20061026021899A

Accident · Substantial damage

FAA accident report · Maule M-5-235C · New Braunfels, TX · October 26, 2006

Date
October 26, 2006 · 17:10 local
Place
New Braunfels, TX
Airport
New Braunfels Municipal Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N32CX
NTSB investigation
NTSBDFW07CA015
Reported as
Maule M5235C
Reported engine
Lycoming O540*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
500 total5 in this make and model30 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.

(-23) On October 26, 2006 (approx 1710 LCL), a Maule model M-5 (registration N23CX) crashed following a ground loop. Pilot in command stated that he lost control during the landing phase due to a frontal gust of wind. The aircraft came off the runway during landing phase. The right landing gear broke at the right "a" frame assembly point, then the aircraft propeller struck the ground causing the aircraft to veer 180 degrees to the right. The aircraft came to rest outside the runway, by the apron. The aircraft received substantial damage to the propeller, right wing, left elevator, and a broken right landing gear spar. The fuselage skin surrounding the main landing gear appeared warped. No other property damage, no injuries reported, and no fire.

As the FAA filed it

(-23) ON OCTOBER 26, 2006 (APPROX 1710 LCL), A MAULE MODEL M-5 (REGISTRATION N23CX) CRASHED FOLLOWING A GROUND LOOP. PILOT IN COMMAND STATED THAT HE LOST CONTROL DURING THE LANDING PHASE DUE TO A FRONTAL GUST OF WIND. THE AIRCRAFT CAME OFF THE RUNWAY DURING LANDING PHASE. THE RIGHT LANDING GEAR BROKE AT THE RIGHT "A" FRAME ASSEMBLY POINT, THEN THE AIRCRAFT PROPELLER STRUCK THE GROUND CAUSING THE AIRCRAFT TO VEER 180 DEGREES TO THE RIGHT. THE AIRCRAFT CAME TO REST OUTSIDE THE RUNWAY, BY THE APRON. THE AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE TO THE PROPELLER, RIGHT WING, LEFT ELEVATOR, AND A BROKEN RIGHT LANDING GEAR SPAR. THE FUSELAGE SKIN SURROUNDING THE MAIN LANDING GEAR APPEARED WARPED. NO OTHER PROPERTY DAMAGE, NO INJURIES REPORTED, AND NO FIRE.

NTSB investigation

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