Hughes 269 Safety Record
Complete NTSB accident and incident history. 390 events recorded from 1982 to 2026.
| Date | Location | Reg# | Severity | Damage | Probable Cause |
|---|---|---|---|---|---|
| Jul 15, 1999 | JUNEAU, AK | N8926F | Minor | substantial | The pilot's failure to maintain rotor rpm, and an inadequately planned approach. A factor associated with the accident was a tailwind. |
| Jun 01, 1999 | PARKMAN, WY | N7052L | Minor | substantial |
The pilot's inadequate in-flight planning by exceeding the helicopter's performance climb capability. Factors were the downdraft encountered during i…The pilot's inadequate in-flight planning by exceeding the helicopter's performance climb capability. Factors were the downdraft encountered during initial climb following takeoff, and the high density altitude. |
| Dec 16, 1998 | HANCEVILLE, AL | N271JB | Minor | substantial | The loss of engine power for undetermined reasons. Factors were a dark night and terrain condition. |
| Aug 17, 1998 | HOUSTON, TX | N1103R | Minor | substantial |
The pilot's failure to refuel the helicopter which resulted in the loss of engine power due to fuel exhaustion. A factor was the lack of suitable ter…The pilot's failure to refuel the helicopter which resulted in the loss of engine power due to fuel exhaustion. A factor was the lack of suitable terrain for the forced landing. |
| Jan 22, 1998 | BRACKETTVILLE, TX | N1093N | Minor | substantial |
failure of splines on the drive shaft coupling after separation of the forward bubber boot and loss of lubrication (grease), which resulted in a disco…failure of splines on the drive shaft coupling after separation of the forward bubber boot and loss of lubrication (grease), which resulted in a disconnect of the rotor drive system and an autorotation/forced landing. Lack of suitable terrain in the forced landing area was a related factor. |
| Jul 20, 1997 | YAMHILL, OR | N1105B | Minor | substantial | Loss of engine power for undetermined reasons. |
| Jul 14, 1997 | PADUCAH, KY | N9398F | Minor | substantial |
The failure of maintenance personnel to identify and correct the worn holes on the lower fuselage fairing and the failure of the flight instructor to…The failure of maintenance personnel to identify and correct the worn holes on the lower fuselage fairing and the failure of the flight instructor to maintain main rotor RPM during the autorotative landing. A contributing factor was the flight instructor's lack of recent experience in performing autorotations to a landing. |
| Sep 24, 1996 | HOUSTON, TX | N7492F | Minor | substantial |
company maintenance personnel not complying with maintenance procedures and directives to inspect the helicopter's skids, which allowed the right skid…company maintenance personnel not complying with maintenance procedures and directives to inspect the helicopter's skids, which allowed the right skid to wear beyond the manufacturer's tolerances. |
| Aug 19, 1996 | CEDAR RAPIDS, IA | N7052A | Minor | substantial | partial blocking of the fuel injection control, and a fracture of the induction air ducting for reasons undetermined. A factor was trees. |
| Jul 27, 1995 | REDLANDS, CA | N747MK | Minor | substantial | The company's maintenance personnel improper servicing of the landing skid actuators. |
| Jun 04, 1995 | CALDWELL, ID | N9474F | Minor | destroyed | THE PILOT'S FAILURE TO MAINTAIN CLEARANCE FROM POWER LINES. FACTORS INCLUDE SUNGLARE ENCOUNTERED WHEN HE TURNED INTO THE SUN. |
| Mar 16, 1995 | VAN NUYS, CA | N8873F | Minor | destroyed |
the operation of the helicopter with improper adjustment of the landing gear and main rotor dampers due to the inadequate maintenance inspection of th…the operation of the helicopter with improper adjustment of the landing gear and main rotor dampers due to the inadequate maintenance inspection of the helicopter by maintenance personnel and an inadequate preflight inspection by the pilot. |
| Jun 20, 1994 | LONDON, TX | N7404F | Minor | destroyed |
THE PARTIAL POWER LOSS DUE TO A STICKING VALVE. FACTORS WERE THE REMAINING WORN LOBES ON THE CAMSHAFT AND THE LACK OF SUITABLE TERRAIN ONTO WHICH A SU…THE PARTIAL POWER LOSS DUE TO A STICKING VALVE. FACTORS WERE THE REMAINING WORN LOBES ON THE CAMSHAFT AND THE LACK OF SUITABLE TERRAIN ONTO WHICH A SUCCESSFUL FORCED LANDING COULD BE EXECUTED. |
| May 25, 1994 | TOULON, IL | N9375S | Minor | destroyed |
the improper reassembly of the main rotor blade dampers and the underservicing of the landing gear skid hydraulic struts which resulted in ground reso…the improper reassembly of the main rotor blade dampers and the underservicing of the landing gear skid hydraulic struts which resulted in ground resonance of the helicopter when the first takeoff after reassembly was attempted. |
| Mar 02, 1994 | MERCED, CA | N9593F | Minor | substantial | the pilot's misjudgement of the descent rate and his delayed throttle application. |
| Sep 01, 1991 | GALLOWAY, OH | N9590F | Minor | substantial |
IMPROPER SUPERVISION BY THE FLIGHT INSTRUCTOR WHICH RESULTED IN AN INADVERTENT GROUND CONTACT AND A DYNAMIC ROLLOVER. A FACTOR RELATED TO THE ACCIDENT…IMPROPER SUPERVISION BY THE FLIGHT INSTRUCTOR WHICH RESULTED IN AN INADVERTENT GROUND CONTACT AND A DYNAMIC ROLLOVER. A FACTOR RELATED TO THE ACCIDENT WAS IMPROPER USE OF THE FLIGHT CONTROLS BY THE NON-RATED STUDENT PILOT. |
| Jun 19, 1991 | WARRENTON, OR | N9380F | Minor | substantial | THE PILOT FAILED TO MAINTAIN PROPER ROTOR SPEED DURING A SIMULATED AUTOROTATION. |
| Jun 13, 1991 | CANBY, OR | N8944F | Minor | substantial | A HARD LANDING AFTER AN UNDETERMINED LOSS OF POWER. FACTORS INCLUDE AN EXCESSIVE EMERGENCY DESCENT RATE. |
| May 26, 1991 | PALM SPRINGS, CA | N7033H | Minor | destroyed |
LACK OF TOTAL EXPERIENCE BY THE UNQUALIFIED PERSON AT THE CONTROLS; IMPROPER USE OF ROTORCRAFT FLIGHT CONTROLS BY AN UNQUALIFIED PERSON. A FACTOR IN T…LACK OF TOTAL EXPERIENCE BY THE UNQUALIFIED PERSON AT THE CONTROLS; IMPROPER USE OF ROTORCRAFT FLIGHT CONTROLS BY AN UNQUALIFIED PERSON. A FACTOR IN THE ACCIDENT WAS THE FENCE. |
| Jun 29, 1990 | CARLSBAD, CA | N1102H | Minor | substantial | FAILURE OF THE PILOT TO MAINTAIN DIRECTIONAL CONTROL AT A HOVER. |
| Jun 21, 1990 | PITTSTOWN, NJ | N110ES | Minor | destroyed | GROUND RESONANCE DUE TO INADEQUATE SERVICING AND MAINTENANCE OF THE LANDING GEAR DAMPERS. |
| May 23, 1990 | LA VERNE, CA | N8793F | Minor | substantial | GROUND RESONANCE DUE TO AN INADEQUATELY MAINTAINED STRUT. |
| May 09, 1990 | FORT PIERCE, FL | N58275 | Minor | destroyed |
IMPROPER TOUCHDOWN DURING THE AUTOROTATION BY THE DUAL STUDENT (ATP), HIS FAILURE TO MAINTAIN RUNWAY ALIGNMENT, INADEQUATE SUPERVISION BY THE CFI, AND…IMPROPER TOUCHDOWN DURING THE AUTOROTATION BY THE DUAL STUDENT (ATP), HIS FAILURE TO MAINTAIN RUNWAY ALIGNMENT, INADEQUATE SUPERVISION BY THE CFI, AND INADEQUATE CREW COORDINATION. A FACTOR RELATED TO THE ACCIDENT WAS THE OBSTRUCTION (TAXIWAY LIGHT). |
| Sep 21, 1989 | LEXINGTON, MS | N9318F | Minor | substantial | FATIGUE FAILURE OF THE LINEAR ACTUATOR LUG. A RELATED FACTOR WAS: TREES IN THE EMERGENCY LANDING AREA. |
| Aug 25, 1989 | JACKSONVILLE, FL | N9014N | Minor | substantial |
INADEQUATE VISUAL LOOK-OUT BY THE PILOT AND HIS FAILURE TO MAINTAIN CONTROL OF THE HELICOPTER, WHILE MANEUVERING TO AVOID OBSTRUCTIONS. THE TRANSMISS…INADEQUATE VISUAL LOOK-OUT BY THE PILOT AND HIS FAILURE TO MAINTAIN CONTROL OF THE HELICOPTER, WHILE MANEUVERING TO AVOID OBSTRUCTIONS. THE TRANSMISSION LINES WERE CONSIDERED TO BE FACTORS. |