# NTSB SEA67A0052: Hughes 269A, N8888F, Yakima, WA, March 19, 1967

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Closed
- Date: March 19, 1967
- Place: Yakima, WA · YAKIMA, WA
- Location: 46.5909° N, 120.5494° W: Placed by OpenAirDocs: center of Yakima, WA, within about 6 miles (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=46.5909&lon=-120.5494&mi=10
- Phase of flight: [Initial climb](https://openairdocs.org/ntsb-phases/350) (OpenAirDocs' grouping)
- Highest injury: No injuries
- Injuries: 1 uninjured
- Status: Completed, report July 13, 1967
- Report: Brief approved by the director
- NTSB case key (mKey): 119145
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=SEA67A0052
- Page: https://openairdocs.org/ntsb/SEA67A0052

## NTSB brief

```
----------------------------------------------------------------------------------------------------------------------------
 FILE    DATE          LOCATION          AIRCRAFT DATA       INJURIES       FLIGHT                        PILOT DATA
                                                               F  S M/N     PURPOSE
----------------------------------------------------------------------------------------------------------------------------
2-0124  67/3/19    YAKIMA,WASH         HUGHES 269A         CR-  0  0  1  COMMERCIAL                COMMERCIAL, AGE 58, 14310
        TIME - 1130                    N8888F              PX-  0  0  0  ASSOC CROP CTL ACTIVITY   TOTAL HOURS, 400 IN TYPE,
                                       DAMAGE-SUBSTANTIAL  OT-  0  0  0                            NOT INSTRUMENT RATED.
        TYPE OF ACCIDENT                                         PHASE OF OPERATION
           ENGINE FAILURE OR MALFUNCTION                            TAKEOFF: INITIAL CLIMB
           HARD LANDING                                             LANDING: LEVEL OFF/TOUCHDOWN
        PROBABLE CAUSE(S)
           POWERPLANT - ENGINE STRUCTURE: PISTON,PISTON RINGS
           MISCELLANEOUS ACTS,CONDITIONS - MATERIAL FAILURE
           POWERPLANT - FUEL SYSTEM: CARBURETOR
           POWERPLANT - FUEL SYSTEM: FILTERS,STRAINERS,SCREENS
           MISCELLANEOUS ACTS,CONDITIONS - OBSTRUCTED
           MISCELLANEOUS ACTS,CONDITIONS - FUEL STARVATION
        PARTIAL POWER LOSS - PARTIAL LOSS OF POWER - 1 ENGINE
        EMERGENCY CIRCUMSTANCES - FORCED LANDING OFF AIRPORT ON LAND
         SPECIAL DATA
          TOTAL HOURS IN CROP CONTROL - UNKNOWN/NOT REPORTED       KIND OF OPERATION - FERTILIZING (LIQUID)
          KIND OF CROP - FRUIT ORCHARDS                            TYPE OF CHEMICAL USED - LIQUID CHEMICAL-NONTOXIC
          PILOT' S SEAT BELT -UNKNOWN/NOT REPORTED                 GLOVES - USED
          GOGGLES - NOT USED                                       CRASH HELMET - AVAILABLE-NOT USED
          COCKPIT CRASHPAD - NOT INSTALLED                         CRASH BAR - NOT INSTALLED
          TANK/HOPPER-LOCATION - SIDES                             TERRAIN-TYPE -ROLLING
          ELEVATION-AREA BEING TREATED-FEET -  1150                SWATH RUN-HOW FLOWN - WIND CALM
        REMARKS- BROKEN PISTON RING NO.1 CYL.CARBURETOR FINGER STRAINER PARTIALLY BLOCKED BY LINT AND SEDIMENT.
```

## Aircraft

- Registration: [N8888F](https://openairdocs.org/deregistered/N8888F-2015-04-27), registration cancelled 2015-04-27, S/N 0231, built 1963 (OpenAirDocs)
- Reported make and model: HUGHES 269A
- Registry model: [Hughes 269A](https://openairdocs.org/model/hughes-269a) (registry code 4470402) (OpenAirDocs)
- Registry engine: [Lycoming HO-360 series](https://openairdocs.org/engine/lycoming-ho-360-series) (registry code 41513, reciprocating) (OpenAirDocs)
- Category: Helicopter
- Engines: reciprocating
- Damage: Substantial damage

## Other investigations on N8888F (3)

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.

- [NTSB SEA90LA084](https://openairdocs.org/ntsb/SEA90LA084), May 22, 1990: Hughes 269A (N8888F), Bremerton, WA, substantial damage. Probable cause: FAILURE OF THE TAIL ROTOR CONTROL FOR AN UNDETERMINED REASON.
- [NTSB SEA68D0281](https://openairdocs.org/ntsb/SEA68D0281), Mar 31, 1968: Hughes 269A (N8888F), Yakima, WA, substantial damage
- [NTSB OAK65A0052](https://openairdocs.org/ntsb/OAK65A0052), Jan 12, 1965: Hughes 269A (N8888F), Visalia, CA, substantial damage

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.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.