19960311006089I

Incident · Minor damage

FAA incident report · Maule M-8-235 · Amarillo, TX · March 11, 1996

Date
March 11, 1996 · 16:15 local
Place
Amarillo, TX
Airport
Amarillo International Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N3003A
Reported as
Maule M8235
People aboard
3
Fatal injuries
0
Pilot’s flight hours
12,500 total400 in this make and model110 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: following a normal approach and touchdown under VMC conditions, this ATP pilot and two passengers experienced a severe tail wheel shimmy on rollout. This shimmy caused the tail wheel steering cable to detach itself from the tail wheel steering horn causing a loss of directional control. The aircraft weather vained into the crosswind, and corrective brake and rudder applied. During the correction, the right main gear axle broke causing the right main wheel assy to depart the acft. The acft. Slid and skidded to a stop on the runway without any injuries to the occupants and only minor damage to the acft. (This investigation is closed.)

As the FAA filed it

NARRATIVE: FOLLOWING A NORMAL APPROACH AND TOUCHDOWN UNDER VMC CONDITIONS, THIS ATP PILOT AND TWO PASSENGERS EXPERIENCED A SEVERE TAIL WHEEL SHIMMY ON ROLLOUT. THIS SHIMMY CAUSED THE TAIL WHEEL STEERING CABLE TO DETACH ITSELF FROM THE TAIL WHEEL STEERING HORN CAUSING A LOSS OF DIRECTIONAL CONTROL. THE AIRCRAFT WEATHER VAINED INTO THE CROSSWIND, AND CORRECTIVE BRAKE AND RUDDER APPLIED. DURING THE CORRECTION, THE RIGHT MAIN GEAR AXLE BROKE CAUSING THE RIGHT MAIN WHEEL ASSY TO DEPART THE ACFT. THE ACFT. SLID AND SKIDDED TO A STOP ON THE RUNWAY WITHOUT ANY INJURIES TO THE OCCUPANTS AND ONLY MINOR DAMAGE TO THE ACFT. (THIS INVESTIGATION IS CLOSED.)

Other reports on N3003A · 1

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