CONCHAS DAM, NM, USA
N93272
CESSNA A185F
THE AIRPLANE WATERLOOPED DURING THE TAKEOFF RUN AFTER NEARLY WATERLOOPING ON THE PREVIOUS LANDING. POSTACCIDENT EXAMINATION DISCLOSED THE LANDING GEAR CABLE WAS IMPROPERLY RIGGED, ALLOWING THE LEFT AFT PONTOON WHEEL TO DEPLOY. MAXIMUM RPM COULD NOT BE ATTAINED BECAUSE THE PROPELLER GOVERNOR WAS NOT PROPERLY ADJUSTED. A REVIEW OF THE ACCIDENT VIDEO TAPE REVEALED AIRCRAFT HAD ATTAINED SUFFICIENT FLYING SPEED. PILOT DID NOT DEPLOY TAKEOFF FLAPS.
LANDING GEAR LOCKING MECHANISM LOOSE, LANDING GEAR WHEEL DEPLOYED INADVERTENTLY, AND MAINTENANCE ALIGNMENT NOT PERFORMED. FACTORS WERE: PROPELLER GOVERNOR UNDERSPEED, MAINTENANCE ADJUSTMENT NOT CORRECTED, AND LOWERING OF FLAPS NOT PERFORMED.
Source: NTSB Aviation Accident Database
Aviation Accidents App
In-Depth Access to Aviation Accident Reports
