19960718034149I

Incident · Minor damage

FAA incident report · Piper PA-18-150 · Fairbanks, AK · July 18, 1996

Date
July 18, 1996 · 23:00 local
Place
Fairbanks, AK
Airport
Fairbanks International
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N7384D
Reported as
Piper PA18150
People aboard
2
Fatal injuries
0
Pilot’s flight hours
520 total160 in this make and model13 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.

Narrative: on approach to float pond one the pilot heard a loud bang, followed by a yaw and rapid rate of descent. The pilot was able to arrest the rate of descent and landed with a reduction of power. The right wing started to fall. The pilot had to maintain full power to keep the right wing out of the water. He was able to maintain a balance of speed and power to the shore. The aircraft did not sustain any damage as a result of beaching. A post flight inspection found the left rear fuselage fitting and the right front float fitting had failed.

As the FAA filed it

NARRATIVE: ON APPROACH TO FLOAT POND ONE THE PILOT HEARD A LOUD BANG, FOLLOWED BY A YAW AND RAPID RATE OF DESCENT. THE PILOT WAS ABLE TO ARREST THE RATE OF DESCENT AND LANDED WITH A REDUCTION OF POWER. THE RIGHT WING STARTED TO FALL. THE PILOT HAD TO MAINTAIN FULL POWER TO KEEP THE RIGHT WING OUT OF THE WATER. HE WAS ABLE TO MAINTAIN A BALANCE OF SPEED AND POWER TO THE SHORE. THE AIRCRAFT DID NOT SUSTAIN ANY DAMAGE AS A RESULT OF BEACHING. A POST FLIGHT INSPECTION FOUND THE LEFT REAR FUSELAGE FITTING AND THE RIGHT FRONT FLOAT FITTING HAD FAILED.

Other reports on N7384D · 2

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