N638AE

Part: NONE — NONE · airframe 48,694 hrs · 45,434 cycles

PDIS 638 36-21 2745471 30NOV21 ROA CLOSE BLEED 2 LEAK MSG IN FLIGHT FACT 30NOV21 12:33 ROA C/W FIM TASK 36-20-00-810-802 INSPECTED AND FOUND V BAND CLAMP ON IB SIDE OF Y PIPE IN PYLON LOOSE REMOVED AND REPLACED CLAMP PER AMM 36-11-09 C/Q AIR BLEED SYSTEM OPS CHECK PER AMM 36-00-00. OPS AND LEAK CHECK GOOD

Part: CONTROL CABLE — FRAYED (ELEVATOR SERVO) · airframe 47,954 hrs · 44,610 cycles

FLIGHT CREW: WHEN DOING THE FLIGHT CONTROL CHECK (FWD AND AFT) CREW FELT A STICKING POINT. MAINTENANCE: DISCOVERED THAT THE ELEVATOR SERVO BRACKET CABLE WAS CORRODED AND FRAYED. REMOVED AND REPLACED ELEVATOR SERVO BRACKET ASSEMBLY AND TENSIONED CABLE IAW 27-31-01 AND 22-11-04. OPTS CHECK GOOD OK FOR SERVICE AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 47,890 hrs · 44,526 cycles

COMING THROUGH 31K FEET. STRONG ODER NOTICED IN COCK PIT/CABIN. DISSIPATED GOING BACK THROUGH 31K FEET. OCCURRING INTERMITTENTLY ON DESCENT. COULD DUPLICATE ON GROUND WITH PACKS. INSPECTED RELAY AND DISTRIBUTION BOX PANELS, NO DEFECTS NOTED. R/R'D #2 RE-CIRCULATION FAN. OPS CHECKS GOOD IAW 221-24-01-04.

Part: PUMP — FAULTED (HYD SYSTEM) · airframe 47,866 hrs · 44,496 cycles

IN CRUISE FLIGHT AT 10K, $2 HYD PSI SPIKED TO 3,800 PSI FOLLOWED BY LOSS OF #2 HYD QUNTY AND SYSTEM PSI DROPPED TO ZERRO. ELECTRIC DRIVEN PUMP TURNED OFF AFTER 5 TO 10 MINUTES. (EICAS MESSAGE OF HYD SYS 2 FAIL). REMOVED AND REPLACED #2 HYD ENG DRIVEN PUMP IAW AMM 29-10-03. OPS CHECK GOOD. LEAK CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: ECS — ODOR (COCKPIT) · airframe 47,619 hrs · 44,228 cycles

PDIS 638 21-01 2554732 10APR21 CMI CLOSE BURNING SMELL AT 100 KNOTS IN COCKPIT QUICKLY DISSIPATED AFTER REJECTED TAKE OFF, FACT 11APR21 04:10 CMI PERFORMED FIM 21-20-00-810-801-A. NO DEFECTS NOTED NO BURNING SMELL FOUND. GROUND RAN ENG AND PACK TO FULL POWER NO SMELL FOUND PERFORMED TAXI CHECK NO SMELL OR DEFECTS NOTED AC OK FOR SERVICE CLEAR MEL 21-13-3

Part: A/C PACK — OVERHEATED (NR 1) · airframe 47,221 hrs · 43,791 cycles

POOR AIR FLOW COCKPIT AND PACK 1 OVERHEAT WITH BURNING SMELL. OPERATED PACKS CORRECTLY, IAW AMM 21-00-00-810-001A AND FOLLOWED FIM TASK 21-51-00-810-803A AND CONFIRMED A TRANSITORY CONDITION CAUSED BY OPERATOR ERROR. OPERATIONS CHECK GOOD. AIRCRAFT OK FOR SERVICE. CLEAR MEL.

Part: CONTACTOR — BURNED (APU LINE) · airframe 47,154 hrs · 43,716 cycles

PDIS 638 49-10 2346991 13DEC20 MDT CLOSE. WHEN PILOT TURNED ON HIS APU HE HAD SHED BUS 1 AND 2 OFF LINE FOLLOWED BY APU GEN OFF BUSS AND ELECTRICAL BURNING SMELL. FACT 13DEC20 23:10 MDT. APU LINE CONTACTOR SHOWS SIGNS OF BURN DAMAGE. R & R APU LINE CONTACTOR, REF AMM 24-34-03. RAN APU FOR 30 MIN. OPERATIONS CHECK GOOD, NO ELECTRICAL SMELLS AT THIS TIME. OK FOR SERVICE.

Part: STARTER GEN — MALFUNCTIONED (APU) · airframe 47,150 hrs · 43,712 cycles

APU GEN OFF BUS MESSAGE APPEARED ON EICAS WITH CLICKING NOISE AND ELECTRICAL BURNING SMELL IN COCKPIT. RESTARTED APU WITH GEN OFF NO SMELL NOTED OR CB S POPPED. R & R APU START GEN, IAW W/C 24-80-01. OPERATIONS CHECK GOOD.

Part: SLEEVE — DAMAGED (A/C PACK DUCT) · airframe 47,045 hrs · 43,598 cycles

PDIS 638 21-01 2346581 07NOV20 PHL CLOSE. FOLLOWING A/I TEST IN FLT, F/A REPORTED RUSHING AIR NOISE FROM MIDDLE OF CABIN, BURNING SMELL NOTED SHORTLY AFTER. SHUT OFF PAC 1 AND NOISE AND SMELL DISAPATED. 36444 00 SMS FACT 07NOV20 09:53 PHL. R & R FLEX SLEEVE ON NR 1 AC PACK DUCT, IAW EMB 145 AMM 36-11-09-04. OPERATIONS CHECK GOOD, OK FOR SERVICE THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,934 hrs · 43,470 cycles

PDIS 638 21-21 2416061 07SEP20 RIC CLOSE. STRONG CHEMICAL ODOR PRESENT IN COCKPIT. OBSERVED WITH PACKS RUNNING. FACT 07SEP20 06:21 RIC. R/R APU CONTACTOR K0291 IN REF TO AMM 24-60-01-000/400-801A. AS MAINTENANCE PRECAUTION R/R APU GCU IAW AMM 34-24-02-000/400-801A . OPERATIONS CHECK GOOD, OK FOR SERVICE. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: CONTACTOR — BURNED (FUEL PUMP) · airframe 46,880 hrs · 43,418 cycles

ON ARRIVAL TO FLIGHT DECK, NOTICED PLASTIC, ELECTRICAL ODOR. MX FOUND CONTACTOR K0119 FOR 1A FUEL PUMP BURNED. ACFT HAS PRIOR HISTORY. R & R THE CONTACTOR IAW AMM 28-21-14. OPS CHECKED IAW AMM 28-45-00. OPS CHECK GOOD, OK FOR SERVICE.

Part: CONTACTOR — BURNED (COCKPIT) · airframe 46,866 hrs · 43,398 cycles

BURNING PLASTIC SMELL IN FLIGT DECK. FOUND BURNT CONTACTOR K0291 BEHIND LIFE VEST STORAGE PANEL. R/R CONTACTOR IAW AMM 24-34-04. OPS CHECK GOOD. OK FOR SERVICE. PERFORMED MAIN GENERATOR TEST IAW AMM 24-31-00.

Part: WIRE — DETACHED (EMERGENCY LIGHT) · airframe 46,512 hrs · 42,988 cycles

EMERGENCY LIGHT ON MAIN DOOR INOP.... RE-ATTACHED WIRES TO THE ELECTRIC CONNECTORS FOR THE EMERGENCY LIGHT. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,360 hrs · 42,807 cycles

AFTER TAKEOFF CREW NOTED PUNGENT ELECTRICAL/BURNING ODOR IN COCKPIT. SMELL CLEARD SHORTLY AFTER LANDING. MX T/S ISSUE IN REF TO FIM 21-20-00-810-801-A. NO DEFECTS NOTED. PERFORMED OPS CHECKS OF BOTH BLEED SYST EMS, BOTH PACK SYSTEMS AND ANTI ICING SYSTEMS WITH CREW. NO DEFECTS NOTED. OK FOR SERVICE. MX T/S BURNING SMELL REF LP 221437-1. REMOVED R/H AND L/H RELAY PANELS AND INSPECTED RELAYS. NO DEFECTS NOTED. REINSTALLED BOTH R/H AND L/H RELAY PANELS. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,123 hrs · 42,515 cycles

PDIS 638 05-50 1995782 20OCT19 GSO CLOSE BURNING ODOR OBSERVED A 26,000 ICING CONDITIONS. SME LL DISSIPATED AT 5000 FT. FACT 20OCT19 13:37 GSO INSP LIGHTS AND PUSHBUTTONS IN COCKPIT NO DISCREPANC IES FOUND PERFORMED OPS CHECK OF ANTI ICE IAW AMM 30 -00-00 OPS CHECK GOOD PERFORMED TEST OPS CHECK OF BO TH 1 AND 2 W/S HT OPS CHECK GOOD. NO DEFECTS FOUND N O BURNING ODOR DETECTED OK FOR SERVICE.

Part: GENERATOR — MALFUNCTIONED (NR 3) · airframe 45,906 hrs · 42,278 cycles

GEN #3 SHOWING AMBER DASHES AND 0 AMPS DURING FLIGHT. FIX: R&R GEN 3 IAW AMM 24-31-01 LEAK AND OPS CHECK GOOD. NOTE: AIRCRAFT DIVERTED FROM YQB TO ALB TO BE FIXED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 45,233 hrs · 41,531 cycles

NDIS 638 33-51 0011560 28APR19 SBY CLOSE SERVICE DOOR EMERGENCY LIGHT IS INOP 30100 00 BAD FACT 28APR19 08:18 SBY R&R'D LAMP NO FIX. INSPECTED & FOUND BROKEN WIRE R&R PIN AT QUICK DISCONNECT P/N ON 1015743

Part: A/C PACK — ODOR · airframe 45,164 hrs · 41,452 cycles

638 21-01 2098402 16APR19 FLO CLOSE ON TAKEOFF FLIGHT DECK FILLED WITH SMELL.ON APPROACH SMELL/HAZE RETURNED AND DISAPATED BEFORE LANDING. 26803 00 SMK MEL 16APR19 14:25 FLO C10615 21-13-3 AIR CONDITIONING PACK FACT 16APR19 18:07 CLT PER INSTRUCTIONS FROM MX CONTROL THIS ITEM IS CLOSED AND REPLACEMENT WITH ALTERNATIVE 21-13-1 REF LP 209841-2

Part: FLAP — OUT OF RIG (WING) · airframe 44,740 hrs · 40,983 cycles

PDIS 638 27-50 2047071 23JAN19 PHL CLOSE FLAPS FAIL MSG IN FLT AFTER T/O WHEN SETTING FLAPS TO ZERO. FACT 24JAN19 22:25 PHL FOUND FLAPS TO BE OUT OF RIG. PERFORMED FLAP ZERO-DEGREE RIGGING IAW AMM 27-53-04. OPS CHECK GOOD OK FOR SERVICE AT THIS TIME.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 44,304 hrs · 40,461 cycles

NDIS 638 33-51 0007300 30OCT18 RIC CLOSE AFT CABIN EMERGENCY FLASHLIGHT INOP 28629 00 NGR FACT 30OCT18 07:35 RIC R/R BULB IN AFT CABIN EMERGENCY FLASHLIGHT AS REQ OPS CHECK GOD OK FOR SERVICE.

Part: FAN — ODOR · airframe 44,241 hrs · 40,387 cycles

PDIS 638 21-24 1595132 17OCT18 PHL CLOSE ELECTRICAL SMELL OBSERVED AFTER APU ATTEMPTED START. OUTSIDE OF AIRCRAFT NEAR GPU PLUG-IN. 76840 00 VAG HISTORY: FACT 17OCT18 22:20 PHL INSP AND FOUND EXHAUST FAN SMELLING BURNT R&R EXHAUST FAN. OPS CHECK FAILED. SEE SEQ 3 FOR MEL.

Part: UNKNOWN — FUMES (CABIN) · airframe 44,106 hrs · 40,241 cycles

PDIS 638 21-01 1682341 21SEP18 PHL CLOSE WHILE STARTING EITHER #1 OR #2 ENG OFF APU, FUMES ARE PRESENT THROUGHOUT A/C. APU TEMP SPIKES TO MID 600 DEGREES 21585 00 EK HISTORY: . FACT 21SEP18 18:07 PHL WHILE STARTING ENGS OFF OF APU IAW PIEDMONT MAINTENANCE OPERATING MANUAL, NO FUMES IN A/C ARE OBSERVED. OK FOR SERVICE

Part: UNKNOWN — ODOR (COCKPIT) · airframe 43,019 hrs · 39,928 cycles

DURING CRUISE, CREW BEGAN TO SMELL AN UNUSUAL ODOR ACCOMPANIED BY RADIO STATIC. ODOR AND STATIC DISAPPEARED AFTER LEAVING PRECIP. FA DID NOT NOTE THE ODOR IN THE CABIN. PERFORMED ENGINE RUN, CAN NOT DUPLICATE ODOR IN THE FLIGHT DECK. AIRCRAFT OKAY FOR SERVICE.

Part: INDICATOR — FALSE INDICATION (FUEL SYS) · airframe 43,398 hrs · 39,422 cycles

DURING TAXI OUT, THE NR 1 FUEL TANK LEVEL FLUCTUATED FROM 42 - 4600 LBS. AFTER DEPARTURE THE NR 2 TANK CONTENTS AND TOTAL FOB INDICATIONS ON MFD AND EICAS SHOWED DASHES AND FUEL 1 LOW LEVEL EICAS MESSAGE DISPLAYED. COMPLIED WITH QRH PROCEDURES. R & R THE REPEATER INDICATOR IAW MM 28-23-08. OPS CHECKED GOOD.

Part: INLET — ICED (NR 2 ENGINE) · airframe 43,177 hrs · 39,191 cycles

NR 2 ENGINE REPORTED FOD IN INLET. REMOVED ICE FROM THE NR 2 ENGINE INLET

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 43,019 hrs · 39,025 cycles

CABIN ALTITUDE REACHED 13,500 FT AT FL190. AUTO PRESSURE MODE HAD NO EFFECT. MANUAL MODE BEGAN TO WORK AT 10,000 FT, MAINTAINING CABIN ALTITUDE OF 5,500 FT. CABIN ALTITUDE JUMPED UNCONTROLLABLY UP IN 200 FOOT INCREMENTS. CABIN DIFFERENTIAL PRESSURE. REMAINED IN GREEN.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 43,017 hrs · 39,024 cycles

SLOW LOSS OF PRESSURIZATION AT 34,000 FT. PRESSURIZATION STABILIZED AROUND 15,500 FT. SMALL POP IN CABIN AT THE TIME CABIN ALTITUDE WENT AMBER. R & R THE CABIN PRESSURE CONTROLLER AND PERFORMED AN OPS CHECK IAW AMM 21-31-01, 21-31-00-700-801-A, AND 21-31-00-700-802-A. OPS CHECKED GOOD. OKAY FOR SERVICE.

Part: OXYGEN MASK — MALFUNCTIONED (SEAT 6A) · airframe 43,017 hrs · 39,024 cycles

SEAT 6A OXYGEN MASK DID NOT DEPLOY. PERFORMED AN OPS CHECK OF THE PAX OXYGEN MASK IAW AMM 35-20-00, NO DEFECTS NOTED. OKAY FOR SERVICE.

Part: INDICATOR — MALFUNCTIONED (FUEL QTY) · airframe 43,014 hrs · 39,020 cycles

FUEL 1 LOW LEVEL MESSAGE AND NR 2 TANK INDICATED ZERO. RANDOM INDICATIONS. ALSO LOST TOTAL FUEL USED. CMC SHOWS FUEL 1 LO LEVEL MESSAGE. PERFORMED A CHECK ON THE REFUELING PANEL, NO FAULTS FOUND. CLEANED CONNECTORS ON FCU AND PERFORMED AN ELECTRICAL FUEL QTY OPS CHECK IAW AMM 28-41-00-700-801-A-500. OPS CHECKED GOOD, NO DEFECTS NOTED. VERIFIED FUEL QTY ON COCKPIT AND REFUELING PANEL MATCHES MAGNASTICK READING.

Part: FRAME — CHAFED (FRM 65) · airframe 43,010 hrs · 39,015 cycles

RIGHT FRAME 65 IN CARGO BAY HAS A CHAFE NEAR STINGER 12R. REPAIRED IAW ERS-EM-53MR-3082.

Part: FRAME — CRACKED (FRM 66) · airframe 43,010 hrs · 39,015 cycles

FRAME 66 IS CRACKED BETWEEN STRINGERS 17 TO 18L. REPAIRED THE FRAME IAW SRM 53-00-04, AND SRM 51-40-02.

Part: SKIN — PUNCTURED (RUDDER) · airframe 43,010 hrs · 39,015 cycles

RIGHT SIDE OF RUDDER HAS A HOLE IN THE SKIN NEAR THE LOWER AFT CORNER. REPAIRED THE RUDDER LOWER SKIN IAW ERS EM-55MR-632.

Part: FITTING — GOUGED (RT AILERON) · airframe 43,010 hrs · 39,015 cycles

RIGHT AILERON PCA FITTING IS GOUGED. REMOVED AND REPLACED THE RT AILERON PCA FITTING IAW EO EM-27MR-112.

Part: FLOOR SUPPORT — CORRODED (FRAMES 58 - 59) · corrosion level 2 · airframe 43,010 hrs · 39,015 cycles

LEFT OMEGA BEAM IS CORRODED BETWEEN FRAMES 58-59. REPAIRED THE LEFT OMEGA BEAM IAW EO EM-53MR-1518.

Part: FLOOR SUPPORT — CORRODED (FRAMES 58-59) · corrosion level 2 · airframe 43,010 hrs · 39,015 cycles

RIGHT CENTER OMEGA BEAM IS CORRODED BETWEEN FRAMES 58 - 59. REPAIRED THE OMEGA BEAM IAW EO EM-53MR-1518.

Part: TORQUE BOX — CRACKED (PAX DOOR) · airframe 43,010 hrs · 39,015 cycles

PAX DOOR INNER HANDLE TORQUE BOX HAS A .750 INCH CRACK. REPAIRED THE SUPPORT IAW EO EM-52MR-250.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 43,010 hrs · 39,015 cycles

CARGO DOOR SILL HAS AN AREA OF CORROSION. INSTALLED A NEW DOOR SILL IAW 51-40-02.

Part: ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 43,010 hrs · 39,015 cycles

LEFT WING UPPER WING TO FUSELAGE PANEL, LOWER ANGLE, SECOND FROM AFT END IS CRACKED AT THE AFT END. R & R THE LT WING SECOND FROM AFT UPPER WING TO FUSELAGE PANEL ANGLE IAW SRM 51-20-02 AND ETN-EM-53-142.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 43,010 hrs · 39,015 cycles

SHEAR TIE AT FRAME 80, STRINGER 7R IS CRACKED APPROXIMATELY 1 INCH. R & R THE SHEAR TIE IAW SRM 51-40-02.

Part: ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 43,010 hrs · 39,015 cycles

LEFT WING UPPER WING TO FUSELAGE PANEL, LOWER ANGLE, FIRST FROM AFT END IS CRACKED AT FORWARD END. R & R THE ANGLE IAW SRM-51-20-02 AND ETN-EM-53-142.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 43,010 hrs · 39,015 cycles

SHEAR TIE AT FRAME 80, STRINGER 7L IS CRACKED APPROXIMATELY 1 INCH. R & R THE SHEAR TIE IAW SRM 51-40-02.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,615 hrs · 38,660 cycles

ROW 3 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 3 INVERTER IAW AMM 33-50-11 AND WM 33-50-50. EMERGENCY LIGHTING SYSTEM OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME

Part: LIGHT — INOPERATIVE (LTWING) · airframe 42,505 hrs · 38,536 cycles

LT WING AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP AT LT WING AFT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-50-10. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,234 hrs · 38,271 cycles

ROW 12 CEILING EMERGENCY LT INOP. REMOVED AND REPLACED ROW 12 CEILING EMERGENCY LIGHT BULB IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A OPC GOOD END.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 41,653 hrs · 37,784 cycles

AFT EMERGENCY FLOOR LIGHTING INOPERATIVE. SECURED INVERTER CONNECTOR. OPS CHECKED GOOD IAW AMM 33-50-11.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 41,294 hrs · 37,486 cycles

MAIN DOOR EXTERIOR EMERENCY LIGHT INOPERATIVE. FOUND A WIRE BROKEN AT SPLICE REMOVED AND REPLACED WIRE TERMINAL AND RECEPTICLE IAW SWPM 20-21-00. OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 41,231 hrs · 37,434 cycles

OVERHEAD EMERGENCY LIGHT INOP IN ROW 12 (EXIT SIGN). RESECURED EMERGENCY LIGHT CONNECTOR AND OPS CHECK GOOD IAW EMERGENCY LIGHT TEST AMM 33-50-00.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 41,163 hrs · 37,379 cycles

FA FWD FLASHLIGHT INOPERATIVE. REMOVED & REPLACED THE FLASHLIGHT, OPS OK IAW AMM 33-51-01.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 41,053 hrs · 37,277 cycles

FWD CABIN FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD CABIN FLASHLIGHT IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,850 hrs · 37,095 cycles

LT FWD OVERWING EMERGENCY EXIT LIGHT INOP. R&R NR 1 BATTERY POWER SUPPLY IAW AMM 33-50-04. EMERGENCY LIGHTS OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,205 hrs · 36,536 cycles

DURING PS-1 CHECK FOUND FORWARD FLOOR PROXIMITY STRIP INOPERATIVE. EMERGENCY LIGHTING PROXIMITY STRIP. R & R FORWARD FLOOR PROXIMITY EMERGENCY LIGHTING STRIP IAW AMM 33-50-12. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM IAW AMM 33-50-00. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,193 hrs · 36,527 cycles

AFT CABIN CEILING EMERGENCY LIGHT INOPERATIVE. R & R AFT CABIN CEILING EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-08-000-801-A AND TASK 33-50-08-400-801-A. OPS CHECK GOOD.

Part: BOLT — SHEARED (PAX DOOR HANDLE) · airframe 39,907 hrs · 36,242 cycles

FA REPORTED MAIN CABIN DOOR HANDLE LAST 2 INCHES OF TRAVEL DIFFICULT AND DOOR SEAL SQUEALING IN FLIGHT. FOUND BOLT ON MAIN PAX DOOR HANDLE BOX ASSY SHEARED. INSTALLED NEW BOLT IAW AMM 20-10-01. ALSO LUBRICATED DOOR AND ALL MECHANISMS IAW AMM 52-18-00. OPS CHECKED GOOD IAW AML PG 4011626 ITEM 3 FOR SQUEALING FOUND ON SERVICE DOOR.

Part: CONTROL MODULE — FAILED (CABIN LIGHTS) · airframe 39,901 hrs · 36,238 cycles

CREW REPORT ELECTRICAL BURNING ODOR NEXT TO PASSENGER DOOR. CABIN LIGHTS CONTROL MODULE FOUND BAD. REMOVED AND REPLACED IAW AMM 33-21-01 AND OPS CHECKED GOOD. NO OTHER ELECTRICAL BURNING ODORS NOTICED.

Part: CONTROL MODULE — FAILED · airframe 39,872 hrs · 36,210 cycles

ARRIVAL, ACFT NO POWER SELECTED, BUT GPU AVAILABLE LIGHT, NOT SELECTED) FO TURNED BATTS ON MFD SHOWED GPU VOLTAGE AT 37.7 V INTERIOR SIDE WALL LIGHTS ON ALL LEFT HAND SIDE INOP AND SHE (FA) SMELLED A FAINT BURNING ODOR. REMOVED AND REPLACED CONTROL MODULE I.A.W EMB 145 AMM 33-21-01. OPS CHK GOOD AT THIS TIME.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 39,539 hrs · 35,898 cycles

FLIGHT ATTENDANT HAS DIFFICULT TIME CLOSING THE MAIN DOOR. THE TOP PART OF THE DOOR STAYS OPEN. LUBED AIRFRAME DOOR ROLLERS. PERFORMED OPERATIONS CHECK OF MAIN PAX DOOR IAW AMM 52-18-00. OPERATIONS CHECKED GOOD.

Part: REINFORCEMENT — CRACKED (FUSELAGE) · airframe 39,076 hrs · 35,465 cycles

REINFORCEMENT FRAME ABOVE LT WINDSHIELD LATERAL POST CRACKED, PERMANENT REPAIR. R & R REINFORCEMENT ABOVE LATERAL POST IAW ERS-EM-53MR-203.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,100 hrs · 35,485 cycles

FRAME 75, STRINGER 1R - 3R, UPPER AREA FASTENER HAS CRACKS. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-1959.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,100 hrs · 35,485 cycles

FRAME 75, STRINGER 1L - 3L, UPPER AREA SKIN HAS CRACKS. PERFORMED PERMANENT REPAIR OF UPPER SKIN AT FRAME 75, STRINGER 1L - 3L, IAW ERS-EM-53MR-195.

Part: WIRE — BROKEN (CABIN) · airframe 39,076 hrs · 35,465 cycles

LEFT 66 FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRE AT BASE OF LIGHT. R & R NR 6 PROXIMITY LIGHT STRIP IAW AMM 33-50-12.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,076 hrs · 35,465 cycles

CORROSION ON SKIN, FRAME 67, BETWEEN STRINGER 21L - 21R. ACCOMPLISHED PERMANENT REPAIR IAW ERS-EM-53MR-1945.

Part: WIRE — BROKEN (CABIN) · airframe 39,076 hrs · 35,465 cycles

LEFT NR 5 FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRE AT BASE OF LIGHT. R & R NR 5 PROXIMITY LIGHT STRIP IAW AMM 33-50-12.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,076 hrs · 35,465 cycles

SKIN CORROSION FRAME 65 - 66, BETWEEN STRINGER 21L - 21R. ACCOMPLISHED PERMANENT REPAIR IAW ERS-EM-53MR-1944.

Part: WIRE — DAMAGED (CABIN) · airframe 39,076 hrs · 35,465 cycles

LEFT NR 1 EMER LIGHT STRIP WIRES PULLED OFF. R & R LT NR 1 FLOOR EMER LIGHT STRIP IAW AMM 33-50-12.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,076 hrs · 35,465 cycles

E492453 INTERNAL SKIN CORRODED, BETWEEN FRAME 13 - 14, STRINGER 21L - 20L. PERFORMED PERMANENT REPAIR OF INTERNAL SKIN CORROSION IAW ERS- EM-53MR-1933.

Part: HOLDER — CRACKED (CABIN) · airframe 39,076 hrs · 35,465 cycles

FOUR EACH PROXIMITY LIGHT HOLDERS, TWO EACH RT SIDEWALLS & ONE RAMP PANEL TRIM ARE CRACKED. R & R FOUR EACH PROXIMITY LIGHT HOLDERS, TWO EACH RT SIDEWALLS & ONE RAMP PANEL TRIM IAW AMM 33-50-12.

Part: WIRE — DAMAGED (CABIN) · airframe 39,076 hrs · 35,465 cycles

EMERGENCY LIGHT STRIPS HAVE DAMAGED WIRE INSULATION AT FLOOR PANELS 241DF, 251DF & 251HF. REPAIRED EMER LIGHT STRIP WIRES, TWO EACH AT FLOOR PANELS 241DF, 251DF & 251HF IAW SWPM 20-21-00, FOR OPERATIONS CHECK SEE E495678.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 39,076 hrs · 35,465 cycles

FORWARD GALLEY LOWER EXIT IDENTIFIER INOPERATIVE. R & R NR 2 EMER LIGHT DC & AC INVERTER IAW AMM 33-50-11. FWD GALLEY LWR EXIT IDENTIFIER LIGHT CHECKED GOOD. COMPLIED WITH OPERATIONAL CHECK OF THE EMER LIGHTING SYS.

Part: BATTERY — DISCONNECTED (FLASHLIGHT) · airframe 39,076 hrs · 35,465 cycles

CABIN AFT FLASHLIGHT INOPERATIVE. UPON FURTHER INVESTIGATION FOUND INTERNAL BATTERY DISCONNECTED. RE-CONNECTED BATTERY AS REQUIRED. OPERATIONAL CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 39,076 hrs · 35,465 cycles

NUMBER 1 EMER FLOOR LIGHT STRIP INOPERATIVE. R & R NR 2 EMER LIGHT DC & AC INVERTER IAW AMM 33-50-11. COMPLIED WITH OPERATIONAL CHECK OF THE EMER LIGHTING SYS.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 38,880 hrs · 35,311 cycles

RIGHT WING, EXT EMER LIGHT INOPERATIVE. R & R BULB RT WING LIGHT EMER IAW AMM 33-50-10. NO DEFECT NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,674 hrs · 34,195 cycles

LEFT SIDE CTR FAIRING EXTERNAL EMER LIGHT INOPERATIVE. R & R LT OVERWING EMER LIGHT LAMP IAW AMM 33-50-07. OPERATIONS CHECKED OK.

Part: SIGN — INOPERATIVE (CABIN) · airframe 37,238 hrs · 33,806 cycles

CEILING EMER EXIT ILLUMINATED SIGN AT OVERWING EXITS IS INOPERATIVE ON FWD SIDE. R & R FWD CEILING EMER EXIT ILLUMINATED SIGN AT OVERWING EXITS IAW AMM 33-50-15. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 37,181 hrs · 33,749 cycles

AISLE EMER LIGHT AT ROW 3 INOPERATIVE. R & R AISLE EMER LIGHT LAMP AT ROW 3 IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A, NO FIX. R & R NR 1 EMER LIGHT BATTERY POWER SUPPLY IAW WC 33-700-19. OPERATIONS CHECKED GOOD. EMER LIGHT BATTERY PN 2013-1ASMI, SN 67260.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 37,181 hrs · 33,749 cycles

COCKPIT EMER LIGHT INOPERATIVE. R & R COCKPIT EMER LIGHT LAMP IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A.. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 36,742 hrs · 33,329 cycles

OVERWING EMER LIGHT OUT. R & R LIGHT BULB IAW AMM 33-50-07.

Part: PRESSURE SWITCH — FAILED (NR 2 A/C PACK) · airframe 36,434 hrs · 33,006 cycles

ABORTED TAKEOFF DUE TO NR 2 PACK OCLD & NR 2 PACK OVERHEAT CAUTION MESSAGES. R & R OF HIGH STAGE PRESSURE SWITCH.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 36,259 hrs · 32,874 cycles

CAPTAIN`S FLASHLIGHT DIM. R & R CAPTAIN`S FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: COUPLING — DAMAGED · airframe 36,177 hrs · 32,803 cycles

TRANSFERRED FROM LOG PAGE 3715116 ITEM 1 MEL 21-27. C PACK 1 OVLD PACK 1 OVLD EICAS MSG DURING TAKEOFF ROLL. TAKEOFF ABORTED LOW SPEED. INSPECTED & FOUND COUPLING 11 WITH LARGE HOLE BLOWN THROUGH IT. R & R COUPLING IAW AMM 21-51-03 & ETN-EM-21-056. OPERATIONS CHECKED GOOD, LEAK CHECKED GOOD. THIS ACTION RESTORES MEL21-27.

Part: COWLING — CRACKED (LT ENGINE) · airframe 35,914 hrs · 32,564 cycles

WHILE ACCOMPLISHING PART C OF ERS-EM-54DF-164, HFEC INDICATED 2 1/2 INCH CRACK, 3/8 INCH FWD OF RIVET ROW, LT LOWER ENG COWL, IN LOWER FWD AREA, IN 6 INCH X 6INCH PRIMED AREA AFTER CONTOURED. R & R LOWER ENG COWLING IAW AMM 71-11-01.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 35,864 hrs · 32,526 cycles

HI SPEED ABORT 80 KNOTS GPWS INOPERATIVE. TERR INOP CAUTION. ITEM DEFERRED IAW MEL 34-10. PERFORMED HIGH ENERGY STOP INSPECTION IAW MM 5-20-16 NO DEFECTS NOTED AT THIS TIME.

Part: SIGN — INOPERATIVE (CABIN) · airframe 35,600 hrs · 32,279 cycles

EMERGENCY EXIT SIGN ON FWD BULKHEAD IN FRONT OF 3B INOPERATIVE. INSPECTED CONNECTORS FOR NR 3 DC & AC INVERTER. RECONNECTED AS REQUIRED. OPERATIONS CHECKED EMER LIGHT IAW AMM 33-50-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 35,568 hrs · 32,242 cycles

BLEED 2 LEAK INDICATION ON EICAS ONLY, APPLIED PROCEDURE & MSG REMAINED. WENT OUT AFTER APPROX 10 - 12 MINUTES. NO FURTHER INDICATION. PERFORMED LEAK TEST OF RT BLEED. OPERATIONS CHECK & LEAK CHECKED GOOD IAW AMM 36-00-00. NO FURTHER DEFECT NOTED.

Part: CONTROL UNIT — FAILED (BRAKE SYSTEM) · airframe 35,082 hrs · 31,744 cycles

ON LANDING BRAKE DEGRADE MSG FLASHED ON EICAS BRAKES WORKED ABOUT 1/2 NORMAL. USED THRUST REVERSE TO STOP. BRAKE TEMP ON OTBD BRAKES HIGH TO MID AMBER RANGE. INBD BRAKE TEMP LOW TO MID GREEN RANGE. R & R BCU IAW AMM 32-41-02, OPERATIONS CHECKED GOOD.

Part: ROLLER — DIRTY (PAX DOOR) · airframe 34,894 hrs · 31,557 cycles

PASSENGER DOOR DIFFICULT TO OPEN. CLEANED & LUBRICATED MAIN DOOR FRAME ROLLERS IAW EMB MM 53-21-02. OPERATIONS CHECK OF DOOR OK IAW MM 56-10-01.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 34,790 hrs · 31,460 cycles

FIRST OFFICER`S FLASHLIGHT CHARGING STATION NOT CHARGING. REPOSITIONED FIRST OFFICER`S FLASHLIGHT 33-5-16 AMM WORKING GOOD.

Part: SPAR — CRACKED (RT WING) · airframe 34,683 hrs · 31,370 cycles

RIGHT SPAR III CRACKED AT HARNESS CUTOUT. PERFORMED PERMANENT REPAIR ON RT SPAR III IAW ERS-EM-57MR-074.

Part: SPAR — CRACKED (LT WING) · airframe 34,683 hrs · 31,370 cycles

LEFT SPAR III CRACKED AT THE HARNESS CUTOUT. PERFORMED PERMANENT REPAIR ON LT SPAR III IAW ERS-EM-57MR-083.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,683 hrs · 31,370 cycles

FOUND LT LATERAL WINDSHIELD POST SKIN CRACKED. CUT OUT DAMAGE, INSTALLED DOUBLER & SHIMS IAW ERS-EM-53MR-203.

Part: WIRE — BROKEN (CABIN) · airframe 34,683 hrs · 31,370 cycles

EMERGENCY FLOOR PROXIMITY LIGHT STRIPS NR 2, 5 & 6 HAVE BROKEN OR DAMAGED WIRES. R & R NR 2, 5 & 6 EMERGENCY PROXIMITY LIGHT STRIPS TO COVER PANEL AS REQUIRED.

Part: WIRE — BROKEN (CABIN) · airframe 34,683 hrs · 31,370 cycles

EMERGENCY LIGHT STRIP WIRE IS BROKEN BETWEEN FRAMES 43 & 44. INSTALLED SPLICES SP9115 & SP9116 TO EMERGENCY LIGHT STRIP WIRE BETWEEN FRAMES 43 & 44 IAW SWPM 20-21-00 STEP 5.

Part: LIGHT — UNKNOWN (CABIN) · airframe 34,683 hrs · 31,370 cycles

LEFT NR 1 PROXIMITY LIGHT STRIP IS INCORRECT. R & R LT NR 1 PROXIMITY LIGHT STRIP IAW AMM 33-50-12.

Part: ROLLER — LACK OF LUBE (MAIN CABIN DOOR) · airframe 34,201 hrs · 31,005 cycles

MAIN CABIN DOOR HARD TO OPEN, CLOSE AND LOCK. LUBRICATED MAIN CABIN DOOR FRAME ROLLERS IAW 52-11-00. CHECKED GOOD IAW AMM 52-10-01.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,923 hrs · 30,784 cycles

F/A'S FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW CMM 25-60-02. OPS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,799 hrs · 30,681 cycles

SERVICE DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R SERVICE FOOR OVERHEAD EMERGENCY LIGHT LAMP IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,413 hrs · 30,371 cycles

LEFT OVERWING EMERGENCY LIGHT INOP. R & R LAMP IAW AMM TASKS 33-50-10-000-801-A/ 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 33,008 hrs · 30,049 cycles

THE CREW REPORTED THE F/A’S FLASHLIGHT WOULD NOT STAY SECURED IN ITS CHARGER. THE ACFT WAS REMOVED FROM SERVICE. R & R THE F/A’S FLASHLIGHT IAW AMM 33 51 01. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 32,710 hrs · 29,820 cycles

ON FLIGHT 3250 THE CREW REPORTED THAT ON TAXI-IN, INTPH 2 CB POPPED (33B). THE CREW NOTICED AN ELECTRICAL BURNING ODOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. CHECKED WIRE HARNESS' BEHIND GLARESHIELD PTT SWITCH, F/O HEADSET JACK PANEL, #2 ACP. NO EVIDENCE OF BROKE WIRES, NOR BURNT INSULATION, NOR ARCING. ABLE TO RESET CIRCUIT BREAKER (33B INTPH 2). BENT AND TWISTED ALL WIRE HARNESS' AND CIRCUIT BREAKER STAYED-IN. FIRST OFFICER’S AUDIO SYSTEM OPERATIONAL CHECK WAS GOOD IAW AMM 23-51-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 32,637 hrs · 29,762 cycles

DURING MAINTENANCE INSPECTION FOUND THE CAPTAIN’S EMERGENCY FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTIAN’S EMERGENCY FLASHLIGHT CRADLE IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — LOOSE (EMERGENCY LIGHT) · airframe 31,923 hrs · 29,245 cycles

FOR FLIGHT 4110 THE CREW REPORTED THE EMERGENCY LIGHT ARMING SWITCH WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TIGHTENED JAM NUT ON EMERGENCY LIGHT ARM SWITCH IAW STANDARD MTX PRACTICES. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 31,900 hrs · 29,226 cycles

DURING B INSPECTION FOUND THE FORWARD FACING CENTER AISLE EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. SECURED LOOSE CONNECTION ROW 12 FORWARD CEILING EXIT MARKING SIGN IAW EMB AMM 33-50-15-000-801/33-50-15-400-801. COMPLIED WITH EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK W/C 33-700-17. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 31,542 hrs · 28,945 cycles

ON FLIGHT 3536 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE FIRST OFFICER’S FLASHLIGHT. THE OPERATIONAL CHECK WAS GOOD IAW AMM 25-60-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 31,542 hrs · 28,945 cycles

ON FLIGHT 3536 THE CREW REPORTED THE CRADLE AND FLASHLIGHT BEHIND THE CAPTAIN’S SEAT WAS INOPERABLE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,539 hrs · 28,943 cycles

ON FLIGHT 9513 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT BATTERY AS PER EMB 145 MM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — UNSERVICEABLE (CABIN) · airframe 30,781 hrs · 28,379 cycles

FOR FLIGHT 3546 THE CREW REPORTED THAT WHEN THEY ARRIVED AT THE AIRCRAFT THE EMERGENCY LIGHTS WERE ON. THE AIRCRAFT HAD BEEN UNOCCUPIED FOR AT LEAST 25 MINUTES AND COULD NOT DETERMINE STATUS OF THE EMERGENCY LIGHT BATTERIES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 & 4 EMERGENCY BATTERY PACK IAW MM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — DIRTY (PAX DOOR) · airframe 30,639 hrs · 28,270 cycles

FLIGHT 4361, FLIGHT ATTENDANT UNABLE TO CLOSE MAIN CABIN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED CABIN DOOR SEAL IAW EMB 145 AMM 52-18-00. OPS CHECKED GOOD. THE AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LH OVERWING EMER) · airframe 30,381 hrs · 28,076 cycles

DURING B INSPECTION, FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB ON THE LEFT OVERWING IAW AMM TASK: 33-50-07-000-801-A, AND 33-50-07-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,011 hrs · 27,769 cycles

DURING B INSPECTION, FOUND THE AISLE EMERGENCY EXIT SIGN FORWARD SIDE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 EMERGENCY POWER SUPPLY UNIT IAW AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,999 hrs · 27,756 cycles

DURING B INSPECTIONS, FOUND THE NUMBER 4 AISLE EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 AISLE EMERGENCY LIGHT IAW AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — NOT SEATED (CABIN) · airframe 29,916 hrs · 27,695 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT EMERGENCY EXIT LIGHT IN AISLE CEILING INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEATED BULB IN AFT EMERGENCY EXIT AISLE CEILING AS REQUIRED. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MOUNT FITTING — CRACKED (RT ENGINE) · airframe 29,915 hrs · 27,694 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT LOWER YOKE 1 FORWARD ENGINE MOUNT FITTING CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FITTING IAW EO-EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — BROKEN (CABIN) · airframe 29,920 hrs · 27,698 cycles

DURING B INSPECTION FOUND THE AFT CABIN EMERGENCY FLASHLIGHT CHARGER HAS BROKEN HOLDING BRACKET/BASE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT CHARGER IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — FAILED (MLG) · airframe 29,751 hrs · 27,569 cycles

ON FLIGHT 2736 THE CREW REPORTED ON TAKEOFF REQUIRED A SIGNIFICANT AMOUNT OF RIGHT RUDDER AND THEN HEARD A CLANKING NOISE AT ROTATION, ON LANDING RUDDER CONTROL FELT NORMAL. THE CREW DECLARED AN EMERGENCY AND CALLED CRASH, FIRE AND RESCUE FOR LANDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DOWNLOCK PROXIMITY SWITCH HARNESS CONNECTOR P4667 IAW WM 20-50-00 NO CLUNKING NOISE AT THIS TIME. THE OPERATIONAL CHECK WAS GOOD REF NRWC 638-DFW-00867. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TIRE — DAMAGED (NLG) · airframe 29,433 hrs · 27,330 cycles

ON FLIGHT 2716 THE CREW REPORTED THAT AT ROTATION HEARD A LOUD GRINDING NOISE SOUND FROM NOSE WHEEL AND FELT AND SOUNDED LIKE THE TIRE WAS COMING APART. THE FLIGHT ATTENDANT ALSO CONFIRMED THE NOISE AS WELL. THE CREW ELECTED TO RETURN FOR LANDING. AFTER GETTING DOWN TO LANDING WEIGHT, AFTER TOUCH DOWN WHILE SLOWING THE NOSE WHEEL STARTING TO SHIMMY. THE CREW STOPPED THE AIRCRAFT AND WAS TOWED TO GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AND LEFT NOSE TIRE IAW WORK CARD 32-700-17. MAINTENANCE PERFORMED HIGH SPEED TAXI WITH CREW. NO DEFECTS NOTED. NO FURTHER MAINTENANCE ACTION REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,844 hrs · 26,901 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT EXTERIOR FORWARD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 POWER SUPPLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 28,744 hrs · 26,821 cycles

ON FLIGHT 3475 THR CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO LOCK AND UNLOCK. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED EXTERNAL MECHANISM OF MAIN CABIN DOOR IAW EMB 145 AMM 52-18-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERIVCE.

Part: WARNING SYSTEM — FALSE ACTIVATION (BRAKE SYSTEM) · airframe 28,130 hrs · 26,364 cycles

ON FLIGHT 3988 DURING THE CLIMBOUT THE CREW REPORTED, RECEIVED A BRAKE OVERHEAT MESSAGE. THE CREW DECLARED AN EMERGENCY AND CONTINUED TO DESTINATION. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED MAIN BRAKE TEMPERATURE INDICATION TESTING AND THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM P/T 32-47-01, STEP 3(I)3. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — OBSTRUCTED (CABIN DOOR) · airframe 28,053 hrs · 26,292 cycles

ON FLIGHT 4330 THE CREW REPORTED THE MAIN CABIN DOOR IS EXTREMELY HARD TO CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DEBRIS FROM MAIN PASSENGER DOOR SEAL AND LUBED ROLLERS IAW EMB145 AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — DIRTY (CABIN DOOR) · airframe 28,022 hrs

MAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE. CLEANED DEBRIS FROM MAIN CABIN DOOR SEAL AND LUBED WITH REFERENCE TO EMB-145 AMM 52-18-00. OPS CHECKS GOOD.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 27,686 hrs · 26,001 cycles

ON FLIGHT 3975 THE CREW REPORTED THE CABIN DOOR HARD TO CLOSE. THE RED LINES ON THE LEFT SIDE OF CABIN DOOR DO NOT MATCH UP. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL TEST OF MAIN CABIN DOOR IN A EMB AMM 52-18-00. THE OPERATIONAL TEST WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SLEEVE — DEFECTIVE (HEAT EXCHANGER) · airframe 27,351 hrs · 25,766 cycles

ON FLIGHT 2765 THE CREW REPORTED, RECEIVED A PACK 1 OVERLOAD CAUTION MESSAGE. THE CAPTAIN ELECTED TO DIVERT TO SGF. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SLEEVE AND CLAMP ON THE DUAL HEAT EXCHANGER TUBE IAW EMB 145 AMM 21-51-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 27,032 hrs · 25,511 cycles

ON FLIGHT 2793 UPON LANDING THE CREW REPORTED, RECEIVED A BAGGAGE SMOKE WARNING MESSSAGE. THE BAGGAGE EXTINGUISHER BUTTON WAS PRESSED. THE CAPTAIN DECLARED AN EMERGENCY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD AND AFT CARGO SMOKE DETECTORS IAW EMB-145 AMM 26-15-01, PART NUMBER 47359713, SERIAL NUMBERS 2836 AND 1221. REMOVED AND REPLACED METERING BOTTLE IAW EMB 145 AMM 26-23-01, PART NUMBER 346000731 AND SERIAL NUMBER 16935F1. REMOVED AND REPLACED HIGH RATE FIRE BOTTLE IAW EMB 145 AMM 26-23-01, PART NUMBER 337000271, SERIAL NUMBER 30764D1. THE OPERATIONAL CHECKS WERE GOOD IAW EMB-145 AMM 26-15-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,237 hrs · 24,099 cycles

ON FLIGHT 3332 THE CREW REPORTED A BURNING OIL ODOR IN THE COCKPIT DURING THE TAKEOFF ROLL & CLIMBOUT. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS REMOVED FROM SERVICE. PERFORMED BLACKLIGHT AND BRIGHT LIGHT INSPECTION. CW ETN EM-72-034 R4 ENGINE ODOR EVENT TROUBLESHOOTING ALL VISUAL EXAMINATION NEGATIVE NO ODOR NOTICEABLE IN AIRCRAFT. NO PARTS REMOVED OR REPLACED. A FUNCTIONAL FLIGHT CHECK WAS FLOWN AND FOUND SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — INOPERATIVE (NR 2) · airframe 25,018 hrs · 23,934 cycles

ON FLIGHT 3310 THE CAPTAIN REPORTED THAT AFTER TAKEOFF FROM DFW, RECEIVED A RUDDER SYSTEM 1 AND 2 FAIL AND AUTOPILOT FAIL MESSAGE. THE CAPTAIN ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PRESSURE SWITCH NR 2 IAW EMB-145 AMM 27-23-04. THE OPERATIONAL CHECK AND LEAK CHECK WAS GOOD. NO MESSAGE NOTICED. THE AUTOPILOT OPERATIONAL CHECKS WERE GOOD IAW AMM 22-11-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIVET — MISINSTALLED (FUSELAGE) · airframe 25,011 hrs · 23,927 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE PREVIOUS REPAIR BETWEEN FRAMES 27-28 AT STRINGER 21 RIGHT HAD IMPROPERLY INSTALLED RIVETS THAT ARE AGAINST STRINGER 21 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1574 FOR THE INSTALLATION OF THE DOUBLER AND FILLER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 25,011 hrs · 23,927 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT NR 3 EMERGENCY LIGHT STRIP HAS A BROKEN A WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,011 hrs · 23,927 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE GALLEY RAMP ON THE LEFT BEAM CORRODED FORWARD OF FRAME 20. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CORRODED GALLEY RAMP ON THE LEFT BEAM FORWARD OF FRAME 20 AND INSTALLED SERVICEABLE RAMP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — POWER LOSS (NR 2) · airframe 22,766 hrs · 22,048 cycles

ON FLIGHT 3996 CREW REPORTED IN CRUISE ENGINE 2 ROLL BACK OCCURRED. AIRCRAFT RETURNED TO CHA. AIRCRAFT LANDED SAFELY. AIRCRAFT REMOVED FROM SERVICE. ISSUED MEL 78-1, PER FLIGHT DATA RECORDER, DATA READOUT TESTED ENGINE 2 THRUST REVERSER FADEC INTERFACE WIRING BETWEEN FADEC 2A AND 2B AND TR 2 STOW RELAYS AND ENGINE 2 RELAY RESISTOR MODULE FOR CONTINUITY INTERRUPTS WIRING MANUAL 78-31-55 AND 76-12-53 IAW SWPM 20-20-03. NO DEFECTS NOTED. ENGINE RUNS SATISFACTORY. MEL STILL OPEN. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (FIRE BOTTLE) · airframe 22,758 hrs · 22,041 cycles

ON FLIGHT 4136 - CREW REPORTS SHORTLY AFTER TAKEOFF RECEIVED A SMOKE IN LAV INDICATION ON EICAS. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CONNECTOR ON ENGINE 1 FIRE BOTTLE. AIRCRAFT RETURNED TO SERVICE.

Part: SOLENOID VALVE — MALFUNCTIONED (NLG)

ON FLIGHT 3942 CREW REPORTED AT 22,000 FT .77 MACH GEAR UNSAFE MSG ON EICAS. GEAR DOOR OPEN. CREW DECLARED EMERGENCY INTO ORD AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. C/A REPLACED NLG DOOR SOLENOID VALVE. IAW EMB 145 AMM 32-33-02. OPS CHECK GOOD. ACFT RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2)

ON FLIGHT 3457 - CREW REPORTED TWO TIMES DURING FLIGHT E2 N1 DROPPED TO IDLE (N1-60 PRECENT AND N1-72-73 PERCENT) WITH NO INDICATION ON EICAS. (S)

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 19,793 hrs · 19,515 cycles

ON FLIGHT 4306, CREW REPORTED WHILE CLIMBING THRU 19000 THEY RECEIVED CABIN ALT WARNING AND AURAL WARN. CREW REQUESTED EMERGENCY DESCENT TO 10000 AND RETURNED TO CVG. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DIGITAL PRESSURIZATION CONTROLLER IAW AMM 21-31-01. OPERATIONAL CHECKED GOOD. NO FURTHER FAULTS FOUND AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 19,775 hrs · 19,495 cycles

ON FLIGHT 4331, CREW REPORTED SMOKE IN CABIN BEFORE BOARDING WITH APU RUNNING. AIRCRAFT REMOVED FROM SERVICE. FOUND MAIN DISTRIBUTION DUCT OVERHEATED. REMOVED AND REPLACED MAIN DISTRIBUTION DUCT, DUAL TEMP CONTROL VALVE, PACK OVER TEMP SWITCH IAW AMM 21-51-08. OPERATIONAL CHECK GOOD AND NR 8194, AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 8,405 hrs · 7,868 cycles

DURING AN MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED DOOR SILL TO REMOVE CORROSION. FABRICATED AN INTERNAL DOUBLER. REPAIR DONE IAW AEA. (SW21200501984) (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED PREVIOUS REPAIR FROME THE LT OMEGA BEAM. FABRICATED A DOUBLER, FILLER, 2 SHIMS AND PLATE. REPAIR DOEN IAW SRM. (SW21200501984) (K)

Part: FLOORBEAM — CORRODED (GALLEY)

DURING AN MBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. BLENDED DIGITAL TO REMOVED CORROSION. FABRICATED A DOUBLER FOR REPAIR. REPAIR DONE IAW SRM. (SW21200501984) (K)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

ORD - FLT 4065 - FOUND EMERGENCY EXIT LIGHTS ON BOTH WALLS NEAR OVERWING EMERGENCY EXITS ARE INOPERATIVE. REPLACED EMERGENCY BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (GALLEY)

ABI - DURING AN IMBV INSPECTION, A PREVIOUS REPAIR ON THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED EXISTING SHIM AND DOUBLERS. REMOVED SECTION OF THE FORWARD DIGITAL. FABRICATED TWO DOUBLERS AND SHIMS. PREPARED NEW SECTION STRAP. REPAIR DONE IAW EMB 145 SRM (EMB SRM 145/1142 REV 20) CHAPTERS 53-21-10 FIG 203. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION, THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 23. BLENDED THE DAMAGE AREA TO COMPLETELY REMOVE THE CORROSION. APPLIED ALODINE AND EPOXY PRIMER TO THE REPAIR AREA. FABRICATED A U-SHAPED DOUBLER. REPAIR DONE IAW EMB145 SRM (145/1142 REV 20) 53-21-0 FIG 207 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 23. BLENDED THE DAMAGE AREA TO COMPLETELY REMOVE THE CORROSION. APPLIED ALODINE AND EPOXY PRIMER TO THE REPAIR AREA. FABRICATED A U-SHAPED DOUBLER. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) 53-21-10 FIG 207 AND STANDARD SRM PRACTICES. (M)

Part: GUSSET — CORRODED (LAVATORY)

DURING AN IMBV INSPECTION A LEVEL 2 FINDING FOUND LAVATORY CENTER BEAM GUSSET CORRODED. REMOVED AND REPLACED LAVATORY CENTER GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

ABI - DURING IMBV INSPECTION A LEVEL 2 FINDING FOUND, LEFT LOWER FORWARD NR 1 SEAT TRACK CORRODED AROUND HARDWARE. REMOVED AND INSTALLED LEFT LOWER NR 1 SEAT TRACK IAW EMB 145 SRM 53-01-06. (M)

Part: SILL — CORRODED (CARGO DOORWAY)

ABI - DURING AN IMBV INSPECTION, THE CARGO OPENING LOWER CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CARGO LOWER SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM (SRM 145/1142 REV 20) CHAPTERS 51-20-01, 51-20-03, 51-40-02, 51-40-04, 51-20-06, AND THE EMB 145 CORROSION PREVENTION MANUAL CHAPTER 51-21-04 ANF 51-21-05. (M)

Part: SILL — CORRODED (GALLEY)

ABI - DURING AN IMBV INSPECTION A LEVEL 2 FINDING WAS FOUND. CORROSION ON LEFT SILL BETWEEN FRAME 19 AND 23. INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-02, 51-40-06. (M)

Part: SILL — CORRODED (GALLEY)

ABI - DURING AN IMBV INSPECTION A LEVEL 2 FINDING WAS FOUND. CORROSION ON SERVICE DOOR AFT SILL. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 51-40-02, 51-20-03, 51-40-04, 51-40-06. (M)

Part: DOUBLER — CORRODED (GALLEY)

DURING IMBV INSPECTION, A LEVEL 2 FINDING WAS FOUND. CORROSION ON DIAMOND DOUBLER ON RIGHT HAT BEAM AT FRAME 22. INSTALLED SERVICEABLE DIAMOND DOUBLER IAW EMB 145 SRM 51-20-01, 51-20-03 AND 51-40-02, 51-40-04, 51-40-06. (M)

Part: DOUBLER — CORRODED (GALLEY)

ABI - DURING IMBV INSPECTION A LEVEL 2 FINDING FOUND. DIAMOND DOUBLER ON RIGHT HAT BEAM AT FRAME 20 CORRODED. INSTALLED NEW DIAMOND DOUBLER IAW EMB 145 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-04, 51-40-06. (M)

Part: SKIN — CORRODED (FWD DIGITAL)

ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE FORWARD DIGITAL CORRODED. CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW EMB GST-1595/01. (M)

Part: SKIN — CORRODED

ABI - MAINTENANCE FOUND CORROSION IN FLOOR CENTER BEAM AT FRAME 20 AND 22. CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW EMB GST-159/01. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED

ABI - OMEGA BEAM AT FRAME 20 WAS FOUND TO BE OUT OF LIMITS AFTER REMOVAL OF CORROSION. DAMAGE WAS REPAIRED IAW EMB SRM 53-21-01. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: SENSOR — FAILED (LT MLG)

SAV - FLT 3478 - LEFT INBOARD BRAKE INDICATOR IS ON MEL AND THE CREW GOT A LEFT INBOARD BRAKE TEMP WARNING ON TAKEOFF. CREW ABORTED AND RETURNED TO GATE. REMOVED AND REPLACED NR 4 BRAKE TEMP SENSOR IAW AMM. OPS CHECK GOOD. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

TXK - FLT 3417 - CAPTAIN WINDSHIELD SHATTERED IN FLIGHT. AIRCRAFT DIVERTED TO TXK AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ORD - FLT 9754 - FORWARD EMERGENCY LIGHTS ARE STAYING ON WHILE LIGHTS ARE IN ARMED ONLY. REMOVED AND REPLACED POWER SUPPLY. OPS CHECK GOOD. (M)

Part: POWER SUPPLY — INOPERABLE (CABIN)

ORD - FLT 4296 - CABIN EMERGENCY LIGHTS ON WITH NO POWER ON AIRCRAFT. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)