19960213006269I

Incident · Minor damage

FAA incident report · Beech E18S · Rochester, NY · February 13, 1996

Date
February 13, 1996 · 13:10 local
Place
Rochester, NY
Airport
Greater Rochester Internationa
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
Air taxi and commuter (Part 135)
Operator
VPDA
Damage
Minor damage
Aircraft
N32M
Reported as
Beech E18S
People aboard
1
Fatal injuries
0

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: on 2/13/96 at 1310 local time a Beech E-18S, N32M owned by piedmont air cargo experienced a tailwheel retraction on landing. VFR conditions prevailed and an IFR flight plan was filed. Aircraft suffered minor damage. Flight originated in gastonia, NC on 2/13/96 at 9:00 EST. Tailwheel shear bolt on the extend/retract cable was found sheared as a result of slide binding on tube, and bent tube; suspect lack of lubrication as cause. Aircraft ferried with tailwheel extended and disconnected from gear drive mechanism. M & d was sent. Pmi notified and advised to address lack of lubrication (700-800 hrs between lub. Interval). This incident is considered closed.

As the FAA filed it

NARRATIVE: ON 2/13/96 AT 1310 LOCAL TIME A BEECH E-18S, N32M OWNED BY PIEDMONT AIR CARGO EXPERIENCED A TAILWHEEL RETRACTION ON LANDING. VFR CONDITIONS PREVAILED AND AN IFR FLIGHT PLAN WAS FILED. AIRCRAFT SUFFERED MINOR DAMAGE. FLIGHT ORIGINATED IN GASTONIA, NC ON 2/13/96 AT 9:00 EST. TAILWHEEL SHEAR BOLT ON THE EXTEND/RETRACT CABLE WAS FOUND SHEARED AS A RESULT OF SLIDE BINDING ON TUBE, AND BENT TUBE; SUSPECT LACK OF LUBRICATION AS CAUSE. AIRCRAFT FERRIED WITH TAILWHEEL EXTENDED AND DISCONNECTED FROM GEAR DRIVE MECHANISM. M & D WAS SENT. PMI NOTIFIED AND ADVISED TO ADDRESS LACK OF LUBRICATION (700-800 HRS BETWEEN LUB. INTERVAL). THIS INCIDENT IS CONSIDERED CLOSED.

Other reports on N32M · 2

Matched to the same aircraft by N-number and date.