Casualties unknown

2007-07-12: Piper PA-23-160 (N4043P) — Quinton Jenkins — Enterprise, AL

Enterprise, AL, US

On July 12, 2007, a Piper PA-23-160 (registration N4043P) operated by Quinton Jenkins was involved in an aviation accident near Enterprise, AL. Investigators recorded the probable cause as: The designated examiner's improper decision to simulate an engine failure on short final approach, in conjunction with a short-field landing maneuver, and his inadequate remedial action. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

During a private pilot's commercial checkride, the examiner simulated a right engine failure on short-field approach. The pilot feathered the propeller but thought the examiner had de-feathered it. A go-around attempt led to left propeller speed decrease; the examiner landed in a grass field. No preimpact malfunctions were found.

Incident Description

A Federal Aviation Administration (FAA) designated pilot examiner was conducting a checkride for a private pilot seeking a commercial pilot certificate with a multi-engine land rating. Toward the end of the flight, the private pilot had completed single-engine maneuvers, including a simulated single-engine instrument approach to a full-stop landing. The pilot believed the remaining tasks were a short-field landing and an emergency descent.

During the final approach for the short-field landing, the examiner simulated a failure of the right engine. The private pilot feathered the right propeller but suspected that the examiner may have "bumped it out of feather and set it to zero thrust." Shortly after, the pilot realized the airplane would not reach the runway and initiated a go-around. When power was increased on both engines, the airplane began to turn left, and the left propeller speed was observed decreasing.

The examiner then took control of the airplane, reduced power on both engines, and executed a landing in a grass field.

Examination Findings

Post-landing examination of the airplane revealed no preimpact mechanical malfunctions. The left propeller was found in the feathered position. Both propeller controls were positioned mid-range, with the left propeller control trailing the right propeller control by approximately 1 inch.

Regulatory Context

The FAA Commercial Pilot Practical Test Standards include instructions for the applicant to actually feather a propeller, but specify that this procedure should be performed at altitude. All other references in the standards pertain to simulating propeller feathering. Additionally, the standards state: "The examiner is expected to use good judgment in the performance of simulated emergency procedures. The use of the safest means for simulation is expected. Consideration must be given to local conditions, both meteorological and topographical, at the time of the test, as well as the applicant's workload, and the condition of the aircraft used."

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20070806X01111. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.