Piper PA24 N6872P

Summary

On 3 January 2019 at about 21:00 local time, a Piper PA24 registered N6872P was involved in an accident near Wilkes-Barre, Pennsylvania, United States. 2 people were on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

3 January 2019 at 21:00

Classification

Accident

Location

Wilkes-Barre, Pennsylvania, United States

Nearest airport

Wilkes-Barre Wyoming Valley (WBW)

Coordinates

41.0000, -75.0000

Aircraft

Piper PA24

Registration

N6872P

Category

Airplane

Year built

1960

Engines

1

Operator

Not recorded

Operating rule

Part 91: General Aviation

Purpose of flight

Instructional

Phase of flight

Not recorded

Route

Towanda → Wilkes-Barre

Aircraft damage

Substantial

Weather

VMC

Light

Day

NTSB number

ERA19LA085

Nobody was injured.

The pilot/mechanic's improper installation and securing of the mixture control cable, which led to a simultaneous loss of total engine power and failure of the nose landing gear to fully extend when the cable caught on the nose landing gear assembly.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot, who was an airframe and powerplant mechanic, and the flight instructor both reported that, after turning onto the base leg at the end of the instructional flight, the pilot extended the landing gear in preparation to land; however, the gear did not fully extend, and the engine stopped producing power. The pilots made a forced landing to a soccer field short of the runway, during which the airplane struck a ditch and sustained substantial damage to the airframe. A postaccident examination of the airplane and engine revealed no obvious preimpact mechanical anomalies with the landing gear system or the engine. However, the pilot later stated that he had opened the engine cowling after the forced landing and saw the mixture cable was caught in the nose gear assembly. The pilot said he then unsnagged the cable, so it was not immediately obvious to investigators. He said that the mixture cable had gotten caught on the nosewheel assembly when it was trying to extend, which had caused the mixture control arm on the carburetor to move to the lean position. The pilot had performed maintenance on the landing gear a few weeks before the accident. He used plastic tie-wraps to ensure the throttle/mixture/carburetor heat cables were positioned away from the nose gear, which does not have a protected well on this make/model airplane. He then flew the airplane and placed it back in his hangar until the accident flight. The pilot said there were a lot of mice in his hangar, and he thought a mouse got up in the engine and chewed off the plastic tie-wraps, which allowed the mixture cable to come loose. However, there was no evidence to support this theory. A review of the airplane's Illustrated Parts Catalogue showed the mixture, throttle, and carburetor heat cables routed and secured away from the nose landing gear via metal clamps. Additional research of the Federal Aviation Administration Service Difficulty Reports (SDRs) revealed only one reported instance in which the mixture control cable got caught in the nose landing gear on this make/model airplane. The December 2003 report stated that, due to the mixture control cable not being properly secured or routed, it encountered the nose gear assembly during extension and fuel to the engine was shut off. The mechanic who submitted the SDR corrected the situation by properly routing and securing the mixture control cable. Given the available evidence, the mixture control cable in the accident airplane was not properly installed/secured. As a result, the cable caught on the nose landing gear assembly when the landing gear were extended and subsequently pulled the mixture control arm on the carburetor, thus shutting off fuel to the engine.

Quoted verbatim from the NTSB record.