ANC71IA015

NTSB incident investigation · Grumman G-21A · Juneau, AK · August 30, 1970

Incident · No injuriesClosed
Date
August 30, 1970
Place
Juneau, AK · JUNEAU, AK
Injuries
6 uninjured
Damage
Minor damage
Phase of flight
Enroute
Aircraft
N4773CGrumman G-21A
Status
Completed · report February 11, 1971
Report
Brief approved by the director
Case key
158797

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

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
----------------------------------------------------------------------------------------------------------------------------
4-0052  70/8/30  NR.JUNEAU,ALAS        GRUMMAN G-21A       CR-  0  0  1  SCHED DOM PASSG SRV       CERTIFICATE UNKNOWN, AGE
        TIME - 1530                    N4773C              PX-  0  0  5                            41, 13500 TOTAL HOURS,
                                       DAMAGE-MINOR        OT-  0  0  0                            800 IN TYPE, INSTRUMENT
                                                                                                   RATED.
        CLASSIFIED AS INCIDENT
        OPERATOR - ALASKA AIRLINES,INC.
        DEPARTURE POINT             INTENDED DESTINATION
          KETCHIKAN,ALAS              JUNEAU,ALAS
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           PROPELLER/ROTOR FAILURE: PROPELLER                       IN FLIGHT: NORMAL CRUISE
           ENGINE FAILURE OR MALFUNCTION                            IN FLIGHT: NORMAL CRUISE
        PROBABLE CAUSE(S)
           POWERPLANT - PROPELLER AND ACCESSORIES: BLADES
           MISCELLANEOUS ACTS,CONDITIONS - FATIGUE FRACTURE
           MISCELLANEOUS ACTS,CONDITIONS - CORRODED/CORROSION
           MISCELLANEOUS ACTS,CONDITIONS - VIBRATION,EXCESSIVE
           MISCELLANEOUS ACTS,CONDITIONS - OVERLOAD FAILURE
        FACTOR(S)
           MISCELLANEOUS ACTS,CONDITIONS - SEPARATION IN FLIGHT
        COMPLETE POWER LOSS - COMPLETE ENGINE FAILURE/FLAMEOUT-1 ENGINE
        EMERGENCY CIRCUMSTANCES - FORCED LANDING OFF AIRPORT ON WATER
                                  UNUSUAL NOISE
                                  PROP/ENGINE VIBRATION
        REMARKS- 3 FT OF LT PROP BLADE SEPARATED. CAUSED FURTHER DMG TO L ENG. MACHINE TOOL MARKS,CORROSION FOUND.

Aircraft

Registration
N4773C
Reported as
Grumman G-21A
Category
Airplane
Engine
turbo prop
Damage
Minor damage