20010425006709I

Incident · Minor damage

FAA incident report · Cessna 172R · Oklahoma City, OK · April 25, 2001

Date
April 25, 2001 · 13:45 local
Place
Oklahoma City, OK
Airport
Sundance Airpark Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N330JE
Reported as
Cessna 172R
People aboard
3
Fatal injuries
0
Pilot’s flight hours
14,000 total600 in this make and model120 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) At approx. 1400 hours local time, the pilot was acting as PIC of a/c N330JE during a training flight at Sundance airport. The pilot was demonstrating a forward slip to land on runway 17, when on short final the sink rate suddenly increased resulting in a tail low hard landing. The pilot added power becoming airborne and chose to return to will rogers world airport. Examination of the a/c revealed that the bottom tail skin and tail tie down skid was damaged. The vertical stabilizer and rudder had wrinkled skin at the upper and lower hinge points. The horizontal stabilizer lower skins were oil canned.

As the FAA filed it

(-23) AT APPROX. 1400 HOURS LOCAL TIME, THE PILOT WAS ACTING AS PIC OF A/C N330JE DURING A TRAINING FLIGHT AT SUNDANCE AIRPORT. THE PILOT WAS DEMONSTRATING A FORWARD SLIP TO LAND ON RUNWAY 17, WHEN ON SHORT FINAL THE SINK RATE SUDDENLY INCREASED RESULTING IN A TAIL LOW HARD LANDING. THE PILOT ADDED POWER BECOMING AIRBORNE AND CHOSE TO RETURN TO WILL ROGERS WORLD AIRPORT. EXAMINATION OF THE A/C REVEALED THAT THE BOTTOM TAIL SKIN AND TAIL TIE DOWN SKID WAS DAMAGED. THE VERTICAL STABILIZER AND RUDDER HAD WRINKLED SKIN AT THE UPPER AND LOWER HINGE POINTS. THE HORIZONTAL STABILIZER LOWER SKINS WERE OIL CANNED.