20120127001419A

Accident · Destroyed

FAA accident report · Cessna 340A · Ocala, FL · January 27, 2012

Date
January 27, 2012 · 12:27 local
Place
Ocala, FL
Airport
Ocala International-Jim Taylor Field
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N340HF
NTSB investigation
NTSBERA12FA161
Reported as
Cessna 340A
Reported engine
Continental TSIO-520 series
People aboard
2
Fatal injuries
1
Other injuries
1
Pilot’s certificate
Private pilot
Pilot’s flight hours
1,005 total84 in this make and model16 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.

A Cessna 340 aircraft flying IFR en route to the Ocala international airport from the middle Georgia regional airport in macon, Georgia on a controlled flight crashed less than a mile from the end of the runway where the pilot was attempting to land the plane. The crash happened just before 12:30 p.m. it was noted from radar that the aircraft descended at a rate of 600 feet per minute from 1000 feet, winds were 260 @ 9 gusting 15 flying a south downwind approach to runway 36, with a pattern to the west of the airport. The aircraft turned left to base and was transitioning to the left turn for final approach coming in from the south gear was identified down but, the aircraft was noted in a slightly unusual location and attitude for approach. When speaking with the tower, again the flight considered controlled stated that no distress call was ever made and no indications of an emergency were present. The pilot deceased, needed to be extricated from the plane; his passenger privacy data omitted who was seated in the cabin survived and was transferred to a nearby hospital with serious injuries. Witness's stated they heard the engine cut out and then saw an explosion. Initial assessments observed as such, the strikes to the ground show a pattern of what would exhibit his left wing/tip tank low during turn, followed by propeller strikes, nose strike then the aircraft completing a flat spin placing it in the opposite direction of travel, the debris field shows it was contained; the aircraft upright pointing toward an easterly direction after impact. The left wing bent up and partially separated. The flaps were actuated to be in approach position at 15 degrees. It appears the nose area impacted the ground giving lift and causing the aircraft to spin and at this time cannot rule out a possible fire within the janitrol heater and although it appears intact the oxygen cylinder installed. The propellers blades were severely curled showing rotation with multiple ground strikes apparent and depict the engines were running on impact. The tail section broke off just aft of the cabin, as most damage significant to the left given the approach. The fire appeared contained within the nose compartment/ hull area with indications of smaller fire damage to underlying areas. Further investigation sequentially shows the throttles were full forward and the gear handle was in the up position in which the pilot may have been initiating a go around, speaking with the descendants wife later, she stated he made mention that they were too low and she remembers hearing warning horns. When reiterating the question, it was noted she heard two different alarms, in which given the circumstances may have been gear warning & stall warning. As noted previously his present position, unusual location and attitude. After further inspection at an alternate site, it was noted the gear itself was in transition, the left fuel selector in the right tank position but, the right fuel selector in the auxiliary position not consistent with landing positions. The engine preliminary inspections and associated accessories appear to be functioning and awaiting further instructions. The aircraft equipped with an engine monitoring system will be evaluated for possible engine problems undetected in flight. The pilot's flight log book was recovered from the wreckage with minimal damage and is still under review. At this time preliminary investigation indicates the aircraft was performing as required without distress and information obtained to date is the aircraft angle while on approach may have been too low to recover or initiating a go around for landing.

As the FAA filed it

A CESSNA 340 AIRCRAFT FLYING IFR EN ROUTE TO THE OCALA INTERNATIONAL AIRPORT FROM THE MIDDLE GEORGIA REGIONAL AIRPORT IN MACON, GEORGIA ON A CONTROLLED FLIGHT CRASHED LESS THAN A MILE FROM THE END OF THE RUNWAY WHERE THE PILOT WAS ATTEMPTING TO LAND THE PLANE. THE CRASH HAPPENED JUST BEFORE 12:30 P.M. IT WAS NOTED FROM RADAR THAT THE AIRCRAFT DESCENDED AT A RATE OF 600 FEET PER MINUTE FROM 1000 FEET, WINDS WERE 260 @ 9 GUSTING 15 FLYING A SOUTH DOWNWIND APPROACH TO RUNWAY 36, WITH A PATTERN TO THE WEST OF THE AIRPORT. THE AIRCRAFT TURNED LEFT TO BASE AND WAS TRANSITIONING TO THE LEFT TURN FOR FINAL APPROACH COMING IN FROM THE SOUTH GEAR WAS IDENTIFIED DOWN BUT, THE AIRCRAFT WAS NOTED IN A SLIGHTLY UNUSUAL LOCATION AND ATTITUDE FOR APPROACH. WHEN SPEAKING WITH THE TOWER, AGAIN THE FLIGHT CONSIDERED CONTROLLED STATED THAT NO DISTRESS CALL WAS EVER MADE AND NO INDICATIONS OF AN EMERGENCY WERE PRESENT. THE PILOT DECEASED, NEEDED TO BE EXTRICATED FROM THE PLANE; HIS PASSENGER ^PRIVACY DATA OMITTED^ WHO WAS SEATED IN THE CABIN SURVIVED AND WAS TRANSFERRED TO A NEARBY HOSPITAL WITH SERIOUS INJURIES. WITNESS'S STATED THEY HEARD THE ENGINE CUT OUT AND THEN SAW AN EXPLOSION. INITIAL ASSESSMENTS OBSERVED AS SUCH, THE STRIKES TO THE GROUND SHOW A PATTERN OF WHAT WOULD EXHIBIT HIS LEFT WING/TIP TANK LOW DURING TURN, FOLLOWED BY PROPELLER STRIKES, NOSE STRIKE THEN THE AIRCRAFT COMPLETING A FLAT SPIN PLACING IT IN THE OPPOSITE DIRECTION OF TRAVEL, THE DEBRIS FIELD SHOWS IT WAS CONTAINED; THE AIRCRAFT UPRIGHT POINTING TOWARD AN EASTERLY DIRECTION AFTER IMPACT. THE LEFT WING BENT UP AND PARTIALLY SEPARATED. THE FLAPS WERE ACTUATED TO BE IN APPROACH POSITION AT 15 DEGREES. IT APPEARS THE NOSE AREA IMPACTED THE GROUND GIVING LIFT AND CAUSING THE AIRCRAFT TO SPIN AND AT THIS TIME CANNOT RULE OUT A POSSIBLE FIRE WITHIN THE JANITROL HEATER AND ALTHOUGH IT APPEARS INTACT THE OXYGEN CYLINDER INSTALLED. THE PROPELLERS BLADES WERE SEVERELY CURLED SHOWING ROTATION WITH MULTIPLE GROUND STRIKES APPARENT AND DEPICT THE ENGINES WERE RUNNING ON IMPACT. THE TAIL SECTION BROKE OFF JUST AFT OF THE CABIN, AS MOST DAMAGE SIGNIFICANT TO THE LEFT GIVEN THE APPROACH. THE FIRE APPEARED CONTAINED WITHIN THE NOSE COMPARTMENT/ HULL AREA WITH INDICATIONS OF SMALLER FIRE DAMAGE TO UNDERLYING AREAS. FURTHER INVESTIGATION SEQUENTIALLY SHOWS THE THROTTLES WERE FULL FORWARD AND THE GEAR HANDLE WAS IN THE UP POSITION IN WHICH THE PILOT MAY HAVE BEEN INITIATING A GO AROUND, SPEAKING WITH THE DESCENDANTS WIFE LATER, SHE STATED HE MADE MENTION THAT THEY WERE TOO LOW AND SHE REMEMBERS HEARING WARNING HORNS. WHEN REITERATING THE QUESTION, IT WAS NOTED SHE HEARD TWO DIFFERENT ALARMS, IN WHICH GIVEN THE CIRCUMSTANCES MAY HAVE BEEN GEAR WARNING & STALL WARNING. AS NOTED PREVIOUSLY HIS PRESENT POSITION, UNUSUAL LOCATION AND ATTITUDE. AFTER FURTHER INSPECTION AT AN ALTERNATE SITE, IT WAS NOTED THE GEAR ITSELF WAS IN TRANSITION, THE LEFT FUEL SELECTOR IN THE RIGHT TANK POSITION BUT, THE RIGHT FUEL SELECTOR IN THE AUXILIARY POSITION NOT CONSISTENT WITH LANDING POSITIONS.THE ENGINE PRELIMINARY INSPECTIONS AND ASSOCIATED ACCESSORIES APPEAR TO BE FUNCTIONING AND AWAITING FURTHER INSTRUCTIONS. THE AIRCRAFT EQUIPPED WITH AN ENGINE MONITORING SYSTEM WILL BE EVALUATED FOR POSSIBLE ENGINE PROBLEMS UNDETECTED IN FLIGHT. THE PILOT'S FLIGHT LOG BOOK WAS RECOVERED FROM THE WRECKAGE WITH MINIMAL DAMAGE AND IS STILL UNDER REVIEW. AT THIS TIME PRELIMINARY INVESTIGATION INDICATES THE AIRCRAFT WAS PERFORMING AS REQUIRED WITHOUT DISTRESS AND INFORMATION OBTAINED TO DATE IS THE AIRCRAFT ANGLE WHILE ON APPROACH MAY HAVE BEEN TOO LOW TO RECOVER OR INITIATING A GO AROUND FOR LANDING.

NTSB investigation

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