19960415014769I

Incident · Minor damage

FAA incident report · Piper PA-28-181 · Red Wing, MN · April 15, 1996

Date
April 15, 1996 · 17:00 local
Place
Red Wing, MN
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N39609
Reported as
Piper PA28181
Reported engine
Lycoming O360A4M
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,300 total1,100 in this make and model26 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Narrative: en route from kenosha, WI (dnw) to blaine, MN anoka/crystal (ane) at 2500' MSL VFR conditions, engine began to lose power and run rough. Smoke started to enter the cabin. Decided to initiate off airport landing. Landed on Wisconsin highway 35 approximately 20 miles south of Red Wing, Minnesota (rwg). Secured aircraft in enerson's yard. 2 hours and 30 minutes of fuel on board. #3 engine cylinder separated 1.5" below head approximately 75% around. Complete separation did not occur. Total time on part 2800 hours time since overhaul 400 hours. FAA form 8010-4 ( m or d report) submitted. No unusual maintenance recorded.

As the FAA filed it

NARRATIVE: EN ROUTE FROM KENOSHA, WI (DNW) TO BLAINE, MN ANOKA/CRYSTAL (ANE) AT 2500' MSL VFR CONDITIONS, ENGINE BEGAN TO LOSE POWER AND RUN ROUGH. SMOKE STARTED TO ENTER THE CABIN. DECIDED TO INITIATE OFF AIRPORT LANDING. LANDED ON WISCONSIN HIGHWAY 35 APPROXIMATELY 20 MILES SOUTH OF RED WING, MINNESOTA (RWG). SECURED AIRCRAFT IN ENERSON'S YARD. 2 HOURS AND 30 MINUTES OF FUEL ON BOARD. #3 ENGINE CYLINDER SEPARATED 1.5" BELOW HEAD APPROXIMATELY 75% AROUND. COMPLETE SEPARATION DID NOT OCCUR. TOTAL TIME ON PART 2800 HOURS TIME SINCE OVERHAUL 400 HOURS. FAA FORM 8010-4 ( M OR D REPORT) SUBMITTED. NO UNUSUAL MAINTENANCE RECORDED.