N673AE

Part: PRESSURE SWITCH — CORRODED (ZONE 300) · airframe 47,713 hrs · 43,711 cycles

RUDDER SYSTEM 1-2 INOP MSG DISPLAYED AT APROX 3000FT 210K. T/S IRW FIM 27-22-00-810-804-A R&R #2 RUDDER PSI SWITCH IAW AMM 27-23-04 OPS CHECK AND LEAK CHECK GOOD. ACFT OK FOR SERVICE AT THIS TIME

Part: EXHAUST FAN — ODOR (ZONE 200) · airframe 46,334 hrs · 42,154 cycles

WITH E-1 RUNNING AFTER PUSH-BACK SPS 1 INOP WARNING DISPLAYED WITH A BURNING PLASTIC SMELL. FACT 29DEC24 10:56 CLT PERFORMED STALL OPS CHECK IAW AMM 27-36-00. OPS CHECK GOOD. A/C OK FOR SERVICE. SEE SEQ.2 THIS LOG PAGE FOR BURNING SMELL. (NOTE...FOUND SMELL TO BE ELEC BAY COOL EXHAUST FAN 2 PULLED IN INSULATION. PUT FAN ON MEL.)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

53-2369 CTR OMEGA BEAM CORRODED AT FR20. RAR BEAM IAW SRM 51-40-02

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

53-2365 2 INTERNAL INTERCOSTALS CORRODED ON TOILET WASTE CUP. RAR INTERCOSTALS IAW SRM51-40-02

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

53-2365 2 INTERNAL INTERCOSTALS CORRODED ON TIOLET WASTE CUP. RAR INTERCOSTALS IAW SRM51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2361 LH OMEG BEAM #1 CRACKED AT FR22. REPAIRED IAW EO 1-53-24-0612

Part: SKIN — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2339 FUSE SKIN CRACKED ABOVE FWD RH WINDSHIELD BTW FR12 -12A. REPAIRED IAW EO1-53-24-0618

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2308 SHEAR CLIP CRACKED AT FR80 BTW STR5-7R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2306 LH SHEAR CLIP CRACKED AT FR80 BTW STR5-7L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SKIN — CRACKED (ZONE 300) · airframe 45,991 hrs · 41,789 cycles

55-2310 VERT STAB AFT OF REAR SPAR 3, SKIN PROFILE CRACKED AT 2 PLACES. FARICATED NEW PROFILE IAW SRM 55-30-01. RAR PROFILE IAW SRM 51-40-02

Part: PLATE — CRACKED (NLG WW) · airframe 45,991 hrs · 41,789 cycles

53-2297 NLG WW PLATE CRACKED. RAR PLATE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

53-2153 RH OMEGA BEAM CORRODED AROUND NUTPLAE AT BTW FR59-61. REPAIRED IAW EO1-53-24-0588

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,450 cycles

53-2040 CTR OMEGA BEAM #2 CRACKED AT FR29. REPAIRED IAW EO1-53-24-0610

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

53-2153 RH OMEGA BEAM CORRODED AROUND NUTPLATE AT BTW FR59-61. REPAIRED IAW SRM 53-24-10 AND EO1-53-24-0588

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2038 OMEGA BEAM #1 CRACKED AT FR23. REPAIRED IAW EO1-53-24-0606

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2104 SUPPORT ANGLE UNDER MIDDLE GUSSET CRACKED AT BTW FR19-20. RAR ANGLE IAW SRM 51-40-02

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2104 UPPER MIDDLE GUSSET SUPPORT ANGLE CRACKED AT BTW FR19-20. RAR ANGLE IAW SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

53-2097 TOILET AREA RH GUSSET CORRODED AT BTW FR59-62. RAR GUSSET IAW SRM 51-40-02

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

TOILET AREA LH GUSSET CORRODED AT BTWFR59-62. R & R GUSSET IAW SRM51-40-02

Part: WEB — CRACKED (ZONE 100) · airframe 45,991 hrs · 41,789 cycles

57-2054 RH MLG WHEEL WELL AFT WEB CRACKED. REPAIRED IAW EO 1-05-24-0634 AND SRM 53-23-12.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2070 SHEAR CLIP CRACKED AT FR73 BTW STR8-10L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: ANGLE — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,450 cycles

53-2082 ANGLE CRACKED AT LEVEL OF FR15 AND STR16L. RAR ANGLE IAW SRM 51-40-02

Part: SUPPORT — CRACKED (ZONE 800) · airframe 45,991 hrs · 41,789 cycles

53-2074 CARGO DOOR OPERATING MECHANISM LWR SUPPORT CRACKED BTW FR67-68 BTW 4-5R. RAR SUPPORT IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2063 OMEGA BEAM CRACKED AT FR36. REPAIRED IAW EO1-53-24-0611

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2067 SHEAR CLIP CRACKED AT FR66 BTW SRT6-7L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2069 SHEAR CLIP CRACKED AT FR68 BTW STR6-8L. RAR SHEAR CLIP IAW SRM51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2071 SHEAR CLIP CRACKED AT FR73 BTW STR 8-10R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SUPPORT — CORRODED (ZONE 600) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

53-2086 RH SIDE, FWD SLL CORRODED AT BTW FR19-20. RAR SILL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2068 SHEAR CLIP CRACKED AT FR67 BTW STR6-7L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2088 LH OMEGA BEAM CRACKED AT FR21. REPAIRED IAW EO1-53-24-0606

Part: SUPPORT — CRACKED (ZONE 800) · airframe 45,991 hrs · 41,789 cycles

CARGO DOOR OPERATING MECHANISM UPPER SUPPORT CRACKED AT BTW FR67-68 STR4R. RAR SUPPORT IAW SRM 51-40-02

Part: SUPPORT — CRACKED (ZONE 800) · airframe 45,991 hrs · 41,789 cycles

53-2073 CARGO DOOR OPERATING MECHANISM MIDDLE SUPPORT CRACKED AT BTW FR67-68 BTW STR4-5R. RAR SUPPORT IAW SRM 51-40-02

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

53-2058 CARGO ENTRANCE LWR BEAM CORRODED BTW FR65-68. RAR BEAM IAW SRM 51-40-02

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

53-2087 SERVICE DOOR CHANNEL CORRODED. RAR CHANNEL IAW SRM 51-40-02

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

53-2057 CARGO DOOR ENTRANCE FWD L-SHAPE AT FR65 CORRODED. REPAIRED IAW EO1-53-24-0622

Part: ANGLE — WORN (ZONE 600) · airframe 45,991 hrs · 41,789 cycles

57-2079 RETAINING ANGLE WORN ON RH WING LE SPLICE 612AR. RAR ANGLE IAW SRM 51-40-02

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 45,991 hrs · 41,789 cycles

53-2077 CARGO DOOR OPERATING MECHANISM SUPPORT ANGLE CRACKED AT FR62 BTW STR4-5R. RAR ANGLE IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,991 hrs · 41,789 cycles

53-2045 SHEAR CLIP CRACKED AT FR26 BTW STR15-16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,991 hrs · 41,789 cycles

53-2044 SHEAR CLIP CRACKED AT FR24 BTW STR16-17R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,991 hrs · 41,789 cycles

53-2043 SHEAR CLIP[ CRACKED AT FR24 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2041 LH OMEGA BEAM CRACKED AT FR34. REPAIRED OMEGA BEAM IAW EO1-53-24-0613

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2047 SHEAR CLIP CRACKED AT FR27 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 45,991 hrs · 41,789 cycles

53-2039 LH OMEGA BEAM #2 CRACKED AT FR24. REPAIRED IAW EO 1-53-24-0607

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,991 hrs · 41,789 cycles

53-2046 SHEAR CLIP CRACKED AT FR25 BTW STR15-16R. RAR SHEAR CLIP IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,991 hrs · 41,789 cycles

53-2020 EXTERNAL FUSE, TOILET WASTE VALVE SUPPORT CORRODED. RAR SUPORT IAW SRM 51-40-02

Part: WARNING SYSTEM — FAULTED (STALL) · airframe 45,885 hrs · 41,677 cycles

STALL PRTOECTION TEST PERFORMED DURING PREFLIGHT WITH NO ISSUES. PRIOR TO 60KNOTTS ON T/O SPS FAIL EICAS MESSAGE APPEARED. NOTED STRONG CROSSWINDS AND NO CMC MESSAGES. PERFROMED TEST AGAIN WITH NO ISSUES

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,179 hrs · 39,709 cycles

RUDDER SYSTEM 2 INOP AFTER TAKEOFF......TROUBLESHOT PER FIM 27-22-00-810-804-A STEPS 1 AND 8. FOUND RUDDER SYS 2 PRESS SWITCH BAD. R&R RUDDER SYS 2 PRESSURE SWITCH PER AMM 237-23-04. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE... ACTUAL LP 288223-1.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,179 hrs · 39,709 cycles

RUDDER SYSTEM 2 INOP AFTER TAKEOFF......TROUBLESHOT PER FIM 27-22-00-810-804-A STEPS 1 AND 8. FOUND RUDDER SYS 2 PRESS SWITCH BAD. R&R RUDDER SYS 2 PRESSURE SWITCH PER AMM 237-23-04. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE... ACTUAL LP 288223-1.

Part: NONE — NONE · airframe 43,010 hrs · 38,446 cycles

PDIS 673 21-01 2777201 31JAN23 CHO ASSGN ODOR OBSERVED WITH PACK 1 ON INTERMITTENTLY. RAN #1 PAC SYSTEM & FOUND #1 ACM INOP.R&R # 100 ACM IAW AMM 21-51-03. OPS CHECK GOOD. NO MORE SMELL CLEAR MEL 21-15-2

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,893 hrs · 38,318 cycles

RH OVERWING EMERGENCY WING LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY WING LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A OPS CHECK GOOD

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 42,860 hrs · 38,286 cycles

FA EMERGENCY FLASHLIGHT HOLDER CLIP BROKEN-C/A-RAR FA EMERGENCY FLASHLIGHT HOLDER CLIP IAW ASTRONICS DME CMM 25-60-14. OPS CHECK GOOD.

Part: NONE — INOPERATIVE (AFT) · airframe 41,915 hrs · 37,210 cycles

AFT CABIN EMERGENCY FLASHLIGHT WONT CHARGE-C/A-RE-INSTALLED FLASHLIGHT IN ASSEMBLY IAW EMB 145 AMM 33-50-16. OPC GOOD.

Part: NONE — NONE · airframe 41,646 hrs · 36,879 cycles

HEAVY CHECK MBV, NRWC# E900820 - RH MLG FORWARD MAIN BRACE FITTING HOUSING HAS PITTING ON BORE FOR BEARING - OUT OF LIMITS-C/A-RAR RH MLG FWD SIDE BRACE FITTING IAW ERS-EM-57MR-1382

Part: NONE — NONE · airframe 41,646 hrs · 36,879 cycles

E899729-LH ENGINE YOKE FORWARD LINKAGE FITTING IS CRACKED. (MAJOR REPAIR)-C/A-REPLACED YOKE FITTING IAW ERS-EM-54MR-698.

Part: NOT REPORTED — NOT REPORTED · airframe 41,646 hrs · 36,879 cycles

WING RIB JUST O/B OF RIGHT PCA IS CRACKED AT RIVET THRU UPPER SKIN N900663 (MAJOR REPAIR)-C/A-REPAIRED WING RIB JUST O/B OF RIGHT PCA SRM 57-20-07-RE FIG 203.

Part: NOT REPORTED — NOT REPORTED · airframe 41,646 hrs · 36,879 cycles

N900664-WING RIB JUST O/B OF LEFT PCA IS CRACKED AT RIVET THRU UPPER SKIN (MAJOR REPAIR)-C/A-REPAIRED WING RIB JUST O/B OF LEFT PCA SRM 57-20-07-RE FIG 203.

Part: NONE — NONE · airframe 41,499 hrs · 36,709 cycles

MAIN ENTRY CEILING EMERGENCY LIGHT INOP-C/A-RAR MAIN ENTRY EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC GOOD. END.

Part: CRADLE — BROKEN (C/P FLASHLIGHT) · airframe 41,131 hrs · 36,258 cycles

FLASHLIGHT BRACKET BROKEN ON CA SIDE.-C/A-RAR LH FLIGHT DECK FLASH LIGHT ASSY IAW EMB 145 AMM 33-50-16.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,091 hrs · 36,205 cycles

12A OVERHEAD EMERGENCY LIGHT INOP-C/A-RAR SEAT 12A OVERHEAD EMERGENCY LIGHT BULB IAW EMB AMM 33-50-07-000-801-QA AND 33-50-07-400-801-A OPC GOOD END

Part: A/C PACK — ODOR (NR 1) · airframe 40,727 hrs · 35,780 cycles

DURING CLIMB OUT OF ORD MINOR SMELL OF POSSIBLE OVERHEATED PLASTIC AND OR RUBBER SEEMINGLY COMING FROM OVER #1 PACK. SMELL WENT AWAY RATHER QUICKLY NO ABNORMAL MESSAGES OR INDICATIONS OTHERWISE. ON APPROACH INTO GSP SMELL RETURNED STRONGLY AND PACK STRUGGLED TO COOL COCKPIT SIGNIFICANTLY AT THE GATE. WE RECEIVED A PACK 1 OVERHEAT CAUTION. NO EMERGENCY DECLARED-C/A-PERFORMED #1 ACM REMOVAL AND ADDITIONAL INSPECTION ACTIONS IAW EO NUMBER EM-2100-048. OPS CHECK GOOD. LEAK CHECK GOOD. MEL ITEM RESTORED. C/W ETN-EM-72-034 ODOR EVENT T/S FOUND PACK 1 ACM DAMAGED. DEFERRED PER MEL 21-30.

Part: ACM — SEIZED (NR 2) · airframe 40,658 hrs · 35,691 cycles

SMOKE IN THE CABIN AND ASSOCIATED BURNING SMELL WHEN PACK 2 WAS RESET AFTER T/O FA NOTED ITSEEMED TO COME FROM CENTER OF A/C-SMOKE IN CABIN WORK SCOPE ISSUED BY REPEAT CONTROL REQUIRES CMC DOWNLOAD AND REVIEW. C/W CMC DOWNLOAD IAW MM 45-45-00 AND UPLOADED TO DATA FILES. REVIEWED DOWNLOAD & FOUND NO OTHER DESCREPANCIES. ANY MSG WAS RELATED TO ACM FAILURE. FLIGHT DECLARED EMERGENCY SMOKE IN TCABIN & ASSOCIATED BURNING SMELL WHEN PACK 2 WAS RESET AFTER T/O, FA NOTED IT SEEMED PACK 2 WAS RESET AFTER T/O FA NOTED ITSEEMED TO COME FROM CENTER OF A/C. WHILE TROUBLE SHOOTING FOUND #2 ACM SEIZED REQUIRING EO EM-2100-048 TO BE COMPLIED WITH. COMPLETED EO-EM-2100-048. R & R RH ACM REF NRWC 673-ORD-04797LEAK CHK AND OPS CHK OF ACM..

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,432 hrs · 35,453 cycles

AFT AISLE EMERGENCY LIGHT INOP-C/A-RAR AFT AISLE EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END.

Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKE SYS) · airframe 40,379 hrs · 35,401 cycles

MECH OUTBD BRAKE INOP.BRK- OUTB INOP MESSAGE APPEARED WHEN LANDING GEAR EXTENDED. WENT MISSED AND RETRACTED THE LANDING GEAR AND MESSAGE WENT AWAY. ON 2ND ATTEMPT TO LAND MESSAGE REAPPEARED WHEN GEAR EXTENDED AND STAYED ON. REMOVED AND REPLACED LEFT HAND BRAKE CONTROL VALVE IAW AMM 32-41-06. FUCTION CHECK MAIN BRAKE SYSTEM IAW AMM 32-41-00 WITH BRAKE ANALYZER. FUCTION CHECK IS GOOD. TRANSFER FROM NRWC 673-DFW-04699

Part: FLASHLIGHT — MISSING (CABIN) · airframe 39,909 hrs · 34,967 cycles

DURING PS-2 FOUND REAR AIR LIGHT 2R LED EMERGENCY FLASHLIGHT MISSING FROM MOUNT. C/A: INSTALLED NEW AIR LIGHT 2R LED EMERGENCY FLASHLIGHT, IAW CMM 25-60-14.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 39,884 hrs · 34,946 cycles

2ND FROM AFT CABIN FLOOR EMERGENCY LIGHT STRIP INOPERABLE. C/A: REPAIRED WIRE FOR 2ND FROM AFT EMERGENCY FLOOR LIGHT STRIP,AW SWPM 20-21-00. OPERATIONS CHECK GOOD, REFERENCE WIP NR 1. INSTALLED 2ND FROM AFT EMERGENCY FLOOR LIGHT STRIP, IAW EMB145 AMM 33-50-12-400-801.

Part: WINDSHIELD WIPER — STUCK (WINDSHIELD) · airframe 39,168 hrs · 34,223 cycles

WINDSHIELD WIPER ON CA SIDE STUCK AT MID POINT OF WINDSHIELD DURING TAKEOFF-C/A-PEFORMED PRESSURE CHECK OF CAPT WIPER ARM ASSY IAW EMB-145 M/M 30-41-03 OPS GHECK GOOD

Part: DOOR — LACK OF LUBE (CABIN) · airframe 38,856 hrs · 33,929 cycles

FA REPORTS THAT THE MAIN CABIN DOOR IS DIFFICULT TO OPEN .-C/A-GVI ON MAIN PAX DOOR LUBED ALL MOVEABLE PARTS CHECK OPERATION OF DOOR OPEN AND CLOSE OPS CHECK GOOD NO ISSUES FOUND .

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 38,828 hrs · 33,902 cycles

MAIN CABIN DOOR NOT OPENING AND CLOSING CORRECTLY-C/A-INSPECTED MAIN CABIN DOOR VERIFIED OPERATION OF DOOR REF EMB 145 AMM 52-10-01 ALL CHECKS GOOD OK FOR SERVICE

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,592 hrs · 33,645 cycles

EMERGENCY EXIT ROW PSU LIGHTS ON RH AND LH INOP-C/A-REMOVED AND REPLACED EMERGENCY BATTERY AND CHARGER IAW EMB AMM 33-50-04 OPS CK GOOD.

Part: ANTI-ICE VALVE — FAILED (INOPERATIVE) · airframe 38,050 hrs · 33,161 cycles

E-1 ANTI-ICE FAIL ON TAKEOFF WITH ENGINE ANTI-ICE DISAGREE CAUTION-C/A-DEFERRED ENG-1 ANTI-ICE VALVE PER MEL 30-11, AUTH# 100923DM-C, EXPIRATION 11-06-19. M PROCEDURES C/W. RAR E1 ANTI ICE VALVE IAW E-1 ANTI-ICE FAIL ON TAKEOFF WITH ENGINE ANTI-ICE DISAGREE CAUTION-C/A-DEFERRED ENG-1 ANTI-ICE VALVE PER MEL 30-11, AUTH# 100923DM-C, EXPIRATION 11-06-19. M PROCEDURES C/W. RAR E1 ANTI ICE VALVE IAW AMM 30-21-01 OPS CHECK GOOD MEL RESTOREDAMM 30-21-01 OPS CHECK GOOD MEL RESTORED

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,760 hrs · 32,917 cycles

REAR HALF OF EMERGENCT EXIT LIGHTS BATTERY DIES AFTER 2 MINUTES. C/A-REMOVED AND REPLACED #4 EMERGENCY LIGHT BATTERY AND CHARGER IAW WC# 33-700-19.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 37,760 hrs · 32,916 cycles

STRINGER 6R IS CRACKED BTW FR 12A-13. C/A-REPAIRED STRINGER 6R BTW FR 12A-13 IAW SRM 51-20-03 AND 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,760 hrs · 32,916 cycles

CARGO DOOR LOWER SILL IS CORRODED. C/A-REMOVED AND INSTALLED CARGO DOOR SILL BETWEEN FR65 AND 68 IAW SRM51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 37,760 hrs · 32,916 cycles

SSI 53-30-48 CORROSION ON SHEAR CLIP AT FRAME 68 LOWER BAGGAGE DOOR CUT-OUT PREVIOUS REPAIR. C/A-REMOVED AND INSTALLED NEW SHEAR CLIP AT FRAME 68 LOWER SECTION IAW SRM 51-40-02 & SRM 53-31-04.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 37,760 hrs · 32,916 cycles

CFI FUSELAGE SKIN HAS 2 SMALL SCRATCHES BTW FR21-22 AND STR 19R-20R. C/A-REPAIRED CFI FUSELAGE SKIN 2 SMALL SCRATCHES BTW FR21-22 AND STR 19R-20R IAW SRM 53-21-01.

Part: SKIN — GOUGED (FUSELAGE) · airframe 37,760 hrs · 32,916 cycles

FUSELAGE SKIN SCRATCHED/GOUGED BETWEEN F77/80 AND STR 9L/10L. C/A-REPAIRED FUSELAGE SKIN BETWEEN FR 77/80 AND STR 9L/10L IAW ERS-EM-53MR-3869.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,760 hrs · 32,916 cycles

FFLL TOP SKIN CRACKED AT RIVET BTW LT DV WINDOW AND PILOT WINDSHIELD. C/A-REPAIRED FFLL TOP SKIN CRACKED AT RIVET BTW LT DV WINDOW AND PILOT WINDSHIELD IAW EO EM-5300-2232.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 37,760 hrs · 32,916 cycles

L/H OVER WING EMERGENCY EXIT IDENTIFIER SIGN IS INOP.-C/A-COMPLETE:UP ON FURTHER INVESTIGATION FOUND ELECTRICAL CONNECTOR TO BE DISCONNECTED. RECONNECTED ELECTRICAL CONNECTOR TO THE EXIT INDENTIFIER SIGN IAW EMB145 AMM 33-50-13 OPS CHECK GOOD. SEE WIPS FOR DETAILS

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,760 hrs · 32,916 cycles

EMERGENCY LIGHT STRIPS #4 #5 ARE INOP-C/A-COMPLETE:REMOVED AND REPLACED SPLICE FOR EMERGENCY LIGHT STRIP #5 IAW EMB145 SWPM 20-21-00, REMOVED AND REPLACED EMERGENCY LIGHT STRIP ASSY #4 IAW 145 AMM 33-50-12 OPS CHECK GOOD. EASI #4745,102,5241

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,300 hrs · 32,529 cycles

TRANSFERRED FROM AML PAGE 4391436 ITEM 2" SEE ITEM 1 LOGPAGE 4391435FOUND DAMAGE BETWEEN FRAME 61-64 AND STRINGER 19L AND 20L. MULTIPLE DENTS AND SCRATCHES NOTED. INSPECTED AND FOUND INTERNAL STRUCTURE TO BE A SERVICEABLE CONDITION . MAJOR REPAIR-C/A-REPAIRED DAMAGED FUSELAGE SKIN BETWEEN FRAMES 61-64 AND STR 19L-20L IAW ERS EM-53MR-3791.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 37,300 hrs · 32,529 cycles

EMERGENCY LIGHT STRIPS 4 & 5 AND BOTH EMERGENCY EXIT SURROUND PANEL LIGHTS COME ON AND GO OUT. C/A-C/W EMERGENCY LIGHTING ADUJSTMENT/TEST IAW AMM 33-50-00. NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 36,248 hrs · 31,470 cycles

ABORTED TAKEOFF DUE TO BURNING SMELL.PACK #2 VALVE CLOSE MESSAGE IN FLIGHT AIRCRAFT WOULD NOT MAINTAIN PRESSURIZATION"TRANSFERRED TO NRWC 673-ORD-03323"-C/A-TRANSFERRED FROM NRWC 673-ORD-03324. COMPLIED WITH FIM TASK 21-51-00-810-804-A. PERFORMED OPS CHECK OF RH PACK IAW EMB-145 AMM 21-00-00. OPS CHECK GOOD, FOUND TO BE TRANSITORY CONDITION PER THE FIM BLOCK DIAGRAM 002 (POST MOD SB 145-21-0015 STEP 2).

Part: UNKNOWN — ODOR (COCKPIT) · airframe 34,894 hrs · 30,324 cycles

ODOR OF SMOKE IN THE COCKPIT. COMPLIED WITH A THREE MINUTE HIGH POWER RUN IAW MM 72-00-00. NO ODOR NOTED. FCF FOUND SATISFACTORY

Part: LIGHT — INOPERATIVE (RT WING) · airframe 34,684 hrs · 30,106 cycles

RIGHT WING FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: DUCT — BROKEN (NR 2 ANTI-ICE) · airframe 34,666 hrs · 30,087 cycles

NR 2 BLEED LEAK EICAS MESSAGE AND SWITCH BLEED DURING CRUISE. TROUBLESHOT BLEED 2 LEAK ON EICAS AND BLEED SWITCH AND DURING INSPECTION FOUND ENGINE NR 2 ANTI ICE DUCT TO BE BROKEN ON FWD SIDE OF ANTI ICE VALVE. REMOVED AND REPLACED THE NR 2 ENGINE ANTI ICE DUCT IAW AMM 30-21-05 AND PERFORMED OPS CHECK IAW AMM 30-21-00 OPS CHECKED GOOD.

Part: WHEEL — DAMAGED (MLG) · airframe 34,478 hrs · 29,915 cycles

AIRCRAFT WONT STOP, USED EMERGENCY BRAKE, FOUND FLAT SPOT ON ALL TIRES. PERFORMED BRAKE INSPECTIONS ON ALL 4 BRAKES IAW WC 32-700-18 AND AIRCRAFT TAXI OPS CHECKED GOOD IAW 09-20-00. REMOVED AND REPLACED THE NR 1, 2, 3 AND 4 MLG WHEEL ASSY IAW WC 32-700-11. ZERO BRAKING ON RUNWAY DUE TO ICE.

Part: O-RING — FAILED (NR 2 BLEED) · airframe 34,475 hrs · 29,911 cycles

NR 2 BLEED LEAK WARNING DURING CLIMBOUT. CLIMB THRUST, O' SAT, 5' TAT, ANTI-ICE SYSTEM ON FL 200. REMOVED AND REPLACED THE O-RINGS AT JOINT 18 IAW AMM 36-11-10. OPS OK.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 34,394 hrs · 29,836 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-50-16. TESTED SATISFACTORY.

Part: SKIN — BURNED (FUSELAGE) · airframe 32,778 hrs · 28,337 cycles

EXTERNAL FUSELAGE SKIN HAS BURN MARK FR-15 STR-21L. ACCOMPLISHED FABRICATION AND PREP OF REPAIR DOUBLER AND FILLER, ALODINED AND PRIMERED REPAIR PIECES IAW SRM 53-00-01, SRM 53-21-01, CPM 51-21-05 AND ETN-EM-51-091

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,776 hrs · 28,335 cycles

NR 3 EMERGENCY LIGHT STRIP INOP, FOUND DURING CLOSE UP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT STRIP IAW 33-50-12. OPS CHK GOOD.

Part: DOOR — CORRODED (CARGO BAY) · airframe 32,776 hrs · 28,335 cycles

CARGO DOOR IS CORRODED AROUND 1 SCREW HOLE FWD LOWER END. ACCOMPLISHED DOUBLER AND FILLER REPAIR AROUND SCREW HOLE FWD LOWER END IAW ERS-EM-52MR-741.

Part: YOKE — CRACKED (RT ENGINE) · airframe 32,776 hrs · 28,335 cycles

RT ENGINE FWD LOWER YOKE CRACKED. R&R RT ENGINE FWD LOWER YOKE IAW EO EM-54MR-386R1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,764 hrs · 28,323 cycles

SERVICE DOOR SWING ARM COVER EMERGENCY LIGHT INOP. R&R SERVICE DOOR SWING ARM EMERGENCY LIGHT LAMP IAW AMM 33-50-09. OPC GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,356 hrs · 27,959 cycles

SERVICE DOOR EMERGENCY LIGHT 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: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,327 hrs · 27,931 cycles

SERVICE DOOR HINGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICED DOOR EXTERNAL EMERGENCY LIGHT BULB IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A OPC GOOD END.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,627 hrs · 27,240 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A , OPC GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,094 hrs · 26,728 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD AT THIS TIME.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 31,036 hrs · 26,667 cycles

WHILE PERFORMING PS-1 INSPECTION FOUND NR 1 FLOOR PROXIMITY STRIP LIGHT INOPERTIVE AND SERVICE DOOR SHROUD EXIT MARKER LIGHT INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-50-11. OPS CHECK GOOD.

Part: HOLDER — DAMAGED (FLASHLIGHT) · airframe 30,919 hrs · 26,553 cycles

CAPTAINS EMER FLASHLIGHT HOLDER IS DAMAGED. R & R CAPTAINS EMER FLASHLIGHT HOLDER IAW AMM 33-50-16.

Part: FLASHLIGHT — WEAK (COCKPIT) · airframe 30,919 hrs · 26,553 cycles

CAPTAINS & FIRST OFFICER EMER FLASHLIGHTS ARE WEAK. R & R CAPTAINS & FIRST OFFICERS EMER FLASHLIGHTS IAW AMM 33-50-16 STEP 3 H 4 & 3 I 1 & 2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,724 hrs · 26,363 cycles

THE CREW REPORTED THAT THE AISLE EMERGENCY LIGHTS BETWEEN ROWS 17 & 18 WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,560 hrs · 24,217 cycles

DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE ROW 1 AND ROW 2 EMERGENCY LIGHTS WERE NOT WORKING. MAINTENANCE R & R LIGHT STRIP FOR ROW 1 AND ROW 2, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — DENTED (LT WING) · airframe 28,141 hrs · 23,889 cycles

AIRCRAFT ARRIVED FOR IMBV INSPECTION WITH A DEFERRAL FOR DAMAGE TO THE LOWER OTBD SIDE OF LT WING. ACFT WAS REMOVED FROM SERVICE & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR IAW ERS-EM-57MR-270. REPAIR MATERIALS, DOUBLER 2024-T3 .063.

Part: FITTING — CRACKED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

DURING IMBV INSPECTION, QA FOUND FRAME 65 SHEAR CLIP CRACKED BETWEEN STRINGERS 7L - 9L. ACFT WAS REMOVED FROM SERVICE & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-1073. REPAIR MATERIALS SHEAR CLIP PN 140-04096-605 & 140-04096-603.

Part: SLEEVE — CRACKED (HYDRAULIC LINE) · airframe 28,141 hrs · 23,889 cycles

LEFT MLG NR 1 & 2 BRAKE HYD HOSES HAVE CRACKED CHAFE PROTECTION SLEEVES. R & R LT MLG NR 1 & 2 BRAKE HYD HOSES IAW AMM 32-49-03, CMM 32-10-01 & ETN-EM-32-222.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

INTERNAL SKIN DOUBLER IS CORRODED BETWEEN FRAMES 61 - 62, STRINGERS 20L - 21L. R & R INTERNAL SKIN DOUBLER IAW SRM 51-40-02 & SRM 51-20-01. SEE TURNOVER FOR DETAILS.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

INTERNAL SKIN DOUBLER IS CORRODED BETWEEN FRAMES 62 - 62A, STRINGERS 19L - 20L. R & R INTERNAL SKIN DOUBLER IAW SRM 51-40-02 & SRM 51-20-01. SEE TURNOVER FOR DETAILS.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

APU FIREWALL CRACKED INSIDE 312 AR ABOVE FIRE EXTINGUISHER LINE AT TOP FASTENER. REPAIRED APU FIREWALL CRACK IAW EO EM-53AD-1883 PART C.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

LAVATORY RT FLOORBOARD SUPPORT CORRODED AT AFT END. R & R LAVATORY RT FLOORBOARD SUPPORT IAW SRM 51-20-01 & 51-40-02.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

APU FIREWALL CRACKED AT UPPER LT MOUNTING POINT ON FRAME 81. REPAIRED APU FIREWALL CRACK IAW EO EM-53AD-1883 PART C.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

PASSENGER DOOR ENTRANCE FWD FLOORBOARD SUPPORT HAS CORROSION. R & R PAX DOOR ENTRANCE FWD FLOORBOARD SUPPORT IAW SRM 51-40-02.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

INTERNAL SKIN DOUBLER IS CORRODED BETWEEN FRAMES 61 - 62, STRINGERS 19L - 20L. R & R INTERNAL SKIN DOUBLER IAW SRM 51-40-02 & SRM 51-20-01. SEE TURNOVER FOR DETAILS.

Part: PANEL — CRACKED (CABIN) · airframe 28,141 hrs · 23,889 cycles

RIGHT EMER EXIT, EMER LIGHT PANEL ON PSU, CRACKED AT LATCH. REPAIRED RT EMER EXIT, EMER LIGHT PANEL ON PSU, AT LATCH IAW AMM 25-00-00 & ETN-GN-25-068R2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

LAVATORY RIGHT FLOORBEAM CORRODED AROUND NUTPLATES. R & R LAVATORY RT FLOORBEAM IAW SRM 51-20-01 & 51-40-02. SEE TURNOVER FOR DETAILS.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 28,141 hrs · 23,889 cycles

EMERGENCY LIGHTS BATTERY NR 1 WILL NOT ILLUMINATE LIGHTS. R & R EMER LIGHTS NR 1 BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

GALLEY AREA RT FLOORBEAM HAS CORROSION AT AFT NUTPLATE. REPAIRED GALLEY AREA RT FLOORBEAM AT AFT NUTPLATE IAW SRM 53-21-10 REPAIR 6.

Part: REINFORCEMENT — CRACKED (PAX DOOR) · airframe 28,141 hrs · 23,889 cycles

PASSENGER DOOR REINFORCEMENT IS CRACKED AT FRAME 20 & STRINGER 3L. REMOVED & INSTALLED NEW SERVICEABLE PAX DOOR REINFORCEMENT IAW SRM 51-40-02, SRM 51-20-01 & AMM 20-10-01. SEE TURNOVER FOR DETAILS.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 28,141 hrs · 23,889 cycles

EMERGENCY LIGHTS BATTERY NR 3 WILL NOT ILLUMINATE LIGHTS. R & R EMER LIGHT NR 3 BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

CRACK AROUND RIVET ON RT FRAME 7. INSTALLED BUSHING ON FRAME 77 IAW ERS-EM-5300-1060. SEE TASK & WIP ENTRIES FOR DETAILS.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

INTERNAL SKIN DOUBLER IS CORRODED BETWEEN FRAMES 62 - 62A, STRINGERS 20L - 21L. R & R INTERNAL SKIN DOUBLER BETWEEN FRAMES 62 - 62A, STRINGERS 20L - 21L IAW SRM 51-40-02 & SRM 51-20-01. SEE TURNOVER FOR DETAILS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

CRACK AROUND RIVET ON FRAME 75 BETWEEN STRINGERS 2R - 3R. INSTALLED BUSHING IAW ERS-EM-5300-1060. SEE TASK & WIP ENTRIES FOR DETAILS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,141 hrs · 23,889 cycles

CRACK AROUND RIVET ON RT FRAME 79. INSTALLED BUSHING ON RT FRAME 79 IAW ERS-EM-5300-1060. SEE TASK & WIP ENTRIES FOR DETAILS.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 25,987 hrs · 22,057 cycles

AT CRUISE FLT 370, WE RECEIVED A LAVATORY SMOKE EICAS MSG. AOM PROCEDURES FOLLOWED CB'S E11 & E12 PULLED. SMOKE MSG WENT AWAY, WE CONTINUED TO MONITOR LAVATORY. INSPECTED LAVATORY FOR EVIDENCE OF SMOKE OR DAMAGE, NO DEFECTS NOTED. DEFERRED IAW MEL 26-2. PERFORMED OPERATIONS CHECK OF LAVATORY SMOKE DETECTOR IAW AMM 26-14-00, NO DEFECTS OR FAULTS NOTED. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,586 hrs · 21,743 cycles

EMERGENCY EXIT LIGHT ABOVE FLIGHT ATTENDANT HEADREST INOPERATIVE. R & R NR 1 EMERGENCY LIGHT INVERTER. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 25,549 hrs · 21,714 cycles

CAPTAIN`S FLASHLIGHT HOLDER BROKEN. R & R CAPTAIN`S FLASHLIGHT CRADLE IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — LOOSE (CABIN) · airframe 25,133 hrs · 21,396 cycles

AFT CABIN FLASHLIGHT IS LOOSE. R & R EMERGENCY FLASHLIGHT AFT CABIN IAW EMB AMM 33-50-16.

Part: SCREW — LOOSE (LIGHT TERMINAL) · airframe 24,712 hrs · 21,060 cycles

COCKPIT CEILING EMERGENCY LIGHT INOPERATIVE. R & R COCKPIT CEILING EMERGENCY LT LAMP IAW AMM TASKS 33-50-05-000-801-A/33-50-05-400-801-A NO FIX. FOUND GROUND WIRE TERMINAL SCREW LOOSE. RESECURED TERMINAL SCREW IN REF WITH AMM TASK 33-50-05-400-802-A. OPS CHECK GOOD END.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,421 hrs · 20,807 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R NR 4 BATTERY AND CHARGER IAW WC 33-700-19, OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: BATTERY — DEFECTIVE · airframe 23,763 hrs · 20,300 cycles

DURING MX INSPECTION FOUND THE BATTERY AND BATTERY CHARGER WOULD NOT CHARGE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE BATTERY PN 2013-1A, SN 101808, AND THE BATTERY CHARGER, PN 11-0049, SN 20527. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,795 hrs · 20,329 cycles

DURING B INSPECTION, FOUND THE LAST 3 FLOOR EMERGENCY LIGHTS INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R WITH NEW AND SERVICEABLE NR 4 BATTERY AND POWER SUPPLY IAW AMM 33-50-04. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: TAPE — DEPARTED (WINDSHIELD) · airframe 22,928 hrs · 19,649 cycles

ON FLIGHT 4326 THE CREW REPORTED AT CRUISE AT 24,000 FT AN APPROXIMATELY 3 FOOT LONG PIECE OF SPEED TAPE ON THE CAPTAIN'S WINDSHIELD COMPLETELY DETACHED FROM THE AIRCRAFT. IMMEDIATELY AFTER THE TAPE DETACHED A PLASTIC LIKE ODOR WAS DETECTED IN THE COCKPIT. THE ODOR LASTED FOR APPROXIMATELY 5 MINUTES ALL ENGINE INDICATION APPEARED NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. SPEED TAPE REPLACED. THE AIRCRAFT TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,576 hrs · 19,376 cycles

DURING B INSPECTION FOUND THE FURTHEST FORWARD FLOOR STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY STRIP IAW EMB AMM 33-50-12-000-801-A AND 33-50-12-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,564 hrs · 19,364 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR 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: SIGN — INOPERATIVE (CABIN) · airframe 22,520 hrs · 19,330 cycles

DURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY EXIT SIGN IAW EMB AMM 33-50-14-000-801-A AND 33-50-14-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 20,884 hrs · 17,994 cycles

ON FLIGHT 4305 THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT’S JUMPSEAT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEATED CONNECTOR IAW EMB145 AMM 33-50-14. NO PARTS REMOVED OR REPLACED. PERFORMED OPERATIONAL TEST AND THE CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — FAULTY (LAVATORY) · airframe 20,670 hrs · 17,831 cycles

ON FLIGHT 4335 THE CREW REPORTED WHILE AT THE GATE AFTER THE PLANE LANDED THEY RECEIVED A LAV SMOKE WARNING. NO EVIDENCE OF FIRE OR SMOKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAV SMOKE SENSOR IAW EMB 145 AMM 26-14-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,524 hrs · 17,712 cycles

DURING B-INSPECTION FOUND THE 2ND FLOOR STRIP EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE 2ND FLOOR EMERGENCY STRIP LIGHT ASSEMBLY IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SCREW — LOOSE (SMOKE GOGGLES) · airframe 19,467 hrs · 16,958 cycles

DURING MAINTENACE BASE VIST FOUND THE STRAP THAT SECURES THE FIRST OFFICER’S SMOKE GOGGLES TO AIRCRAFT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED SCREW FOR STRAP ON FIRST OFFICER'S SMOKE GOGGLES HOLDER IAW EMB-145 AMM 20-10-07. THE OPERATIONAL CHECK WAS GOOD.

Part: DISPLAY — ODOR (COCKPIT) · airframe 19,389 hrs · 16,892 cycles

ON FLIGHT 4143 THE CREW REPORTED THAT IN CRUISE NOTICED A SMOKE AND ELECTRICAL ODOR IN THE COCKPIT AND FORWARD CABIN. THE CREW ELECTED TO DIVERT TO DTW. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S PFD UNIT IAW EMB145 AMM 34-22-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DIMMER — DEFECTIVE (COCKPIT) · airframe 17,216 hrs · 15,346 cycles

FOR FLIGHT 4029 WHILE ON THE GROUND A BURNING ODOR WAS NOTICED IN THE COCKPIT. FOUND THAT AN OVERHEAD LIGHTING CIRCUIT BREAKER HAD POPPED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED OVERHEAD PANEL DIMMER NR 2 IAW EMB 145 AMM 33-12-01. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-12-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 17,179 hrs · 15,319 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE FORWARD GALLEY FLASHLIGHT ASSEMBLY DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLASHLIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (STABILIZER) · airframe 17,105 hrs · 15,263 cycles

ON FLIGHT 3699 THE CREW REPORTED THAT DURING THE APPROACH IN ICING CONDITIONS RECEIVED A STAB ANTI-ICE FAIL MESSAGE ON EICAS FOLLOWED BY ICE COND NO ANTI-ICE WARNING MESSAGE. THE CREW PERFORMED AIRCRAFT OPERATIONS MANUAL PROCEDURE WITH NO POSITIVE EFFECT. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED TROUBLE SHOOTING OF THE STABILIZER ANTI-ICE SYSTEM IAW FIM 30-12-00 AND OPERATIONS CHECKED ANTI-ICE SYS IAW AMM 30-00-00. FOUND CONDITION TO BE TRANSITORY. THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — ODOR (CABIN) · airframe 17,030 hrs · 15,203 cycles

ON FLIGHT 4038 THE CREW NOTICED A SMOKE ODOR OF AN UNIDENTIFIED NATURE IN THE FORWARD CABIN IN THE AREA OF THE MAIN CABIN ENTRY DOOR. THE CAPTAIN ELECTED TO RETURN TO ORD. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ODOR TO BE COMING FROM FLIGHT ATTENDANT FLASHLIGHT. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW AMM 33-50-16 THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUT — LOW (MLG) · airframe 15,884 hrs · 14,306 cycles

ON FLIGHT 3248 ON APPROACH THE CREW REPORTED AN EXCESSIVE RUBBING NOISE FROM THE MAIN GEAR AREA DURING RETRACTION. THE CREW DECLARED AN EMERGENCY WHEN AMA TOWER ADVISED OF POSSIBLE BLOWN TIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION OF MAIN LANDING GEAR AREAS. NO DISCREPANCY NOTED. LUBED GEAR IAW EMB AMM 32-34-00 AND SERVICED STRUTS IAW AMM 32-10-02 AND PERFORMED GEAR SWINGS MULTIPLE TIMES WITH NO DEFECTS NOTED AND PASSED FUNCTIONAL CHECK FLIGHT. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CRACKED (LT WING) · airframe 14,217 hrs · 12,983 cycles

DURING MAINTENANCE CHECK FOUND THE LEFT OVERWING PANEL LOWER MOUNT BRACKET NUMBER 2 CRACKED. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE. REMOVED AND REPLACED NEW LEFT OVERWING PANEL LOWER MOUNT BRACKET NUMBER 2 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 14,217 hrs · 12,983 cycles

DURING MAINTENANCE CHECK FOUND THE RIGHT OVERWING PANEL AFT BRACKET SKIN CRACKED. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE. REPAIRED THE RIGHT OVERWING PANEL AFT BRACKET IAW SRM 53-23-12 AND 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CRACKED (LT WING) · airframe 14,217 hrs · 12,983 cycles

DURING MAINTENANCE CHECK FOUND THE LEFT PANEL LOWER MOUNT BRACKET NUMBER 3 CRACKED. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE. REMOVED AND REPLACED NEW LEFT OVERWING PANEL LOWER MOUNT BRACKET NUMBER 3. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 9,226 hrs · 8,772 cycles

DURING IMBV INSPECTION, THE CARGO DOOR CUT OUT CENTER SILL WAS FOUND TO BE CORRODED. REPLACED THE CARGO DOOR CUT OUT CENTER SILL PER EMBRAER SRM (SRM-145/1142 REV 38) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (BS 236) · airframe 9,225 hrs · 8,772 cycles

DURING MBV INSPECTION, THE FRAME AT FS 236.5 WAS FOUND TO BE CORRODED. REPAIRED FRAME AT FS 236.5 PER SAAB SRM (72LKS 3079 REV 49) CHAPTER 53-70-30. AIRCRAFT RETURNED TO SERVICE.

Part: BOLT — BROKEN (BEARING CAP)

NEW BOLT BROKEN DURING TORQUE. TORQUE VALUE NEVER OBTAINED BEFORE THE BOLT BROKE. THIS BOLT HOLDS THE BEARING CAP IN PLACE THAT HOLDS THE MAIN LANDING GEAR ON THE AIRCRAFT. (K)

Part: INDICATOR — INOPERATIVE (ALTIMETER)

STANDBY ALTIMETER GAUGE INOP AFTER TO. A/C RETURNED TO FIELD. NO OVERWEIGHT LANDING.

Part: BEAM — CORRODED (CABIN)

DURING MBV INSPECTION FOUND OMEGA BEAM CORRODED AT FRAME 20. REPAIRED OMEGA BEAM AT FRAME 20 BY CUTTING OUT DAMAGE AND INSTALLING A DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SKIN — BIRD STRIKE (FUSELAGE)

SAW - DURING A BIRDSTRIKE, MAINTENANCE FOUND DAMAGE/DENT TO FUSELAGE SKIN BETWEEN STRINGERS 01L AND 04L AND FRAMES 11 AND 13 OVER COCKPIT LEFT SIDE FROM BIRDSTRIKE. REMOVED AND INSTALLED NEW UPPER SKIN IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — MALFUNCTIONED (E/E BAY)

DURING DESCENT, CREW REPORTED FAILURE OF BOTH PITCH TRIM SYSTEMS. AUTO-PILOT DID NOT DISCONNECT. CREW FOLLOWED AOM PROCEDURES AND RECOVERED BACK UP TRIM. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETUREND TO SERVICE. (SW21200501219)

Part: CHARGER — DISCHARGED (EMERGENCY LIGHT)

ROC - FLT 4399 - CREW FOND THE FORWARD EMERGENCY LIGHTS INOPERATIVE ON THE PREFLIGHT INSPECTION. REPLACED NR 1 AND PACK NR 2 EMERGENCY BATTERY PACK AND NR 2 EMERGENCY BATTERY CHARGER ASSEMBLY IAW EMB 145MM 33-50-04. PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM WITH NO DISCREPANCIES NOTED. A/C RETURNED TO SERVICE. (M)