CHI97LA012

NTSB accident investigation · Piper PA-32-260 · Mancelona, MI · October 20, 1996

Accident · No injuriesLimited investigationFinal report
Date
October 20, 1996, 17:30 local (21:30 UTC)
Place
Mancelona, MI
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N56155Piper PA-32-260
Weather
Visual (VMC) · Day
Status
Completed · report May 23, 1997
Report
Approved by Office Director
FAA report
19961020033169A
Case key
10481

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

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Probable cause

the worn fuel system pump (actuator arm). A factor was the unsuitable terrain encountered by the pilot.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine powerClimb
Fuel system,pump - wornCause
Forced landingEmergency landing
On ground/water encounter with terrain/waterEmergency landing
Terrain condition - none suitableFactor

Analysis

The pilot stated that during initial climb the engine lost power. He attempted to restart the engine, but was unable to do so. He made a forced landing in unsuitable terrain. A postaccident examination of the mechanical fuel pump found that the actuator arm was worn and fuel pressure and volume were not sufficient to maintain engine power. There is no manufacturer's requirement for inspection of the fuel pump during its service life. The pump had accumulated 1,007 hours.

Factual narrative

On October 20, 1996, at 1730 eastern daylight time, a Piper PA-32-260, N56155, sustained substantial damage during a forced landing about one-quarter mile west of the Lakes of the North Airport, near Mancelona, Michigan. The pilot reported a loss of engine power and the smell of smoke in the cockpit, prior to the forced landing. The private pilot and one passenger reported no injuries. The personal 14 CFR Part 91 flight was operating in visual meteorological conditions. No flight plan was on file for the local flight. The flight was originating at the time of the accident.

The pilot said that the engine quit completely and that he could not get it to restart. He then set up for a forced landing.

An examination of the airplane after the accident revealed that the actuator arm for the mechanical fuel pump was worn to the extent that adequate fuel pressure and volume was not available. See the Federal Aviation Administration, inspector's report attached as an addendum to this report including drawing of affected part.

There is no manufacturer's requirement for inspection of the mechanical fuel pump during its service life. The pump in the accident airplane had accumulated a total time in service of 1,007 hours at the time of the accident.

Aircraft

Registration
N56155
Reported as
Piper PA-32-260
Category
Airplane
Serial number
32-7300053
Airframe hours
1,007
Engine
Lycoming O-540-E4B5, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Mark E. Lulfs
Airworthiness certificate
Standard, Normal
Last inspection
Annual · November 30, 1995
Departed
4Y4

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
41
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
753 total · 67 in this make and model · 659 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
80° at 6 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
55 °F, dew point 37 °F
Altimeter
29.00 inHg
Observed at
KHT, 35 nm away

FAA reports on this event · 1

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