20080919849859A

Accident · Substantial damage

FAA accident report · Cessna 120 · Jesup, GA · September 19, 2008

Date
September 19, 2008 · 11:00 local
Place
Jesup, GA
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N77068
NTSB investigation
NTSBMIA08LA196
Reported as
Cessna 120
Reported engine
Lycoming O290D
People aboard
2
Fatal injuries
0
Pilot’s flight hours
152 total88 in this make and model13 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) As reported by the pilot, after approximately one hour and twenty minutes of flight at an altitude of 3100 feet AGL the pilot noticed a film of oil beginning to accumulate on the windshield. Further examination by the pilot indicated the source of the oil to be coming over the forward right side of the engine cowling and onto the windshield. Within one minute, forward visibilty was severely restricted and the pilot relied on instruments and visual reference to the ground from the side window. The pilot went through his emergency checklist and scanned the engine instruments which were indicating normal oil pressure and temperature limits. The pilot reduced power and decided to ditch the aircraft in a clear hay field within gliding distance of his current position. Upon positioning the aircraft to land he lost forward visibility reference because of the oil obscured windshield and was unable to obtain a proper flair angle for touchdown. Subsequently, the aircraft landed firmly and the right main landing gear wheel and brake assembly separated upon touchdown, the aircraft came to rest on the nose substantially damaging the engine mounts, wings and the aircraft structure forward of the cockpit.

As the FAA filed it

(-23) AS REPORTED BY THE PILOT, AFTER APPROXIMATELY ONE HOUR AND TWENTY MINUTES OF FLIGHT AT AN ALTITUDE OF 3100 FEET AGL THE PILOT NOTICED A FILM OF OIL BEGINNING TO ACCUMULATE ON THE WINDSHIELD. FURTHER EXAMINATION BY THE PILOT INDICATED THE SOURCE OF THE OIL TO BE COMING OVER THE FORWARD RIGHT SIDE OF THE ENGINE COWLING AND ONTO THE WINDSHIELD. WITHIN ONE MINUTE, FORWARD VISIBILTY WAS SEVERELY RESTRICTED AND THE PILOT RELIED ON INSTRUMENTS AND VISUAL REFERENCE TO THE GROUND FROM THE SIDE WINDOW. THE PILOT WENT THROUGH HIS EMERGENCY CHECKLIST AND SCANNED THE ENGINE INSTRUMENTS WHICH WERE INDICATING NORMAL OIL PRESSURE AND TEMPERATURE LIMITS. THE PILOT REDUCED POWER AND DECIDED TO DITCH THE AIRCRAFT IN A CLEAR HAY FIELD WITHIN GLIDING DISTANCE OF HIS CURRENT POSITION. UPON POSITIONING THE AIRCRAFT TO LAND HE LOST FORWARD VISIBILITY REFERENCE BECAUSE OF THE OIL OBSCURED WINDSHIELD AND WAS UNABLE TO OBTAIN A PROPER FLAIR ANGLE FOR TOUCHDOWN. SUBSEQUENTLY, THE AIRCRAFT LANDED FIRMLY AND THE RIGHT MAIN LANDING GEAR WHEEL AND BRAKE ASSEMBLY SEPARATED UPON TOUCHDOWN, THE AIRCRAFT CAME TO REST ON THE NOSE SUBSTANTIALLY DAMAGING THE ENGINE MOUNTS, WINGS AND THE AIRCRAFT STRUCTURE FORWARD OF THE COCKPIT.

NTSB investigation

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

Other reports on N77068 · 1

Matched to the same aircraft by N-number and date.