Robinson R22 Beta Safety Record
Complete NTSB accident and incident history. 168 events recorded from 1989 to 2025.
| Date | Location | Reg# | Severity | Damage | Probable Cause |
|---|---|---|---|---|---|
| May 14, 2023 | Brady, TX | N40506 | Fatal (1) | substantial |
The non-certificated pilot’s failure to ensure the collective friction control was adequately engaged during an on-ground engine run, which resulted i…The non-certificated pilot’s failure to ensure the collective friction control was adequately engaged during an on-ground engine run, which resulted in the helicopter inadvertently becoming airborne. Contributing to the crash were the pilot’s various physical and mental conditions and his use of potentially impairing medications. |
| Jun 27, 2011 | Del Valle, TX | N7779M | Fatal (1) | substantial |
The divergence of the main rotor from its normal plane of rotation for reasons that cannot be determined because the pilot’s control inputs leading up…The divergence of the main rotor from its normal plane of rotation for reasons that cannot be determined because the pilot’s control inputs leading up to the event are unknown, resulting in mast bumping and main rotor blade separation. |
| Jun 02, 2010 | Spokane, WA | N522SA | Fatal (1) | substantial |
A loss of engine power for reasons that could not be determined because postaccident examination of the airframe and engine did not reveal any anomali…A loss of engine power for reasons that could not be determined because postaccident examination of the airframe and engine did not reveal any anomalies that would have precluded normal operation and the student pilot's failure to maintain main rotor rpm. Contributing to the accident was the student pilot's low total flight experience. |
| Mar 13, 2008 | Wilmington, NC | N2215R | Fatal (1) | substantial | The pilot's failure to maintain proper rotor rpm after a partial loss of engine power. |
| Jul 22, 2007 | San Salvador, ES | HR-ASO | Fatal (1) | destroyed | Investigation pending |
| Aug 10, 2006 | Tucson, AZ | N7059S | Fatal (1) | substantial |
The pilot's failure to maintain adequate rotor rpm and adequate terrain clearance while maneuvering to reverse direction. Contributing factors were t…The pilot's failure to maintain adequate rotor rpm and adequate terrain clearance while maneuvering to reverse direction. Contributing factors were the high density altitude, that exceeded the helicopter's performance capability, and the rising mountainous terrain. |
| Apr 13, 2006 | Chelsea, MI | N887BC | Fatal (2) | substantial |
The pilot's inadequate preflight inspection of the helicopter that failed to discover water in the fuel, resulting in a loss of engine power while man…The pilot's inadequate preflight inspection of the helicopter that failed to discover water in the fuel, resulting in a loss of engine power while maneuvering, and an in-flight collision with trees and terrain. Factors associated with the accident were inadequate fuel storage, and the low altitude of the helicopter. |
| Nov 27, 2004 | Arlington, WA | N4029Q | Fatal (2) | destroyed |
The divergence of the main rotor from its normal plane of rotation for an undetermined reason, resulting in rotor contact with the aircraft's left win…The divergence of the main rotor from its normal plane of rotation for an undetermined reason, resulting in rotor contact with the aircraft's left windscreen. The failure of the door pins to be installed was a factor. |
| Aug 13, 2004 | McIvor Lake, BC, CA | C-FHGH | Fatal (1) | destroyed | Investigation pending |
| Aug 11, 2004 | Sazava, EZ | OK-YIT | Fatal (1) | destroyed | Investigation pending |
| Aug 02, 2004 | Miami, FL | N2566W | Fatal (1) | destroyed |
The failure of company maintenance personnel to secure the push/pull tube to the left lug of the non-rotating portion of the swashplate assembly follo…The failure of company maintenance personnel to secure the push/pull tube to the left lug of the non-rotating portion of the swashplate assembly following maintenance, and the inability of the pilot to control the helicopter resulting in the in-flight collision with terrain. |
| Dec 15, 2003 | Redlands, CA | N1225D | Fatal (1) | destroyed |
a loss of engine power due to the pilot inadvertently turning off the magnetos and his failure to initiate an autorotation and to maintain main rotor …a loss of engine power due to the pilot inadvertently turning off the magnetos and his failure to initiate an autorotation and to maintain main rotor rpm. A factor in the accident was the pilot's use of an over-the-counter medication that impaired his judgment and/or performance. |
| Jul 22, 2003 | Tulalip, WA | N7190K | Fatal (1) | destroyed | A loss of control for unknown reasons. |
| Dec 23, 2002 | Dolan Springs, AZ | N888KB | Fatal (2) | destroyed |
the pilot's inadequate visual lookout and failure to maintain clearance from power lines. A factor was the pilot's decision to conduct cruise flight …the pilot's inadequate visual lookout and failure to maintain clearance from power lines. A factor was the pilot's decision to conduct cruise flight at a low altitude. |
| May 22, 2002 | Mammoth Lakes, CA | N7194J | Fatal (2) | destroyed |
The pilot's poor decision to continue the flight into the rising mountainous terrain, and subsequent failure to maintain clearance with the trees. Co…The pilot's poor decision to continue the flight into the rising mountainous terrain, and subsequent failure to maintain clearance with the trees. Contributing factors were rising mountainous terrain, the high density altitude, and the exceeded weight and balance and performance capability of the helicopter. |
| Aug 19, 2000 | WATSONVILLE, CA | N8313Z | Fatal (2) | destroyed |
The divergence of the main rotor from its normal plane of rotation for an undetermined reason, which resulted in mast bumping and rotor contact with t…The divergence of the main rotor from its normal plane of rotation for an undetermined reason, which resulted in mast bumping and rotor contact with the fuselage. |
| Apr 27, 2000 | SAN DIEGO, CA | N622EH | Fatal (1) | destroyed | The failure of the flight instructor to maintain control of the helicopter, resulting in skid contact with an obstacle and dynamic roll over. |
| Mar 24, 2000 | RIALTO, CA | N8328Q | Fatal (1) | destroyed | The pilot's in-flight loss of control for undetermined reasons. |
| Mar 26, 1999 | HOUSTON, TX | N2323V | Fatal (2) | destroyed |
The pilot's failure to maintain control of the helicopter while maneuvering. A factor was the pilot's impairment due to his use of a prescription nar…The pilot's failure to maintain control of the helicopter while maneuvering. A factor was the pilot's impairment due to his use of a prescription narcotic. |
| Dec 16, 1997 | BELLE VERNON, PA | N55TP | Fatal (1) | destroyed | The pilot's improper out-of-ground hover procedure, which resulted in a loss of tailrotor effectiveness. |
| Oct 19, 1996 | HALSEY, OR | N512HH | Fatal (1) | destroyed |
The pilot-in-command's failure to maintain main rotor RPM, resulting in loss of control of the helicopter and collision with terrain. Factors include…The pilot-in-command's failure to maintain main rotor RPM, resulting in loss of control of the helicopter and collision with terrain. Factors included the pilot's lack of experience in helicopters, and interpersonal relationship problems between the pilot and his girlfriend. |
| Oct 14, 1994 | EUNICE, LA | N80546 | Fatal (1) | destroyed |
THE PILOT'S FAILURE TO PROPERLY USE CARBURETOR HEAT, THE FORMATION OF CARBURETOR ICE, AND FAILURE OF THE PILOT TO MAINTAIN ROTOR RPM AFTER LOSS OF ENG…THE PILOT'S FAILURE TO PROPERLY USE CARBURETOR HEAT, THE FORMATION OF CARBURETOR ICE, AND FAILURE OF THE PILOT TO MAINTAIN ROTOR RPM AFTER LOSS OF ENGINE POWER, WHICH RESULTED IN A LOSS OF CONTROL AND COLLISION WITH TERRAIN. A FACTOR RELATED TO THE ACCIDENT WAS: THE WEATHER CONDITION, WHICH WAS CONDUCIVE TO CARBURETOR ICING. |
| Sep 24, 1993 | WILDOMAR, CA | N40049 | Fatal (2) | destroyed |
THE FAILURE OF THE TAIL ROTOR BLADE AFTER BEING STRUCK BY THE PILOT'S KNEE BOARD, AND THE FAILURE OF THE PILOT TO ADEQUATELY SECURE THE KNEE BOARD WHI…THE FAILURE OF THE TAIL ROTOR BLADE AFTER BEING STRUCK BY THE PILOT'S KNEE BOARD, AND THE FAILURE OF THE PILOT TO ADEQUATELY SECURE THE KNEE BOARD WHILE IN FLIGHT. |
| May 23, 1990 | GRIFFIN, GA | N8064K | Fatal (1) | destroyed | LOSS OF ENGINE POWER FOR AN UNKNOWN REASON. THE PRESENCE OF TREES IN THE EMERGENCY LANDING AREA WAS A RELATED FACTOR. |
| Apr 20, 1989 | STOCKTON, CA | N26198 | Fatal (2) | destroyed |
POOR JUDGEMENT OF THE PILOT BY FLYING WHILE PHYSICALLY IMPAIRED FROM CONSUMPTION OF ALCOHOL & DRUGS, AND HIS FAILURE TO MAINTAIN PROPER ALTITUDE. THE…POOR JUDGEMENT OF THE PILOT BY FLYING WHILE PHYSICALLY IMPAIRED FROM CONSUMPTION OF ALCOHOL & DRUGS, AND HIS FAILURE TO MAINTAIN PROPER ALTITUDE. THE LIGHT CONDITION (AT NIGHT) AND THE OBSTRUCTIONS (POWER LINES AND BUILDING) WERE CONSIDERED TO BE CONTRIBUTING FACTORS. |