De Havilland Dhc Safety Record

Complete NTSB accident and incident history. 353 events recorded from 1982 to 2025.

353

All Events

198

Incidents

26

Minor

34

Serious

79

Fatal (356 fatalities)

Date Location Reg# Severity Damage Probable Cause
Apr 03, 1995 MOLINE, IL N828MA Incident
the defective weld and the subsequent in flight failure of the welded plug located in the piston of the roll spoiler actuator. The manufacturer's ina…

the defective weld and the subsequent in flight failure of the welded plug located in the piston of the roll spoiler actuator. The manufacturer's inadequate design is a related factor.

Mar 16, 1995 HONOLULU, HI N37ST Incident destroyed
Intentional ditching due to the flightcrew's failure to properly manage the fuel system, and operation of the airplane in an excessively overweight co…

Intentional ditching due to the flightcrew's failure to properly manage the fuel system, and operation of the airplane in an excessively overweight condition.

Sep 17, 1994 WHITTIER, AK N1433Z Incident substantial
THE PILOT'S INADEQUATE IN-FLIGHT PLANNING AND INADEQUATE COMPENSATION FOR THE WIND CONDITIONS. AN INITIAL TAIL WIND AND LATER A CROSSWIND WERE FACTOR…

THE PILOT'S INADEQUATE IN-FLIGHT PLANNING AND INADEQUATE COMPENSATION FOR THE WIND CONDITIONS. AN INITIAL TAIL WIND AND LATER A CROSSWIND WERE FACTORS IN THE ACCIDENT.

Aug 19, 1994 SKWENTA, AK N1785R Incident substantial THE FAILURE OF THE PILOT-IN-COMMAND TO MAINTAIN ADEQUATE CLEARANCE FROM AN OBJECT (TREE).
Jul 16, 1994 KENAI, AK N2297R Incident substantial THE PILOT DID NOT USE THE TAKEOFF CHECKLIST TO CONFIRM THAT THE FLAPS WERE EXTENDED FOR THE TAKEOFF.
Jul 09, 1994 NONDALTON, AK N2297R Incident substantial THE PILOT'S INADEQUATE COMPENSATION FOR THE WIND CONDITION. A FACTOR IN THE ACCIDENT WAS THE GUSTY WIND CONDITION.
Mar 12, 1993 KETCHIKAN, AK N67667 Incident substantial THE PILOT SELECTED UNSUITABLE TERRAIN FOR TAKEOFF. A FACTOR IN THE ACCIDENT WAS THE BUILDING SITUATED AT THE END OF THE TAKEOFF SITE.
Jan 09, 1993 SAVOY, IL N433AW Incident minor THE TOTAL FAILURE OF THE INBOARD RIGHT MAIN LANDING GEAR WHEEL AXLE DURING THE INITIAL CLIMB.
Jan 08, 1993 DETROIT, MI N826MA Incident THE MANUFACTURER'S INADEQUATE DESIGN OF THE FUEL TRANSFER TUBE SYSTEM, WHICH LOOSENED/DISCONNECTED DURING ENGINE OPERATION.
Dec 24, 1992 TWO MOON BAY, AK N737KA Incident substantial
AN INADVERTANT LANDING GEAR EXTENSION AND WHEELS DOWN WATER LANDING BY THE PILOT IN COMMAND. A FACTOR RELATING TO THE ACCIDENT WAS THE LACK OF CHECKL…

AN INADVERTANT LANDING GEAR EXTENSION AND WHEELS DOWN WATER LANDING BY THE PILOT IN COMMAND. A FACTOR RELATING TO THE ACCIDENT WAS THE LACK OF CHECKLIST USE BY THE PILOT.

Oct 08, 1992 ANCHORAGE, AK N680MA Incident
IMPROPER ATC CLEARANCE INSTRUCTIONS BY THE APPROACH CONTROLLER, RESULTING IN A FAILURE TO INSURE SAFE SEPARATION BETWEEN AN AIRPLANE IN VISUAL CONDITI…

IMPROPER ATC CLEARANCE INSTRUCTIONS BY THE APPROACH CONTROLLER, RESULTING IN A FAILURE TO INSURE SAFE SEPARATION BETWEEN AN AIRPLANE IN VISUAL CONDITIONS WITH AN AIRPLANE IN INSTRUMENT METEOROLOGICAL CONDITIONS ON CONVERGING COURSES. A FACTOR WHICH CONTRIBUTED WAS INSUFFICIENT INFORMATION PROVIDED TO BOTH PILOTS BY THE CONTROLLER.

Sep 19, 1992 CHITINA, AK N513F Incident substantial
PILOT IN COMMAND PREFLIGHT DECISION/PLANNING IN ATTEMPTING TAKEOFF WITHOUT PRUDENT AND SUFFICIENT PREPARATION TO ASSESS WIND DIRECTION. A FACTOR RELA…

PILOT IN COMMAND PREFLIGHT DECISION/PLANNING IN ATTEMPTING TAKEOFF WITHOUT PRUDENT AND SUFFICIENT PREPARATION TO ASSESS WIND DIRECTION. A FACTOR RELATING TO THE ACCIDENT WAS: THE TREES IN THE CLEARWAY AT THE AIRSTRIP END.

Jul 22, 1992 MCGRATH, AK N41755 Incident substantial THE FIRE IN THE ENGINE ACCESSORY DRIVE ASSEMBLY. FACTOR WAS THE ROUGH AN UNEVEN FORCED LANDING AREA.
May 24, 1992 ALEXANDER CREEK, AK N4478 Incident substantial
THE PILOT'S INADVERTENT DEACTIVATION OF THE ENGINE'S FUEL SUPPLY BY SWITCHING OFF THE FUEL SHUT OFF. FACTOR RELATED TO THE ACCIDENT WAS THE SOFT MUD …

THE PILOT'S INADVERTENT DEACTIVATION OF THE ENGINE'S FUEL SUPPLY BY SWITCHING OFF THE FUEL SHUT OFF. FACTOR RELATED TO THE ACCIDENT WAS THE SOFT MUD IN THE FORCED LANDING AREA.

Feb 04, 1992 METLAKATLA, AK N13GA Incident substantial TOTAL FAILURE OF THE RIVETS ATTACHING THE TRIM TAB CONTROL HORN TO THE RIGHT ELEVATOR TRIM TAB.
Jan 12, 1992 BALTIMORE, MD N923HA Incident minor
IMPROPER INSTALLATION OF THE LOW FUEL PRESSURE WARNING SWITCH SNUBBER ON THE #1 ENGINE, RESULTING IN FATIGUE FAILURE OF THE SNUBBER, A FUEL LEAK (SPRA…

IMPROPER INSTALLATION OF THE LOW FUEL PRESSURE WARNING SWITCH SNUBBER ON THE #1 ENGINE, RESULTING IN FATIGUE FAILURE OF THE SNUBBER, A FUEL LEAK (SPRAY), AND SUBSEQUENT EXPLOSION/FIRE DAMAGE. A FACTOR RELATED TO THE INCIDENT WAS: INADEQUATE DESIGN OF THE FIREWALL, WHICH ALLOWED FUEL VAPORS TO MIGRATE TO THE HOT SECTION OF THE ENGINE.

Jan 02, 1992 PORT WALTER, AK N64396 Incident substantial THE DESIGN STRESS LIMITS OF THE AIRPLANE WERE EXCEEDED. A FACTOR TO THE ACCIDENT WAS: ROUGH WATER.
Oct 26, 1991 CHEVAK, AK N724CA Incident substantial
THE HIGH CROSSWIND CONDITION, THE PILOT IN COMMANDS INABILITY TO COMPENSATE FOR THE WIND CONDITIONS, AND HIS FAILURE TO FOLLOW COMPANY PROCEDURES AND …

THE HIGH CROSSWIND CONDITION, THE PILOT IN COMMANDS INABILITY TO COMPENSATE FOR THE WIND CONDITIONS, AND HIS FAILURE TO FOLLOW COMPANY PROCEDURES AND THE PROCEDURES RECOMMENDED IN THE AIRCRAFT FLIGHT MANUAL. FACTOR RELATING TO THE ACCIDENT WAS THE CAPTAIN'S OVERCONFIDENCE IN HIS PERSONAL ABILITY.

Aug 31, 1991 CUBE COVE, AK N2738G Incident substantial THE ENCOUNTER WITH WINDSHEAR.
Aug 14, 1991 UGASHIK, AK N5371G Incident substantial
WAS THE PILOT-IN-COMMAND'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL OF THE AIRPLANE DURING THE TAKEOFF RUN. CONTRIBUTING TO THE ACCIDENT WAS THE ROUGH …

WAS THE PILOT-IN-COMMAND'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL OF THE AIRPLANE DURING THE TAKEOFF RUN. CONTRIBUTING TO THE ACCIDENT WAS THE ROUGH WATER.

Jul 17, 1991 SAVANNAH, GA N922HA Incident minor
THE INADEQUATE INSPECTION PROCEDURES WHICH ALLOWED THE LOSS OF TORQUE ON THE TOP RETRACTION FITTING ATTACHMENT BOLT WHICH SUBSEQUENTLY FAILED IN FATIG…

THE INADEQUATE INSPECTION PROCEDURES WHICH ALLOWED THE LOSS OF TORQUE ON THE TOP RETRACTION FITTING ATTACHMENT BOLT WHICH SUBSEQUENTLY FAILED IN FATIGUE. FACTORS WERE THE LOSS OF HYDRAULIC FLUID THROUGH A SEVERED LINE, AND THE CORROSION OF A HYDRAULIC QUANTITY LIMITING VALVE.

Jul 16, 1991 ILIAMNA, AK N6LU Incident minor
THE PILOT-IN-COMMAND'S ATTEMPTED FLIGHT INTO KNOWN ADVERSE WEATHER CONDITIONS. CONTRIBUTING TO THE ACCIDENT WAS THE HIGH AND GUSTY WINDS IN THE ACCID…

THE PILOT-IN-COMMAND'S ATTEMPTED FLIGHT INTO KNOWN ADVERSE WEATHER CONDITIONS. CONTRIBUTING TO THE ACCIDENT WAS THE HIGH AND GUSTY WINDS IN THE ACCIDENT AREA.

Jul 05, 1991 KING SALMON, AK N5538G Incident substantial THE FORCED LANDING ON THE ROUGH TERRAIN AND THE ENGINE POWER LOSS DUE TO THE FAILURE OF THE ENGINE COLLECTOR INTERMEDIATE BEARINGS.
Sep 23, 1990 KING SALMON, AK N5322G Incident substantial THE PILOT-IN-COMMAND'S FAILURE TO MAINTAIN AIRPLANE CONTROL DURING THE TAKEOFF ROLL, AND FAILURE OF NOT ATTAINING AIRSPEED ON TAKEOFF.
Aug 31, 1990 ALAGNAK RIVER, AK N24BR Incident substantial THE PILOT-IN-COMMAND'S INADEQUATE PREFLIGHT PLANNING/PREPARATION, HIS SELECTION OF UNSUITABLE TERRAIN, AND HIS DELAY IN ABORTING THE TAKEOFF.
Disclaimer: This data is sourced from the NTSB Aviation Accident Database. NTSB events reflect reported accidents and incidents and do not necessarily indicate a defect in the aircraft type. Many events involve pilot error, weather conditions, maintenance issues, or other factors unrelated to the aircraft design. This information is provided for research purposes only — consult official NTSB reports for complete details.
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