20211022021849A

Accident · Substantial damage

FAA accident report · Cessna 208B · Juneau, AK · October 22, 2021

Date
October 22, 2021 · 08:50 local
Place
Juneau, AK
Airport
Juneau International
Phase of flight
Takeoff: Rotation
Operating rules
Air taxi and commuter (Part 135)
Operator
P9KA
Damage
Substantial damage
Aircraft
N754KP
NTSB investigation
NTSBANC22LA003
Reported as
Cessna 208B
Reported engine
Pratt & Whitney Canada PT6A-114A
People aboard
6
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
2,480 total

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.

On October 22, 2021, the pilot of a Cessna 208 lost control of the aircraft during rotation. The pilot stated that as the aircaft reached rotation speed, it abrupty began to pull to the right. The pilot was unable to regain directional control and stated that the left rudder felt limited. Due to the speed of the aircraft and because it was partially airborne with a high liklihood of reaching the float pond if a full abort was initiated, the pilot attempted to steer the aircraft back towards the runway. This manuevar resulted in a violent ground loop causing substantial damage. There were no injuries. The cause of the control issue was unable to be determined.

A passenger seated in the co-pilot's seat stated that he did not come in contact with the rudder pedals at any point.

As the FAA filed it

ON OCTOBER 22, 2021, THE PILOT OF A CESSNA 208 LOST CONTROL OF THE AIRCRAFT DURING ROTATION. THE PILOT STATED THAT AS THE AIRCAFT REACHED ROTATION SPEED, IT ABRUPTY BEGAN TO PULL TO THE RIGHT. THE PILOT WAS UNABLE TO REGAIN DIRECTIONAL CONTROL AND STATED THAT THE LEFT RUDDER FELT LIMITED. DUE TO THE SPEED OF THE AIRCRAFT AND BECAUSE IT WAS PARTIALLY AIRBORNE WITH A HIGH LIKLIHOOD OF REACHING THE FLOAT POND IF A FULL ABORT WAS INITIATED, THE PILOT ATTEMPTED TO STEER THE AIRCRAFT BACK TOWARDS THE RUNWAY. THIS MANUEVAR RESULTED IN A VIOLENT GROUND LOOP CAUSING SUBSTANTIAL DAMAGE. THERE WERE NO INJURIES. THE CAUSE OF THE CONTROL ISSUE WAS UNABLE TO BE DETERMINED.

A PASSENGER SEATED IN THE CO-PILOT'S SEAT STATED THAT HE DID NOT COME IN CONTACT WITH THE RUDDER PEDALS AT ANY POINT.

NTSB investigation

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

Other reports on N754KP · 1

Matched to the same aircraft by N-number and date.