LAX82FA005

NTSB accident investigation · Bell 205A-1 · Fremont, CA · October 22, 1981

Accident · FatalClosed
Date
October 22, 1981
Place
Fremont, CA · FREMONT, CA
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N1496WBell 205A-1
Status
Completed · report November 16, 1981
Report
Brief approved by the director
Case key
123837

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

NTSB brief

NTSB’s brief of the accident, as it was printed: the coded facts, with the probable cause and factors.

----------------------------------------------------------------------------------------------------------------------------
 FILE    DATE          LOCATION          AIRCRAFT DATA       INJURIES       FLIGHT                        PILOT DATA
                                                               F  S M/N     PURPOSE
----------------------------------------------------------------------------------------------------------------------------
3-2394  81/10/22   FREMONT,CA          BELL 205A-1         CR-  1  0  0  MISCELLANEOUS             COMMERCIAL, AGE 35, 2142
        TIME - 0033                    N1496W              PX-  0  0  0  FERRY                     TOTAL HOURS, 240 IN TYPE,
                                       DAMAGE-DESTROYED    OT-  0  0  0                            NOT INSTRUMENT RATED.
        DEPARTURE POINT             INTENDED DESTINATION         LAST ENROUTE STOP
          HAYWARD,CA                  HAYWARD,CA                   SAN JOSE,CA
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           COLLIDED WITH: WIRES/POLES                               IN FLIGHT: OTHER
        PROBABLE CAUSE(S)
           PILOT IN COMMAND - CONTINUED VFR FLIGHT INTO ADVERSE WEATHER CONDITIONS
           PILOT IN COMMAND - SPATIAL DISORIENTATION
        FACTOR(S)
           WEATHER - LOW CEILING
           WEATHER - FOG
        WEATHER BRIEFING - NO RECORD OF BRIEFING RECEIVED
        SKY CONDITION                                            CEILING AT ACCIDENT SITE
          OVERCAST                                                  250
        VISIBILITY AT ACCIDENT SITE                              PRECIPITATION AT ACCIDENT SITE
          3/4 MILE OR LESS                                         NONE
        OBSTRUCTIONS TO VISION AT ACCIDENT SITE                  TEMPERATURE-F
          FOG                                                       60
        TYPE OF WEATHER CONDITIONS                               TYPE OF FLIGHT PLAN
          IFR                                                      NONE
         FIRE AFTER IMPACT
        REMARKS- AFTER TURNING,OBSD TO PULL UP NOSE,SLIDE DWN & BACKWARDS INTO PWR LN.

Aircraft

Registration
N1496W
Reported as
Bell 205A-1
Category
Helicopter
Engine
turbo shaft
Damage
Destroyed

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.