Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 20001026SH005Cable Guard · inadequateDURING INITIAL INSPECTION OF THE AILERON INTERCONNECT CABLE QUADRANTS (RT AND LT) IAW CESSNA SB SB00-27-02, IT WAS DETERMINED THE REQUIRED RADIUS AROUND THE EDGE OF THE HOLE WHERE THE INTERCONNECT CABLE PASSES WAS NOT PRESENT. SUBSEQUENT INSPECTION OF THE INTSDR 20001026SH004Cable Housing · inadequateDURING INITIAL INSPECTION OF THE AILERON INTERCONNECT CABLE QUADRANTS (RT AND LT) IAW CESSNA SB SB00-27-02, IT WAS DETERMINED THE REQUIRED RADIUS AROUND THE EDGE OF THE HOLE WHERE THE INTERCONNECT CABLE PASSES WAS NOT PRESENT. SUBSEQUENT INSPECTION OF THE INTSDR 20000720SH019Engine · failedPILOT REPORTED ENGINE SURGING ON TAKEOFF WITH SIGNIFICANT FUEL FLOW FLUCTUATION WHICH WAS CORRECTED WITH A DECREASE IN ENGINE POWER BY ADJUSTMENT OF THE PROP CONTROL AND ACTIVATION OF THE STANDBY ELECTRIC FUEL PUMP. POST-GROUND RUNS DUPLICATED THE PROBLEM, BUSDR 20000720SH018Engine · failedPILOT REPORTED ENGINE SURGING ON TAKEOFF WITH SIGNIFICANT FUEL FLOW FLUCTUATION WHICH WAS CORRECTED WITH A DECREASE IN ENGINE POWER BY ADJUSTMENT OF THE PROP CONTROL AND ACTIVATION OF THE STANDBY ELECTRIC FUEL PUMP. POST-GROUND RUNS COULD NOT DUPLICATE THE PRSDR 20000802SH013Line · damagedDURING THE AIRCRAFT''S FIRST 100-HOUR INSPECTION, DISCOVERED FUEL LEAK AT FUEL SELECTOR VALVE AROUND FITTING ON FUEL LINE FROM SELECTOR TO LT HEADER TANK. UPON REMOVAL OF LINE, DISCOVERED DAMAGED FLARE. TOTAL AIRCRAFT TIME: 98.6 HRS. (X)SDR 20000518SH014Shroud · crackedDISCOVERED OIL LEAK IN ENGINE COMPARTMENT COMING FROM RIGHT SIDE PUSH ROD TUBE SHROUD ON NR 5 CYLINDER ASSEMBLY. ON FURTHER INSPECTION, TUBE WAS FOUND CRACKED APPROXIMATELY ONE INCH DIAGONALLY THEN EXTENDING AROUND THE CIRCUMFERENCE OF THE TUBE (APPROX HALF W
Other aircraft with N7281M · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N7281M now.