20081215856039I

Incident · No damage

FAA incident report · Cessna 182N · Sanford, ME · December 15, 2008

Date
December 15, 2008 · 12:05 local
Place
Sanford, ME
Airport
Sanford Regional
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N92207
Reported as
Cessna 182N
Reported engine
Continental O470P
People aboard
2
Fatal injuries
0
Pilot’s flight hours
4,250 total200 in this make and model100 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) Flight instructor and student on crosscountry from B19 to lwm. Reaching 4500 ft CFI noticed smoke from the cowling followed by falling oil pressure. CFI decided to land at sfm. CFI contacted pwm approach informed them of engine failure and prop stoppage. Attempted landing on 25 at sfm. Strong winds forced them to land in an open field 3 miles short of runway. No damage and no injuries from landing. Aircraft engine sustained catastrophic damage from what appeared to be the number 2 cylinder connecting rod breaching the top of the engine case. Aircraft wings were disassembled and aircraft relocated to sfm.

As the FAA filed it

(-23) FLIGHT INSTRUCTOR AND STUDENT ON CROSSCOUNTRY FROM B19 TO LWM. REACHING 4500 FT CFI NOTICED SMOKE FROM THE COWLING FOLLOWED BY FALLING OIL PRESSURE. CFI DECIDED TO LAND AT SFM. CFI CONTACTED PWM APPROACH INFORMED THEM OF ENGINE FAILURE AND PROP STOPPAGE. ATTEMPTED LANDING ON 25 AT SFM. STRONG WINDS FORCED THEM TO LAND IN AN OPEN FIELD 3 MILES SHORT OF RUNWAY. NO DAMAGE AND NO INJURIES FROM LANDING. AIRCRAFT ENGINE SUSTAINED CATASTROPHIC DAMAGE FROM WHAT APPEARED TO BE THE NUMBER 2 CYLINDER CONNECTING ROD BREACHING THE TOP OF THE ENGINE CASE. AIRCRAFT WINGS WERE DISASSEMBLED AND AIRCRAFT RELOCATED TO SFM.