19990801010169A

Accident · Destroyed

FAA accident report · Piper PA-32-260 · Youngstown, OH · August 1, 1999

Date
August 1, 1999 · 13:59 local
Place
Youngstown, OH
Airport
Youngstown Elser Metro Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N5526J
NTSB investigation
NTSBNYC99FA187
Reported as
Piper PA32260
Reported engine
Lycoming O540E4B5
People aboard
4
Fatal injuries
4
Pilot’s flight hours
1,768 total23 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.

Acft crashed shortly after take-off under unknown circumstances, the pilot and 3 pax sustained fatal injuries, another pax has serious injuries, the acft was destroyed, other circumstances are unknown. (.4)after landing, the airplane's main fuel tanks were filled, and the five people got back onboard. The tail was almost touching the ground, and the airplane was sitting nose high. After takeoff, the airplane appeared to have a hard time climbing out, and was 'hanging on the prop.' The airplane turned toward a left downwind. It was initially nose high, then started to slowly lose altitude. Altitude loss quickened, the airplane's nose fell through, and the airplane maintained a sliding, left turn until it impacted the ground about 1/2 mile southwest of the airport. The engine was heard 'roaring' prior to impact, chordwise scratches were found on the propeller blades, and rotational marks were found on the starter housing. The estimated weight of the airplane was approximately 10 pounds under maximum gross weight, while center of gravity computations, using several different baggage loading scenarios, ranged from 1.1 inches, to 0.3 inches, forward of the aft center of gravity limit. Temperture at the time of the accident was 81 degrees fahrenheit, and the density was about 2,600 feet MSL.

As the FAA filed it

ACFT CRASHED SHORTLY AFTER TAKE-OFF UNDER UNKNOWN CIRCUMSTANCES, THE PILOT AND 3 PAX SUSTAINED FATAL INJURIES, ANOTHER PAX HAS SERIOUS INJURIES, THE ACFT WAS DESTROYED, OTHER CIRCUMSTANCES ARE UNKNOWN. (.4)AFTER LANDING, THE AIRPLANE'S MAIN FUEL TANKS WERE FILLED, AND THE FIVE PEOPLE GOT BACK ONBOARD. THE TAIL WAS ALMOST TOUCHING THE GROUND, AND THE AIRPLANE WAS SITTING NOSE HIGH. AFTER TAKEOFF, THE AIRPLANE APPEARED TO HAVE A HARD TIME CLIMBING OUT, AND WAS 'HANGING ON THE PROP.' THE AIRPLANE TURNED TOWARD A LEFT DOWNWIND. IT WAS INITIALLY NOSE HIGH, THEN STARTED TO SLOWLY LOSE ALTITUDE. ALTITUDE LOSS QUICKENED, THE AIRPLANE'S NOSE FELL THROUGH, AND THE AIRPLANE MAINTAINED A SLIDING, LEFT TURN UNTIL IT IMPACTED THE GROUND ABOUT 1/2 MILE SOUTHWEST OF THE AIRPORT. THE ENGINE WAS HEARD 'ROARING' PRIOR TO IMPACT, CHORDWISE SCRATCHES WERE FOUND ON THE PROPELLER BLADES, AND ROTATIONAL MARKS WERE FOUND ON THE STARTER HOUSING. THE ESTIMATED WEIGHT OF THE AIRPLANE WAS APPROXIMATELY 10 POUNDS UNDER MAXIMUM GROSS WEIGHT, WHILE CENTER OF GRAVITY COMPUTATIONS, USING SEVERAL DIFFERENT BAGGAGE LOADING SCENARIOS, RANGED FROM 1.1 INCHES, TO 0.3 INCHES, FORWARD OF THE AFT CENTER OF GRAVITY LIMIT. TEMPERTURE AT THE TIME OF THE ACCIDENT WAS 81 DEGREES FAHRENHEIT, AND THE DENSITY WAS ABOUT 2,600 FEET MSL.

NTSB investigation

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