19980714016659I

Incident · Minor damage

FAA incident report · Piper PA-24-250 · Columbus, OH · July 14, 1998

Date
July 14, 1998 · 18:44 local
Place
Columbus, OH
Airport
Rickenbacker Angb Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N5451P
Reported as
Piper PA24250
Reported engine
Lycoming O540A1A5
People aboard
5
Fatal injuries
0
Pilot’s flight hours
408 total28 in this make and model11 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.

The aircraft landed with the landing gear not in the down and locked postion. A cmh FSDO maintenance inspection of the landing gear system could not duplicate any problems. The landing gear safe indicator, green light, functioned properly during the test. The landing gear actuating motor functioned properly during the test. Due to damage, the landing gear was not connected to the actuating system. However, the gear was tested by manually swinging them from the down and locked position. No binding was noticed. The landing gear warning horn functioned properly during the test.

As the FAA filed it

THE AIRCRAFT LANDED WITH THE LANDING GEAR NOT IN THE DOWN AND LOCKED POSTION. A CMH FSDO MAINTENANCE INSPECTION OF THE LANDING GEAR SYSTEM COULD NOT DUPLICATE ANY PROBLEMS. THE LANDING GEAR SAFE INDICATOR, GREEN LIGHT, FUNCTIONED PROPERLY DURING THE TEST. THE LANDING GEAR ACTUATING MOTOR FUNCTIONED PROPERLY DURING THE TEST. DUE TO DAMAGE, THE LANDING GEAR WAS NOT CONNECTED TO THE ACTUATING SYSTEM. HOWEVER, THE GEAR WAS TESTED BY MANUALLY SWINGING THEM FROM THE DOWN AND LOCKED POSITION. NO BINDING WAS NOTICED. THE LANDING GEAR WARNING HORN FUNCTIONED PROPERLY DURING THE TEST.

Other reports on N5451P · 2

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