20180919013339A

Accident · Destroyed

FAA accident report · Calvin Nate H CALVIN-VELOCITY · Blountville, TN · September 19, 2018

Date
September 19, 2018 · 20:05 local
Place
Blountville, TN
Airport
Tri Cities Regional Airport
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N67WR
NTSB investigation
NTSBERA18TA255
Reported as
Calvin Nate H CALVIN-VELOCITY
Reported engine
Franklin 6A-350SER
People aboard
2
Fatal injuries
0
Other injuries
2
Pilot’s certificate
Private pilot
Pilot’s flight hours
433 total61 in this make and model32 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.

N67WR departed columbus airport (kcsg) enroute to tri Cities airport (ktri). No issues were reported by the pilot in command (PIC) during transit to ktri. N67WR arrived in ktri airspace at approximately 2005 local. The PIC stated that upon arrival that it was nearly night fall with little ambient light. Once in ktri airspace the PIC made contact with approach control. Approach control transferred him ktri tower. The PIC stated that he entered the traffic pattern on the downwind leg and was approximately 4000 feet AGL. He also stated that on the downwind leg the aircraft was on an angle that was parallel to the runway or slightly closing on the runway. Ktri tower cleared him to land using visual flight rules. The PIC reported that he had the runway in sight. The PIC felt as if his approach was fast so he partially deployed the aircaft air brake to slow his approach and to lower his altitude. He also raised the nose of the aircraft to help with the slowing of the aircraft but continued his decent. During his decent the PIC noticed that his altitude was too low and input more throttle to gain airspeed and altitude. The PIC states that the engine did not respond. The aircraft struck the approach approximately 700 feet short of runway 23. After the initial impact the aircraft struck two additional sets of approach lights before impacting the ground approximately 450 feet short of the runway. The first three sets of approach lights were knocked to the ground. The aircraft slid between two more sets of approach lights, striking both sets, and came to rest approximately 200 feet short of the runway. The aircraft was pointing approximately 180 degrees from the original direction of travel. The PIC and passenger suffered serious injuries but were able to climb from the aircraft. Upon inspection of the aircraft, orange paint could be seen on the left side of the aircraft nose, the left wing leading edge and trailing edge. All three areas suffered substantial damage. Orange paint was also observed on the left main landing gear assembly and the nose landing gear wheel. Both were detached from the aircraft. The orange paint matches the orange paint of the airport approach light assemblies. All flight control surfaces were found either still attached to the aircraft on in the debris field. However, flight control continuity was not able to be tested due to the extent of damage. Upon examination of the ground impact area, ground scars of the propeller were noted to indicate the propeller was turning. Photographs of the scene and aircraft were taken.

As the FAA filed it

N67WR DEPARTED COLUMBUS AIRPORT (KCSG) ENROUTE TO TRI CITIES AIRPORT (KTRI). NO ISSUES WERE REPORTED BY THE PILOT IN COMMAND (PIC) DURING TRANSIT TO KTRI. N67WR ARRIVED IN KTRI AIRSPACE AT APPROXIMATELY 2005 LOCAL. THE PIC STATED THAT UPON ARRIVAL THAT IT WAS NEARLY NIGHT FALL WITH LITTLE AMBIENT LIGHT. ONCE IN KTRI AIRSPACE THE PIC MADE CONTACT WITH APPROACH CONTROL. APPROACH CONTROL TRANSFERRED HIM KTRI TOWER. THE PIC STATED THAT HE ENTERED THE TRAFFIC PATTERN ON THE DOWNWIND LEG AND WAS APPROXIMATELY 4000 FEET AGL. HE ALSO STATED THAT ON THE DOWNWIND LEG THE AIRCRAFT WAS ON AN ANGLE THAT WAS PARALLEL TO THE RUNWAY OR SLIGHTLY CLOSING ON THE RUNWAY. KTRI TOWER CLEARED HIM TO LAND USING VISUAL FLIGHT RULES. THE PIC REPORTED THAT HE HAD THE RUNWAY IN SIGHT. THE PIC FELT AS IF HIS APPROACH WAS FAST SO HE PARTIALLY DEPLOYED THE AIRCAFT AIR BRAKE TO SLOW HIS APPROACH AND TO LOWER HIS ALTITUDE. HE ALSO RAISED THE NOSE OF THE AIRCRAFT TO HELP WITH THE SLOWING OF THE AIRCRAFT BUT CONTINUED HIS DECENT. DURING HIS DECENT THE PIC NOTICED THAT HIS ALTITUDE WAS TOO LOW AND INPUT MORE THROTTLE TO GAIN AIRSPEED AND ALTITUDE. THE PIC STATES THAT THE ENGINE DID NOT RESPOND. THE AIRCRAFT STRUCK THE APPROACH APPROXIMATELY 700 FEET SHORT OF RUNWAY 23. AFTER THE INITIAL IMPACT THE AIRCRAFT STRUCK TWO ADDITIONAL SETS OF APPROACH LIGHTS BEFORE IMPACTING THE GROUND APPROXIMATELY 450 FEET SHORT OF THE RUNWAY. THE FIRST THREE SETS OF APPROACH LIGHTS WERE KNOCKED TO THE GROUND. THE AIRCRAFT SLID BETWEEN TWO MORE SETS OF APPROACH LIGHTS, STRIKING BOTH SETS, AND CAME TO REST APPROXIMATELY 200 FEET SHORT OF THE RUNWAY. THE AIRCRAFT WAS POINTING APPROXIMATELY 180 DEGREES FROM THE ORIGINAL DIRECTION OF TRAVEL. THE PIC AND PASSENGER SUFFERED SERIOUS INJURIES BUT WERE ABLE TO CLIMB FROM THE AIRCRAFT. UPON INSPECTION OF THE AIRCRAFT, ORANGE PAINT COULD BE SEEN ON THE LEFT SIDE OF THE AIRCRAFT NOSE, THE LEFT WING LEADING EDGE AND TRAILING EDGE. ALL THREE AREAS SUFFERED SUBSTANTIAL DAMAGE. ORANGE PAINT WAS ALSO OBSERVED ON THE LEFT MAIN LANDING GEAR ASSEMBLY AND THE NOSE LANDING GEAR WHEEL. BOTH WERE DETACHED FROM THE AIRCRAFT. THE ORANGE PAINT MATCHES THE ORANGE PAINT OF THE AIRPORT APPROACH LIGHT ASSEMBLIES. ALL FLIGHT CONTROL SURFACES WERE FOUND EITHER STILL ATTACHED TO THE AIRCRAFT ON IN THE DEBRIS FIELD. HOWEVER, FLIGHT CONTROL CONTINUITY WAS NOT ABLE TO BE TESTED DUE TO THE EXTENT OF DAMAGE. UPON EXAMINATION OF THE GROUND IMPACT AREA, GROUND SCARS OF THE PROPELLER WERE NOTED TO INDICATE THE PROPELLER WAS TURNING. PHOTOGRAPHS OF THE SCENE AND AIRCRAFT WERE TAKEN.

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 N67WR · 1

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