N465QS

ATA 5510

Part: FITTING — CORRODED (ZONE 300) · airframe 11,223 hrs · 5,599 cycles

HORIZONTAL / VERTICAL STABILIZER ATTACH PIVOT FITTING HAS RUST BLEED FROM LT AND RT FITTINGS. COMPLIED WITH REPAIR OF HORIZONTAL / VERTICAL STABILIZER ATTACH PIVOT FITTINGS IAW ENGINEERING DISPOSITION TO USE DRAWING SE05455106

ATA 5753

Part: FITTING — CORRODED (FLAP TRACK) · airframe 11,223 hrs · 5,599 cycles

CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE ON LT FLAP TRACK FITTINGS A, B, C, D AND RT FLAP TRACK FITTINGS A, B, C, D. REQUESTED ENGINEERING DISPOSITION FOR REPAIRS. REMOVED CORROSION AND NDT AS REQUIRED. REPLACED UPPER/LOWER FITTINGS AND TRACKS THAT WERE OUT OF LIMITS AND INSTALLED REPAIR BUSHINGS AS REQUIRED. WORK DONE IAW DWGS 1159W20014, 1159W20223, 1159W40003, SE45811104 AND WORK ORDER CS467799.

ATA 2160

Part: UNKNOWN — UNKNOWN (COCKPIT TEMP)

AT FL 450 SMOKE IN CABIN AND COCKPIT. COCKPIT TEMP WOULD NOT GO ABOVE 67 DEGREES F AT A DUCT TEMP OF 176 DEGREES F. UNABLE TO DUPLICATE, COCKPIT TEMP CONTROLLER AND BOTH WATER SEPARATOR BAGS WERE REPLACED AS PRECAUTION. THE ACFT WAS FLOWN ON AN OPERATIONAL CHECK FLIGHT AND DISCREPANCY DID NOT REOCCUR. TEMP CONTROLLER P/N 607714-6-4 S/N 061C-2510 WATER SEPARATOR BAGS (2 EACH) P/N 832237-30. (S)

ATA 7830

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 4,124 hrs · 1,950 cycles

CREW RECEIVED HYDRAULIC FLUID LOW CASS MESSAGE, HYDRAULIC ACTUATOR FOR THRUST REVERSER WAS LEAKING.

ATA 2120

Part: MIST — DETECTED (CABIN) · airframe 4,023 hrs · 1,900 cycles

DURING FLIGHT, HEAVY PETROLEUM MIST WHEN ANTI ICE SELECTED ON.

ATA 3213

Part: ADAPTER — CORRODED (LT MLG AXLE) · airframe 3,826 hrs · 1,794 cycles

LEFT AXLE ADAPTER WAS FOUND TO HAVE CORROSION AND PITTING DURING INSPECTION.

ATA 3213

Part: ADAPTER — CORRODED (RT MLG AXLE) · airframe 3,826 hrs · 1,794 cycles

RIGHT AXLE ADAPTER WAS FOUND TO HAVE CORROSION AND PITTING DURING INSPECTION.

ATA 5610

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 3,216 hrs · 1,519 cycles

WINDSHIELD CRACKED.