Undetermined · NTSB WPR09FA414
PIPER PA-25 — Creswell, OR
| Date | August 23, 2009 |
| Location | Creswell, OR |
| Aircraft | PIPER PA-25 |
| Purpose of flight | Glider Tow |
| Conditions | Day · Visual Meteorological Cond |
| Phase / occurrence | Prior to flight Miscellaneous/other |
| Pilot age | 41 |
| Pilot total time | 400 hrs · Building experience |
| Time in type | 82 hrs |
| Fatalities | 1 |
Probable cause
NTSB findings
- Personnel issues-Physical-Impairment/incapacitation-Illicit drug-Pilot - F
- Environmental issues-Physical environment-(general)-(general)-Ability to respond/compensate - F
- Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Altitude-Not specified - F
What happened
Shortly after the airplane with a glider in tow departed, witnesses reported that it appeared that the glider overtook the tow airplane. One witness stated it appeared that the glider moved ahead of the tow airplane as the tow airplane descended. The witness reported that the accident airplane appeared to be slow and, approximately 200 feet above the ground, abruptly nosed over and impacted terrain. The student pilot of the glider reported that the takeoff roll, lift off and climb to 200 feet was normal. He stated that shortly after the glider reached 200 feet he heard a loud bang and glanced over his right should to find the rear door unlatched. As he looked back he noted that the glider was now above the normal tow position. The glider pilot pushed the stick forward to maneuver the glider to the proper tow position. The glider pilot noted slack in the tow line, and stated the tow airplane descended below the glider to a point where he lost sight of the airplane. He stated that the tow airplane did not seem to be in distress or out of control, and appeared to be in a 10 degree nose-down attitude prior to release. The glider pilot released from the tow airplane, turned 180 degrees back towards the airport, and landed without further incident. He stated that the release felt normal; the glider did not pitch up or down, and no abnormal yaw was noted. Examination of the tow airplane tail hook assembly revealed that the mounting plate was bent upward and the heads of two connecting bolts were in contact with the base of the rudder. The tail hook was intact and remained attached to the mounting plate. The hook was in the locked position, closed around the tow ring. The release cable remained attached to the hook and was continuous to the cockpit release handle. Functional testing of the tail hook assembly revealed no anomalies, and the assembly functioned appropriately. Examination revealed no evidence of mechanical malfunction or failure with the engine or airframe. Toxicology testing indicated the presence of marijuana in the tow pilot's blood and lung tissue. The levels of marijuana noted in the toxicology report suggest use of the illegal drug within 3 hours of the accident, which likely impaired him during the flight.