N613AE

Part: LIGHT — UNSERVICEABLE (RH OVERWING) · airframe 50,108 hrs · 46,162 cycles

DURING PS-1 CHECK FOUND EXTERNAL EMERGENCY LIGHT RH OVERWING INOP-C/A-RAR EXTERNAL EMERGENCY LIGHT ASSEMBLY RH OVERWING IAW EMB 145 AMM 33-50-10, OPS CHECK GOOD IAW EMB 145 AMM 33-50-00 NO FURTHER DEFECTS NOTED AT THIS TIME

Part: LAMP — INOPERATIVE (RH) · airframe 50,038 hrs · 46,083 cycles

R/H OVERWING EMERGENCY LIGHT INOP-C/A-REPLACED EMERGENCY LIGHTY LAMP IAW AMM 33-50-10.OPS CHECK GOOD

Part: LAMP — INOPERATIVE (RH) · airframe 50,012 hrs · 46,056 cycles

DURING PS-1 CHECK, FOUND RH OVER WING EMERGENCY LIGHT INOP-C/A-RAR OVER WING EXTERIOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-07. OPC GOOD

Part: LAMP — INOPERATIVE (RH) · airframe 49,895 hrs · 45,915 cycles

RH OVER WING EMERGENCY LIGHT INOP-C/A-RAR RH OVER WING EMERGENCY LIGHT LAMP WITH REFERENCE TO EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: LIGHT — INOPERATIVE (ROW 8 AND 9) · airframe 49,742 hrs · 45,737 cycles

FLOOR EMERGENCY LIGHT STRIP INOP AT ROW 8 AND 9.-C/A-REPAIRED QUICK DISCONECT ON FLOOR EMERGENCY LIGHTING STRIP IAW SWPM 20-50-00 AND OPC GOOD IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (RH OVERWING) · airframe 49,742 hrs · 45,737 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCYT LIGHT LAMP IAW AMM 33-50-10 OPC GOOD

Part: LAMP — INOPERATIVE (RH) · airframe 49,452 hrs · 45,419 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LAMP IAW AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECK GOOD. END.

Part: NONE — NONE · airframe 49,412 hrs · 45,376 cycles

RUBBER BURNING SMELL INSIDE CABIN WENT AWAY AFTER LANDING COMPLETION OF FIM TASK 21-20-00-810-801-A REF AML 4815459 ITEM 3 REQUIRED-C/A-CA PENDING

Part: LAMP — INOPERATIVE (RH) · airframe 49,385 hrs · 45,340 cycles

FOUND RH OVERWING REAR EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING REAR EMERGENCY LIGHT BULB IAW EMB145 AMM 33-50-10. OPC GOOD.

Part: LAMP — INOPERATIVE (RH) · airframe 49,318 hrs · 45,259 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LAMP IAW AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECK GOOD. END.

Part: NONE — BROKEN (FA) · airframe 49,318 hrs · 45,259 cycles

FWD FA FLASHLIGHT CRADLE BROKEN-C/A-RAR FWD FA FLISHLIGHT CRADLE IAW CMM 25-60-14. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: LAMP — INOPERATIVE (RH) · airframe 49,297 hrs · 45,235 cycles

RIGHT HAND OVER WING EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR BULB IAW AMM 33-50-10, OPS CHECK GOOD

Part: NONE — UNSERVICEABLE ([0000] [RAFT]) · airframe 49,265 hrs · 45,199 cycles

ELECTRICAL SMOKE IN COCKPIT LOW VIB SOUND LIKE MAY BE A BAD FAN MOTOR.FOUND LH AVI EXHAUST FAN INOPERATIVE. TROUBLE SHOOTING ITEM #1 LGPG 4878054,-C/A-REMOVED AND REPLACED LH AVI EXHAUST FAN IAW EMB 145 AMM 21-26-02 OPS TEST GOOD

Part: LAMP — INOPERATIVE (RH) · airframe 49,179 hrs · 45,114 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LAMP IAW AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECK GOOD. END.

Part: NONE — NONE · airframe 49,009 hrs · 44,924 cycles

EMERGENCY LIGHTING FLOOR STRIPS 2 AND 3 INOP.-C/A-RAR BATTERY AND CHARGER #2 OPC BAD IAW WC 33-700-19. SEE ITEM 2 THIS NRWC

Part: NONE — NONE · airframe 48,947 hrs · 44,860 cycles

ROW 8A EMERGENCY FLOOR STRIP WONT ILLUMINATE ORIGINAL LOGPAGE 4715621 ITEM 3 MEL 3323 - AUTH# 02-53-C-C/A-RAR ROW 8A EMERGENCY FLOOR LT STRIP IAW EMB AMM 33-50-12-000-801-A AND 33-50-12-400-801-A. OPS CHECK GOOD. MEL RESTORED. END.

Part: NONE — NONE · airframe 48,928 hrs · 44,838 cycles

"TRANSFERRED FROM NRWC 613-CMI-04165 ITEM 1" ROW 8A EMERGENCY LIGHT STRIP INOP-C/A-DEFERRED PER MEL 33-23. AUTH# 020053-C

Part: NONE — NONE · airframe 48,724 hrs · 44,622 cycles

FOUND FA FLASHLIGHT ASSEMBLY TO BE UNSERVICEABLE PER PS-2 CHECK-C/A-REMOVED AND REPLACED FA FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-51-01. OPS CHECK GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 48,625 hrs · 44,502 cycles

SMOKE INDICATION IN THE CARGO BAY BAGGAGE COMPT SMOKE DETECTION SYSTEM REQS MEL 26-3 DUE TO LACK OF EVIDENCE OF FIRE MEL 2603 - AUTH# 11-255D-C-C/A-REF LG PG 4832556 ITEM 3 RAR CARGO SMOKE DETECTOR IAW AMM 26-15-00. OPS CHECK GOOD. MEL ITEM CLOSED.

Part: NONE — NONE · airframe 48,519 hrs · 44,381 cycles

LH WINDSHIELD OUTER LAYER CRACKED AT 15K DECLARED EMERGENCY "TRANSFERRED TO NRWC 613-ORD-03900"-C/A-REF NRWC 613-ORD-03900 FOR CORRECTIVE ACTION AND APPLICABLE RII. RAR CAPT WINDSHIELD. ALL OPS/LEAK TESTS GOOD. NO DEFECTS NOTED.

Part: NONE — NONE · airframe 48,458 hrs · 44,311 cycles

RH OVERWING AFT EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING AFT EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPERATIONAL CHECK GOOD.

Part: NONE — NONE · airframe 48,365 hrs · 44,217 cycles

LH SIDE OVER THE WING EMER.LIGHT INOP.-C/A-RAR LH SIDE OVER THE WING EMER.LIGHT BULB IAW EMB 145 AMM 33-50-10..OPERATIONAL CHECK GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,239 hrs · 44,058 cycles

SEAT 12A EMERGENCY EXIT PLACARD INOP-C/A-T/S IAW FIM TASK 33-50-00-810-804-A. RAR EMERGENCY LIGHT DC/AC INVERTER 5 IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A OPS CHECK GOOD

Part: MUFFLER — DISCONNECTED (RECIRC FAN) · airframe 48,177 hrs · 43,985 cycles

PAX COMPLAINING OF A SMOKE SMELL IN THE AFT HALF OF THE CABIN."TRANSFERRED TO NRWC 613-DFW-03690-C/A-FOUND MUFFLER CONNECTING RECIRC. FAN 2 AND PACK 2 TO BE DISCONNECTED. REINSTALLED MUFFLER TO RECIRCULATION FAN 2 AND FUSELAGE FITTING IAW EMB 145 AMM 21-24-02. OPC, LEAK AND SMELL CHECK GOOD IAW EMB 145 AMM 21-00-00. NO FURTHER SMELLS DETECTED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 48,177 hrs · 43,985 cycles

EMERGENCY LIGHT FLOOR STRIP AT FLOOR PANEL 261BF WIRE BROKEN-C/A-RAR EMEREGNCY LIGHT FLOOR STRIP IAW AMM 33-50-12 OPERATIONAL CHECK GOOD

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,131 hrs · 43,929 cycles

RH OVERWING LATERAL PANEL EMERGENCY LIGHT INOP.-C/A-RAR RH OVERWING LATERAL PANEL EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPC GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,108 hrs · 43,904 cycles

DURING PS1 CHECK FOUND LH UPPER FAIRING EMERGENCY LIGHT OUT-C/A-RAR LH UPPER FAIRING LAMP IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE · airframe 48,019 hrs · 43,811 cycles

ROW 12 EMERGENCY LIGHTS INOP-C/A-T/S IAW FIM TASK 33-50-00-810-804-A. RAR BATTERY CHARGER ASSY AND BATTERY PACK IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A AND 33-50-04-000-802-A AND 33-50-04-400-802-A OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,931 hrs · 43,705 cycles

ROWS 8-12 EMERGENCY LIGHTS INOP-C/A-T/S IAW EMB FIM 33-50-00-810-804-A. FOUND #3 BATTERY BAD. RAR #3 BATTERY AND CHARGER IAW ENVOY W/C 33-700-19. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,902 hrs · 43,670 cycles

DURING PS-1 CHECK FOUND RH SIDE CENTER FAIRING EMERGENCY LIGHT INOP-C/A-RAR RH SIDE CENTER FAIRING EMERGENCY LAMP IAW EMB AMM 33-50-10. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 47,895 hrs · 43,661 cycles

DURING DESCENT WE SMELT ELECTRICAL SMOKE SMELL IN COCKPIT. FLIGHT ATTENDANT CONFIRMED SMELL IN CABIN-C/A-T/S PER WORKSCOPE AND FIM 21-20-00-810-801-A AND FOUND NO DEFECTS AT THIS TIME

Part: TRANSDUCER — FAULTED (OIL PRESS IND) · airframe 47,875 hrs · 43,638 cycles

ENG 1 LOSS OF OIL PRESS IND DURING TAKEOFF ROLL (LOW SPEED REJECT ABOUT 40 KTS). THERE WAS NO EICAS "E1 OIL LOW PRESS" MESSAGE. OIL PSI WENT TO MOSTLY 6 PSI.-C/A-RAR OIL TEMPERATURE/PRESSURE SENSOR TRANSDUCER IAW AMM 79-31-01. PERFORMED OPERATIONAL CHECK. DID NOT FIX PROBLEM. REFERENCE AML PAGE 4761644 ITEM 2 FOR DISCREPANCY.

Part: RADIO ALTIMETER — FAULTED · airframe 47,795 hrs · 43,556 cycles

CLIMBING THROUGH 15,000FT RA MOMENTARILY STUCK AT 20FT AND GOT TO LOW TERRAIN AURAL WARNING.-C/A-DEFERRED PER MEL 34-8 AUTH # 060025 DM-A EXP 6-5-21 ?M? PROCEDURES C/W

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,749 hrs · 43,507 cycles

EMERGENCY LIGHT STRIPS 4 AND 5 AND LH AND RH LOWER DOOR SHROUD EXIT PLACARDS NOT ILLUMINATING-C/A-RAR #3 BATTERY AND POWER SUPPLY IAW AMM 33-50-04 OPS CHECK FAIL PERFORMED ELECTRICAL POWER RESET OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,558 hrs · 43,316 cycles

LEFT HAND OVER WING EMERGANCY LIGHT INOP-C/A-REMOVED AND REPLACED LEFT HAND OVER WING EMERGANCY LIGHT BULB IAW AMM 33-50-10. OPERATIONAL CHECK GOOD.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 47,256 hrs · 42,995 cycles

RH EXTERNAL OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH EXTERNAL OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: STRUCTURE — CRACKED (COCKPIT CEILING) · airframe 47,250 hrs · 42,986 cycles

THE COCKPIT RT DIAGONAL CEILING MEMBER IS CRACKED JUST FORWARD OF THE SPEAKER, AS MARKED. C/A: R & R COCKPIT RT DIAGONAL CEILING MEMBER, IAW EMB 145 SRM 51-40-02. REPLACEMENT PN: 123-07751-006.

Part: YOKE — CRACKED (RT PYLON) · airframe 47,250 hrs · 42,986 cycles

DURING IMBV INSPECTION, QC FOUND RT PYLON FWD LOWER YOKE FITTING CRACKED. C/A: REMOVED AND REPLACED RT FWD LOWER YOKE FITTING, IAW ERS-EM-54MR-698.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,250 hrs · 42,986 cycles

LT OMEGA BEAM AT FRAME 20 PREVIOUS REPAIR IS CORRODED. C/A: REACCOMPLISHED REPAIR ON LT OMEGA BEAM AT FRAME 20, IAW EMB 145 SRM 53-00-10RE.

Part: SHEAR TIE — CORRODED (CARGO BAY) · airframe 47,250 hrs · 42,986 cycles

CARGO DOOR CUTOUT STRUCTURE FR 65 SHEAR CLIP CORRODED. LEVEL 1 CORROSION. C/A: PERFORMED A PERMANENT REPAIR ON THE CARGO DOOR CUTOUT STRUCTURE FR 65 LOWER END OF THE SHEAR CLIP, IAW EMB 145 SRM 53-31-04 ITEM 4 FIGURE 212.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 47,250 hrs · 42,986 cycles

CARGO DOOR CUTOUT STRUCTURE LOWER FLOOR SILL CORRODED. LEVEL 1 CORROSION. C/A: REMOVED AND REPLACED THE CARGO DOOR CUTOUT STRUCTURE LOWER FLOOR SILL, IAW EMB 145 SRM 51-40-02.

Part: SUPPORT — CORRODED (TOILET VALVE) · airframe 47,250 hrs · 42,986 cycles

TOILET WASTE VALVE SUPPORT EXTERIOR HAS CORROSION. C/A: REMOVED AND REPLACED THE TOILET WASTE VALVE SUPPORT, IAW EMB 145 SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,250 hrs · 42,986 cycles

FUSELAGE SKIN CRACKS AROUND 2 RIVETS AT FRAME 75 BETWEEN STGR 01R-02R. C/A: ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN CRACKS AT FRAME 75 BETWEEN STRINGERS 01R-02R, IAW EMB 145 SRM 53-31-01RE FIGURE 219 SHEET 2.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 47,250 hrs · 42,986 cycles

BAGGAGE DOOR EXTERNAL SKIN ACTUATING HANDLE CUTOUT EDGE HAS 2 CRACKS, 0.3 IN LENGTH. C/A: ACCOMPLISHED A PERMANENT REPAIR ON CRACKS ON THE BAGGAGE DOOR EXTERNAL SKIN ACTUATING HANDLE CUTOUT WITH CUTOUT DOUBLER AND FILLER, IAW ERS-EM-52MR-1103.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 47,250 hrs · 42,986 cycles

CARGO DOOR INTERNAL LOWER SKIN CHAFED AT VB5 BETWEEN HB4 AND HB3. C/A: REMOVED PREVIOUS REPAIR DOUBLER AND FABRICATED AND INSTALLED A NEW DOUBLER, IAW EMB 145 SRM 51-40-02, 52-30-01 AND ETN-EM-52-043.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 47,250 hrs · 42,986 cycles

CARGO DOOR INTERNAL LOWER SKIN CHAFED BETWEEN HB3 AND HB2. C/A: REMOVED PREVIOUS REPAIR DOUBLER AND FABRICATED AND INSTALLED A NEW DOUBLER ON CARGO DOOR LOWER INNER SKIN BETWEEN HB3 AND HB2, IAW EMB 145 SRM 51-40-02, 52-30-01 AND ETN-EM-52-043.

Part: PROFILE — CORRODED (R EMERGENCY EXIT) · airframe 47,250 hrs · 42,986 cycles

RT EMERGENCY EXIT LOWER PROFILE L UNDER AFT TEFLON GUIDE CORRODED. LEVEL 2 CORROSION. C/A: REMOVED AND REPLACED RT EMERGENCY EXIT LOWER L PROFILE, IAW EMB 145 SRM 51-20-03 AND 51-40-02.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 47,250 hrs · 42,986 cycles

CARGO DOOR INTERNAL LOWER SKIN CHAFFED AT HB4 APPROXIMATELY 2' FROM FWD EDGE. C/A: REMOVED PREVIOUS REPAIR DOUBLER AND FABRICATED AND INSTALLED A NEW DOUBLER ON CARGO DOOR LOWER INNER SKIN AT HB4 APPROXIMATELY 2 FROM FWD EDGE, IAW EMB 145 SRM 52-30-01 AND ETN-EM-52-043.

Part: SPAR — CRACKED (LT WING) · airframe 47,250 hrs · 42,986 cycles

LT WING SPAR I CRACKED AT RIB 9. CRACK LENGHT 0.3 NUMBER OF CRACKS 1. C/A: ACCOMPLISHED PERMANENT REPAIR ON LT WING SPAR I AT RIB 9, IAW EMB 145 SRM 57-20-05 ITEM 3.

Part: STRIP — BROKEN (CABIN EMER LIGHT) · airframe 47,250 hrs · 42,986 cycles

EMERGENCY LIGHT STRIPS MISSING FILLER STRIPS. INSTALLED EMERGENCY LIGHT STRIP FILLER STRIPS AS REQUIRED IAW EMB 145 AMM 33-50-12.

Part: STRIP — INOPERATIVE (LT FLR EMER PROX) · airframe 47,250 hrs · 42,986 cycles

LEFT FLOOR EMERGENCY PROX LIGHT STRIPS NR 4 AND NR 5 ARE INOPERATIVE. COMPLETE: REMOVED AND INSTALLED EMERGENCY LIGHT INVERTER NR 5 IAW EMB 145 AMM 33-50-11 OPC GOOD.

Part: LIGHT — BROKEN (GALLEY SER DOOOR) · airframe 47,250 hrs · 42,986 cycles

FWD GALLEY TO SERVICE DOOR LOWER EMERGENCY LIGHT BROKEN AT CONNECTOR REQUIRES REPLACEMENT. R & R FWD GALLEY TO SERVICE DOOR LOWER EMERGENCY LIGHT IAW EMB 145 AMM 33-50-13 OPS CHECK GOOD.

Part: BATTERY PACK — DEPLETED (CABIN EMER LIGHT) · airframe 47,250 hrs · 42,986 cycles

INSTALL THE EMERGENCY LIGHTING BATTERY POWER SUPPLY. NOTE AND RECORD P/N AND S/N ON. SEE NRTC E836645 FOR INSTALL THE EMERGENCY LIGHTING BATTERY POWER SUPPLY. NOTE AND RECORD P/N AND S/N ON.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,000 hrs · 42,809 cycles

L/H FWD EXTERIOR EMER LIGHT, OVERHEAD COCKPIT EMER LIGHT AND ROW 3 OVERHEAD EMER LIGHT ARE INOP-C/A-REMOVED AND REPLACED FUSE ON #1 BATTERY POWER SUPPLY IAW CMM 25-60-03 AND WM 33-50-00. OPS CHECK GOOD

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,871 hrs · 42,711 cycles

EMERGENCY EXIT ROW OVERHEAD FWD EXIT SIGN INOP.-C/A-REMOVED AND REPLACED EMERGENCY EXIT ROW OVERHEAD FWD LIGHT IAW EMB 145 AMM 33-50-15 AND REMOVED AND REPLACED EMERGENCY LIGHT INVERTER 6 IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD.

Part: DISPLAY — SMOKE (COCKPIT) · airframe 46,331 hrs · 42,151 cycles

SMOKE IN COCKPIT-C/A-INSPECTED FOUND CTR DU TO BE THE SOURCE OF SMOKE. C/W POST MOD ADS-B FMS DATA BASE UPLOAD IAW ENVOY W/C 34-800-01. NO DEFECTS NOTED

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 45,834 hrs · 41,732 cycles

CLIMBING THROUGHT FL330 DELTA P RISES TO 8.0 CAUTION RANGE. WE WERE IN AUTO MODE. REMOVED AND REPLACED ELECTROPNEUMATIC OUTFLOW VALVE IAW AMM 21-31-03. OPS CHECK GOOD. M. PROCEEDURE REVERSED. MEL RESTORED.

Part: MODULE — FAILED (CABIN PRESSURE) · airframe 45,834 hrs · 41,732 cycles

CABIN ALTITUDE WENT TO DASHES DURING INITIAL CLIMBOUTAT AROUNG 10,000 FT. DURING MANUAL PRES PROCEDURES. REMOVED AND REPLACED CPAM IAW EMB AMM 21-32-01.

Part: FUSE — BLOWN (CABIN) · airframe 45,590 hrs · 41,449 cycles

EMERGENCY EXIT PATHWAY LIGHTING AT 9-10 NOT WORKING. C/A-FOUND 3 FUSES BLOWN ON #3 EMERGENCY LIGHTING BATTERY CHARGER. REMOVED AND REPLACED THE 3 BLOWN FUSES, REF: AMM 33-50-04. ALL EMERGENCY LIGHTS NOW OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 45,137 hrs · 41,064 cycles

ABORTED TAKEOFF AT 40KTS MASTER CAUTION FOR ICE COND A/I INOP ICE DETECTION OVERRIDE KNOB WAS IN ENG. C/A-INTEROGATED CMC, NO ASSOCIATED MSGS FOUND. C/W A/I SYSTEM OPC IAW AMM 30-00-00. FOUND SATISFACTORY AT THIS TIME.

Part: COUPLING — LEAKING (AC BAY) · airframe 45,134 hrs · 41,061 cycles

PACK 1 OVLD T FL180 ON CLIMB. PACK 2 MEL ALREADY. CABIN DEPRESSURIZED, EMERGENCY DESCENT. MAX OBSERVED CABIN ALT 7000'. C/A-PERFORMED GVI OF PACK 1. FOUND COUPLING LEAKING AT ACM. REPOSITIONED CLAMP ON COUPLING IAW AMM 21-51-03. OPS CHECK GOOD IAW AMM 21-51-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,957 hrs · 40,867 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-LH FWD OVERWING EMERGENCY LIGHT RELAMPED IAW EMB 145 AMM 33-50-10, OPS CHK. GOOD

Part: CONDENSER — FAILED (AC BAY) · airframe 44,946 hrs · 40,856 cycles

SUPPLEMENTAL SMOKE IN CABIN CLIMBING THROUGH ~ 19000 FT "TRANSFERRED TO NRWC 613-MIA-02438". PACK 2 OVLD ON LANDING. C/A-REMOVED AND REPLACED NR 2 ACM IAW AMM 21-51-03 REF AML #436403812 & NRWC 613-MIA-02436 FOR WORK PERFORMED. ALSO REMOVED AND REPLACED NR 2 CONDENSER / MIXER IAW AMM 21-51-04. NO DEFECTS NOTED AT THIS TIME. ITEM DEFERRED PER MEL 21-28 AUTH #030919D-C. REMOVED AND REPLACED NR 2 PACK OVERTEMP SENSOR IAW AMM 21-58-01. REMOVED AND REPLACED NR 2 PACK PACK VLV IAW AMM 21-51-01. OPS CK GOOD IAW 21-51-00 WITH TAKE-OFF PWR ON ENGINES AND ALSO WITH APU. ALSO COMPLETED ETN-EM-72-034. NO DEFECTS NOTED. MEL 21-28 IS RESTORED. PACK OVERTEMP SWITCH P/N 815291-5 S/N 6105. PACK PRESSURE REGULATOR P/N 816604-1 S/N 200312059.

Part: SWITCH — FAILED (AC BAY) · airframe 44,925 hrs · 40,840 cycles

PACK 1 OVERLOAD WITH PACK 2 PREVEUSLY MEL. C/A-DEFERRED PER MEL 21-29 AUTH 030669DM-C. "M" PROCEDURES C/W. LT PACK OPS CK GOOD IAW AMM 21-51-00. MEL RESTORED. REMOVED AND REPLACED RT PACK OVER TEMP SWITCH IAW AMM 21-51-08 OPS AND LEAK CHECK SATISFACTORY. MEL RESTORED. MAINT ACTIONS C/W. REMOVED AND REPLACED RT PACK OVER PRESSURE SWITCH IAW AMM 21-51-06. OPS AND LEAK CHECK SATISFACTORY. MEL RESTORED. PACK OVERTEMP SWITCH P/N 815291-5 S/N 6096.

Part: ACM — FAILED (RIGHT) · airframe 44,724 hrs · 40,673 cycles

SMOKE SMELL BRIEFLY IN CABIN AND COCKPIT. BISIBLE SMOKE IN CABIN BRIEFLY.-C/A-TS PER FIM 21-00-00-810-801-A FOUND ACM #2 SEIZED. DEFERED #2 ACM SEIZED IAW E145 MEL 21-28. NO M PROCEDUREL. REMOVED AND REPLACED #2 PACK AIR CYCLE MACHINE IAW 21-51-03. OPS CHECK GOOD IAW 21-51-00. MEL 21-28 IS RESTORED

Part: PRESSURE SWITCH — FAILED (NR 2) · airframe 44,666 hrs · 40,598 cycles

HIGH SPEED REJECT AT 122 KNOTS FOL EICAS PACK 2 OVLD MESSAGE POP UP AND STILL REMAINS ON EICAS WHILE PARKED BACK AT GATE-C/A-PACK 2 OVERLOAD ITEM DEFFERED. PERFORMED HIGH ENERGY STOP INSP PER AMM 05-50-16 NO DEFFECT NOTED. RAR OVERPRESSURE SWITCH IAW AMM 21-51-06. OPS CK GOOD THIS CLEARS MEL #21-28

Part: RETAINER — DAMAGED (FUSELAGE) · airframe 44,494 hrs · 40,452 cycles

312AR DOOR FRAME SURROUND HAS RECEPTACLE PULLED THROUGH. C/A-REPAIRED DAMAGE IAW ERS-EM-T3MR-3590.

Part: HANDLE — FAILED (PAX DOOR) · airframe 43,999 hrs · 40,012 cycles

MAIN CABIN DOOR WILL NOT OPEN. R & R THE MAIN CABIN DOOR INTERNAL ACTUATING HANDLE, OPS CHECKED GOOD, NO DEFECTS.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 43,309 hrs · 39,394 cycles

SERVICE DOOR IS DIFFICULT TO OPEN. CLEANED AND LUBRICATED THE DOOR HANDLE. OPS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 43,172 hrs · 39,267 cycles

FWD CABIN EMERGENCY FLASH LIGHT HOLDER IS BROKEN. REMOVED AND REPLACED FWD CABIN EMERGENCY FLASH LIGHT ASSEMBLY.

Part: BULB — INOPERATIVE (EXTERIOR) · airframe 42,499 hrs · 38,690 cycles

RT AFT WING/FUSELAGE FAIRING EXTERIOR LIGHT (#6) INOP. R & R RT AFT WING/FUSELAGE FAIRING EXTERIOR LIGHT BULB (#6), OPS CHECK GOOD.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 42,423 hrs · 38,628 cycles

ACFT WILL NOT PRESSURIZE IN THE MANUAL MODE. R & R DIGITAL CONTROLLER, OPS CHECKED GOOD.

Part: PROXIMITY SWITCH — FAILED (MLG) · airframe 42,417 hrs · 38,622 cycles

LANDING GEAR AIR TO GROUND FAIL MESSAGE. R & R NLG WEIGHT ON WHEELS PROX SWITCH OPS. CHECK GOOD.

Part: PROXIMITY SWITCH — FAILED (MLG) · airframe 42,416 hrs · 38,621 cycles

LANDING GEAR AIR TO GROUND FAIL AFTER ROTATION. R & R WEIGHT ON WHEELS NR 2 PROXIMITY SWITCH, OPS CHECKED GOOD.

Part: STRINGER — CRACKED (FRAMES 52-53) · airframe 42,182 hrs · 38,220 cycles

STRINGER 20R BETWEEN FRAMES 52 - 53 FOUND CRACKED. PERFORMED CUTOUT TO REMOVE THE DAMAGED SECTION OF THE STRINGER. FABRICATED AND INSTALLED THE NEW STRINGER SECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,405 hrs · 38,613 cycles

LEFT UPPER FUSELAGE SKIN HAS 4 CRACKS.

Part: LIGHT — INOPERATIVE (SEAT 1A) · airframe 41,073 hrs · 37,464 cycles

MAIN CABIN EMERGENY LIGHTING SEAT 1A INOPERATIVE. R & R MAIN CABIN EMERGENY LIGHT. OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 38,763 hrs · 35,585 cycles

EMERGENCY LIGHT INOPERATIVE AT 12A FWD OF THE DOOR. RECONNECTED CONNECTOR ON EMERGENCY LIGHT FWD OF EMEGENCY EXIT DOOR AT 12A. OPS CHECK GOOD.

Part: LIGHT — FAILED (CABIN) · airframe 38,579 hrs · 35,442 cycles

EMERGENCY LIGHTS NR 8, & 9 WILL NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED BOTH LIGHTS, OPS CHECK GOOD.

Part: DOUBLER — CORRODED (CARGO DOOR) · airframe 38,580 hrs · 35,442 cycles

CARGO DOOR WEB PREVIOUS REPAIR DOUBLER HAS CORROSION ABOUT THE NUTPLATE. R & R INTERNAL DOUBLER ON THE CARGO DOOR IAW ETN-EM-52-043 & SRM 51-40-02.

Part: YOKE — CRACKED (LT ENGINE) · airframe 38,580 hrs · 35,442 cycles

WHILE PERFORMING ENG RUN LEAK CHECKS, FOUND THE LT ENG FWD LOWER YOKE CRACKED. REMOVED & INSTALLED NEW LT ENG FWD LOWER ENG YOKE IAW EO EM-54MR-386.

Part: RIB — CHAFED (LT WING) · airframe 38,580 hrs · 35,442 cycles

LEFT WING RIB 21 CHAFED. FABRICATE & INSTALL LT ANGLE ON RIB 21, ANGLE CAP 1 MM HIGHER THAN RIB CAP IAW ERS-EM-57MR-460.

Part: SKIN — CORRODED (FUSELAGE) · airframe 38,577 hrs · 35,439 cycles

CORROSION ON INTERNAL SKIN BETWEEN FRAMES 18 & 17, BETWEEN STRINGERS 21L - 21R. 1 INCH CIRCULAR CUT OUT, INSTALL FILLER & DOUBLER IAW ERS-EM-53MR-1373. REPAIR MATERIALS, DOUBLER AL2024-T3 .040", FILLER AL2024-T3 .040.

Part: STRUCTURE — GOUGED (CARGO DOOR) · airframe 38,577 hrs · 35,439 cycles

CARGO DOOR AFT SIDE STRUCTURE IS GOUGED AT A NUTPLATE AT THE CTR INBD EDGE. REPAIRED CARGO DOOR AFT STRUCTURE CTR INBD EDGE IAW ERS-EM-52MR-363.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 38,577 hrs · 35,439 cycles

RIGHT OMEGA BEAM INBD SUPPORT CRACKED AT FRAME 47. REMOVED & INSTALLED NEW PARTS FOR RT OMEGA BEAM INBD SUPPORT FRAME 47 IAW SRM 53-23-02 & 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 38,577 hrs · 35,439 cycles

RIGHT OMEGA BEAM OTBD SUPPORT CRACKED AT FRAME 47. REMOVED & INSTALLED NEW PARTS FOR RT OMEGA BEAM OTBD SUPPORT IAW SRM 53-23-02 & 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 38,577 hrs · 35,439 cycles

LEFT OMEGA BEAM OTBD SUPPORT CRACKED AT FRAME 47. R & R LT OMEGA BEAM OTBD SUPPORT AT FRAME 47, FWD & AFT SECTIONS, IAW SRM 53-23-02, SRM 51-40-02 & SRM 51-20-01.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 38,577 hrs · 35,439 cycles

LEFT OMEGA BEAM INBD SUPPORT CRACKED AT FRAME 47. R & R LT OMEGA BEAM INBD SUPPORT AT FRAME 47, FWD & AFT SECTIONS, IAW SRM 53-23-02, SRM 51-40-02 & SRM 51-20-01.

Part: CRADLE — DEFECTIVE (FLASHLIGHT) · airframe 38,572 hrs · 35,432 cycles

FLIGHT ATTENDANT REPORTS HOT WIRING SMELL IN FLIGHT CABIN DURING DESCENT. FOUND FLIGHT ATTENDANT FLASHLIGHT SMELLING BURNED. R & R FWD FLIGHT ATTENDANT FLASHLIGHT CRADLE ASSEMBLY IAW AMM 33-50-06.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,136 hrs · 35,076 cycles

RIGHT SIDE AFT EXTERNAL OVERWING EMER LIGHT FAILS TO ILLUMINATE. REPLACED THE BULB IN THE RT SIDE AFT EXTERNAL OVERWING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — LOOSE (EXTERIOR) · airframe 38,130 hrs · 35,069 cycles

DURING PS 2 INSPECTION FOUND RT AFT EXTERIOR OVERWING EMER LIGHT INOPERATIVE. FOUND LAMP TO BE LOOSE IN SOCKET. SECURED LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: ACM — SEIZED (AC BAY) · airframe 38,026 hrs · 34,948 cycles

SMOKE IN THE CABIN & COCKPIT AT 24000. FLIGHT ATTENDANT NOTED A HAZY SMOKE FROM THE REAR CABIN. SMOKE FROM EL RELAY BOX BEHIND FIRST OFFICERS SEAT. SMOKE DISSIPATING ON DESCEND TRANSFERRED TO NRWC 613-RSW-02186. REF NRWC 613-RSW-02186 FOR DETAILS. FOUND LT ACM SEIZED, REPLACED LT ACM IAW AMM CH 21-51-03. OPERATIONS CHECKED OK IAW AMM CH 21-51-00.

Part: DOOR SEAL — UNKNOWN (CABIN DOOR) · airframe 37,702 hrs · 34,633 cycles

LOUD NOISE COMING FROM MAIN CABIN DOOR. FOUND NO DAMAGE TO SEAL. SERVICED MAIN DOOR SEAL IAW AMM 52-18-04.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,442 hrs · 34,388 cycles

RIGHT EXTERNAL OVERWING EMER LIGHT INOPERATIVE. R & R LIGHT LAMP IN EXTERNAL OVERWING EMER LIGHT IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,778 hrs · 33,741 cycles

LEFT SIDE PAX COMPARTMENT, AFT OF OVERWING EMER EXIT, EXIT MARKER UPPER WILL NOT ILLUMINATE WHEN SWITCHED ON. R & R EMER LIGHT DC & AC INVERTER IAW AMM 33-50-11. COMPLIED WITH OPERATIONS CHECK IAW AMM 33-50-00-700-801A. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,737 hrs · 33,689 cycles

SEAT 12A UPPER EMER EXIT SIGN INOPERATIVE. TROUBLE SHOT & FOUND EMER LIGHT DC & AC INVERTER. R & R INVERTER IAW AMM 33-50-11-000-801-A & 33-50-11-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SIGN — INOPERATIVE (CABIN) · airframe 36,618 hrs · 33,595 cycles

INTERIOR LT OVERWING EXIT SIGN INOPERATIVE. R & R INTERIOR LT OVERWING EXIT SIGN IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 36,577 hrs · 33,567 cycles

RIGHT OVERWING EMER LIGHT INOPERATIVE. R & R RT OVERWING EMER LIGHT ASSEMBLY, OPERATIONS CHECKED GOOD IAW AMM 33-50-10.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 36,216 hrs · 33,258 cycles

OVERWING AFT EMERGENCY LIGHT INOPERATIVE. R & R OVERWING AFT EMERGENCY LIGHT LAMP, OPERATIONS CHECK GOOD IAW AMM 33-50-10.

Part: INVERTER — FAILED (CABIN) · airframe 35,951 hrs · 33,040 cycles

SERVICE DOOR EXIT LIGHT INOPERATIVE. REMOVED & INSTALLED NEW SERVICE DOOR EXIT LIGHT, DID NOT FIX IAW EMB-145 AMM 33-50-14. REMOVED & INSTALLED NEW NR 2 INVERTER IAW AMM 33-50-11, OPERATIONS CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 35,913 hrs · 33,010 cycles

STRONG OIL SMELL NOTED IN COCKPIT & CABIN DURING APPROACH & TAXI IN. IAW NRWC 613-DFW-01774 R & R NR 1 ENG IAW WORK CARD 71-000-00, OPERATIONS & LEAK CHECKED NORMAL.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,909 hrs · 33,004 cycles

CONTINUOUS OIL SMELL IN COCKPIT STRONG ON CLIMB OUT & DESCENT. TRANSFERRED TO NRWC 613-SGF-01764. TROUBLESHOT ODOR EVENT, NO OIL SMELL OCCURRED DURING ENG RUNS IAW ETN-EM-72-034.

Part: TRIM PANEL — BROKEN (PAX DOOR) · airframe 35,787 hrs · 32,911 cycles

PAX DOOR DIFFICULT TO OPEN. FOUND DOOR TRIM ON LOWER LT CORNER BROKEN & CATCHING ON FUSELAGE. DEFERRED DOOR TRIM IAW NEF 52 10B AUTH 030515M-N.

Part: ACM — FAILED (AC BAY) · airframe 35,715 hrs · 32,852 cycles

10 MINS OUT OF LANDING MLU FLIGHT ATTENDANT REPORTED PASSENGERS COMPLAINING OF ACRID SMOKE SMELL IN AFT OF CABIN. FLIGHT ATTENDANT CONFIRMED THE ACRID SMELL OF SMOKE. THEY NOTED THAT THEY REALLY COULD NOT SEE ANY SMOKE BUT DID SMELL IT. WE HAD A KIND OF DIRTY PACK SMELL IN COCKPIT & AGAIN NO SMOKE WAS SEEN IN COCKPIT OR CABIN.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 35,702 hrs · 32,841 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR IS HARD TO OPEN & IS GETTING JAMMED AT THE LT LOWER CORNER OF THE DOOR. EXERCISED & CLEANED ROLLERS & LUBED DOOR IAW AMM 52-18-00 & PERFORMED PULL TEST ON HANDLE IAW AMM 52-10-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: DOOR SEAL — DIRTY (CABIN DOOR) · airframe 35,601 hrs · 32,760 cycles

MAIN CABIN DOOR FLIGHT ATTENDANT REPORTS TOO HARD TO OPEN. CLEANED & LUBED DOOR SEAL IAW AMM 52-18-00.

Part: INDICATION SYS — FAULTY (SPOILER) · airframe 35,574 hrs · 32,743 cycles

ITEM 1 SPOILER FAIL EICAS MSG DURING DESCENT. CMC MSG GND SPOILER ENG CKT FAULT. TROUBLE SHOT IAW FIM TASK 27-63-00-810-808. FOUND OPEN INDICATION AT P 7209 - Y TO GND IAW STEP 5 BLOCK 2.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 35,416 hrs · 32,610 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. RECONNECTED CONNECTOR IAW AMM 33-50-10. OPERATIONS CHECKED OK.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,267 hrs · 32,494 cycles

ON FLIGHT 3592 CREW REPORTED STRONG OIL SMELL IN BLEED SYS AFTER TAKEOFF & IN THE DESCENT BELOW APPROXIMATELY 15000. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED FIM TASK 21-20-00-810-803-A & PERFORMED ENG OPERATIONAL CHECK IAW AMM 72-00-00. OPERATIONS CHECKED GOOD NO SMELL NOTED AT THIS TIME. PERFORMED ETN-EM-72-034 FOR ENG ODOR EVENTS. THE AIRCRAFT RETURN TO SERVICE.

Part: HOLDER — CRACKED (FLASHLIGHT) · airframe 35,221 hrs · 32,460 cycles

FORWARD CABIN EMERGENCY FLASHLIGHT HOLDER CRACKED. R & R FWD CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: HANDLE — CRACKED (CABIN DOOR) · airframe 35,187 hrs · 32,433 cycles

MAIN CABIN DOOR INNER HANDLE CRACKED, CAUSING DOOR NOT TO OPEN. R & R MAIN CABIN DOOR INNER ACTUATING HANDLE IAW EMB-145 AMM 52-18-05. OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — ODOR · airframe 35,167 hrs · 32,415 cycles

PACK NR 1 OUTPUTS STRONG DIRTY SOCK SMELL WHILE ENG NR 1 IS THE AIR SOURCE ONLY. FCF REQUIRED FOR STRONG DIRTY SOCK SMELL WHILE ENG NR 1 IS THE AIR SOURCE ONLY. AIRCRAFT RELEASED FOR FCF PURPOSES ONLY. C/W ETN-EM-72-034 FOR ENG ODOR EVENT TROUBLESHOOTING SUPPLEMENT. NO SMELL NOTICE AT16'S TIME.

Part: WIRE — DAMAGED (CABIN) · airframe 35,167 hrs · 32,415 cycles

EMERGENCY FLOOR LIGHT STRIP AT ROW 6ABC. REPAIRED WIRE & SPLICE IAW AMM 33-50-12, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,123 hrs · 32,375 cycles

RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EXTERNAL UPPER WING EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 35,105 hrs · 32,359 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR HARD TO OPEN. PERFORM THE ADJUSTMENT OF THE PASSENGER MAIN DOOR IAW ACFT EMB145 AIRCRAFT PN SN EMB145 & 145081. PERFORMED TEST MAIN DOOR IAW EMB AMM 52-18-00-820-801. LUBRICATED ROLLERS IAW EMB AMM 52-18-00-600-801 TEST AT 38LBF AVG AFTER LUBE OPC GOOD AT THIS TIME.

Part: DOOR — BINDING (MAIN PAX) · airframe 34,873 hrs · 32,178 cycles

F/A REPORTED MAIN CABIN DOOR HARD TO OPEN. PERFORM ADJUSTMENT OF THE PAX DOOR IAW AMM 52-18-00.

Part: FLASHLIGHT ASSY — BROKEN (COCKPIT) · airframe 34,658 hrs · 32,008 cycles

CAPTAIN`S FLASHLIGHT BROKEN. R & R FLASHLIGHT IAW AMM 33-50-16.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,658 hrs · 32,008 cycles

RIGHT OVERWING AFT EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-50-07, OPS CHECKED GOOD.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 34,211 hrs · 31,642 cycles

DURING HMBV INSPECTION, FOUND CORROSION AROUND NUTPLATE HOLE ON AFT LOWER SURFACE OF DOOR CUTOUT BELOW DOOR STOP. ACFT REMOVED FROM SERVICE. PERFORMED REPAIR OF DOOR FRAME IAW EO-EM-53MR-2166.

Part: SKIN — DENTED (FORWARD FUSELAGE) · airframe 34,211 hrs · 31,642 cycles

DURING HMBV INSPECTIONI, FOUND A FORWARD FUSELAGE DENT WITH TOOLING DAMAGE BETWEEN FRAMES 5-6 AT STRINGER 13L. PERFORMED REPAIR IAW EO-EM-53MR-2165.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 34,211 hrs · 31,642 cycles

NR 6 EMERGENCY PROXIMITY LIGHT STRIP WIRES DAMAGED. RAR NR 6 EMERGENCY FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 34,252 hrs · 31,678 cycles

VERTICAL STABILIZER FWD DRAG ANGLE CRACKED. REPAIRED IAW EO EM-53MR-1281.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,211 hrs · 31,642 cycles

AFT LOWER FUSELAGE HAS A PROTRUSION AT FR 67 BETWEEN STGR 21L AND 21R. REPAIRED AFT LOWER FUSELAGE SKIN AT FR 67 BETWEEN STGR 21L AND 21R IAW AEA EO EM-53MR-2163.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 34,211 hrs · 31,642 cycles

NR 1 EMERGENCY PROXIMITY LIGHT STRIP WIRES DAMAGED. RAR NR 1 FLOOR PROXIMITY STRIP TO COVER PANEL AS REQUIRED. SEE BOW131733 FOR INSTALLATION OF FLOOR STRIPS.

Part: SHEAR TIE — CORRODED (CARGO DOOR) · airframe 34,211 hrs · 31,642 cycles

CARGO DOOR SHEAR TIE AT FR 65 IS CORRODED. REPAIRED SHEAR TIE IAW EO EM-53MR-1129.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 34,211 hrs · 31,642 cycles

NR 4 EMERGENCY PROXIMITY LIGHT STRIP WIRES DAMAGED. R & R NR 4 FLOOR PROXIMITY STRIP TO COVER PANEL AS REQUIRED.

Part: DOOR — BINDING (MAIN) · airframe 34,202 hrs · 31,631 cycles

THE F/A REPORTED THE MAIN DOOR WAS DIFFICULT TO OPERATE. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED MAIN DOOR HANDLE ACTUATION TEST WITH NO DEFECTS NOTED IAW AMM CH 52-10-01 PEAK LOAD 40LBS. THE ACFT WAS RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 34,108 hrs · 31,550 cycles

THE CREW REPORTED THE PASSENGER DOOR WAS HARD TO OPEN & CLOSE. THE ACFT WAS REMOVED FROM SERVICE. LUBRICATED OPEN AND CLOSE MECHANISM ON MAIN PASSENGER DOOR IAW MM 52-18-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FAN — FAILED (LT RECIRCULATION) · airframe 33,955 hrs · 31,423 cycles

FLIGHT 2908, CREW REPORTED DURING CRUISE, DETECTED AN ELECTRICAL BURNING ODOR. ODOR DISSIPATED AFTER TURNING RECIRCULATION FANS OFF. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R THE LT RECIRCULATION FAN. OPS CHECKED GOOD IAW AMM 21-24-01. NO ODOR WAS PRESENT AT THIS TIME. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,178 hrs · 30,820 cycles

DURING B INSPECTION FOUND THE EMERGENCY AISLE LIGHT AT ROW 7 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT AISLE EMERGENCY LIGHT ROW 7 IAW EMB AMM TASK 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — FAILED (RIGHT) · airframe 33,154 hrs · 30,801 cycles

FLIGHT 3917. DURING CRUISE ALTITUDE FL 360, NR 2 ENGINE ITT ON EICAS SPIKED TWICE, AND TEMP AS HIGH AS 1015 DEGREES. WITH THE SPIKES TWO SEPARATE VIBRATIONS WERE FELT. NR 2 ENGINE THEN HAD AN UN-COMMANDED SHUTDOWN. OIL SHOWED TO BE 4 QUARTS. AT DEPARTURE, HAD AT LEAST 10 QUARTS. FOLLOWED EMERGENCY PROCEDURES FOR AN ENGINE FAILURE. DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. CHECKED AIRCRAFT AND DID NOT FIND ANY DEBRIS, LEAKAGE, SMOKE OR FIRE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 ENGINE IAW WC 71-000-00. ALL REQUIRED CHECKS ACCOMPLISHED, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSERVICEABLE (CABIN) · airframe 33,021 hrs · 30,698 cycles

ON FLIGHT 4286 THE CREW REPORTED THE AFT CABIN FLASHLIGHT HOLDER CLIP FELL OFF (CABIN BULKHEAD). THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,399 hrs · 30,191 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OVER THE WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ELECTRICAL CONNECTOR ON RIGHT OVER THE WING EMERGENCY LIGHT LOOSE, AND RE-SECURED RIGHT OVER THE WING EMERGENCY LIGHT AND PERFORMED AN OPERATIONAL CHECK IAW EMB145 AMM 33-50-10. REMOVED AND REPLACED THE RIGHT AFT EXTERIOR LIGHT BULB. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,310 hrs · 30,116 cycles

DURING B INSPECTION FOUND THE RIGHT OVER THE WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ELECTRICAL CONNECTOR ON RIGHT OVER THE WING EMERGENCY LIGHT LOOSE, AND RE-SECURED RIGHT OVER THE WING EMERGENCY LIGHT AND PERFORMED OPERATION CHECK IAW EMB145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 32,269 hrs · 30,077 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OVER WING EMERGENCY LIGHT IS NOT WORKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REINSTALLED CONNECTOR TO RIGHT OVER WING EMERGENCY LIGHT FIXTURE IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,236 hrs · 30,041 cycles

DURING MAINTENANCE INSPECTION FOUND THE OVERWING FORWARD EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND CRADLE IAW AMM 33-50-04 OPS. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 32,061 hrs · 29,907 cycles

DURING B-INSPECTION FOUND THE FIRST OFFICER’S EMERGENCY FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S EMERGENCY FLASHLIGHT HOLDER IAW EMB 145 AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,849 hrs · 29,737 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS AND LEFT EMERGENCY EXIT AFT ILLUMINATED "EXIT" SIGN INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EPSU BATTERY AND CHARGER IAW AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,718 hrs · 29,639 cycles

DURING B INSPECTION, FOUND THE SERVICE DOOR MOUNTED EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMPS AT SERVICE DOOR, AND OVER LEFT AND RIGHT WINGS IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A, . REMOVED AND REPLACED BATTERY AND BATTERY CHARGERS. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,957 hrs · 29,030 cycles

DURING MAINTENANCE INSPECTION FOUND THE COCKPIT DOOR STEP AND GALLEY CEILING PANEL EMERGENCY LIGHTS OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT DC/AC INVERTER IAW EMB-145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,879 hrs · 28,963 cycles

DURING B-INSPECTION FOUND THE LOWER COCKPIT DOOR EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND CHARGER IAW WORK CARDS 33-700-19 AND 33-700-17. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 30,491 hrs · 28,676 cycles

ON FLIGHT 3274 THE CREW REPORTED THE CAPTAINS FLASHLIGHT HOLDER WAS BROKEN. THE UPPER CLIP HAD BROKEN OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS FLASHLIGHT HOLDER IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,310 hrs · 28,548 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,106 hrs · 28,407 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,031 hrs · 28,359 cycles

DURING MAINTENANCE VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT BULB IAW AE WC 33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 29,839 hrs · 28,229 cycles

ON FLIGHT 2913 THE CREW REPORTED THE MAIN DOOR WAS EXTREMELY HARD TO OPEN UP. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED DOOR PER ERJ 145 AMM 52-18-00 AND PERFORMED OPERATIONAL CHECK IAW EMB 145 AMM 52-00-00. FOUND TO BE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 29,783 hrs · 28,196 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EXIT AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED CONNECTOR ON LIGHT ASSEMBLY. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 29,783 hrs · 28,196 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OVERWING EXIT AFT EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND CONNECTOR ON RIGHT AFT EXTERNAL OVERWING EMERGENCY LIGHT NOT CONNECTED. CONNECTED CONNECTOR IAW EMB-145 AMM 33-50-07. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,726 hrs · 28,150 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND APROXIMATELY 1.5 INCH CRACK ON AFT UPPER CORNER OF THE LEFT HAND DV WINDOW CUTOUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-1888 PT B. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,726 hrs · 28,150 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND APROXIMATELY 2 INCH CRACK ON AFT UPPER CORNER OF THE RIGHT DV WINDOW CUTOUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-1888 PT A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 29,726 hrs · 28,150 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE RIGHT WING 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH AEA EO EM-57MR-587. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 29,726 hrs · 28,150 cycles

DURING MAINTENANCE VISIT FOUND THE LEFT WING 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERIVCE. COMPLIED WITH AEA EO EM-57MR-588. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 29,726 hrs · 28,150 cycles

DURING MAINTENANCE VISIT FOUND THE RIGHT WING 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERIVCE. COMPLIED WITH AEA EO EM-57MR-587. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 29,726 hrs · 28,150 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT WING 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH AEA EO EM-57MR-588. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,726 hrs · 28,150 cycles

DURING MAINTENANCE BASE VISIT FOUND THE COCKPIT UNDERFLOOR CENTER BAYS FROM FRAME 13--15 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED COCKPIT UNDER FLOOR FRAME 13 TO FRAME 15 CORROSION IAW EO EM-53MR-1882. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 29,726 hrs · 28,150 cycles

DURING A MBV INSPECTION DISCOVERED THE LT WING RIB NR 5 TO BE CRACKED. THE CRACKS ARE VISIBLE LOOKING I/B THROUGH 532AB LOOK THROUGH THE LIGHTENING HOLES IN RIB 6. THE CRACKS EXTEND OUT FROM THE LIGHTENING HOLES IN RIB 5.

Part: RIB — CRACKED (RT WING) · airframe 29,726 hrs · 28,150 cycles

DURING A MBV INSPECTION DISCOVERED THE RT WING RIB NR 5 TO BE CRACKED. THE CRACKS EXTEND OUT FROM THE LIGHTENING HOLES. THE CRACKS CAN BE VISIBLE SEEN BY LOOKING THROUGH ACCESS PANELS 632AB. LOOK THROUGH THE ACCESS PANEL HOLE AND LOOK I/B THROUGH THE LIGHTENING HOLES OF RIB 6. WE HAVE SEEN CRACKS ON A PREVIOUS AIRCRAFT WITH THE CRACKS FROM THE LIGHTENING HOLES ALONG WITH A CRACK EXTENDING UP FROM THE BOTTOM FLANGE.

Part: HYDRAULIC LINE — DAMAGED (HYDRAULIC SYS) · airframe 29,614 hrs · 28,069 cycles

BURNING SMELL FROM BEHIND CAPT SEAT. REPAIRED HYD LINE UNDER CAPT FLOORBOARD IN COCKPIT.

Part: WIRE — CUT (EMERGENCY LIGHT) · airframe 28,495 hrs · 27,183 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT BELOW THE COCKPIT DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. DURING TROUBLESHOOTING, FOUND WIRE CUT. INSTALLED SPLICE IAW EMB AMM P/T 20-21-00, STEP B4. THE OPERATIONAL CHECK WAS GOOD IAW AE W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GEARBOX — DEFECTIVE (TE FLAP) · airframe 26,974 hrs · 26,076 cycles

ON FLIGHT 3940 THE CREW REPORTED DURING DESCENT INTO LEX RECEIVED AN EICAS MESSAGE FLAPS FAIL, ALSO THE FLAPS WOULD NOT MOVE. THE CAPTAIN DECLARED AN EMERGENCY. THE RUNWAY WAS NOT LONG ENOUGH TO LAND IN LEX, SO THE CREW ELECTED TO DIVERT INTO SDF. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND RIGHT INBOARD ANGLE GEAR BOX BAD. REPLACED GEAR BOX PER AMM 27-51-0. THE OPERATIONAL CHECK PER AMM 27-51-00 IS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — BROKEN (COCKPIT) · airframe 25,492 hrs · 25,302 cycles

FOR FLIGHT 3995 THE CREW DISCOVERED THE TOP PRONG THAT HOLDS THE CAPTAINS SIDE FLASHLIGHT IS BROKEN OFF AND DOES NOT HOLD FLASHLIGHT SECURELY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS FLASHLIGHT ASSEMBLY IAW EMB145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 24,860 hrs · 24,448 cycles

DURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR CENTER SILL TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 23,233 hrs · 22,973 cycles

ON FLIGHT 3322, CREW REPORTED BAG SMOKE INDICATION AT 400 AGL AOM PROCEDURES FOLLOWED. AFTER LANDING CFR INSPECTED NO FIRE INDICATED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT CARGO FORWARD SMOKE DETECTOR IAW WITH EMB 145 AMM 26-15-01. OPS CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT CARGO BAY) · airframe 23,146 hrs · 22,907 cycles

ON FLIGHT 3890 CREW REPORTED AT 400 FEET ON FINAL. BAGG SMOKE MESSAGE ON EICAS AND OVERHEAD EXT BUTTON ILLUMINATED. PERFORMED EPC AOM VOL PROCEDURES NO SMOKE/FIRE NOTED BY FLIGHT ATTENDANT OR CFR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BAGGAGE METERING EXTINGUISHER BOTTLE IAW AMM 26-23-01. OPERATIONAL CHECK GOOD IAW AMM 26-15-00. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 22,674 hrs · 22,467 cycles

ON FLIGHT 9805 CREW REPORTED ON CLIMB-OUT STRONG ODOR OF SMOKE IN COCKPIT. CREW RETURNED TO FIELD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT WINDSHIELD CONTROLLER IAW AMM 30-42-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,049 hrs · 20,844 cycles

ON FLIGHT 4227 - DURING CRUISE, CREW REPORTED A STRONG ELECTRICAL ODOR AT FL280. THE F/A NOTED THE ODOR AS SHE APPROACHED THE COCKPIT DOOR. ODOR DISSIPATED SHORTLY BEFORE THE APPROACH TO DSM. AIRCRAFT REMOVED FROM SERVICE. PERFORMED INSPECTION OF COCKPIT AND FORWARD AVIONICS. NO DEFECTS NOTED IAW AMM 06-41-02, 30-42-03 AND 20-17-03. AIRCRAFT RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — MALFUNCTIONED (NLG) · airframe 20,435 hrs · 10,693 cycles

FLT 4105 - CREW CALLED TO REPORT LANDING GEAR AIR GROUND FAIL MSG ON TAKEOFF AND GEAR WOULD NOT INITIALLY RETRACT. CREW DID GET GEAR UP. ALSO RECEIVED BLEED 2 CLOSED MESSAGE. AC LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR PROX SWITCH AND FUNCTIONAL CHECK OF PROX SWITCH IAW EMB 145 32-63-00 AND PERFORMED EXTENSION RETRACTION TEST IAW EMB AMM 32-30-00. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED · airframe 20,435 hrs · 10,693 cycles

CREW REPORT LANDING GEAR AIR GROUND FAIL MSG ON TAKEOFF AND GEAR WOULD NOT INITIALLY RETRACT. CREW DID GET GEAR UP. ALSO RECEIVED BLEED 2 CLOSED MESSAGE. AC LANDED WITHOUT INCIDENT.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,068 hrs · 19,901 cycles

DURING MBV INSP, AFT LOWER SERVICE DOOR FRAME CORRODED. REPAIRED FRAME IAW EO EM-53MR-842. AIRCRAFT RETURN TO SERVICE.

Part: FAN BLADE — OUT OF BALANCE (NR 1 ENGINE) · airframe 17,991 hrs · 18,119 cycles

ENGINE ONE VIBRATIONS. REMOVED AND REPLACED 2 BLADE SETS IAW ROLLS ROYCE MM 72-21-15. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: HANDLE — CRACKED (PAX DOOR)

A CRACK WAS DISCOVERED ON THE PASSENGER DOOR INNER HANDLE BRACKET. STOP DRILLED THE CRACK ON THE PAX DOOR HANDLE BRACKET. FABRICATED A REINFORCEMENT ANGLE. REPAIR DONE IAW SRM. (K)

Part: SUPPORT — DAMAGED (APU MOUNT)

THE APU COWLING RT LOWER MOUNTING SUPPORT AREA WAS FOUND DAMAGED. FABRICATED A REINFORCEMENT DOUBLER. REPAIR DONE IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING CUTOUT. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (FUSELAGE)

THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED LOWER SILL. INSTALLED SERVICEABLE SILL IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED AHT PREVIOUS REPAIR. PREPARED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)

Part: SWITCH — LEAKING (HYDRAULIC SYS)

CREW REPORTED AIRCRAFT HAD HYDRAULIC SYSTEM 2 FAIL IN FLIGHT. THEY FOLLOWED THE AOM AND CONTINUED AND PERFORMED AN EMERGENCY LANDING. AIRCRAFT LANDED SAFELY WITH NO OTHER INCIDENTS. FOUND NR 2 HYDRAULIC SYSTEM SWITCH LEAKING REPLACED SWITCH. FOUND NR 2 EDMP PRESSURE LINE LEAKING REPLACED LINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. PARTS REPLACED SWITCH 156221 AND LINE 15622101. (SW21200501199)

Part: SOLENOID — MALFUNCTIONED (NLG)

DFW - FLT 3819 - CAPTAIN REPORTED NOSE GEAR DOOR FAILED TO CLOSE AFTER GEAR RETRACTION. INSTALLED NEW NOSE LANDING GEAR DOOR SOLENOID VALVE IAW EMB AMM 32-33-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) SIMA

Part: WINDOW POST — CORRODED (COCKPIT)

WHILE CHANGING THE CO-PILOTS WINDSHIELD TWO FASTENER HOLES IN THE LOWER AFT CORNER OF THE AIRFRAME OPENING WERE FOUND TO BE CORRODED. ONE OF THE FASTENER HOLES REMAINED WITHIN MANUFACTURERS LIMITS AFTER REMOVAL OF CORROSION. APPLIED ALODINE AND EPOXY PRIMER TO THIS HOLE. REMOVED NUTPLATE FROM SECOND HOLE AND REAMED WINDSHIELD LOWER BEAM AND BELT STRAP TO .313 IN. FABRICATED A BUSHING WITH 100 DEGREE COUNTERSINK TO FILL THE REAMED HOLE. REPAIR DONE IAW AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-039 AND EMB REPAIR STATEMENT 1C2004-145/1439. (M)

Part: ACM — INOPERATIVE (NR 2)

ORD - FLT 4246 - DURING CLIMB CREW REPORTED AN ELECTRICAL/SULPHUR ODOR IN THE COCKPIT AND THE FLIGHT ATTENDANT REPORTED A SMALL AMOUNT OF SMOKE IN THE CABIN. THE AIRCRAFT WAS RETURNED TO ORD AND THE SMOKE DISSIPATED DURING THE LANDING. MAINTENANCE REMOVED AND REPLACED THE NR 2 ACM IAW EMB MM. OPERAITONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — PUNCTURED (FUSELAGE)

DURING A PS2 INSPECTION A 1.5 INCH PUNCTURE WAS DISCOVERED BETWEEN FRAMES 65-66 AND STRINGERS 20L AND 21L. PERFORMED A CUT OUT OF THE DAMAGED AREA. PERFORMED A EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW STATEMENT GST300602.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, FORWARD GIGITAL IN GALLEY HAS CORROSION. INSTALLED REPAIR DOUBLER IAW EMB GST-1140/02 AND 1169/02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, RIGHT OMEGA BEAM CORRODED AT FRAME 25. BLENDED CORROSION, PERFORMED NDT INSPECTION. RESTORED SURFACE FINISH, IAW EMB GST-1140/02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIGHT OMEGA BEAM BETWEEN FRAMES 23 AND 25. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMBRAER GST-1140/02 DAMAGE NR 13, GST-1169/02, ITEM 2 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND CORROSION IN TWO AREAS, FORWARD AND AFT, ON FORWARD DIGITAL. REMOVED CORROSION BY BLENDING AREAS. FABRICATED TWO REPAIR DOUBLERS. REPAIR DONE IAW EMB GST-1140/02, DAMAGE NR 9, GST-1169/02, ITEM 4, AND STANDARD SRM PRACTICES. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20. REMOVED PREVIOUS REPAIR (CORROSION LIMITED TO PREVIOUS REPAIR). FABRICATED A DOUBLER ANGLE, AND FILLER. REPAIRED IAW EMB145 SRM-145/1142, CHAPTERS 53, REV 17, 53-21-10, GST-1140/02 DAMAGE NR 11 AND STANDARD SRM PRACTICES. (M)

Part: BEAM — CORRODED (FUSELAGE)

ABI - DURING ABV INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY RIGHT BEAM AT FRAME 23. REMOVED CORROSION BY BLENDING. FABRICATED A U-SHAPE REPAIR. REPAIRED IAW EMB GST-1140/02, DAMAGE NR 7 AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIGHT SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. FABRICATED AND INSTALLED DOUBLER IAW EMB GST-1140/02 AND STANDARD SRM PRACTICES. (M)

Part: FRAME — CHAFED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND FRAME 81 CHAFED. REPLACED CHAFED FRAME IAW EMB 145 SRM 51-20-03, 51-40-03, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY CENTER BEAM. REPLACED GALLEY CENTER BEAM IAW EMB 145 EMB SRM 145 51-40-02, GST-1128/02, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. RIGHT OMEGA BEAM HAS CORROSION BETWEEN FRAMES 23 AND 25. FABRICATED DOUBLER IAW EMB145 SRM 51-40-02, 51-40-06, 51-20-03 AND GST-1169/02. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

THIS IS A LEVEL 2 FINDING. RIGHT AFT SILL IN GALLEY HAS CORROSION. INSTALLED NEW AFT SILL IAW EMB 145 SRM 51-40-02, 51-40-06, 51-20-03. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

THIS IS A LEVEL 2 FINDING. GALLEY LEFT SILL HAS CORROSION. INSTALLED LEFT SILL IAW EMB 145 SRM 51-40-02. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. GALLEY CENTER BEAM GUSSET CORRODED. INSTALLED SERVICEABLE GUSSET BEAM IAW EMB 145 SRM 51-40-02. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. GALLEY RIGHT CROSSBEAM HAS CORROSION AT NUTPLATE FORWARD OF CROSSBEAM AND PROFILE. REPAIRED IAW EMB145 GST-1140/02, SRM 51-40-02, 51-40-06, 51-40-03. (M)

Part: FLOOR SUPPORT — CORRODED (GALLEY) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. GALLEY CENTER BEAM CORRODED. INSTALLED SERVICEABLE CENTER BEAM IAW EMB145 SRM 51-40-02. (M)

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. LEFT OMEGA BEAM REPAIR AT FRAME 20 HAS MINOR CORROSION. INSTALLED NEW OMEGA BEAM REPAIR AT FRAME 20 IAW EMB GST-1140-/02 AND SRM 51-40-02. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. PASSENGER ENTRY FLOORBOARD SUPPORT HAS CORROSION. INSTALLED NEW FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02, 51-40-03, 51-40-06. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, RIGHT FORWARD SILL IN GALLEY HAS CORROSION. REMOVED DAMAGED FORWARD SILL, INSTALLED NEW FORWARD SILL IAW EMB 145 SRM 51-40-02, 51-40-06, 51-20-03. (M)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. GALLEY RAMP SUPPORT CORRODED. INSTALLED SERVICEABLE GALLEY RAMP IAW EMB145 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

THIS IS A LEVEL 2 FINDING. AFT DIAMOND GUSSET IN GALLEY HAS CORROSION. INSTALLED SERVICEABLE AFT DIAMOND IAW EMB 145 SRM 51-40-02, 51-20-03, 51-40-06. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. LEFT OMEGA BEAM CORRODED AT FRAME 25. BLENDED CORROSION, PERFORMED NDT, RESTORED PROTECTIVE FINISH, ACCEPTED AS IS IAW EMB 145 GST-1140/02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

THIS IS A LEVEL 2 FINDING. LEFT OMEGA BEAM HAS CORROSION BETWEEN FRAMES 22 AND 23. BLENDED CORROSION, PERFORMED NDT, RESTORED PROTECTIVE FINISH, ACCEPTED AS IS IAW EMB GST-1140/02. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. RIGHT CENTER SILL IN GALLEY HAS CORROSION. REPAIRED IAW EMB GST-1140/02. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. RIGHT CABIN FORWARD FLOOR SUPPORT HAS CORROSION. BLENDED CORROSION, RESTORED PROTECTIVE TREATMENT, ACCEPTED AS IS IAW EMB 145 GST-1140/02. (M)

Part: DUCT — DAMAGED (NR 1 ENGINE)

TVC - FLT 4253 - ENGINE FIRE WARNING JUST AFTER CLIMB-OUT, THEN EXTINGUISHED. THE CREW SHUT DOWN NR 1 ENGINE, DECLARED EMERGENCY AND RETURNED TO TVC FOR MAINTENANCE, LANDED SAFELY. REPLACED BROKEN DUCT BETWEEN HIGHT STAGE VALVE AND ENGINE ANTI-ICE VALVE. (M)

Part: FIRE WARNING — ACTIVATED (COCKPIT)

TVC - FLT 4253 - CREW REPORTED, A E1 FIRE WARNING JUST AFTER CLIMB-OUT AND THEN IT WENT OUT. THE CREW DECLARED AN EMERGENCY AND SHUTDOWN THE ENGINE. THE AIRCRAFT WAS RETURNED TO TVC AND LANDED WITH NO FURTHER INCIDENTS. (M)

Part: CONTROL VALVE — FAULTY (THRUST REVERSER)

SHV - FLT 3370 - ABORTED TAKEOFF, NR 2 THRUST REVERSE DISAGREE ICAS MESSAGE. MEL REMOVED AND REPLACED NR 2 ISOLATION CONTROL VALVE UNIT IAW EMB 78-33-01. OPS CHECK GOOD. (M)

Part: COMPUTER — MALFUNCTIONED (COCKPIT)

MKE - FLT 4030 - ON APPROACH INTO ORD TUNING NR 2 RMU WENT TO DASHES. CHANGED TO NR 1 SYSTEM AND IT WENT TO DASHES. BACK UP CONTROL HEAD ALSO WENT TO DASHES. DIVERTED INTO MKE BECAUSE THEY LOST THEIR ILS SYSTEM AND THEY NEEDED IT TO LAND IN ORD. RESET CIRCUIT BREAKERS FOR RMU, DAU AND 1-C600 WITH OUT RESETTING POWER. MAINTENANCE WENT OUT AND PERFORMED OPS CHECK AND FOUND TO BE GOOD IAW AMM. (M)

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB)

ORD - FLT 4117 - CREW REPORTED THAT THE PITCH TRIM 1 FAILED AT ABOUT 3000 AGL AND 220 KIAS AFTER TAKEOFF. CREW ALSO NOTED THAT THE STANDY TRIM DID NOT WORK. MAINTENANCE REMOVED AND REPLACED THE HSCU. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ENGINE — FAILED (NR 2 FAILED)

ORF - FLT 4365 - CREW REPORTED UPON TOUCH DOWN AND THRUST REVERSERS DEPLOYED, A LOUD BANG WAS HEARD FOLLOWED BY THE NR 2 ENGINE SHUTTING DOWN. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACTUATOR — OUT OF ADJ (NR 1 T/R)

DFW - FLT 3437 - DURING TAKEOFF ROLL, CREW NOTED ENGINE NR 1 THRUST REVERSER DISAGREE MESSAGE ON EICAS. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE ADJUSTED LOWER T/R ACTUATOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — FAILED (LT WING) · airframe 3,245 hrs · 3,535 cycles

OMA - FLT 4148 - LEFT OVER WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT EXTERNAL ASSY. OPS CHECK GOOD. (X)