N3607Y is a Cessna 210C. It is a fixed-wing single-engine aircraft with 4 seats, powered by a Cont Motor I0-470 series rated at 260 horsepower. The registration is active, with the registrant based in Haines, AK. Its standard airworthiness certificate was issued in Dec 1962. It has been registered to its current owner since Sep 2021. This page also carries 2 NTSB events.
2021
1962
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On January 14, 2018, about 1445 Alaska standard time, a Cessna 210 airplane, N3607Y, was substantially damaged when it was involved in an accident in Juneau, Alaska. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.
The pilot stated that, while approaching JNU for landing, he extended the landing gear; the nose gear extended fully, but the left and right main gear only partially extended and the landing gear position indicator light did not illuminate. He attempted to manually extend the gear by use of the emergency hand pump; however, after a few pumps, he felt a loss of pressure feedback in the handle and the landing gear failed to fully extend. He then extended the wing flaps, but no flap movement was evident. During the landing roll, the left and right main landing gear collapsed and the right wing tip and right horizontal stabilizer impacted the runway, resulting in substantial damage. The pilot noted hydraulic fluid leaking from under the airplane as it was subsequently removed from the runway.
Examination of the hydraulic system revealed that the right main landing gear hydraulic actuator (P/N 1280501-2, Electrol EA1614-2) was fractured about the barrel section adjacent to the end cap. (see Figure 1.)
Figure 1. Right main landing gear actuator exhibiting fractures.
A detailed examination was conducted at the National Transportation Safety Board Materials Laboratory. The actuator was partially disassembled, and a singular, thumbnail-shaped crack was present at the retainer clip groove. The fracture surface exhibited striations consistent with fatigue crack propagation when examined using a scanning electron microscope. Fractured surfaces outside of the fatigue crack area exhibited dimple rupture, consistent with an overstress fracture. The retaining ring groove revealed multiple small corrosion pits.
The airplane manufacturer issued a service letter (SE75-21) in 1975 that recommended that Electrol actuators in certain Cessna 210 airplanes be modified with an actuator repair kit during the next annual or 100-hour inspection. The instructions required disassembly, inspection, and replacement of certain internal parts. In 1976, the Federal Aviation Administration issued an airworthiness directive (AD 76-04-01) that mandated the service letter instructions for the actuator. In 2011, the manufacturer also issued a service manual Supplemental Inspection Number 32-10-01 that required visual inspection of the main landing gear actuators for cracks, wear, and corrosion at regular intervals. Due to limited maintenance records available, it could not be determined if the accident airplane had been maintained in accordance with the AD or supplemental inspections.
On July 11, 2015, about 1648 Alaska daylight time, a retractable landing gear-equipped Cessna 210 airplane, N3607Y, sustained substantial damage during landing at Juneau Airport (JNU), Juneau, Alaska. The pilot and passenger were uninjured. The airplane was registered to, and operated by, the pilot under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91 as a personal flight. Visual meteorological conditions prevailed at the time of the accident. No flight plan was on file.
During an interview with the National Transportation Safety Board (NTSB) investigator-in-charge on July 11, 2015, the pilot stated that while approaching the Hoonah Airport, Hoonah, Alaska, the flaps were set to 20 degrees down and the landing gear handle was selected to the down position. The nose gear fully extended and locked into place, but the left and right main landing gear extended about halfway and stopped. The landing gear selector was then placed back into the up position in an effort to cycle the landing gear. The pump was heard running, but the gear failed to move. The landing gear selector was placed again in the down position and in the interest of safety, the pilot decided to change the destination from the Hoonah Airport to the Juneau Airport where there was Aircraft Rescue and Fire Fighting (ARFF) equipment and personnel. He estimates that during the flight from Hoonah to Juneau, he pumped the landing gear emergency hand pump hundreds of times, but he never felt any resistance in the hydraulic lines.
During removal of the airplane from the runway, it was lifted with a crane so the landing gear could be physically pulled into place and secured with pins to prevent retraction. When the airplane was lifted and positioned in a level attitude, hydraulic fluid was observed leaking from the bottom of the airplane.
On August 5, 2015, an FAA air safety inspector from the Juneau Flight Standards District Office, along with a certified airframe and power plant mechanic, under the direction of the NTSB IIC, examined the airplane's hydraulic system. They hydraulic reservoir was serviced to a full level and the landing gear emergency hand pump was manipulated. A large leak was evident under the pilot seat. When the floor inspection panel was removed, the left main landing gear hydraulic actuator was discovered to be fractured at the end cap and along the side. The actuator was removed and sent to the NTSB Materials Laboratory in Washington, DC, for a more detailed examination by a Materials Research Engineer.
The hydraulic actuator (P/N 1280501-1, S/N 21058107) was cracked about the barrel section adjacent the endcap with a circumferential and a longitudinal component. Once the endcap was removed, a crescent fragment of the actuator barrel with the circumferential crack fell away. The fracture surface exhibited two thumbnail-shaped cracks, which were examined using a scanning electron microscope. The thumbnail region displayed striations consistent with fatigue crack propagation. Portions of the fracture surface outside of the fatigue crack revealed dimple rupture, consistent with overstress. The thumbnail-shaped fatigue cracks exhibited ratchet marks, consistent with multiple fatigue crack initiation. Examination of these initiation sites did not reveal any discernible material or mechanical defects. However, examination of the surface of the retaining ring groove did reveal multiple corrosion pits.
A detailed examination report including microscopic images is available in the public docket for this accident.
The closest weather reporting facility is Juneau Airport, Juneau. At 1553, an aviation routine weather report (METAR) from the Juneau Airport was reporting in part: wind from 120 degrees at 11 knots; sky condition, few at 500 feet above ground level (agl), broken at 2,700 feet agl, overcast at 5,500 feet agl; visibility 10 statute miles; light rain; temperature 60 degrees F; dewpoint 55 degrees F; barometric pressure 29.72 inHg.
The pilot did not complete and return the required NTSB Accident Reporting Form 6120.1.
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