20080601857559A

Accident · Substantial damage

FAA accident report · Cessna 172H · Sweeden, NY · June 1, 2008

Date
June 1, 2008 · 12:00 local
Place
Sweeden, NY
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N3910R
NTSB investigation
NTSBNYC08LA199
Reported as
Cessna 172H
Reported engine
CONTIN 0-300
Fatal injuries
0
Pilot’s flight hours
16,750 total316 in this make and model70 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.

During a 14CFR part 91 training flight, a/c crashed 1 mile west of 7G0 due to probable fuel starvation. Both pilots onboard were seriously injured and the aircraft received substantial damage. Significant observations of this inspector: 1) fuel was insufficient for duration of flight. 2) flaps were not used during emergency landing. 3) no shoulder harnesses were installed and would have prevented many of the more serious injuries. 4)angle of impact was consistent with a stall and no spin. Accident was survivable due to low altitude at the time of stall. Impact forces would have been reduced if aircraft had impacted at a lower angle in controlled flight resulting in a longer skid.

As the FAA filed it

DURING A 14CFR PART 91 TRAINING FLIGHT, A/C CRASHED 1 MILE WEST OF 7G0 DUE TO PROBABLE FUEL STARVATION. BOTH PILOTS ONBOARD WERE SERIOUSLY INJURED AND THE AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE. SIGNIFICANT OBSERVATIONS OF THIS INSPECTOR: 1) FUEL WAS INSUFFICIENT FOR DURATION OF FLIGHT. 2) FLAPS WERE NOT USED DURING EMERGENCY LANDING. 3) NO SHOULDER HARNESSES WERE INSTALLED AND WOULD HAVE PREVENTED MANY OF THE MORE SERIOUS INJURIES. 4)ANGLE OF IMPACT WAS CONSISTENT WITH A STALL AND NO SPIN. ACCIDENT WAS SURVIVABLE DUE TO LOW ALTITUDE AT THE TIME OF STALL. IMPACT FORCES WOULD HAVE BEEN REDUCED IF AIRCRAFT HAD IMPACTED AT A LOWER ANGLE IN CONTROLLED FLIGHT RESULTING IN A LONGER SKID.

NTSB investigation

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