20001121024829A

Accident · Substantial damage

FAA accident report · Piper PA-32RT-300 · Wewahitchka, FL · November 21, 2000

Date
November 21, 2000 · 09:30 local
Place
Wewahitchka, FL
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9658C
NTSB investigation
NTSBMIA01LA032
Reported as
Piper PA32RT300
Reported engine
Lycoming IO540K1G5D
People aboard
3
Fatal injuries
0
Pilot’s flight hours
10,500 total400 in this make and model125 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.

(-23) A Piper PA-32RT-300, owned by grady and francis inc., lost engine power and was forced to land in rough terrain near Wewahitchka, Florida. (.4) on November 21, 2000, about 0930 central standard time, a Piper PA-32RT-300, N9658C, owned by grady and francis inc., lost engine power and was forced to land in rough terrain near Wewahitchka, Florida. Visual meteorological conditions prevailed at the time, and an IFR flight plan was filed for the 14 CFR part 91 personal flight. The airplane was substantially damaged. The airline transport-rated pilot and two passengers reported no injuries. The flight departed from orlando executive airport, Florida, at an unknown time, en route to panama city, Florida. According to the pilot he smelled something, and when he checked the instruments he noticed that the oil pressure had decreased. He felt that he could not make an on airport landing so he decided to land in rough terrain. At touchdown, the landing gear tore off, causing damage to the wings. Examination of the engine revealed no visible oil on top of the engine, but oil was observed at the lower portion of the firewall. The engine was torndown and examined at atlanta air salvage, griffin, george, under the supervision of phil power, senior air safety investigator, atlanta, Georgia, on February 1, 2001. The examination revealed that the number 5 cylinder connecting rod had separated at the rod cap. The crankcase had a 3 inches by 1 1/2 inch hole in the bottom of the case between the crankshaft and the oil sump at the number 5 location of the crankshaft. Pieces of the number 5 connecting rod cap,rod cap bolts, and nuts wererecovered fragmented.

As the FAA filed it

(-23) A PIPER PA-32RT-300, OWNED BY GRADY AND FRANCIS INC., LOST ENGINE POWER AND WAS FORCED TO LAND IN ROUGH TERRAIN NEAR WEWAHITCHKA, FLORIDA. (.4) ON NOVEMBER 21, 2000, ABOUT 0930 CENTRAL STANDARD TIME, A PIPER PA-32RT-300, N9658C, OWNED BY GRADY AND FRANCIS INC., LOST ENGINE POWER AND WAS FORCED TO LAND IN ROUGH TERRAIN NEAR WEWAHITCHKA, FLORIDA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME, AND AN IFR FLIGHT PLAN WAS FILED FOR THE 14 CFR PART 91 PERSONAL FLIGHT. THE AIRPLANE WAS SUBSTANTIALLY DAMAGED. THE AIRLINE TRANSPORT-RATED PILOT AND TWO PASSENGERS REPORTED NO INJURIES. THE FLIGHT DEPARTED FROM ORLANDO EXECUTIVE AIRPORT, FLORIDA, AT AN UNKNOWN TIME, EN ROUTE TO PANAMA CITY, FLORIDA. ACCORDING TO THE PILOT HE SMELLED SOMETHING, AND WHEN HE CHECKED THE INSTRUMENTS HE NOTICED THAT THE OIL PRESSURE HAD DECREASED. HE FELT THAT HE COULD NOT MAKE AN ON AIRPORT LANDING SO HE DECIDED TO LAND IN ROUGH TERRAIN. AT TOUCHDOWN, THE LANDING GEAR TORE OFF, CAUSING DAMAGE TO THE WINGS. EXAMINATION OF THE ENGINE REVEALED NO VISIBLE OIL ON TOP OF THE ENGINE, BUT OIL WAS OBSERVED AT THE LOWER PORTION OF THE FIREWALL. THE ENGINE WAS TORNDOWN AND EXAMINED AT ATLANTA AIR SALVAGE, GRIFFIN, GEORGE, UNDER THE SUPERVISION OF PHIL POWER, SENIOR AIR SAFETY INVESTIGATOR, ATLANTA, GEORGIA, ON FEBRUARY 1, 2001. THE EXAMINATION REVEALED THAT THE NUMBER 5 CYLINDER CONNECTING ROD HAD SEPARATED AT THE ROD CAP. THE CRANKCASE HAD A 3 INCHES BY 1 1/2 INCH HOLE IN THE BOTTOM OF THE CASE BETWEEN THE CRANKSHAFT AND THE OIL SUMP AT THE NUMBER 5 LOCATION OF THE CRANKSHAFT. PIECES OF THE NUMBER 5 CONNECTING ROD CAP,ROD CAP BOLTS, AND NUTS WERERECOVERED FRAGMENTED.

NTSB investigation

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