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Accidents · NTSB ERA16FA194 · Final report

Jihlavan Airplanes Sro KP 5 ASA accident near Rhoadesville, Virginia, May 24, 2016

On May 24, 2016 at about 8:25 pm local time, a 2007 Jihlavan Airplanes Sro KP 5 ASA, registered N440JM, was destroyed in an accident during uncontrolled descent near Rhoadesville, Virginia. It was an instructional flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilots' loss of control that necessitated the activation of the parachute system and the airplane manufacturer's inadequate design of the front parachute anchor attachment structure, which resulted in a failure of the parachute after it was deployed in flight and precluded the pilots from safely recovering from the spin.

Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.

What the record shows

Date
May 24, 2016 · about 8:25 pm local time
Place
Rhoadesville, Virginia · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Jihlavan Airplanes Sro KP 5 ASA NO SERIES, built 2007 · all KP 5 ASAs on the register
Registration
N440JM · no longer on the register · serial 5141163M
Damage
Destroyed
Flight
Instructional flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The sport pilot had recently purchased the airframe-parachute-equipped light sport airplane and was receiving instruction in it to satisfy insurance requirements. Radar data indicated that, during the flight, the airplane's groundspeed decreased from 94 to 62 knots, consistent with airwork including slow flight and stall practice. Subsequently, several witnesses observed the airplane descending nose-down with the parachute still attached, but with the canopy only partially inflated, before the airplane impacted terrain. The parachute handle was located on the left side of the instrument panel, and the sport pilot likely activated the parachute due to inadvertent spin entry. The previous owner of the airplane stated that he had to be vigilant during stall practice because the airplane always seemed to yaw abruptly right and into a spin, more so than any other airplane he had flown. The parachute attached to the airframe via four risers. Two of the risers shared a front anchor attached to the aluminum bulkhead behind the seats. The other two risers attached to a rear anchor located at each wing root. Examination of the wreckage revealed that the two front risers remained attached to the shared front anchor but that the anchor had separated from the airframe. The two rear risers had separated in overstress. The front anchor was designed to carry the majority load. The remaining two rear risers were designed to stabilize the airplane in an optimal descent attitude and could not carry the full load if the front anchor failed. Metallurgical examination of the separated front anchor revealed that it had been bolted into aluminum bulkhead skin that was about 0.022-inch thick. Although the anchor and seven of its eight bolts remained intact, the surrounding aluminum skin of the airplane had separated from the airplane in overstress. Without any additional supporting structure such as longerons, stringers, or bathtub fittings, it is likely the thin aluminum skin could not withstand the force applied to the front anchor during parachute deployment. The investigation noted that the first in-flight deployment of the parachute on the make and model airplane was on the accident airplane during the accident flight. During certification, one test deployment was performed on the ground. Further, the airplane manufacturer was unable to provide any data or testing of the amount of shock force the surrounding aluminum skin could withstand during deployment. The airplane's maximum takeoff weight was 1,279 lbs. According to the parachute manufacturer, the parachute could be deployed at a maximum weight of 1,350 lbs and a maximum speed of 138 mph. A representative of the parachute manufacturer stated that, although the engine should be off during parachute deployment, it did not have as significant an effect on deployment as airplane speed and weight. Although the airplane was about 50 lbs over its maximum takeoff weight at the time of deployment, it was under the parachute manufacturer maximum weight of 1,350 lbs. Additionally, the pilot likely activated the parachute in the early stages of a spin and closer to stall speed, significantly slower than the 138-mph parachute limit. The sport pilot had chronic pain treated with multiple medications, including Methadone, an impairing opioid medication, which was detected in blood at levels consistent with chronic use. Further, the sport pilot had insomnia and depression treated with quetiapine and doxepin, both of which are sedating medications. The pilot's recent use of the combination of two potentially impairing medications likely impaired his cognitive and psychomotor function to some degree. However, the investigation could not determine if the pilot's impairment led to a situation that required activation of the parachute. Additionally, there was no evidence that the decision to activate the parachute was inappropriate. Therefore, it is likely that the pilot was impaired by the combination of medications, but there is no evidence that his impairment contributed to the cause of the accident.

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 from the NTSB's investigation tables, in plain English

What happened, in order

  1. Aerodynamic stall/spin during maneuvering
  2. Sys/Comp malf/fail (non-power) during uncontrolled descent defining event
  3. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • cause Aircraft › Aircraft systems › Equipment/furnishings › Parachute › Failure
  • cause Aircraft › Aircraft systems › Equipment/furnishings › Parachute › Design
  • cause Organizational issues › Development › Design › Equipment design › Manufacturer
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Instructor/check pilot
  • Personnel issues › Physical › Impairment/incapacitation › Prescription medication › Pilot

Pilot

  • Certificate: sport pilot
  • Ratings: single-engine land; rotorcraft: powered-lift
  • Flight time: 120.6 hours in all; 2.5 in this make and model; 4.5 in the last 90 days; 0 in the last 30 days; 84.5 as pilot in command
  • Last flight review: January 20, 2016
  • Medical certificate: Sport Pilot
  • Seat: left
  • Injury: fatal

Flight instructor

  • Certificate: airline transport pilot, flight instructor
  • Ratings: multi-engine land; single-engine land; single-engine sea
  • Flight time: 32,840 hours in all; 0 in this make and model; 99 in the last 90 days; 43 in the last 30 days
  • Medical certificate: Class 2
  • Seat: rgt
  • Injury: fatal

The aircraft

  • Airframe total time: 534 hours
  • Last inspection: condition inspection, May 6, 2016
  • Maximum gross weight: 1,278 lb
  • Seats: 2
  • Landing gear: retractable
  • Engine: Rotax 914 UL (piston); 534 hours total

The flight

  • Departed from: CJR Culpeper VA at 7:30 pm
  • Destination: CJR Culpeper VA
  • Flight plan: none
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Visibility: 10 statute miles
  • Sky: scat at 11,000 ft
  • Temperature: 82°F (28°C), dew point 50°F (10°C)
  • Altimeter: 30.03 inHg
  • Observation at 8:35 pm from OMH, 9 miles away

Injuries

FatalSeriousMinorNone
Flight crew2

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.

About this page

Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The documents and photographs are the NTSB's docket, the folder of records gathered during the investigation, shown as the NTSB released them (the NTSB redacts some personal details first) and listed under the NTSB's own titles. This site's own text never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number ERA16FA194.