19970118007059I

Incident · Minor damage

FAA incident report · Piper PA-23-160 · Staunton-Waynes, VA · January 18, 1997

Date
January 18, 1997 · 13:00 local
Place
Staunton-Waynes, VA
Airport
Shenandoah Valley Regional
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N4322P
Reported as
Piper PA23160
People aboard
1
Fatal injuries
0
Pilot’s flight hours
120 total49 in this make and model49 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: on January 18, 1997, at 13:00 local time, a Piper PA-23, N4322P, landed at Shenandoah Valley Regional Airport, Staunton, Virginia. The pilot allowed the aircraft to drift to the left side of the runway prior to landing. The left propeller hit a runway light, and as the aircraft decelerated, the left wing hit a distance marker sign. Prior to landing the pilot had complained that the right throttle had stuck at 1500 rpm's, the right prop control was stiff, and the elevator trim was not functioning. Examination of the right engine controls found them stiff but workable. privacy data omitted Incident closed.

As the FAA filed it

NARRATIVE: ON JANUARY 18, 1997, AT 13:00 LOCAL TIME, A PIPER PA-23, N4322P, LANDED AT SHENANDOAH VALLEY REGIONAL AIRPORT, STAUNTON, VIRGINIA. THE PILOT ALLOWED THE AIRCRAFT TO DRIFT TO THE LEFT SIDE OF THE RUNWAY PRIOR TO LANDING. THE LEFT PROPELLER HIT A RUNWAY LIGHT, AND AS THE AIRCRAFT DECELERATED, THE LEFT WING HIT A DISTANCE MARKER SIGN. PRIOR TO LANDING THE PILOT HAD COMPLAINED THAT THE RIGHT THROTTLE HAD STUCK AT 1500 RPM'S, THE RIGHT PROP CONTROL WAS STIFF, AND THE ELEVATOR TRIM WAS NOT FUNCTIONING. EXAMINATION OF THE RIGHT ENGINE CONTROLS FOUND THEM STIFF BUT WORKABLE. ^PRIVACY DATA OMITTED^ INCIDENT CLOSED.

Other reports on N4322P · 1

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