N680AE

Part: NONE — NONE · airframe 41,502 hrs · 36,899 cycles

12C PSU EMERGENCY LIGHT INOP-C/A-RAR 12C PSU EMERGENCY LIGHT IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: NONE — NONE · airframe 41,113 hrs · 36,444 cycles

EXIT ROW CABIN AISLE CEILING EMERGENCY EXIT LOCATOR SIGN, AFT FACING LIGHTED SIGN INOP-C/A-RAR AFT FACING EXIT ROW EMERGENCY EXIT LOCATOR LIGHTED SIGN IAW AMM 33-50-15. DID NOT FIX. RE-ENTERED AS ITEM #2 THIS NRWC.

Part: PUMP — LEAKING (NR 1 HYD SYSTEM) · airframe 40,909 hrs · 36,210 cycles

E 1 HYD PUMP FAIL EICAS MSG @ 3100 FT. HYD SYS 1 FAIL. LANDED SAFELY IN DFW DECLARED EMERGENCY.DURING TROUBLE SHOOTING FOUND ENGINE 1 HYD PUMP UPPER PRESSURE HOSE CHAFFED AND LEAKING FLUID. REF LOG PAGE 4759892 ITEM # 2 -C/A-REMOVED AND REPLACED ENGINE 1 HYD PUMP UPPER PRESSURE HOSE IAW EMB 145 AMM CH 29-10-20, 29-10-03. SEE ITEM #2 THIS NRWC 680-DFW-04976 FOR LEAK CHECK

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,631 hrs · 35,874 cycles

DURING PS-2 CHECK, FOUND LH FWD EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR LH FWD EXTERNAL EMERGENCY LIGHTS IAW EMB 145 AMM TASK 33-50-10. OPC GOOD

Part: WIRE — DETACHED (EMERGENCY LIGHT) · airframe 40,534 hrs · 35,756 cycles

AFT EMERGENCY FLOOR STRIP LIGHT, OVER FLOOR PANEL 251HF. WIRE SEPARATED FROM PLUG. INSTALLED CONNECTOR ON EMERGENCY STRIP LIGHT IAW E145 SWMP 20-21-00.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,445 hrs · 35,653 cycles

AFT AISLE EMERGENCY SIGN AND SEAT 12A EMERGENCY OVER HEAD LIGHT INOP-C/A-T/S IAW FIM TASK 33-50-00-810-804-A RAR #3 BATTERY POWER SUPPLY 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 NO FURTHER DEFECTS NOTED AT THIS TIME

Part: BATTERY PACK — INOPERATIVE (EXTERIOR LIGHTS) · airframe 40,266 hrs · 35,455 cycles

EXTERNAL EMERGENCY LIGHTS OVER L/H AND R/H WINGS INOP-C/A-TROUBLESHOT AND FOUND EMERGENCY BATTERY #4 INOP. RAR #4 EMERGENCY BATTER IWA W/C 33-700-19. OPS CHECK GOOD

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,266 hrs · 35,455 cycles

EMERGENCY EXIT SIGN, AFT MID CEILING INOP.-C/A-RAR AFT MID CEILING EMERGENCY EXIT SIGN IAW AMM 33-50-15.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,250 hrs · 35,437 cycles

AFT EMERGENCY EXIT SIGN ABOVE EMERGENCY EXIT ROWS INOP-C/A-RAR #4 BATTERY AND CHARGER ASSY OPC GOOD IAW AMM 33-50-04

Part: BATTERY PACK — MISINSTALLED (EMERGENCY LIGHTS) · airframe 40,196 hrs · 35,383 cycles

LAST 3 FLOOR EMERGENCY LIGHT STRIP INOP-C/A-T/S IAW EMB FIM 33-50-00-810-804-A. FOUND #4 BATTERY TO BE INSTALLED IMPROPERLY. INSTALLED BATTERY PACK IAW EMB AMM 33-50-04-400-802-A. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,161 hrs · 35,343 cycles

EMERGENCY CEILING LIGHT INOP-C/A-FOUND OVER AISLE CEILING PANEL AND AISLE LIGHT 4 INOP T/S IAW FIM TASK 33-50-00-810-804-A. RAR #4 BATTERY POWER SUPPLY AND #4 BATTERY PACK IAW W/C 33-700-19 NO FIX. FOUND ASILE LIGHT 4 BULB INOP RAR IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A OPS CHECK GOOD. FOUND OVER AISLE CONNECTOR LOOSE ADJUSTED IN REF WITH EMB AMM 33-50-15-400-801-A OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,116 hrs · 35,295 cycles

EMEREGNCY EXIT SIGN, MID CEILING. AFT SIDE OF SIGN NO ILLUMINATION-C/A-RAR AFT SECTION OF EMERGENCY EXIT SIGN IAW EMB145 AMM 33-50-15. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,100 hrs · 35,277 cycles

OVERWING EMERGENCY LIGHTS INOP-C/A-RAR # EMERGENCY LIGHT BATTERY CHARGER ASSY, OPC GOOD, IAW EMB AMM 33-50-04

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,971 hrs · 35,152 cycles

LH AND RH OVER WING EMERGENCY EXIT LIGHTS INOP-C/A-RAR #4 BATTERY AND CHARGER ASSEMBLY IAW W/C 33-700-19. OPC GOOD IAW W/C 33-700-17

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 39,924 hrs · 35,108 cycles

MAIN DOOR WILL NOT CLOSE (TOP FLAP WILL NOT SHOT)-C/A-LUBRICATED MAIN DOOR ROLLERS IAW AMM 52-11-00. OPS CHK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,244 hrs · 34,457 cycles

GALLEY EMERGENCY LIGHT INOPERABLE. C/A R & R GALLEY EMERGENCY LIGHT LAMP, IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,078 hrs · 34,310 cycles

DURING PS CHECK FOUND OVERWING EMER EXIT LIGHT INOPERATIVE. R 7 R BATTERY POWER SUPPLY IAW AMM 33-50-04-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,046 hrs · 34,281 cycles

EXTERNAL EMERGENCY LIGHT ON MAIN CABIN DOOR INOPERATIVE. R & R EXTERNAL EMERGENCY LIGHT ON MAIN CABIN DOOR IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 38,923 hrs · 34,164 cycles

LT AFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT AFT OVERWING EMERGENCY LIGHT LAMP IAW 33-50-10, OPC GOOD IAW 33-50-00.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 38,862 hrs · 34,119 cycles

FUEL SMELL IN COCKPIT AFTER STARTING APU AFTER LANDING. C/A-PERFORMED FIM 21-20-00-810-803-A GROUND RAN ENGINE 1 AND 2 IAW AMM 71-00-01 AND AMM 49-10-00 COULD NOT DUPLICATE FUEL SMELL WITH THE APU RUNNING. PERFORMED DETAILED VISUAL INSPECTION ON NR 1 ENGINE, NR 2 ENGINE, NR 1 WING, NR 2 WING, AND APU FOR FUEL OR OTHER LEAKS. NO LEAKS NOTED. PERFORMED DETAILED VISUAL INSPECTION OF NR 1 PACK AND NR 2 PACK FOR ANY LEAKS, DAMAGE, OR BLOWN DUCTING. NO DAMAGE, NO LEAKS, OR BLOWN DUCTING NOTED. RAN BOTH ENGINES AND APU AT THE SAME TIME FOR 1 HOUR AT IDLE AND POWER TO TRY AND DUPLICATE SMELL. NO FAULTS FOUND. REF AMM 71-00-01 AND AMM 49-10-00. RELEASED PER TECH SUPPORT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,855 hrs · 34,110 cycles

#3 EMERGENCY LIGHTING SYSTEM BATTERY WILL NOT ILLUMINATE EMERGENCY LIGHTS-C/A-REMOVED AND REPLACED #3 EMERGENCY LIGHTING SYSTEM BATTERY ASSY IAW ENVOY WC 33-700-19 OPS CHECK GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 19231

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,741 hrs · 34,001 cycles

CABIN EMERGENCY LIGHT ON AND OFF INTERMITTENTLY-C/A-RAR BATTERY POWER SUPPLY #4 IAW AMM 33-50-04. REMOVED AND REPLACED BATTERY #4 IAM AMM 33-50-04. REMOVED AND REPLACED INVERTER #6 IAW AMM 33-50-11 SYSTEM OPS CHECK GOOD IAW AMM 33-50-00. OK FOR SERVICE. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 104837; INVERTER P/N 7824-1

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,633 hrs · 33,896 cycles

ATA3350 EMERGENCY LIGHTS REMAINED ON HALF OF THE CABIN AND FLOOR.-C/A-UPON ARRIVAL ALL LIGHT S OFF SUSPECT LOW BATTERY #4 PERFOMED BATTERY CHARGE WITH APU PERFORMED OPS CHECKS IAW EMB 145 AMM 33-50-00 ALL CHECKS GOOD

Part: UNKNOWN — ODOR (CABIN) · airframe 37,848 hrs · 33,329 cycles

FA REPORTS STRONG ODOR IN CABIN-C/A-GROUND RUN FOR # 1 ENG, INSPECTED FOR LEAKS NO NOTED, RAN A/C AIR CONDITIONING SYSTEM NO ODORS NOTED IN CABIN. A/C GOOD FOR RETURN TO SERVICE IAW AMM 21-20-00. ALSO PERFORMED ETN-EM-72-034 FOR ODOR EVENT. NO ODOR NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,846 hrs · 33,327 cycles

EMERGENCY LIGHT FROM EXIT ROW AFT TURNING ON AND OFF INTERMITENTLY DURING FLIGHT-C/A-RAR EMERGENCY LIGHT BATTERY ASSY NO:3 IAW EMB 145 AMM 33-50-04

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 37,842 hrs · 33,322 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-UPON FUTHER INVESTIGATION FOUND SPLICE SP7376 TO BE BENT. REMOVED AND REPLACED SPLICE IAW EMB 145 SWPM 20-21-00. OPC GOOD.

Part: BRACKET — CHAFED (CARGO DOOR) · airframe 37,841 hrs · 33,321 cycles

CARGO DOOR LWR FWD CORNER BRACKET CHAFFE -C/A-REMOVED AND INSTALLED NEW CARGO DOOR LWR FWD PROFILE IAW EMB 145 SRM 51-40-02 AND 51-20-03.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,841 hrs · 33,321 cycles

CARGO DOOR CENTER CUTOUT FLOOR SILL CORRODED-C/A-REMOVED AND INSTALLED NEW SERVICEABLE CARGO DOOR CENTER SILL IAW EMB 145 SRM 51-40-02 AND 51-20-03.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 37,841 hrs · 33,321 cycles

FRAME 68 SHEAR CLIP AT CARGO DOOR CUTOUT CORRODED-C/A-REMOVED AND INSTALLED SERVICEABLE SECTION OF FRAME 68 SHEAR CLIP AT CARGO DOOR CUTOUT IAW EMB 145 SRM 53-31-04 ITEM 4 FIGURE 212.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 37,841 hrs · 33,321 cycles

FRAME 65 SHEAR CLIP AT CARGO DOOR CUTOUT CORRODED-C/A-REMOVED AND INSTALLED SERVICEABLE SECTION OF FRAME 65 SHEAR CLIP AT CARGO DOOR CUTOUT IAW EMB 145 SRM 53-31-04 ITEM 4 FIGURE 212.

Part: FRAME — CRACKED (FRAME 80) · airframe 37,841 hrs · 33,321 cycles

CRACK INDICATED FOUND ON FR 80 IN APU SHUNT AREA AROUND FASTENER HOLE-C/A-REPAIRED FRAME 80 I/A/W ENVOY ERS-EM-53MR-3938

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,841 hrs · 33,321 cycles

EMERGENCY FLOOR LIGHTS STRIPS #4, 5, AND ALL INTERNAL EMERGENCY EXIT ROW MARKERS IDENTIFIERS ARE INOP.-C/A-COMPLETE:REMOVED AND REPLACED #3 BATTERY AND BATTERY CHARGER ASSY IAW ENVOY W/C 33-700-19. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 37,841 hrs · 33,321 cycles

SEAT 12 EMERGENCY FLOOR PROXIMITY CONNECTOR IS BROKEN-C/A-COMPLETE:REPAIRED BROKEN EMERGENCY FLOOR PROXIMITY CONNECTOR IAW EMB 145 SWPM 20-21-00. EASI #102 S/N 5241. OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,841 hrs · 33,321 cycles

AFT FACING EMERGENCY EXIT SIGN AT OVERWING EMERGENCY EXIT IS INOP-C/A-COMPLETE:REMOVED AND REPLACED AFT FACING EMERGENCY EXIT SIGN AT OVERWING EMERGENCY EXIT IAW EMB 145 AMM 33-50-15. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,671 hrs · 33,183 cycles

12 B/C OVERHEAD EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED 12 B/C OVERWING EMERGENCY LAMP IAW AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. OPC GOOD. END.

Part: SIGN — INOPERATIVE (CABIN) · airframe 36,800 hrs · 32,395 cycles

DURING PS-1 CHECK, FOUND EXIT SIGN NEAR THE MAIN DOOR TO BE INOP. C/A-REMOVED AND REPLACED EXIT SIGN IAW AMM 33-50-14. OPS CHECK GOOD.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 36,516 hrs · 32,103 cycles

FO SIDE WINDOW SHATTERED. REMOVED AND REPLACED FO WINDSHIELD IAW AMM 56-10-01. LEAK CHECK GOOD. OPS CHECK OF W/S HEATING SYSTEM GOOD IAW EMB 145 AMM 30-42-00. OPS CHECK OF W/S WIPER SYS GOOD IAW AMM 30-41-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,156 hrs · 31,805 cycles

LH FWD OVER WING EMERGENCY LIGHT INOP-C/A-RAR LH FWD OVER WING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND EMB AMM 33-50-400-801-A. OPS CHECK GOOD. END.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 35,820 hrs · 31,430 cycles

DURING EMERGENCY LIGHT OPC FOUND EMERGENCY LIGHT FWD OF RH WING, SERVICE DOOR LIGHTING AND FLOOR EMERGENCY LIGHT STRIPS 1A-6A INOP.-C/A-TROUBLE SHOT. FOUND #2 EPSU INOP. REMOVED AND REPLACED #2 EMERGENCY LIGHT POWER SUPPLY AND CHARGER IAW ENVOY W/C 33-700-19. OPS CHECKS GOOD NO FURTHER DEFECTS NOTED. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 109939

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,809 hrs · 31,419 cycles

WHILE PERFORMING PS-1 CHECK FOUND SERVICE-DOOR EMERGENCY LIGHT OUT.-C/A-REMOVED AND REPLACED SERVICE-DOOR EMERGENCY LIGHT BULD IAW EMB 145 AMM TASK 33-50-09-000-801-A AND AMM TASK 33-50-09-400-801-A. OPS CHECK GOOD.

Part: WIRE HARNESS — MALFUNCTIONED · airframe 35,575 hrs · 31,198 cycles

ON TAKEOFF ROLL CAUTION MSG'S IC 1 WOW INOP, SPOILER FAIL, SPS ADVANCED, LG AIR/GND FAIL CAUTION AND FLT IDLE 1 STOP FAIL ADVISORY ON EICAS. PERFORMED HIGH SPEED ABORT @ APROX 110 KTS "TRANSFERRED TO NRWC 680-MIA-03210"-C/A REMOVED AND REPLACED LGEU IAW AMM 32-32-01 AND WOW AIR/GRD HARNESS IAW AMM 32-00-03-800-801A. PERFORMED OPS CHECK IAW AMM 32-32-01. OPS CHECK OK.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 34,552 hrs · 30,207 cycles

SPS ADVANCE CAUTION ON EICAS AFTER ROTATION RAN QRH PROCEDURE AND RETURN TO DEPARTURE. REMOVED AND REPLACED THE STALL PROTECTION COMPUTER, OPS CHECKED GOOD IAW AMM 27-36-02 & W/C 27-700-20.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,404 hrs · 30,066 cycles

RED ATT IN ISIS DURING FLIGHT. FOLLOWED FIM 34-01-00-810-801-A, FOUND TO BE IN A TRANSITORY CONDITION

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 33,465 hrs · 29,166 cycles

SPOILER FAIL MESSAGE IN FLIGHT. REMOVED AND REPLACED SCU IAW AMM 27-63-02, CLEANED AND CHECKED THE LT AND RT OTBD SPOILER PROXIMITY SENSORS IAW AMM 27-63-03, OPS CHECKED GOOD IAW AMM 27-63-01.

Part: DUCT — DETACHED (NR 1 ACM) · airframe 33,000 hrs · 28,714 cycles

NR 1 PACK VALVE CLOSES IN FLIGHT. REMOVED AND REPLACED THE NR 1 A/C PACK VALVE IAW AMM 21-51-01. PERFORMED AN OPS CHECK IAW AMM 21-60-00, OPS CHECKED FAILED DUE TO THE NR 1 PACK OVERHEAT. FOUND THE NR 1 A/C PACK ACM DUCT DETACHED. SECURED IAW AMM 21-20-00/21-51-00. OPS CHECKED GOOD.

Part: SUPPORT — CORRODED (FRAME 18) · airframe 32,992 hrs · 28,708 cycles

GALLEY RT OMEGA BEAM CORRODED AT FRAME 18. PERFORMED A DOUBLER REPAIR IAW ERS-EM-53MR-2878.

Part: SPAR — CRACKED (LT WING) · airframe 32,992 hrs · 28,708 cycles

PERFORM HFEC INSPECTION ON LT WING SPAR I LOWER FLANGES AT RIB NR 9 IAW NDTM CRACK NOTED AND MARKED. ACCOMPLISHED REPAIR TO LT WING SPAR I LOWER FLANGE AT RIB 9 IAW ERS-EM-57MR-843.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,992 hrs · 28,708 cycles

FR 65 IS CORRODED BELOW CARGO DOOR LOWER GUIDE. ACCOMPLISHED REPAIR TO FR 65 BTW STR 15L AND 18L BELOW CARGO DOOR LOWER GUIDE IAW ERS-EM-53MR-2867.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,677 hrs · 28,404 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROWS 1 - 7 ON FLOOR, 3AC BULKHEAD, SERVICE DOOR HINGE, AND RT FWD BELLY PANEL. REMOVED AND REPLACED ALL EMERGENCY LIGHT CHARGERS AND BATTERIES IAW 33-700-19. OPS CHECKED GOOD.

Part: STRIP — MISSING (EMERGENCY LIGHT) · airframe 32,677 hrs · 28,404 cycles

EMERGENCY LIGHT AT SEAT 3A MISSING FILLER STRIP. INSTALLED THE FILLER STRIP IAW AMM 33-50-12.

Part: LIGHT — DEBONDED (ROW 12) · airframe 32,677 hrs · 28,404 cycles

ROW 12 CEILING PANEL EMERGENCY LIGHT DISBONDED ON FWD SIDE. BONDED THE EMERGENCY LIGHT CELING PANEL IAW ETN-GN-20-023, AND AMM 25-00-00

Part: SKIN — CRACKED (LT WING) · airframe 28,150 hrs · 23,711 cycles

LEFT LOWER SKIN DAMAGED BY PANEL 5711 HINGE PANEL. LEFT LOWER SKIN DAMAGED BY PANEL 5711 HINGE PANEL.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 28,150 hrs · 23,711 cycles

CARGO DOOR SILL IS CORRODED. COMPLETED REPAIR TO CARGO DOOR SILL IAW ERS-EM-53MR-1094.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 28,150 hrs · 23,711 cycles

SERVICE DOOR LOWER HORIZONTAL BEAM IS CRACKED AT FWD INBD FLANGE. INSTALLED NEW SERVICE DOOR INNER LOWER HORIZONTAL BEAM IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 28,150 hrs · 23,711 cycles

LEFT GEAR WELL UPPER SUPPORT BRACKET FOR PANEL 155QZ IS CRACKED APPROX 1 1/2" LONG. R & R LT GEAR WELL UPPER SUPPORT BRACKET FOR PANEL 155QZ IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 28,150 hrs · 23,711 cycles

RIGHT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 3 IS CRACKED. REPAIRED RT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 3 IAW SRM 51-40-02 & ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 28,150 hrs · 23,711 cycles

RIGHT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 4 IS CRACKED. REPAIRED RT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 4 IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 28,150 hrs · 23,711 cycles

LEFT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 5 IS CRACKED. REMOVED & INSTALLED LT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 5 IAW SRM 51-40-02 & ETN-EM-53-142.

Part: FITTING — CRACKED (FUSELAGE) · airframe 28,150 hrs · 23,711 cycles

SHEAR CLIP ON FRAME 80 AT STRINGER 7 LT IS CRACKED. R & R SHEAR CLIP ON FRAME 80 TO 7L IAW SRM 51-40-02. LEAK CHECKED GOOD.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 28,150 hrs · 23,711 cycles

COCKPIT WINDSHIELD CUT OUT STRUCTURE HAS EVIDENCE OF 2 CRACKS. BOTH SIDES OF THE GRAB HANDLE NUTPLATES. REPAIRED AREAS IAW SRM CH 53-12-16.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 28,150 hrs · 23,711 cycles

LEFT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 1 HAS TWO CRACKS. REPAIRED LT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 1 FWD & AFT END IAW ETN- EM-53-142.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 28,150 hrs · 23,711 cycles

LEFT UPPER WING TO FUSELAGE LOWER ATTACH ANGLE NR 3 IS CRACKED. REPAIRED LT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 3 IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 28,150 hrs · 23,711 cycles

LEFT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 4 IS CRACKED. REPAIRED LT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 4 IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 28,150 hrs · 23,711 cycles

LEFT UPPER WING TO FUSELAGE FAIRING UPPER ATTACH ANGLE IS CRACKED BETWEEN FRAMES 48 - 49. REPAIRED LT UPPER WING TO FUSELAGE FAIRING UPPER ATTACH ANGLE IAW SRM 53-23-12 TYPE 2.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 28,150 hrs · 23,711 cycles

RIGHT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 5 IS CRACKED. RE-EVALUATED RT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 5 & FOUND NO DEFECTS.

Part: DOOR — DENTED (CABIN) · airframe 28,150 hrs · 23,711 cycles

ERS-EM-52DF-173 PTD THREE DENTS ON PAX DOOR. PERMANENT REPAIR. COMPLIED WITH PERMANENT REPAIR OF THREE DENTS ON PAX DOOR IAW ERS-EM-52DF-173 PTD.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 28,150 hrs · 23,711 cycles

LEFT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 2 IS CRACKED, 2" LONG. REPAIRED LT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 2 IAW ETN-EM-53-142 CHANGED ZONE TO ZONE 500.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 28,150 hrs · 23,711 cycles

LEFT UPPER WING TO FUSELAGE FAIRING UPPER ATTACH ANGLE IS CRACKED BETWEEN FRAMES 48 & 49. 2 & 1/2" LONG. REPAIRED LT UPPER WING TO FUSELAGE FAIRING UPPER ATTACH ANGLE IAW SRM 53-23-12 TYPE 2. CHANGED ZONE TO ZONE 200.

Part: WIRE — BROKEN (CABIN) · airframe 28,150 hrs · 23,711 cycles

CABIN AISLE FLOOR EMER LIGHT STRIP NR 3 WIRES BROKEN OFF. INSTALLED NEW NR 3 FLOOR EMER LIGHT STRIP IAW AMM 33-50-12.

Part: DUCT — CRACKED (BLEED AIR SYS) · airframe 28,150 hrs · 23,711 cycles

PNEUMATIC DUCT BETWEEN LT SIDE FUSELAGE BLEED AIR JOINT 9 & 11 IS CRACKED. R & R IAW AMM 36-11-09.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,150 hrs · 23,711 cycles

LEFT OMEGA BEAM IS CORRODED AT FRAME 29 CROSS MEMBER. REPAIRED LT OMEGA BEAM AT FRAME 29 IAW SRM 53-22-10. COMPLIED WITH D T CHECKLIST 15 - 27.

Part: STRIP — CRACKED (CABIN) · airframe 28,150 hrs · 23,711 cycles

CABIN AISLE EMER LIGHT STRIP NR 1 PLASTIC EXTRUSION IS CRACKED & BROKEN. R & R CABIN AISLE EMER LIGHT STRIP NR 1 PLASTIC EXTRUSION IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 28,150 hrs · 23,711 cycles

CABIN AISLE FLOOR EMER LIGHT STRIP NR 1 WIRES BROKEN OFF. R & R CABIN AISLE FLOOR EMER LIGHT STRIP NR 1 IAW AMM 33-50-12.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 28,150 hrs · 23,711 cycles

RIGHT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 3 IS CRACKED, 1/2" LONG. REPAIRED RT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 3 IAW SRM 51-40-02 & ETN-EM-53-142. CHANGED ZONE TO ZONE 600.

Part: WIRE — BROKEN (CABIN) · airframe 28,150 hrs · 23,711 cycles

CABIN AISLE FLOOR EMER LIGHT STRIP NR 5 WIRES BROKEN OFF. R & R CABIN AISLE FLOOR EMER LIGHT STRIP NR 5 IAW AMM 33-50-12.

Part: CROSSMEMBER — CORRODED (FUSELAGE) · airframe 28,150 hrs · 23,711 cycles

ALUMINUM CROSS MEMBER AT FRAME 20 IS CORRODED. REPAIRED ALUMINUM CROSS MEMBER AT FRAME 20 IAW ETN-EM-53-241.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 28,150 hrs · 23,711 cycles

RIGHT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 4 IS CRACKED, 1/2" LONG. REPAIRED RT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 4 IAW ETN-EM-53-142.

Part: UNKNOWN — MALFUNCTIONED (GUST LOCK) · airframe 27,694 hrs · 23,356 cycles

GUST LOCK AMBER INDICATION IN DESCENT, CB POPPED. DEFERRED IAW MEL 27-11 COMPLIED WITH MX ACTION. TROUBLE SHOT GUST LOCK CB, SUSPECT SHORT TO GND BETWEEN K0848 & ACTUATOR IAW WM 27-70-50. MEL REMAINS OPEN. R & R K1013 RELAY & K0848. OPERATIONS CHECKED BAD IAW AMM 20-13-02 & 27-70-00. MEL REMAINS OPEN.

Part: LIGHT — SMOKE (CABIN) · airframe 27,228 hrs · 22,946 cycles

WHEN READING LIGHT AT 3A WAS TURNED ON IT FLICKERED & STARTED TO SMELL OF SMOKE, IT WAS TURNED OFF & SMELL DISSIPATED. FLIGHT CREW PLACARDED IAW MEL 25-20. R & R SEAT 3A READING LIGHT ASSEMBLY IAW AMM 33-25-02, OPERATIONS CHECKED GOOD. MEL ITEM RESTORED M PROCEDURES COMPLIED WITH.

Part: WARNING SYSTEM — ACTIVATED (HYDRAULIC SYS) · airframe 26,848 hrs · 22,646 cycles

HYDRAULIC NR 1 SYS LOW CAUTION MSG. TRANSFERRED HYD FROM NR 2 TO NR 1 IAW ETN-EM-29-023. NO LEAKS NOTED ACFT OK FOR SERVICE

Part: STRAP — MALFUNCTIONED (NR 1 NAV UNIT) · airframe 26,672 hrs · 22,497 cycles

LOST ALL NAV'S ADF, VOR & LOC, DME, GLIDESLOPE CAPTAIN SIDE, DUE TO POWER SURGE AT INU RACK. SMELL OF ELEC BURN NOTICED. R & R NR 1 NAV UNIT STRAP BOARD IAW AMM 34-32-11. OPERATIONS CHECKED GOOD. SEE NRWC 680-DFW-01857 ACFT REMAINS COMPLIANT FOR CONTINUED CAT II OPERATION.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 25,758 hrs · 21,771 cycles

FLASHLIGHT BASE IN FWD CABIN BROKEN. R & R FLASHLIGHT ASSEMBLY IN FWD CABIN, OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 25,486 hrs · 21,566 cycles

DURING MX INSPECTION OF FLIGHT 3090 FOUND LOWER RETAINING CLIP ON CAPTAIN`S FLASHLIGHT HOLDER IS BROKEN. ACFT WAS REMOVED FROM SERVICE. R & R CAPTAIN’S FLASHLIGHT ASSEMBLY, OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,467 hrs · 21,549 cycles

AFT CEILING EMERGENCY LAMP INOPERATIVE. R & R AFT OVERHEAD AISLE EMERGENCY LIGHT LAMP IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.

Part: BALLAST — FAULTY (CABIN) · airframe 25,406 hrs · 21,484 cycles

BURNT RUBBER ODOR IN COCKPIT ON TAXI OUT. R & R CEILING BALLASTS AT SEAT 10A IAW EMB-145 AMM 33-21-05. OPERATIONS CHECKED GOOD, NO DEFECT NOTED.

Part: SWITCH — BROKEN (FLASHLIGHT) · airframe 24,953 hrs · 21,162 cycles

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

Part: FLASHLIGHT — MISINSTALLED (CABIN) · airframe 24,371 hrs · 20,669 cycles

F/A FLASHLIGHT NOT CHARGING. FOUND FLASHLIGHT TO BE INSTALLED IN CHARGER BACKWARDS, REMOVED AND REINSERTED FLASHLIGHT IN ITS PROPER ORIENTATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,244 hrs · 20,562 cycles

DURING MBV INSPECTION, FOUND REAR FUSELAGE SKIN HAS A CRACK APPROXIMATELY .2500 IN LONG AT FR 75, STR 2L. REPAIRED FUSELAGE SKIN IAW EO EM-53MR-2174.

Part: CROSSBEAM — CRACKED (NLG WW) · airframe 24,244 hrs · 20,562 cycles

DURING MBV INSPECTION, FOUND CROSSBEAM SUPPORT IN THE NOSE WHEELWELL CRACKED. R & R CROSSBEAM IAW SRM 51-40-02.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,234 hrs · 20,552 cycles

LEFT NR 2 FLOOR PROXIMITY LIGHT STRIP HAS A BROKEN WIRE. R & R LT NR 2 FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 24,234 hrs · 20,552 cycles

PAX DOOR INNER HANDLE HOUSING SUPPORT BRACKET CRACKED. REPAIRED PAX DOOR INNER HANDLE HOUSING SUPPORT ASSY IAW EO EM-52MR-250.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,234 hrs · 20,552 cycles

LT NR 6 FLOOR PROXIMITY LIGHT STRIP HAS A BROKEN WIRE. R & R LT NR 6 FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 24,234 hrs · 20,552 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. REPOSITIONED BULB IN SOCKET LIGHT WORKS FINE IAW AMM 33-50-10.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,105 hrs · 20,451 cycles

DURING MX INSPECTION, FOUND THE GALLEY EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R BULB FOR GALLEY EMERGENCY LIGHT PERFORMED OPS CHECKED IAW AMM 33-50-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,123 hrs · 19,690 cycles

DURING MAINTENANCE INSPECTION, FOUND THE FLOOR LEVEL EMERGENCY LIGHT STRIP AT ROW 15 INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENGY LIGHT STRIP EXTENDING FROM ROW 14 TO ROW 16 IAW AMM 33-50-12-000-801/33-50-12-400-801. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (CONTROL PANEL) · airframe 22,936 hrs · 19,530 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT SWITCH AT FLIGHT ATTENDANT PANEL NOT WORKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT PANEL IAW EMB145 AMM 25-27-09. ALL OPERATIONAL CHECKS WERE GOOD IAW EMB145 AMM 33-50-00-700-801A, 33-25-00-700-801A, 33-21-00-700-801A, AND 21-60-00-700-801A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — FAILED (AC PACK) · airframe 22,557 hrs · 19,237 cycles

ON FLIGHT 3584 THE CREW REPORTED PRESSURIZATION FAIL. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MIA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 PACK OVERPRESSURE SWITCH IAW AMM 21-51-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CLAMP — LOOSE (AC BAY)

WING ANTI ICE FAIL WARNING /TROUBLESHOT FAULT IAW EMB-FIM 30-11-00-810-801-A. UPON FURTHER INVESTIGATION FOUND LEFT DUAL HEAT EXCHANGE DUCT'S CLAMPS LOOSE. RE-SECURED DUCT AND CLAMPS IAW AMM 21-51-02. OPER TEST GOOD. NO DEFECT NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,399 hrs · 19,111 cycles

ON FLIGHT 4325 THE CREW REPORTED THE FLOOR EMERGENCY LIGHTING REAR AND EXIT ROWS EMERGENCY LIGHT NOT WORKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY POWER SUPPLY IAW 33-50-64 SYSTEM CHECK NORMAL. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,911 hrs · 18,755 cycles

DURING B INSPECTION FOUND THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EXTERNAL OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 21,911 hrs · 18,755 cycles

DURING B INSPECTION FOUND THE AFT CABIN EMERGENCY FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT CRADLE IAW EMB AMM TASKS 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,624 hrs · 18,527 cycles

DURING B INSPECTION, FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS ON PSU PANEL INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY ASSEMBLY AND CHARGER ASSEMBLY IAW W/C 33-700-19. OPS CHECKED GOOD IAW AE W/C 33-700-17. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 21,625 hrs · 18,528 cycles

FLIGHT 4264, CREW REPORTED THAT CLIMBING-OUT OF 27,600 FL CABIN PRESSURE WAS LOWER THAN CHART ON 21-24. INCREASED TO STAY ON CHART. AT 3000FL CABIN ALT LOST. INITIATED AN EMERGENCY DESCENT, DECLARED AN EMERGENCY AND COMPLIED WITH AOM VOL 1 CHECKLIST AND DIVERTED TO DEPARTURE. LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT IAW FIM 21-31-00, HAD DIFFICULTY WITH THE MANUAL CONTROLLER. REMOVED AND REPLACED THE MANUAL CONTROLLER IAW AMM 21-31-02. OPS CHECKED GOOD. NO FURTHER FAULTS FOUND. DISCREPANCY CLEARED. OUTFLOW VALVES CHECKED GOOD IAW AMM 21-31-00. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,177 hrs · 18,179 cycles

DURING B INSPECTION FOUND THE LEFT OVERHEAD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY LIGHT LAMP IAW EMB 145 AMM TASK 33-50-09-000-801-A AND TASK 33-50-09-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,305 hrs · 17,495 cycles

DURING B-INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT IS NOT WORKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT BULB IAW EMBRAER AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,295 hrs · 17,488 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,183 hrs · 17,407 cycles

DURING MTX INSPECTION FOUND FLIGHT ATTENDANT FLASHLIGHT INOPERABLE BRACKET BROKEN. 3176883 MEL 25-53. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT HOLDER OPERATIONAL WAS CHECK GOOD IAW 33-50-16. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 20,176 hrs · 17,403 cycles

ON FLIGHT 3126 THE CREW FOUND FLIGHT ATTENDANTS FLASHLIGHT BRACKET BROKEN. DEFERRED PER MEL 25-53. AUTH TRAINS TO MIC SHEET/(M) PROCEDURE C/W. MEL STILL OPEN. CORRECTIVE ACTION IS PENDING.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 19,861 hrs · 17,155 cycles

ON FLIGHT 2796 THE CREW REPORTED THE F/A REAR FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,843 hrs · 13,276 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DEFECTIVE POWER SUPPLY AND CHARGER AND REPLACED WITH SERVICEABLE UNITS IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 14,843 hrs · 13,276 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY EXIT SIGN AT ROW 12 ON THE CEILING PANEL INOPERABLE ON THE FORWARD SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DEFECTIVE INVERTER AND REPLACED WITH A SERVICEABLE ONE IAW EMB 145 AMM 30-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,843 hrs · 13,276 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE TOILET WASTE DRAIN VALVE SUPPORT CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE TOILET WASTE DRAIN VALVE SUPPORT IAW EMB 145 SRM 51-40-02, 51-20-03, 51-40-04, 51-40-06, AND 51-20-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 12,118 hrs · 11,083 cycles

ON FLIGHT 4019, CREW REPORTED ON CLIMB-OUT A BURNING CAMPFIRE ODOR, NO ODOR IN COCKPIT.

Part: SILL — CORRODED (FUSELAGE) · airframe 9,926 hrs · 9,184 cycles

DURING A MBV INSPECTION, THE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. REMOVED THE EXISTING SILL TO REMOVE THE DAMAGED AND CLEANED THE AREA. POSITIONED NEW SILL, MARK AND DRILLED FASTENERS HOLES. TREATED PART AND INSTALLED. REPAIR DONE IAW EMBRAER 145 SRM, EMB-145/1142 REV 39, CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 9,594 hrs · 8,895 cycles

ON FLIGHT 9804, CREW REPORTED DURING PREFLIGHT DUTIES THE F/A FOUND THE FLOOR PROXIMITY LIGHTS FROM ROW 7 THRU 12 INOP. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 3 BATTERY EMERGENCY BATTERY PACK IAW AMM 33-50-11. OPERATIONAL CHECKED GOOD. ALSO, REPLACED NR 5 INVERTER IAW AMM 30-50-11. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FUEL SYS — LEAKING (WING) · airframe 7,179 hrs · 6,579 cycles

FOUND FUEL STREAMING FROM WING ON CLIMB-OUT.

Part: BEAM — CORRODED (FUSELAGE)

THE LEFT OMEGA BEAM AT FRAME 20 CORRODED. REMOVED THE CORRODED AREA BY PERFORMING A CUTOUT. FABRICATED 2 SHIMS, PLATE, FILLER AND DOUBLER FOR REPAIR. REPAIR DONE IAW EMB145 SRM 145/1142 REV 33 53-00-10 FIG 1 AND STANDARD SRM PRACTICES. AIRCRAFT RETURNED TO SERVICE. (M)