Nanchang CJ6 - A accident near Flushing, Michigan, April 19, 2014
On April 19, 2014 at about 6:10 pm local time, a 1983 Nanchang CJ6 - A, registered N594T, was substantially damaged in an accident during emergency descent near Flushing, Michigan. It was a personal 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 pilot’s failure to maintain adequate airspeed during an off-airport forced landing after a loss of engine power due to carburetor icing and his exceedance of the airplane’s critical angle-of-attack, which resulted in an aerodynamic stall. Contributing to the accident was the pilot’s delayed application of carburetor heat while operating in conditions conducive to carburetor icing. Contributing to the severity of both occupants’ injuries was the lack of adequate restraint.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- April 19, 2014 · about 6:10 pm local time
- Place
- Flushing, Michigan · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Nanchang CJ6 - A, built 1983 · all CJ6 - As on the register
- Registration
- N594T · no longer on the register · serial 4032008
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The private pilot was conducting a personal cross-country flight with a pilot-rated passenger on board. A witness reported hearing the engine "sputter" and seeing the propeller slow as the airplane began descending toward an open field with the landing gear extended. Another witness, who was watching the airplane fly eastbound at low altitude, reported that it suddenly pitched down and impacted terrain in an approximate 45-degree, nose-down attitude, indicative of a stall. Based on the evidence, it is likely that the pilot was conducting a forced landing to the field due to a loss of engine power and subsequently failed to maintain adequate airspeed and exceeded the airplane's angle-of-attack, which resulted in the aerodynamic stall. An examination of the dry, flat field showed that it was an adequate emergency forced landing area. A postaccident examination of the airframe, engine, and propeller revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. Weather conditions at the time of the accident were conducive to carburetor icing at glide and cruise power. Although the carburetor heat control was found in the "on" position, it is possible that the pilot delayed the application of carburetor heat, which likely resulted in the formation of carburetor ice and the loss of engine power. An examination of damage to the airplane's structure showed that both the front seat and rear seat cockpit areas remained substantially intact and had provided a protective shell around both occupants during the crash sequence. Both pilot seats were equipped with a five-point lap belt and shoulder harness system. Evidence at the scene showed that the front seat pilot had been ejected from his seat during the crash sequence and had impacted the front cockpit instrument panel; however, he remained inside the cabin area. Examination of the front seat's lap belt and shoulder harness system latch, which was found unfastened, did not allow for a determination of whether the latch was unfastened, was fastened and failed, or whether it separated at the time of impact. The passenger in the rear seat remained restrained by his lap belt during the crash sequence; however, he impacted the rear cockpit instrument panel due to the failure and complete separation of his shoulder harness fitting. It is likely that the lack of adequate restraint for both occupants contributed to the severity of their injuries.
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
- Loss of engine power (total) during maneuvering
- Off-field or emergency landing during emergency descent
- Aerodynamic stall/spin during emergency descent defining event
- Collision with terrain or object (not controlled flight into terrain) during emergency descent
The NTSB's findings
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Capability exceeded
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › Conducive to carburetor icing › Effect on equipment
- factor Personnel issues › Action/decision › Action › Delayed action › Pilot
- factor Aircraft › Aircraft systems › Ice/rain protection system › Intake anti › ice, deice › Incorrect use/operation
- Aircraft › Aircraft structures › Fuselage › Seat/cargo attach fitting › Failure
- Aircraft › Aircraft structures › Fuselage › Seat/cargo attach fitting › Incorrect use/operation
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 1,525 hours in all; 145 in this make and model; 13 in the last 90 days
- Last flight review: July 20, 2013
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: frt
- Injury: fatal
Pilot-Rated Passenger
- Certificate: private
- Ratings: single-engine land; rotorcraft: helicopter
- Flight time: 300 hours in all; 0 in this make and model
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: rear
- Injury: fatal
The aircraft
- Airframe total time: 2,737 hours
- Last inspection: condition inspection, February 13, 2014
- Maximum gross weight: 3,087 lb
- Seats: 2
- Landing gear: retractable
- Engine: Huosai HS-6A (piston); 0 hours total
The flight
- Departed from: CFS Caro MI at 5:50 pm
- Destination: 65G Fowlerville MI
- Flight plan: none
- A second pilot was aboard
Weather at the time
- Light: daylight
- Wind: from 080° at 10 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 54°F (12°C), dew point 30°F (-1°C)
- Altimeter: 30.43 inHg
- Observation at 5:53 pm from KFNT, 10 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 |
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.
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 never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
