19990606010729A

Accident · Substantial damage

FAA accident report · Cessna 182E · Rolling Fork, MS · June 6, 1999

Date
June 6, 1999 · 14:30 local
Place
Rolling Fork, MS
Airport
Wade Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9267X
NTSB investigation
NTSBMIA99LA166
Reported as
Cessna 182E
Reported engine
Continental O470R
People aboard
5
Fatal injuries
0
Pilot’s flight hours
196 total30 in this make and model50 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.

On JUNE6,1999, about 1430 central daylight time, a Cessna 182E,N9267X, registered to Wade and son, inc., made a forced landing in a field following loss of engine power near Rolling Fork, Mississippi, while on a title 14CFR part 91 parachute drop flight. Visual metierological conditions prevailed at the time and no flight plan was filed. The aircraft received substantial damage and the private-rated pilot and four parachutists were not injured. The flight orginated from Rolling Fork airport, a few minutes before the accident. The pilot stated to an FAA inspector that while climbing through 600 feet AGL after takeoff, the engine lost power. He made a forced landing in a field, at which time, the nose landing gear collapsed. (.4)while climbing through 600 feet after takeoff, a loud bang was heard and a hole appeared in the top of the engine cowling. Oil leaked from the engine and covered the windshield. The engine did not stop running, but did loose power. A forced landing was landing was made in a field and the nose landing gear collapsed during rollout. Post crash examination of the engine s howed the number 3 connecting rod had separated from the crankshaft. Examination of the number three connecting rod bolts showed one bolt in the dowel area. The other bolt separated due to bending overstress. Examination of connecting rod bolts from the numbers 1 and 2 connecting rods showed slight rubbing in the dowel area of the bolts. Breakaway torque on the numbers 1,2,5, and 6 connecting rod bolts showed torque values below the manufacturers requirements.

As the FAA filed it

ON JUNE6,1999, ABOUT 1430 CENTRAL DAYLIGHT TIME, A CESSNA 182E,N9267X, REGISTERED TO WADE AND SON, INC., MADE A FORCED LANDING IN A FIELD FOLLOWING LOSS OF ENGINE POWER NEAR ROLLING FORK, MISSISSIPPI, WHILE ON A TITLE 14CFR PART 91 PARACHUTE DROP FLIGHT. VISUAL METIEROLOGICAL CONDITIONS PREVAILED AT THE TIME AND NO FLIGHT PLAN WAS FILED. THE AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE AND THE PRIVATE-RATED PILOT AND FOUR PARACHUTISTS WERE NOT INJURED.THE FLIGHT ORGINATED FROM ROLLING FORK AIRPORT, A FEW MINUTES BEFORE THE ACCIDENT. THE PILOT STATED TO AN FAA INSPECTOR THAT WHILE CLIMBING THROUGH 600 FEET AGL AFTER TAKEOFF, THE ENGINE LOST POWER. HE MADE A FORCED LANDING IN A FIELD, AT WHICH TIME, THE NOSE LANDING GEAR COLLAPSED. (.4)WHILE CLIMBING THROUGH 600 FEET AFTER TAKEOFF, A LOUD BANG WAS HEARD AND A HOLE APPEARED IN THE TOP OF THE ENGINE COWLING. OIL LEAKED FROM THE ENGINE AND COVERED THE WINDSHIELD. THE ENGINE DID NOT STOP RUNNING, BUT DID LOOSE POWER. A FORCED LANDING WAS LANDING WAS MADE IN A FIELD AND THE NOSE LANDING GEAR COLLAPSED DURING ROLLOUT. POST CRASH EXAMINATION OF THE ENGINE S HOWED THE NUMBER 3 CONNECTING ROD HAD SEPARATED FROM THE CRANKSHAFT. EXAMINATION OF THE NUMBER THREE CONNECTING ROD BOLTS SHOWED ONE BOLT IN THE DOWEL AREA. THE OTHER BOLT SEPARATED DUE TO BENDING OVERSTRESS. EXAMINATION OF CONNECTING ROD BOLTS FROM THE NUMBERS 1 AND 2 CONNECTING RODS SHOWED SLIGHT RUBBING IN THE DOWEL AREA OF THE BOLTS. BREAKAWAY TORQUE ON THE NUMBERS 1,2,5, AND 6 CONNECTING ROD BOLTS SHOWED TORQUE VALUES BELOW THE MANUFACTURERS REQUIREMENTS.

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 N9267X · 1

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