N197GB

Substantial
None

Rockwell 690S/N: 11282

Accident Details

Date
Monday, June 10, 2019
NTSB Number
CEN19LA168
Location
Jacksonville, FL
Event ID
20190611X81231
Coordinates
30.218889, -81.877220
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The overstress fracture of the roll pin in the nose landing gear (NLG) spacer assembly which caused interference between the nose wheel actuator rod and the left forward gear door actuating rods preventing the NLG to fully extend into the full down and locked position resulting in a nose gear collapse during landing.

Aircraft Information

Registration
Make
ROCKWELL
Serial Number
11282
Engine Type
Turbo-prop
Year Built
1975
Model / ICAO
690AC90
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
11
FAA Model
690A

Registered Owner (Current)

Name
REGISTRATION PENDING
Address
4500 E AVIATION WAY
City
SAFFORD
State / Zip Code
AZ 85546-9479
Country
United States

Analysis

On June 10, 2019, about 1846 eastern daylight time, a Rockwell 690A airplane, N197GB, was substantially damaged when it was involved in an accident near Jacksonville, Florida. The pilot and two crew members were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 135 firefighting flight.

One of the pilots reported that, while returning to the airport after a reconnaissance flight, he extended the landing gear, but the nose landing gear (NLG) position light did not illuminate. The crew cycled the gear, then completed the checklist for a gear malfunction; but were unable to resolve the discrepancy. The pilot advised the tower controller of their situation and requested a low approach to verify the position of the NLG. The tower controller told the crew that the landing gear appeared to be down. They requested a second flyby to allow a company representative to look; he also reported that the landing gear appeared down, but suggested diverting to another airport where crash rescue was available. The flight crew agreed and diverted. During the subsequent landing, the NLG collapsed.

Examination of the NLG assembly found that the roll pin installed in the spacer assembly was fractured. The fractured roll pin remained installed in the right and left sides of the spacer, which connects the nose wheel steering cylinder and the NLG strut. Metallurgical examination of the fractured roll pin revealed evidence of bending and shear stresses, which had resulted in an overstress fracture.

With the assistance of maintenance personnel, the NLG was cycled using the gear extension handle in the cockpit. As the NLG was lowered, the nose wheel cylinder and actuator arm interfered with the nose wheel well main frame and jammed; the nose wheel would not extend past its gear doors. The forward nose landing gear doors were reinstalled and the NLG was cycled again. The nose wheel actuator rod jammed on the left forward gear door actuating rods, matching impact marks observed on the actuating rods.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN19LA168