20050416006639A

Accident · Substantial damage

FAA accident report · Tcraft BC12-D · Denver, CO · April 16, 2005

Date
April 16, 2005 · 12:38 local
Place
Denver, CO
Airport
Centennial Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N39230
NTSB investigation
NTSBDEN05LA069
Reported as
Tcraft BC12D
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,527 total5 in this make and model10 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 April 16, 2005 at approximately 1238 MDT, N39230 a Taylorcraft BC-12D ground looped after touchdown on runway 28 at Centennial Airport (apa). The pilot in command, sole occupant held a commercial pilot certificate, with airplane sel/mel and instrument rating was not injured. Weather at 1753Z was 0804KT 10SM few 050 sct 220 13/03 AT3020. The pilot stated after touchdown the wind shifted to a 90 degree crosswind and control was lost. Damage included the right wing spar broke outboard of strut attach points, rudder tip, propeller and engine cowling.

As the FAA filed it

(-23) ON APRIL 16, 2005 AT APPROXIMATELY 1238 MDT, N39230 A TAYLORCRAFT BC-12D GROUND LOOPED AFTER TOUCHDOWN ON RUNWAY 28 AT CENTENNIAL AIRPORT (APA). THE PILOT IN COMMAND, SOLE OCCUPANT HELD A COMMERCIAL PILOT CERTIFICATE, WITH AIRPLANE SEL/MEL AND INSTRUMENT RATING WAS NOT INJURED. WEATHER AT 1753Z WAS 0804KT 10SM FEW 050 SCT 220 13/03 AT3020. THE PILOT STATED AFTER TOUCHDOWN THE WIND SHIFTED TO A 90 DEGREE CROSSWIND AND CONTROL WAS LOST. DAMAGE INCLUDED THE RIGHT WING SPAR BROKE OUTBOARD OF STRUT ATTACH POINTS, RUDDER TIP, PROPELLER AND ENGINE COWLING.

NTSB investigation

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