N804AE

Part: FAN — INOPERATIVE (RT A/C PACK) · airframe 35,215 hrs · 31,223 cycles

FUMES (ELECTRICAL BURNING SMELL IN COCKPIT AND CABIN) SOURCE NOT IDENTIFIED. ACCOMPLISHED FIM 21-20-00. FOUND CABIN SIDEWALL LIGHTS OUT AT 6CB AND 2A AND CA CHART HOLDER LIGHT MISSING ONE BULB. PERFORMED ETN-EM-72-034. NO ODOR DETECTED. RAN ENGINES WITH CREW. PERFORMED TROUBLESHOOTING OF ELECTRICAL ODOR AND FOUND THE NR 2 RECIRCULATION FAN INOPERATIVE. REMOVED AND INSTALLED CONDENSER, MIXER ON THE RT PACK IAW AMM 21-51-04. REMOVED AND REPLACED PAX CABIN SIDEWALL LIGHTS IAW AMM 33-21-067 CHECKED GOOD. INSTALLED BULBS IAW AMM 33-11-06. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI-ICE SYSTEM) · airframe 35,148 hrs · 31,159 cycles

WING A/I FAIL FOLLOWED BY ICE COND-A/I INOP WARNING ON APPROACH INTO ORD, ALL OF THIS WITHOUT LOW CAPACITY. CAPACITY WAS GOOD.-C/A-PERFORMED OPS CHECK I/A/W AMM 30-00-00 NO DEFECTS NOTED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,100 hrs · 31,113 cycles

PER PS-1 INSPECTION, FOUND RH AND LH OVER THE WING EMERGENCY LIGHTS INOP-C/A-REMOVED AND REPLACED #4 EMERGENCY LIGHT BATTERY AND CHARGER IAW EMB AMM 33-50-04. OPC BAD. BATTERY CHARGER ASSY P/N 11-0049 S/N 25338; LIGHT EMERGENCY L/H P/N 30-2510-3

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 35,054 hrs · 31,054 cycles

COCKPIT EMERGENCY LIGHT INOP-C/A-RAR COCKPIT EMERGENCY LIGHT IAW AMM TASK 33-50-05-000-801-A AND 33-50-05-400-801-A. OPC GOOD. END.

Part: CHARGER — FAILED (CABIN) · airframe 35,027 hrs · 31,026 cycles

BOTH OVERWING EXTERNAL AFT EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED BULBS IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A NO FIX, T/S PER WM 33-50-50 SLAVED IN INVERTER IAW EMB AMM 33-50-11-400-801-A NO FIX, T/S FURTHER RAR #4 EMERGENCT BATTERY AND CHARGER IAW W/C 33-700-19 OPC GOOD NO DEFECTS NOTED AT THIS TIME END. BULB P/N 6100928; EMERGENCY BATTERY P/N 2013-1A S/N 104892

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 34,966 hrs · 30,976 cycles

BOTH OVERWING EMERGENCY LIGHTS INOP-C/A--REMOVED AND REPLACED BOTH OVERWING EMERGENCY LIGHTS IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX. TROUBLESHOT, SUSPECTED EMERGENCY BATTERY. REMOVED AND REPLACED EPSU AT THE #3 AND #4 POSITION IAW 33-700-19 W/C. OPC GOOD END. EMERGENCY LIGHTING P/N 2013-1ASMI S/N 9817 (4); S/N 67826 (3); CHARGER ASSY BATTERY P/N BA5-0933-901 (3)

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 34,833 hrs · 30,847 cycles

LT AND RT LATERAL PANEL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND BATTERY CHARGER ASSY IAW AMM 33-50-04. OPS CHECKS OK.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 34,735 hrs · 30,751 cycles

EXTERNAL AFT OVERWING EMERGENCY LIGHTS INOP ON LT AND RT SIDE. C/A-REMOVED AND REPLACED F1 FUSE ON #4 BATTERY CHARGER IAW CMM 25-60-03. OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 34,722 hrs · 30,740 cycles

MAIN ENTRY DOR DIFFICULT TO OPEN. C/A-OPENED & CLOSED DOOR NO DEFECTS NOTED LUBRICATED AS REQUIRED IAW AMM 52-00-00. OPS CHECK OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,723 hrs · 30,741 cycles

MULTIPLE EMER LIGHTS INOP. C/A-REMOVED AND REPLACED #3 EMER BATTERY IAW W/C 33-700-19 AND PERFORMED EMER LIGHT CHECK IAW W/C 33-700-17. OPC GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 34,497 hrs · 30,546 cycles

FA REPORTS MAIN DOOR IS HARD TO OPEN AND CLOSE. LUBED DOOR ROLLERS AS NECESSARY. OPS CHK GOOD. NO FURTHER DEFECTS NOTED.

Part: DOOR — BINDING (MAIN CABIN) · airframe 34,100 hrs · 30,200 cycles

MAIN CABIN DOOR VERY HARD TO OPEN-C/A-PERFORMED LUBRICATION AND ADJUSTMENT OF MAIN CABIN DOOR IAW EMB 140 AMM 52-18-00. OPC GOOD. NO DEFECTS NOTED.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 34,048 hrs · 30,154 cycles

MAIN DOOR HARD TO OPEN. C/A-PERFORMED OPC AND LUBRICATED MAIN DOOR IAW AMM 52-11-00. NO FURTHER DEFECTS NOTED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 33,744 hrs · 29,853 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. UP-ON INVESTIGATION FOUND BROKEN WIRE AT CONNECTOR P8530. REPAIRED WIRE AT CONNECTOR P8530 PIN D PER SWPM 20-21-00. OPS CK GOOD.

Part: O-RING — FAILED (BLEED SYSTEM) · airframe 33,744 hrs · 29,853 cycles

ENG 1 LEAK BLEED "TRANSFERRED TO NRWC 804-DFW-02207"-C/A- REMOVED AND REPLACED BLEED JOINT O RINGS # 17,19,26 AND 30 IAW EMB 140 AMM 36-11-10 OPS AND LEAK CKECKS GOOD IAW EMB 140 AMM 36-00-00

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,583 hrs · 29,683 cycles

RT WING TO FUSELAGE EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED RT WING TO FUSELAGE EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD.

Part: MOTOR — FAILED (VALVE) · airframe 33,350 hrs · 29,418 cycles

PACK 1 VLV CLSD IN LIGHT. TEMPERATURE IN CABIN TOO LOW IN FLIGHT. AT THE GATE WHILE OPERATING PACK 1&2 VIA APU BLEED, PACK 1 NUMEROUS TIMES STOPPED SUPPLYING AIR AND TURNED OFF. TIRED TEMP CONTROLLERS IN AUTO AND MANUAL MODE WITH SAME RESULTS. NO EICAS MESSAGES PRESENTED-C/A-PERFORMED PACK #1 OPC IAW EMB 140 AMM 21-51-00 OPC GOOD. NO DEFECTS NOTED AT THIS TIME. CND MSG. REMOVED AND REPLACED DUAL TEMP CONTROL VALVE ON PACK #2 IAW EMB 140 AMM 21-60-01. PERFORMED PACK #2 OPC IAW EMB 140 AMM 21-51-00 OPC GOOD. NO DEFECTS NOTED AT THIS TIME. DEFERRED PER MEL 21-30. FOUND JOINT BETWEEN THE CONDENSER/MIXER AND WATER COLLECTOR TORN AND LEAKING ON LH PACK. REMOVED AND REPLACED JOINT ON LH PACK BETWEEN CONDENSER/MIXER AND WATER COLLECTOR AS PER EMB-140 AMM 21-51-03, OPS CHECK AND LEAK CHECK GOOD IAW EMB-140 AMM 21-51-00. MEL ITEM RESTORED.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 33,352 hrs · 29,419 cycles

PACK 2 OVHT PRESENTED RESET PACK MESSAGE CAME BACK. UNABLE TO CONTROL CABIN TEMP-C/A-T/S PER FIM 21-60-00-810-810-A. REMOVED AND REPLACED NR 2 PACK DUAL TEMP CONTROL VALVE IAW AMM 21-60-01. OPS CHECKS GOOD IAW AMM 21-51-00. PACK RAN FOR 45 MINUTES WITH NO TROUBLE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,178 hrs · 29,265 cycles

RH TOP EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR RH TOP EXTERIOR EMERGENCY LIGHT, OPC GOOD IAW AMM 33-50-10

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,796 hrs · 28,934 cycles

RT OVERWING PANEL EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT OVERWING PANEL EMERGENCY LIGHT LAMP IAW AMM 33-50-10 OPS CK GOOD.

Part: SENSOR — FAILED (LAVATORY) · airframe 32,700 hrs · 28,837 cycles

LAV SMOKE INTERMITTENT. REMOVED AND REPLACED THE LAV SMOKE DETECTOR AND LAV SMOKE PANEL IAW AMM 26-12-01 AND 26-12-02, DID NOT FIX PROBLEM. SMOKE DETECTOR P/N FTA719-01 S/N 70528 P/N TRA72-20 S/N 70249. REMOVED AND REPLACED LAV SMOKE DETECTOR SENSOR IAW AMM 26-14-01. OPS CHECK GOOD.

Part: CIRCUIT BREAKER — TRIPPED (CABIN PRESSURE) · airframe 32,303 hrs · 28,431 cycles

AFTER T/O LOSS OF ALL PRESSURIZATION INDICATIONS ALONG W/ CB F8 POPPED. UNABLE TO DEPRESSURIZE AFTER LANDING. MTX REQ TO RESET CB IN ORDER TO DEPRESSURIZE. RETURNED TO CLT. RESET CB AND PERFORMED OPS CHECK OF PRES SYSTEM IAW AMM 21-31-00. CB STAYED IN OPS CHECKS GOOD. NO DEFECTS NOTED

Part: WIRE — DISCONNECTED (CABIN) · airframe 32,228 hrs · 28,359 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED SERVICE DOOR MIDDLE LINER ASSEMBLY, FOUND EMERGENCY LIGHT WIRES NOT CONNECTED, CONNECTED EMERGENCY LIGHT WIRES AND REINSTALLED SERVICE DOOR MIDDLE LINER ASSEMBLY IAW AMM 25-23-05. OPERATIONAL CHECK OF SERVICE DOOR EMERGENCY LIGHT GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,228 hrs · 28,359 cycles

NR 3 EMERGENCY FLOOR LIGHT STRIP INOP. REMOVED AND REPLACED NR 3 EMERGENCY FLOOR LIGHT STRIP IAW AMM 33-50-12. OPC GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,227 hrs · 28,358 cycles

FUSELAGE AFT UPPER SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STINGER 2L. INSTALLED REPAIR DOUBLER FILLER, DRAG ANGLE AND SHIM IAW SRM 53-31-01.

Part: FRAME — GOUGED (FUSELAGE) · airframe 32,227 hrs · 28,358 cycles

FRAME 65 IS GOUGED BETWEEN STR 2L-3L. REPAIRED IAW ERS WORK CARD NUMBER: ERS-EM-53MR-3314.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,227 hrs · 28,358 cycles

CARGO DOOR LOWER SILL IS CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,227 hrs · 28,358 cycles

LT FR 10 CRACKED AT UPPER END UNDER DV WINDOW. REMOVED CRACKED LT FRAME 10 AT UPPER END UNDER DV WINDOW AND INSTALLED SERVICEABLE LT FRAME 10 IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,227 hrs · 28,358 cycles

RT FR 10 CRACKED AT UPPER END UNDER DV WINDOW. REMOVED CRACKED RT FRAME 10 AT UPPER END UNDER DV WINDOW AND INSTALLED SERVICEABLE RT FRAME 10 IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 32,227 hrs · 28,358 cycles

FR 65 SHEAR CLIP IS CORRODED AT CARGO DOOR LOWER SILL. REPAIR SECTION OF FRAME 65 SHEAR CLIP AT CARGO DOOR LOWER SILL IAW SRM 53-31-04.

Part: ISIS — FAILED (COCKPIT) · airframe 31,924 hrs · 28,073 cycles

ABORTED TAKEOFF BEFORE 80KTS DUE TO STD ATT FAIL. R & R ISIS IAW AMM 34-01-01, PERFORM FUNCTIONAL TEST IAW 34-01-01-700-801-A. OPERATIONS CHECKED GOOD, NO LEAKS NOTED.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 31,918 hrs · 28,069 cycles

MAIN DOOR DIFFICULT TO OPEN & CLOSE. LUBRICATED & PERFORM OPERATIONS CHECK OF MAIN CABIN DOOR IAW AMM CH 52-10-00 NO OTHER DEFECTS NOTED.

Part: BRACKET — DEFECTIVE (FLASHLIGHT) · airframe 31,898 hrs · 28,050 cycles

FLIGHT ATTENDANT FRONT FLASHLIGHT IS NOT CHARGING. R & R FLASHLIGHT BRACKET IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 31,296 hrs · 27,496 cycles

MAIN CABIN DOOR EMER EXIT SIGN INOPERATIVE. R & R NR 1 INVERTER IAW AMM 33-50-04.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 31,112 hrs · 27,353 cycles

FLOOR PROXIMITY LIGHTS 2, 3 FROM FWD & PAX EXIT LIGHTED SIGN AT GALLEY BULKHEAD ARE INOPERATIVE. REPLACED NR 2 EMER LIGHT BATTERY, BATTERY CHARGER & NR 3 EMER LIGHT INVERTER IAW AMM 33-50-04 & 33-50-11. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY NR 2 PN 11-0049, SN 15615. EMER BATTERY NR 2 PN 2013-1A, SN 105185.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,837 hrs · 26,269 cycles

ON FLIGHT 3741 CREW REPORTED LANDING GEAR AIR, GROUND FAIL MESSAGE & MADE AN EMERGENCY LANDING. THE ACFT WAS REMOVED FROM SERVICE. AIR GND WOW SYS TEST IAW EMB 145 AMM 32-63-00. CHECKED GOOD AT THIS STATION, OK FOR FLIGHT. THE AIRCRAFT RETURN TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 29,228 hrs · 25,704 cycles

F/A FLASHLIGHT HOLDER BROKEN. R & R F/A'S FLASHLIGHT ASSY IAW CMM 25-60-11. OPS CK GOOD.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 28,675 hrs · 25,166 cycles

THE CREW REPORTED THE F/O’S FLASHLIGHT WAS INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE F/O’S FLASHLIGHT ASSY IAW AMM 33-50-16. THE OPS TEST WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — DAMAGED (COCKPIT) · airframe 28,675 hrs · 25,166 cycles

THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT SWITCH MISSING. THE ACFT WAS REMOVED FROM SERVICE. R & R THE CAPTAIN’S FLASHLIGHT ASSY IAW AMM 33-50-16. THE OPS TEST WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 28,149 hrs · 24,658 cycles

ON FLIGHT 4070 THE CREW REPORTED THE CABIN DOOR WAS DIFFICULT TO OPERATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. DURING PHASE CHECK 1A/3A PERFORMED W/C 52-600-00 SIDE HINGED MAIN DOOR ACTUATING AND LOCKING MECHANISM LUBRICATE. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 27,874 hrs · 24,407 cycles

DURING B INSPECTION FOUND THE RIGHT FORWARD ABOVE WING EMERGENCY LIGHT BULB INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD ABOVE WING EMERGENCY LIGHT BULB IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,730 hrs · 24,288 cycles

DURING B INSPECTION FOUND THE NR 3 EMERGENCY LIGHT POWER SUPPLY FAILING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK PER EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD PER EMB 140 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 27,624 hrs · 24,198 cycles

DURING B-INSPECTION FOUND THE EMERGENCY FLOOR LIGHT STRIP WIRING BROKEN OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OLD STRIP AND INSTALLED NEW ELECTRICAL ILLUMINESCENT LIGHT STRIP TO PLASTIC SIDEWALL RETAINER ASSY IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 27,678 hrs · 24,239 cycles

DURING B INSPECTION FOUND A WIRE BROKEN ON EMERGENCY LIGHT STRIP NR 5. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED WIRE ON EMERGENCY LIGHT STRIP NR 5 REF EMB 140 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,624 hrs · 24,198 cycles

DURING B INSPECTION FOUND THE RACK EMERGENCY FLOOR LIGHT STRIP TORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP WITH NEW UNIT REF EMB 140 AMM FOR INSTALL TASK 2001 33-50-92. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (FLASHLIGHT) · airframe 27,675 hrs · 24,238 cycles

DURING B INSPECTION UPON INSERTION PIN BROKE ON THE RIGHT EMERGENCY FLASHLIGHT AFT EQUIPMENT STOWAGE UNIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED WIRING AT SPLICE 3557 FOR EMERGENCY FLASHLIGHT REF EMB 145 SWPM 20-23-00 EMERGENCY FLASHLIGHT AT AFT RIGHT EQUIPMENT STOWAGE OPS CHECKS GOOD REF EMB 145 AMM 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 27,502 hrs · 24,081 cycles

DURING MAINTENANCE INSPECTION, FOUND CORROSION ON LOWER CARGO DOOR CUTOUT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED LOWER CARGO DOOR CUTOUT IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,496 hrs · 24,072 cycles

DURING MAINTENANCE INSPECTION FOUND SHEAR CLIP CRACKED AT FRAME 68 BETWEEN STRINGERS 6L & 7L. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L & 7L IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — UNSERVICEABLE (CABIN) · airframe 27,527 hrs · 24,109 cycles

DURING B INSPECTION FOUND THE EMERGENCY POWER SUPPLY UNIT NEEDS TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED EMERGENCY BATTERY PACK AND CHARGER REF EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,415 hrs · 23,997 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT WING EMERGENCY LAMP IAW EMB140 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (NR 3) · airframe 27,057 hrs · 23,641 cycles

DURING B INSPECTION FOUND THE FORWARD CAPTAIN EMERGENCY EXIT SIGN AT 3BC INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 INVERTER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 26,507 hrs · 23,107 cycles

DURING B INSPECTION FOUND THE RIGHT WING AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WING AFT EMERGENCY LIGHT BULB IAW EMB AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 25,877 hrs · 22,500 cycles

FLIGHT 3319, CREW REPORTED ON TAKEOFF, COCKPIT FILLED WITH SMOKE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE IAW W/C 71-000-00, NO LEAKS OR SMOKE NOTED AT THIS TIME. ALL PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE. THE CAUSE OF THE SMOKE WAS FOUND TO BE A FAULTY NR 4 CARBON SEAL.

Part: ROLLER — DIRTY (MAIN ENTRY DOOR) · airframe 25,763 hrs · 22,421 cycles

ON FLIGHT 2778 THE CREW REPORTED THE FLAP AT THE TOP OF THE MAIN ENTRY DOOR INTERMITTENTLY STICKS MAKING THE DOOR DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND DOOR FRAME ROLLERS STICKY CLEANED AND LUBED ROLLERS IAW EMB 140AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,258 hrs · 22,305 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR PROXIMITY LIGHT AT ROW 13 TO 15 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHT IAW EMB-140 AMM 33-50-17. THE OPERATIONAL CHECK WAS GOOD IAW EMB-140 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — OUT OF POSITION (CABIN) · airframe 24,996 hrs · 21,819 cycles

ON FLIGHT 4463 THE CREW REPORTED THE AFT FLIGHT ATTENDANTS FLASHLIGHT WAS MISSING. THE FLIGHT CREW PLACARD PER MEL 2553. FOUND FLASHLIGHT IN AIRCRAFT DURING PS CHECK. RE-INSTALLED IN AFT FLIGHT ATTENDANT LOCATION IAW EMB 140 AMM 33-50-16. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — FAILED (NR 1) · airframe 23,574 hrs · 20,594 cycles

ON FLIGHT 4153 DURING CRUISE THE CREW REPORTED SMOKE IN CABIN AROUND ROW 9 COMING FROM THE FLOOR AND IN THE COCKPIT. AN EMERGENCY WAS DECLARED AND THE CAPTAIN ELECTED TO DIVERT TO MDT. THE AIRCRAFT SAFELY LANDED AT DESTINATION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AIR CYCLE MACHINE IAW EMB AMM 21-51-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,765 hrs · 19,965 cycles

ON FLIGHT 2730 THE CREW REPORTED THE FLASHLIGHT BEHIND THE CAPTAINS SEAT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT BEHIND THE CAPTAINS SEAT PER EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK PER EMB140 AMM 33-51-01 WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,654 hrs · 19,879 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 23 CRACKED BETWEEN STRINGER 15 RIGHT AND 16 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1738. THE AIRCRAFT RETURNED TO SERVICE.

Part: FUEL/OIL COOLER — DEFECTIVE (NR 1) · airframe 22,060 hrs · 19,390 cycles

ON FLIGHT 4166 DURING THE CLIMB THE CREW REPORTED, RECEIVED AN ENGINE 1 HIGH OIL TEMPERATURE MESSAGE. THE TEMPERATURE WENT TO 150 C. THE CREW REDUCED THRUST AND DROPPED DOWN IN GREEN RANGE. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE OIL QUANITY REMAINED AT 12 QUARTS THROUGHOUT THE INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 FUEL COOLED OIL COOLER IAW ROLLS-ROYCE MM 79-25-15. PART NUMBER AND SERIAL NUMBER: 23077047, SN VR2964. REMOVED AND REPLACED THE OIL PRESSURE SWITCH IAW ROLLS-ROYCE MM 79- 33-10. PART NUMBER AND SERIAL NUMBER: 23078098, SN KB10276. REMOVED AND REPLACED THE OIL TEMPERATURE/PRESSURE SENSOR IAW ROLLS-ROYCE MM 79-31-10. PART NUMBER AND SERIAL NUMBER: 23073715, SN QW83644. THE LEAK CHECK AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — FAILED (CABIN) · airframe 21,391 hrs · 18,831 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT SIGN FAILED TO ILLUMINATE AT THE CENTER FORWARD OVERHEAD CEILING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 INVERTER IAW EMB AMM 33-50-11. NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 21,388 hrs · 18,829 cycles

WHILE PARKED AT FSD THE RAMP REPORTED THE AIRCRAFT WAS HIT BY A BAGGAGE CART. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FRAME 27 IAW SRM 51-40-02. COLD WORKED STRINGER 13 LEFT IAW SRM 51-20-04, AND PER ETA-EM-5300-1329. INSTALLED 2 NEW SHEAR CLIPS AT STRINGER 12 LEFT AND 13 LEFT IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 20,956 hrs · 18,436 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FORWARD CENTER AISLE EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CENTER AISLE EMERGENCY EXIT SIGN. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 20,872 hrs · 18,366 cycles

ON FLIGHT 4537 AFTER TAKEOFF, CREW REPORTED A BURNING ODOR IN COCKPIT & JUST BEHIND COCKPIT DOOR. CREW DECLARED AN EMERGENCY & RETURNED TO RDU. UPON POWER REDUCTION PRIOR TO LANDING, ODOR WENT AWAY. PERFORMED OVERWEIGHT LANDING AT 43000 LBS AT 300 FT/MIN. ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED OPS TESTS OF BOTH ENGINES IAW RMM 72-00-00 & ETN EN 72-034R4. ODOR EVENT TROUBLESHOOTING COULD NOT DUPLICATE, NO ODOR IN COCKPIT OR CABIN AT THIS TIME. NO PARTS REMOVED OR REPLACED. FOUND EVIDENCE OF OIL AT SIX O’CLOCK BEHIND IGV’S IN ENGINE NR 1 INLET. R & R LT ENGINE. ACFT RETURNED TO SERVICE. THE CAUSE OF THE ODOR/LEAK WAS DETERMINED TO BE A FAULTY NR 4 CARBON SEAL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,073 hrs · 15,991 cycles

DURING HMBV INSPECTION FOUND RIGHT OMEGA BEAM CORRODED AROUND FLOOR SUPPORT AT FRAME 27. OMEGA BEAM REPAIRED IAW EMBRAER SRM 53-00-01 AND AEAI ETA EM-5300-478. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,073 hrs · 15,991 cycles

DURING HMBV INSPECTION, FOUND SERVICE DOOR SILL CORRODED. MAINTENANCE REPLACED SERVICE DOOR SILL IAW 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,073 hrs · 15,991 cycles

DURING HMBV INSPECTION FOUND LEFT OMEGA BEAM CORRODED AROUND FLOOR SUPPORT AT FRAME 27. OMEGA BEAM REPLACED IAW EMBRAER SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,073 hrs · 15,991 cycles

DURING HMBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AROUND FLOOR SUPPORT AT FRAME 38. OMEGA BEAM REPAIRED IAW EMBRAER SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SQUAT SWITCH — FAILED (LT MLG)

ON FLIGHT, CREW REPORTED A LG AIR/GRD FAIL ANNUNCIATION AFTER TAKEOFF. LANDING GEAR HANDLE STUCK IN DOWN POSITION. OTHER ANNUNCIATIONS INCLUDED 1-2 WOW INOP AND SPS ADVANCED. AC RETURNED TO FIELD. AC REMOVED FROM SERVICE. REMOVED AND REPLACED NLG WOW SWITCH IAW AMM 32-63-01. OPS CHECK GOOD. REMOVED AND REPLACED LT MLG AFT WOW SWITCH IAW AMM 32-63-02. OPS CHECK GOOD. AC RETURNED FOR SERVICE. (K)

Part: NONE — NONE (NONE) · airframe 15,738 hrs · 14,138 cycles

ON FLIGHT 4188, CREW REPORTED WHILE EN ROUTE "LO FUEL NR 2" WARNING WITH NR 1 TANK ON EICAS SHOWING BLANK. CLEARED IT SELF THEN REAPPEARED. FUEL QUANTITY ON FMS SYSTEM ALL NORMAL. APPROACHING ORD, ANOTHER WARNING AND NR 2 FUEL ON EICAS SHOWED BLANK. DECLARED EMERGENCY/PRIORITY APPROACH AND LANDED SHORTLY AFTER. AIRCRAFT REMOVED FROM SERVICE. FOUND REFUEL PANEL POWER SWITCH IN "BATTERY" POSITION. RESET POWER SWITCH TO "POWER" POSITION. OPERATIONAL CHECK GOOD AND NR 8194; AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — OPEN (EXTERNAL POWER) · airframe 14,664 hrs · 13,400 cycles

NOTED A HIGH FREQUENCY SOUND AND VIBRATION AFTER TAKEOFF AND NOTED AS AIRSPEED SLOWED DOWN SOUND WENT AWAY. PERFORMED INSPECTION ON AIRCRAFT FOUND 6PV DOOR OPEN NO EXTERNAL DAMAGE TO THE SKIN WAS FOUND AT THIS TIME RE-SECURED THE DOOR AS REQUIRED AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,150 hrs · 11,784 cycles

LEFT OMEGA BEAM FOUND CORRODED AT FRAME 25. PERFORMED CUT OUT OF CORROSION, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,150 hrs · 11,784 cycles

FOUND CENTER OMEGA BEAM CORRODED BETWEEN FRAME 23 AND FRAME 25. CLEANED, TREATED AND RESTORED PROTECTIVE FINISH. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,150 hrs · 11,784 cycles

FOUND CENTER OMEGA BEAM CORRODED AT FRAME 23. PERFORMED CUT TO REMOVE CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,150 hrs · 11,784 cycles

FOUND CARGO DOOR FRAME LOWER SILL CORRODED. REMOVED AND REPLACED SILL. CLEANED, TREATED AND RESTORED PROTECTIVE FINISH IAW EMB SRM 51-20-03, 51-40-03 AND 51-40-06. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,150 hrs · 11,784 cycles

FOUND LEFT OMEGA BEAM FOUND CORRODED AT FRAME 20. FABRICATED AND INSTALLED FILLER AND DOUBLER. CLEANED, TREATED AND RESTORED PROTECTIVE FINISH IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: PITOT SYSTEM — CONTAMINATED · airframe 12,801 hrs · 11,495 cycles

SPS ADVANCE, LOST ALL FIRST OFFICER INSTRUMENTATION, EMERGENCY DECLARED. DRAINED WATER FROM PITOT STATIC SYSTEM IAW EMB AMM 34-15-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: ANTI-ICE SYSTEM — FAILED

DFW - FLT 3712 - AIRCRAFT STRUCK BY LIGHTNING AT 36000 FEET IN CRUISE FLIGHT WITH GEAR UP AND FLAPS UP CONFIGURATION. AFTER STRIKE COCKPIT CREW AND CABIN CREW COULD BOTH SMELL A BURNING/ELECTRICAL ODOR WHICH LASTED APPROX 6-8 MINUTES THAN DISSIPATED. ONLY SYSTEMS AFFECTED APPEARED TO BE EICAS. ICE DETECTION FAIL AND ICE DET 1-2 FAIL. ALL OTHER AIRCRAFT AND ELECTRICAL SYSTEMS APPEARED NORMAL. POST FLIGHT INSPECTION FOUND DAMAGE ON UPPER LEFT WING TIP. (M)

Part: LANDING GEAR — MALFUNCTIONED (NLG & MLG)

SFO - FLT 3185 - AFTER TAKEOFF, LG AIR GROUND FAIL MESSAGE GEAR WOULD NOT RETRACT LOCKED IN DOWN POSITION, LANDED AND RETURN TO GATE. NO EMERGENCY DECLARED, NORMAL DEPLANING CMC MESSAGE LG AIR GROUND PROX SWITCH FAIL 1 EVENT. COMPLETED TROUBLESHOOTING OF ENTIRE AIR/GRD PROX SYSTEM WHICH CHECKED GOOD. CMC ONLY SHOWED 1 INSTANCE OF PROX SYSTEM FAIL. BREAK OUT BOX CHECK WAS GOOD. GEAR SWINGS WERE GOOD. ENTIRE SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT SIGN FOR OVERWING EXIT INOPERATIVE. REPLACED INVERTER NR 6 IAW EMB MM 33-50-11. OPERATIONAL CHECK GOOD. REMOVED AND REPLACED BATTERY POWER SUPPLY NR 4 (BT 8503) IAW EMB MM 33-50-04. OPERATIONAL CHECK GOOD, P/N 20131A S/N 63075. AIRCRAFT RETURNED TO SERVICE. (M)

Part: GUSSET — CORRODED (FLOORBEAM)

SAW - DURING CPCP INSPECTION MAINTENANCE, FOUND THE GUSSET OVER LEFT OUTBOARD FLOORBEAM BETWEEN FRAMES 16-17 HAS CORROSION. INSTALLED NEW GUSSET IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, MAINTENANCE FOUND THE AFT SERVICE DOOR SILL CORRODED BETWEEN FRAMES 22-23. INSTALLED NEW SILL IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — DAMAGED (PITCH TRIM)

CREW REPORTED A PITCH TRIM CONFIG WARNING ON EICAS DURING TAKEOFF. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED PIN C ON CONNECTOR J0886. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SENSOR — INOPERATIVE (LEFT FLAP)

DURING DESCENT CREW REPORTED THE FLAPS FAILED TO DEPLOY. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE LEFT FLAP VELOCITY SENSOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BEAM — CORRODED (GALLEY)

THIS IS A LEVEL TWO FINDING FOUND DURING AN MBV INSPECTION, CENTER BEAM RAMP IS CORRODED AT FRAME 20. REMOVED CORRODED CENTER BEAM RAMP AND INSTALLED NEW SERVICEABLE RAMP IAW EMB 140 SRM 51-40-02, 51-20-03. (M)

Part: SILL — CORRODED (SERVICE DOOR) · corrosion level 2

THIS IS LEVEL TWO FINDING FOUND DURING A MBV INSPECTION, THE SERVICE DOOR AFT SILL WAS FOUND CORRODED. REMOVED AND INSTALLED NEW SERVICE DOOR SILL IAW EMB 140 SRM 51-40-02, 51-20-03 AND 51-40-06. (M)

Part: SILL — CORRODED (SERVICE DOOR)

THIS IS A LEVEL TWO FINDING FOUND DURING AN MBV INSPECTION SERVICE DOOR CENTER SILL CORRODED. BLENDED OUT CORROSION ON SERVICE DOOR SILL. FABRICATED 3 REPAIR DOUBLERS AND INSTALLED IAW ETN NR EB-53-032R1 AND IC2003-145-1094. (M)