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 09, 2001 | Clay, NY | N7028V | Minor | substantial |
Failure of the left aft cluster fitting due to a fatigue crack. Factors in the accident were the mechanic's failure to identify the crack at the last…Failure of the left aft cluster fitting due to a fatigue crack. Factors in the accident were the mechanic's failure to identify the crack at the last annual inspection, and the pilot's failure to identify the crack during the last daily inspection |
| Jun 25, 2001 | Paso Robles, CA | N8724F | Serious (1) | substantial | the pilot's failure to maintain rotor rpm during a practice autorotational landing, which resulted in a hard landing. |
| May 28, 2001 | Fairfield, KY | N9660F | Minor | substantial | The pilot's inadequate visual lookout during takeoff, and his inadequate reconnoiter of the area prior to takeoff. |
| Apr 27, 2001 | Nacogdoches, TX | N9508F | Minor | substantial | the pilot's failure to maintain clearance with the wires during takeoff. Contributory factors were the sunglare and the unmarked wires. |
| Dec 04, 2000 | CARLSBAD, CA | N1097N | Incident | substantial |
The CFI's inadequate supervision and failure to maintain control of the helicopter during a practice autorotation. A contributing factor was the stud…The CFI's inadequate supervision and failure to maintain control of the helicopter during a practice autorotation. A contributing factor was the student's improper in-flight planning/decision. |
| Sep 27, 2000 | LAUREL, MT | N9503F | Incident | substantial | Failure to maintain aircraft control during hover operations. Inadequate remedial action by the pilot was a factor. |
| Sep 24, 2000 | BURLINGTON, WA | N9355F | Minor | substantial |
Mintenance personnel not following the mandatory service bulletin procedure of not exceeding 0.0005 inch paint thickness on the cylinder flange. Fact…Mintenance personnel not following the mandatory service bulletin procedure of not exceeding 0.0005 inch paint thickness on the cylinder flange. Factors were the fatigue separation of multiple cylinder hold down bolts resulting in looseness of the cylinder; and the subsequent vibration and fatigue separation of the fuel injector line. An additional factor was the pilot's operation of the rotorcraft outside the height/velocity parameters for a successful autorotation. |
| Sep 07, 2000 | RANCHO MURIETA, CA | N50638 | Fatal (1) | destroyed | The pilot's inadequate visual lookout during cruise, which subsequently led to a wire strike. |
| Jun 16, 2000 | MANSFIELD, NJ | N9014N | Minor | substantial |
The pilot's failure to comply with published emergency procedures. A factor in the accident was the pilot's inadequate preflight planning which resul…The pilot's failure to comply with published emergency procedures. A factor in the accident was the pilot's inadequate preflight planning which resulted in a take-off with the inadequate amount of fuel for the flight. |
| Jun 14, 2000 | SANTA CLARITA, CA | N9692F | Incident | substantial |
Settling with power precipitated by a wind direction change during the approach to land sequence and the check pilot's delayed remedial action to corr…Settling with power precipitated by a wind direction change during the approach to land sequence and the check pilot's delayed remedial action to correct the event. Factors in the accident were crew resource management coordination concerning flight control authority and unsuitable terrain for landing. |
| May 03, 2000 | ABERDEEN, SD | N456EM | Incident | substantial | the ground resonance encountered by the pilot. |
| May 03, 2000 | LOVELAND, CO | N1098B | Incident | substantial | The pilot misjudged the run on landing during a full autorotation. Factors were a total loss of power for unknown reasons and soft terrain. |
| May 01, 2000 | RIALTO, CA | N5395S | Minor | substantial |
The student's misjudged altitude and failure to maintain rotor rpm while practicing an autorotation, and, the instructor's delayed remedial corrective…The student's misjudged altitude and failure to maintain rotor rpm while practicing an autorotation, and, the instructor's delayed remedial corrective action and inadequate supervision of the flight. |
| Mar 27, 2000 | DEL RIO, TX | N1110N | Fatal (2) | destroyed |
An in-flight loss of control while maneuvering for undetermined reasons resulting in an in-flight collision with terrain. A factor in the accident was…An in-flight loss of control while maneuvering for undetermined reasons resulting in an in-flight collision with terrain. A factor in the accident was the in-flight loss of engine power and rotor rpm. |
| Mar 08, 2000 | TYSFORD, UK | GZAPS | Fatal (2) | destroyed | Investigation pending |
| Jan 18, 2000 | SHERWOOD, OR | N9297F | Incident | substantial | The pilots failure to arrest the helicopter's descent rate during a planned approach to a hover. Factors include uneven terrain. |
| Dec 18, 1999 | BROWNSBORO, TX | N575PF | Serious (1) | substantial | The loss of tail rotor effectiveness as a result of tail rotor vortex ring state. |
| Dec 13, 1999 | SALINA, KS | N58408 | Serious (2) | substantial | The pilot's failure to follow the published practice autorotation procedures, the improper use of throttle, and the inadequate flare. |
| Sep 01, 1999 | UTICA, NY | N58397 | Incident | substantial |
The pilot's failure to maintain control of the helicopter while maneuvering, which resulted in a hard landing. A factor in this accident was the pilo…The pilot's failure to maintain control of the helicopter while maneuvering, which resulted in a hard landing. A factor in this accident was the pilot's lack of total experience in helicopters. |
| Aug 23, 1999 | RUSSELLVILLE, AR | N44KH | Minor | substantial | The improper touchdown by the flight instructor. |
| 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. |
| Jul 15, 1999 | HOUSTON, TX | N7491F | Minor | substantial |
The hard landing as a result of the flight instructor's failure to attain the proper airspeed before simulating an engine failure, which resulted in t…The hard landing as a result of the flight instructor's failure to attain the proper airspeed before simulating an engine failure, which resulted in the development of a high sink rate. Factors were the night illumination and the soft ground. |
| 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. |