20061210030319I

Incident · Minor damage

FAA incident report · Piper PA-23-250 · Fremont, OH · December 10, 2006

Date
December 10, 2006 · 16:00 local
Place
Fremont, OH
Airport
Sandusky County Regional
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N54077
Reported as
Piper PA23250
Reported engine
Lycoming IO540C4B5
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,500 total1,000 in this make and model10 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.

(-23) On approach, an extension of the flaps was initiated with no result (zero degrees) in flap travel. Suspecting a problem with the hydraulic system, the pilot privacy data omitted attempted to extend the main landing gear, which resulted in no action, thus confirming a hydraulic system faillure. The pilot then activated the compressed CO2 emergency gear extension system. The result of this procedure was a complete, and indicated, extension of both the nose and l/h main landing gear assemblies, with a partial, non-indicated, extension of the r/h main landing gear. During a fly-by it was witnessed by ground personnel that the r/h gear doors were opened and the gear assembly was still in the gear well. Upon final approach the engines were shut down, and propellers fully feathered. The pilot landed the aircraft on the nose and l/h main landing gear, until the airspeed bled off resulting in the aircraft step and r/h wing tip striking the runway. This caused the aircraft to make an uncontrollable right hand turn, entering the grass, striking a runway recong light, rotating 120 degrees and coming to rest approximately 150 feet from the right hand edge of the runway. No injuries were sustained.

As the FAA filed it

(-23) ON APPROACH, AN EXTENSION OF THE FLAPS WAS INITIATED WITH NO RESULT (ZERO DEGREES) IN FLAP TRAVEL. SUSPECTING A PROBLEM WITH THE HYDRAULIC SYSTEM, THE PILOT ^PRIVACY DATA OMITTED^ ATTEMPTED TO EXTEND THE MAIN LANDING GEAR, WHICH RESULTED IN NO ACTION, THUS CONFIRMING A HYDRAULIC SYSTEM FAILLURE. THE PILOT THEN ACTIVATED THE COMPRESSED CO2 EMERGENCY GEAR EXTENSION SYSTEM. THE RESULT OF THIS PROCEDURE WAS A COMPLETE, AND INDICATED, EXTENSION OF BOTH THE NOSE AND L/H MAIN LANDING GEAR ASSEMBLIES, WITH A PARTIAL, NON-INDICATED, EXTENSION OF THE R/H MAIN LANDING GEAR. DURING A FLY-BY IT WAS WITNESSED BY GROUND PERSONNEL THAT THE R/H GEAR DOORS WERE OPENED AND THE GEAR ASSEMBLY WAS STILL IN THE GEAR WELL. UPON FINAL APPROACH THE ENGINES WERE SHUT DOWN, AND PROPELLERS FULLY FEATHERED. THE PILOT LANDED THE AIRCRAFT ON THE NOSE AND L/H MAIN LANDING GEAR, UNTIL THE AIRSPEED BLED OFF RESULTING IN THE AIRCRAFT STEP AND R/H WING TIP STRIKING THE RUNWAY. THIS CAUSED THE AIRCRAFT TO MAKE AN UNCONTROLLABLE RIGHT HAND TURN, ENTERING THE GRASS, STRIKING A RUNWAY RECONG LIGHT, ROTATING 120 DEGREES AND COMING TO REST APPROXIMATELY 150 FEET FROM THE RIGHT HAND EDGE OF THE RUNWAY. NO INJURIES WERE SUSTAINED.

Other reports on N54077 · 1

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