20040613018179A

Accident · Destroyed

FAA accident report · Piper PA-25-235 · Peoria, AZ · June 13, 2004

Date
June 13, 2004 · 15:04 local
Place
Peoria, AZ
Airport
Pleasant Valley Airport
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N4602Y
NTSB investigation
NTSBLAX04LA240
Reported as
Piper PA25235
Reported engine
Lycoming O540B2B5
People aboard
1
Fatal injuries
1
Pilot’s flight hours
1,775 total

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) Witnesses to the events stated that they observed the pawnee (tow plane) enter a higher than normal climb after a normal take-off. The glider which was on tow attempted to match the rate of climb but was unable to keep up. The tow rope between the aircraft went slack. The pawnee (tow plane) dropped its nose and gained sufficient airspeed to pull the slack out of the tow rope. The pawnee initiated an excessively nose high condition again, and the rope between the aircraft went slack again. At approximately 300 ft. AGL the glider released from the tow rope and executed a 270 degree turn to the right and landed across the runways. During this time the pawnee's nose stayed high and then the aircraft stalled and entered a spin to the right. The pawnee impacted the ground in an excessively nose down condition and was destroyed.

As the FAA filed it

(-23) WITNESSES TO THE EVENTS STATED THAT THEY OBSERVED THE PAWNEE (TOW PLANE) ENTER A HIGHER THAN NORMAL CLIMB AFTER A NORMAL TAKE-OFF. THE GLIDER WHICH WAS ON TOW ATTEMPTED TO MATCH THE RATE OF CLIMB BUT WAS UNABLE TO KEEP UP. THE TOW ROPE BETWEEN THE AIRCRAFT WENT SLACK. THE PAWNEE (TOW PLANE) DROPPED ITS NOSE AND GAINED SUFFICIENT AIRSPEED TO PULL THE SLACK OUT OF THE TOW ROPE. THE PAWNEE INITIATED AN EXCESSIVELY NOSE HIGH CONDITION AGAIN, AND THE ROPE BETWEEN THE AIRCRAFT WENT SLACK AGAIN. AT APPROXIMATELY 300 FT. AGL THE GLIDER RELEASED FROM THE TOW ROPE AND EXECUTED A 270 DEGREE TURN TO THE RIGHT AND LANDED ACROSS THE RUNWAYS. DURING THIS TIME THE PAWNEE'S NOSE STAYED HIGH AND THEN THE AIRCRAFT STALLED AND ENTERED A SPIN TO THE RIGHT. THE PAWNEE IMPACTED THE GROUND IN AN EXCESSIVELY NOSE DOWN CONDITION AND WAS DESTROYED.

NTSB investigation

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