19990126000759A

Accident · Substantial damage

FAA accident report · Beech A36 · Charleston, SC · January 26, 1999

Date
January 26, 1999 · 16:00 local
Place
Charleston, SC
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4976M
NTSB investigation
NTSBMIA99LA069
Reported as
Beech A36
Reported engine
Continental IO520BA
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,375 total1,875 in this make and model44 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 engine failed, and the pilot made an emergency landing in a field. (.4) the pilot reported that about 7 minutes after takeoff the airplane's engine lost oil pressure and started to lose oil, followed by a loss of engine power. The airplane started a descent that the pilot could not arrest, and continued to descend at a rate of about 100-200 feet per minute. The pilot then heard, 'a loud bang...a shudder occurred in the engine compartment, and the engine lost power.' The pilot banked the airplane, and headed towards a clearing. The engine compartment appeared to be on fire, and smoke began to enter the cockpit. He elected to make a forced landing in a field. The engine was examined at the crash site, and a hole was noted in the case at the no. 4 cylinder. Oil was observed on the no. 4 cylinder wall, the oil dip stick did not show any oil, and there was evidence that oil had leaked out of the engine. The engine was examined on February 12, 1999, and the examination revealed that oil had leaked at the engine oil filter adapter. In addition, there were more threads showing on one stud than on the other. A torque wrench was used to check torque on the nuts. It was noted t hat one nut rotated 1 1/2 rotations before reaching the specified torque. The other nut rotated 1 rotation before reaching torque. The oil filter adapter was removed for further examination, and revealed that the gasket was found with a gap at the corner with a opening of about 1/16 of an inch. It was concluded, that the leak caused the engine to exhaust the oil supply, causing the no. 4 cylinder connecting rod to fail, which resulted in a total loss of engine power. (-23)pilot reported engine failure during climbout. Force landing in a plowed field. Aircraft sustained substantial damage. Examination of engine disclosed complete loss of oil quantity causing #4 connecting rod to break and come through the engine case.

As the FAA filed it

ACFT ENGINE FAILED, AND THE PILOT MADE AN EMERGENCY LANDING IN A FIELD. (.4) THE PILOT REPORTED THAT ABOUT 7 MINUTES AFTER TAKEOFF THE AIRPLANE'S ENGINE LOST OIL PRESSURE AND STARTED TO LOSE OIL, FOLLOWED BY A LOSS OF ENGINE POWER. THE AIRPLANE STARTED A DESCENT THAT THE PILOT COULD NOT ARREST, AND CONTINUED TO DESCEND AT A RATE OF ABOUT 100-200 FEET PER MINUTE. THE PILOT THEN HEARD, 'A LOUD BANG...A SHUDDER OCCURRED IN THE ENGINE COMPARTMENT, AND THE ENGINE LOST POWER.' THE PILOT BANKED THE AIRPLANE, AND HEADED TOWARDS A CLEARING. THE ENGINE COMPARTMENT APPEARED TO BE ON FIRE, AND SMOKE BEGAN TO ENTER THE COCKPIT. HE ELECTED TO MAKE A FORCED LANDING IN A FIELD. THE ENGINE WAS EXAMINED AT THE CRASH SITE, AND A HOLE WAS NOTED IN THE CASE AT THE NO. 4 CYLINDER. OIL WAS OBSERVED ON THE NO. 4 CYLINDER WALL, THE OIL DIP STICK DID NOT SHOW ANY OIL, AND THERE WAS EVIDENCE THAT OIL HAD LEAKED OUT OF THE ENGINE. THE ENGINE WAS EXAMINED ON FEBRUARY 12, 1999, AND THE EXAMINATION REVEALED THAT OIL HAD LEAKED AT THE ENGINE OIL FILTER ADAPTER. IN ADDITION, THERE WERE MORE THREADS SHOWING ON ONE STUD THAN ON THE OTHER. A TORQUE WRENCH WAS USED TO CHECK TORQUE ON THE NUTS. IT WAS NOTED T HAT ONE NUT ROTATED 1 1/2 ROTATIONS BEFORE REACHING THE SPECIFIED TORQUE. THE OTHER NUT ROTATED 1 ROTATION BEFORE REACHING TORQUE. THE OIL FILTER ADAPTER WAS REMOVED FOR FURTHER EXAMINATION, AND REVEALED THAT THE GASKET WAS FOUND WITH A GAP AT THE CORNER WITH A OPENING OF ABOUT 1/16 OF AN INCH. IT WAS CONCLUDED, THAT THE LEAK CAUSED THE ENGINE TO EXHAUST THE OIL SUPPLY, CAUSING THE NO. 4 CYLINDER CONNECTING ROD TO FAIL, WHICH RESULTED IN A TOTAL LOSS OF ENGINE POWER. (-23)PILOT REPORTED ENGINE FAILURE DURING CLIMBOUT. FORCE LANDING IN A PLOWED FIELD. AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE. EXAMINATION OF ENGINE DISCLOSED COMPLETE LOSS OF OIL QUANTITY CAUSING #4 CONNECTING ROD TO BREAK AND COME THROUGH THE ENGINE CASE.

NTSB investigation

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