20160516005089A

Accident · Destroyed

FAA accident report · Beech A36TC · Tupelo, MS · May 16, 2016

Date
May 16, 2016 · 08:32 local
Place
Tupelo, MS
Airport
Tupelo Regional Airport
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N60RW
NTSB investigation
NTSBERA16FA185
Reported as
Beech A36TC
Reported engine
Continental TSIO-520 series
People aboard
4
Fatal injuries
4
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
5,675 total

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 may 16, 2016 about 0835 Beech A36TC N60RW impacted terrain north of the Tupelo airport (tup). An instrument flight plan was filed for this flight. According to air traffic control recordings, shortly after departing runway 36, the pilot advised the tower controller that there was smoke in the cockpit and that they needed to return to the airport. According to witnesses, the airplane made a left, westbound turn, at an altitude of about 500-1,000 feet. Witnesses reported seeing the airplane turning back towards the approach end of runway 18. Witnesses also reported seeing the airplane in a descent with smoke and flames coming from the front left side of the airplane before hearing it impact terrain.

The wreckage was mostly consumed by fire. The airplane struck several trees along an estimated 190 feet during its descent to where it impacted terrain. All flight controls were accounted for at the accident site. Flight control continuity was confirmed to respective inputs. The outboard portion of the right wing was separated from the airplane and heavily burned about 60 feet from the main wreckage. The left wing was still attached to the fuselage. The propeller blades signs of bending and gouging. A few propeller chop marks were visible on the limbs. The exhaust pipe was missing from the engine at the accident site.

The exhaust pipe, fractured v-band clamp and two pieces of heat insulation wrap were recovered from the runway by airport personnel. The items were found in the following order from initial take off roll: 10 piece of insulation wrap, 2) piece of insulation wrap, 3) v-band clamp, 4) exhaust pipe.

As the FAA filed it

ON MAY 16, 2016 ABOUT 0835 BEECH A36TC N60RW IMPACTED TERRAIN NORTH OF THE TUPELO AIRPORT (TUP). AN INSTRUMENT FLIGHT PLAN WAS FILED FOR THIS FLIGHT. ACCORDING TO AIR TRAFFIC CONTROL RECORDINGS, SHORTLY AFTER DEPARTING RUNWAY 36, THE PILOT ADVISED THE TOWER CONTROLLER THAT THERE WAS SMOKE IN THE COCKPIT AND THAT THEY NEEDED TO RETURN TO THE AIRPORT. ACCORDING TO WITNESSES, THE AIRPLANE MADE A LEFT, WESTBOUND TURN, AT AN ALTITUDE OF ABOUT 500-1,000 FEET. WITNESSES REPORTED SEEING THE AIRPLANE TURNING BACK TOWARDS THE APPROACH END OF RUNWAY 18. WITNESSES ALSO REPORTED SEEING THE AIRPLANE IN A DESCENT WITH SMOKE AND FLAMES COMING FROM THE FRONT LEFT SIDE OF THE AIRPLANE BEFORE HEARING IT IMPACT TERRAIN.

THE WRECKAGE WAS MOSTLY CONSUMED BY FIRE. THE AIRPLANE STRUCK SEVERAL TREES ALONG AN ESTIMATED 190 FEET DURING ITS DESCENT TO WHERE IT IMPACTED TERRAIN. ALL FLIGHT CONTROLS WERE ACCOUNTED FOR AT THE ACCIDENT SITE. FLIGHT CONTROL CONTINUITY WAS CONFIRMED TO RESPECTIVE INPUTS. THE OUTBOARD PORTION OF THE RIGHT WING WAS SEPARATED FROM THE AIRPLANE AND HEAVILY BURNED ABOUT 60 FEET FROM THE MAIN WRECKAGE. THE LEFT WING WAS STILL ATTACHED TO THE FUSELAGE. THE PROPELLER BLADES SIGNS OF BENDING AND GOUGING. A FEW PROPELLER CHOP MARKS WERE VISIBLE ON THE LIMBS. THE EXHAUST PIPE WAS MISSING FROM THE ENGINE AT THE ACCIDENT SITE.

THE EXHAUST PIPE, FRACTURED V-BAND CLAMP AND TWO PIECES OF HEAT INSULATION WRAP WERE RECOVERED FROM THE RUNWAY BY AIRPORT PERSONNEL. THE ITEMS WERE FOUND IN THE FOLLOWING ORDER FROM INITIAL TAKE OFF ROLL: 10 PIECE OF INSULATION WRAP, 2) PIECE OF INSULATION WRAP, 3) V-BAND CLAMP, 4) EXHAUST PIPE.

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 N60RW · 1

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