# NTSB DEN80FTE45: Grumman G-164A, N5410, Delta, CO, May 26, 1980

- Type: NTSB accident investigation
- Classification: Accident · Serious injuries · Closed
- Date: May 26, 1980
- Place: Delta, CO · DELTA, CO
- Location: 38.7574° N, 108.0880° W: Placed by OpenAirDocs: center of Delta, CO, within about 6 miles (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=38.7574&lon=-108.0880&mi=10
- Phase of flight: [Maneuvering](https://openairdocs.org/ntsb-phases/450) (OpenAirDocs' grouping)
- Highest injury: Serious injuries
- Injuries: 1 serious
- Status: Completed, report November 10, 1980
- Report: Brief approved by the director
- NTSB case key (mKey): 130548
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=DEN80FTE45
- Page: https://openairdocs.org/ntsb/DEN80FTE45

## NTSB brief

```
----------------------------------------------------------------------------------------------------------------------------
 FILE    DATE          LOCATION          AIRCRAFT DATA       INJURIES       FLIGHT                        PILOT DATA
                                                               F  S M/N     PURPOSE
----------------------------------------------------------------------------------------------------------------------------
3-2610  80/5/26  NR.DELTA,CO           GRUMMAN G-164A      CR-  0  1  0  COMMERCIAL                COMMERCIAL, AGE 28, 2606
        TIME - 2030                    N5410               PX-  0  0  0  AERIAL APPLICATION        TOTAL HOURS, 344 IN TYPE,
                                       DAMAGE-DESTROYED    OT-  0  0  0                            INSTRUMENT RATED.
        DEPARTURE POINT             INTENDED DESTINATION
         DELTA,CO                     LOCAL
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           ENGINE FAILURE OR MALFUNCTION                            IN FLIGHT: SWATH RUN
           COLLIDED WITH: TREES                                     LANDING: FINAL APPROACH
        PROBABLE CAUSE(S)
           POWERPLANT - ENGINE STRUCTURE: CYLINDER ASSEMBLY
           MISCELLANEOUS ACTS,CONDITIONS - MATERIAL FAILURE
        FACTOR(S)
           MISCELLANEOUS ACTS,CONDITIONS - LOAD NOT JETTISONED
        PARTIAL POWER LOSS - PARTIAL LOSS OF POWER - 1 ENGINE
        EMERGENCY CIRCUMSTANCES - FORCED LANDING OFF AIRPORT ON LAND
         SPECIAL DATA
          TOTAL HOURS IN CROP CONTROL -  700                       KIND OF OPERATION - OTHER
          KIND OF CROP - MOSQUITO CONTROL                          TYPE OF CHEMICAL USED - LIQUID CHEMICAL-TOXIC
          PILOT' S SEAT BELT -FASTEN-LOOSELY                       GLOVES - NOT USED
          GOGGLES - USED                                           CRASH HELMET - AVAILABLE USED
          COCKPIT CRASHPAD - INSTALLED                             CRASH BAR - INSTALLED
          TANK/HOPPER-LOCATION - FORWARD OF PILOT                  TERRAIN-TYPE -ROLLING
          ELEVATION-AREA BEING TREATED-FEET -  5000                SWATH RUN-HOW FLOWN - WIND CALM
         FIRE AFTER IMPACT
        REMARKS- SPRAYING W MALATHION & DIESEL FUEL.PORTION OF #3 CYL MISSING.
```

## Aircraft

- Registration: [N5410](https://openairdocs.org/deregistered/N5410-1982-11-15), registration cancelled 1982-11-15, S/N 969 (OpenAirDocs)
- Reported make and model: GRUMMAN G-164A
- Registry model: [Grumman G-164A](https://openairdocs.org/model/grumman-g-164a) (registry code 3952704) (OpenAirDocs)
- Category: Airplane
- Engines: reciprocating
- Damage: Destroyed

## 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 19800526016469A](https://openairdocs.org/incident/19800526016469A), May 26, 1980: Gulstm G164A, Delta, CO, Destroyed. Portion of engine cylinder head broke off, caused fire in flight. Slipped aircraft through trees for hard landing.

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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