WPR19LA011

NTSB accident investigation · Piper PA32R · Indianapolis, IN · October 21, 2018

Accident · No injuriesClass 3 · LimitedFinal report
Date
October 21, 2018, 14:44 local (18:44 UTC)
Place
Indianapolis, IN
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N2920QPiper PA32R
Defining event
Enroute-cruise: Loss of engine power (total)
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 3
NTSB office
Western Pacific Region
FAA report
20181021020509A
Case key
98525

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

A total loss of engine power due to displacement of the dual magneto’s internal camshaft, which resulted in the magneto’s inability to produce spark.

Findings · 1

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Ignition system: magneto/distributorAircraft › Aircraft power plant · InoperativePiper PA-32R-300: 2 casesAll aircraft: 101 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilot reported that he was approaching his destination airport at 1,000 ft above ground level when the engine lost total power. After an unsuccessful attempt to restart the engine, the pilot performed a forced landing to a nearby parking lot, during which the airplane sustained substantial damage. A postaccident examination of the engine revealed that the single-drive dual magneto failed to produce spark due to the displacement of its camshaft. As a result, when the camshaft was positioned to neutral, the contact points were opened instead of closed, and when the camshaft was rotated approximately 8°, the points were closed when they should have been open. The magneto was then re-assembled to manufacturer specifications, tested, and found to produce spark on all ignition leads. The displacement of the camshaft resulted in the magneto not producing spark on any of its ignition leads, and a subsequent loss of engine power. It could not be determined if the displacement of the magneto camshaft was a result of an improper installation or if it moved in flight.

Factual narrative

On October 21, 2018, at 1444 eastern daylight time, a Piper PA-32R-300 airplane, N2920Q, was substantially damaged when it was involved in an accident near Indianapolis, Indiana. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight. The pilot reported that he was about 4 miles north of his destination airport, at 1,000 ft above ground level (agl), when the engine experienced a complete loss of power. He attempted to restart the engine, but was unsuccessful, and chose to perform a forced landing in a parking lot. During the landing roll, the airplane struck a curb, and the wing impacted a tree. During examination of the engine, a Federal Aviation Administration (FAA) inspector manually rotated the single-drive dual magneto drive shaft, and the magneto failed to produce spark on any of its leads. Review of maintenance logbooks revealed that the magneto was overhauled and tested on February 8, 2018 and had accumulated 87 hours since the overhaul. The magneto was examined and tested, during which the impulse coupling was rotated by hand and the magneto timing was tested using a timing light. When the impulse coupling was rotated to neutral position, contact points were open when they should have been closed. When impulse coupling was rotated counterclockwise about 8° to the L mark, the timing light indicated that contact points were closed when they should have been open. The magneto camshaft was displaced when viewed through magneto timing port. When the cam was positioned to neutral, the points were opened instead of being closed. When the camshaft was rotated approximately 8°, the points should have opened, but they closed at that position. Such displacement of the camshaft would cause the magneto not to produce spark. The magneto was disassembled, inspected, and reassembled, with the cam shaft installed per the manufacturer’s specifications, and when subsequently tested, it produced sparks on all leads.

Aircraft

Registration
N2920Q
Reported as
Piper PA32R (300)
Category
Airplane
Serial number
32R-7780266
Built
1977
Airframe hours
3,788.9
Engine
Lycoming TIO 540, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · March 18, 2018
Departed
UMP · Indianapolis, IN
Destination
EYE · Indianapolis, IN
Equipment
Electronic multifunction display, Electronic flight bag or handheld device, Auto-pilot, Stall warning system, Satellite tracking device, Handheld GPS

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
70
Injuries
None
Certificate
Flight instructor
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, With waivers/limitations
Last flight review
October 23, 2017
Seat
Front
Restraint
3-point
Flight hours
5,046 total · 3,468 in this make and model · 4,821 as pilot in command · 34 in the last 90 days · 13 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
None
Temperature
50 °F, dew point 28 °F
Altimeter
30.29 inHg
Observed at
KEYE, 4 nm away

Docket · 5

The files NTSB released with the investigation on January 19, 2022, on NTSB’s docket system: statements, records, photos and specialists’ reports. 24.5 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.