20200608008959A

Accident · Substantial damage

FAA accident report · Piper PA-12 · Anchorage, AK · June 8, 2020

Date
June 8, 2020 · 10:30 local
Place
Anchorage, AK
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N3188M
NTSB investigation
NTSBANC20LA059
Reported as
Piper PA-12
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
5,900 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.

The aircraft departed lake hood waterway for the purposes of an instructional flight. All preflight checks were completed before takeoff and the flight commenced. Shortly after takeoff, the student pilot flying noticed an significant change in control feel specifically with respect to rudder control just after leveling of from a left turn from the airport. The instructor pilot assumed control of the aircraft and verified the change in rudder and aircraft control. The instructor pilot advised the tower for a return to landing request. The aircraft landed without further incident.

During post flight, it was discovered that the top of the rudder and broken in half still attached to the plane almost at a 90 degree angle. Initial inspector suggests possible metal fatigue.

As the FAA filed it

THE AIRCRAFT DEPARTED LAKE HOOD WATERWAY FOR THE PURPOSES OF AN INSTRUCTIONAL FLIGHT. ALL PREFLIGHT CHECKS WERE COMPLETED BEFORE TAKEOFF AND THE FLIGHT COMMENCED. SHORTLY AFTER TAKEOFF, THE STUDENT PILOT FLYING NOTICED AN SIGNIFICANT CHANGE IN CONTROL FEEL SPECIFICALLY WITH RESPECT TO RUDDER CONTROL JUST AFTER LEVELING OF FROM A LEFT TURN FROM THE AIRPORT. THE INSTRUCTOR PILOT ASSUMED CONTROL OF THE AIRCRAFT AND VERIFIED THE CHANGE IN RUDDER AND AIRCRAFT CONTROL. THE INSTRUCTOR PILOT ADVISED THE TOWER FOR A RETURN TO LANDING REQUEST. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.

DURING POST FLIGHT, IT WAS DISCOVERED THAT THE TOP OF THE RUDDER AND BROKEN IN HALF STILL ATTACHED TO THE PLANE ALMOST AT A 90 DEGREE ANGLE. INITIAL INSPECTOR SUGGESTS POSSIBLE METAL FATIGUE.

NTSB investigation

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