PLT OF AA5 SUFFERS CATASTROPHIC ENG FAILURE NEAR ZZZZ. LANDS ON THE BEACH ZZZ1 NE OF ARPT.

Date: 2004-05 · Aircraft: Cheetah; Tiger; Traveler AA5 Series

Anomalies: aircraft-equipment-problem-critical|conflict-ground-conflict|less-severe|deviation-discrepancy-procedural-published-material-policy|deviation-discrepancy-procedural-far|deviation-discrepancy-procedural-maintenance|ground-event-encounter-other-unknown|inflight-event-encounter-weather-turbulence|other-off-airport-landing

Synopsis

PLT OF AA5 SUFFERS CATASTROPHIC ENG FAILURE NEAR ZZZZ. LANDS ON THE BEACH ZZZ1 NE OF ARPT.

Narrative

THE ENG OF GRUMMAN TIGER (AA5B) FAILED DURING FLT. AFTER RUNNING ROUGHLY FOR ABOUT 15 MINS; THE ENG SEIZED. A FORCED LNDG WAS MADE ON THE BEACH APPROX 3 MI NE OF ZZZ. THIS EVENT OCCURRED APPROX 1 HR AND 10 MINS INTO A FLT THAT ORIGINATED AT ZZZ2. THE FLT WAS UNEVENTFUL. AFTER TURNING FOR THE FINAL LEG OF THE FLT; I NOTICED SHOWERS BTWN MYSELF AND ARPT. I ELECTED TO TURN DUE E; CROSS OVER THE NORTHERN END OF ANOTHER LCL ARPT AND THEN TURN S ALONG THE COAST; FLYING AT 1500 FT MSL. AS I TURNED S; I EXPERIENCED A DROP IN RPM FROM 2500 TO 2000 RPM. I IMMEDIATELY TURNED ON THE FUEL PUMP; ADJUSTED BOTH THROTTLE AND MIXTURE. THESE ACTIONS HAD NO EFFECT ON THE ROUGH RUNNING ENG. AT THAT POINT; I THOUGHT IT WAS POSSIBLY FOULED PLUGS AND PROCEEDED TO TRY TO ISOLATE THE MAGNETOS. THIS HAD NO EFFECT ON THE ENG. I THEN NOTICED THAT OIL PRESSURE WAS DROPPING AND SOME OIL DROPS ON THE CANOPY. DURING THIS TIME; I WAS ABLE TO INITIATE A SLIGHT CLB AT APPROX 100-200 FPM. MY AIRSPD WAS APPROX 90 KIAS. I CONTACTED ZZZ UNICOM AND ADVISED THAT THE ENG WAS RUNNING ROUGH AND LOSING OIL PRESSURE; BUT WAS CLBING. I ADVISED MY INTENTIONS WERE TO FLY ALONG THE COAST S AND THEN OVER THE WATERWAY TO LAND ON RWY 13 (THE WIND-FAVORED RWY). AFTER APPROX 10 MINS OF FLT AND AS I WAS APCHING THE N END OF ZZZ; THE ENG STOPPED. I IMMEDIATELY ATTEMPTED A RESTART. THE ENG TURNED OVER FOR 2-3 SECONDS AND THEN STOPPED. I NOTICED A PUFF OF WHITE SMOKE COMING OUT FROM THE FRONT R SIDE OF THE COWLING. I IMMEDIATELY ADVISED UNICOM OF THE SIT AND ADVISED I WOULD BE MAKING A BEACH LNDG. I THEN CONFIGURED THE ACFT FOR BEST GLIDE; SHUT THE FUEL OFF; AND OPENED THE CANOPY. I LEFT THE MASTER ON; BUT TURNED OFF ALL ELECTRONICS EXCEPT THE RADIOS TO ADVISE UNICOM OF POS. THE BEACH WAS SPARSELY POPULATED. I DID NOT SEE ANYONE ON THE BEACH EXCEPT FOR 1 BLUE CHAIR AT THE POINT I EXPECTED TO TOUCH DOWN. I ELECTED TO TOUCH DOWN ON THE TOP PORTION OF THE BEACH TO AVOID THE CHAIR AND ANY POTENTIAL INDIVIDUALS. THE ACFT TOUCHED DOWN AND ROLLED TO A STOP WITHOUT FURTHER INCIDENT. THE ROLLOUT WAS APPROX 330 FT. THERE WAS NO DAMAGE TO THE AIRFRAME. I EXITED THE ACFT AND WAITED FOR EMER SVCS TO ARRIVE. UPON INITIAL VISUAL INSPECTION; THE #3 CYLINDER WAS FOUND TO HAVE FAILED. THERE WAS EXTENSIVE DAMAGE TO THE CYLINDER; AS IT HAD SEPARATED INTO 2 DISTINCT PARTS. LATER INSPECTION REVEALED A HOLE HAD BEEN PUNCTURED IN THE FRONT L SIDE OF THE ENG BLOCK. UPON INSPECTION OF THE LOGS; THE ACFT WAS WITHIN ITS ANNUAL (DUE JUL 2004). THE ENG; A LYCOMING 0-360; WAS 100 HRS OVER ITS TBO (TIME BTWN OVERHAULS) OF 2100 HRS.

Source: NASA Aviation Safety Reporting System (public domain). Reports are voluntary submissions and are not verified by NASA.