20140815016999I

Incident · Minor damage

FAA incident report · Stinson L-5 · Hondo, TX · August 15, 2014

Date
August 15, 2014 · 14:30 local
Place
Hondo, TX
Airport
Hondo
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N178
Reported as
Stinson L-5
Reported engine
Lycoming 0-435
People aboard
2
Fatal injuries
0
Other injuries
0

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.

Upon the first landing of an instructional flight for a commemorative air force aircraft check-out, the aircraft veered left and ground looped. The outboard two feet of right wing sustained damage, as well as tail wheel assembly, and right main tire and wheel assembly. No injuries. The right tail wheel control cable was detached from tail wheel assembly; the attachment clip had been torn loose. During landing roll-out, as aircraft speed slowed, the rudder became ineffective and the tail wheel did not respond to rudder pedal input. FAA inspector found that the tail wheel control cable attachment clips and cables were suspected unapproved parts.

As the FAA filed it

UPON THE FIRST LANDING OF AN INSTRUCTIONAL FLIGHT FOR A COMMEMORATIVE AIR FORCE AIRCRAFT CHECK-OUT, THE AIRCRAFT VEERED LEFT AND GROUND LOOPED. THE OUTBOARD TWO FEET OF RIGHT WING SUSTAINED DAMAGE, AS WELL AS TAIL WHEEL ASSEMBLY, AND RIGHT MAIN TIRE AND WHEEL ASSEMBLY. NO INJURIES. THE RIGHT TAIL WHEEL CONTROL CABLE WAS DETACHED FROM TAIL WHEEL ASSEMBLY; THE ATTACHMENT CLIP HAD BEEN TORN LOOSE. DURING LANDING ROLL-OUT, AS AIRCRAFT SPEED SLOWED, THE RUDDER BECAME INEFFECTIVE AND THE TAIL WHEEL DID NOT RESPOND TO RUDDER PEDAL INPUT. FAA INSPECTOR FOUND THAT THE TAIL WHEEL CONTROL CABLE ATTACHMENT CLIPS AND CABLES WERE SUSPECTED UNAPPROVED PARTS.

Other reports on N178 · 1

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