N360AX

ATA 7603

Part: CONTROLLER — SHEARED (RT ENGINE) · airframe 12,909 hrs · 6,331 cycles

AFTER START UP OF ENGINES, ACFT BEGAN TO TAXI AND THE PILOT REPORTED RT THROTTLE LEVER BECAME UNRESPONSIVE DURING TAXI. THEY RETURNED AND AFTER TROUBLESHOOTING IT WAS DETERMINED THE CONTROL ASSY, PN 7-43489-2, FOR THE RT ENGINE HAD SHEARED IN HALF, 6" FROM THE END AT THE ENGINE SIDE CONNECTION.

ATA 2612

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 11,101 hrs · 10,832 cycles

DURING CLIMB TO ALTITUDE THE RT ENGINE FIRE LIGHT ILLUMINATED MOMENTARILY. THROTTLE LEVER WAS RETARDED MOMENTARILY BUT LIGHT WENT OUT WITH NO OTHER INDICATIONS OR WARNINGS. AIRCRAFT FIRE DETECTION SYSTEM CURRENTLY BEING INVESTIGATED FOR CAUSE OF MOMENTARY LIGHT.

ATA 7260

Part: BEARING — FAILED (#3 ENG) · airframe 75,112 hrs · 30,845 cycles

DURING CLIMBOUT #3 ENGINE OIL STRAINER CLOGGED LIGHT CAME ON AND THROTTLE WAS REDUCED AND LIGHT WENT OUT. SHORTLY THERE AFTER OIL QTY DROPPED TO "0" AND ENGINE WAS SHUT DOWN PER COM PROCEDURES. ACCOMPLISHED FUEL DUMP INFLIGHT. REMOVED AND REPLACED RADIAL MID SHAFT AND TRANSFER GEAR BOX DRAIN LINE DUE TO RADIAL MIDSHAFT BEARING FAILURE. REMOVED AND REPLACED LUBE AND SCAVENGE PUMP AND MAIN OIL SCREEN. LK AND OPS CKD GOOD IAW GE MM.

ATA 5330

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,572 hrs · 30,379 cycles

AFT CARGO PIT FS 1921 LOWER REPAIR DOUBLER CORRODED FROM LONGERON 50L TO 50R. REMOVED FASTENERS. REMOVED CORROSION, TREATED, PRIMED, AND REINSTALLED DOUBLER IAW SRM 51-31-01.

ATA 5347

Part: SEAT TRACK — CORRODED (CABIN) · airframe 73,572 hrs · 30,379 cycles

A 20 INCH SECTION OF SEAT TRACK CORRODED INBOARD OF L2 DOOR. REPAIRED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00.

ATA 5330

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,572 hrs · 30,379 cycles

LOWER BEACON MOUNTING PLATE CORRODED. REMOVED, CLEANED, TREATED AND PRIMED MOUNTING PLATE. MOUNTING PLATE REINSTALLED.

ATA 5711

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 73,567 hrs · 30,377 cycles

DURING C-CHECK, FOUND LEFT WING AFT SPAR T-CAP FASTENER HOLE CORRODED AT STA XORS 582. CORROSION WAS REMOVED BY SPOTFACING FASTENER HOLE FROM LOWER SIDE OF HOLE AND INSTALLING A FILLER AND DOUBLER USING 7075-T6 .125 THICKNESS. MAJOR REPAIR APPROVED BY 8110-3.

ATA 5313

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,572 hrs · 30,379 cycles

STRINGER 49R AT FS 1986 CORRODED COMPLETELY THROUGH. INSTALLED NEW SECTION OF STRINGER IAW SRM 53-10-00.

ATA 5313

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,572 hrs · 30,379 cycles

LONGERON 49R BETWEEN FS 1975 AND FS 1986 EXFOLIATED AT AFT END. ACCOMPLISHED LONGERON REPAIR IAW SRM 53-10-00.

ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,572 hrs · 30,379 cycles

LEVEL 2 CORROSION FOUND ON FLOORBEAM STATION 1841 LEFT TO RIGHT DURING C-CHECK INSPECTION. REMOVED DAMAGED AREA ON LT SIDE FROM LBL 25-30 AND RT SIDE FROM LBL 25-35. FABRICATED L-ANGLE REPAIR AND FILLER IAW SRM 53-00-01.

ATA 5270

Part: SWITCH — MISALIGNED (PAX DOOR)

AIRCRAFT DEPARTED KMSP. UNABLE TO PRESSURIZE MAIN CABIN ABOVE 5000 FEET MSL. L1 DOOR WARNING INDICATION LIGHT ILLUMINATED AFTER TAKEOFF. L1 DOOR HAD APPROXIMATELY ONE-EIGHT INCH TO ONE-QUARTER INCH GAP BETWEEN DOOR AND DOOR FRAME. INITIATED PROCDEURES TO DUMP FUEL AND RETURN TO KMSP. INSPECTED DOOR STRUCTURE AND ROLLERS INCLUDING TRACKS WITH NO DEFECTS NOTED. L1 DOOR CLOSE LIMIT SWITH ADJUSTED AND DOOR OPERATED NORMAL.

ATA 2700

Part: PIVOT — BROKEN (HORIZONTAL STAB)

DURING ROUTINE ''A'' CHECK, A LUBE CARD WAS ISSUED FOR THE HORIZ STAB, WHICH INCLUDED THE HINGE FITTING PIVOT SHAFT. DURING THIS TASK, IT WAS NOTED THAT THE HINGE PIVOT SHAFT AND SLEEVE HAD MIGRATED APPROXIMATELY .125 INCH OUT OF THE HINGE FITTING. FURTHER INVESTIGATION AND INSPECTION REVEALED THE PIVOT SHAFT HAD FAILED. THE PIVOT SHAFT THREADED END SHEARED FROM THE SHANK. ALL OTHER HORIZONTAL STAB ATTACH POINTS WERE INSPECTED WITH NO FINDINGS. PRELIMINARY VISUAL INSPECTION OF THE SHEARED SHAFT INDICATE POSSIBLE METALLURGICAL OR MACHINING FLAWS, SINCE THE SEPARATION AT THE ROOT OF A MACHINED CHAMFER. A FOLLOW UP REPORT WILL BE GENERATED AS MORE INFO BECOMES AVAILABLE. THE TWO PIECES OF THE SHEARED SHAFT