20151017019249A

Accident · Destroyed

FAA accident report · Piper PA-28R-180 · Palm Springs, CA · October 17, 2015

Date
October 17, 2015 · 15:52 local
Place
Palm Springs, CA
Airport
Palm Springs International
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N4972J
NTSB investigation
NTSBWPR16FA014
Reported as
Piper PA-28R-180
Reported engine
Lycoming I0360 series
People aboard
2
Fatal injuries
2
Other injuries
0
Pilot’s certificate
Private pilot

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.

The aircraft departed Palm Springs (psp) airport at approx. 15:20 local time enroute to santa barbara. Psp radar showed several instances of 360 degree climbing turns near san gorgonio mountain. At approx. 15:52 the aircraft impacted the east side of the san gorgonio mountain heading north west (aprox 330 deg. Magnetic.) The elevation of the impact was at approx. 7,140 ft.

The impact was at high velocity with all debris forward of the impact area. Neither the engine nor the propeller departed the aircraft due to the angle of the terrain (approx. 25 deg uphill slope). The attitude of the aircraft was slight nose up. The forward half of the fuselage was completely incinerated back to the rear seats.

As the FAA filed it

THE AIRCRAFT DEPARTED PALM SPRINGS (PSP) AIRPORT AT APPROX. 15:20 LOCAL TIME ENROUTE TO SANTA BARBARA. PSP RADAR SHOWED SEVERAL INSTANCES OF 360 DEGREE CLIMBING TURNS NEAR SAN GORGONIO MOUNTAIN. AT APPROX. 15:52 THE AIRCRAFT IMPACTED THE EAST SIDE OF THE SAN GORGONIO MOUNTAIN HEADING NORTH WEST (APROX 330 DEG. MAGNETIC.) THE ELEVATION OF THE IMPACT WAS AT APPROX. 7,140 FT.

THE IMPACT WAS AT HIGH VELOCITY WITH ALL DEBRIS FORWARD OF THE IMPACT AREA. NEITHER THE ENGINE NOR THE PROPELLER DEPARTED THE AIRCRAFT DUE TO THE ANGLE OF THE TERRAIN (APPROX. 25 DEG UPHILL SLOPE). THE ATTITUDE OF THE AIRCRAFT WAS SLIGHT NOSE UP. THE FORWARD HALF OF THE FUSELAGE WAS COMPLETELY INCINERATED BACK TO THE REAR SEATS.

NTSB investigation

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