ASN Wikibase Occurrence # 292157
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| Date: | Thursday 22 June 2006 |
| Time: | 11:30 LT |
| Type: |  Cessna R182 |
| Owner/operator: | Private |
| Registration: | N6124T |
| MSN: | R18201911 |
| Total airframe hrs: | 3010 hours |
| Engine model: | Lycoming O-540-J3C5D |
| Fatalities: | Fatalities: 0 / Occupants: 1 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | Lebanon, Tennessee -
 United States of America
|
| Phase: | Unknown |
| Nature: | Ferry/positioning |
| Departure airport: | Jackson-Hawkins Field, MS (HKS/KHKS) |
| Lebanon, TN (M54) | |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
The pilot stated that upon arrival at the destination airport he completed the before landing checklist. He activated the landing gear lever, the nose gear extended; however the main landing gear did not extend. The pilot completed the landing gear malfunction procedures with negative results. The pilot contacted personnel on the ground over the UNICOM radio frequency, entered left traffic, and made a low pass down the runway for ground personnel to observe the landing gear. The ground personnel informed the pilot the nose landing gear appeared to be extended, and the main gear was "dangling." The pilot remained in left closed traffic, landed, and the airplane went off the left side of the runway during landing roll out. Examination of the landing gear well by the pilot revealed the presence of hydraulic fluid on the airframe. The registered owner stated the airplane had an annual inspection on November 7, 2005, and had not been flown except for the accident flight. The airplane was recovered from the accident site to a hangar and the airplane was placed on jacks. The airplane seats and main gear actuator access plate were removed to locate the origin of the hydraulic leak. The hydraulic reservoir was serviced and the hydraulic system was pressurized. Hydraulic fluid was observed exiting the right gear hydraulic down line. The screw penetrated the hydraulic down line resulting in a complete loss of hydraulic fluid in the down line and failure of the main landing gear to extend.
Probable Cause: Improper maintenance by other maintenance personnel resulting in the puncture of the landing gear hydraulic down line and the failure of the main landing gear to extended on landing.
Accident investigation:
 |
|
Sources:
NTSB ATL06CA097
History of this aircraft
Other occurrences involving this aircraft
| 27 June 1987 | N6124T | Fredrick Harold | 0 | Deming, NM | |
sub |
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 08-Oct-2022 15:09 | ASN Update Bot | Added |
Corrections or additions? ... Edit this accident description
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