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|
Attributes | |
ACN | 786309 |
Time | |
Date | 200805 |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : zzz.airport |
State Reference | US |
Altitude | agl single value : 0 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Operator | general aviation : personal |
Make Model Name | Experimental |
Operating Under FAR Part | Part 91 |
Flight Plan | None |
Person 1 | |
Affiliation | other |
Function | oversight : pic |
Qualification | pilot : private |
Experience | flight time last 90 days : 29 flight time total : 273 flight time type : 74 |
ASRS Report | 786309 |
Events | |
Anomaly | aircraft equipment problem : critical |
Independent Detector | other flight crewa |
Resolutory Action | none taken : anomaly accepted |
Consequence | other |
Supplementary | |
Problem Areas | Aircraft |
Primary Problem | Aircraft |
Narrative:
Aircraft's rear (main) landing gear lock failed and the main gear collapsed on landing. The aircraft skidded on its keel (it's a seaplane) 100-200 ft to a stop. Nose gear remained down and locked throughout event. I believe it was caused by a too weak spring on the overcenter locking mechanism which will be replaced by a stronger spring. Prior to the event; the flight had been completely normal. Callback conversation with reporter revealed the following information: reporter stated both left and right main landing gears on his spencer amphibian aircar are cessna L-19 birddog spring gear legs. They are mounted to a 6.50 inch diameter tube that runs left to right inside the fuselage. Both main gears rotate together when the gear is raised or lowered; using a hand crank chain system drive sprocket. When the overcenter locking pin did not engage; the 3400 pound weight of the spencer forced the main landing gears to rotate aft; as if retracting.
Original NASA ASRS Text
Title: AN EXPERIMENTAL SPENCER AMPHIBIAN AIRCAR S-12-E REAR MAIN LANDING GEAR LOCK FAILED AND MAIN GEAR COLLAPSED ON LANDING.
Narrative: ACFT'S REAR (MAIN) LNDG GEAR LOCK FAILED AND THE MAIN GEAR COLLAPSED ON LNDG. THE ACFT SKIDDED ON ITS KEEL (IT'S A SEAPLANE) 100-200 FT TO A STOP. NOSE GEAR REMAINED DOWN AND LOCKED THROUGHOUT EVENT. I BELIEVE IT WAS CAUSED BY A TOO WEAK SPRING ON THE OVERCENTER LOCKING MECHANISM WHICH WILL BE REPLACED BY A STRONGER SPRING. PRIOR TO THE EVENT; THE FLT HAD BEEN COMPLETELY NORMAL. CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING INFO: REPORTER STATED BOTH LEFT AND RIGHT MAIN LANDING GEARS ON HIS SPENCER AMPHIBIAN AIRCAR ARE CESSNA L-19 BIRDDOG SPRING GEAR LEGS. THEY ARE MOUNTED TO A 6.50 INCH DIAMETER TUBE THAT RUNS LEFT TO RIGHT INSIDE THE FUSELAGE. BOTH MAIN GEARS ROTATE TOGETHER WHEN THE GEAR IS RAISED OR LOWERED; USING A HAND CRANK CHAIN SYSTEM DRIVE SPROCKET. WHEN THE OVERCENTER LOCKING PIN DID NOT ENGAGE; THE 3400 LB WEIGHT OF THE SPENCER FORCED THE MAIN LANDING GEARS TO ROTATE AFT; AS IF RETRACTING.
Data retrieved from NASA's ASRS site as of May 2009 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.