N820AE

Part: DRAIN VALVE — LEAKING (RIGHT) · airframe 34,427 hrs · 30,109 cycles

ON TAXI OUT PAX AND FLT ATTENDANT REPORTED STRONG SMELL OF FUEL IN THE CABIN "TRANSFERRED TO NRWC 820-LGA-02856"-C/A-FOUND RH INBOARD FUEL DRAIN VALVE OPEN POSITION WITH FUEL DRIPPING, CLOSED DRAIN VALVE, NO FUEL LEAKS NOTED, REF AMM 12-11-03. NO SMELL IN THE CABIN NOTICED AT THIS TIME. MOC TRIAD REQUIRE FOR FUEL SMELL IN CABIN. REF FIM TASK 21-20-00-810-803-A. FOLLOWED FIM TASK 21-20-00-810-803-A. PERFORMED OPS CHECK WITH APU IAW EMB 140 AMM 49-13-00. OPS CHECK GOOD. PERFORMED OPS CHECK WITH BOTH ENGINES IAW EMB 140 AMM 71-00-01. OPS CHECK GOOD. NO FUEL/ABNORMAL SMELL NOTED. INSTALLED FLOOR PANEL 252CF, 251GF, 251JF, 251DF IAW EMB 140 AMM 53-01-02. NO DEFECTS NOTED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,944 hrs · 29,621 cycles

MAIN DOOR FAIRING EMERGENCY LIGHT INOP. REMOVED AND REPLACED MAIN DOOR LINING PANEL IAW AMM TASK 25-23-04. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 33,423 hrs · 29,164 cycles

AFT CABIN EMERGENCY LIGHT FLOOR PANEL INOP. REMOVED AND INSTALLED NR 4 CHARGE AND BATTERY, IAW EMERGENCY LIGHTING SYSTEM POWER SUPPLIES WORKCARD 33-700-19, OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 83000

Part: CONTROL PANEL — FAILED (SMOKE DETECTOR) · airframe 33,322 hrs · 29,049 cycles

LAVATORY SMOKE IN FLIGHT, DURING APPROACH. NO EVIDENCE OF SMOKE OBSERVED. PERFORMED GVI OF THE LAVATORY AREA. NO SMOKE, HOT SPOTS, OR OTHER DESCREPANCIES NOTED. CYCLED THE LAVATORY SMOKE DETECTOR CIRCUIT BREAKER, THE SMOKE MESSAGE CAME BACK WITHIN TWO MINUTES. REMOVED AND REPLACED THE SMOKE DETECTOR PANEL IAW AMM 26-14-02, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 32,912 hrs · 28,630 cycles

AFT COURTESY CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW IAW AMM 33-26-00. OPS CHECKED GOOD.

Part: CONTROL HANDLE — FAILED (NLG STEERING) · airframe 32,625 hrs · 28,322 cycles

NOSE WHEEL STEERING GOING OUT INTERMITTENTLY. T/S AND FOUND TILLER NOT ENGAGED AS REQUIRED. REMOVED AND REPLACED STEERING CONTROL HANDLE IAW AMM 32-50-01. READJUSTED FEEDBACK UNITE/LOAD POTENTIOMETER IAW 32-50-07/32-50-05 FOLLOWED AMM 32-50-00 FOR OPS CHECK. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,154 hrs · 27,665 cycles

NR 1 EMERGENCY LIGHT HAS A BROKEN WIRE. REPAIRED THE WIRE IAW SWPM 20-21-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,154 hrs · 27,665 cycles

NR 5 EMERGENCY LIGHT HAS A BROKEN WIRE. REPAIRED THE WIRE IAW SWPM 20-21-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,154 hrs · 27,665 cycles

NR 8 EMERGENCY LIGHT AT 261BF HAS A BROKEN WIRE. REPAIRED THE WIRE IAW SWPM 20-21-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,154 hrs · 27,665 cycles

EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY AND ASSEMBLY IAW AMM 33-50-04

Part: SHEAR TIE — CORRODED (FR 65) · airframe 32,154 hrs · 27,665 cycles

CARGO DOOR CUT-OUT FRAME 65 SHEAR TIE CORRODED AT LOWER END. REPAIRED SHEAR TIE IAW SRM 53-31-04.

Part: SKIN — CRACKED (FRAME 77) · airframe 32,154 hrs · 27,665 cycles

RH EXTERNAL FUSELAGE SKIN CRACKED AT 2 FASTENERS FRAME 77. REPAIRED THE SKIN CRACKED IAW ERS-EM-53MR-2918.

Part: FITTING — CRACKED (FRAME 18-19) · airframe 32,154 hrs · 27,665 cycles

MACHINED FITTING BETWEEN FRAMES 18 AND 19, STRINGER 3L CRACKED. REMOVED AND REPLACED THE FITTING. IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 33-34) · airframe 32,154 hrs · 27,665 cycles

LEFT OMEGA BEAM IS CORRODED BETWEEN FRAMES 33 AND 34. REPAIRED IAW SRM 53-00-10, FIGURE 202, SHEET 1.

Part: SKIN — DENTED (LT WING LE) · airframe 32,154 hrs · 27,665 cycles

LEFT LE DENTED IN THE UNPAINTED AREA APPROX 57 INCHES. FROM THE INBD EDGE. REPAIRED THE LEADING EDGE IAW SRM 57-40-00 AND ETN-EM-57-060.

Part: SKIN — CRACKED (FRAME 75) · airframe 32,154 hrs · 27,665 cycles

RIGHT REAR FUSELAGE SKIN CRACKED AT FRAME 75, BETWEEN STRINGERS 1R AND 2R. REPAIRED THE SKIN IAW SRM 53-31-01.

Part: FRAME — GOUGED (FRM 15) · airframe 32,154 hrs · 27,665 cycles

FRAME 15 FOUND CHAFED AT STRINGER 2R. REPAIRED THE FRAME IAW ERS-EM-53MR-2906.

Part: YOKE — CRACKED (RT PYLON) · airframe 32,154 hrs · 27,665 cycles

RIGHT FWD PYLON LOWER YOKE CRACKED. REMOVED AND THE YOKE IAW EO EM-54MR-386.

Part: FRAME — CRACKED (FRM 10) · airframe 32,154 hrs · 27,665 cycles

FRAME 10 CRACKED BELOW COPILOTS DV WINDOW. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.

Part: FRAME — CRACKED (FRM 23) · airframe 32,154 hrs · 27,665 cycles

FRAME 23 CRACKED AT THE RT OTBD FLOOR SUPPORT. REPAIRED THE FRAME IAW EM-53MR-1808.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 32,154 hrs · 27,665 cycles

CARGO DOOR LOWER SILL IS CORRODED. R & R THE DOOR SILL IAW SRM 51-40-02

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,117 hrs · 27,623 cycles

DURING PS-2 INSPECTION, FOUND EMER BATTERY SUPPLY NR 2 INOPERATIVE. R & R BATTERY NR 2 & POWER SUPPLY NR 2 IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 15221.

Part: WIRE — BROKEN (CABIN) · airframe 31,908 hrs · 27,420 cycles

3RD PROX LIGHT STRIP FWD FROM LAVATORY HAS BROKEN WIRES. R & R 3RD PROX LIGHT FWD FROM LAVATORY IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 31,287 hrs · 26,850 cycles

FLIGHT ATTENDANTS REAR FLASHLIGHT ASSEMBLY BROKEN, DETACHED. R & R FLIGHT ATTENDANTS REAR FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 31,119 hrs · 26,700 cycles

WHILE CLIMBING THROUGH FL220 BLD 2 LEAK MSG ON EICAS, EPC & AOM 1 PROCEDURE COMPLIED WITH. R & R O RINGS AT JOINT 12 IAW MM 36-11-10. PERFORMED LEAK CHECK OF BLD SYS IAW MM 36-00-00. NO LEAKS NOTED.

Part: CONTROL PANEL — FAILED (BLEED AIR SYS) · airframe 31,060 hrs · 26,649 cycles

BLEED 2 LEAK WARNING MSG ON CLIMB OUT. MSG EXTINGUISHED AFTER COMPLYING WITH EMER PROCEDURES HOWEVER, ACFT STARTED DEPRESSURIZING AFTER COMPLYING WITH PROCEDURES. R & R PNEUMATIC CONTROL PANEL IAW AMM 20-13-10. COMPLIED WITH TEST OF BLEED SYS IAW AMM 36-00-00. OPERATIONS CHECKED GOOD, NO FAULTS NOTED. ACCOMPLISHED FUSELAGE DUCT LINES OF THE AIR BLEED SYS INSPECTION IAW AMM 36-11-09. NO LEAKS NOTED. OPERATIONS CHECKED GOOD.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 31,058 hrs · 26,647 cycles

BLEED LEAK 2 WARNING MSG ON CLIMB OUT ABOVE FL200. MSG EXTINGUISHED AFTER COMPLYING WITH EMER PROCEDURE. RETURNED NOT OVER WEIGHT LANDING. LANDING WEIGHT 39,000 LBS. FOUND LEAK AT JOINT 10. R & R ORINGS & SLEEVE IAW AMM 36-11-09. R & R BLEED SYS FOR AN HOUR, NO LEAKS NOTED AT THIS TIME.

Part: WIRE — BROKEN (BLEED AIR SYS) · airframe 31,026 hrs · 26,617 cycles

CLIMBING THROUGH ICING CONDITION INDICATION OF BLEED 2 LEAK. ACFT BACK TO NORMAL AFTER RUNNING PROCEDURE IN AOM 1. PERFORMED PHYSICAL INSPECTION OF ALL NR 2 BLEED SYS JOINTS, NO LEAKS NOTED. AT GND ENG START CONNECTOR FOUND TEMP SENSOR WIRE W772-0004 BROKEN LOOSE FROM S0790 & CONTACTING FUSELAGE. REATTACHED WIRE TO S0790, BLEED 2 OPERATIONS CHECKED OK IAW AMM CH 36-00-00-700-803A & 30-00-00-700-802A.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 31,002 hrs · 26,596 cycles

AFTER TAKEOFF ACFT WOULD NOT PRESS, RETURNED. R & R DIGITAL CONTROLLER, CABIN, IAW AMM 21-31-01. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 30,710 hrs · 26,346 cycles

COPILOT FLASHLIGHT INOPERATIVE. R & R COPILOT FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,553 hrs · 26,211 cycles

MAIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,395 hrs · 26,069 cycles

MAIN DOOR EMER EXIT LAMP INOPERATIVE. R & R MAIN DOOR EMER EXIT LIGHT LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD.

Part: ACTUATOR — MALFUNCTIONED (SPEED BRAKE) · airframe 30,320 hrs · 25,994 cycles

DURING DESCENT WHILE USING SPEED BRAKE THE ACFT ROLLED LT FOLLOWED BY SPOILER FAIL EICAS MSG, THIS WAS MOMENTARY. R & R RT SPEED BRAKE ACTUATOR IAW AMM 27-62-02. OPERATIONS CHECKED GOOD. LEAK CHECKED GOOD.

Part: SENSOR — FAULTY (CARGO BAY) · airframe 30,128 hrs · 25,835 cycles

AFTER LANDING EICAS PRESENTED A BAGG SMOKE INDICATION. FOLLOWED AOM PROCEDURES, MEMORY ITEMS & PRESSED BAGG EXTINGUISHER BUTTON. NO VISUAL INDICATION OF FIRE. EMER DECLARED. R & R METERING FIRE BOTTLE FOR CARGO COMPARTMENT IAW AMM 26-23-01. OPERATIONS CHECKED GOOD IAW AMM 26-15-00. R & R BAGGAGE COMPARTMENT SMOKE DETECTION SENSORS IAW 26-15-01. OPERATIONS CHECKED GOOD IAW AMM 26-15-00. CARGO AREA SMOKE DETECTOR PN 473597-13, SN 1032 & 3041.

Part: TUBE — FAULTY (NR 2 ENGINE) · airframe 29,583 hrs · 25,370 cycles

ON FLIGHT 2789 CREW REPORTED LATE IN CLIMB, FL300 IN CLIMB MODE, THRUST LEVERS IN DETENT. ENG 2 ITT WENT INTO YELLOW. REDUCTION OF THRUST KEPT ITT IN GREEN BUT AT 100 DEG HIGHER THAN ENG 1. SAME FOR CR2 MODE. R & R COMPRESSOR ACCELERATION BLEED CONTROL TUBES IAW MM 75-00-00-990-805. THE ACFT WAS REMOVED FROM SERVICE. R & R COMPRESSOR ACCELERATION BLEED CONTROL TUBES IAW MM 75-00-00-990-805. THE ACFT RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,498 hrs · 25,282 cycles

RIGHT FWD EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R RT FWD EXTERNAL EMERGENCY LIGHT ASSEMBLY IAW TASK 33-50-10-000-801-A & TASK 33-50-10-400-801-A, OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 29,498 hrs · 25,282 cycles

ROW 7 OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R NR 2 EMERGENCY LIGHT BATTERY & CHARGER IAW WORK CARD 33-700-19. OPERATIONS CHECKED GOOD IAW WORK CARD 33-700-17, NO DEFECTS NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,498 hrs · 25,282 cycles

GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R NR 2 EMERGENCY BATTERY & CHARGER IAW NRWC 820-CMI-01670.

Part: BATTERY — FAILED (CABIN) · airframe 29,464 hrs · 25,251 cycles

REPLACE EMERGENCY LIGHTING SYS NR 2 BATTERY WC 33-700-19. R & R EMERGENCY LIGHTING SYS NR 2 BATTERY IAW WC 33-700-19.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,211 hrs · 25,026 cycles

CAPTAIN'S FLASHLIGHT INOPERATIVE. R & R CAPTAIN'S FLASHLIGHT IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 29,109 hrs · 24,927 cycles

FLASHLIGHT BEHIND CAPTAIN INOPERATIVE, SWAPPED WITH AFT FLASHLIGHT. FLIGHT CREW PLACARD IAW MEL 25-53 AUTH 030511-C MOC 696863. RELAMPED CAPTAIN`S FLASHLIGHT AS NEEDED IAW STANDARD MT PRACTICES MEL ITEM RESTORED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,058 hrs · 24,883 cycles

PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. R & R MAIN PAX DOOR EMERGENCY LIGHT BULB IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: CONTROL TUBE — FAULTY (NR 2 ENGINE) · airframe 28,987 hrs · 24,818 cycles

IN CLIMB E2 WENT TO 903 DEGREE EVEN WITH THRUST LEVER PULLED BACK AN INCH, THE LT WAS RUNNING ABOUT 100 DEGREE WARMER. TRANSFERRED TO NRWC 820-DFW-01586. R & R CABV CONTROL TUBE IAW RR MM 75-00-00, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,667 hrs · 24,535 cycles

DURING PS 2 INSPECTION FOUND RT AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R RT AFT EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 28,512 hrs · 24,402 cycles

FIRST OFFICER`S FLASHLIGHT HOLDER BROKEN. R & R FIRST OFFICER`S FLASHLIGHT HOLDER IAW AM 33-50-16.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,014 hrs · 23,945 cycles

F/O FLASHLIGHT QUIT WORKING. R & R F/O FLASHLIGHT. OPS CHECKED GOOD IAW AMM 33-50-16.

Part: FAN — FAILED (LT RECIRC) · airframe 27,496 hrs · 23,541 cycles

CREW REPORTED A HEAVY ELECTRICAL ODOR IN THE COCKPIT, DESCENDING ON ARRIVAL OUT OF 10000 FT (NO SMOKE NOTED). LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R LT RECIRCULATION FAN IAW AMM 21-24-01. NO SMOKE NOTED. CHECK FLIGHT WAS SATISFACTORY. ACFT RETURNED TO SERVICE.

Part: FITTING — WORN (AILERON) · airframe 26,959 hrs · 23,083 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON OUTBOARD PCA ATTACH LUG HAS MIGRATED HAT BUSHING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AILERON PCA FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,959 hrs · 23,083 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 59. THE AIRCRAFT WAS REMOVED FROM SERVICE. LEVEL OF CORROSION NOT SPECIFIED. REPAIRED OMEGA BEAM IAW EO EM-53MR-1518. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,959 hrs · 23,083 cycles

DURING MAINTENANCE INSPECTION FOUND THE CENTER OMEGA BEAM CORRODED AT FRAME 59. THE AIRCRAFT WAS REMOVED FROM SERVICE. LEVEL OF CORROSION NOT SPECIFIED. REPAIRED OMEGA BEAM IAW EO EM-53MR-1518. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 27,072 hrs · 23,185 cycles

DURING MX INSPECTION, FOUND THE NR 2 EMERGENCY LIGHT STRIP HAS BROKEN WIRE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 2 EMERGINGY LIGHT STRIP ASSY IAW AMM 33-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 27,072 hrs · 23,185 cycles

DURING MX INSPECTION FOUND THE LAST EMERGENCY LIGHT STRIP HAS A BROKEN WIRE ON ACFT SIDE OF CONNECTOR. THE ACFT WAS REMOVED FROM SERVICE. REPLACED THE CONNECTOR AT SP9502 IAW SWPM 20-50-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,960 hrs · 23,083 cycles

CENTER OMEGA BEAM HAS LIGHT CORROSION WHERE FLOORBEAM ATTACHES AT FRAME 59. REPAIRED IAW EO EM-53MR-1518, PART B.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 27,072 hrs · 23,185 cycles

DURING MX INSPECTION, FOUND THE EMERGENCY LIGHT ON THE MAIN DOOR DID NOT ILLUMINATE. THE ACFT WAS REMOVED FROM SERVICE. FOUND BULB LOOSE IN SOCKET. TIGHTENED BULB IAW 33-50-06. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 27,072 hrs · 23,185 cycles

DURING MX INSPECTION FOUND THE NR 2 EMERGENCY PROXIMITY FLOOR STRIP MISSING. THE ACFT WAS REMOVED FROM SERVICE. REPLACED THE NR 2 EMERGENCY PROXIMITY FLOOR STRIP ASSY IAW AMM 33-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CONTACTOR — MALFUNCTIONED (WINDOW HEAT) · airframe 26,634 hrs · 22,769 cycles

ON FLIGHT 3261 THE CREW REPORTED THAT WHILE ON FINAL THEY RECEIVED AN "EICAS" WINDSHIELD HEAT 2 FAIL. WITH THE MESSAGE, GOT A SLIGHT O-ZONE SMELL. DESELECTED HEAT 2 + SMELL DISSIPATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE WINDSHIELD HEAT 2 CONTACTOR, NO SMELL NOTED IAW EMB AMM 30-42-02. OPC BAD MSG WS HEAT 2 FAIL APPEARS IAW AMM 30-42-00. REMOVED AND REPLACED THE WINDSHIELD TEMP CONTROLLER IAW MM 30-42-01, OPS CHECK GOOD. CLEARED MEL 30-23, AUTH020654DM-C. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOUSING — BROKEN (FLASHLIGHT) · airframe 26,586 hrs · 22,728 cycles

ON FLIGHT 3248 THE CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT HOUSING WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT HOUSING IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 26,489 hrs · 22,649 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT ON THE PASSENGER DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT ON THE PASSENGER DOOR IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — WRONG PART (CABIN) · airframe 26,366 hrs · 22,543 cycles

ON FLIGHT 2975 THE FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHT ORANGE EXIT STRIP WAS OUT OF PLACE AND WAS OF THE WRONG SIZE STRIP LOCATED ON AISLE FLOOR A B AT ROW 10. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY STRIP AT EXIT ROW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,158 hrs · 22,372 cycles

DURING B INSPECTION FOUND THE ROW 7 EMERGENCY LIGHT STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ROW 7 EMERGENCY LIGHT STRIP IAW EMB-140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,771 hrs · 20,261 cycles

THE CREW REPORTED THE FIRST OFFICER'S FLASHLIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER'S FLASHLIGHT AS REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,431 hrs · 19,982 cycles

DURING MAINTENANCE VISIT FOUND THE FLOOR PROXIMITY EMERGENCY LIGHT STRIP AT 15A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW EMERGENCY LIGHT STRIP AT 15A IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,431 hrs · 19,982 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR PROXIMITY EMERGENCY LIGHT STRIP AT 15A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW EMERGENCY LIGHT STRIP AT 15A IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MOUNT — OUT OF POSITION (COCKPIT) · airframe 23,416 hrs · 18,872 cycles

ON FLIGHT 3267 THE CREW REPORTED THE FIRST OFFICERS FLASHLIGHT CHARGER MOUNT IS NOT MOUNTED THE RIVETS PULLED OUT. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16. THE OPEERATIONAL CHECK WAS GOOD. MEL ITEM RESTORED, MIC SHEET CLEARED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,112 hrs · 19,707 cycles

DURING MAINTENANCE BASE VISIT FOUND THE SERVICE DOOR TRIM PANEL EMERGENCY LIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EXTERIOR LIGHT LAMP IAW AMM 33-50-09. TROUBLESHOT AND FOUND NO VOLTAGE TO SPLICE SP 7376. ALL OTHER EMREGENCY LIGHT OPERATIONAL CHECKS WERE GOOD IAW AMM 30-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — JAMMED (MAIN DOOR) · airframe 22,285 hrs · 19,022 cycles

ON FLIGHT 2713 THE CREW REPORTED THE MAIN DOOR HANDLE JAMS IN THE VERTICAL POSITION AND THE DOOR IS EXTREMELY DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH MAIN DOOR HANDLE TEST. FOUND MAXIMUM PRESSURE AT 36 LBS TO OPEN, 25 LBS TO CLOSE. NO FURTHER ACTION REQUIRED IAW AMM 25-18-00-820-801-A. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 22,213 hrs · 18,967 cycles

ON FLIGHT 2710 THE CREW REPORTED THAT DURING THE DESCENT ENTERED AREA OF PRECIPITATION AND STARTED SMELLING LIGHT ELECTRIC SMOKE BUT SAW NONE. THEY EXITED THE PRECIPITATION AND THE ODOR WENT AWAY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RAN AIRCRAFT APU IAW EMB 140 AMM 49-13-00 NO FAULTS FOUND AT THIS TIME COULD NOT DUPLICATE PROBLEM AT THIS TIME. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DRAIN LINE — UNSECURE (WINDOW) · airframe 22,175 hrs · 18,936 cycles

ON FLIGHT 2801 THE CREW REPORTED THAT DURING THE CLIMB (20,000FT) NOTICED A STRONG ODOR OF ELECTRICAL SMOKE/FIRE (NO SMOKE, NO FIRE) IN THE COCKPIT AND CABIN. THE AUTOPILOT FAILED WHEN INITIATED DURING TURN AND DESCENT. THE CREW FOLLOWED PROCEDURES AND THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO SGF. WHILE RETURNING TO SGF THE FLIGHT ATTENDANT IDENTIFIED THE ODOR COMING FROM ABOVE HER JUMPSEAT. THE AIRCRAFT LANDED WITHOUT INCIDNET. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/A: INSPECTED LEFT HAND POWER DISTRBUTION, FOUND CAPTAIN’S DV WINDOW LEAKING WATER ON RELAYS, RESECURED CAPTAIN’S WINDOW DUCT DRAIN TUBE IAW STANDARD MAINT PRACTICES. DRIED RELAYS AND RELAY RACK FOUND NO DEFECTS TO RELAYS OR RACK. REPAIRED CAPTAIN’S DV WINDOW FRAME SEAL IAW EMB AMM 56-11-03. RAN AIRCRAFT AND PRESSURIZED TO DELTA P 4.5 PSIG IAW EMB AMM 21-31-00. FOUND NO LEAKS, FAULTS, ODORS OR FUMES. THE AUTOPILOT SYSTEM CHECKED GOOD IAW EMB AMM 22-11-00. NO DEFECTS NOTED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 21,875 hrs · 18,662 cycles

ON FLIGHT 4417 DURING CLIMB THROUGH AT FLIGHT LEVEL 190-2000 IN MODERATE TURBURLANCE THE CREW REPORTED, BEGAN TO SMELL A STRONG ELECTRICAL BURNING ODOR LASTING ABOUT 1 MINUTE. THE CREW COULD NOT ISOLATE IT BUT SOMETHING WAS THERE. ICE PROTECTION WAS NOT ON. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. MAINTENANCE COULD NOT ISOLATE ANY ODOR ALL CIRCUIT BREAKERS CHECKS WERE OK. NO NEW CMC MESSAGES, ALL SYSTEMS OK. INSPECTED IAW EMB WM 20-10-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT OK FOR SERVICE AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (DOOR FRAME) · airframe 20,353 hrs · 17,343 cycles

ON FLIGHT 3949 FLIGHT ATTENDANT REPORTS CABIN DOOR VERY HARD TO OPEN GETS HUNG UP AND WONT OPERATE SMOOTHLY. AIRCRAFT REMOVED FROM SERVICE. CLEANED AND LUBRICATED ALL MAIN DOOR FRAME ROLLERS IAW EMB-140 AMM 53-21-02. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FS 24)

THE LEFT OMEGA BEAM AFT OF FRAME 24 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. PREPARED A DOUBLER, FILLER AND SHIMS FOR REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 30, CHAPTER 53-00-10 FIG 202. (M)

Part: FRAME — CRACKED (FUSELAGE)

FOUND FRAME 68 WAS FOUND CRACKED AT THE BAGGAGE DOOR STAY ROD HOLDER CUP BRACKET. PERFORMED CUT OUT OF FRAME 68 TO REMOVE THE DAMAGE. FABRICATED AN ANGLE SPLICE AFT AND ONE FOR FORWARD. FABRICATED A CUP SUPPORT. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/5216A, DATED SEPT 21, 2005. (M)

Part: SILL — CORRODED (FUSELAGE)

THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND CLEANED THE AREA. INSTALLED SERVICEABLE SILL IAW EMB REPAIR STATEMENT IC2005-145/5419 DATED SEPT 27, 2005. (M)

Part: FLOOR SUPPORT — CORRODED (FS 20)

THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. PREPARED DOUBLER, FILLER AND SHIMS FOR THE REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 30, CHAPTER 53-00-10 FIG 201. (M)

Part: BEAM — CORRODED (FRAME 24)

THE CENTER BEAM AT FRAME 24 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. FABRICATED A FILLER, DOUBLER AND SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC 2005-145/5255 DATED SEPT 21, 2005 AND EMB 145 SRM, SRM EMB 145/1142 REV 30, CHAPTER 53-00-10 FIG 203. (M)

Part: SILL — CORRODED (CARGO DOOR)

THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. REMOVED EXISTING LOWER SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 30) CHAPTERS 51-40-2, 51-20-03 AND 51-40-06. (M)

Part: BATTERY — DISCHARGED (CABIN)

DISC SEVERAL EMERGENCY EXIT SIGNS IN THE FORWARD CABIN WILL NOT ILLUMINATE. REPLACED BATTERY CHARGER AND BATTERY PACK IAW WC 33-700-19. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. CHARGER ASSEMBLY PN OFF IS 110049 AND SN OFF IS 17435. (K)

Part: MODULE — FAILED (EMERGENCY LIGHT)

NOTIFIED BY MAINTENANCE, EMERGENCY LIGHTS DO NOT TURN OFF AFTER F/A TESTS WITH BATTERIES ON AND EMERGENCY LIGHT ARMED ALSO SHOWING 'EMER LT NOT ARMED' ON EICAS. REPLACED EMERGENCY LIGHT OVERHEAD PANEL MODULE ASSEMBLY. OPS CHECK GOOD. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING A MBV INSPECTION, FOUND STRINGER 19L WAS FOUND TO BE CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-24-02 FIGURE 201. (M)

Part: FLASHLIGHT — ODOR (CABIN)

FLT 3803 - CREW REPORTED AN ELECTRICAL ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS AND FLIGHT ATTENDANTS FLASHLIGHT ASSEMBLIES. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)