20130113001929I

Incident · No damage

FAA incident report · Cessna 560XL · Peachtree City, GA · January 13, 2013

Date
January 13, 2013 · 18:18 local
Place
Peachtree City, GA
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Operator
DXTA
Damage
No damage
Aircraft
N662QS
NTSB investigation
NTSBERA13IA114
Reported as
Cessna 560XL
Reported engine
Pratt & Whitney Canada PW545 series
People aboard
2
Fatal injuries
0
Other injuries
0

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Climbing out of FL350 in known icing (-23C, 1000 feet per minute, autopilot engaged, wing/engine anti-ice on), the aircraft suddenly pitched nose down. Upon detecting the pitch change the autopilot was disengaged. The controls were difficult to move along the vertical axis and each control input required excessive force to pitch the aircraft in a climb or descent. The aircraft seemed unstable and the nose would continue to pitch down or up excessively with gentle control inputs. After descending to below the freezing level (FL18), there was a sudden loosening of the rigidity in the controls and normal inputs and

Force could be used to adjust the pitch of the aircraft. Landing was uneventful.

As the FAA filed it

CLIMBING OUT OF FL350 IN KNOWN ICING (-23C, 1000 FEET PER MINUTE, AUTOPILOT ENGAGED, WING/ENGINE ANTI-ICE ON), THE AIRCRAFT SUDDENLY PITCHED NOSE DOWN. UPON DETECTING THE PITCH CHANGE THE AUTOPILOT WAS DISENGAGED. THE CONTROLS WERE DIFFICULT TO MOVE ALONG THE VERTICAL AXIS AND EACH CONTROL INPUT REQUIRED EXCESSIVE FORCE TO PITCH THE AIRCRAFT IN A CLIMB OR DESCENT. THE AIRCRAFT SEEMED UNSTABLE AND THE NOSE WOULD CONTINUE TO PITCH DOWN OR UP EXCESSIVELY WITH GENTLE CONTROL INPUTS. AFTER DESCENDING TO BELOW THE FREEZING LEVEL (FL18), THERE WAS A SUDDEN LOOSENING OF THE RIGIDITY IN THE CONTROLS AND NORMAL INPUTS AND

FORCE COULD BE USED TO ADJUST THE PITCH OF THE AIRCRAFT. LANDING WAS UNEVENTFUL.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.