20260403010559A

Accident · Substantial damage

FAA accident report · Textron T206H · Wichita, KS · April 3, 2026

Date
April 3, 2026 · 15:16 local
Place
Wichita, KS
Airport
Wichita Dwight D Eisenhower Nt
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N411CV
NTSB investigation
NTSBCEN26LA163
Reported as
Textron T206H
Reported engine
Lycoming TIO-540-AJ1A
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
2,714 total

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.

During a part 91 instructional proficiency flight at kict, the aircraft completed a planned no-flap landing and subsequent touch-and-go. During climb out on the upwind leg at approximately 700–800' AGL, the aft cargo door unlatched and blew open in flight. The door structurally impacted the airframe, causing substantial cosmetic/structural cracking to the RH aft window and the surrounding fuselage bulkhead attach points. The open door safety switch successfully triggered an inoperative flap configuration. Post-flight inspection revealed both cockpit door handles/latches were still physically selected to the engaged/closed position.

As the FAA filed it

DURING A PART 91 INSTRUCTIONAL PROFICIENCY FLIGHT AT KICT, THE AIRCRAFT COMPLETED A PLANNED NO-FLAP LANDING AND SUBSEQUENT TOUCH-AND-GO. DURING CLIMB OUT ON THE UPWIND LEG AT APPROXIMATELY 700–800' AGL, THE AFT CARGO DOOR UNLATCHED AND BLEW OPEN IN FLIGHT. THE DOOR STRUCTURALLY IMPACTED THE AIRFRAME, CAUSING SUBSTANTIAL COSMETIC/STRUCTURAL CRACKING TO THE RH AFT WINDOW AND THE SURROUNDING FUSELAGE BULKHEAD ATTACH POINTS. THE OPEN DOOR SAFETY SWITCH SUCCESSFULLY TRIGGERED AN INOPERATIVE FLAP CONFIGURATION. POST-FLIGHT INSPECTION REVEALED BOTH COCKPIT DOOR HANDLES/LATCHES WERE STILL PHYSICALLY SELECTED TO THE ENGAGED/CLOSED POSITION.

NTSB investigation

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