N810FX

Part: FLEX HOSE — LEAKING (OXYGEN BOX) · airframe 34,787 hrs · 34,629 cycles

DURING PREFLIGHT OF FLIGHT 7500 MYR-CAE WITH AIRCRAFT N810FX, IT WAS DISCOVERED THAT THE F/O OXYGEN MASK WAS LEAKING. MAC MAINTENANCE TROUBLESHOT THE ISSUE TO THE OXYGEN LINE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,218 hrs · 34,101 cycles

AFTER TAKEOFF, LEAVING MAX RPM, RT ENGINE BEGAN SURGING. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO GSP UNEVENTFULLY. CLEANED CANNON PLUG CONNECTIONS ON RT ENGINE ECU. PERFORMED ENGINE RUN. UNABLE TO REPLICATE ENGINE SURGING. NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,043 hrs · 33,886 cycles

CAPT'S O2 MASK FAILS PREFLIGHT CHECK IN 100% MODE. MASK WILL NOT PRSSURIZE. REMOVED AND REPLACED CAPT'S O2 MASK BOX. LEAK AND OPS CHECKED GOOD.

Part: ROLLER — INOPERATIVE (EMERGENCY BRAKE) · airframe 32,942 hrs · 32,962 cycles

DURING POST FLIGHT INSPECTION, FOUND EMERGENCY BRAKE DIFFICULT TO ENGAGE AND GRINDING. REMOVED AND REPLACED SPRING LOADED PIN ROLLER ON EMERGENCY BRAKE. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 30,313 hrs · 30,887 cycles

LT LONGITUDINAL FLOORBEAM IS CRACKED AT FRAME 23D. REMOVED BEAM, FABRICATED NEW BEAM FROM BAC 1518-344 7075-T6, PO 201739. ALODINED, PRIMED, AND INSTALLED NEW BEAM IAW M7 IPC SUP 53-00-00 AND SRM 51-21-17, 51-27-28, AND 51-25-01.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 30,313 hrs · 30,887 cycles

LT LONGITUDINAL FLOORBEAM IS DAMAGED AT FRAME 23C. REMOVED BEAM, FABRICATED NEW BEAM FROM BAC 1518-344 7075-T6, PO 201739. ALODINED, PRIMED, AND INSTALLED NEW BEAM IAW M7 IPC SUPPLEMENT 53-00-00 AND SRM 51-21-17, 51-27-28, AND 51-25-01.

Part: PAN — DAMAGED (CARGO DOORWAY) · airframe 29,494 hrs · 30,202 cycles

AIRCRAFT HAD DAMAGE ON THE CARGO DOOR PAN. THE DAMAGE WAS REPAIRED IAW THE M7 DWG NR 72R47001-03 AND THE ACFT WAS RETURN TO SERVICE.

Part: STRINGER — DAMAGED (ZONE 200) · airframe 29,013 hrs · 29,811 cycles

FOUND DAMAGE ON STRINGER 1L BETWEEN FRAMES 23 AND 23A OUT OF LIMITS. REPLACED SECTION OF STRINGER, IAW SRM.

Part: WEB — CORRODED (ZONE 100) · airframe 29,013 hrs · 29,811 cycles

FOUND WEB, CORRODED OUT OF LIMITS. REPLACED WEB IAW SRM.

Part: STRINGER — DAMAGED (ZONE 200) · airframe 29,013 hrs · 29,811 cycles

FOUND DAMAGE ON STRINGER 2R BETWEEN FRAME 21 AND 22 OUT OF LIMITS. REPAIRED DAMAGED STRINGER, IAW SRM.

Part: STRINGER — CORRODED (FRAMES 32-33) · airframe 29,013 hrs · 29,811 cycles

CORROSION ON STRINGER 20R BETWEEN FRAMES 32 AND 33. REPLACED SECTION OF STRINGER IAW INSTRUCTION DT/S-124/14-21175.

Part: SKIN — CORRODED (ZONE 600) · airframe 29,013 hrs · 29,811 cycles

RT WING LOWER SKIN INTERNAL CORROSION AT FEEDER PUMP BETWEEN RIBS 4/5 ON LOWER PANEL, PN S57112378-200. BLENDED CORROSION IAW SRI DT/S-7009/13-21067 IDENTIFIED AS MAJOR REPAIR, FINAL APPROVAL IS ATR STRUCTURAL REPAIR APPROVAL SHEET DT/S-7009/13.

Part: STRINGER — CORRODED (FRAMES 16-17) · airframe 29,013 hrs · 29,811 cycles

CORROSION ON STRINGER 20R BETWEEN FRAMES 16-17. REPLACED SECTION OF STRINGER, PN S53371420206 IAW SRM.

Part: SEAT TRACK — CRACKED (FRAME 36) · airframe 29,013 hrs · 29,811 cycles

FOUND LEFT SEAT TRACK AT FRAME 36 CRACKED, R & R SEAT TRACK IAW SRM.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 29,013 hrs · 29,811 cycles

FOUND CORROSION ON FLOOR PANEL 214BF, OUT OF LIMITS. REPLACED FLOOR PANEL IAW SRM.

Part: PIN — OUT OF LIMITS (RT MLG) · airframe 28,775 hrs · 29,602 cycles

DISCOVERED A BASE METAL CHANGE THAT WAS OUT OF LIMITS ON RIGHT MAIN LANDING GEAR AFT PINTLE PIN PN D61000. THIS WAS DISCOVERED DURING AN ATTEMPT TO EXTEND THE TBO FOR THE LANDING GEAR COMPONENTS. THE RIGHT LANDING GEAR ASSEMBLY IS GOING TO BE SENT TO AN OVERHAUL FACILITY. THE FULL RIGHT MAIN LANDING GEAR P/N IS D2318900047161820.

Part: UNIVERSAL — OUT OF LIMITS (RT MLG) · airframe 28,775 hrs · 29,602 cycles

DISCOVERED A BASE METAL CHANGE THAT WAS OUT OF LIMITS ON RIGHT MAIN LANDING GEAR UNIVERSAL P/N D61036. THIS WAS DISCOVERED DURING AN ATTEMPT TO EXTEND THE TBO FOR THE LANDING GEAR COMPONENTS. THE RIGHT LANDING GEAR ASSEMBLY IS GOING TO BE SENT TO AN OVERHAUL FACILITY. THE FULL RIGHT MAIN LANDING GEAR P/N IS D2318900047161820.

Part: PIN — OUT OF LIMITS (LT MLG) · airframe 28,775 hrs · 29,602 cycles

DISCOVERED A BASE METAL CHANGE THAT WAS OUT OF LIMITS ON LEFT MAIN LANDING GEAR AFT PINTLE PIN P/N D61000. THIS WAS DESCOVERED DURING AN ATTEMPT TO EXTEND THE TBO FOR THE LANDING GEAR COMPONENTS. THE LEFT LANDING GEAR ASSEMBLY IS GOING TO BE SENT TO AN OVERHAUL FACILITY. THE FULL LEFT MAIN LANDING GEAR P/N IS D23189000-4-/-/-7-16-/-18-20.

Part: DOOR — DAMAGED (CARGO BAY) · airframe 28,366 hrs · 29,304 cycles

DURING A INSPECTION THE CARGO DOOR ON AIRCRAFT 810FX WAS FOUND DAMAGED. THE AIRCRAFT WAS FERRIED TO THE MAINTENANCE HANGAR. THE CARGO DOOR WAS REPLACED IAW ART72 JIC 52-31-00 RAI 10000.

Part: SMOKE DETECTOR — FALSE ACTIVATION (SMOKE WARNING) · airframe 26,296 hrs · 27,560 cycles

WHILE EN ROUTE FROM MEM TO BHM A SMOKE WARNING LIGHT ILLUMINATED. THERE WAS NO SMOKE PRESENT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MEM. A SMOKE DETECTOR WAS REMOVED AND REPLACED AND THE SYSTEM CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (ZONE 200) · airframe 25,868 hrs · 27,245 cycles

ON CLIMBOUT OF MEM, THE NR 2 ZONE SMOKE DETECTOR LIGHT ILLUMINATED. NO SMOKE WAS FOUND. THE PILOT DID A PRECAUTIONARY TURNBACK INTO MEM. THE SMOKE DETECTOR WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 25,672 hrs · 27,111 cycles

FOUND CORROSION INSIDE LEFT FUEL FEEDER TANK BETWEEN RIBS 4 AND 5. THERE WERE SEVERAL AREAS FROM STIFFENER 1 TO STIFFENER 10. CORROSION REMOVED AS PER SRM ATR72 CH 51-21-42. APPLIED TREATMENT TO NEUTRALIZE ANY HEDDIN CORROSION. PERFORMED FINAL BLEND OUT IAW SRM ATR72 CH 51-21-58. CONFIRMED THAT REMAINING THICKNESS OF BLEADED AREAS HAVE NOT CHANGED REF TABLE 1 OF ATR SRI NUMBER DO/TS-4240/08-10776. CONFIRMED THE ABSENCES OF CRACKS BY USE OF HF EDDY CURRENT. RESTORED PROTECTION OF REWORKED AREAS WITH ALODINE 1200 IAW SRM ATR72 CH 51-21-17 AND CH 51-21-28. REFERENCE ANA/E/4462/2008/E-001 AND ANA/E/4462/2008/E-003.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 25,470 hrs · 26,928 cycles

ON TAKEOFF ROLL, THE ANNUNCIATOR ILLUMINATED. ON CROSS CHECK THE F/O`S AIRSPEED INDICATOR INDICATED ZERO. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE F/O`S AIRSPEED INDICATOR WAS REPLACED AND OPS CHECK NORMAL. RETURNED AIRCRAFT TO SERVICE.

Part: PITOT TUBE — OBSTRUCTED (PITOT STATIC SYS) · airframe 25,470 hrs · 26,928 cycles

ON TAKEOFF ROLL, THE ANNUNCIATOR ILLUMINATED. ON CROSS CHECK THE F/O`S AIRSPEED INDICATOR INDICATED ZERO. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE NR 2 PITOT TUBE WAS REMOVED AND REPLACED THE SYSTEM CHECKED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MASTER CYLINDER — DEFECTIVE (BRAKE SYSTEM)

AFTER ARRIVAL, THE PILOT REPORTED THE CAPT SIDE RIGHT BRAKE INOPERATIVE. THE MASTER CYLINDER WAS REPLACED AND THE BRAKE LOW PRESSURE SIDE WAS BLED.

Part: FILTER — CLOGGED (FUEL SYSTEM) · airframe 25,296 hrs · 26,778 cycles

ON DEPARTURE FROM MEM-BHM FLT 8375, THE NR 1 ENGINE FUEL CLOG LIGHT ILLUMINATED. THE PIC DECIDED TO RETURN TO MEM. MAINTENANCE WAS NOT AVAILABLE IN BHM. MAINTENANCE REPLACED THE HP FUEL PUMP INLET FILTER. THE SYSTEM TESTED GOOD AND THE A/C WAS RETURNED TO SERVICE AND DEPARTED FOR BHM.

Part: METERING VALVE — MALFUNCTIONED (BRAKE SYSTEM) · airframe 25,321 hrs · 26,796 cycles

DURING TAXI ON INITIAL BRAKE CHECK, LOW RIGHT BRAKE PRESSURE WAS DISCOVERED ON BOTH THE PIC AND SIC SIDES. THE A/C RETURNED TO THE GATE. THE BRAKE METERING VALVE WAS REPLACED.

Part: FRAME — CORRODED (FUSLEAGE) · airframe 25,138 hrs · 26,661 cycles

DURING INSPECTION, CORROSION WAS FOUND ON FRAME 39 AT BL 0 REQUIRING A FRAME REPAIR. THE CORROSION ORIGINATED FROM A BLUE WATER SPILL AT SOMETIME IN THE PAST. THE LAV WAS PREVIOUSLY REMOVED DURING A RECONFIGURATION OF THE A/C. THIS IS AN ISOLATED CASE AND HAS NOT BEEN FOUND ON OTHER A/C IN OUR FLEET. REPAIR REF: ATR 72 SRM 53-61-40 FIG 110 SHEET 1.