SEA04LA162

NTSB accident investigation · Universal Moulded Pdts. Monocoach · Pullman, WA · August 17, 2004

Accident · No injuriesLimited investigationFinal report
Date
August 17, 2004, 09:30 local (16:30 UTC)
Place
Pullman, WA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Unknown
Aircraft
N11872Universal Moulded Pdts. Monocoach
Weather
Visual (VMC) · Day
Status
Completed · report January 24, 2005
Report
Approved by Office Director
Parties
Spokane FSDO
FAA report
20040817019379A
Case key
59930

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The failure of a landing gear oleo retaining nut safety clip (snap ring) at an unknown point in time, leading to the partial separation of the landing gear strut while in flight, and the full collapse of the strut during the subsequent landing. Factors include the grassy terrain that the pilot chose to execute the landing on.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionUnknown
Miscellaneous,dowel/pin - failureCause
Landing gear,main gear shock absorbing strut - separationCause
Gear collapsedLanding - roll
Landing gear,main gear strut - overload
Terrain condition - grassFactor

Analysis

During a landing, just as the aircraft's two main wheels touched the surface of the runway, it suddenly jerked to the side and started to veer from the runway heading. The pilot therefore immediately added power and pulled the aircraft off the ground. He then climbed out to an altitude where he could visually inspect the gear legs and evaluate his situation. When he looked at the gear legs, he discovered that the left main gear strut oleo had come out of its housing, and the gear strut structure was hanging from the aircraft by two of its attach points. He therefore circled the area for awhile, waiting for emergency vehicles to get in place at the airport prior to his attempt to land on the remaining main gear. Once the equipment was in place, he landed on the grass alongside of the paved runway. The aircraft touched down on the right main gear, and the pilot kept the other gear leg elevated as long as possible. Eventually, as the aircraft slowed, the left gear strut dug into the terrain and collapsed. A post-accident inspection of the gear system determined that the landing gear shock strut retaining nut safety clip (snap ring) had failed, thus allowing the shock strut retaining nut to back off of its threads. Without this retaining nut in place, the oleo piston was free to drop out of its housing, leaving the landing gear only partially attached to the fuselage.

Factual narrative

On August 17, 2004, approximately 0930 Pacific daylight time, a Universal Moulded Products Monocoach, N11872, experienced a gear collapse during the landing roll at Pullman-Moscow Regional Airport, Pullman, Washington. The commercial pilot and his passenger were not injured, but the aircraft, which is owned and operated by the pilot, sustained substantial damage. The 14 CFR Part 91 personal pleasure flight, which departed Porthill, Idaho, at 0745, was being operated in visual meteorological conditions. There was no report of an ELT activation. The aircraft was not on a flight plan.

According to the pilot, just as the aircraft's two main wheels touched the surface of the runway, it suddenly jerked to the side and started to veer from the runway heading. He therefore immediately added power and pulled the aircraft off the ground. He then climbed out to an altitude where he could visually inspect the gear legs and evaluate his situation. When he looked at the gear legs, he discovered that the left main gear strut oleo had come out of its housing, and the gear strut structure was hanging from the aircraft by two of its attach points. He therefore circled the area for awhile, waiting for emergency vehicles to get in place at the airport prior to his attempt to land on the remaining main gear. Once the equipment was in place, he landed on the grass alongside of the paved runway. The aircraft touched down on the right main gear, and the pilot kept the other gear leg elevated as long as possible. Eventually, as the aircraft slowed, the left gear strut dug into the terrain and collapsed.

A post-accident inspection of the gear system determined that the landing gear shock strut retaining nut safety clip (snap ring) had failed, thus allowing the shock strut retaining nut to back off of its threads. Without this retaining nut in place, the oleo piston was free to drop out of its housing, leaving the landing gear only partially attached to the fuselage.

Aircraft

Registration
N11872
Reported as
Universal Moulded Pdts. Monocoach
Category
Airplane
Serial number
5012
Airframe hours
1,904
Engine
Wright R760-8, 235 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
William C. Piper
Registered owner
Carsons Investments Inc.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · May 1, 2004 · 2 hours before
Departed
1S1 · Porthill, ID
Destination
PUW · Pullman, WA
Airport
PUW · Pullman-Moscow Reg., runway 23, 6,730 × 100 ft, grass/turf

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
74
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land, Single-engine sea, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Last flight review
August 11, 2004
Seat
Left
Flight hours
5,175 total · 10 in this make and model · 5,000 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 5 knots
Visibility
20 statute miles
Lowest ceiling
None
Temperature
75 °F

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.