ASN Wikibase Occurrence # 198950
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Date: | Sunday 18 September 2016 |
Time: | 15:00 |
Type: | Seawind 3000 |
Owner/operator: | Private |
Registration: | N57TJ |
MSN: | 52 |
Year of manufacture: | 2012 |
Total airframe hrs: | 132 hours |
Engine model: | Lycoming AEIO540-L1B5 |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Renton, WA -
United States of America
|
Phase: | Landing |
Nature: | Private |
Departure airport: | Lakeport, CA (1O2) |
Destination airport: | Renton Airport, WA (RNT/KRNT) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The private pilot was conducting a cross-country personal flight. He reported that, after arriving at his destination and trying to ensure that the airplane was configured for the water landing, he observed that the right main landing gear (MLG) indicator light was off and that the hydraulic pressure read 0. The pilot then attempted to retract the right MLG several times to no avail. He chose to fly to a nearby airport with a paved runway, where the tower controller confirmed that the right MLG was extended but that the left MLG and nose landing gears were retracted. The pilot attempted to use the backup manual hydraulic pump and abrupt maneuvers to extend the remaining landing gear to no avail. The pilot chose to land on the runway with the landing gear partially retracted. The airplane touched down on the runway with the right MLG first. The pilot held the left wing off the runway as long as possible, but then the wing touched the runway, and the airplane veered off the runway surface. The airplane slid along the grass, impacted an airport sign and light, spun 180°, and then came to a rest.
Postaccident examination of the airplane revealed that a hydraulic leak had originated from a cracked flare in a hydraulic line fitting, which caused the hydraulic fluid to leak, decreased the hydraulic pressure to 0, and prevented the landing gear system from fully extending or retracting.
Probable Cause: The failure of the landing gear system to either fully retract or extend due to a cracked hydraulic fitting flare, which resulted in the loss of hydraulic pressure.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | WPR16LA187 |
Status: | Investigation completed |
Duration: | |
Download report: | Final report |
|
Sources:
NTSB
History of this aircraft
Other occurrences involving this aircraft Location
Revision history:
Date/time | Contributor | Updates |
19-Aug-2017 16:04 |
ASN Update Bot |
Added |
15-Sep-2023 19:11 |
harro |
Updated |
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