N148Z

MINR
None

SHORT BROS SD3 60 SHERPAS/N: SH3428

Accident Details

Date
Thursday, October 13, 2016
NTSB Number
WPR17IA007
Location
Missoula, MT
Event ID
20161014X31149
Coordinates
46.916389, -114.090553
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the nose landing gear down-lock piston to engage due to paint accumulation, which resulted in a nose landing gear collapse during landing. Also causal was the failure of the facility that performed the painting to comply with manufacturer guidance regarding painting of the airplane.

Aircraft Information

Registration
Make
SHORT BROS
Serial Number
SH3428
Engine Type
Turbo-prop
Year Built
1998
Model / ICAO
SD3 60 SHERPASH36
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
39
FAA Model
SD3-60 SHERPA

Registered Owner (Current)

Name
USDA FOREST SERVICE
Address
3833 S DEVELOPMENT AVE
City
BOISE
State / Zip Code
ID 83705-5354
Country
United States

Analysis

On October 13, 2016, about 1645 mountain daylight time, a Short Bros SD3-60 Sherpa airplane, N148Z, sustained minor damage following a nose gear collapse during landing, at the Missoula International Airport (MSO) Missoula, Montana. The two airline transport pilots, were not injured. The airplane was registered to and operated by United States Department of Agriculture (USDA), as a public aircraft in support of the Forest Service. Visual meteorological conditions prevailed and a visual flight rules (VFR) flight plan was filed for the ferry flight which originated from Kingman Airport, Kingman, Arizona, about 1253.

The pilots reported that prior to landing, they had an unsafe nose gear indication. After multiple unsuccessful attempts to get the nose gear to extend and indicate that it was down and locked, they decided to come in for a landing. During the landing roll, as the airplane's nose was lowered, the nose gear collapsed, and the forward section of the bottom of the fuselage, made contact with the runway surface. Once the airplane came to a stop, both pilots egressed.

Examination of the airplane by the operator revealed minor damage on the underside of the fuselage.

The airplane was returning to MSO, on its first flight, after being re-painted by a vendor in Kingman, Arizona. According to the operator, examination of the nose gear revealed that it failed to lock in the extended position and collapsed during landing. The flight crew attempted to extend and lock the nose gear during the flight but were unsuccessful.

Post incident examination of the nose gear down-lock actuator piston (plunger), revealed that its chrome surface had been painted, which resulted in the locking piston not engaging, and prevented the locking of the nose gear during landing gear extension. The painting of the nose gear down-lock actuator piston was not observed by maintenance personnel or the flight crew on their pre-flight exterior checks.

The airplane manufacturer Shorts issued a SD3-60 Sherpa Service Information Letter (SIL) Sherpa L-23, in April 2007, titled: Servicing/Painting – Removal of masking material/paint from nose landing gear down-lock actuator piston after cleaning/painting operations. The SIL described a similar incident where the nose gear failed to lock in the down position, on the first flight after the airplane had been re-painted. The subsequent investigation revealed paint spray on the exposed chrome piston of the nose landing gear down-lock actuator. The SIL stated "to ensure that all masking material has been removed from the exposed piston after cleaning/painting, and that the piston is free from any paint or cleaning materials."

Additionally, the landing gear emergency accumulator was observed during the pre-flight checks to indicate below the specified pressure. The accumulator was serviced by maintenance to an adequate pressure, prior to takeoff. However, the pressure bled down during the incident flight, and when the emergency landing gear extension was used, the accumulator did not have adequate pressure. According to the operator's maintenance inspector, when activated, a fully serviced emergency accumulator forces the rapid application of hydraulic pressure into the system, however, according to the airplane's manufacturer, this is reliant on the main system hydraulic pressure being depleted so that the emergency pressure can change a control valve position. In this situation, the emergency pressure would be greater than the residual pressure of the failed main hydraulic system.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR17IA007