Wichita - Wichita

The crew was performing a lateral and directional stability test. Changes from earlier tests combined new leading edge fairing, new flap setting, lower reference airspeed, and trial settings for the stall protection system (shaker and pusher). Engineers had briefed the crew data would be sufficient if the steady heading sideslip (shss) maneuver ended at a 15° sideslip, or at onset of stall warning; crew agreed to end at stall warning. During the test the capt continued past stall warning to 21° sideslip at full rudder. The airplane rolled rapidly through 360 deg° and entered a deep stall. The copilot attempted to deploy the anti-spin chute. However, all the chute system cockpit switches were not properly preset; instead of assisting recovery, the chute parted from the airplane. Full control was not regained before impact. The chute system design allowed deployment of the chute even when the hyd lock switch was in the unlocked position and the hooks clasping the chute shackle to the airframe were open. System tested ok before flight. All three crew members were killed.

Flight / Schedule

Wichita - Wichita

Registration

C-FCRJ

MSN

7001

Year of Manufacture

1991

Date

July 26, 1993 at 01:52 PM

Type

CRASH

Flight Type

Test

Flight Phase

Flight

Crash Site

Plain, Valley

Crash Location

Byers Kansas

Region

North America • United States of America

Coordinates

37.7875°, -98.8670°

Crash Cause

Human factor

Narrative Report

On July 26, 1993 at 01:52 PM, Wichita - Wichita experienced a crash involving Canadair RegionalJet CRJ-100, operated by Bombardier Aerospace, with the event recorded near Byers Kansas.

The flight was categorized as test and the reported phase was flight at a plain, valley crash site.

3 people were known to be on board, 3 fatalities were recorded, 0 survivors were identified or estimated. This corresponds to an estimated fatality rate of 100.0%.

Crew on board: 3, crew fatalities: 3, passengers on board: 0, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is human factor. The crew was performing a lateral and directional stability test. Changes from earlier tests combined new leading edge fairing, new flap setting, lower reference airspeed, and trial settings for the stall protection system (shaker and pusher). Engineers had briefed the crew data would be sufficient if the steady heading sideslip (shss) maneuver ended at a 15° sideslip, or at onset of stall warning; crew agreed to end at stall warning. During the test the capt continued past stall warning to 21° sideslip at full rudder. The airplane rolled rapidly through 360 deg° and entered a deep stall. The copilot attempted to deploy the anti-spin chute. However, all the chute system cockpit switches were not properly preset; instead of assisting recovery, the chute parted from the airplane. Full control was not regained before impact. The chute system design allowed deployment of the chute even when the hyd lock switch was in the unlocked position and the hooks clasping the chute shackle to the airframe were open. System tested ok before flight. All three crew members were killed.

Aircraft reference details include registration C-FCRJ, MSN 7001, year of manufacture 1991.

Geospatial coordinates for this crash are approximately 37.7875°, -98.8670°.

Fatalities

Total

3

Crew

3

Passengers

0

Other

0

Crash Summary

The crew was performing a lateral and directional stability test. Changes from earlier tests combined new leading edge fairing, new flap setting, lower reference airspeed, and trial settings for the stall protection system (shaker and pusher). Engineers had briefed the crew data would be sufficient if the steady heading sideslip (shss) maneuver ended at a 15° sideslip, or at onset of stall warning; crew agreed to end at stall warning. During the test the capt continued past stall warning to 21° sideslip at full rudder. The airplane rolled rapidly through 360 deg° and entered a deep stall. The copilot attempted to deploy the anti-spin chute. However, all the chute system cockpit switches were not properly preset; instead of assisting recovery, the chute parted from the airplane. Full control was not regained before impact. The chute system design allowed deployment of the chute even when the hyd lock switch was in the unlocked position and the hooks clasping the chute shackle to the airframe were open. System tested ok before flight. All three crew members were killed.

Cause: Human factor

Occupants & Outcome

Crew On Board

3

Passengers On Board

0

Estimated Survivors

0

Fatality Rate

100.0%

Known people on board: 3

Operational Details

Schedule / Flight

Wichita - Wichita

Flight Type

Test

Flight Phase

Flight

Crash Site

Plain, Valley

Region / Country

North America • United States of America

Aircraft Details

Registration

C-FCRJ

MSN

7001

Year of Manufacture

1991