# NTSB FTW81FA007: Bell 212, N16863, Galveston, TX, October 26, 1980

- Type: NTSB accident investigation
- Classification: Accident · Serious injuries · Closed
- Date: October 26, 1980
- Place: Galveston, TX · GALVESTON, TX
- Location: 29.3014° N, 94.7978° W: Placed by OpenAirDocs: center of Galveston, TX, within about 6 miles (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=29.3014&lon=-94.7978&mi=10
- Phase of flight: [Initial climb](https://openairdocs.org/ntsb-phases/350) (OpenAirDocs' grouping)
- Highest injury: Serious injuries
- Injuries: 1 serious
- Status: Completed, report November 12, 1980
- Report: Brief approved by the director
- NTSB case key (mKey): 128482
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=FTW81FA007
- Page: https://openairdocs.org/ntsb/FTW81FA007

## NTSB brief

```
----------------------------------------------------------------------------------------------------------------------------
 FILE    DATE          LOCATION          AIRCRAFT DATA       INJURIES       FLIGHT                        PILOT DATA
                                                               F  S M/N     PURPOSE
----------------------------------------------------------------------------------------------------------------------------
3-2697  80/10/26   GALVESTON,TX        BELL 212            CR-  0  1  0  COMMERCIAL                COMMERCIAL, AGE 35, 8816
        TIME - 1405                    N16863              PX-  0  0  0  AIR TAXI-CARGO            TOTAL HOURS, 409 IN TYPE,
                                       DAMAGE-SUBSTANTIAL  OT-  0  0  0                            NOT INSTRUMENT RATED.
        DEPARTURE POINT             INTENDED DESTINATION
          GALVESTON,TX                GULF OF MEXICO
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           ENGINE FAILURE OR MALFUNCTION                            TAKEOFF: INITIAL CLIMB
           HARD LANDING                                             LANDING: POWER-OFF AUTOROTATIVE LANDING
        PROBABLE CAUSE(S)
           POWERPLANT - TURBINE ASSEMBLY: BLADE,TURBINE WHEEL
           MISCELLANEOUS ACTS,CONDITIONS - MATERIAL FAILURE
           PILOT IN COMMAND - FAILED TO FOLLOW APPROVED PROCEDURES,DIRECTIVES,ETC.
           MISCELLANEOUS ACTS,CONDITIONS - IMPROPER EMERGENCY PROCEDURES
        FACTOR(S)
           MISCELLANEOUS ACTS,CONDITIONS - DOWNWIND
        COMPLETE POWER LOSS - COMPLETE ENGINE FAILURE/FLAMEOUT-1 ENGINE
        EMERGENCY CIRCUMSTANCES - FORCED LANDING OFF AIRPORT ON LAND
        REMARKS- NO2 ENG BLADE SEPN.ENG LEFT IN OPN CAUSING OVRTEMP.TORQUE SET FOR NO1 ENG 13% ABOVE MAX.
```

## Aircraft

- Registration: N16863 (not matched to a registry record)
- Reported make and model: BELL 212
- Category: Helicopter
- Engines: turbo shaft
- Damage: Substantial damage

## FAA reports on this event (1)

The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs).

- [Accident 19801026058329A](https://openairdocs.org/incident/19801026058329A), Oct 26, 1980: Bell 212, Galveston, TX, Substantial damage. Lost one engine & pilot attempted emergency landing downwind. Helicopter hit hard with forward motion.

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

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