No fatalities

6 Sep 2012: PIPER PA-25-235 (N7655Z) — Jasper, MO

Jasper, MO, United States

On 6 Sep 2012, a PIPER PA-25-235 (registration N7655Z) was involved in an aviation accident near Jasper, MO. No fatalities were reported. Investigators recorded the probable cause as: Separation of a support bracket in the carburetor air box, which entered the carburetor and blocked the venturi, obstructing airflow and resulting in loss of engine power. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On September 6, 2012, a Piper PA-25-235 (N7655Z) conducting aerial application experienced engine power loss and force-landed near Jasper, Missouri. The pilot was uninjured; the aircraft sustained substantial damage. Postaccident examination revealed a separated carburetor air box bracket obstructed the venturi.

Accident Overview

On September 6, 2012, at approximately 1700 central daylight time, a Piper PA-25-235, registration N7655Z, was substantially damaged during a forced landing near Jasper, Missouri. The commercial pilot was not injured. The airplane was owned and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 137 without a flight plan. Visual meteorological conditions prevailed at the time of the accident. The aerial application flight had departed Lamar Municipal Airport (KLLU), Lamar, Missouri, approximately 1630.

Sequence of Events

The pilot reported that while spreading turnip seeds, the engine started to lose power. He elected to perform a precautionary landing to the field. During the precautionary landing, he observed a fence and berm ahead, so he added power to go over the fence; however, the engine lost all power. During the subsequent forced landing, the airplane hit a fence, resulting in damage to the propeller, the left main landing gear, and substantial damage to the left wing spar.

Postaccident Examination

The postaccident engine examination revealed that a support bracket in the carburetor air box had separated and entered the carburetor. The separated piece blocked the venturi and obstructed the airflow within the engine, resulting in the subsequent loss of engine power. An examination of the remaining engine and airframe systems revealed no anomalies.

The last annual inspection was completed on September 3, 2012. According to the Federal Aviation Administration inspector who examined the airplane, this support bracket would not be included in the examination and work conducted for an annual inspection and would require the removal of the carburetor air box.

Probable cause

Separation of a support bracket in the carburetor air box, which entered the carburetor and blocked the venturi, obstructing airflow and resulting in loss of engine power.

Contributing factors

Fuel control/carburetor — Failure