20160813014419A

Accident · Destroyed

FAA accident report · Cirrus Design SR20 · Des Moines, IA · August 13, 2016

Date
August 13, 2016 · 10:10 local
Place
Des Moines, IA
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N314BF
NTSB investigation
NTSBCEN16LA320
Reported as
Cirrus Design SR20
Reported engine
Continental IO-360-ES
People aboard
4
Fatal injuries
0
Other injuries
3
Pilot’s certificate
Private pilot
Pilot’s flight hours
252 total66 in this make and model66 in the last 90 days

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.

Shortly after take off from run way 31 at the dsm airport on a heading of 330 the pilot reported sudden engine power loss. Immediately after the radio call to the tower and at an altitude between 800-900 ft AGL the pilot deployed the parachute system. The aircraft descended through power lines and came to rest in the intersection of 56th and park ave nw of the Des Moines airport. All personnel on board the aircraft exited before it was consumed by fire. The aircraft was nearly intact firewall forward which allowed for an examination of the engine at the accident site. A disconnected intake tube coupler was discovered on the #1 cylinder along with a fractured intake tube flange on the #3 cylinder. Follow on inspections were performed by Cirrus and Continental. It was determined that the loss of engine power was the result of the disconnected coupler and fractured intake tube flange.

As the FAA filed it

SHORTLY AFTER TAKE OFF FROM RUN WAY 31 AT THE DSM AIRPORT ON A HEADING OF 330 THE PILOT REPORTED SUDDEN ENGINE POWER LOSS. IMMEDIATELY AFTER THE RADIO CALL TO THE TOWER AND AT AN ALTITUDE BETWEEN 800-900 FT AGL THE PILOT DEPLOYED THE PARACHUTE SYSTEM. THE AIRCRAFT DESCENDED THROUGH POWER LINES AND CAME TO REST IN THE INTERSECTION OF 56TH AND PARK AVE NW OF THE DES MOINES AIRPORT. ALL PERSONNEL ON BOARD THE AIRCRAFT EXITED BEFORE IT WAS CONSUMED BY FIRE. THE AIRCRAFT WAS NEARLY INTACT FIREWALL FORWARD WHICH ALLOWED FOR AN EXAMINATION OF THE ENGINE AT THE ACCIDENT SITE. A DISCONNECTED INTAKE TUBE COUPLER WAS DISCOVERED ON THE #1 CYLINDER ALONG WITH A FRACTURED INTAKE TUBE FLANGE ON THE #3 CYLINDER. FOLLOW ON INSPECTIONS WERE PERFORMED BY CIRRUS AND CONTINENTAL. IT WAS DETERMINED THAT THE LOSS OF ENGINE POWER WAS THE RESULT OF THE DISCONNECTED COUPLER AND FRACTURED INTAKE TUBE FLANGE.

NTSB investigation

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