N5114

Part: FUEL TANK — LEAKING (WING)

WING TANK (0) FILL ON AND VENTING FUEL FOR 3 MIN. 3400 LBS. FUEL. CREW REMINDED OF SL750-28-02 LETTER IN ALL AIRCRAFT LOG BOOKS REGARDING THIS CONDITION AND WHAT STEPS ARE NEEDED TO CORRECT THIS CONDITION. NO ACTION TAKEN. CONDITION IS NORMAL REGARDING THE LATE FILING OF THIS SDR, IT WAS DISCOVERED AS REPORTABLE, FOUND DURING AN AUDIT OF AIRCRAFT RECORDS.

Part: LATCH — UNSECURE (NLG DOOR)

NOSE DOOR OPEN R, CAS MESSAGE ILLUMINATED AFTER TAKEOFF. INSPECTED RIGHT NOSE DOOR AND FOUND LATCH OPEN. INSPECTED LATCH AND TEE BOLT FOR DEFECTS AND FOUND NONE. RELATCHED DOOR IAW PROCEDURES OUTLINED IN CESSNA MM. CAS MESSAGE EXTINGUISHED AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — FAILED (AFT CABIN)

EXIT LIGHT OVER EMERGENCY EXIT INOPERATIVE ON BATTERY. REPLACED AFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL TEST IN GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: TRANSMITTER — MALFUNCTIONED (VERTICAL STAB)

ON PREFLIGHT PRETEST SECONDARY TRIM FAILED SEVERAL TIMES IN THE NOSE UP DIRECTION. MOVEMENT STOPPED AND AMBER CAS 'SEC TRIM FALL' ILLUMINATED. REPLACED FAULTY STABILIZER POSITION TRANSMITTER. RIGGED AND TESTED PER CESSNA MM. OPERATIONAL CHECK IS GOOD AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE)

FOUND DURING INSPECTION TAILCONE BELTFRAME AT FUSELAGE STATION 691 IS CRACKED. RANDOM CRACKING ORIGINATING AT ASSEMBLY PROCESS OF TAILCONE. REPLACED BELTFRAME P/N 6712617-13. (M)

Part: ACTUATOR — FAULTY (RUDDER)

DURING CLIMB-OUT OF DTW, THE RUDDER LIMIT FAIL AT 24 PERCENT AMBER CAS MESSAGE ILLUMINATED. ALSO,THE PITOT HEATER FAIL SB AMBER CAS MESSAGE ILLUMINATED. REPLACED FAULTY LINEAR ACTUATOR. REPLACED FAULTY LOGIC MODULE. (M)

Part: COMPUTER — MALFUNCTIONED (PITCH TRIM)

PITCH FEEL FAIL LIGHT CAME ON, COULD NOT EXTINGUISH. SYSTEM LOCKUP. RESET PITCH FEEL SYSTEM, CLEARED EICAS FAIL MESSAGE. OPERATION RETURNED TO NORMAL.

Part: B-NUT — LOOSE (HYDRAULIC LINE)

TOTAL LOSS OF (A) HYDRAULIC SYSTEM FLUID. B-NUT ON LINE ASSEMBLY LOOSENED AND BACKED OFF DUE TO INCORPORATION OF SB. FURTHER INSTALLATIONS OF THIS BULLETIN HAVE BEEN TEMPORARILY TERMINATED BY MFG. SECURED B-NUT, SERVICED (A) HYDRAULIC SYSTEM. SERVICED EMERGENCY GEAR AND BRAKE BOTTLE WITH NITROGEN PER MFG MM.

Part: SWITCH — BENT (CABIN DOOR)

DOOR LIGHT WONT EXTINGUISH. MALFUNCTION OF CABIN DOOR WARNING SYSTEM. STRAIGHTENED FORWARD LOWER DOOR SWITCH PLUNGER, OPS CHECK NORMAL.

Part: MODULE — FAILED (E/E BAY)

PRIOR TO TAXI THE CREW NOTED AND AMBER CONFIG MISMATCH CAS MESSAGE. FAILED NR 2 CONFIGURATION MODULE. REPLACED NR 2 CONFIGURATION MODULE PER AMM. OPERATIONAL CHECK IS GOOD.

Part: BATTERY — OVERTEMP (RIGHT)

FOUND RIGHT BATTERY OVERTEMPED 75 DEGREES CELSIUS, SHUT OFF BATTERY AND RETURNED TO DTW. REPLACED BATTERY, CLEANED TEMP SENSOR CONNECTOR. (M)

Part: SENSOR — FAULTY (NR 1 BATTERY) · airframe 1,826 hrs

AGC - FLT 14740 - AFTER TAKEOFF WHILE IN CRUISE, CREW REPORTED THE NR 1 BATTERY AS INDICATING AN OVERHEAT CONDITION. THE CREW ISOLATED THE BATTERY WITH THE BATTERY SWITCH AND MONITORED THE TEMPERATURE PER THE EMERGENCY CHECK LIST. THE TEMPERATURE CONTINUED TO RISE AND THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT WAS, WITHOUT INCIDENT, LANDED AT THE PITTSBURGH. APPARENT CAUSE: FAULTED BATTERY. BATTERY DEFERRED AND SECURED PER THE MEL AND REPLACED AT DWG UPON ARRIVAL. (X)

Part: COMPUTER — FAILED (RT TE FLAP SYS) · airframe 1,807 hrs

KDTW - FLT 14223 - FLAPS FAILED AFTER TAKEOFF. FAILED RIGHT FLAP POSITION RESOLVER. REPLACED RIGHT FLAP RESOLVER, RIGGED AND CHECKED FLAPS IAW CESSNA CITATION X MM. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. (X)

Part: STRUT — MALFUNCTION (NLG)

THE AIRCRAFT DEPARTED DTW AND ON CLIMB-OUT, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION. THE AIRCRAFT RETURNED TO DTW AND MAINTENANCE WAS ABLE TO DUPLICATE. UNDER CESSNA'S RECOMMENDATION, NEW SB 750-32-05 AND SB 750-32-10 INCORPORATED TO ELIMINATE PROBLEMS IN NOSE STRUT EXTENSION.