NYC72AN163

NTSB accident investigation · Bell 206A · New Cumberland, PA · June 26, 1972

Accident · FatalClosed
Date
June 26, 1972
Place
New Cumberland, PA · NEW CUMBERLAND, PA
Injuries
4 fatal
Damage
Destroyed
Phase of flight
Approach
Aircraft
N25BBBell 206A
Status
Completed · report December 13, 1972
Report
Brief approved by the director
Safety recommendations
Yes
Case key
79412

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
----------------------------------------------------------------------------------------------------------------------------
3-0924  72/6/26    NEW CUMBERLAND,PA   BELL 206A           CR-  1  0  0  NONCOMMERCIAL             ATP,FLIGHT INSTR., AGE
        TIME - 1305                    N25BB               PX-  3  0  0  CORP/EXEC                 45, 9464 TOTAL HOURS,
                                       DAMAGE-DESTROYED    OT-  0  0  0                            1063 IN TYPE, INSTRUMENT
                                                                                                   RATED.
        NAME OF AIRPORT - CAPITAL CITY
        DEPARTURE POINT             INTENDED DESTINATION         LAST ENROUTE STOP
          NEW CUMBERLAND,PA           NEW CUMBERLAND,PA            HARRISBURG,PA
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           PROPELLER/ROTOR FAILURE: MAIN ROTOR                      LANDING: FINAL APPROACH
           COLLISION WITH GROUND/WATER: UNCONTROLLED                IN FLIGHT: UNCONTROLLED DESCENT
        PROBABLE CAUSE(S)
           ROTORCRAFT - ROTOR ASSEMBLIES: OTHER
           MISCELLANEOUS ACTS,CONDITIONS - MATERIAL FAILURE
        FACTOR(S)
           MISCELLANEOUS ACTS,CONDITIONS - SEPARATION IN FLIGHT
         FIRE AFTER IMPACT
        REMARKS- MAIN ROTOR RETENTION STRAP FITTING PN206-010-155.7 FAILED,CAUSE UNDETERMINED.BLADE NOT RECOVERED.

Aircraft

Registration
N25BB
Reported as
Bell 206A
Category
Helicopter
Engine
turbo shaft
Damage
Destroyed
Airport
Capital City

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.