19961025038049I

Incident · Minor damage

FAA incident report · Piper PA-24-400 · Easton, PA · October 25, 1996

Date
October 25, 1996 · 10:30 local
Place
Easton, PA
Airport
Easton Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N8515P
Reported as
Piper PA24400
Reported engine
Lycoming IO720A1A
People aboard
1
Fatal injuries
0
Pilot’s flight hours
10,000 total1,000 in this make and model60 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 October 25, 1996, N8515P, a PA-24-400 aircraft landed gear up on runway 18 at Easton Airport, Easton, PA (N43). The pilot, Mr. William j. waldron stated that he placed the gear handle down but failed to check for the gear down and lock indication. The aircraft received minor damage and the pilot was uninjured. A landing gear swing was accomplished immediately after the incident and an in-depth gear swing and inspection of the landing gear system was conducted on October 29, 1996 and no malfunctions were evident on either of these occasions. It was noted that the landing gear warning horn was inoperative, but the gear functioned normally. privacy data omitted We consider this matter closed.

As the FAA filed it

NARRATIVE: ON OCTOBER 25, 1996, N8515P, A PA-24-400 AIRCRAFT LANDED GEAR UP ON RUNWAY 18 AT EASTON AIRPORT, EASTON, PA (N43). THE PILOT, MR. WILLIAM J. WALDRON STATED THAT HE PLACED THE GEAR HANDLE DOWN BUT FAILED TO CHECK FOR THE GEAR DOWN AND LOCK INDICATION. THE AIRCRAFT RECEIVED MINOR DAMAGE AND THE PILOT WAS UNINJURED. A LANDING GEAR SWING WAS ACCOMPLISHED IMMEDIATELY AFTER THE INCIDENT AND AN IN-DEPTH GEAR SWING AND INSPECTION OF THE LANDING GEAR SYSTEM WAS CONDUCTED ON OCTOBER 29, 1996 AND NO MALFUNCTIONS WERE EVIDENT ON EITHER OF THESE OCCASIONS. IT WAS NOTED THAT THE LANDING GEAR WARNING HORN WAS INOPERATIVE, BUT THE GEAR FUNCTIONED NORMALLY. ^PRIVACY DATA OMITTED^ WE CONSIDER THIS MATTER CLOSED.