N825HK

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 38,692 hrs · 32,240 cycles

DURING CRUISE, BAGGAGE SMOKE CASS MESSAGE, MASTER WARNING, BAG SMOKE LIGHT TURNED ON, LATER EXTINGUISHED. AIRCRAFT LANDED AT KAUS WITHOUT INCIDENT. BAGGAGE COMPARTMENT WAS INSPECTED WITH NO EVIDENCED OF FIRE OR SMOKE. MAINTENANCE TROUBLESHOOTING PROBLEM, WILL REPORT FINDINGS WHEN AVAILABLE. MAINTENANCE COULD NOT DUPLICATE THE REPORTED PROBLEM. REMOVED AND REPLACED THE FORWARD SMOKE DETECTOR IN ACCORDANCE WITH THE EMB-145 AMM 26-15-01 AS PRECAUTIONARY MAINTENANCE. SYSTEM OPERATIONAL CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 38,671 hrs · 32,222 cycles

FLIGHT KAUS - KTUS“ BAGGAGE SMOKE” MASTER WARNING MESSAGE ILLUMINATED ON EICAS WHILE IN CRUISE AT FL 280. CREW FOLLOWED QRC AND DISCHARGED BAGGAGE COMPARTMENT FIRE EXTINGUISHER BOTTLES. DECLARED AN EMERGENCY AND DIVERTED TO KELP AND LANDED WITHOUT INCIDENT. FIRE DEPARTMENT INSPECTED BAGGAGE COMPARTMENT AND FOUND NO EVIDENCE OF FIRE OR SMOKE. MAINTENANCE FOLLOWED THE FIM REFERENCE: 26-15-00-810-805-A. THIS LEAD TO A TRANSITORY CONDITION OF THE BAGGAGE SMOKE DETECTION SYSTEM ELECTRICAL CIRCUIT (WM 26-15-50). CLEANED BOTH SMOKE DETECTORS AND PERFORMED OPERATIONAL CHECK OF SYSTEM IAW AMM 26-15-00-700-804-A. SYSTEM CHECKED GOOD. BAGGAGE COMPARTMENT FIRE EXTINGUISHER BOTTLES WERE REPLACED AND AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — FAULTED (SMOKE DETECTION) · airframe 38,486 hrs · 32,072 cycles

AFTER TAKEOFF, CREW RECEIVED A LAVATORY SMOKE CDS MESSAGE. AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MECHANIC ON BOARD FLIGHT REPORTED NO SMOKE IN LAVATORY OR ANY UNUSUAL ORDERS. MAINTENANCE TROUBLESHOT AND FOUND THE LAVATORY SMOKE PANEL AT FAULT. REMOVED AND REPLACED THE PANEL. AIRCRAFT RETURNED TO SERVICE.

Part: ACM — FAILED (RIGHT) · airframe 38,483 hrs · 32,068 cycles

AFTER TAKEOFF, CREW RECEIVED A NR 2 PACK 2 OVERLOAD AMBER CAS MESSAGE. FLIGHT ATTENDANT HEARD A LOUD BANG AND SMELLED ELECTRICAL SMOKE. CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPORTED THE RIGHT AIR CYCLE MACHINE HAD FAILED. THE ACM WAS REPLACED.

Part: ACM — FAILED (RIGHT) · airframe 38,448 hrs · 32,038 cycles

FLIGHT ATTENDANT REPORTED THAT SMOKE WAS IN THE PASSENGER CABIN, AS THE AIRCRAFT WAS PASSING THROUGH 6000 FT. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FIM 21-20-00 AND FOUND THE RIGHT AIR CONDITIONING PACK TO BE FAULTY. REMOVED AND REPLACES THE RIGHT AIR CYCLE MACHINE. AIRCRAFT RETURNED TO SERVICE.

Part: A/C PACK — SMOKE (RIGHT) · airframe 38,448 hrs · 32,038 cycles

FLIGHT ATTENDANT REPORTED THAT SMOKE WAS IN THE PASSENGER CABIN AS THE AIRCRAFT WAS PASSING THROUGH 6000 FT. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE FOLLOWED THE AIRCRAFT FIM 21-20-00 AND FOUND RIGHT AIR CONDITIONING PACK TO BE FAULTY.

Part: SWITCH — FAILED (CABIN PRESSURE) · airframe 38,210 hrs · 31,837 cycles

RETURNED DUE TO A LOSS OF CABIN PRESSURIZATION AT FL330, CAPTAIN NOTED RISING CABIN ALTITUDE. DONNED OXYGEN MASKS, DESCENDED TO 10,000. CABIN ALTITUDE REACHED 11,000 WITH ASSOCIATED WARNINGS BEFORE FINALLY STARTING TO GO DOWN. MAINTENANCE PERFORMED FIM 21-51-00 STEP 5 (1-15). R & R THE NR 2 PACK PUSHBUTTON SWITCH IAW AMM 20-13-04. OPS CHECKED GOOD. TORQUED NUMEROUS CLAMPS ON THE NR 2 PACK IAW AMM 21-51-02. LEAK CHECKED GOOD. PERFORMED AN AIRCRAFT PRESSURIZATION LEAK TEST IAW AMM 21-31-00. LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (ROW 12) · airframe 36,183 hrs · 29,794 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 12. MAINTENANCE REPLACED EMERGENCY LIGHT, OPS CHECKED GOOD.

Part: SKIN — CRACKED (RT WING) · airframe 36,183 hrs · 29,794 cycles

RIGHT WING LOWER SKIN HAS CRACK BETWEEN FORWARD 2 HI-LOCKS SECURING NR 5 RIB TO WING SKIN. PERFORMED MAJOR REPAIR TO LOWER RT WING SKIN IAW EO EMB145-57-005-R1, ETD2015-145-083959 AND TI-145-15-239, REV.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,125 hrs · 29,745 cycles

AFT OVERWING EXTERIOR FLOOD LIGHT NR 5 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,274 hrs · 29,028 cycles

RIGHT OVERWING EXTERIOR EMERGENCY LIGHT NR 6 IS INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,274 hrs · 29,028 cycles

LEFT OVER WING EXTERIOR EMERGENCY LIGHT NR 5 IS INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECK GOOD.

Part: CLAMP — LOOSE (BLEED DUCT) · airframe 34,875 hrs · 28,677 cycles

DURING CLIMB, BLEED LEAK INDICATED ON EICAS. RETURNED TO DEPARTURE. MAINTENANCE INSPECTED AND FOUND LOOSE CLAMP ON DUCT FROM PRE-COOLER TO ENGINE BLEED VALVE, RESECURED CLAMP AND OPS AND LEAK CHECK GOOD.

Part: PRECOOLER — INOPERATIVE (BLEED AIR) · airframe 34,838 hrs · 28,642 cycles

NR 1 BLEED OVERTEMP IN FLT IN ICING CONDITION DURING CLIMB, RETURNED TO DEPARTURE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 PRE-COOLER, OPS CHECK GOOD.

Part: FILTER — DIRTY (BLEED AI) · airframe 34,578 hrs · 28,404 cycles

ENG 1 AND ENG 2 BLEED OVER TEMP ON EICAS DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND CLEANED FAN AIR FILTERS, OPS CHECKED GOOD.

Part: BRACKET — CORRODED (ZONE 500) · airframe 17,896 hrs · 16,460 cycles

RIGHT INBD L/E HAS A CRACKED FAIRING BRACKET. R & R STRIP ASSY.

Part: CONTROL CABLE — CORRODED (ZONE 500) · airframe 17,896 hrs · 16,460 cycles

LEFT AILERON CONTROL CABLES ARE WORN BEYOND LIMITS. R & R CABLE.

Part: SILL — CORRODED (ZONE 100) · airframe 17,896 hrs · 16,460 cycles

RIGHT SILL AT FR 41-47 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: SILL — CORRODED (ZONE 100) · airframe 17,896 hrs · 16,460 cycles

LEFT SILL AT FR 48-52 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: GUSSET — CORRODED (ZONE 100) · airframe 17,896 hrs · 16,460 cycles

RT GUSSET AT FR 46-52 IS CORRODED BEYOND LIMITS. R & R GUSSET.

Part: SILL — CORRODED (ZONE 100) · airframe 17,896 hrs · 16,460 cycles

SILL FWD OF SERVICE DOOR CORRODED BEYOND LIMITS. R & R SILL.

Part: SILL — CORRODED (ZONE 100) · airframe 17,896 hrs · 16,460 cycles

LEFT SILL AT FR 42-48 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: PANEL — CORRODED (ZONE 100) · airframe 17,896 hrs · 16,460 cycles

PANEL AT END OF CTR BEAM AT STA 23 IS CORRODED BEYOND LIMITS. R & R PANEL.

Part: SILL — CORRODED (ZONE 100) · airframe 17,896 hrs · 16,460 cycles

RIGHT SILL AT FR 36-41 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: CONTROL CABLE — CORRODED (AILERONS) · airframe 17,896 hrs · 16,460 cycles

AILERON CONTROL CABLES ARE WORN BEYOND LIMITS. R & R CABLES.

Part: CONTROL CABLE — CORRODED (ZONE 100) · airframe 17,896 hrs · 16,460 cycles

AILERON CONTROL CABLES ARE WORN BEYOND LIMITS. R & R CABLES.

Part: CONTROL CABLE — CORRODED (AILERONS) · airframe 17,896 hrs · 16,460 cycles

AILERON CONTROL CABLES ARE WORN BEYOND LIMITS. R & R CABLES.

Part: CONTROL CABLE — CORRODED (AILERONS) · airframe 17,896 hrs · 16,460 cycles

AILERON CONTROL CABLES ARE WORN BEYOND LIMITS. R & R CABLES.

Part: SILL — CORRODED (ZONE 100) · airframe 17,896 hrs · 16,460 cycles

SERVICE DOOR SILL CORRODED BEYOND LIMITS. R & R SILL.

Part: CONTROL CABLE — CORRODED (ZONE 500) · airframe 17,896 hrs · 16,460 cycles

LEFT AILERON CONTROL CABLES ARE WORN BEYOND LIMITS. R & R CABLE.

Part: SILL — CORRODED (ZONE 100) · airframe 17,896 hrs · 16,460 cycles

RT SILL AT FR 47-52 IS CORRODED BEYOND LIMITS. R & R SILL.

Part: ANGLE — CORRODED (ZONE 100) · airframe 17,896 hrs · 16,460 cycles

U SHAPE ANGLE UNDER PAX THRESHOLD DOOR CORRODED BEYOND LIMITS. R & R SHAPE.

Part: ANGLE — CORRODED (ZONE 100) · airframe 17,896 hrs · 16,460 cycles

U SHAPE ANGLE UNDER PAX THRESHOLD DOOR CORRODED BEYOND LIMITS. R & R SHAPE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 17,924 hrs · 13,082 cycles

PRE FLT 5545 - STL - EMERGENCY LIGHTING FLOOR STRIPS INOPERATIVE. MAINTENANCE RESEATED A LOOSE CONNECTOR TO THE LIGHT STRIP. SYSTEM OPS CHECKED GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 17,794 hrs · 12,976 cycles

FLT 5530 - STL - CREW REPORTED RECEIVING A SPS ADVANCED AND FLAP FAIL MESSAGE ON THE EICAS DURING CLIMBOUT. FLAP INDICATION SHOWED AMBER DASHES. MAINTENANCE RESET THE FLAP SYSTEM AND PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM WITH NO DEFECTS NOTED.

Part: DOOR — LACK OF LUBE (PAX DOOR) · airframe 17,772 hrs · 12,957 cycles

POST FLT NR 5542 - STL - AIRCRAFT DOOR IS DIFFICULT TO CLOSE. MAINTENANCE CLEANED AND LUBED THE PASSENGER DOOR. OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 16,218 hrs · 11,721 cycles

POST FLT NR 5522 - STL - PAX DOOR DIFFICULT TO OPEN. MAINTENANCE LUBRICATED MAIN DOOR ROLLERS AND CLEANED ACTUATING CAMS. NO FURTHER FAULTS NOTED.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,615 hrs · 11,239 cycles

PRE FLT 5587 - STL - EMERGENCY LIGHTS INOP THROUGHOUT THE CABIN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPS CHECKED GOOD.

Part: HEATER — ODOR (WINDSHEILD HEAT) · airframe 15,245 hrs · 10,958 cycles

FLT NR 5576 - STL - STRONG ODOR IN COCKPIT WHEN WINDSHIELD HEAT NR 2 IS SELECTED ON. MAINTENANCE REMOVED AND REPLACED COCKPIT WINDSHIELD, OPS CHECK GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (AIRSTAIRS) · airframe 15,065 hrs · 10,822 cycles

PRE FLT NR 5493 - STL - EMERGENCY LIGHT ON HAND RAIL HINGE OF AIRSTAIRS INOP. MAINTENANCE DEFERRED LIGHT PER MEL.

Part: UNKNOWN — UNKNOWN (ENGINE) · airframe 14,809 hrs · 10,637 cycles

FLT NR 5486 - DEN - E2 NO MARGIN MSG. MAINTENANCE PERFORMED ENGINE RUN, COULD NOT REPRODUCE PROBLEM AT THIS TIME ENGINE STAYED WITHIN LIMITS.

Part: INDICATOR — FAILED (COCKPIT) · airframe 13,900 hrs · 9,984 cycles

INTERGRATED STAND-BY INSTRUMENT SYSTEM FAILED. MAINTENANCE REMOVED THE INTERGRATED STAND-BY INSTRUMENT.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 13,853 hrs · 9,951 cycles

PRE FLIGHT NR 5482 - STL - EMERGENCY LIGHTS INOP ON THE RIGHT SIDE OF THE AISLE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY.

Part: LINE — BROKEN (BLEED VALVE) · airframe 11,345 hrs · 8,252 cycles

5533 - STL - ENGINE NR 2 ITT EXCEEDED TO YELLOW BRIEFLY HIGHER. MAINTENANCE REMOVED AND REPLACED BROKEN ACCELERATION BLEED VALVE LINE, OPS CK GOOD.

Part: LIGHT — BURNED OUT (CABIN) · airframe 10,979 hrs · 8,005 cycles

MX - STL - ONE EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB.

Part: CONNECTOR — UNSECURE (LT ENGINE) · airframe 10,269 hrs · 7,531 cycles

FLT 5502 - DEN - LEFT ENGINE ITT WENT TO 948C. MAINTENANCE RESEATED CONNECTOR AT NR 1 TRIM PLUG PERFORMED ENGINE GRN PENALTY RUN ALL INDICATIONS OK.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 7,896 hrs · 6,082 cycles

TAKE-OFF CONFIG WARNING LIGHT ON. MAINTENANCE REMOVED AND REPLACED AURAL WARNING UNIT.

Part: STARTER — INOPERATIVE (NR 2 ENGINE) · airframe 7,607 hrs · 5,906 cycles

AUS - ENGINE NR 2 WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 2 STARTER.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 7,143 hrs · 5,624 cycles

DEN - LEFT ENGINE HIGH ITT UPON SETTING T/O TRUST. MAINTENANCE INSPECTED NR 1 ENGINE AND PERFORMED ENGINE RUN. ALL INDICATIONS NORMAL IAW ROLLS ROYCE MM 72-00-00.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 5,821 hrs · 4,852 cycles

STL - MAIN PITCH TRIM INOP. MAINTENANCE RE-RACKED HORIZONTAL STAB CONTROL UNIT AND CHECKED OK.