- 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.
On this page
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.
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.