19980325004269A

Accident · Substantial damage

FAA accident report · Grtlks 2T-1A-2 · Pierson, FL · March 25, 1998

Date
March 25, 1998 · 13:30 local
Place
Pierson, FL
Airport
Pierson Municipal Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N3751F
NTSB investigation
NTSBMIA98LA108
Reported as
Grtlks 2T1A2
Reported engine
Lycoming AEIO360B1G6
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,196 total320 in this make and model75 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.

Flight of 4 aircraft 3 landed rwy 23 this one nosed over when brakes applied landing. Tailwind complacent factors. (-23) pilot landed downwind on 2600' grass runway in a tailwheel aircraft. Wind at nearby airports was estimated to be approximately from 040 degrees at 10 KTS. Pilot landed on runway 23. During rollout, pilot applied heavy braking and the aircraft nosed over, and came to rest inverted. The vertical stabilizer, rudder, upper wing, nose cowling, propeller sustained substantial damage. The engine was partially broken out of the engine mount.

As the FAA filed it

FLIGHT OF 4 AIRCRAFT 3 LANDED RWY 23 THIS ONE NOSED OVER WHEN BRAKES APPLIED LANDING. TAILWIND COMPLACENT FACTORS. (-23) PILOT LANDED DOWNWIND ON 2600' GRASS RUNWAY IN A TAILWHEEL AIRCRAFT. WIND AT NEARBY AIRPORTS WAS ESTIMATED TO BE APPROXIMATELY FROM 040 DEGREES AT 10 KTS. PILOT LANDED ON RUNWAY 23. DURING ROLLOUT, PILOT APPLIED HEAVY BRAKING AND THE AIRCRAFT NOSED OVER, AND CAME TO REST INVERTED. THE VERTICAL STABILIZER, RUDDER, UPPER WING, NOSE COWLING, PROPELLER SUSTAINED SUBSTANTIAL DAMAGE. THE ENGINE WAS PARTIALLY BROKEN OUT OF THE ENGINE MOUNT.

NTSB investigation

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