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Airwork Flight 23

Airwork Flight 23
Summary
Date   May 3 2005
Type   Pilot error
Site   Stratford, New Zealand
Fatalities   2
Injuries   0
Aircraft
Aircraft type   Swearingen SA.227AC Metro III
Operator   Airwork
Tail number   ZK-POA
Passengers   0
Crew   2
Survivors   0

Airwork Flight 23 was a New Zealand Post cargo flight between Auckland International Airport (AKL/NZAA) and Woodbourne Airport (BHE/NZWB) that disintegrated on May 3, 2005.


Contents

History of the flight

The aircraft was scheduled for take off at 9:00 P.M. local time, but it was delayed while cargo was being loaded. During the delay the pilots ordered an extra 570 L (about 150.5 gallons) of fuel and told the person refueling to put all the fuel in the left wing fuel tank, instead of splitting the fuel exactly between the two tanks, as was company procedure. The flight eventually took off at 9:36 P.M. local time.

Immediately after take off the autopilot was engaged and it controlled the aircraft during its climb to flight level 220. The flight was continued at full power instead of cruise setting to make up for lost time for the next fifteen minutes. On powering down to cruise power, the captain noticed fuel imbalance on the plane and initiated cross flow procedures. Shortly after, at 10:13 P.M. local time, the plane entered a spiral descent and broke up, killing both pilots.

Investigation

The accident was investigated by the New Zealand Transport Accident Investigation Commission. It found that when the captain noted the fuel imbalance, he said, "We'll just open the cross flow again… sit on left ball and trim it accordingly." He repeated the instruction five times in the next 19 seconds, to which the co-pilot replied, "I was being a bit cautious". The captain said, "Don't be cautious mate, it'll do it good".

This resulted in the plane being flown at a large sideslip angle while still under autopilot control, by means of the rudder trim mechanism. Forty-seven seconds after the cross flow was opened, the captain said, "Doesn't like that one mate… you'd better grab it." One second later they received a "bank angle" warning, followed by a warning chime that was presumably a warning they were straying from their correct altitude.

The investigation came to the conclusion that this was due to the autopilot disengaging, probably due to a servo reaching its torque limit. This meant that there was no compensation applied for the rudder trim impute, and the plane entered a roll and steep descent, disintegrating around flight level 199. The investigation found poor visibility at night in low cloud was a factor in preventing the pilots realizing sooner.

Aftermath

The following improvements were implemented as a result:

Categories


Airliner crashes caused by pilot error | In-flight airliner structural failures | 2005 disasters

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