19980302002419A

Accident · Destroyed

FAA accident report · Cessna T303 · Midvale, ID · March 2, 1998

Date
March 2, 1998 · 18:05 local
Place
Midvale, ID
Phase of flight
Unknown/Not Reported
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N727RT
NTSB investigation
NTSBSEA98FA042
Reported as
Cessna T303
Reported engine
Continental TSIO520AE
People aboard
6
Fatal injuries
6
Pilot’s flight hours
7,743 total319 in this make and model169 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.

(.4)Radar data indicated that the aircraft completed a figure-eight maneuver at about 3,000 feet AGL, with an estimated airspeed of 140 knots and approximate 40 degree bank angle before leveling out at the completion of the maneuver. The radar data then indicated level flight before a rapid descent. A witness reported observing the aircraft in visual conditions and flying at a high altitude and that it 'appeared fast.' The witness stated that he observed the aircraft make a wide, shallow left turn, then turn back the other way. The nose of the aircraft then started to gradually lower, and the airplane eventually came straight down and started to spin. The witness lost sight of the airplane behind hilly terrain and he did not see the impact. Post-accident examination of the wreckage indicated that the aircraft collided with the terrain in a slight nose-down attitude, located in a gully with approximate 30 degree bank angle. The aircraft then slid downhill to the right and came to rest with the fuselage upright and the empennage was twisted to the right and inverted. No evidence was found to indicate a mechanical failure or malfunction.

As the FAA filed it

(.4)RADAR DATA INDICATED THAT THE AIRCRAFT COMPLETED A FIGURE-EIGHT MANEUVER AT ABOUT 3,000 FEET AGL, WITH AN ESTIMATED AIRSPEED OF 140 KNOTS AND APPROXIMATE 40 DEGREE BANK ANGLE BEFORE LEVELING OUT AT THE COMPLETION OF THE MANEUVER. THE RADAR DATA THEN INDICATED LEVEL FLIGHT BEFORE A RAPID DESCENT. A WITNESS REPORTED OBSERVING THE AIRCRAFT IN VISUAL CONDITIONS AND FLYING AT A HIGH ALTITUDE AND THAT IT 'APPEARED FAST.' THE WITNESS STATED THAT HE OBSERVED THE AIRCRAFT MAKE A WIDE, SHALLOW LEFT TURN, THEN TURN BACK THE OTHER WAY. THE NOSE OF THE AIRCRAFT THEN STARTED TO GRADUALLY LOWER, AND THE AIRPLANE EVENTUALLY CAME STRAIGHT DOWN AND STARTED TO SPIN. THE WITNESS LOST SIGHT OF THE AIRPLANE BEHIND HILLY TERRAIN AND HE DID NOT SEE THE IMPACT. POST-ACCIDENT EXAMINATION OF THE WRECKAGE INDICATED THAT THE AIRCRAFT COLLIDED WITH THE TERRAIN IN A SLIGHT NOSE-DOWN ATTITUDE, LOCATED IN A GULLY WITH APPROXIMATE 30 DEGREE BANK ANGLE. THE AIRCRAFT THEN SLID DOWNHILL TO THE RIGHT AND CAME TO REST WITH THE FUSELAGE UPRIGHT AND THE EMPENNAGE WAS TWISTED TO THE RIGHT AND INVERTED. NO EVIDENCE WAS FOUND TO INDICATE A MECHANICAL FAILURE OR MALFUNCTION.

NTSB investigation

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