N933JN

Part: THRESHOLD — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,769 hrs · 42,024 cycles

PAX DOOR THRESHOLD ATTACHMENT HAS CORROSION AROUND THE NUTPLATE HOLES. R & R THE PAX DOOR AFT AND FWD THRESHOLD ATTACHMENTS IAW SRM 51-40-02.

Part: THRESHOLD — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,769 hrs · 42,024 cycles

AT THE SERVICE DOOR CUTOUT, THRESHOLD ATTACHMENT HAD CORROSION AROUND THE NUTPLATE HOLES. PERFORMED REPAIR TO SERVICE DOOR THRESHOLD IAW SRM 53-21-02-RE, FIGURE 201, AND EO1-53-26-0029.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,769 hrs · 42,024 cycles

GALLEY, CORROSION ON THE LT LOWER SEAT TRACK BETWEEN FR 20-21. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-06.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,769 hrs · 42,024 cycles

LEFT UPPER SEAT TRACK NR 1 HAS CORROSION IN MULTIPLE AREAS. R & R THE SEAT TRACK IAW AMM 53-01-06.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,769 hrs · 42,024 cycles

CABIN LT FLOORBEAM CORRODED AT FRAME 24. REPAIRED CABIN LT FLOORBEAM AT FRAME 24 IAW ETD2025-145-000131 REV.A AND PIEDMONT EO1-53-26-0016

Part: ATTACH BRACKET — CRACKED (ZONE 800) · airframe 45,769 hrs · 42,024 cycles

CARGO DOOR TORSION BAR AFT ATTACHMENT BRACKET IS CRACKED. RAR CARGO DOOR TORSION BAR AFT ATTACHMENT BRACKET IAW EMB 145 SRM 51-40-02 AND EO1-53-26-0028.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 45,769 hrs · 42,024 cycles

POSSIBLE CRACK ON SHEAR CLIP AT FRAME 67 BETWEEN STRINGERS 6L-7L. R & R THE SHEAR CLIP AT FRAME 67 BETWEEN STRINGERS 6L-7L. IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,769 hrs · 42,024 cycles

RIGHT LOWER SEAT TRACK NR 5 HAD CORROSION IN MULTIPLE AREAS. R & R THE SEAT TRACK IAW AMM 53-01-06.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,769 hrs · 42,024 cycles

CABIN LT FLOORBEAM CORRODED AT FRAME 29. REPAIRED CABIN LT FLOORBEAM IAW ETD2026-145-000133, AND PIEDMONT EO1-53-26-0022.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,769 hrs · 42,024 cycles

RIGHT UPPER SEAT TRACK NR 1 HAD CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,789 hrs · 42,024 cycles

CENTER FLOOR OMEGA BEAM LT INBD FLANGE BETWEEN FR52/54 HAVE CORROSION. BLENDED OUT CORROSION ON CENTER FLOOR OMEGA BEAM LH INBD FLANGE BETWEEN FRM-52/54 IAW EMB 145 SRM 51-10-03, AND THE BLENDED AREA IS ACCEPTED AS IS IAW ETD2025-145-000124 REV: B AND PIEDMONT EO1-53-26-0015

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,769 hrs · 42,024 cycles

CABIN LT NR 2 FLOORBEAM GUSSET CORRODED. R & R CABIN LT NR 2 FLOORBEAM GUSSET IAW SRM 51-40-02.

Part: HOUSING — WORN (ZONE 300) · airframe 45,769 hrs · 42,024 cycles

LEFT & RIGHT VERTICAL STABILIZER SPHERICAL BEARING HOUSINGS WORN. ENLARGED LT & RT VERTICAL STAB SPHERICAL BEARING HOUSINGS TO FIRST OVERSIZED (DIMENSION 58.00MM, PN 145-408881-001 (RE-WORK #1) IAW SRM 55-30-02 ND EO1-55-26-0030.

Part: BRACKET — GOUGED (ZONE 100) · airframe 45,769 hrs · 42,024 cycles

SEVERAL GOUGES ON BAGGAGE DOOR LOWER FRAME L BRACKET. R & R LOWER EXTERNAL L-PROFILE ON BAGGAGE DOOR IAW SRM 51-40-02, 51-21-01.

Part: CAP — CORRODED (ZONE 600 FLAP) · corrosion level 2 · airframe 45,769 hrs · 42,024 cycles

RIGHT INBD FLAP INBD END CAP CORRODED AROUND NUT PATES HOLES. R & R RT INBD FLAP INBD END CAP IAW SRM 51-40-02.

Part: DOOR FRAME — DAMAGED (ZONE 200) · airframe 45,769 hrs · 42,024 cycles

DMT 25 COMPLY WITH PERMANENT REPAIR PER ETD2025-145-922984-B, EO1-53-25-0204 AND SRM 145/1142, 53-00-04 RE OF FRAME 20 LOWER SERVICE DOOR WITH -IN 1100 FC AS OF TAT 44,880:30 TAC 40,964. REPAIRED FRAME 20 AT THE SERVICE DOOR CUTOUT LOWER NUTPLATE HOLE IAW EMB 145 SRM 53-00-04 ITEM 16, FIG. 208 AND PIEDMONT EO1-53-26-0021.

Part: STOP FITTING — NOT REPORTED (ZONE 200) · airframe 45,769 hrs · 42,024 cycles

REMOVE AND INSTALL SERVICE DOOR FRAME STOPS FOR INSPECTION. REMOVED AND REINSTALLED SERVICE DOOR FRAME STOPS IAW EMB 145 AMM 53-21-04 AND ETD2026-145-000365 REVISION A AND PIEDMONT EO1-53-26-0026

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 45,537 hrs · 42,767 cycles

AFT BULKHEAD EMERGENCY FLASHLIGHT DOES NOT FUNCTION. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW CMM 25-60-14.

Part: RELAY — FAULTED (ZONE 200) · airframe 43,631 hrs · 39,590 cycles

EMERGENCY LIGHTS NOT ATIVATING ON COMMAND. RAR RELAY K0275 AND EMER LIGHT MODULE IAW AMM 20-13-10

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 43,402 hrs · 39,412 cycles

SERVICE DOOR HINGE EMERGENCY LIGHT INOP. RAR CONNECTOR CONTACTOR AND ENSURED BACKSHELL WAS TIGHT

Part: FUEL UNIT — FAULTED · airframe 43,428 hrs · 39,384 cycles

IN FLT FUEL 1 LOW LEVEL MASTER WARNING FOLLOWED BY LOSS OF ALL FUEL INDICATIONS FACT 21SEP24 01:04 ROA FOUND CMC MESSAGE "FUEL 1 LOW LEVEL FAIL". R/R'D FUEL CONDITIONING UNIT IAW MM 28-41-01, OPS CK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,431 hrs · 37,025 cycles

E987694 RUDDER 2 RIB ZV 1171.0 DAMAGED AT AFT FASTENER HOLE ON LH AND RH SIDES AND HAS TOOLING MARKS ON LH SIDE AT AFT END. FABRICATED SERVICEABLE RUDDER 2 RIB ZV-1171.0 AND INSTALLED SERVICEABLE RUDDER 2 RIB ZV-1171.0 IAW ETD# ETD2023-145-018625 AND EMB 145 SRM 51-40-02 AND PIEDMONT EO1-55-23-0209

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,431 hrs · 37,025 cycles

E987413 LH AND RH RUDDER EXTERNAL SKIN DENTED/CRACKED AT FASTENER HOLE JUST FWD OF TRAILING EDGE ON RIB ZV 1171.0. ACCOMPLISHED REPAIR OF THE LH AND RH RUDDER 2 SKIN AT RIB ZV-1171.0 IAW ETD2023-145-018320 AND PIEDMONT EO1-55-23-0212

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,431 hrs · 37,025 cycles

CARGO DOOR WEBBING PREVIOUS REPAIR AT FWD LOWER ENDIS GOUGED. : REMOVED GOUGED DOUBLER, FABRICATED AND INSTALLED SERVICABLE NEW DOUBLER TO CARGO DOOR WEBBING AT HB4 AND FWD EDGE IAW EMB 145 SRM 52-30-01 RE SECTION 12 FIGURE 213 AND PIEDMONT EO1-52-23-0185.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,431 hrs · 37,025 cycles

E985046 LH WING RIB 21 IS CRACKED. FABRICATED FILER, DOUBLER AND SHIM, AND INSTALLED DOUBLER, SHIM, AND FILLER ON LH WING RIB 21 IAW EMB-145 SRM 57-20-07 RE 4. TABLE 202, DET. C, FIGURE 203 AND EO1-57-23-0199

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,431 hrs · 37,025 cycles

E983976 RH WING RIB 21 AND UPPER SUPPORT "L" SHAPED PROFILE CRACKED. INSTALLED DOUBLER, FILLER, SHIM & "L" SHAPED BRACKET ON RH WING RIB 21 IAW EMB-145 SRM 57-20-07 RE 4. STEPS I & K, DET. B & C, FIGURE 203 AND PIEDMONT EO1-57-23-0190,

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983801 SSI 53-30-03 CORROSION ON SHEAR CLIP AT BAGGAGE DOOR CUT-OUT AT FRAME 65 PREVIOUS REPAIR. REMOVED AND INSTALLED SERVICEABLE SHEAR CLIP AT BAGGAGE DOOR CUTOUT AT FRAME 65 IAW EMB 145 SRM 53-31-04 AND PIEDMONT EO1-53-23-0194.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983799 SSI 53-30-03 CORROSION ON SHEAR CLIP AT BAGGAGE DOOR CUT-OUT AT FRAME 68 PREVIOUS REPAIR. REMOVED AND INSTALLED SERVICEABLE FRAME 68 SHEAR CLIP LOWER SECTION IAW EMB 145 SRM 53-31-04 AND PIEDMONT EO1-53-23-0193.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983530 CORROSION IN LAV AREA ON LH FLOOR SILL. : REMOVED AND REPLACED LH FLOOR SILL IN LAV AREA IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983484 CORROSION ON RH OTBD # 2 FLOOR SILL. RAR R/H #2 OUTB FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983523 L/H #1 OUTBOARD FLOOR SUPPORT CORRODED MARKED. REMOVED AND REPLACED LH #1 OUTBD FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983559 CORROSION ON RH OTBD CROSS FLOORBOARD SUPPORT AT FRAME 53. REMOVED AND REPLACED R/H OTBD CROSS FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983494 CORROSION ON LH BEAM GUSSET # 5. : REMOVED AND INSTALLED NEW & SERVICEABLE L/H BEAM GUSSET #5 IAW EMB-145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983486 CORROSION ON RH OTBD # 3 FLOOR SILL. : RAR R/H OTBD # 3 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983483 CORROSION ON RH OTBD # 1 FLOOR SILL. RAR R/H OTBD # 1 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983491 CORROSION ON CENTER BEAM GUSSET # 4. REMOVED AND REPLACED CENTER BEAM GUSSET # 4 IAW EMB-145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983504 CORROSION ON LH OTBD # 6 FLOOR SILL. RAR L/H OUTBD #6 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983502 CORROSION ON RH OTBD # 4 FLOOR SILL. RAR R/H OTBD # 4 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983499 CORROSION ON LH OTBD # 2 FLOOR SILL. RAR LH OTBD # 2 FLOOR SILL IAW EMB-145 SRM 51-40-02. .

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983490 FRAME 22 CORRODED AT SERVICE DOOR CUT-OUT LOWER AFT CORNER. CUT, FABRICATED, DRILLED AND INSTALLED FR 22 REPLACEMENT SECTION BTW STGR 11R-18R AND L-ANGLE SPLICES IAW EMB 145 SRM 53-00-04 ITEM 17 FIGURE 209, ETD# ETD2023-145-017207, EO1-53-23-0196, AND EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983403 LH #1 OUTBD FLOOR SILL IN CARGO IS CORRODED AT FWD END. REMOVED & REPLACED LH #1 OUTBD FLOOR SILL IN CARGO IAW EMB-145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983561 CORROSION ON RH OTBD # 6 FLOOR SILL. REMOVED AND REPLACED R/H OTBD #6 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,431 hrs · 37,025 cycles

E983412 LH #2 OUTBD FLOOR SILL IN CARGO IS CORRODED. RAR L/H #2 OUTBD CARGO FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,025 cycles

E983372 FUSELAGE INTERNAL RH#3 UPPER SEAT TRACK CORRODED IN NUMEROUS AREAS. : BLENDED OUT CORRSION ON R/H UPPER SEAT TRACK #3 IAW EMB 145 SRM 51--10-03. PART MECHANICALLY MEASURED .32" AND FOUND TO BE OUT OF ALLOWABLE LIMITS IAW EMB 145 SRM 53-00-11 AD. USED EASI CALIPER S/N 08255463. RAR UPPER RH #3 SEAT TRACK IAW EMB 145 AMM 53-01-06.TQW#NS2093 AND SN1099402062.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,431 hrs · 37,025 cycles

E983413 LH #3 OUTBD FLOOR SILL IN CARGO IS CORRODED. REMOVED AND REPLACED LH #3 OUTBD FLOOR SILL IN CARGO IAW EMB-145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,431 hrs · 37,625 cycles

E983407 RH #2 OUTBD FLOOR SILL IN CARGO IS CORRODED. BLENDED CORROSION ON RH #2 OUTBD FLOOR SILL IN CARGO AND FOUND TO BE BEYOND ALLOWABLE LIMITS IAW EMB-145 SRM 51-10-03, & SRM 53-31-10 AD. RAR RH #2 OUTBD FLOOR SILL IN CARGO IAW EMB-145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,431 hrs · 37,025 cycles

RH AILERON FITTING THAT CONNECTS ACTUATOR ROD TO AILERON SPAR TWO OUTBOARD HOLES ARE WORN. REMOVED AND INSTALLED SERVICEABLE RH AILERON FITTING IAW EMB 145 SRM 51-40-02. SEE WIP AND TASK FOR DETAILS. SEE NRTC# E983354 FOR RH AILERON INSTALLATION.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,431 hrs · 37,025 cycles

LH AILERON FITTING THAT CONNECTS ACTUATOR ROD TO AILERON SPAR TWO OUTBOARD HOLES ARE WORN. REMOVED AND INSTALLED SERVICEABLE LH AILERON FITTING IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,431 hrs · 37,025 cycles

E982478 RH UPPER FUSELAGE SKIN CRACK AT FASTENER ON FRAME 77 BETWEEN STRINGER 8-9R. INSTALLED REPAIR BUSHING ON RH UPPER FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGER 8R-9R IAW EMB-145 SRM 53-32-01 RE, ITEM/STEP 9 AND PIEDMONT EO1-53-23-0213

Part: NONE — CRACKED (MAIN) · airframe 40,465 hrs · 36,027 cycles

MAIN DOOR EMERGENCY LIGHT ASSY CRACKED-C/A-RAR MAIN DOOR EMERGENCY LIGHT ASSY MAIN DOOR EMERGENCY LIGHT ASSY IAW EMB AMM 25-23-04-000-801-A AND 25-23-04-400-801-A. OPC GOOD

Part: NONE — BROKEN (AFT) · airframe 40,261 hrs · 35,819 cycles

EMERGENCY PHOTOLUMINESCENT LIGHT STRIP SECOND FROM AFT HAS BROKEN WIRES ON IT.-C/A-RAR THE EMERGENCY LIGHT STRIP SECOND FROM AFT IAW EMB 145 AMM , 33-50-12 OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (MAIN) · airframe 40,184 hrs · 35,723 cycles

MAIN DOOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EMERGENCY LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECK GOOD. END.

Part: LIGHT — INOPERATIVE (FOOR PANEL 241 B) · airframe 40,169 hrs · 35,706 cycles

REMOVED EMERGENCY LIGHT STRIP ON FLOOR PANEL 241BF TO FOM-C/A-INSTALLED EMERGENCY LIGHT STRIP 214BF IAW 33-50-12 OPS CHECK GOOD

Part: NONE — DAMAGED (LH MLG) · airframe 39,826 hrs · 35,288 cycles

SUPPLEMNTAL CA FOR CFR CALLED FOR SMOKE ON LH MLG FROM HYD LEAK / EMERGENCY NOT DECLARED-C/A-CA PENDING-C/A-RAR #1 BRAKE ASSY IAW WC 32-600-14

Part: NONE — MISSING (AFT) · airframe 39,823 hrs · 35,282 cycles

AFT CABIN FLASHLIGHT MISSING-C/A-INSTALLED NEW FLASHLIGHT AND BATTERY AT LAV BULKHEAD AS NEEDED. REF. AMM 33-51-01 AND ETN-EM-33-059

Part: NONE — NONE · airframe 38,891 hrs · 34,234 cycles

LH FWD EXTERIOR EMERGENCY LIGHT INOP.-C/A-REMOVED AND REPLACED LH FWD EXTERIOR EMERGENGY LIGHT BULB IAW EMB 145 33-50-10. OPERATIONAL CHECK GOOD.

Part: WEB — GOUGED (CARGO DOOR) · airframe 37,494 hrs · 32,676 cycles

CARGO DOOR INTERNAL LOWER WEB GOUGED 3 AREAS. C/A: PERFORMED PERMANENT REPAIR TO CARGO DOOR LOWER WEB, IAW EMB 145 SRM 52-30-01-RE AND ETN-EM-52-043.

Part: SKIN — GOUGED (LT ELEVATOR) · airframe 37,494 hrs · 32,676 cycles

GOUGE FOUND ON LH ELEVATOR SKIN LEADING EDGE APPROX. 10 INCHES FROM INBD EDGE.-C/A-REMOVED AND REPLACED LH ELEVATOR INBD LEADING EDGE SKIN IAW EMB 145 SRM 55-20-01-SI, SRM 51-40-02, ETN-EM-55-073 AND ETN-EM-55-076.

Part: FLOOR SUPPORT — CORRODED (CENTER) · airframe 37,494 hrs · 32,676 cycles

CENTER OMEGA BEAM CORRODED BETWEEN FR 58-59.LEVEL 1 CORROSION-C/A-PERFORMED PERMANENT REPAIR TO CENTER OMEGA BEAM BETWEEN FR 58-59 IAW EO EM-53MR-1518 PT B.

Part: FLOOR SUPPORT — CRACKED (RIGHT) · airframe 37,494 hrs · 32,676 cycles

RH OMEGA BEAM INBD SUPPORT CRACKED BETWEEN FR 46-47.1 CRACK, LENGTH 0.02-C/A-PERFORMED PERMANENT REPAIR TO OMEGA BEAM INBD SUPPORT IAW EMB 145 SRM 53-23-02-RE..

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,494 hrs · 32,676 cycles

LT OMEGA BEAM CORRODED BETWEEN FR 58-59. LEVEL 2 CORROSION. C/A: PERFORMED PERMANENT REPAIR TO LT OMEGA BEAM BETWEEN FR 58-59, IAW EO EM-53MR-1518 PT A.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 37,494 hrs · 32,676 cycles

HAT BEAM CRACKED AT NUT PLATE HOLE IN LAV UNDER RT FLOOR GUSSET BETWEEN FRAMES 59-60. CRACK LENGTH .018 NUMBER OF CRACKS 1. C/A: PERFORMED PERMANENT REPAIR TO HAT BEAM IN LAV UNDER RT FLOOR GUSSET, IAW ERS-EM-53MR-4247.

Part: ATTACH FITTING — GOUGED (L AILERON DAMPER) · airframe 37,494 hrs · 32,676 cycles

LT WING AILERON DAMPER ATTACHMENT FITTING GOUGED. C/A: REMOVED AND REPLACED LT AILERON DAMPER FITTING, IAW EO EM-27MR-112.

Part: DOOR SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 37,494 hrs · 32,676 cycles

CARGO DOOR OPENING CENTER SILL CORRODED. CORROSION LEVEL 2. C/A: REMOVED AND REPLACED CARGO DOOR OPENING CENTER SILL, IAW EMB 145 SRM 51-40-02.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 37,494 hrs · 32,676 cycles

CARGO DOOR FWD CONTINUOUS SUPPORT CRACKED AT UPPER CORNER. CRACK LENGTH .185, NUMBER OF CRACKS 1. C/A: REMOVED AND REPLACED CARGO DOOR FWD CONTINUOUS SUPPORT, IAW EMB 145 SRM 51-40-02.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 37,494 hrs · 32,676 cycles

CARGO DOOR AFT FRAME LOWER CORNER CRACKED. CRACK LENGTH .375, NUMBER OF CRACKS 2. C/A: REMOVED AND REPLACED CARGO DOOR AFT FRAME, IAW EMB 145 SRM 51-40-02.

Part: DRAG ANGLE — CRACKED · airframe 37,494 hrs · 32,676 cycles

RT DRAG ANGLE HAS POSSIBLE CRACK AT FR 77 BETWEEN 2 LOOSE FASTENERS. CRACK LENGTH 0.5 NUMBER OF CRACKS 1. C/A: INSTALLED REPAIR DOUBLER AND FILLER AT FR 77, IAW EMB 145 SRM 51-40-02 AND ENVOY ERS-EM-53MR-4253.

Part: STRIP — BROKEN (CABIN EMER LIGHT) · airframe 37,494 hrs · 32,676 cycles

EMERGENCY LIGHT STRIPS 3 EA BROKEN. R & R 3 EA EMERGENCY LIGHT STRIP EXTRUSIONS IAW EMB 145 AMM 33-50-12. SEE BOW 350633 FOR INSTALLATION AND OPS CHECK.

Part: STRIP — BROKEN (CABN FLOOR PROX) · airframe 37,494 hrs · 32,676 cycles

FLOOR PROXIMITY STRIPS 6 EA BROKEN. R & R 6 EA FLOOR PROXIMITY STRIPS IAW EMB 145 AMM 33-50-12. SEE BOW 350633 FOR INSTALLATION AND OPS CHECK.

Part: PIN — CORRODED (RT WG EMER EXIT) · airframe 37,494 hrs · 32,676 cycles

RIGHT OVERWING EMERGENCY EXIT LOWER FWD GUIDE PIN CORRODED. R & R RT OVERWING EMERGENCY EXIT FWD PIN IAW EMB 145 AMM 52-21-00-820-801-A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,282 hrs · 31,403 cycles

DURING PS1 FOUND FLOOR PROX EMER. LIGHT STRIP 2 & 3 INOP.-C/A-REMOVED AND REPLACED FLOOR PROX. LIGHT IAW EMB-145 AMM 33-50-12 OPS CHECK: FAI. INVERTER P/N 7824-1

Part: SWITCH — FAILED (NR 2 A/C PACK) · airframe 35,790 hrs · 30,959 cycles

PRIOR TO DESCENT AFTER MANNUALLY USING ANTI-ICE CREW AND PASSENGERS NOTICED DISTINCT BURNING SMELL IN THE CABIN AND COCPIT ASSOCIATED WITH A WISP IN THE UPPER CABIN BRIEFLY AFTER IT DISSAPATED.-C/A-ACCOMPLISHED ETN-EM-72-034. NO SMOKE OR SMELL NOTED IN AIRCRAFT. PREFORMED INITIAL EVALUATION REF EMB FIM TASK 21-20-00-810-A AND EMB 145 AMM 21-51-03-210-801. CONFIRMED BURNING SMELL AND NOTICED AIR LEAK IN THE AREA OF PACK 2. FURTHER TROUBLESHOOTING REQUIRED. INSPECTED AND FOUND #1 PACK ACM SEIZED. DEFERRED PER MEL 21-30. PERFORMED TROUBLESHOOTING PER FIM 21-51-00 PERFORMED CMC DOWNLOAD PER AMM 45-45-00. NO RELATED MESSAGES. REMOVED AND REPLACED PACK #2 DUCT OVERTEMP SWITCH PER AMM 21-51-09. OPC GOOD. MEL RESTORED. ALL MTX ACTIONS C/W. ACCOMPLISHED ETN-EM-72-034. NO SMOKE OR SMELL NOTED IN AIRCRAFT.

Part: AUTOPILOT SYS — UNKNOWN · airframe 35,627 hrs · 30,818 cycles

AUTOPILOT FAIL WARNING DURING CAT II APPROACH PROCEDURES INSIDE THE FAF. PERFORMED OPERATIONAL CHECK OF AUTOPILOT SYSTEMS IAW W/C 22-700-00, 22-700-01 AND 22-700-02. OPS CHECKS GOOD NO DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 35,090 hrs · 30,313 cycles

SUPPLEMENTAL FLIGHT ATTENDENTS FWD FLASHLIGHT INOP-C/A-FLIGHT CREW PLACARDED FLIGHT ATTEND FWD FLASHLIGHT AUTH 070857-C REF 25-53 MOC 630997. REMOVED AND REPLACED F/A FLASHLIGHT IAW AMM 33-50-16 STEPS 2.I.(1) AND 3.H.(4). OPC GOOD. MEL 25-53 AUTH# 070857-C RESTORED.

Part: LIGHT — INOPERATIVE (ROW 16) · airframe 34,867 hrs · 30,078 cycles

ROW 16 CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED ROW 16 CEILING EMERGENCY LIGHT IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 34,707 hrs · 29,924 cycles

LT OVERWING EMERGENCY LIGHT INOP. C/A-RAR LT OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.

Part: HOSE — LEAKING (ANTI-ICE SYSTEM) · airframe 33,971 hrs · 29,209 cycles

SUPPLEMENTAL TWO ON APPROACH IN ICING CONDITIONS STAB A/ICE FAIL CAUTION MESSAGE FOLLOWED BY AN ICE COND-A/I INOP WARNING MESSAGE ON EICAS. "TRANSFERRED TO NRWC 933-ORD-03489". C/A-TROUBLE SHOT REF. FIM 30-12-00-810-805-A, ACCOMPLISHED VERTICAL-STAB. A/I MONITORING TUBES ADJUSTMENT/TEST IAW MM 30-12-11-700-801-A. VERIFIED THAT HOSE ASSY. WAS LEAKING. REMOVED AND REPLACED VERTICAL-STAB. A/I MONITORING TUBES HOSE ASSY. IAW MM 30-12-11. OPS CHECK GOOD IAW AMM 30-00-00. PERFORMED OPERATIONAL CHECK OF ANTI-ICE SYSTEM IAW AMM 30-00-00 OPS TEST GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (NLG STEERING) · airframe 33,845 hrs · 29,083 cycles

ON TAXI IN, NOSEWHEEL STEERING DIDNT TURN THEN JUMPED FOR A SUDDEN TURN IN DESIRED DIRECTION W/ TILLER DEPRESSED. ON ANOTHER TURN, STEER INOP AFTER STARTING TURN W/ TILLER DEPRESSED. RELEASING AND DEPRESSING TILLER RESTORED STEERING.-C/A-RAR 7 DEGREE PROXIMITY SWITCH IAW EMB 145 AMM 32-50-06. OPC GOOD.

Part: FLASHLIGHT ASSY — LOOSE (FWD CABIN) · airframe 33,842 hrs · 29,079 cycles

CABIN FLASHLIGHT IN FORWARD CABIN IS LOOSE.-C/A-R & R FLASHLIGHT BRACKET WORKS AS REQUIRED OPS CHECK IAW AMM 23-51-01. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 33,677 hrs · 28,912 cycles

LH WING INSPECTION LIGHT INOP-C/A-REMOVED AND REPLACED LH WING INSPECTION LIGHT IAW AMM 33-44-02. OPC GOOD.

Part: LINE — BLOWN (AC BAY) · airframe 32,765 hrs · 28,107 cycles

PACK 2 BLEED 2 KEPT FAILING DURING CLM OUT. THEN FA REPORTS POPING AND HISSING NOISE UNDER FLOOR RIGHT SIDE OF AIRCRAFT. A/I DFW ACCT NOISE FROM NR 2 ENGINE. EMERGENCY DECLARED. FOUND LINE BLOWN OFF NR 2 DUAL TEMP CONTROLLER. REINSTALLED LINE IAW ETNEM-21-056 OPS CHECKS GOOD IAW AMM 21-51-00. E2 BLD OPS CHECKS GOOD IAW AMM 36-11-05.

Part: LINE — DETECTED (AC BAY) · airframe 32,755 hrs · 28,093 cycles

PACK 2 BLEED 2 KEPT FAILING DURING CLIMB OUT. THEN FA REPORTS POPPING AND HISSING NOISE UNDER FLOOR RIGHT SIDE OF AIRCRAFT. FOUND LINE BLOWN OFF NR 2 DUAL TEMP CONTROLLER. REINSTALLED LINE IAW ETNEM-21-056 OPS CHECKS GOOD IAW AMM 21-51-00 E2 BLEED OPS CHECKS GOOD IAW AMM 36-11-05.

Part: WIRE — BROKEN (CABIN) · airframe 32,745 hrs · 28,085 cycles

NR 1 LT EMERGENCY LIGHT STRIP HAS BROKEN WIRE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: WEB — GOUGED (CARGO DOOR) · airframe 32,745 hrs · 28,085 cycles

CARGO DOOR INTERNAL WEB GOUGED 4 AREAS LOWER FORWARD AREA. REMOVED AND REPLACED CARGO DOOR INNER WEB FWD LOWER PREVIOUS REPAIR IAW SRM 52-30-01 AND ETN-EM-52-043.

Part: YOKE — CRACKED (LT ENGINE) · airframe 32,745 hrs · 28,085 cycles

LT ENGINE FORWARD NR 1 YOKE CRACKED LOWER END OUTBOARD SIDE. REMOVED AND REPLACED LT LOWER FORWARD YOKE FITTING IAW EO EM-54MR-386.

Part: SKIN — CORRODED (PAX DOOR) · airframe 32,745 hrs · 28,085 cycles

SKIN AROUND LOWER NUT PLATE HOLES ON BOTTOM OF PAX DOOR ARE CORRODED. REPAIRED SKIN AROUND LOWER NUTPLATE HOLES (2 EACH) IAW SRM 52-10-02, AND ETN-EM-52-041.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,745 hrs · 28,085 cycles

SERVICE DOOR CENTER SILL CORRODED AT FWD NUTPLATE HOLE. REMOVED AND REPLACED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 32,745 hrs · 28,085 cycles

CENTER OMEGA BEAM CORRODED BETWEEN FR 23-25. REPAIRED LT OMEGA BEAM CORROSION BETWEEN FRAMES 23 AND 25 IAW SRM 53-00-10.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,745 hrs · 28,085 cycles

LOWER CARGO DOOR CUTOUT SILL CORRODED. R&R CARGO DOOR SILL IAW SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,565 hrs · 27,931 cycles

MULTIPLE EMERGENCY LIGHTS WERE INOPERATIVE. TROUBLESHOT IAW WM 33-50-50. R & R THE NR 1 AND 4 BATTERIES AND CHARGER IAW W/C 33-700-19. R & R THE NR 6 INVERTER IAW 33-50-11. PERFORMED AN OPS CHECK OF THE EMERGENCY LIGHTS IAW W/C 33-700-17. OPS CHECKED GOOD. NO FURTHER DEFECTS FOUND.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,208 hrs · 27,558 cycles

DURING A PS-2 CHECK, FOUND THE AISLE EMERGENCY LIGHT INOPERATIVE AT ROW 12. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-08. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,997 hrs · 27,380 cycles

RIGHT EXTERNAL OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (NLG STEERING) · airframe 31,883 hrs · 27,282 cycles

RUDDER PEDALS LOCKED UP. INSPECTED STEERING SYSTEM, PERFORMED OPS TEST OF STEERING SYSTEM AND TAXI RUN WITH CREW IAW AMM 32-50-0, OPS CHECK GOOD.

Part: THERMOSTAT — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 31,597 hrs · 27,023 cycles

DURING DECENT/ APPROACH INTO TO ORD 1ST "STAB A/ICE FAIL CAUTION ON EICAS THEN ICE COND A/I INOP WARNING ON EICAS PUT THE OVERRIDE SWITCH IN ALL POSITION AND MSGS WENT AWAY BUT STILL HAD "BLD 1 LOW TEMP CAUTION DUE TO LOW THRUST SETTING “TRANSFERRED TO NRWC 933-ORD-02923". FOUND EICAS MSG BLD 1 LOW TEMP CAUTION TROUBLESHOOTING USING FIM 36-11-00-810-801-A FOUND CLOGGED THERMOSTAT AND RESTRICTOR. R&R THERMOSTAT AND RESTRICTOR IAW AMM 36-11-06.OPS CHECK GOOD IAW 36-00-00.

Part: ANTI-ICE VALVE — FAILED (HORIZONTAL STAB) · airframe 31,592 hrs · 27,016 cycles

STAB ANTI ICE FAIL DURING PNEUMATIC TEST IN FLIGHT-C/A-REMOVED AND REPLACED STAB A/I VALVE IAW AMM 30-12-01 ALL OPS NML IAW AMM 30-00-00.

Part: CRADLE — MALFUNCTIONED (FLASHLIGHT) · airframe 31,529 hrs · 26,970 cycles

REAR CABIN EMERGENCY FLASHLIGH IS DIM-C/A-DURING INSPECTION OF CABIN EMERGENCY EQUIPMENT NOTICED REAR FLASHLIGHT WAS DIM REMOVED AND REPLACED BATTERY NO FIX REMOVED AND REPLACED FLASHLIGHT ASSY AND CRADLE IAW EMB 145 AMM 33--50-16 PER EEL OPS CHECK GOOD

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 31,310 hrs · 26,759 cycles

EMERGENCY LIGHTS NR 2 AND 3 INOPERATIVE. CHARGED THE BATTERIES IAW AMM 33-50-00. OPS CHECKED GOOD

Part: OIL SYSTEM — LOW (NR 2 ENGINE) · airframe 30,770 hrs · 26,185 cycles

A/I SPI DUE LOW OIL QTY. NO EMERGENCY DECLARED. FLT CANCELED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,313 hrs · 25,725 cycles

EMERGENCY LIGHT AFT OF THE EMERGENCY ROW SEATING INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-50-12.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 29,031 hrs · 24,497 cycles

EMERGENCY EXIT SIGN OVER SERVICE DOOR DOES NOT ILLUMINATE. R & R NR 2 EMERGENCY LIGHT INVERTER, OPC GOOD IAW AMM 33-50-11.

Part: CONNECTOR — MISSING (CABIN) · airframe 28,331 hrs · 23,823 cycles

NUMBER 6 EMER LIGHT STRIP ACFT SIDE MISSING CONNECTOR. INSTALLED SERVICEABLE CONNECTOR ON NR 6 EMER LIGHT STRIP ACFT SIDE IAW SWPM 20-21-00.

Part: WIRE — BROKEN (CABIN) · airframe 28,331 hrs · 23,823 cycles

LEFT NR 6 EMER LIGHT STRIP WIRE BROKEN. R & R LT NR 6 EMER LIGHT STRIP IAW AMM 33-50-12.

Part: STOP FITTING — CORRODED (CARGO DOOR) · airframe 28,331 hrs · 23,823 cycles

BAGGAGE DOOR FWD DOOR STOP HAS CORROSION AROUND 3 NUTPLATES. PERFORMED REPAIR OF BAGGAGE DOOR FWD DOOR STOP CORROSION IAW ERS-EM-52MR-554.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,331 hrs · 23,823 cycles

LEFT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1L & 2L. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-2103.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,331 hrs · 23,823 cycles

RIGHT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1R & 2R. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-2104.

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 28,331 hrs · 23,823 cycles

BAGGAGE DOOR LOWER ANGLE HAS CORROSION AROUND 4 NUTPLATES. PERFORMED REPAIR OF BAGGAGE DOOR LOWER ANGLE CORROSION IAW ERS-EM-52MR-555.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 28,331 hrs · 23,823 cycles

RIGHT ELEVATOR TIP FLANGE HAS A BURN MARK WITH MATERIAL MISSING AT AFT LOWER NUTPLATE ATTACHING HOLE. REPAIRED RT ELEVATOR TIP FLANGE IAW ERS-EM-55MR-424.

Part: LIGHT — BROKEN (CABIN) · airframe 28,331 hrs · 23,823 cycles

AISLE FLOOR LT SIDE EMER LIGHT STRIP NR 3 BROKEN. R & R AISLE FLOOR LT SIDE EMER LIGHT STRIP NR 3 IAW AMM 33-50-12.

Part: LIGHT — BROKEN (CABIN) · airframe 28,299 hrs · 23,790 cycles

AISLE FLOOR LT SIDE EMER LIGHT STRIP NR 3 BROKEN. R & R AISLE FLOOR LT SIDE EMER LIGHT STRIP NR 3 IAW AMM 33-50-12. SEE NRTC BOW 217923 FOR INSTALL & OPERATIONAL CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 28,299 hrs · 23,790 cycles

LEFT NR 6 EMER LIGHT STRIP WIRE BROKEN. R & R LT NR 6 EMER STRIP LIGHT IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: FIRE DETECTOR — FAILED (RT ENGINE) · airframe 28,267 hrs · 23,765 cycles

E2 FIRE DETECTOR FAIL PASSING FL 230. R & R NR 2 ENG FIRE DETECTOR IAW AMM 26-11-01. OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 27,233 hrs · 22,796 cycles

AFTER PARKING, NOTICED A CLIP TO RETAIN FLASHLIGHT BEHIND CAPTAIN SEAT IN CRADLE HAS BROKEN OFF. R & R CAPTAIN'S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,979 hrs · 22,544 cycles

COCKPIT STEP EMER LIGHT & FWD CEILING BY GALLEY, EMER LIGHT INOPERATIVE. R & R NR 1 EMER LIGHT INVERTER. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,823 hrs · 22,396 cycles

WING TO FUSELAGE FRONT LT EMER LIGHT INOPERATIVE. R & R WING TO FUSELAGE FRONT LT EMER LIGHT BULB. OPERATIONS CHECKED BAD IAW AMM 33-50-07. SEE ITEM 2 SAME NRWC FOR CORRECTIVE ACTION. EMER LIGHT BATTERY PN 2013-1A & SN 110280.

Part: BATTERY — UNSECURE (EMERGENCY LIGHTS) · airframe 26,310 hrs · 21,894 cycles

SEVERAL FWD INTERIOR EMERGENCY LIGHTS INOPERATIVE. RESEATED THE NR 1 BATTERY IN CHARGER IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,942 hrs · 20,553 cycles

MAIN DOOR OVERHEAD EMER LIGHT INOPERATIVE. R & R MAIN DOOR OVERHEAD EMER LIGHT LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS AT THIS TIME.

Part: CONTROL UNIT — FAILED (BRAKE SYSTEM) · airframe 24,443 hrs · 20,113 cycles

BRAKE INBD INOPERATIVE ON FINAL APPROACH CAUSED GO AROUND. FOUND NO MSG ON CMC DOWNLOAD. R & R BCU IAW AMM 32-41-02, FNC GOOD.

Part: ENGINE — FAILED (NR 2) · airframe 24,441 hrs · 20,112 cycles

AFTER SHUTTING DOWN BOTH ENGS DURING POST FLIGHT WITH NR 2 ENG OFF FOR AT LEAST 10 - 15 MINUTES SMOKE IS STILL COMING OUT OF THE FRONT TAIL PIPE. NO FLAMES PRESENT JUST SMOKE. TRANSFERRED TO NRWC 933-CVG-01622. R & R ENG 2 IAW WC 71-000-00. OPERATION CHECKED GOOD & LEAK CHECKED GOOD.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 24,431 hrs · 20,107 cycles

BAGG SMOKE ON EICAS BAGG EXTINGUISHER BUTTON PRESSED IN RESPONSE. R & R FWD SMOKE DETECTOR IAW AMM 26-15-01.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 24,428 hrs · 20,104 cycles

BAGG SMOKE ON EICAS RAN EPC & COMPLIED WITH EMER PROCEDURES. FLIGHT CREW PLACARDED IAW MEL 260. R & R FWD BAGGAGE SMOKE DETECTOR IAW AMM 26-15-01. OPERATIONS CHECKED GOOD IAW AMM 26-15-00 MEL 26-3. R & R HIGH RATE BAGGAGE FIRE BOTTLE IAW AMM 26-23-01. R & R RELAY K0629 IAW EMB 20-13-02.

Part: SKIN — CRACKED (E&E DOOR) · airframe 24,410 hrs · 20,088 cycles

REAR ELECTRONICS COMPARTMENT ACCESS HATCH FRAME IS CRACKED BELOW PIN ATTACHMENT BRACKET. FABRICATED & INSTALLED REPAIR DOUBLER & FILLER IAW ERS-EM-52MR-176.

Part: SKIN — DENTED (RUDDER) · airframe 24,410 hrs · 20,088 cycles

RUDDER 2 LT SIDE EXTERNAL SKIN HAS TWO DENTS APPROXIMATELY 8 INCHES BELOW PANEL 327BL & 7 INCHES FROM TE. ACCOMPLISHED REPAIR OF RUDDER 2 LT SIDE EXTERNAL SKIN DENTS IAW ERS-EM-55MR-135. FOUND DURING RUDDER MAIN CONTROL FEEDBACK PATH.

Part: LIGHT — BROKEN (CABIN) · airframe 24,410 hrs · 20,088 cycles

NUMBER 4 EMER LIGHT STRIP BROKEN. REPLACED NR 4 EMER LIGHT STRIP IAW AMM 33-50-08. SEE BOW 159701 FOR FINAL INSTALL & OPERATIONAL CHECK.

Part: LIGHT — BROKEN (CABIN) · airframe 24,410 hrs · 20,088 cycles

NUMBER 1 EMER LIGHT STRIP BROKEN. REPLACED IAW AMM 33-50-08. SEE BOW 159701 FOR FINAL INSTALL & OPERATIONAL CHECK.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,410 hrs · 20,088 cycles

LAVATORY RT BEAM GUSSET CORRODED. PERFORMED BLEND OUT OF RT LAVATORY BEAM GUSSET ON AFFECTED AREA. AREA FOUND TO BE ACCEPTABLE IAW ERS-EM-5300-589.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 24,410 hrs · 20,088 cycles

CARGO DOOR SILL CORRODED AT FRAME 66. PERFORMED REPAIR ON CARGO DOOR SILL AT FRAME 66 IAW ERS -EM-5300-608.

Part: STRAP — CORRODED (RT WING) · airframe 24,410 hrs · 20,088 cycles

RIGHT WING TIP HAS CORROSION ON STRAP. REPAIRED IAW ERS-EM-5700-187.

Part: LIGHT — BROKEN (CABIN) · airframe 24,410 hrs · 20,088 cycles

WIRE FOR EMER LIGHT STRIP ON FLOORBOARD 251FF BROKEN. REPAIRED IAW SWPM 20-21-00. SEE BOW 159701 FOR OPERATIONS CHECK OF THE EMER LIGHT STRIPS.

Part: ATTACH FITTING — CORRODED (WINDSHIELD) · airframe 24,410 hrs · 20,088 cycles

PILOT'S WINDSHIELD ATTACHMENT FLANGE ON WINDSHIELD, INNER LOWER EDGE HAS CORROSION. REPAIRED IAW ERS EM-5600-035. SEE WIP & TASK ENTRIES FOR DETAILS.

Part: ROLLER — DIRTY (MAIN DOOR) · airframe 23,382 hrs · 19,227 cycles

MAIN DOOR STIFF, HARD TO OPEN. FOUND UPPER MAIN DOOR ROLLERS STICKING. CLEANED & LUBRICATED UPPER MAIN DOOR ROLLERS IAW AMM 53-21-02 & ETN-EM-52-061. MAIN DOOR OPERATIONS CHECKED GOOD IAW AMM 52-10-01.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 23,209 hrs · 19,104 cycles

AFT CABIN FLASHLIGHT HOLDER BROKE. REPLACED AFT CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: GUST LOCK — JAMMED (FLIGHT CONTROL) · airframe 23,127 hrs · 19,042 cycles

ON FLIGHT 3247 CREW REPORTED GUST LOCK JAMMED AFTER BEING RELEASED BEFORE TAKEOFF & DECLARED EMERGENCY. ALL UNLOCKED INDICATIONS WERE VERIFIED PRIOR TO TAKEOFF. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED ELECTRO MECHANICAL GUST LOCK SYS OPERATION IAW AMM 27-71-00, OPERATION GOOD, UNABLE TO DUPLICATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,202 hrs · 18,337 cycles

NR 4 FROM AFT FLOOR PROXIMITY LIGHT STRIP INOPERATIVE. R & R FLOOR PROXIMITY LIGHTSTRIP, NR 4 FROM AFT, IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 22,135 hrs · 18,281 cycles

ROW 18, EMERGENCY FLOOR LIGHT INOPERATIVE. R & R ROW 18 EMERGENCY LIGHT WIRE CONNECTORS IN REF WITH AMM 20-21-00. OPS CHECK GOOD.

Part: WIRE — BROKEN (THERMOSWITCH) · airframe 21,884 hrs · 18,074 cycles

DURING CRUISE, FL 280, EXPERIENCED A SYS 2 BLEED LEAKING WARNING. APPLIED AOM VOL 1 PROCEDURES AND WERE UNABLE TO RESOLVE ANOMALY. DIVERTED. A CHECKLIST DRIVEN "PRECAUTIONARY" ENGINE SHUTDOWN WAS APPLIED AND AN EMERGENCY WAS DECLARED. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. DURING TROUBLESHOOTING, FOUND RT AFT OVERWING COUPLING O-RING BLOWN, REMOVED AND REPLACED BOTH O-RINGS IAW AMM 36-11-10. PERFORMED LEAK TEST AND OPS CHECKED GOOD. NO EICAS MESSAGES PRESENT AT THIS TIME. FOUND THERMAL SWITCH IN RT PYLON HAD TWO BROKEN WIRES. R & R THERMAL SWITCH IN RT PYLON IAW AMM 36-20-02, PERFORMED TEST OF SWITCH IAW AMM 36-20-02, TASK 36-20-02-700-801-A. TEST CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,566 hrs · 17,841 cycles

DURING MX INSPECTION, FOUND THE CENTER AISLE OVERHEAD EMERGENCY LIGHT SIGN (AFT) IS INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R CENTER AISLE OVERHEAD EMERGENCY LIGHT AFT SIDE. OPS CHECKED GOOD. WORK PERFORMED IAW AMM 33-50-15. ACFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,258 hrs · 17,591 cycles

DURING B INSPECTION, FOUND THE EMERGENCY EXIT SIGN MID AISLE INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED EMERGENCY LIGHT TEST IAW AMM 33-50-00. NO DEFECT NOTED. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,648 hrs · 17,100 cycles

DURING B INSPECTION FOUND THE FORWARD CABIN FLASHLIGHT VERY DIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY IN THE FORWARD CABIN FLASHLIGHT USING GENERAL MAINTENANCE KNOWLEDGE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 20,539 hrs · 17,013 cycles

DURING B INSPECTION FOUND THE EXIT ROW OVERHEAD EMERGENCY EXIT LIGHTED SIGN AFT FACE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TAPPED LIGHT. TURNED EMERGENCY LIGHTS OFF AND BACK ON. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME IAW EMB-145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SCREW — STRIPPED (EXTERIOR LIGHT) · airframe 20,390 hrs · 16,894 cycles

DURING B INSPECTION FOUND THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT HAS STRIPPED SCREWS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB AMM TASKS 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: CONNECTOR — LOOSE (CABIN) · airframe 20,390 hrs

DURING B INSPECTION FOUND THE EMERGENCY LIGHT CB POPPED. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BATTERY 4 CONNECTOR LOOSE REFASTENED PER GENERAL KNOWLEDGE. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 20,297 hrs · 16,825 cycles

ON FLIGHT 3374 THE CREW REPORTED THEY WERE UNABLE TO RESET THE EMERGENCY LIGHTS FROM ROW 6. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET EMERGENCY LIGHTS AND THE OPERATIONAL CHECK WAS GOOD PER EMB AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (COCKPIT) · airframe 19,877 hrs · 16,498 cycles

ON FLIGHT 2931 THE CREW REPORTED THE CRADLE THAT HOLDS THE CAPTAINS FLASHLIGHT WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 19,830 hrs · 16,455 cycles

DURING B INSPECTION FOUND THE RIGHT WING INTERIOR EMERGENCY EXIT DOOR UPPER EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WING INTERIOR EMERGENCY EXIT DOOR UPPER EXIT SIGN INVERTER. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,704 hrs · 16,347 cycles

DURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW CARGO DOOR CENTER SILL IAW EMB SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,704 hrs · 16,347 cycles

DURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR AFT SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICE DOOR AFT SILL IAW EMB SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COVER — BROKEN (CABIN) · airframe 19,704 hrs · 16,347 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT STRIP PANEL COVER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT STRIP PANEL COVER IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — UNSERVICEABLE (REAR CABIN) · airframe 19,300 hrs · 15,999 cycles

FLIGHT 3975, FLIGHT ATTENDANT REPORTED THE FLASHLIGHT OVER ROW 18 WAS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-50-16. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — DISCHARGED (COCKPIT) · airframe 19,059 hrs · 15,798 cycles

DURING B INSPECTION, FOUND THE CAPTAIN’S FLASHLIGHT RED CHARGING LED NOT COMING ON. IN HOLDER THE LIGHT WORKS WHEN TURNED ON. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT AND BATTERY IAW CMM 25-60-11. AIRCRAFT RETURNED TO SERVICE.

Part: JACK — OBSTRUCTED (INTERPHONE SYS) · airframe 18,874 hrs · 15,639 cycles

ON FLIGHT 3219 AFTER ROTATION THE CREW REPORTED A VERY LOUD STATIC OVERWHELMED BOTH INTERCOM AND RADIO COMMUNICATION. IT MOMENTARILY STOPPED AND BEGAN AGAIN, AND MINUTES LATER STOPPED FOR THE REMINDER OF THE FLIGHT. THE AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND TIP OF RAMP HEADSET IN GROUND JACK BROKEN OFF. REMOVED AND PERFORMED AN OPERATIONAL CHECK IAW AMM 23-51-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,389 hrs · 15,250 cycles

DURING B-INSPECTION FOUND THE EXTERNAL MAIN PASSENGER DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN PASSENGER DOOR EMERGENCY LIGHT IAW EMB145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — UNSERVICEABLE (COCKPIT) · airframe 18,367 hrs · 15,232 cycles

ON FLIGHT 2995 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WOULD NOT STAY IN THE CRADLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FIRST OFFICER’S FLASHLIGHT BRACKET IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — FAILED (NR 1) · airframe 18,171 hrs · 15,092 cycles

ON FLIGHT 3548 THE CREW REPORTED THAT DURING THE TAKEOFF ROLL A STRONG BURNING ODOR WAS NOTICED IN THE COCKPIT AND CABIN. THE ODOR SUBSIDED AFTER THE CREW ELECTED TO ABORT THE TAKEOFF. REMOVED AND REPLACED ENGINE NR 1 IAW AE MTX WC 71-000-00. OPS AND LEAK CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SREVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 17,896 hrs · 14,892 cycles

DURING B-INSPECTION FOUND THE FORWARD CABIN AND LEFT FORWARD OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY AND BATTERY HOLDER ASSY IAW AMM 33-50-04. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 17,737 hrs · 14,767 cycles

ON FLIGHT 3360 THE CREW REPORTED THAT AFTER THE FLIGHT ATTENDANT TURNED ON THE EMERGENCY LIGHTS TO TEST THEY STAYED ON AND THE CB POPPED (C19). THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS IAW EMB 145 AMM 33-50-00. THE OPERATIONAL CHECK COULD NOT DUPLICATE PROBLEM AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,598 hrs · 14,680 cycles

DURING MAINTENANCE INSPECTION FOUND GALLEY CEILING EMERGENCY LAMP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY CEILING MOUNTED EMERGENCY LAMP IAW EMB 145 AMM TASKS 33-50-09-000-801-A & 33-50-09-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,178 hrs · 11,313 cycles

ON FLIGHT 3418 THE CREW REPORTED THE MAIN DOOR EMERGENCY LIGHT STRIP WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE LAMP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 12,819 hrs · 11,043 cycles

DURING THE PS2 INSPECTION MAINTENANCE FOUND AN INFANT LIFE VEST THAT HAD A TEAR IN THE PROTECTIVE WRAPPING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE INFANT LIFE VEST IAW EMB 145 EEL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — FAULTY (RT ENGINE) · airframe 11,724 hrs · 10,160 cycles

DURING FLIGHT 3225 ON TAKEOFF THE CREW REPORTED A LAVATORY SMOKE DETECTION MESSAGE AND SMOKE ODOR IN THE AFT CABIN. THE CREW ELECTED TO RETURN TO CID. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT ENGINE IAW WC 11-00-00. REMOVED AND REPLACED THE NR 4 CARBON SEAL. OPERATIONAL LEAK CHECK GOOD. NO SMOKE SMELL FROM PACKS WAS DETECTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTACTOR — DAMAGED (NR 1 BUSS)

ON FLIGHT 3633, DURING FLIGHT HEARD THUMP UNDER FLOOR, "FUEL 2 LO LEVEL" ON EICAS, NR 1 FUEL QUANTITY TO DASHES. MULTIPLE WARNINGS IN COCKPIT. ELECTRIC OR SULPHUR ODOR NOTED IN CABIN AFTER LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ESSENTIAL BUSS CONTACTOR OPERATIONAL CHECK GOOD IAW AMM 24-60-03. AIRCRAFT RETURNED TO SERVICE.

Part: DUCT — LOOSE (NR 1 A/C PACK) · airframe 10,063 hrs · 8,876 cycles

ON FLIGHT 4528, CREW REPORTED CABIN PRES ALT WENT ABOVE 10000 FT AND O2 MASKS DEPLOYED IN CABIN. FLIGHT ATTENDANT ADVISED O2 GEN ABOVE C1 CLOSET WAS HOT AND GETTING HOTTER AND COULD DETECT THE ODOR OF SOMETHING BURNING. AIRCRAFT REMOVED FROM SERVICE. INSPECTED O2 GENS IN CABIN FOUND SEVERAL ACTUATED. THEY BECOME VERY HOT AS SPECIFIED IN AMM 35-20-01-200-801-A PARAGRAPH ( I ). FOUND TUBE DUCT LOOSE ON NR 1 PACK SYSTEM. RESCUED DUCT AS REQ IAW AMM 21-51-03. PRES CK GOOD IAW AMM 21-31-00. AIRCRAFT RETURNED TO SERVICE.

Part: PACKING — DAMAGED (NLG) · airframe 7,407 hrs · 6,402 cycles

ON FLIGHT 3788, CREW REPORTED AFTER TAKEOFF DURING GEAR RETRACTION RECEIVED LANDING AIR/GND FAIL MESSAGE AND E1(2) REVERSE DISAGREE EICAS MESSAGE. AIRCRAFT REMOVED FROM SURVIVE. REMOVED AND REPLACED NLG STRUT SEAL. LEFT AND RIGHT TR OPERATIONAL CHECK GOOD IAW EMB AMM 78-31-01. AIRCRAFT RETURNED TO SERVICE.

Part: STRUT — DISCHARGED (NOSE) · airframe 7,402 hrs · 6,398 cycles

ON FLIGHT 3459, CREW REPORTED AFTER TAKEOFF EICAS LANDING GEAR AIR/GND MESSAGES. SHORTLY AFTER RECEIVING EICAS MESSAGE RETURNED TO DFW AND MESSAGE EXTINGUISHED WITH GEAR DOWN ON APPROACH. AIRCRAFT REMOVED FROM SERVICE. FOUND NOSE STRUT DEPLETED OF NITROGEN NOT EXTENDING SERVICED NOSE GEAR WITH NITROGEN IAW 32-20-01 AND VERIFIED FULL EXTENSION OF NOSE STRUT. WEIGHT WHEEL PROX SWITCH GAP AND WIRING WAS VERIFIED IN GOOD WORKING CONDITION IAW FIM 32-63-00. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (RIGHT)

DURING CLIMB-OUT GOT "LAV SMOKE" WARNING, FLIGHT ATTENDANT CALLED SAID LOTS OF SMOKE IN CABIN. REMOVED AND REPLACED RIGHT ENGINE IAW WC NR 71-000-00. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (LAVATORY) · airframe 6,553 hrs · 5,716 cycles

AFTER TAKEOFF "LAV SMOKE WARNING" ODOR OF SMOKE IN COCKPIT AND CABIN FLIGHT ATTENDANT VERIFIED NO FIRE IN LAV BUT COULD STILL ODOR SMOKE. CW GVI OF LAV SIDE WALL AND IN THE LAV GVI OF ENGINE AND RAN BOTH ENGINE TO TAKE POWER. ALL CHECK GOOD AIRCRAFT RETURNED TO SERVICE.

Part: HOSE — CRACKED (LT PYLON) · airframe 6,553 hrs · 5,716 cycles

AFTER TAKEOFF "LAV SMOKE WARNING" SMELL OF SMOKE IN COCKPIT AND CABIN NO FIRE IN LAV BUT COULD STILL SMELL SMOKE. FOUND CRACKED HOSE ASSY IN LEFT PYLON REMOVED AND REPLACED HOSE IAW EMB 135 AMM 20-10-03. OPS CK SATISFACTORY IAW AMM 36-00-00. AIRCRAFT RETURNED TO SERVICE.

Part: CONTACTOR — FAILED (ESSENTIAL BUSS) · airframe 5,716 hrs · 5,025 cycles

RECEIVED EMERGENCY ABNORMAL AND EMERGENCY LIGHT NOT ARMED MESSAGE. ALL FOUR GENERATORS AMPS DOUBLED AFTER APU START, DIVERTED TO GGG. REMOVED AND REPLACED NR 2 ESSENTIAL BUSS CONTACTOR IAW EMB AMM 24-60-03 AND ESSENTIAL TIMER RELAY ONE IAW EMB AMM 20-13-02. ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PROFILE — DAMAGED (ZONE 200) · airframe 4,893 hrs · 4,369 cycles

FOUND SERVICE DOOR SURROUND PROFILE AT STRINGER 15R WAS DAMAGED. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-20-03 AND 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: PROFILE — DAMAGED (ZONE 200) · airframe 4,893 hrs · 4,369 cycles

SERVICE DOOR SURROUND PROFILE AT STRINGER 13R WAS DAMAGED. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-20-03 AND 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: PROFILE — DAMAGED (ZONE 200) · airframe 4,893 hrs · 4,369 cycles

SERVICE DOOR SURROUND PROFILE AT STRINGER 7R WAS DAMAGED. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-20-03, 51-40-02 AND 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: PROFILE — DAMAGED (ZONE 200) · airframe 4,893 hrs · 4,369 cycles

SERVICE DOOR SURROUND PROFILE AT STRINGER 9R FORWARD AND AFT WAS DAMAGED. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-20-03 AND 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: PROFILE — DAMAGED (ZONE 200) · airframe 4,893 hrs · 4,369 cycles

SERVICE DOOR SURROUND PROFILE AT STRINGER 11R WAS DAMAGED. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-20-03 AND 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 4,880 hrs · 4,357 cycles

LEFT OMEGA BEAM CORRODED AT FRAME 20. PERFORMED CUTOUT FOR CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.