N923AE

Part: UNKNOWN — ODOR (CABIN) · airframe 44,693 hrs · 40,194 cycles

SMELL OF BURNING RUBBER AROUND 18K. RAN ENGINES W APU ON AIR GROUNDS OPEN HYDRAULICS AND PACKS RUNNING INSPECTED MAIN BATT 1,2 & BACKUP RELAY BOX. INSPECTED RIGHT & LEFT HAND RELAY SUPPORT AND RIGHT & LEFT POWER CONTROL DIST BOXES INSPECTED BOTH PACK 1 & 2 NO SMELL OF BURNING RUBBER. A/C OK FOR SERVICE

Part: CONTACTOR — BURNED (BUSS) · airframe 44,822 hrs · 40,118 cycles

FA REPORTS ELECTRICAL BURNING SMEILL FOR 10MIN IN FWD CABIN DURING APPROACH STARTING AT 8000FT, PREV HISTORY FOR FUMES WITH BURNED CONTACTOR SUPPORT IN LH DIST BUSS. INSPECTED FWD CABIN AREA FOR ANY SIGNS OF ELEC DAMAGE, NONE FOUND. INSPECTED LT & RT ELECTRICAL DIS BUSS. NO DEFECTS NOTED. INSP LT DIST BUSS FOR DAMAGE AROUND PREVIOUS OVERHEAT DAMAGE AREA REF EO1-24-25-0176. DAMAGE HAS NOT INCREASED. CLEANED PANLE WITH CONTACT CLEANER. REF LP 348825-1 FOR BROKEN RH DIST VENTILATION VENT. CONT ON LP348825-2. RAN PACKS & ELECTRICAL SYSTEMS. NO FUMES NOTED. A/C OK FOR SERVICE.

Part: CONTROLLER — ABNORMAL (ZONE 200) · airframe 44,404 hrs · 39,863 cycles

WINDSHIELD HEAT #2 FAILED IN FLIGHT, CMC MESSAGE W/S HEATING INOP, MOMENTARY IN ICING. R+R WINDSHIELD HEAT TEMP CONTROLLER IAW 30-42-01. PERFORMED OPS CHECK IAW AMM 30-42-00. OPS CHECK GOOD. AC OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — ODOR (CABIN)

AFTER POSSIBLE LIGHTNING STRIKE SMELLED FAINT BURNING SMELL THAT DISSIPATED.

Part: UNKNOWN — ODOR (CABIN)

AFTER POSSIBLE LIGHTNING STRIKE SMELLED FAINT BURNING SMELL THAT DISIPATED.

Part: UNKNOWN — SMOKE (ZONE 200) · airframe 43,864 hrs · 39,264 cycles

AFTER E-1 START, SMOKE IN FLIGHT DECK AND CABIN. PULLED BOTH "T" HANDLES,(DID NOT BLOW BOTTLES), AND EVACUATED THROUGH PAX DOOR AND GALLEY DOOR. NO ABNORMAL ENGINE INDICATIONS. FACT 24JAN25 02:57 CLT REMOVED PACK 1 ACM REF AMM 21-51-03 (SS) FACT 24JAN25 02:57 CLT INSTALLED PACK 1 ACM AND R+R HEAT EXCHANGER IAW AMM 21-51-02 AND 21-51-03 23JAN25 15:41 CLT C/W FIM TASK 21-20-00-810-801-A STEPS 1-8. FOUND PACK 1 ACM SEIZED WITH BLADE FAILURE. PERFORMED ENGINE RUN IAW MX OPS MANUAL. OPERATED PACK 1 ON SEPARATE BLEED SOURCES (ENG & APU) WITH NO DEFECTS NOTED. ALL EMERGENCY EXITS PERFORMED AS DESIGNED

Part: SENSOR — FAULTED (FLAP SYS) · airframe 43,787 hrs · 39,183 cycles

REJECTED TAKE OFF AT 50 KNOTS DUE TO SPS ADVANCED AND FLAP LOW SPEED ON EICAS. FOUND "FLAP FEEDBACK POS FAIL" ON CMC. R&R FPTU IAW AMM 27-53-05. OPS CHECK GOOD. ALSO INSPECTED CANON PLUGS ON FECU, FPTU, AND FLAP SELECTOR LEVER. NO DEFECTS NOTED AT THIS TIME

Part: ANTI-ICE VALVE — FAULTED (NR 2 ENGINE) · airframe 42,417 hrs · 37,654 cycles

ON T/O ROLL AT 60 KNTS ICE COND-A/I INOP, NO T/O CONFIG AND E2 A/ICE FAIL DISPLAYED. E2 A/ICE FAIL REMAINS DISPLAYED. FACT 08MAY24 19:00 TRI PERFORMED A/ICE VALVES OPS CHECK IAW AMM 30-00-00-00-700-803-A. OPS CHECK GOOD. CONFIGURED A/C IN TAKEOFF CONFIGURATION AND TESTED T/O CONFIG BUTTON WITH NO DEFECTS NOTED. TAXI AICRAFT TO 40KNTS WITH NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 42,417 hrs · 37,654 cycles

FUEL LIKE SMELL AROUND ROW 12 FACT 08MAY24 23:55 CLT INSPECTED PACK SYSTEMS AND FUEL SYS AT WING STUB. NO LEAKS FOUND. TAXI'D A/C. PERFORMED 4 HIGH PWR RUNS, NO SMELLS OR FUMES NOTED AT ANY POINT. A/C OKAY FOR SERVICE AT THIS TIME.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 42,169 hrs · 37,376 cycles

E022752 NLG WHEEL WELL RH BULKHEAD CRACKED INSIDE NOSE HYDRAULIC COMPARTMENT, AT AFT UPPER END OF BULKHEAD. PERFORMED REPAIR ON NLG WHEEL WELL R/H BULKHEAD INSIDE NOSE HYDRAULIC COMPARTMENT AT AFT UPPER END OF BULKHEAD IAW ETD2024-145-004757 AND PIEDMONT EO1-53-24-0141

Part: RIB — CRACKED (RT WING) · airframe 42,169 hrs · 37,376 cycles

E017252 POSSIBLE CRACKS ON RH WING RIB 21. FABRICATED AND DRILLED DOUBLER, FILLER, AND SHIM AND INSTALLED REPAIR OF R/H WING RIB 21 IAW EMB 145 SRM 57-50-07 ITEM 4 FIG 203 AND EO1-57-24-0130

Part: BEARING RACE — CORRODED (NLG TRUNNION) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E021954 NLG LEG RH TRUNNION BEARING RACE PITTED. REMOVED AND REPLACED NLG RH TRUNNION IAW EMB SRM 51-40-02

Part: SKIN — DAMAGED (FRM 14 S20-21R) · airframe 42,169 hrs · 37,376 cycles

E020842 BURN MARK ON SKIN AT FR14 BETWEEN STRINGERS 20R - 21R. REPAIRED BURN MARK ON EXTERNAL SKIN AT FR14 BETWEEN STRINGERS 20R-21R IAW EMBRAER ETD2024-145-004117 AND EO1-53-24-0128

Part: SKIN — DAMAGED (FRM 22 S18-19R) · airframe 42,169 hrs · 37,376 cycles

E020841 BURN MARK ON FR22 BETWEEN STRINGERS 18R - 19R. PERFORMED THE CUT OUT OF THE DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER ON BURN MARK AT FR 22 BETWEEN STR 18R-19R IAW EMBRAER ETD2024-145-004115 AND EO1-53-24-0138

Part: SKIN — DAMAGED (FRM 26 S18-19R) · airframe 42,169 hrs · 37,376 cycles

E020843 BURN MARK ON FR26 BETWEEN STRINGERS 18R - 19R. REPAIRED BURN MARK AT FR26 BETWEEN STRINGERS 18R - 19R IAW EMB ETD2024-145-003973 REV. A AND EO1-53-24-0127

Part: FLOOR SUPPORT — CORRODED (NR 1) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020482 RH OUTBD FLOOR SILL #1 HAS CORROSION. REMOVED AND REPLACED WITH SERVICEABLE RH OUTBD FLOOR SILL #1 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRMS 45-50) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020497 LH OMEGA BEAM HAS CORROSION BETWEEN FRAMES 45-50. PERFORMED REAPIRS TO LH OMEGA BEAM HAS CORROSION BETWEEN FRAMES 45-50 IAW ETD2024-145-003653 AND EO1-53-24-0137

Part: DOOR SILL — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020578 SERVICE DOOR CENTER SILL CORRODED AROUND NUT PLATE HOLES. BLENDED OUT CORROSION ON SERVICE DOOR CENTER SILL AROUND NUTPLATE HOLES, FOUND THE AFT NUPLATE HOLE TO BE WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 53-21-02-AD, AND THE FWD AND CENTER NUTPLATE HOLES FOUND TO BE OUT OF LIMITS, PERFORMED REPAIRS IAW EMB-145 SRM 53-21-02 RE, ITEM 2, FIGURE 201 AND PDT EO1-53-24-0129

Part: SUPPORT PLATE — DAMAGED (AFT BULKHEAD) · airframe 42,169 hrs · 37,376 cycles

E020609 PILOT SIDE AFT BULKHEAD OTBD GUIDE PIN HOLE SUPPORT PLATE ELONGATED. FABRICATED, DRILLED UP REPAIR DOUBLER AND SACRIFICIAL PLATE TO FIT AND INSTALLED PILOTS SIDE AFT BULKHEAD OUTBD GUIDE PIN HOLE ELONGATED IAW EMB 145 SRM 53-21-02-RE, ITEM 4, FIG 204 AND EO1-53-24-0125

Part: FLOOR SUPPORT — CORRODED (NR 5) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020481 LH OUTBD FLOOR SILL #5 HAS CORROSION. REMOVED AND REPLACED LH OUTBD FLOOR SILL #5 IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (AFT SERVICE DOOR) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020579 AFT SERVICE DOOR SILL CORRODED AROUND NUT PLATE HOLE. REMOVED AND REPLACED WITH NEW SERVICEABLE AFT SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (NR 4) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020480 LH OUTBD FLOOR SILL #4 HAS CORROSION. REMOVED AND REPLACED WITH SERVICEABLE LH OUTBD FLOOR SILL #4 IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (NR 2) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020478 LH OUTBD FLOOR SILL #2 HAS CORROSION. REMOVED AND REPLACED LH OUTBD FLOOR SILL #2 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRM 40) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020508 LH CENTER FLOOR SILL HAS CORROSION AT FRAME 40. RAR LH CENTER FLOOR SILL AT FRAME 40 IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (NR 5) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020513 LH UPPER SEAT TRACK #5 IS CORRODED. RAR LH UPPER SEAT TRACK #5 IAW EMB 145 AMM 53-01-06.

Part: SEAT TRACK — CORRODED (NR 3) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020488 RH UPPER SEAT TRACK #3 IS GOUGED AND CORRODED. RAR RH UPPER SEAT TRACK #3 IAW EMB 145 AMM 53-01-06

Part: FLOOR SUPPORT — CORRODED (FRM 49) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020502 LH CENTER FLOOR SILL IS CORRODED AT FRAME 49. REMOVED AND INSTALLED LH CENTER FLOOR SILL AT FRAME 49. IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FRM 62 S19-20R) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020549 SHEAR CLIP AT FR 62 BETWEEN STGR19R / 20R CORRODED. RAR SHEAR CLIP AT FR 62 BETWEEN STGR19R / 20R IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (FRMS 30-33) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020486 RH CENTER FLOOR SILL HAS CORROSION BETWEEN FRAMES 30-33. : RAR R/H CENTER FLOOR SILL BETWEEN FRAMES 30-33 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRM 38) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020510 LH CENTER FLOOR SILL HAS CORROSION AT FRAME 38. RAR L/H CENTER FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (FRM 24) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020483 LH CENTER FLOOR SILL HAS CORROSION AT FRAME 24. REMOVED AND INSTALLED SERVICEABLE LH CENTER FLOOR SILL AT FRAME 24 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (NR 6) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020471 RH FLOOR SILL #6 CORRODED ON MULTIPLE AREAS. REMOVED AND INSTALLED SERVICEABLE RH FLOOR SILL #6 IAW EMB 145 SRM 51-40-02,

Part: FLOOR SUPPORT — CORRODED (NR 3) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020479 LH OUTBD FLOOR SILL #3 HAS CORROSION. REMOVED AND REPLACED LH OUTBD FLOOR SILL #3 IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (NR 4) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020512 LH UPPER SEAT TRACK #4 IS CORRODED. RAR NEW LH UPPER SEAT TRACK #4 IAW EMB 145 AMM 53-01-06.

Part: MOUNT — CORRODED (APU CONTAINMENT) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020403 RH LOWER APU COWLING MOUNT FITTING IS CORRODED, INSIDE 312AR AT FWD SIDE OF FIREWALL. REMOVED AND REPLACED RH LOWER APU COWLING MOUNT FITTING IN IAW EMB 145 SRM 51-40-02.

Part: FRAME — GOUGED (FRM 65 S11-16L) · airframe 42,169 hrs · 37,376 cycles

E020365 Z FRAME NUT PLATE HOLES GOUGED AT FR 65 BETWEEN STRGS 16L-11L. REMOVED AND REPLACED Z FRAME AT FR65 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (FRMS 71-73) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020342 CARGO RH FLOOR BOARD SUPPORT BETWEEN FR 71 / 73 CORRODED. RAR CARGO RH FLOOR BOARD SUPPORT BETWEEN FR 71 / 73 IAW EMB 145 SRM 51-40-02

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 42,169 hrs · 37,376 cycles

E020332 CARGO DOOR CUT-OUT CENTER SILL CORRODED IN NUMEROUS AREAS REMOVED AND REPLACED WITH SERVICEABLE CARGO DOOR CUT-OUT CENTER SILL IAW EMB 145 SRM 51-40-02

Part: FRAME — GOUGED (CARGO DOOR) · airframe 42,169 hrs · 37,376 cycles

E020167 BAGGAGE DOOR AFT LATERAL FRAME IS GOUGE AROUND NUTPLATE HOLE. PERFORMED CUTOUT ON BAGGAGE DOOR AFT LATERAL FRAME TO REMOVE DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW EMBRAER ETD2024-145-003957 AND EO1-52-24-0139

Part: WEB — CRACKED (CARGO DOOR) · airframe 42,169 hrs · 37,376 cycles

E020163 BAGGAGE DOOR INTERNAL LWR WEB HAS A HOLE AT HB4 BETWEEN VB3 AND VB4. REMOVED DAMAGED & REPLACED WITH NEW & SERVICEABLE BAGGAGE DOOR INTERNAL LWR WEB (SKIN) IAW EMB-145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,020 hrs · 37,230 cycles

SERVICE DOOR EMERGENCY LT INOP-C/A-RAR SERVICE DOOR EMERGENCY LT IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. END.

Part: LAMP — INOPERATIVE (SD) · airframe 41,870 hrs · 37,090 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR ERMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,656 hrs · 36,882 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. R & R SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECK GOOD. END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,611 hrs · 36,840 cycles

AFT AISLE CEILING EMERGENCY LIGHT INOPERATIVE. -R & R AFT AISLE CEILING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,486 hrs · 36,713 cycles

EMERGENCY FLASHLIGHT ABOVE F/A SEAT IS NOT CHARGING AND IS DIM.-C/A-RAR EMERGENCY FLASHLIGHT ASSY ABOVE F/A SEAT IAW EMB 145 AMM 33-50-16.

Part: FLASHLIGHT — UNSERVICEABLE (F/A) · airframe 41,486 hrs · 36,713 cycles

EMERGENCY FLASHLIGHT ABOVE F/A SEAT IS NOT CHARGING AND IS DIM.-C/A-RAR EMERGENCY FLASHLIGHT ASSY ABOVE F/A SEAT IAW EMB 145 AMM 33-50-16.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,367 hrs · 36,582 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECK GOOD. END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,850 hrs · 35,972 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.

Part: FLAG — FAILED (LH RH) · airframe 40,756 hrs · 35,858 cycles

FLAP FAIL AFTER TAKEOFF FLAPS STUCK AT 9 COMPLIED WITH QRH-C/A-TS PER FIM 27-51-00 FOUND TO BE TRANSITORY CONDITION. PERFORMED OPS CHECK THROUGH 3 FAULT FREE CYCLES REF. AMM 27-50-00. OPS CHECK GOOD AC GOOD FOR SERVICE

Part: LAMP — INOPERATIVE (SD) · airframe 40,672 hrs · 35,759 cycles

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

Part: NONE — BROKEN (FA) · airframe 40,515 hrs · 35,587 cycles

SUPPLEMENTAL C/A FOR FA EMERGENCY FLASHLIGHT CHARGER UPPER BRACKET CLAMP BROKEN--C/A-RAR FA EMERGENCY FLASHLIGHT CHARGER UPPER BRACKET CLAMP IAW EMB AMM 33-50-16. MEL ITEM RESTORED.

Part: NONE — NONE · airframe 40,189 hrs · 35,211 cycles

EXTERIOR OVERWING L/H EMERGENCY LIGHT DOES NOT ILLUMINATE.-C/A-REMOVED AND REPLACED #4 BATTERY AND CHARGING ASSEMBLY IAW AMM 33-50-04. OPERATIONAL CHECK GOOD.

Part: NONE — NONE · airframe 40,138 hrs · 35,157 cycles

BOTH OVER WING EMERGENCY LIGHTS ARE INOP-C/A-FOUND PROBLEM TO BE BATTERY POWER SUPPLY REPLACED WITH NEW UNIT IAW AMM 35-50-04 OPS CHECK GOOD

Part: NOT REPORTED — NOT REPORTED · airframe 40,086 hrs · 35,095 cycles

LH AFT OVERWING EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR #4 EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK IAW AMM 33-50-04. OPC GOOD.

Part: NONE — NONE · airframe 40,048 hrs · 35,060 cycles

BOTH EXTERIOR AFT OVERWING EMEERGENCY EXIT LIGHTS INOP-C/A-RAR EMERGENCY LIGHT BATTERY SUPPLY AND BATTERY PACK NO.4 IAW EMB 145 AMM 33-50-04. OPC GOOD.

Part: NONE — NONE · airframe 39,816 hrs · 34,794 cycles

CABIN DPRESSURIZED SLOWLY IN AUTO. EMERGENCY DECLARED. #2 RH OUTFLOW VALVE REQUIRES REPLACMENT, FOUND LEAKING DURING PRESSURIZATION CHECK-C/A-REMOVED AND REPLACED RH OUTFLOW VALVE IAW EMB 145 AMM 21-31-04. OPS CHECK GOOD

Part: NONE — NONE · airframe 39,778 hrs · 34,744 cycles

REF. ITEM #2 OF THIS LOG PAGE EMERGENCEY LIGHTS OVERWINGED LH AND RH INOP-C/A-REMOVED AND REPLACE BATTERY POWER SUPPLY #4 IAW AMM 33-50-04 OPS CHECK GOOD

Part: NONE — NONE · airframe 39,778 hrs · 34,744 cycles

OVERWINGED EMERGENCEY LIGHTS ON LH AND RH ARE INOP-C/A-REMOVED AND REPLACED BATTERY PACK #4 IAW AMM 33-50-04 OPS CHECK GOOD

Part: NONE — NONE · airframe 39,694 hrs · 34,641 cycles

LH AND RH OVERWING EMERGENCY LIGHTS INOP-C/A-RAR #4 EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPC GOOD

Part: NONE — NONE · airframe 39,662 hrs · 34,607 cycles

LH AND RH OVERWING EMERGENCY LIGHTS INOP-C/A-RAR #4 EMERGENCY LIGHTING BATTERY AND CHARGER ASSY IAW ENVOY WC 33-700-19. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: NONE — NONE · airframe 39,641 hrs · 34,582 cycles

SERVICE DOOR EMERGENCY LIGHT NOT ILLUMINATING-C/A-REMOVED AND REPLACED EMERGENCY LIGHT LAMP ON SERVICE DOOR, OPERATIONAL CHECKED GOOD IAW EMB 145 AMM CH 33-50-09

Part: NONE — NONE · airframe 39,641 hrs · 34,582 cycles

CENTER ISLE EMERGENCY LIGHT NEXT TO LAV ,NOT ILLUMINATING-C/A-REMOVED AND REPLACED EMERGENCY LIGHT LAMP IN CENTER ISLE NEXT TO LAV, OPERATIONAL CHECKED GOOD IAW EMB 145 AMM CH 33-50-08

Part: NONE — NONE · airframe 39,454 hrs · 34,355 cycles

LH AND RH AFT EXTERIOR EMERGENCY LIGHTS INOP-C/A-#4 EMERGENCY BATTERY AND CHARGER RAR IAW EMB 145 AMM 33-50-04. OPS CHK GOOD.

Part: NONE — NONE · airframe 39,383 hrs · 34,285 cycles

RH EXTERIOR AFT EMERGENCY EXIT LIGHT INOP-C/A-RAR RH EXTERIOR AFT EMERGENCY EXIT LIGHT LAMP IAW EMB145 AMM 33-50-10. OPS CHECK GOOD

Part: NONE — NONE · airframe 39,324 hrs · 34,219 cycles

FLOOR PROXIMITY STRIP #2 AND #3 INOP-C/A-RAR #2 EMERGENCY BATTERY AND CHARGER IAW ENVOY W/C 33-700-19. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,190 hrs · 34,070 cycles

SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EXTERIOR EMERGENCY LIGHT LAMP IN REFERENCE WITH EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. END.

Part: RETAINER — BROKEN (FWD FLASHLIGHT) · airframe 39,034 hrs · 33,888 cycles

FOUND FWD CABIN EMERGENCY FLASHLIGHT CLIP BROKEN-C/A-REMOVED AND REPLACED FWD CABIN EMERGENCY FLASHLIGHT ASSY PER AMM 33-50-16

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,878 hrs · 33,709 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,667 hrs · 33,495 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IN REFERENCE WITH EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 38,632 hrs · 33,456 cycles

MAIN CABIN DOOR HARD TO OPEN.-C/A-LUBED MAIN DOOR ROLLERS AND HANDLE, DOOR OPEN AND CLOSED OK AFTER REF AMM 52-10-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,318 hrs · 33,114 cycles

EMERGENCY LIGHT ON HINGE OF SERVICE DOOR INOP-C/A-RAR EMERGENCY LIGHT LAMP ON HINGE OF SERVICE DOOR IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: SHEAR TIE — CORRODED (CRGO DOOR FRAME) · airframe 38,258 hrs · 33,059 cycles

CARGO DOOR CUTOUT SHEAR CLIP CORRODED IN PREVIOUS BLENDED (BLUE PAINT) AREA AT FR 68 JUST ABOVE CARGO DOOR SILL.CORROSION LEVEL 1-C/A-PERFORMED PERMANENT REPAIR TO FR 68 SHEAR CLIP JUST ABOVE CARGO DOOR SILL IAW EMB 145 SRM 53-21-04-RE ITEM 4.

Part: STRUCTURE — CORRODED (LAVATORY) · corrosion level 2 · airframe 38,258 hrs · 33,059 cycles

THE LAV BUCKET HAS EVIDENCE OF CORROSION UNDER THE LOCK HANDLE AND AT THE LANYARD ATTACHMENT. CORROSION LEVEL 2-C/A-REMOVED AND REPLACED LAV BUCKET IAW EMB 145 SRM 51-40-02.

Part: RIB — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 38,258 hrs · 33,059 cycles

FRAME 65 LOWER CLOSE OUT RIB CORRODED FWD OF CARGO DOOR CUT OUT.CORROSION LEVEL 2-C/A-REMOVED AND REPLACED FRAME 65 LOWER CLOSE OUT RIB FWD OF CARGO DOOR CUT OUT IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 38,258 hrs · 33,059 cycles

FRAME 65 SHEAR CLIP CORRODED BETWEEN STR 16L AND 17L.CORROSION LEVEL 1-C/A-REMOVED AND REPLACED FRAME 65 SHEAR CLIP BETWEEN STR 16L AND 17L IAW EMB 145 SRM 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,258 hrs · 33,059 cycles

FRAME 65 CORRODED BETWEEN STR 16L AND 17L.CORROSION LEVEL 1-C/A-REMOVED AND REPLACED LH FRAME 65 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 38,258 hrs · 33,059 cycles

LAVATORY RH OMEGA BEAM HAS CORROSION AT AFT NUT PLATE HOLE. CORROSION LEVEL 2-C/A-PERFORMED PERMANENT REPAIR TO LAV RH OMEGA BEAM AT AFT NUTPLATE HOLE IAW ERS-EM-53MR-4283.

Part: DOOR FRAME — CORRODED (FRAME 20) · corrosion level 2 · airframe 38,258 hrs · 33,059 cycles

NUTPLATE HOLE AT SERVICE DOOR CUT OUT, FRAME 20, BTW STGR 15R-16R CORRODED.CORROSION LEVEL 2-C/A-PERFORMED PERMANENT REPAIR TO NUT PLATE HOLE AT SERVICE DOOR CUT OUT FRAME 20 BTW STGR 15R-16R IAW ERS-EM-53MR-4287.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 38,258 hrs · 33,059 cycles

THE SERVICE DOOR FORWARD SILL IS CORRODED.CORROSION LEVEL 2-C/A-INSTALLED SERVICEABLE REPAIR DOUBLER IAW EMB145 SRM 53-21-10 ITEM 4 FIG 203 SHEET 1, 51-40-02.

Part: SUPPORT — CRACKED (CABIN LEFT) · airframe 38,258 hrs · 33,059 cycles

CABIN LH OMEGA BEAM OTBD SUPPORT IS CRACKED AT FR 47 1 CRACK , .240" ,LENGTH-C/A-PERFORMED PERMANENT REPAIR TO LH OMEGA BEAM OTBD SUPPORT IAW EMB 145 SRM 53-23-02-RE.

Part: SUPPORT — CRACKED (CABIN RIGHT) · airframe 38,258 hrs · 33,059 cycles

CABIN RH OMEGA BEAM OTBD SUPPORT IS CRACKED AT FR 47. 1 CRACK , LENGTH .240-C/A-PERFORMED PERMANENT REPAIR TO RH OMEGA BEAM OTBD SUPPORT IAW EMB 145 SRM 53-23-02-RE.

Part: SUPPORT — CRACKED (CABIN) · airframe 38,258 hrs · 33,059 cycles

CABIN RH OMEGA BEAM INBD SUPPORT IS CRACKED AT FR 47.1 CRACK , LENGTH .240"-C/A-PERFORMED PERMANENT REPAIR TO RH OMEGA BEAM INBD SUPPORT IAW EMB 145 SRM 53-23-02-RE.

Part: DOOR SILL — CORRODED (CARGO DOOR) · airframe 38,258 hrs · 33,059 cycles

CARGO DOOR LOWER SILL HAS NUMEROUS (PREVIOUSLY REPAIRED) SPOTS OF CORROSION. CORROSION LEVEL 1-C/A-REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW EMB 145 SRM 51-40-02.

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 38,258 hrs · 33,059 cycles

CARGO DOOR UPPER EDGE INBD ANGLE HAS 2 NUT PLATE HOLES (PREVIOUS REPAIRS) THAT ARE CORRODED. .CORROSION LEVEL 1-C/A-REMOVED AND REPLACED CARGO DOOR UPPER EDGE ANGLE IAW EMB 145 SRM 51-40-02.

Part: SKIN — PUNCTURED (RUDDER) · airframe 38,258 hrs · 33,059 cycles

RUDDER 2 PUNCTURED 1" ABOVE LOWER EDGE 2" FROM TRAILING EDGE ON LH SIDE.-C/A-INSTALLED REPAIR DOUBLER AND FILLER TO RUDDER II 2" FROM TRAILING EDGE ON LH SIDE IAW EMB 145 SRM 51-40-02 AND ERS-EM-55MR-876

Part: WEB — CHAFED (CARGO DOOR) · airframe 38,258 hrs · 33,059 cycles

CARGO DOOR INTERIOR WEB FRAME HAS 12 CHAFES (4 ARE PREVIOUS REPAIRS)-C/A-REMOVED AND REPLACED CARGO DOOR INNER LOWER WEB IAW EMB 145 SRM 51-40-02.

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 38,258 hrs · 33,059 cycles

CARGO DOOR LOWER EDGE INBD ANGLE NUT PLATE HOLES (PREVIOUS REPAIRS) ARE CORRODED. CORROSION LEVEL 1-C/A-REMOVED AND REPLACED CARGO DOOR LOWER EDGE ANGLE IAW EMB 145 SRM 51-40-02.

Part: YOKE — CRACKED (RT ENGINE) · airframe 38,258 hrs · 33,059 cycles

RH ENGINE FWD YOKE UPPER FWD SIDE CRACKED. 1 CRACK, .275" IN LENGTH-C/A-REMOVED AND REPLACED RH FWD LOWER YOKE FITTING IAW ERS-EM-54MR-698.

Part: RIB — CRACKED (LT WING) · airframe 38,258 hrs · 33,059 cycles

LT WING FR21 IN 551CB IS CRACKED. 1 CRACK, LENGTH .3"-C/A-PERFORMED PERMANENT REPAIR TO LT WING RIB 21 IAW EMB 145 SRM 57-20-07-RE ITEM 4.

Part: SKIN — CRACKED (FRAME 77) · airframe 38,258 hrs · 33,059 cycles

FUSELAGE SKIN IS CRACKED AROUND 5 FASTENERS FR 77 LH SIDE BELOW VERTICAL STAB 4 CRACKS, MAX LENGTH .375"-C/A-INSTALLED THE DOUBLER AND 3 FILLERS FOR REPAIR ON FUSELAGE EXTERNAL SKIN AROUND 5 FASTENERS AT FR 77 STGR 5L-6L AREA IAW ERS-EM-53MR-4285.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 38,258 hrs · 33,059 cycles

LAST EMERGENCY LIGHT STRIP AT FR 58 WIRE SP9213 CONNECTOR BROKEN.-C/A-COMPLETE:INSTALLED SP9213 CONNECTOR FOR LAST EMERGENCY LIGHT STRIP IAW SWPM 20-21-00 AND 20-50-01. SEE NRTC BOW352171 FOR OCK. SEE TASK/WIP ENTRIES FOR DETAILS.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,258 hrs · 33,059 cycles

LH AND RH OVERWING EMERGENCY LIGHTS INOP-C/A-COMPLETE:RAR THE BATTERY POWER SUPPLY #4 IAW EMB145 AMM 33-50-04. PERFORMED OPERATIONAL CHECK OF THE LH AND RH OVERWING EMERGENCY LIGHTS IAW EMB145 AMM 33-50-00. OPS CHECK GOOD.

Part: LIGHT — CRACKED (CABIN) · airframe 38,258 hrs · 33,059 cycles

#5 FLOOR PROXIMITY LIGHT STRIP CRACKED-C/A-COMPLETE:RAR #5 FLOOR PROXIMITY LIGHT STRIP IAW EMB145 AMM 33-50-12. SEE NRTC# BOW 352152 FOR AIRCRAFT INSTALLATION AND OPERATIONAL CHECK.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 38,258 hrs · 33,059 cycles

8EA LH CENTER FLOOR PROXIMITY LIGHT STRIP COVER PANELS DAMAGED-C/A-COMPLETE:REPLACED 8EA LH CENTER FLOOR PROXIMITY LIGHT STRIP COVER PANELS IAW EMB145 AMM 33-50-12. SEE NRTC# BOW 352152 FOR AIRCRAFT INSTALLATION AND OPERATIONAL CHECK OF FLOOR EMERGENCY POXIMITY LIGHTS

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,186 hrs · 32,983 cycles

NR 1 AISLE EMERGENCY LIGHT INOPERABLE. C/A: R & R LAMP ON NR 1 AISLE EMERGENCY LIGHT, REF AMM 33-50-08. OPERATIONS CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (NR 1 OIL LEVEL) · airframe 38,184 hrs · 32,979 cycles

HIGH SPEED ABORT AT 90 KTS DUE TO OIL PRESS FLUX NR 1 OIL LEVEL DROPPED TO 2 QTS AT 90 KTS ABORTED THE T/O AND RTG. C/A: REMOVED AND REPLACED NR 1 ENGINE OIL LEVEL SENSOR, IAW ROLLS ROYCE MAINTENANCE MANUAL 79-35-20. PERFORMED OPERATIONAL CHECK, IAW 79-35-20-700-801. OPERATIONS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,108 hrs · 32,916 cycles

OVERWING EMERGENCY LIGHTS INOPERABLE. C/A: R & R NR 4 EMERGENCY BATTERY POWER SUPPLY AND NR 4 EMERGENCY BATTERY, IAW ENOY W/C 33-700-19. OPERATIONS CHECK GOOD.

Part: STRUT — LOW PRESSURE (RT MLG) · airframe 37,360 hrs · 32,192 cycles

"LG AIR/GND FAIL" EICAS MSG WHEN RAISING GEAR ON TAKEOFF. ON LANDING AIRCRAFT DIPPED RT WING LOW. INSPECTED AND FOUND RIGHT MLG STRUT TO HAVE LOW NITROGEN PRESSURE AND HIGH HYD FLUID, SERVICED IAW AMM 32-10-02 PERFORMED GEAR SWING IAW AMM 32-30-00 ALL CLEARANCES GOOD NO FURTHER DEFECTS NOTED OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 37,302 hrs · 32,128 cycles

SUPPLEMENTAL DURING CLIMB WHILE PERFORMING THE ANTI-ICE CHECK BLD VLV FAIL #2 AND PACK 2 OVT CAME ON.-C/A-PERFORMED PNEU. A/I CHECK WITH CREW REF. AMM 30-00-00 OPS CHECK GOOD. CHECKED CMC AND FOUND 2 OCCURANCES OF PRECOOLR 1 SYS FAIL. DEFERRED PACK 1. MEL AUTH# 050130D-C REF# 21-30 MOC# 628765. PERFORMED OPS CHECK OF #1 PACK SYSTEM NO DEFECTS NOTED I/A/W AMM 21-51-00 MEL ITEM RESTORED

Part: STATIC INVERTER — FAILED (AC) · airframe 36,711 hrs · 31,573 cycles

MECH. LANDED SAFELY NO EMERGENCY DECLARED. 115 VAC BUS OFF,GPWS INOP,WINDSHEAR INOP,TERR INOP ENROUTE FL320-C/A-RAR AC STATIC INVERTER IAW E 145 AMM 24-20-01.OPS CHECK GOOD IAW AMM 24-20-00.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 35,631 hrs · 30,668 cycles

L/H AND R/H OVER WING EMER. LIGHTS INOP. REMOVED AND REPLACED #4 EMERG. LIGHT CHARGER AND BATTERY ASSYS, OPC GOOD, IAW AMM 33-50-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,641 hrs · 29,768 cycles

AISLE EMERGENCY LIGHT AT 3A INOP.-C/A-REMOVED AND REPLACED AISLE EMERGENCY LIGHT AT 3A, OPC GOOD IAW AMM 33-50-08

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 33,548 hrs · 28,681 cycles

SSI 53-20-10; SERVICE DOOR CENTER SILL IS CORRODED-C/A-PERFORMED REPAIR,REWORKED AREAS ON SERVICE DOOR CENTER SILL. IAW SRM 53-21-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,548 hrs · 28,681 cycles

FWD DIGITAL IS CORRODED AT FRAME 15 AND CENTER FLOORBEAM-C/A-COMPLETE: REPAIRED FWD DIGITAL AT FRAME 15 AND CENTER FLOORBEAM IAW SRM 53-21-10, FIGURE 201, SHEET 5.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 33,548 hrs · 28,681 cycles

NR 4 EPSU BATTERY AND CHARGER DEFECTIVE.-C/A-COMPLETE: REMOVED AND REPLACED NR 4 EPSU BATTERY AND CHARGER IAW AMM 33-50-04. EASI 6488. OHM CHECK GOOD. OPERATIONAL CHECK GOOD.

Part: LIGHT — CRACKED (CABIN) · airframe 33,548 hrs · 28,681 cycles

LT NR 8 EMERGENCY LIGHT STRIP CRACKED-C/A-COMPLETE: REMOVED AND REPLACED LT NR 8 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. SEE BOW304301 FOR OCK

Part: WIRE — BROKEN (CABIN) · airframe 33,548 hrs · 28,681 cycles

LT NR 4 EMERGENCY LIGHT STRIP WIRE IS BROKEN ON STRIP SIDE-C/A-COMPLETE:REMOVED AND REPLACED LT NR 4 CABIN FLOOR EMERGENCY LIGHT STRIP LIGHT STRIP IAW AMM 33-50-12. SEE BOW304301 FOR OPS CHECK.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 33,548 hrs · 28,681 cycles

NR 1 EPSU BATTERY AND CHARGER DEFECTIVE.-C/A-COMPLETE: R&R NR 1 EPSU BATTERY AND CHARGER IAW AMM 33-50-04. EASI 6488. OHM CHECK GOOD. OPERATIONAL CHECK GOOD.

Part: HOUSING — DEFECTIVE (EMERGENCY LIGHT) · airframe 33,548 hrs · 28,681 cycles

MAIN DOOR EMERGENCY LIGHT WORKS INTERMITTENTLY.-C/A-COMPLETE: R&R MAIN DOOR EMERGENCY LIGHT HOUSING ASSEMBLY IAW AMM 33-26-04. OPS CHECK GOOD.

Part: FITTING — CRACKED (EMERGENCY LIGHT) · airframe 33,548 hrs · 28,681 cycles

LT EMERGENCY LIGHT STRIP EXTRUSIONS NR 1, 3, 4, 6, 7 AND 8 ARE CRACKED-C/A-COMPLETE: REMOVED AND REPLACED LT EMERGENCY LIGHT STRIP EXTRUSIONS NR 1, 3, 4, 6, 7 AND 8 IAW AMM 33-50-12. SEE BOW304301 FOR OCK

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 33,535 hrs · 28,667 cycles

FLOOR PROXIMITY LIGHTS 6-8 ARE INOPERATIVE-C/A-REMOVED AND REPLACED BATTERY POWER SUPPLY NR 4 IAW AMM-33-50-04. OPS CHECK GOOD

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,396 hrs · 28,519 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10-04. OPS CHECKED GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (FIRE DETECTION) · airframe 32,945 hrs · 28,111 cycles

FIRE DETECTOR TEST FAILED AT THE NR 2 FIRE HANDLE, LIGHT NOT COMING ON. REMOVED AND REPLACED FIRE DETECTION PANEL AND THE NR 2 FIRE HANDLE IAW AMM 26-00-01, AND 26-21-01. OPS CHECKED GOOD IAW AMM 26-10-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,656 hrs · 27,817 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT LAMP INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-09-000-801-A, AND 33-50-09-400-801-A. OPS CHECKED GOOD.

Part: FLASHLIGHT — INTERMITTENT (FWD CABIN) · airframe 32,412 hrs · 27,585 cycles

FWD CABIN FLASHLIGHT SWITCH INTERMITTANT. R & R THE FLASHLIGHT IAW AMM 33-50-16-000-801-A, AND 33-50-16-400-801-A. OPS CHECKED GOOD.

Part: MODULE — FAILED (LIGHT PANEL) · airframe 32,362 hrs · 27,542 cycles

AFTER STARTING THE NR 1 ENGINE, THIN TRAIL OF SMOKE VISIBLE AND ODOR FROM BEHIND THE NR 2 LIGHTING PANEL. SMOKE STARTED WHEN FO CHART HOLDER LIGHT WENT OUT. FOUND THE CO PILOT`S LIGHTING CONTROL PANEL CHART HOLDER KNOB BURNED. REMOVED AND REPLACED CO PILOT LIGHTING CONTROL PANEL IAW AMM 20-13-10. OPS CHECKED GOOD IAW AMM 33-11-00

Part: LIGHT — INOPERATIVE (SEAT 12A) · airframe 32,262 hrs · 27,447 cycles

SEAT 12A OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM 33-50-07-000-801-A, AND 33-50-07-400-801-A, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,339 hrs · 25,711 cycles

EMERG LIGHT INOP FLOOR. R&R NR 4 BATTERY AND BATTERY CHARGER AND INVERTER FOR EMERGENCY SEAT 15A,16A,17A AND 18A IAW AMM 33-50-04 AND AMM 33-50-11 OPS GOOD AT THIS TIME. CHARGER ASSY BATTERY P/N BA5-0933-901 S/N C02722. INVERTER P/N 7824-1

Part: LIGHT — INOPERATIVE (LT WING) · airframe 29,831 hrs · 25,257 cycles

LT MAIN WING NAVIGATION LIGHT IS INOP. REMOVED AND REPLACED LT MAIN WING NAVIGATION LIGHT IAW 33-43-03. OPS CHECK GOOD. NO DEFECTS AT THIS TIME.

Part: HOSE — LEAKING (NR 2 A/C PACK) · airframe 29,418 hrs · 24,889 cycles

BURNING ODOR IN COCKPIT WITH APU ON & PACK 2 ON. DUPLICATED ODOR WITH NR 2 PACK OPERATING. FOUND HOSE DISCONECTED ON NR 2 PACK FROM FRONT OF DUAL TEMP CONTROL VALVE TO HEAD EXCHANGER, REMOVED AND REPLACED HOSES AND HARDWERE IAW AMM 21-51-02 GROUND RAN LEAK CHECK GOOD. NO ODORS NOTED.

Part: FUSE — BLOWN (CABIN) · airframe 29,160 hrs · 24,625 cycles

MEL 33-29, EMERGENCY LIGHT ON PASSENGER DOOR INOPERATIVE. R & R FUSE FOR EMERGENCY LIGHT ON PASSENGER DOOR AT POWER SUPPLY. OPS CHECK GOOD MEL HAS BEEN RESTORED, REF CMM 25-60-03.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,150 hrs · 24,614 cycles

MAIN CABIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R FUSE FOR EMERGENCY LIGHT ON PASSENGER DOOR AT POWER SUPPLY. OPS CHECKED GOOD.

Part: BRAKE — FAILED (TE FLAP) · airframe 29,128 hrs · 24,597 cycles

AFTER TAKEOFF, FLAPS WOULD NOT RETRACT FROM 9 DEGREES, FLAP FAIL MESSAGE ON EICAS, RAN QRH PROCEDURES, RETURNED TO DEPARTURE. R & R FLAP TRANSMISSION BRAKE IAW AMM 27-51-01. OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,958 hrs · 24,422 cycles

CAPTAIN REPORTED FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT STANDARD MAINTENANCE PRACTICE.

Part: FLAP SYSTEM — FAILED · airframe 28,923 hrs · 24,388 cycles

FLAP FAIL DURING CLIMBOUT. PERFORMED ZERO DEGREE FLAP RIGGING IAW AMM 27-53-04 CKS GOOD, NO DEFECTS NOTED.

Part: DOOR SILL — CORRODED (FRAME 66) · airframe 28,923 hrs · 24,388 cycles

CARGO DOOR LOWER SILL CORRODED. PERFORMED REPAIR IAW SRM 53-31-15 ITEM 2 FIG 202.

Part: TEE FITTING — CORRODED (FRAME 68) · airframe 28,923 hrs · 24,388 cycles

CARGO DOOR LOWER SILL AFT TEE BRACKET CORRODED. REMOVED AND REPLACED THE TEE BRACKET IAW SRM 51-40-02, AND 51-20-03.

Part: YOKE — CRACKED (LT NACELLE) · airframe 28,923 hrs · 24,388 cycles

LEFT ENGINE PYLON FWD LOWER YOKE CRACKED. REMOVED AND REPLACED YOKE IAW EO EM-54MR-386

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 28,474 hrs · 24,015 cycles

SYSTEM 1 HYD SYS LOW. SERVICED HYD 1 SYS IAW AMM 12-13-01, NO LEAKS NOTED. ACFT OK FOR SERVICE. PERFORMED OPERATIONS IAW AMM 29-10-00. NO DEFECTS NOTED. NO LEAKS NOTED. ACFT OK FOR SERVICE.

Part: CRADLE — CRACKED (FLASHLGHT) · airframe 27,454 hrs · 23,133 cycles

FOWARD CABIN FLASHLIGHT CRADLE IS CRACKED. R & R FWD FLIGHT ATTENDANT FLASHLIGHT HOLDER. OPERATIONS CHECKED GOOD IAW 33-50-06 AMM.

Part: SWITCH — INOPERATIVE (BLEED AIR SYS) · airframe 26,997 hrs · 22,709 cycles

BLEED 2 LOW TEMP IN ICING CONDITIONS, WHILE IN THE CLIMB WITH THRUST LEVERS IN THE THRUST SET POSITION, N2 WAS ABOVE 86%, N2 NR 2 BLEED TEMP POINTER WAS IN THE WHITE RANGE. TRANSFERRED TO NRWC 923-MIA-02210 ITEM 1. R & R NR 2 BLEED PUSHBUTTON IAW AMM 20-13-04. OPERATIONS CHECK OF BLEED AIR SYS SATISFACTORY IAW AMM 36-00-00. SEE NRWC 923-MIA-02210 FOR CORRECTIVE ACTION.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,841 hrs · 22,545 cycles

CAPTAINS FLASHLIGHT BULB BURNED OUT. R & R CAPTAINS EMER FLASHLIGHT SYS IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — NOT SEATED (CABIN) · airframe 26,786 hrs · 22,493 cycles

RT WING AFT EMER EXIT LIGHT INOPERATIVE. RE-SEATED LAMP IN FIXTURE IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 26,357 hrs · 22,071 cycles

RIGHT INBD FLAP TOP SKIN DELAMINATED. ACCOMPLISHED TOP SKIN REPAIR ON RT INBD FLAP IAW ERS-EM-57MR-424.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 26,203 hrs · 21,901 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EMER LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: STARTER GEN — FAILED (APU) · airframe 25,336 hrs · 21,170 cycles

TAXING FOR DEPARTURE WITH NR 2 ENGINE RUNNING & APU ON, A BURNING ODOR WAS OBSERVED ON THE FLIGHT DECK. AFTER DECIDING TO RETURN TO THE GATE, THE ODOR INTENSIFIED & WAS VERY STRONG IN THE CABIN & THE FLIGHT DECK. GROUND PERSONNEL SIGNALED TO SHUTDOWN & OBSERVED SPARKS COMING FROM THE REAR OF THE ACFT. THE APU FAIL EICAS MESSAGE CAME ON AS WE WERE PERFORMING THE GROUND EVACUATION CHECKLIST. TROUBLESHOT ODOR IAW ETN-EM-72-034. NO ODORS ASSOCIATED WITH ENGINES OR PACKS. APU FAILED TO START. TROUBLESHOT APU FAIL MESSAGE IAW MANUAL. FOUND STARTER GENERATOR FAILED & APU UNDER SPEED ON CMC. ODOR DETERMINED TO BE BURNED APU STARTER GENERATOR. R & R APU STARTER GEN IAW WC 24-800-01. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 25,244 hrs · 21,081 cycles

FIRST OFFICER`S FLASHLIGHT INOPERATIVE. R & R FIRST OFFICER`S FLASHLIGHT LIGHT BULB AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE · airframe 25,057 hrs · 20,870 cycles

LEADING EDGE EMER LIGHT INOPERATIVE. R & R BULB IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,979 hrs · 20,791 cycles

COCKPIT FLASHLIGHT INOPERATIVE. R & R IAW AMM 33-50-16.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,972 hrs · 20,785 cycles

HIGH SPEED ABORT ENG 1 REV DEPLOYED & REV DISAGREE MSG DISPLAYED. DEFERRED NR 1 THRUST REVERSER IAW MEL 78-2. M PROCEDURE COMPLIED WITH. NO INSPECTION REQUIRED FOR HIGH SPEED ABORT DUE TO NO MSGS RECEIVED IN AMM 5-50-16. TROUBLE SHOT IAW FIM 78-34-00-810-803-A. FOUND NO RELEVANT FAULT MSGS ON CMC. PERFORMED OPERATIONS CHECK OF THRUST REVERSER IAW AMM 78-31-01-700-801-A. OPERATIONS CHECKED GOOD. COULD NOT DUPLICATE EICAS MSG. MEL RESTORED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,821 hrs · 20,626 cycles

COCKPIT STEP EMER LIGHT & FWD CEILING PANEL EMER LIGHT INOPERATIVE. R & R NR 1 INVERTER IAW AMM 33-50-11. PERFORMED OPERATIONS CHECK IAW AMM 33-50-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,272 hrs · 20,193 cycles

MAIN ENTRY DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EXTERNAL EMER LIGHT IAW AMM 33-50-06. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,117 hrs · 20,069 cycles

RIGHT TOP FUSELAGE SKIN HAS 2 CRACKS AFT OF FRAME 75 & ABOVE STRINGER 2R. CRACK 1 APPROX 1/2 INCHES IN LENGTH AFT OF FRAME 75 & ABOVE STRINGER 2R. CRACK 2 IS APPROX 1/4 INCHES LONG ABOVE TOP MOST FRAME 75 FASTENER. PERFORMED PRIMARY REPAIR TO RT FUSELAGE TOP SKIN AFT OF FRAME 75 ABOVE STRINGER 2R IAW ERS-EM-53MR-495.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,117 hrs · 20,069 cycles

FOWARD THREE FLOOR EMERGENCY LIGHT STRIPS INOPERATIVE. R & R NR 2 EMER BATTERY POWER SUPPLY, BATTERY CHARGER & BATTERY HOLDER IAW AMM 33-50-04. OPERATIONS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,117 hrs · 20,069 cycles

LEFT TOP FUSELAGE SKIN HAS APPROX 3/4 INCH CRACK JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. PERFORMED PRIMARY REPAIR TO LT FUSELAGE TOP SKIN JUST AFT OF FRAME 75 ABOVE STRINGER 2L IAW ERS-EM-53MR-495.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 24,117 hrs · 20,069 cycles

FRAME 22 CORRODED AROUND SERVICE DOOR LOWER DOOR STOP IN TWO AREAS. PERFORMED PERMANENT REPAIR OF FRAME 22 CORROSION AROUND SERVICE DOOR LOWER DOOR STOP IAW ERS-EM-53MR-495.

Part: WIRE — BROKEN (CABIN) · airframe 24,117 hrs · 20,069 cycles

EMERGENCY LIGHT STRIP NR 6 HAS A BROKEN WIRE. INSTALLED THE EMER LIGHT STRIP NR 6 IAW AMM 33-50-12. SEE BOW 157180 FOR OPERATIONAL CHECK.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 24,117 hrs · 20,069 cycles

NLG BAY UPPER DECK CRACKED AT UPLOCK BOX SUPPORT, AFT BRACE, RT END. REPAIRED UPPER DECK IAW ERS-EM-53MR-489.

Part: SUPPORT — CORRODED (RT AILERON) · airframe 24,117 hrs · 20,069 cycles

RIGHT AILERON TORQUE TUBE SUPPORT CORRODED AROUND FASTENER. BLEND AREA ON RT AILERON TORQUE TUBE SUPPORT ACCEPTED AS IS IAW ERS-EM-5300-485. SEE WIP & TASK ENTRIES FOR DETAILS.

Part: HOLDER — FAILED (CABIN) · airframe 24,117 hrs · 20,069 cycles

BATTERY HOLDER ASSEMBLY FAILED CHECKS. R & R BATTERY HOLDER ASSEMBLY.

Part: REINFORCEMENT — CRACKED (FUSELAGE) · airframe 24,117 hrs · 20,069 cycles

FORWARD TO AFT DIGITAL SPLICE REINFORCEMENT CRACKED AT LT FLOORBEAM BETWEEN FRAME 16 & 17. REMOVED CRACKED REINFORCEMENT & INSTALLED SERVICEABLE REINFORCEMENT AT LT FLOORBEAM BETWEEN FRAME 16 & 17 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,117 hrs · 20,069 cycles

FORWARD DIGITAL CORRODED AT NUTPLATE AT PAX DOOR ENTRANCE AT FRAME 15. REPAIRED FWD DIGITAL AT PAX DOOR ENTRANCE AT FRAME 15 IAW ERS-EM-5300-488.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,117 hrs · 20,069 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EMER LIGHT BULB IAW AMM 33-50-10 & OPERATIONS CHECKED GOOD.

Part: TRIM PANEL — CRACKED (CABIN) · airframe 24,117 hrs · 20,069 cycles

FOUR EACH RT FLOOR TRIM EXTRUSIONS CRACKED. R & R FOUR EACH RT FLOOR TRIM EXTRUSIONS IAW AMM 33-50-12.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 23,916 hrs · 19,873 cycles

CAPTAIN` S EMERGENCY FLASHLIGHT INOPERATIVE. R & R CAPTAIN`S EMERGENCY FLASHLIGHT BATTERY IAW ETN-EM-33-038, OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 23,425 hrs · 19,454 cycles

OVER THE WING EMERGENCY LIGHTS INOPERATIVE ON BOTH SIDES. R & R NR 4 POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,279 hrs · 19,351 cycles

SERVICE DOOR EMERGENCY LAMP INOPERATIVE. R & R SERVICE DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,273 hrs · 19,346 cycles

LEFT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. DEFERRED IAW MEL 33-29 AUTH 010608D-C.

Part: HYDRAULIC SYSTEM — LEAKING · airframe 21,870 hrs · 18,185 cycles

RECEIVED AN EICAS MESSAGE "HYD 1 LO QTY" INFLIGHT, HYD PAGE INDICATES SYS 1 QTY IN AMBER. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED A WALK AROUND FOR LEAKS NO DEFECTS NOTED. SERVICED BOTH HYD SYSTEMS IAW AMM 12-13-01. ALSO PERFORMED WALK AROUND FOR LEAKS NO DEFECTS NOTED. SERVICED HYD SYS IAW AMM 12-13-01. THE ACFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 21,569 hrs · 17,947 cycles

THE CREW REPORTED THAT ON CLIMB OUT THEY RECEIVED TRIM MAIN INOP AND BACKUP INOP EICAS MESSAGE. THE CREW DECLARED AN EMERGENCY AND COMPLIED WITH AOM VOL 1 PROCEDURES. THE CREW WAS ABLE TO RECOVER THE BACKUP PITCH TRIM AND CONTINUED TO CVG. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R THE HORIZONTAL STAB CONTROL UNIT IAW AMM 27-40-01. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: ANTENNA — MALFUNCTIONED (LOC/VOR) · airframe 21,374 hrs · 17,788 cycles

ON FLIGHT 4239 THE CREW REPORTED THEY LOST LOCALIZER SIGNAL ON TWO ATTEMPTS OF ILS 10L IN ORD WHILE ESTABLISHED INBOUND. UNABLE TO ID NAVAID. NO OTHER AC REPORT PROBLEMS. DEFERRED BOTH ILS LOCALIZERS IAW MEL 34-15 AUTH#050119D. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. TROUBLESHOT AND REMOVED AND REPLACED THE LEFT AND RIGHT LOC/VOR ANTENNAS IAW EMB 145 AMM TASKS 34-32-03-000-801-A/34-32-03-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME, NO DEFECTS NOTED. MEL 34-15 RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 21,307 hrs · 17,724 cycles

DURING B INSPECTION FOUND THE FORWARD CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT BATTERY USING GENERAL MAINTENANCE KNOWLEDGE. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,290 hrs · 16,930 cycles

DURING B INSPECTION FOUND THE FURTHEST AFT CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED BURNT OUT BULB AT FURTHEST AFT CEILING EMERGENCY LIGHT IAW AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (LT MLG) · airframe 19,694 hrs · 16,488 cycles

ON FLIGHT 4168 THE CREW REPORTED THAT AFTER TAKEOFF RECEIVED AN EICAS LANDING AIR/GROUND FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH LEFT MAIN LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCHES. PART NUMBER 80-057-01, SERIAL NUMBERS 24063 & 10430. REMOVED AND REPLACED THE NOSE GEAR WEIGHT ON WHEELS PROXIMITY SWITCH. PART NUMBER 80-057-01, SERIAL NUMBER 24484. ADJUSTED THE RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH CLEARANCE IAW EMB 145AMM 32-63-01, 32-63-02 AND 32-63-05. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 19,697 hrs · 16,490 cycles

DURING B INSPECTION FOUND THE RIGHT LOWER OVERWING SUPPORT ANGLE NR 3 IS CRACKED ON BOTH ENDS. FORWARD IS 3/8" LONG AND AFT IS 1 1/2". THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING ANGLE NR 3 IAW SRM 51-40-02, AND ETN-EM-53-142. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,995 hrs · 15,220 cycles

DURING B-INSPECTION FOUND THE LAST CENTER AISLE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LAMP ONLY IN THE LAST CENTER AISLE EMERGENCY LIGHT IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PUMP — MALFUNCTIONED (NR 1 ENGINE) · airframe 17,879 hrs · 15,134 cycles

ON FLIGHT 4344 THE CREW REPORTED THAT AFTER TAKEOFF WHEN RETRACTED GEAR GOT A HYDRAULIC 1 LOW QUANTITY. FLUID LEVEL CONTINUED TO GO DOWN. THE CREW DECLARED AN EMERGENCY AND RETURNED TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE CREW REPORTED THAT ON THE WALK AROUND THEY FOUND HYDRAULIC FLUID ON LEFT SIDE OF AIRCRAFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE HYDRAULIC PUMP IAW EMB AMM 29-10-03. THE OPERATIONAL AND LEAK CHECK WERE GOOD. REMOVED AND REPLACED THE HYDRAULIC NR 1 ENGINE PUMP MAGNETIC SEAL P/N 42520-70 IAW RR MM 72-63-10-990-805. THE LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,398 hrs · 14,754 cycles

DURING MAINTENANCE INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT IAW AMM TASKS 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — FAULTY (CABIN) · airframe 17,030 hrs · 14,483 cycles

ON FLGIHT 4089 DURING THE TAXI THE CREW DETECTED A BURNING ODOR IN THE CENTER CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF THE CABIN AREA LIGHTING SYSTEM, NO DEFECTS NOTED. FOUND ELECTRICAL ODOR COMING FROM AFT FLASHLIGHT ASSEMBLY. REMOVED AND REPLACED THE AFT FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: AUDIO PANEL — MALFUNCTIONED (COCKPIT) · airframe 15,629 hrs · 13,503 cycles

FOR FLIGHT 2820 THE CREW REPORTED WHILE SITTING AT THE GATE WITH EXTERNAL POWER ON STARTED SMELLING SMOKE IN THE COCKPIT SO THEY POWERED EVERYTHING DOWN. THE SMOKE ODOR WAS ACCOMPANIED BY A POPPING, SIZZLING NOISE COMING THROUGH THE FIRST OFFICER’S HEADSET. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DIGITAL AUDIO PANEL IAW AMM 23-51-01. AFTER SUBSEQUENT OPERATIONAL CHECKS NO EVIDENCE OF SMOKE SMELL WAS OBSERVED, ALSO REPLACED SLICE SP 2170 IAW WPM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 13,358 hrs · 11,797 cycles

ON FLIGHT 2958 AT APPROXIMATELY 1000 FEET DURING THE FINAL APPROACH WITHOUT THE AUTO PILOT ON THE CREW PUT THE LANDING GEAR DOWN AND THE PITCH TRIM STARTED TO RUN THE NOSE DOWN BY ITSELF. THE CREW PUSHED AND HELD THE INHIBIT BUTTON AND THE TRIM STOPPED AT 2 PERCENT DOWN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAPPER VALVE — DEFECTIVE (RT WING) · airframe 13,348 hrs · 11,791 cycles

ON FLIGHT 2761 ON TAKEOFF A TRAILING AIRCRAFT REPORTED A WHITE TRAIL COMING FROM THE RIGHT WING. THE CREW REPORTED, OBSERVED A FUEL IMBALANCE AT 400 POUNDS. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WING FUEL FLAPPER CHECK VALVE IAW EMB145 AMM 28-11-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUT — LOW (NLG) · airframe 12,169 hrs · 10,815 cycles

ON FLIGHT 9800 THE CREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. RECEIVED A LANDING GEAR FAIL MESSAGE ON EICAS. CREW ELECTED TO RETURN TO MQT AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED THE NOSE LANDING GEAR AND FOUND THE NOSE LANDING GEAR STRUT LOW. SERVICED THE NOSE LANDING GEAR STRUT IAW EMB AMM 145-32-20-01. NO PARTS WERE REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD PER AMM 32-30-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMEGENCY LIGHTS) · airframe 11,411 hrs · 10,089 cycles

ON FLIGHT 4119 THE FLIGHT ATTENDANT REPORTED THAT THE EMERGENCY EXIT SIGN TOP AFT DOOR JAMB OF LEFT OVERWING EXIT WILL NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT AND FOUND NO DEFECTS EMB AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 11,206 hrs · 9,870 cycles

DURING PS-2 INSPECTION, FOUND LEFT OVERWING EMERGENCY EXIT SIGN ON WALL PANEL INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMBRAER AMM 33-50-11. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — FAILED (COCKPIT WINDOW) · airframe 10,735 hrs · 9,459 cycles

CAPT DV WINDOW BLEW SEAL AT 27,000 FT. EMERGENCY DECLARED AND EMERGENCY DECENT WAS ESTABLISHED. ACFT WAS ABLE TO MAINTAIN PRESSURE THROUGHOUT DECENT. ACFT WAS REMOVED FROM SERVICE. MEL 2118 SYS AND RETURNED BACK TO SERVICE.

Part: SEAL — WORN (WINDOW) · airframe 10,735 hrs · 9,459 cycles

CAPT DV WINDOW BLEW SEAL AT 27,000 FEET. EMERGENCY DECLARED AND EMERGENCY DESCENT WAS ESTABLISHED. AIRCRAFT WAS ABLE TO MAINTAIN PRESSURE THROUGHOUT DESCENT. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DV SEAL. ALL CHECKS GOOD. MEL CLOSED. AIRCRAFT RETURNED BACK TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,832 hrs · 8,580 cycles

DURING MBV INSPECTION FOUND SERVICE DOOR AFT SILL CORRODED. REPAIRED DOOR SILL IN ACCORDANCE WITH SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,832 hrs · 8,580 cycles

DURING MBV INSPECTION FOUND SERVICE DOOR CENTER SILL CORRODED. REPAIRED DOOR SILL IN ACCORDANCE WITH EMBRAER SRM 53-21-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,832 hrs · 8,580 cycles

DURING MBV INSPECTION FOUND LEFT OMEGA BEAM CORRODED AT FRAME 24-25 CROSSMEMBER. REPAIRED OMEGA BEAM IN ACCORDANCE WITH EMBRAER SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (LAVATORY)

ON TAKEOFF, RECEIVED LAV SMOKE ALERT. FOLLOWED AOM PROCEDURES AND CONTINUED UNEVENTFUL. NO OIL OR SMOKE SMELL NOTED. (K) REPLACED ENGINE 2, OPS CHECK AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

AFTER TAKEOFF AT APX 1,000 FT GOT LAV SMOKE LIGHT ON AND FA AND PAX, NOTED OIL ODOR IN AFT CABIN CREW RETURNED, LAV SMOKE LIGHT WENT OUT 3-5 MIN AFTER TURN BACK, NO OTHER PROBLEMS NOTED. (K)

Part: ENGINE — LEAKING (NR 1)

FLT 3598 - CMH - AFTER TAKEOFF, GOT LAV SMOKE LIGHT ON AND FA NOTED OIL SMELL IN AFT CABIN. CREW RETURNED TO CMH, LAV SMOKE LIGHT WENT OUT 3-5 MINUTES AFTER TURN BACK TO CMH. NO OTHER PROBLEMS NOTED. REMOVED AND REPLACED NR 1 ENGINE DUE TO INTERNAL OIL LEAK CAUSING ODOR. OPS CHECK AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DOOR — GROUND DAMAGE (CARGO BAY)

AIRCRAFT WAS STUCK BY GROUND SUPPORT EQUIPMENT WITH DAMAGE TO BAGGAGE DOOR. REPAIRED BAGGAGE DOOR WITH AN EXTERNAL DOUBLER IAW EMB REPAIR STATEMENT IC 2005-145/5995 AND SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)