20090823053599A

Accident · Destroyed

FAA accident report · Piper PA-25 · Creswell, OR · August 23, 2009

Date
August 23, 2009 · 16:25 local
Place
Creswell, OR
Airport
Hobby Field
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N6353Z
NTSB investigation
NTSBWPR09FA414
Reported as
Piper PA-25
Reported engine
Lycoming 0-320 series
People aboard
1
Fatal injuries
1
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
514 total127 in this make and model38 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.

On August 23, 2009 at approximately 2325Z, N6353Z, a PA-25, departed runway 33 at the Creswell Hobby airport with N65974, a Schweizer sgs 2-33A glider in tow. The glider was operated by a student pilot on his second solo flight. After departure, the glider pilot reported that he made a standard 200 foot call out. Shortly thereafter, the glider pilot heard a rattling sound behind his right shoulder. The glider pilot then glanced over his right shoulder to see the door unlatched. As the glider pilot turned back around, he noticed that the tow plane was below him and he could only see the top of the canopy. Shortly thereafter, the glider pilot pitched down in an attempt to get level with the tow plane. As he pitched down he noted slack developing in the tow rope as the glider passed over the top of the tow plane. At this point, the glider pilot released and made a 180 degree turn back to the airport and landed without incident. The tow plane crashed shortly thereafter in a field just north of the airport. The tow pilot died at the scene. On scene, the tow ring was still attached to the tow airplane's tow hook. The hook was a Schweizer design and was mounted in an inverted position. The tow hook was still closed around the tow ring. The plate to which the tow hook was attached was bent up and the heads of two connecting bolts were in contact with the base of the rudder. The tow rope was also present at the accident site with the ring that attaches to the glider. No discontinuities were noted with the in the flight controls. The NTSB subsequently inspected the engine and found no evidence of pre-impact engine damage.

As the FAA filed it

ON AUGUST 23, 2009 AT APPROXIMATELY 2325Z, N6353Z, A PA-25, DEPARTED RUNWAY 33 AT THE CRESWELL HOBBY AIRPORT WITH N65974, A SCHWEIZER SGS 2-33A GLIDER IN TOW. THE GLIDER WAS OPERATED BY A STUDENT PILOT ON HIS SECOND SOLO FLIGHT. AFTER DEPARTURE, THE GLIDER PILOT REPORTED THAT HE MADE A STANDARD 200 FOOT CALL OUT. SHORTLY THEREAFTER, THE GLIDER PILOT HEARD A RATTLING SOUND BEHIND HIS RIGHT SHOULDER. THE GLIDER PILOT THEN GLANCED OVER HIS RIGHT SHOULDER TO SEE THE DOOR UNLATCHED. AS THE GLIDER PILOT TURNED BACK AROUND, HE NOTICED THAT THE TOW PLANE WAS BELOW HIM AND HE COULD ONLY SEE THE TOP OF THE CANOPY. SHORTLY THEREAFTER, THE GLIDER PILOT PITCHED DOWN IN AN ATTEMPT TO GET LEVEL WITH THE TOW PLANE. AS HE PITCHED DOWN HE NOTED SLACK DEVELOPING IN THE TOW ROPE AS THE GLIDER PASSED OVER THE TOP OF THE TOW PLANE. AT THIS POINT, THE GLIDER PILOT RELEASED AND MADE A 180 DEGREE TURN BACK TO THE AIRPORT AND LANDED WITHOUT INCIDENT. THE TOW PLANE CRASHED SHORTLY THEREAFTER IN A FIELD JUST NORTH OF THE AIRPORT. THE TOW PILOT DIED AT THE SCENE. ON SCENE, THE TOW RING WAS STILL ATTACHED TO THE TOW AIRPLANE'S TOW HOOK. THE HOOK WAS A SCHWEIZER DESIGN AND WAS MOUNTED IN AN INVERTED POSITION. THE TOW HOOK WAS STILL CLOSED AROUND THE TOW RING. THE PLATE TO WHICH THE TOW HOOK WAS ATTACHED WAS BENT UP AND THE HEADS OF TWO CONNECTING BOLTS WERE IN CONTACT WITH THE BASE OF THE RUDDER. THE TOW ROPE WAS ALSO PRESENT AT THE ACCIDENT SITE WITH THE RING THAT ATTACHES TO THE GLIDER. NO DISCONTINUITIES WERE NOTED WITH THE IN THE FLIGHT CONTROLS. THE NTSB SUBSEQUENTLY INSPECTED THE ENGINE AND FOUND NO EVIDENCE OF PRE-IMPACT ENGINE DAMAGE.

NTSB investigation

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