20040817019379A

Accident · Substantial damage

FAA accident report · Unipro MONOCOACH · Pullman/Moscow, WA · August 17, 2004

Date
August 17, 2004 · 09:35 local
Place
Pullman/Moscow, WA
Airport
Pullman - Moscow Regional
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N11872
NTSB investigation
NTSBSEA04LA162
Reported as
Unipro Monocoach
People aboard
2
Fatal injuries
0
Pilot’s flight hours
7,000 total11 in this make and model40 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) This aircraft landed at the Pullman, WA airport with the left hand landing gear dangling from the aircraft. The pilot stated that the landing was as slow as possible and on the right hand wheel. At a speed below 15 miles per hour, the left side of the aircraft settled to the sod further damaging the left gear, allowing the propeller to contact the ground, and causing the forward spar in the left wing to break near the upper strut attach point. The retaining nut which holds the piston was allowed to turn off it's threads when the nut retaining clip failed at the juncture of the nut and piston threads. When this nut was free of the piston, the piston came out of it's strut allowing the gear (left) to dangle under the aircraft attached by the rear and forward gear mounting attachments on the lower longerons.

As the FAA filed it

(-23) THIS AIRCRAFT LANDED AT THE PULLMAN, WA AIRPORT WITH THE LEFT HAND LANDING GEAR DANGLING FROM THE AIRCRAFT. THE PILOT STATED THAT THE LANDING WAS AS SLOW AS POSSIBLE AND ON THE RIGHT HAND WHEEL. AT A SPEED BELOW 15 MILES PER HOUR, THE LEFT SIDE OF THE AIRCRAFT SETTLED TO THE SOD FURTHER DAMAGING THE LEFT GEAR, ALLOWING THE PROPELLER TO CONTACT THE GROUND, AND CAUSING THE FORWARD SPAR IN THE LEFT WING TO BREAK NEAR THE UPPER STRUT ATTACH POINT. THE RETAINING NUT WHICH HOLDS THE PISTON WAS ALLOWED TO TURN OFF IT'S THREADS WHEN THE NUT RETAINING CLIP FAILED AT THE JUNCTURE OF THE NUT AND PISTON THREADS. WHEN THIS NUT WAS FREE OF THE PISTON, THE PISTON CAME OUT OF IT'S STRUT ALLOWING THE GEAR (LEFT) TO DANGLE UNDER THE AIRCRAFT ATTACHED BY THE REAR AND FORWARD GEAR MOUNTING ATTACHMENTS ON THE LOWER LONGERONS.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.