Loss of Control in Flight · NTSB CEN16FA212
PIPER PA 28-140 — Wishek, ND
| Date | June 9, 2016 |
| Location | Wishek, ND |
| Aircraft | PIPER PA 28-140 |
| Purpose of flight | Personal |
| Conditions | Day · Visual Meteorological Cond |
| Phase / occurrence | Uncontrolled descent Collision with terr/obj (non-CFIT) |
| Pilot age | 20 |
| Pilot total time | 60 hrs · Student / very low time |
| Time in type | 22 hrs |
| Fatalities | 3 |
Probable cause
NTSB findings
- Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- Aircraft-Aircraft oper/perf/capability-Performance/control parameters-(general)-Not attained/maintained - C
- Personnel issues-Psychological-Personality/attitude-Motivation/respond to pressure-Pilot - F
What happened
The private pilot was flying his aunt and cousin to a location where his cousin could receive urgent dental care. The pilot was a member of the flying club that owned the airplane, and another member of the flying club reported that he thought that the pilot and his passengers were rushing as they prepared to leave. A witness located on the airport ramp saw the airplane take off, climb with a nose-high attitude, turn right, and rapidly pitch down to a nose-low attitude. The airplane was found in a lake 1/2 mile from the airport. Downloaded data from an onboard GPS navigation device were consistent with the observations of the witness and indicated that the airplane began to turn right at 160 ft above ground level with a groundspeed of 48 knots. The right turn continued for 20 seconds during which time the airplane climbed about 40 ft and its groundspeed ranged from 53 to 59 knots. The airplane then rapidly descended into the lake.
The damage to the airplane indicated that it impacted the lake in a near-vertical, nose-down attitude with low forward velocity. Examination of the airframe and engine revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. The GPS data, the witness report, and the damage to the airplane were consistent with the pilot failing to maintain sufficient airspeed during a climbing turn after takeoff, which resulted in the airplane's wing exceeding its critical angle of attack and an aerodynamic stall.
The purpose of the flight was for an urgent medical issue. The pilot's rushed activities before flight, and his actions immediately after takeoff to enter a climbing turn at low altitude without ensuring sufficient airspeed, are consistent with the effects of self-induced pressure.