Incident Overview

Date: Tuesday 31 December 2013
Aircraft Type: Cessna 525A CitationJet CJ2
Owner/operator: private
Registration Number: N380CR
Location: 10,5 km NW of Coventry, Warwickshire – ÿ United Kingdom
Phase of Flight: En route
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 2
Component Affected: Aircraft WingsAircraft Wings
Investigating Agency: AAIBAAIB
Category: Accident
A Cessna 525A CitationJet CJ2+ jet experienced a loss of control accident during a flight from Leeds/Bradford Airport. The pilot and passenger were uninjured. The aircraft rapidly decreased airspeed to approximately 128 knots, then reduced the climb rate to 500 ft/min. A series of five 360ø rolls to the right occurred near FL430, culminating in a stall and subsequent recovery. The aircraft’s wings sustained damage due to an overload caused by a +4.48g peak in acceleration, exceeding the limits of the ‘limit’ and ‘ultimate’ loads. The pilot?s autopilot mode compromised the stall warning system, leaving the aircraft vulnerable to a stall.A Cessna 525A CitationJet CJ2+ jet experienced a loss of control accident during a flight from Leeds/Bradford Airport. The pilot and passenger were uninjured. The aircraft rapidly decreased airspeed to approximately 128 knots, then reduced the climb rate to 500 ft/min. A series of five 360ø rolls to the right occurred near FL430, culminating in a stall and subsequent recovery. The aircraft’s wings sustained damage due to an overload caused by a +4.48g peak in acceleration, exceeding the limits of the ‘limit’ and ‘ultimate’ loads. The pilot?s autopilot mode compromised the stall warning system, leaving the aircraft vulnerable to a stall.

Description

A Cessna 525A CitationJet CJ2+ jet was damaged in a loss of control accident whilst on a flight from Leeds/Bradford Airport. The pilot and passenger were not injured. As the aircraft approached its cruising altitude of FL430, the indicated airspeed decreased to about 128 knots. The pilot then reduced the rate of climb to 500 ft/min. However, over the next 50 seconds, the speed gradually reduced by a further 10 kts. Close to FL430, the pilot checked his tablet to check the forecast. At that moment the aircraft pitched severely nose-down and rolled to the right, departing from controlled flight in a series of five 360ø rolls to the right. The pilot briefly regained control before the aircraft stalled again and in the following recovery. The aircraft’s wings were damaged in overload due to the +4.48g peak in acceleration, which was between the +3.6g (‘limit’ load) and +5.4g (‘ultimate’ load). The pilot returned to Leeds/Bradford at FL280 and made a successful landing. Conclusion: The pilot operated the aircraft in an autopilot mode which left it vulnerable to a stall and did not monitor the reducing airspeed as the aircraft reached its cruising altitude. The ‘sticking’ of the stall warning system removed the safety feature specifically designed to protect against this.

Primary Cause

Autopilot mode operation reduced pilot monitoring of airspeed, leading to a stall.Autopilot mode operation reduced pilot monitoring of airspeed, leading to a stall.

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