N697AB

Part: WINDSHIELD WIPER — BENT (ZONE 200) · airframe 42,772 hrs · 37,068 cycles

F/O WINDSHIELD WIPER GOT STUCK IN THE MIDDLE OF THE WINDSHIELD AFTER TAKEOFF. APPROX 170 KNOTS WIPER WAS FLOPPING ON WINDSHIELD. FACT 06FEB25 14:18 MHT R&R ARM BLADE ASSEMBLY IAW AMM 30-41-03. OPS CHECK IAW AMM 30-41-00. A/C OK FOR SERVICE AT THIS TIME

Part: SUPPORT FITTING — CORRODED (ZONE 900) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F001138 LAV INTERNAL POTABLE WATER FITTING SUPPORT CORRODED. RAR FITTING IAW SRM51-40-02

Part: SKIN — CRACKED (ZONE 800) · airframe 42,384 hrs · 36,658 cycles

F003151 CARGO DOOR INNER SKIN CRACKED AT LWR FWD END AT AFT EDGE. REPAIRED IAW EO 1-52-24-0658

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F001659 RH LWR SEAT TRACK #2 CORRODED. R & R SEAT TRACK IAW AMM 53-01-06

Part: HINGE — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F001692 LH ELEVATOR IB HINGE, IB RIB CORRODED. RAR RIB IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 42,384 hrs · 36,658 cycles

F001837 SHEAR CLIP CRACKED AT FR65 STR16L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F001658 LH LWR SEAT TRACK #2 CORRODED. RAR SEAT TRACK IAW AMM 53-01-06

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F001653 LH UPPER SEAT TRACK #2 CORRODED. RAR SEAT TRACK IAW AMM 53-01-06

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,384 hrs · 36,658 cycles

F001598 LH IB SEAT TRACK OMEGA BEAM CRACKED AT FR23. REPAIRED IAW EO1-53-24-0657

Part: BUSHING — WORN (ZONE 500) · airframe 42,384 hrs · 36,658 cycles

F001346 LH AILERON DAMPER FITTING BUSHING HOLES WORN. RAR DAMPER FITTING IAW SRM 51-40-02

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F001602 RH SERVICE DOOR AFT SILL CORRODED. RAR AFT SILL IAW SRM 51-40-02

Part: DOOR SILL — CORRODED (ZONE 200) · airframe 42,384 hrs · 36,658 cycles

F001603 RH SERVICE DOOR CTR SILL CORRODED AROUND NUTPLATE HOLES. REPAIRED IAW EO1-52-24-0652

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F001436 RH LWR SEAT TRACK #4 CORRODED. RAR TRACK IAW AMM 53-01-06

Part: SUPPORT — CORRODED · airframe 42,384 hrs · 36,658 cycles

F001606 LH OB SILL #1 CORRODED. RAR SILL IAW SRM 51-40-02

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F001601 RH GALLEY COSSBEAM PROFIE ANGLE CORRODED AT FR23. RAR ANGLE IAW SRM 51-40-02

Part: BUSHING — WORN (ZONE 600) · airframe 42,384 hrs · 36,658 cycles

F001347 RH AILERON DAMPER FITTING HAT BUSHING HOLE WORN. RAR FITTING IAW SRM51-40-02

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 42,384 hrs · 36,658 cycles

F000967 2 CRACKS ON SHEAR CLIP AT FR62 BTW STR7-8L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 900) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F001131 LAV FLOOR SILL CORRODED ON AFT END. RAR SILL IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F001163 LH FLOOR SILL #7 CORRODED AFT OF FR53. RAR SILL IAW SRM 51-40-02

Part: TORQUE BOX — DAMAGED (ZONE 600) · airframe 42,384 hrs · 36,658 cycles

F001233 RH WING TQ BOX OB FWD LOCATION HAS OVERSIZED J-BOLT HOLE. REPAIRED IAW EO1-57-24-0639

Part: PROFILE — CORRODED (ZONE 800) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F000830 CARGO DOOR LWR IB PROFILE CORRODED AT NUTPLATE HOLES. RAR PROFILE IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F000935 CARGO DOOR CUTOUT LWR FLOOR SILL BTW FR65-68 CORRODED. RAR FLOOR SILL IAW SRM 51-40-02

Part: WEB — CORRODED (ZONE 800) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F000854 CARGO DOOR LWR INTERNAL WEBBING CORRODED AROUND NUTPLATES. REPAIRED IAW EO 1-53-24-0653

Part: FRAME — CRACKED (ZONE 100) · airframe 42,384 hrs · 36,658 cycles

F000930 FR72 CRACKED AT BTW STR16-17R. RAR FRAME SECTION IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 423,884 hrs · 36,658 cycles

F000933 RH CARGO FLOOR SIL COORODED AT FR68-71 BTW STR17-18R. RAR FLOOR SIL IAW SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 42,384 hrs · 36,658 cycles

F000931 SHEAR CLIP CRACKED AT FR72 BTW STR17-18L. RAR SHEAR CLIP IAW SRM 51-40-02

Part: WEB — GOUGED (CARGO DOOR) · airframe 42,384 hrs · 36,658 cycles

F000856 CARGO DOOR INTERNAL LWR WEBBING GOUGED. REPAIRED IAW EO 1-52-24-0656

Part: PROFILE — CORRODED (ZONE 800) · corrosion level 2 · airframe 42,384 hrs · 36,658 cycles

F000815 CARGO DOOR UPPER IB PROFILE CORRODED AT NUTPLATE HOLES. RAR PROFILE IAW SRM 51-40-02

Part: RIB — CRACKED (ZONE 500) · airframe 42,384 hrs · 36,658 cycles

E060707 LH WING RIB 21 CRACKED. REPAIRED IAW EO 1-57-24-0651

Part: LIGHT — INOPERATIVE (SD) · airframe 42,057 hrs · 36,278 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: LIGHT — INOPERATIVE (CABIN) · airframe 41,922 hrs · 36,118 cycles

AISLE EMERGENCY EXIT SIGN BY GALLEY AND COCKPIT STEP EMERGENCY EXIT SIGN INOP-C/A-RAR #1 DC/AC INVERTER IAW EMB 145 AMM 33-50-11. OPC GOOD

Part: NONE — NONE · airframe 40,996 hrs · 35,057 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. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: NONE — NONE · airframe 40,872 hrs · 34,921 cycles

SEVICE 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. OPS CHECK GOOD. NO DEFECTS NOTED. END.

Part: CRADLE — BROKEN (AFT FLASHLIGHT) · airframe 40,354 hrs · 34,341 cycles

AFT CABIN EMERGENCY FLASHLIGHT BRACKET BROKEN MEL 25-32 - AUTH# 070350M-C REF LOG PAGE 4766000 ITEM: 1 .-C/A-RAR AFT CABIN EMERGENCY FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16 OPC GOOD. MEL 25-32 AUTH# 070350M-C RESTORED

Part: BRACKET — CRACKED (AFT FLASHLIGHT) · airframe 40,333 hrs · 34,317 cycles

AFT CABIN EMERGENCY FLASHLIGHT BRACKET DAMAGED-C/A-DEFERRED AFT CABIN EMERGENCY FLASHLIGHT PER MEL 25-32 AUTH# 070350M-C. "M" PROCEDURES COMPLIED WITH.

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 40,249 hrs · 34,232 cycles

AFT CABIN EMEREGNCY FLASHLIGHT MISSING-C/A-INSTALLED EMERGENCY FLASHLIGHT IN AFT CABIN AS PER EMB 145 AMM 33-50-16. OPC GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 39,512 hrs · 33,460 cycles

REPAIR POSITION FWD FA CREW MEMBER EMERGENCY FLASHLIGHTS AND HOLDERS FWD FS FLASHLIGHT MISSING PLACARDED BY: CREW. RESTORATION OF MEL ITEMS REVIEW THE MEL AND ENSURE APPROPRIATE MAINTENANCE ACTIONS ARE TAKEN TO RESTORE THE ITEM/SYSTEM CONDITIONS AND LIMITATIONS THAT WERE REQUIRED BY THE MEL DURING DEFERRAL. COMPLY WITH PROCEDURES IN MEL MANUAL 1-06 INCLUDING NOTIFICATION TO M ENTER FACT INFORMATION INTO SABRE FMR RECORD PER GPM 04-00 AND 16-00 MOC. C/A: R & R FWD FA EMERGENCY FLASHLIGHT ASSEMBLY, IAW AMM 33-50-16. OPERATIONS CHECK GOOD.

Part: FLASHLIGHT — MISSING (FWD CABIN) · airframe 39,509 hrs · 33,458 cycles

FWD FA FLASHLIGHT MISSING. C/A: FLIGHT CREW PLACARDED FA FLASHLIGHT MEL B AUTH 010390, C REF 25-53 MOC 628765.

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 39,367 hrs · 33,319 cycles

MEL 2553 - AUTH NR 120201-C AFT CABIN FLASHLIGHT MISSING. C/A: R & R AFT CABIN FLASHLIGHT ASSEMBLY, IAW EMB-145 AMM 33-50-16. OPERATIONS CHECK GOOD. MEL 2553 RESTORED.

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 39,350 hrs · 33,298 cycles

FA EMERGENCY FLASHLIGHT MISSING IN BACK OF AIRCRAFT. C/A: DEFERRED AFT EMRGENCY FLASHLIGHT, PER MEL 25-53. C/W MEL PROCEDURE.

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 39,277 hrs · 33,231 cycles

AFT F/A EMERGENCY FLASHLIGHT MISSING MEL 25-53 AUTH NR 120003. C/A: INSTALLED AFT F/A EMERGENCY FLASHLIGHT AND CHARGER, IAW EMB AMM 33-15-16. OPERATIONS CHECK GOOD, MEL ITEM RESTORED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,442 hrs · 32,366 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10. OPC GOOD.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 37,742 hrs · 31,762 cycles

DURING HMBV INSPECTION, QC FOUND FR 65 SHEAR CLIP AT CARGO DOOR LOWER CUTOUT CORRODED-C/A-PERFORMED PERMANENT REPAIR ON FR 65 SHEAR CLIP AT CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 53-31-04 FIGURE 212 AND ETN-EM-53-272. REPAIR MATERIALS: P/N 145-25175-001

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-68) · airframe 37,742 hrs · 31,762 cycles

DURING HMBV INSPECTION, QC FOUND THE CARGO DOOR CUTOUT LOWER FLOOR SILL BETWEEN FR 65 AND FR 68 CORRODED-C/A-REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL BETWEEN FR 65 AND FR 68 IAW EMB 145 SRM 51-40-02. REPAIR P/N 145-25480-603

Part: SKIN — CHAFED (FRAMES 67-68) · airframe 37,742 hrs · 31,762 cycles

DURING HMBV INSPECTION, QC FOUND THE FUSELAGE SKIN UNDER PYLON PANEL 424DB CHAFED.-C/A-PERFORMED PERMANENT REPAIR ON FUSELAGE SKIN UNDER PYLON PANEL 424DB IAW EMB 145 SRM 53-31-01 ITEM 12 FIGURE 220 SHEET 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 29) · airframe 37,742 hrs · 31,762 cycles

LH OMEGA BEAM CORRODED FWD OF CROSSBEAM AT FR 29-C/A-REPAIRED LH OMEGA BEAM FWD OF CROSSBEAM AT FR 29 IAW ENVOY ERS-EM-53MR-3977.

Part: SKIN — CRACKED (FRAME 75) · airframe 37,742 hrs · 31,762 cycles

RH AFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R.-C/A-INSTALLED REPAIR DOUBLER, FILLER, "L" ANGLE AND SHIM FOR REPAIR OF RH AFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R IAW EMB 145 SRM 53-31-01, ITEM 11.

Part: PROFILE — DAMAGED (EMERGENCY LIGHT) · airframe 37,462 hrs · 31,515 cycles

MULTIPLE REMOVED EMERGENCY LIGHT STRIP PROFILES DAMAGED.-C/A-REPLACED ALL DAMAGED EMERGENCY LIGHT STRIP PROFILES AS REQUIRED. REF NRWC 697-MQT-04283 FOR REINSTALLATION.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 37,462 hrs · 31,515 cycles

EMERGENCY LIGHT CONNECTOR AT FLOOR PANEL 251DF IS DAMAGED.-C/A-RAR'D EMERGENCY LIGHT CONNECTOR AT FLOOR PANEL 251DF IAW SWPM 20-21-00.

Part: FLASHLIGHT — ODOR (COCKPIT) · airframe 36,927 hrs · 31,014 cycles

SUPPLEMENTAL COCKPIT SMOKE FUMES @FL 320 STRONG SMELL OF BURNT RUBBER. C/A-RAN BOTH PACKS WITH CREW NO SMELLS NOTED CREW SAID IT WAS NOT A PACK ISSUE. FOUND FOS FLASHLIGHT INOP AND EMITTING ELECTRICAL SMELL SWAPPED FO WITH AFT FLASHLIGHT DEFERRED AFT FLASHLIGHT AS MISSING REF MEL 25-53 AUTH 061053-C. REMOVED AND REPLACED FO F/ LIGHT IAW AMM CH 33-50-16. OPS CHK GOOD, NO FAULTS NOTED AT THIS TIME. MEL RESTORED.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,374 hrs · 30,523 cycles

RIGHT OVERWING EXIT MARKER INOP. REMOVED & REPLACED #5 INVERTER, RIGHT OVERWING EXIT MARKER OPERATES OK IAW EMB AMM 33-50-11.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 36,280 hrs · 30,456 cycles

DIFFICULTY OPENING MAIN CABIN DOOR. C/A-LUBED MAIN DOOR FRAME ROLLERS IAW MM 53-21-02.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 36,235 hrs · 30,411 cycles

SUPPLEMENTAL AFT FA FLASHLIGHT INOP. C/A-FLIGHT CREW PLACARDED AFT FLIGHT ATTENDENT FLASHLIGHT // TEMP INSTALLED AUTH 030706-C REF 25-53 MOC 630997. REMOVED AND REPLACED AFT FA FLASHLIGHT IAW AMM 33-50-16. OPS CHECK GOOD MEL RESTORED.

Part: CONNECTOR — DIRTY (CABIN) · airframe 36,217 hrs · 30,391 cycles

WHILE PERFORMING W/C 33-700-17 EMERGENCY LIGHTING SYS OPS CHECK FOUND RT OVER WING EXIT LIGHT INOP. C/A-CLEANED ELECTRICAL CONNECTORS AT NR 3 EMERGENCY LIGHTING POWER SUPPLY AND NR 4 AND NR 5 EMERGENCY LIGHTING AC/DC INVERTERS IAW AMM 33-50-04 AND 33-50-11. OPS CHECK GOOD AT THIS TIME

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,217 hrs · 30,391 cycles

OVERHEAD EMERGENCY LIGHT NR 3 FROM FWD IN CEILING PANEL INOP. C/A-REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT NR 3 FROM FWD BULB IAW AMM 33-50-08 OPS CHECK GOOD.

Part: OXYGEN MASK — DISCONNECTED (COCKPIT) · airframe 35,661 hrs · 29,892 cycles

OBSERVER MASK LEAKING O2 IN FLIGHT. CREW O2 840 PSI AT 23 C -C/A-INSPECTED FOUND TO BE OBSERVER OXYGEN MASK DISCONNECTED MASK AND RESTOWED REF 4389396 ITEM 1. SERVICED CREW O2 IAW EMB 145 AMM 12-14-00 OK FOR SERVICE

Part: CONNECTOR — LOOSE (BLEED VALVE) · airframe 35,640 hrs · 29,874 cycles

BLD 1 LEAK IN FLIGHT QRH PROCEDURES COMPLIED WITH MESSAGE EXTINGUISHED.-C/A-INSPECTED PACK 1 FOR LOOSE DUCTING/CLAMPS. NO DEFECTS NOTED IAW EMB 145 AMM 21-20-04. FOUND #1 ENG BLEED VALVE CONNECTOR LOOSE. RESECURED CONNECTOR IAW EMB 145 AMM 36-11-05. NO DEFETCS NOTED IN #1 ENG. COMPARTMENT. RESECURED DUCT ON #1 PACK PERFORMED OPERATIONAL TEST OF BLEED SYSTEMS NO BLEED LEAK MESSAGE ON EICAS IAW AMM 21-20-01 AND 36-00-00

Part: CLAMP — LEAKING (TEMP VALVE DUCT) · airframe 35,630 hrs · 29,868 cycles

ON CLIMB OUT NOTICED AIRCRAFT NOT PRESSURIZING. THAT WAS FOLLOWED BY BLD 1 VLV CLSD & PACK 1 VLV CLSD MSG ADVISORY. RESET THEM BUT MESSAGES KEPT COMIMG BACK WITH RUSH OF AIR EACH TIME-C/A-REMOVED AND REPLACED COUPLING AND CLAMP ON DUAL TEMP VALVE DUCT IAW ETN-EM-21-056 OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (SEAT 12C) · airframe 35,156 hrs · 29,497 cycles

EMERGENCY LIGHT ON SEAT 12C INOP-C/A-RAR EMERG LIGHT EXIT SIGN ON SEAT 12C IAW AMM 33-50-14 OPC WAS GOOD AT THIS TIME

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 34,368 hrs · 28,872 cycles

THE FORWARD FA FLASHLIGHT WAS INOPERATIVE. INSTALLED THE FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: CRADLE — INOPERATIVE (AFT FLASHLIGHT) · airframe 33,981 hrs · 28,506 cycles

FLASHLIGHT IN BACK OF CABIN NOT CHARGING. REMOVED AND REPLACED THE FLASHLIGHT CRADLE IAW AMM 33-50-16, OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 33,117 hrs · 27,716 cycles

FA FOWARD FLASHLIGHT INOP.-C/A-REMOVVED AND REPLACED FLASHLIGHT IAW AMM 33-50-16. OPS CK GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAME 60) · airframe 32,746 hrs · 27,402 cycles

LEFT OMEGA BEAM HAS CORROSION AROUND NUTPLATE HOLE AT FRAME 60 AND Y-479. REPAIRED THE OMEGA BEAM IAW SRM 53-24-10.

Part: FLOOR SUPPORT — CORRODED (FRAME 60) · airframe 32,746 hrs · 27,402 cycles

RIGHT OMEGA BEAM HAS CORROSION AROUND NUTPLATE HOLE AT FRAME 60 AND Y-479. REPAIRED THE OMEGA BEAM IAW SRM 53-24-10

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · airframe 32,746 hrs · 27,402 cycles

LEFT OMEGA BEAM HAS CORROSION AROUND NUTPLATE HOLE AT FRAME 59 AND Y-479. REPAIRED THE OMEGA BEAM IAW SRM 53-24-10.

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 32,746 hrs · 27,402 cycles

CRACKED SHEAR TIE AT FRAME 67, STRINGERS 6 - 7L. REMOVED AND THE SHEAR TIE IAW SRM 51-40-02.

Part: SKIN — DAMAGED (FRAME 20-22) · airframe 32,746 hrs · 27,402 cycles

SEVERAL HOLES IN FUSELAGE SKIN ARE ELONGATED WHERE SERVICE DOOR OR THRESHOLD ATTACHES TO SKIN STRINGER 16R, FRAMES 20 - 22. REAMED DISCREPANT HOLES TO REMOVE DAMAGE AND PREP FOR INSTALLATION OF FREEZ PLUG BUSHING.

Part: SHEAR TIE — CRACKED (FRAME 66) · airframe 32,746 hrs · 27,402 cycles

CRACKED SHEAR TIE AT FRAME 66 STRINGERS 6 - 7. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: THRESHOLD — CORRODED (FRAMES 20-22) · airframe 32,746 hrs · 27,402 cycles

CORROSION AROUND THREE NUTPLATES FOR THE SERVICE DOOR THRESHOLD BETWEEN FRAMES 20 - 22. BLENDED THE CORROSION IAW SRM 51-10-03. REPLACED THE THRESHOLD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 18-23) · airframe 32,746 hrs · 27,402 cycles

CENTER OMEGA BEAM AR FR 18-23 IS CORRODED WITH 100% MATERIAL LOSS. REMOVED AND REPLACED THE OMEGA BEAM IAW SRM 51-40-02.

Part: BRACKET — CRACKED (FRAME 3) · airframe 32,746 hrs · 27,402 cycles

NOSE LANDING GEAR UP LOCK BRACKET IS CRACKED. REMOVED AND REPLACED THE LT AND RT SUPPORTS FOR NLG UPLOCK BOX IAW SRM 51-40-02 AND AMM 20-10-01

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,746 hrs · 27,402 cycles

1ST EMERGENCY LIGHT STRIP WIRES BROKEN AT STRIP. NR 1 EMERGENCY LIGHT OPS TESTED IAW AMM 33-50-12 AND ETN EM-33-058

Part: STIFFENER — CRACKED (FRAME 18) · airframe 32,746 hrs · 27,402 cycles

FRAME 18, STRINGER 3L STIFFENER CRACKED. INSTALLED A NEW STIFFENER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,450 hrs · 27,142 cycles

SERVICE DOOR EXIT EMERGENCY LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-10-000-801, AND 33-50-10-400-801. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (ROWS 8-9) · airframe 31,596 hrs · 26,484 cycles

DURING PS-1, FOUND PROXIMITY LIGHT STRIP FOR ROWS 8 AND 9 INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: CHARGER — FAILED (CABIN) · airframe 31,507 hrs · 26,397 cycles

SERVICE DOOR EMERG LT INOP. T/S PER WM 33-50-50 FOUND NR 2 EMERGENCY BATTERY AND CHARGER TO BE BAD. REMOVED AND REPLACED NR 2 BATTERY AND CHARGER IAW WC N697AB. OPC GOOD, NO DEFECTS END. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 68423

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,507 hrs · 26,397 cycles

ROW 6 3RD BACK FROM FRONT EMERG FLOOR STRIP INOP. THIS FLOOR STRIP IS NOT AND EXIT IDENTIFIER. R&R NR 3 FLOOR PROXIMITY STRIP IAW AMM 33-50-12-000-801-A AND 33-50-12-400-801-A. OPS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,457 hrs · 26,357 cycles

FWD CABIN FLOOR PROXIMITY STRIP LIGHT AND EXTERIOR FWD EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT IAW FIM 33-50-00-810-804-A FOUND NR 2 EMERGENCY BACKUP BATTERY BECAME DISCONNECTED FROM BATTERY HOLDER ASSY AND BENT BATTERY CONNECTIONS. R & R NR 2 EMERGENCY BACKUP BATTERY HOLDER ASSY AND BATTERY POWER SUPPLY IAW AMM 33-50-04.

Part: PUMP — FAILED (LT ENGINE) · airframe 31,104 hrs · 26,022 cycles

HYD 1 LOW QTY IN FLIGHT ON EICAS FOLLOWED BY E1 HDY PUMP FAIL. FOLLOWED BY HYD 1 SYSTEM FAIL. AFTER LANDING NO OUTBOARD BRAKES, NO STEERING. REMOVED AND REPLACED THE NR 1 HYDRAULIC PUMP IAW AMM 29-10-03. OPS AND LEAK CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,426 hrs · 25,430 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 29,548 hrs · 24,635 cycles

WHILE IN CRUISE WE RECEIVED HYD PUMP 1 FAIL ADVISORY, IT WAS INTERMITTENTLY, COME OFF & THEN ON, DIVERTED. R & R EDP PRESS SWITCH IAW AMM 29-10-19. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 29,488 hrs · 24,571 cycles

LOWER RT OVERWING EMER LIGHT INOPERATIVE. R & R NR 2 EMER LIGHT POWER SUPPLY. OPERATIONS CHECKED GOOD EMB AMM 33-50-04.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 29,044 hrs · 24,178 cycles

SERVICE DOOR EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED BROKEN WIRE 716-0007-20 & 716-008-20 AT SERVICE DOOR IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD IAW MM 33-50-00.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 28,980 hrs · 24,115 cycles

FIRST OFFICERS FLASHLIGHT ON & OFF SWITCH BROKE OFF. R & R FIRST OFFICERS FLASHLIGHT AS REQUIRED.

Part: DISPLAY — FAILED (COCKPIT) · airframe 28,780 hrs · 23,924 cycles

NUMBER 1 PFD FAILED, WENT BLACK, ASSOCIATED ELEC BURNING SMELL, NO VISIBLE SMOKE. R & R NR 1 PFD, DU-1, IAW AMM 34-22-01. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,648 hrs · 23,800 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EMER LIGHT LAMP IAW AMM 33-50-09. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: ENGINE — SMOKE (NR 1) · airframe 28,340 hrs · 23,516 cycles

20 MIN AFTER SHUTDOWN, NR 1 ENG SMOKING. PERFORMED SMOKE ON SHUTDOWN ETN-EM-79-015. NO PRIOR OCCURRENCE NOTED. IAW ETN NO MX REQUIRED, ACFT OK TO RETURN TO SERVICE.

Part: HOLDER — DEFECTIVE (CABIN) · airframe 27,863 hrs · 23,098 cycles

FLOOR EMER LIGHT STRIPS AT SEATS 9BC - 18BC ARE INOPERATIVE. R & R BATTERY HOLDER & BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04. OPERATIONALLY CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,856 hrs · 23,091 cycles

FRAME 75 SKIN CRACK AT FASTENER AREA BELOW STRINGER 2L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75 BELOW STRINGER 2L IAW ERS-EM-53MR-1491.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,856 hrs · 23,091 cycles

EMERGENCY LIGHT STRIP AT 9BC INOPERATIVE. REPLACED EMER LIGHT STRIP AT 9BC IAW AMM 33-51-10.

Part: CONNECTOR — MISSING (CABIN) · airframe 27,856 hrs · 23,091 cycles

EMERGENCY LIGHT STRIP NR 6, ACFT SIDE, MISSING CONNECTOR. INSTALLED CONNECTORS PN MS39029-31-229 & 48-7191 ON WIRE NUMBERS W192-8830-22 IAW SWPM 20-21-00.

Part: CONNECTOR — MISSING (CABIN) · airframe 27,856 hrs · 23,091 cycles

EMERGENCY LIGHT STRIPS NR 3 & 5 MISSING FLOOR CONNECTORS. INSTALLED CONNECTORS PN MS39029-31-229 & 48-7191 ON WIRE NRS, W192-8678-22 NR 3 & W192-8760-22 NR 5 IAW SWPM 20-21-00.

Part: WIRE — CUT (CABIN) · airframe 27,856 hrs · 23,091 cycles

WIRES AT FRAME 25, STRINGER 15L ARE CUT. REPAIRED FRAME 25 FLOOR PROXIMITY LIGHT WIRES, W192-8680-22 & W192-8681-22, IAW SWPM 20-00-03, 20-00-05, 20-21-00 & AWM 91-10-02.

Part: CONNECTOR — BROKEN (CABIN) · airframe 27,856 hrs · 23,091 cycles

FRAME 20 FLOOR PROXIMITY LIGHT WIRES BROKEN CONNECTORS. REPAIRED FRAME 20 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-21-00. FOUND DURING OPEN UP.

Part: CONNECTOR — BROKEN (CABIN) · airframe 27,856 hrs · 23,091 cycles

FOUND NR 8 FLOOR PROXIMITY LIGHT WIRES BROKEN CONNECTORS. REPLACED NR 8 FLOOR PROXIMITY LIGHT WIRES STRIP IAW AMM 33-50-12. FOUND DURING OPEN UP.

Part: WIRE — BROKEN (CABIN) · airframe 27,856 hrs · 23,091 cycles

AT FRAME NR 33, BROKEN WIRE FOR EMER LIGHT STRIP. BROKEN WIRE REPAIRED IAW SPWM 20-21-00. SEE NRTC BOW 194910 TASK 1 FOR OPERATIONS CHECK.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 27,856 hrs · 23,091 cycles

LEFT OMEGA BEAM OTBD SUPPORT IS CRACKED BETWEEN FRAME 47 - 48. REMOVED CRACKED LT OMEGA BEAM OTBD SUPPORT & INSTALLED SERVICEABLE LT OMEGA BEAM OTBD SUPPORTS BETWEEN FRAME 46 - 50 IAW SRM 53-23-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,856 hrs · 23,091 cycles

RIGHT OTBD FLOOR SUPPORT AT FRAME 31 IS CORRODED. R & R RT OTBD FLOOR SUPPORT FROM FRAME 26 - 31 IAW SRM 51-40-02.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 27,856 hrs · 23,091 cycles

CENTER AISLE CROSSBEAM BETWEEN FRAME 24 - 25 IS CORRODED. R & R CTR AISLE CROSSBEAM IAW ETN-EM-53-139 & SRM 51-40-02.

Part: STRIP — CRACKED (CABIN) · airframe 27,856 hrs · 23,091 cycles

NUMBER 1 EMER LIGHT STRIP EXTRUSION CRACKED. R & R NR 1 EMER LIGHT STRIP EXTRUSION IAW 33-50-12. SEE BOW 194910 FOR INSTALLATION & OPERATIONS CHECK.

Part: STRUCTURE — CRACKED (CABIN) · airframe 27,856 hrs · 23,091 cycles

RIGHT NR 1 FLOOR EXTRUSION CRACKED. R & R RT NR 1 FLOOR EXTRUSION IAW AMM 33-50-12.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 27,856 hrs · 23,091 cycles

RIGHT OVERWING UPPER FLANGE AFT AREA IS CRACKED. COMPLIED WITH ERS-EM-53MR-1482 RT OVERWING UPPER FLANGE REPAIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,673 hrs · 22,945 cycles

EMERGENCY FLOOR PROXIMITY STRIP NR 7 INOPERATIVE. R & R NR 7 EMER FLOOR PROXIMITY STRIP. OPERATIONS CHECKED GOOD IAW AMM 33-50-12.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 27,366 hrs · 22,655 cycles

FLASHLIGHT AT 18 BC MISSING. FLIGHT CREW PLACARDED IAW MEL 25-53.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,044 hrs · 22,402 cycles

CEILING EMER LIGHT AT ROW 7 IS INOPERATIVE. R & R IAW AMM 33-50-08. OPERATIONAL CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 26,064 hrs · 21,652 cycles

AFTER PARKING AT THE GATE & OPERATING PACKS WITH APU BLEED AIR A STRANGE ODOR ENTERED THE FLIGHT DECK, A BURNING ODOR. OPERATED APU BLEED WITH PACK SYS NR 1 & NR 1 SEPARATED FOR ABOUT 15 TO 20 MINUTES BETWEEN FULL HOT & COLD & NO SMELL STRANGE ODOR AT THIS TIME IAW AMM 21-20-00. ALSO OPERATED BOTH ENG BLEED AT 90% OF N2 WITH PACKS ON & NO ODOR AT THIS TIME IAW AMM72-00-00.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 25,350 hrs · 21,082 cycles

FLASHLIGHT BEHIND CAPTAIN`S SEAT IS INOPERATIVE. FLIGHT CREW PLACARDED IAW MEL 2553. REMOVED AND REPLACED COCKPIT FLASHLIGHT ASSY IAW EMB-145 AMM 33-50-16. OPS CHECK GOOD, MEL ITEM RESTORED.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,927 hrs · 20,732 cycles

DURING PS 2, FOUND REAR EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & BATTERY CHARGER IAW AMM 33-50-04. R & R RT EXTERIOR OVERWING EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,868 hrs · 20,673 cycles

FIRST OFFICER`S EMERGENCY FLASHLIGHT CHARGE LIGHT IS NOT LIT. R & R FIRST OFFICER`S EMERGENCY FLASHLIGHT ASSEMBLY AS REQUIRED, OPERATIONS CHECKED OK IAW CMM 25-60-11.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 24,635 hrs · 20,452 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,578 hrs · 20,399 cycles

RT FWD FUSELAGE FAIRING EMERGENCY LAMP INOPERATIVE. R & R RT FWD FAIRING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A & 33-50-10-400-801-A, NO FIX. R & R NR 2 EMERGENCY BATTERY PACK & POWER SUPPLY IAW WC 33-700-19, OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,466 hrs · 20,304 cycles

RIGHT WING FUSELAGE FRONT FAIRING LIGHT INOPERATIVE. R & R BATTERY CHARGER NR 2 IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,347 hrs · 20,212 cycles

AFT CABIN FLASHLIGHT IS INOPERATIVE. VERIFIED THAT BULB NOR BATTERY WERE AT FAULT. R & R FLASHLIGHT AS REQUIRED, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,085 hrs · 20,011 cycles

FLOOR EMERGENCY LIGHT STRIP, BY 16A, IS INOPERATIVE. R & R FLOOR EMERGENCY LIGHT STRIP 16A IAW AMM33-50-12, OPERATIONS CHECKED OK.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,949 hrs · 19,907 cycles

COCKPIT FLASHLIGHT NOT CHARGING. R & R COCKPIT FLASHLIGHT IAW EMB 145 33-51-01 AMM, OPERATIONS CHECKED GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 23,851 hrs · 19,827 cycles

DURING INSPECTION, FOUND RT OMEGA BEAM OTBD SUPPORT FLANGE CRACKED AT FRAME 47. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 53-23-02, AND 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 23,851 hrs · 19,827 cycles

DURING INSPECTION, FOUND CARGO RAMP FLOOR SUPPORT BRACKET AT FRAME 66 HAS CRACKED LOWER ATTACHMENT ANGLE. CRACK IS ONE INCH LONG. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 23,851 hrs · 19,827 cycles

DURING INSPECTION, FOUND LT FLOOR SUPPORT SPLICE CRACKED AT FRAME 23. REPLACED LH FLOOR SUPPORT SPLICE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: BRACKET — CRACKED (LEFT WING) · airframe 23,851 hrs · 19,827 cycles

DURING INSPECTION, FOUND LT WING HAS CRACKED BRACKET, FOR LATERAL WING TO FUSELAGE PANEL 195, AT OR NEAR RIB 1 ABOUT HALFWAY BETWEEN THE LEADING AND T/E OF WING. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 23,851 hrs · 19,827 cycles

DURING INSPECTION, FOUND CARGO DOOR SILL CORRODED JUST AFT OF FRAME 66. REMOVED AND REPLACED SILL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 23,851 hrs · 19,827 cycles

NR 1 AND NR 4 RT EMERGENCY LIGHTS ARE CRACKED. R & R LIGHT STRIPS IAW AMM 33-50-12.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 23,851 hrs · 19,827 cycles

NR 2 FLOOR EMERGENCY LIGHT HAS A BROKE WIRE. R & R NR 2 FLOOR EMRGENCY LIGHT STRIP IAW AMM 33-50-12, OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 11-13) · airframe 23,851 hrs · 19,827 cycles

DURING MBV INSPECTION, FOUND COCKPIT FLOOR SUPPORT CORRODED LOCATED BETWEEN FRAMES 11--13. REPAIRED IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 23,851 hrs · 19,827 cycles

NR 1 AND NR 8 LT EMERGENCY LIGHTS ARE CRACKED. REPLACED EMERGENCY LIGHTS IAW AMM 33-50-12.

Part: O-RING — INOPERATIVE (BLEED SYS) · airframe 23,441 hrs · 19,473 cycles

BLEED 2, LEAK AFTER E1 START. BLEED CONFIG WAS: APU BLEED OPEN, X BLEED OPEN, BLEED 1 & 2 CLOSED AND PACKS 1 & 2 ON PASSENGER ALSO REPORTED ELECTRICAL BURNING SMELL APPROX MID CABIN. PERFORMED LEAK CHECK OF RT FUSELAGE AIR BLEED DUCTS IAW AMM 36-00-00-700-805 R & R O-RINGS AT LOCATIONS 4 AND 20 IAW AMM 36-11-10. PERFORMED LEAK DOWN CHECK OF RT SYS AGAIN LEAK CHECK AND ALL OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,840 hrs · 18,979 cycles

DURING B-INSPECTION, FOUND THE FLOOR EMERGENCY LIGHT INOPERABLE AT THE FWD GALLEY. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FORWARD GALLEY FLOOR EMERGENCY LIGHT STRIP IAW AMM 33-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,978 hrs · 18,290 cycles

DURING MAINTENANCE INSPECTION FOUND THE ABOVE WING LEFT EMERGENCY LAMP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,418 hrs · 17,847 cycles

DURING B INSPECTION FOUND THE MAIN CABIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 20,840 hrs · 17,383 cycles

ON FLIGHT 2976 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 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 — DISCHARGED (CABIN) · airframe 20,840 hrs · 17,383 cycles

DURING B INSPECTION FOUND THE GALLEY EMERGENCY SIGNS, LIGHTS AND FLOOR STRIPS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY BACK UP BATTERY AND CHARGER IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,683 hrs · 17,258 cycles

ON FLIGHT 3248 - THE CREW REPORTED A BAD ODOR IN THE COCKPIT AND WAS UNABLE TO DETERMINE THE ORGIN. ODOR MIGHT BE THE FLIGHT CREW SEAT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED DETAILED VISUAL INSPECTION OF THE FLIGHT COMPARTMENT. RAN PACKS, NO BAD ODOR NOTICE AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 20,600 hrs · 17,184 cycles

FLIGHT 3364, CREW REPORTED FLOOR PROXIMITY LIGHTNING EMERGENCY STOPS WERE NOT INSTALLED CORRECTLY. SHORT STRIPS ARE IN FRONT AND LONG STRIPS ARE IN BACK. AIRCRAFT REMOVED FROM SERVICE. SWAPPED PROXIMITY LIGHTS FROM FRONT TO BACK. THE OPS CHECKED GOOD IAW AMM 33-50-12. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — FAILED (NR 2) · airframe 19,699 hrs · 16,450 cycles

ON FLIGHT 4164 THE CREW REPORTED THE NUMBER 2 ENGINE FAILED ON FINAL APPROACH. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE NR 2 IAW MTX WC 71-000-00. THE OPERATIONAL AND LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FUSE — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 19,686 hrs · 16,439 cycles

DURING B-INSPECTION FOUND THE SECOND AISLE AND RIGHT FORWARD FAIRING EXTERNAL EMERGENCY LIGHTS ARE INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND DEDICATED FUSE IN CIRCUIT POWERING BOTH LIGHTS TO HAVE A RESISTANCE OF 21 OHMS. GAINED ACCESS TO FUSE IN NR 2 EMERGENCY BATTERY CHARGING ASSEMBLY AND RE-INSTALLED HEADLINER IAW STEP 2 OF EMB145 AMM 33-50-04. REMOVED AND REPLACED FUSE IAW EMB145 STANDARD MAINTENANCE PRACTICES. THE OPERATIONAL CHECK OF LIGHTS WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 19,513 hrs · 16,305 cycles

FLIGHT 4199, CREW REPORTED THE EMERGENCY LIGHT OVER SEAT 3 BC IS MISSING CAP. AIRCRAFT REMOVED FROM SERVICE. FOUND LIGHT COVER AND INSTALLED AS REQUIRED PER STANDARD MAINT PRACTICES. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — MISINSTALLED (CALL LIGHT) · airframe 19,513 hrs · 16,305 cycles

ON FLIGHT 4199, THE CREW REPORTED THE CALL LIGHT OVER SEAT 15 B & C IS INOPERATIVE. FOUND CALL BUTTON LIGHT BULB TO BE INSTALLED BACKWARDS. INSTALLED THE CORRECT WAY IAW AIRCRAFT STANDARD MAINTANANCE PRACTICES. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 19,447 hrs · 16,258 cycles

ON FLIGHT 3545 THE CREW REPORTED THAT ON CLIMBOUT AFTER TAKEOFF, THEY RECEIVED AN EICAS MESSAGE "BAGGAGE DOOR OPEN" AND A RED DOOR OPEN INDICATION ON THE MFD. THE CREW DECLARED AN EMERGECNY AND RETURNED TO MIA. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ADJUSTED BAGGAGE DOOR SWITCHES IAW AMM 52-76-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE HARNESS — SHORTED (NR 1 ENGINE) · airframe 18,561 hrs · 15,548 cycles

DURING MAINTENANCE INSPECTION WHILE TROUBLESHOOTING FOUND NR 1 ENGINE FIRE DECT HARNESS WIRE W 4070012-20 SHORTED TO SHIELDING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ENGINE NR 1 HARNESS FOR FIRE DETECTION SYSTEM IAW EMB 145 AMM 71-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,571 hrs · 13,230 cycles

DURING MAINTENANCE BASE VISIT FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LAMP IAW EMB145 AMM 33-50-06. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SLEEVE — LOOSE (AC BAY) · airframe 15,554 hrs · 13,212 cycles

ON FLIGHT 4213 SHORTLY AFTER TAKEOFF THE CREW REPORTED A LOUD POP THEN WHOOSHING SOUND FROM UNDER FLOOR OF THE AIRCRAFT. A STRONG ODOR IN CABIN WAS NOTICED. PACK 1-2 BOTH WENT OFF LINE. THE AIRCRAFT WAS NOT OVERWEIGHT AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DUCT COUPLING SLEEVE AND CLAMPS AT DUAL TEMP CONTROL VALVE IAW EMB 145 AMM 21-60-01. REMOVED AND REPLACED THE HEAT EXCHANGER PLENUM IAW AMM 21-51-02. THE COOLING PACK SYSTEMS 1 AND 2 OPERATIONAL CHECK WAS GOOD IAW AMM 21-51-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 13,932 hrs · 11,970 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS TO BE INOPERABLE DURING AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY HOLDER ASSEMBLY NR 4 AND THE BATTERY SUPPLY IAW EMB 145AMM. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 14,341 hrs · 12,237 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE EMERGENCY LIGHT ON THE HINGE OF THE SERVICE DOOR TO BE OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND EMERGENCY LIGHT CONNECTOR ON SERVICE DOOR HINGE TO HAVE LOOSE RIVETS AND NOT MAKING GROUND. REMOVED AND REPLACED THE 2EA CONNECTOR RIVETS IAW EMB 145 SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — OUT OF POSITION (CABIN) · airframe 13,475 hrs · 11,562 cycles

ON FLIGHT 3558 A PASSENGER REPORTED A RUBBERY BURNING SMELL BETWEEN ROWS 5BC AND 8BC. THE CREW DECLARED AN EMERGENCY AND ELECTED TO DIVERT TO JAN. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THE RUBBER SEAL NEAR ROW 7 ON THE LEFT SIDE VERY CLOSE TO THE CEILING FLUORESCENT LIGHT TUBE. REPOSITIONED THE AFFECTED PULLER SEAL CORRECTLY IAW AMM 25-22-03. NO PARTS REMOVED OR REPLACED. NO FURTHER FUMES OR SMOKE SMELLS WERE NOTED. THE FUNCTIONAL CHECK FLIGHT FOUND TO BE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DAU — MALFUNCTIONED (NR 2) · airframe 7,752 hrs · 6,757 cycles

ABORTED TAKEOFF DUE TO DAU 2 FAIL SELF CLEARED AFTER MOVING THRUST LEVERS TO IDLE. REMOVED AND REPLACED NR 2 DAU IAW EMB 145 AMM 31-41-01. OPS CHECK GOOD. AIRCRAFT RETURN TO SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 6,788 hrs · 5,878 cycles

NUMBER ONE ENGINE HYDRAULIC FAIL MESSAGE, RETURNED TO DFW. REMOVED AND REPLACED ENGINE ONE HYDRAULIC PUMP IAW EMB AMM 29-10-03. LEAK AND OPERATIONAL CHECK WITH NO DEFECTS NOTED, RETURNED AIRCRAFT TO SERVICE.

Part: PROXIMITY SENSOR — FAILED (ZONE 700) · airframe 6,662 hrs · 5,784 cycles

SPOILER FAIL CAUTION MESSAGE AND SPOILER OPEN INDICATION ON CLIMB-OUT THROUGH 10,000 FEET. REMOVED AND REPLACED RIGHT WING OUTBOARD PROXIMITY SENSOR IAW EMB AMM 27-63-04. OPERATIONAL CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: CONNECTOR — LOOSE (NLG) · airframe 6,374 hrs · 5,552 cycles

RECEIVED AIR/GROUND FAIL MESSAGE AFTER TAKEOFF, RETURNED TO MQT. TIGHTENED LOOSE CONNECTOR ON NOSE LANDING GEAR PROXIMITY SWITCH IAW EMB AMM 32-30-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (NR 1)

CUU - FLT 3409 - AIR TURN BACK FOR NR 1 FMS FAILURE AND AUTOPILOT FLIGHT DIRECTOR FUNCTION INOPERATIVE. (M)