20160719022989A

Accident · Substantial damage

FAA accident report · Cessna A185E · Iliamna, AK · July 19, 2016

Date
July 19, 2016 · 10:30 local
Place
Iliamna, AK
Airport
Iliamna
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N85CF
NTSB investigation
NTSBANC16LA046
Reported as
Cessna A185E
People aboard
4
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
14,000 total4,000 in this make and model35 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.

On landing at a remote gravel landing strip, the aircraft sustained substantial damage to the propeller, left wing, left horizontal stabilizer and left main gear strut/axle.

Airman stated after touchdown he felt a shudder in the rudder and when he tried to apply brakes he had no brake pressure. Then he saw the detached left main wheel/tire rolling forward of the aircraft.

Further inspection revealed 4 bolts had broken off at the left main wheel axle which caused the left main gear strut to break free at the left strut gear box attachment point.

As the FAA filed it

ON LANDING AT A REMOTE GRAVEL LANDING STRIP, THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE TO THE PROPELLER, LEFT WING, LEFT HORIZONTAL STABILIZER AND LEFT MAIN GEAR STRUT/AXLE.

AIRMAN STATED AFTER TOUCHDOWN HE FELT A SHUDDER IN THE RUDDER AND WHEN HE TRIED TO APPLY BRAKES HE HAD NO BRAKE PRESSURE. THEN HE SAW THE DETACHED LEFT MAIN WHEEL/TIRE ROLLING FORWARD OF THE AIRCRAFT.

FURTHER INSPECTION REVEALED 4 BOLTS HAD BROKEN OFF AT THE LEFT MAIN WHEEL AXLE WHICH CAUSED THE LEFT MAIN GEAR STRUT TO BREAK FREE AT THE LEFT STRUT GEAR BOX ATTACHMENT 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 N85CF · 2

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