at its destination may have put the crew in a psychological state of mind, which could be the origin of the deviations from standard procedures as noticed.

4. The low reliability of the installed secondary stop safety device that was favoured by the non-application of service bulletin ABSC SB F050-32-4. Also the mode of distribution of the safety information (Fokker Aircraft B.V. - Service letter137) to the operator as well as the operator’s internal distribution to the crews, that did not guarantee that the crews were aware of the potential loss of secondary stop on propeller pitch control.

5. The lack of harmony resulting from the use of various training centres and non-standardised programs that might have impaired the synergy of the crew."

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