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Accidents · NTSB FTW85FA230 · Preliminary: the investigation is not finished

Piper PA-28-140 and Bell UH-1V mid-air collision near Junction City, Kansas, May 22, 1985

On May 22, 1985 at about 6:45 pm local time, 2 aircraft, Piper PA-28-140 (N7053R) and Bell UH-1V (USA), were involved in a mid-air collision near Junction City, Kansas. 1 person was killed; 7 others were unhurt. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The NTSB has not yet published a probable cause for this accident. Investigations usually take one to two years; this page updates when the final report is released.

Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.

What the record shows

Date
May 22, 1985 · about 6:45 pm local time · cases in 1985
Place
Junction City, Kansas · map
Type
Accident · mid-air collision
Injuries
1 person was killed; 7 others were unhurt.
Weather
visual conditions (good weather)
Aircraft 1
Piper PA-28-140 · all PA-28-140s on the register
Registration
N7053R · registry record · serial 28-21751
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)
Aircraft 2
Bell UH-1V · all UH-1Vs on the register
Registration
USA · registered outside the United States · serial 71-20105
Damage
Substantial damage
Flight
Flight · military rules

The NTSB's narrative for the Piper PA-28-140 final · quoted from the NTSB record

ARMY UH-1V AND N7053R, A PIPER PA-28, COLLIDED IN MID AIR AT 700 FEET AGL. BOTH ACFT WERE IN LVL FLT. UH-1V WAS OPERATING ON A MEDICAL EVACUATION FLT WITH A CREW OF FOUR, ONE PATIENT AND TWO ATTENDANTS. THE UH-1V EXECUTED A SUCCESSFUL AUTOROTATION WITH SUBSTANTIAL DAMAGE AND NO INJURIES. THE PIPER CRASHED OUT OF CONTROL AFTER ITS RIGHT WING WAS CUT OFF BY THE HELICOPTER'S ROTOR BLADES. THE ARMY PILOTS REPORTED THAT WHEN THE PIPER WAS FIRST SIGHTED IT WAS 45 DEGREES TO THE RIGHT OF THEIR AIRCRAFT'S NOSE. THE HELICOPTER PILOT BEGAN A DIVING LEFT TURN BUT IT WAS TOO LATE. THE CO-PILOT STATED THAT THE PIPER EXECUTED AN EXTREMELY STEEP RIGHT TURN JUST BEFORE IMPACT. THE PILOT OF THE PIPER RECEIVED FATAL INJURIES. BOTH AIRCRAFT HAD THE FORWARD HALF OF THE ROTATING BEACONS COVERED. THE UH-1V WITH TAPE AND THE PIPER WITH BLACK PAINT.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The NTSB's narrative for the Bell UH-1V final · quoted from the NTSB record

ARMY UH-1V AND N7053R, A PIPER PA-28, COLLIDED IN MID AIR AT 700 FEET AGL. BOTH ACFT WERE IN LVL FLT. UH-1V WAS OPERATING ON A MEDICAL EVACUATION FLT WITH A CREW OF FOUR, ONE PATIENT AND TWO ATTENDANTS. THE UH-1V EXECUTED A SUCCESSFUL AUTOROTATION WITH SUBSTANTIAL DAMAGE AND NO INJURIES. THE PIPER CRASHED OUT OF CONTROL AFTER ITS RIGHT WING WAS CUT OFF BY THE HELICOPTER'S ROTOR BLADES. THE ARMY PILOTS REPORTED THAT WHEN THE PIPER WAS FIRST SIGHTED IT WAS 45 DEGREES TO THE RIGHT OF THEIR AIRCRAFT'S NOSE. THE HELICOPTER PILOT BEGAN A DIVING LEFT TURN BUT IT WAS TOO LATE. THE CO-PILOT STATED THAT THE PIPER EXECUTED AN EXTREMELY STEEP RIGHT TURN JUST BEFORE IMPACT. THE PILOT OF THE PIPER RECEIVED FATAL INJURIES. BOTH AIRCRAFT HAD THE FORWARD HALF OF THE ROTATING BEACONS COVERED. THE UH-1V WITH TAPE AND THE PIPER WITH BLACK PAINT.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record for the Piper PA-28-140 from the NTSB's investigation tables, in plain English

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 127 hours in all; 118 in this make and model; 39 in the last 90 days; 13 in the last 30 days; 82 as pilot in command
  • Medical certificate: Class 3 (valid medical--no waivers/lim.)
  • Seat: left

The aircraft

  • Airframe total time: 2,399 hours
  • Last inspection: annual inspection, October 15, 1984; 10 hours since
  • Maximum gross weight: 2,150 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Lycoming O-320-E2A (piston); 0 hours total

The flight

  • Departed from: 7K1 Herington KS
  • Destination: MHK Manhattan KS
  • Flight plan: none
  • Runway 0

Weather at the time

  • Light: daylight
  • Wind: from 100° at 6 knots
  • Visibility: 15 statute miles
  • Sky: scat at 20,000 ft
  • Temperature: 70°F (21°C), dew point 52°F (11°C)
  • Altimeter: 30.00 inHg
  • Observation at 6:55 pm from FRI, 5 miles away

Injuries

FatalSeriousMinorNone
Crew1

The factual record for the Bell UH-1V from the NTSB's investigation tables, in plain English

Pilot

  • Ratings: single-engine land; instructor: helicopter; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 4,560 hours in all; 60 in the last 90 days; 3,500 as pilot in command
  • Medical certificate: Unknown (valid medical--no waivers/lim.)
  • Seat: left

The aircraft

  • Airframe total time: 4,671 hours
  • Last inspection: 100-hour inspection; 27 hours since
  • Maximum gross weight: 9,500 lb
  • Landing gear: fixed
  • Engine: Lycoming T53-L133A (turboshaft); 0 hours total

The flight

  • Departed from: FRI Ft. Riley KS at 6:30 pm
  • Destination: TOP Topeka KS
  • Flight plan: VFR
  • Runway 0
  • A second pilot was aboard

Injuries

FatalSeriousMinorNone
Crew4
Passengers3

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

Connections how this case links to the rest of the register

Aircraft
Place

The whole map of how records connect · these connections as data: /graph/accident/FTW85FA230.json.

The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.