N696AE

Part: UNKNOWN — ODOR (CABIN) · airframe 42,551 hrs · 37,945 cycles

DESCENDING AROUND 22000FT , A LOT OF STATIC AND TURBULANCE. SMELL AS IF IT WERE A LIT MATCH AND STRONG SMELL FOR ABOUT 90 SECONDS FACT 31MAR25 20:17 PHL COULD NOT DUPLICATE SMELL RAN PACKS INSPECTED PLANE FOR DAMAGE. NO DEFECTS FOUND. OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — ODOR (ZONE 200) · airframe 42,388 hrs · 37,773 cycles

IN FLIGHT STRONG ELECTRICAL BURNING SMELL IN COCKPIT AND FWD CABIN FACT 05MAR25 22:13 ORF REMOVED AND INSPECTED RELAY PANELS NO DEFECTS NOTED. RAN PACK ON ENGINES AND APU 15 MIN IDLE/15MINUTES 63% N1 NO DEFECTS NOTED AC OK FOR SERVICE

Part: GPU — SMOKE

WHILE AT GATE GPU CONNECTED SAW GPU SMOKING. DESELECTED GPU AND AFTER A/C SHUT DOWN AND POWERED UP. FOUND SOMEBODY TO DISCONNECT GPU AND NOTICED STRONG SMOKE SMELL IN A/C. PERFORMED EXTERNAL POWER TEST IAW 24-40-00-700-801-A OPS CHECK'D OK. VISUALLY INSP GROUND POWER AREA, NO DAMAGE NOTED. OK FOR SERVICE

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052117 L/H OMEGA BEAM GUSSET #7 HAS CORROSION IN MULTIPLE AREAS. RAR L/H OMEGA BEAM GUSSET #7 IAW EMB 145 SRM 51-40-02

Part: SKIN — CRACKED (ZONE 200) · airframe 41,647 hrs · 36,944 cycles

E050565 RH SIDE FUSELAGE UPPER SKIN HAS POSSIBLE CRACK AROUND (1) FASTENER AT FRAME 78. REPAIRED IAW EO1-53-24-0571.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052222 CENTER OMEGA BEAM #5 GUSSET HAS CORROSION. REMOVED AND REPLACED CENTER OMEGA BEAM #5 GUSSET IAW EMB 145 SRM 51-40-02.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 41,647 hrs · 36,944 cycles

E053208 RH SHEAR CLIP AT FR 13 BETWEEN STGR 06R AND STGR 07R CRACKED. REMOVED AND REPLACED RH SHEAR CLIP AT FR 13 BETWEEN STGR 06R AND STGR 07R IAW EMB-145 SRM 51-40-02.

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052082 L/H UPPER SEAT TRACK #6 HAS CORROSION, NICKS AND GOUGES IN MULTIPLE AREAS. REMOVED AND REPLACED L/H UPPER SEAT TRACK #6 IAW EMB 145 AMM 53-01-06.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052289 AFT FUSELAGE 1, FWD LOWER CORNER OF THE CARGO DOOR CUTOUT, THERE IS CORROSION IN THE CORNER. REPAIRED FWD LOWER CORNER OF CARGO DOOR CUTOUT (FR65 SHEAR CLIP LOWER SECTION) IAW EMB145 SRM 53-31-04RE, ITEM 4D, FIG 212 AND PDT EO-53-24-0531

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052237 LH OMEGA BEAM #6 GUSSET HAS CORROSION. REMOVED AND REPLACED LH OMEGA BEAM #6 GUSSET IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052163 LH FLOOR SILL #4 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LH FLOOR SILL #4 IAW EMB 145 SRM 51-40-02

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052079 LAV POTABLE WATER DRAIN CABLE SUPPORT BRACKET HAS CORROSION. REMOVED AND REPLACED LAV POTABLE WATER DRAIN CABLE SUPPORT BRACKET IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052164 LH OMEGA BEAM #4 GUSSET HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LH OMEGA BEAM #4 GUSSET IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052180 CENTER OMEGA BEAM #3 GUSSET HAS CORROSION. REMOVED AND REPLACED CENTER OMEGA BEAM #3 GUSSET IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052355 LH FLOOR SILL #3 HAS CORROSION IN MULTIPLE AREAS. REMOVED CORRODED LH FLOOR SILL #3 AND INSTALLED SERVICEABLE FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 41,647 hrs · 36,944 cycles

E053099 LH OMEGA BEAM SIDEWALL CRACKED AT FR 26. PERFORMED DOUBLER AND FILLER REPAIR ON LH OMEGA BEAM AT FR26 IAW ETD2024-145-023732 REV "B" AND EO1-53-24-0566

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 41,647 hrs · 36,944 cycles

E053101 LH OMEGA BEAM SIDEWALL CRACKED AT FR 28. PERFORMED DOUBLER, FILLER REPAIR FOR L/H OMEGA BEAM SIDEWALL AT FRAME 28 IAW ETD2024-145-023732, REV B AND EO1-53-24-0568.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 41,647 hrs · 36,944 cycles

E053100 LH OMEGA BEAM SIDEWALL CRACKED AT FR 27. PERFORMED DOUBLER, FILLER REPAIR FOR L/H OMEGA BEAM SIDEWALL AT FRAME 27 IAW ETD2024-145-023732, REV B AND EO1-53-24-0567.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 41,647 hrs · 36,944 cycles

E053098 CENTER OMEGA BEAM SIDEWALL CRACKED AT FR 27. PERFORMED CUTOUT AS REQUIRED TO REMOVE DAMAGE FROM CENTER OMEGA BEAM SIDEWALL AT FR 27 AND FABRICATED AND INSTALLED FILLER AND DOUBLER IAW ETD2024-145-023735 REV. C AND EO1-53-24-0569.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052973 LAV POTABLE WATER FILL/DRAIN EXTERNAL REINFORCEMENT PLATE HAS CORROSION. REMOVED AND INSTALLED NEW LAV POTABLE WATER FILL/DRAIN EXTERNAL REINFORCEMENT PLATE IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052532 RH LOWER SEAT TRACK #2 HAS CORROSION. REMOVED AND REPLACED RH LOWER SEAT TRACK #2 AND TORQUED SCREWS IAW EMB 145 AMM 53-01-06.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 41,647 hrs · 36,944 cycles

E052588 SHEAR CLIP AT FR24, BETWEEN STR15R-STR16R IS CRACKED. RAR SHEAR CLIP AT FR24, BETWEEN STR15R-STR16R IAW EMB I45 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 416,447 hrs · 36,944 cycles

LH OMEGA BEAM #3 GUSSET HAS CORROSION. REMOVED AND REPLACED LH OMEGA BEAM #3 GUSSET IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052521 RH FLOOR SILL #2 HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE R/H # 2 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052531 RH UPPER SEAT TRACK #2 HAS POSSIBLE CORROSION AT FR31. RAR RH UPPER SEAT TRACK #2 IAW EMB 145 AMM 53-01-06

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052533 CENTER OMEGA BEAM #2 GUSSET HAS CORROSION. REMOVED AND REPLACED CENTER OMEGA BEAM GUSSET #2 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052555 CENTER OMEGA BEAM #1 GUSSET HAS CORROSION. RAR CENTER OMEGA BEAM #1 GUSSET IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052544 RH FLOOR SILL #1 HAS CORROSION AT FR25. RAR RH FLOOR SILL #1 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052562 LH OMEGA BEAM #2 GUSSET HAS CORROSION. RAR LH OMEGA BEAM #2 GUSSET IAW EMB 145 SRM 51-40-02.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052290 AFT FUSELAGE 1, ON THE LOWER EDGE OF THE CARGO DOOR CUT OUT THERE IS CORROSION. AT FR 65-66, STGR 16L-17L. REMOVED AND REPLACED AFT FUSELAGE1 CARGO DOOR CUTOUT LOWER CENTER SILL IAW EMB145 SRM 51-40-02.

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052428 L/H LWR SEAT-TRACK #1 HAS CORROSION, NICKS AND GOUGES IN MULTIPLE AREAS. REMOVED CORRODED, NICKED, GOUGED L/H LWR SEAT TRACK #1 AND INSTALLED SERVICEABLE #1 SEAT TRACK IAW EMB 145 AMM 53-01-06.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052415 SERVICE DOOR LWR CENTER SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SERVICE DOOR LOWER CENTER SILL IAW EMB145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052167 LH LOWER SEAT TRACK #4 HAS CORROSION AT FR38. REMOVED, AND REPLACED THE LH LOWER SEAT TRACK #4 THAT WAS CORRODED AT FR38 IAW EMB 145 AMM 53-01-06.

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052089 L/H LWR SEAT TRACK #6 HAS CORROSION NICKS AND GOUGES IN MULTIPLE AREAS. REMOVED AND REPLACED L/H LWR SEAT TRACK #6 AND TORQUED SCREWS IAW EMB 145 AMM 53-01-06.

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052092 R/H UPPER SEAT TRACK #5 HAS CORROSION, NICKS AND GOUGES IN MULTIPLE AREAS. REMOVED AND REPLACED R/H UPPER SEAT TRACK #5 IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052161 LH FLOOR SILL #5 HAS CORROSION IN MULTIPLE AREAS INCLUDING PREVIOUSLY BLENDED AREA. REMOVED CORRODED LH FLOOR SILL #5 AND INSTALLED SERVICEABLE FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052160 LH UPPER SEAT TRACK #5 HAS CORROSION AT FR48. REMOVED AND REPLACED LH UPPER SEAT TRACK #5 AT FR48 IAW EMB 145 AMM 53-01-06.

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052093 R/H LWR SEAT TRACK #5 HAS CORROSION, NICKS AND GOUGES IN MULTIPLE AREAS. RAR THE R/H LWR SEAT TRACK #5 IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052154 LH FLOOR SILL #6 HAS CORROSION IN MULTIPLE AREAS. REMOVED CORRODED LH FLOOR SILL #6 AND INSTALLED SERVICEABLE FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,647 hrs · 36,944 cycles

E052107 CENTER OMEGA BEAM GUSSET #6 HAS CORROSION IN MULTIPLE AREAS. RAR CENTER OMEGA BEAM GUSSET #6 IAW EMB 145 SRM 51-40-02.

Part: HOUSING — WORN (HOR STAB BEARING) · airframe 41,647 hrs · 36,944 cycles

E051821 HORIZONTAL STABILIZER L/H AND R/H SPHERICAL BEARING HOUSINGS WORN OUT OF LIMITS. REPAIRED IAW EO1-53-24-0548

Part: NUT PLATE — CORRODED (ZONE 500) · corrosion level 2

E051650 CORROSION AROUND NUT PLATE HOLES ON LH WING AT AFT BELLY PANEL LH LOWER ATTACHMENT FLANGES. RAR LH WING AFT BELLY PANEL LOWER ATTACHMENT FLANGE IAW EMB-145 SRM 51-40-02

Part: SKIN — CRACKED (ZONE 200) · airframe 41,647 hrs · 36,994 cycles

E050563 LH SIDE FUSELAGE UPPER SKIN HAS POSSIBLE CRACK AROUND (2) FASTENERS AT FRAME 78. REPAIRED IAW EO1-53-24-0570

Part: NONE — NONE · airframe 41,545 hrs · 36,853 cycles

RH OVERWING EMERGENCY LIGHT INOP.-C/A-RAR RH OVERWING LIGHT LAMP IAW 145 AMM 33-50-07. OPC GOOD. MEL ITEM RESTORED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,393 hrs · 36,702 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMPIAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPC GOOD. END.

Part: NONE — UNSERVICEABLE (ONLY) · airframe 40,874 hrs · 36,143 cycles

ICE COND-A/I INOP WARNING AND WG A/ICE FAIL CAUTION ILLUNINATED IN CLIMB FL 200 , TEMP-13 SAT TAT WING ICE PROTECTION PUSHBUTTON DID NOT ILLUMINATE . EXITED ICE CONDITION IN FLIGHT AND RAN QRH WITH NO EFFECT. "TRANSFERRED FROM AML PAGE 4922319 ITEM 1"-C/A-RAR DUAL HEAT EXCHANGER OUTLET GRATE AND RUBBER SLEEVE IAW EMB 145 AMM 21-51-02. LEAK CHECKS GOOD NO DEFECTS NOTED.

Part: NONE — NONE · airframe 39,473 hrs · 34,527 cycles

AFT CABIN EMERGENCY FLASHLIGHT HOLDER BROKEN.MEL 25-32 AUTH. #110172M-C ORIGINAL AML P. 4590238 ITEM #1.-C/A-RAR AFT CABIN EMERGENCY FLASHLIGHT ASSY.IAW AMM 33-50-16 OPC CHECK GOOD MEL 25-32 RESTORED

Part: NONE — NONE · airframe 39,433 hrs · 34,481 cycles

# 1 AFT EMERGENCY CABIN FLASHLIGHT HOLDER BROKEN IN REF LG PG 4590238 ITEM-C/A-AFT EMERGENCY CABIN FLASHLIGHT DEFERRED (M) PROCEDURE C/W

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,860 hrs · 33,856 cycles

AFT EMERGENCY CEILING LIGHT, AFT FACING LIGHT INOP.-C/A-RAR'D LIGHT ASSY PER AMM 33-50-15, AND RAR'D INVERTER PER AMM 33-50-11. OPS CHECK IS GOOD

Part: TRANSPONDER — FAILED (AVIONICS BAY) · airframe 38,164 hrs · 33,135 cycles

AVIONICS ISSUES TRANSPONDER 1 FAIL NO FMS GS AFTER ROTATION FD WENT AWAY MFD TRACKING INCORRECTLY NO EICAS MESSAGE EMERGENCY NOT DECLARED. -C/A-INSPECTED FMS 1 AND 2 AND FOUND BOTH GPS 1 AND 2 FAIL ON CAPT'S SIDE PERFORMED RESET OF ELECTRICAL SYSTEM AS PER AMM 24-60-00 AND AMM 34-62-00

Part: DUCT — LEAKING (PNEM SYSTEM) · airframe 37,517 hrs · 32,500 cycles

BLEED 1 LIEAK ENROUTE CLIMBING THROUGH FL210. QRH PROCEDURE COMPLIED WITH, MESSAGE EXTINGUISHED, DECLARED EMERGENCY CHG EQ FLT CONT. C/A: GROUND FOUND NR 7 JOINT LEAKING AIR. R & R NR 7 O-RINGS IN REF TO AMM 36-11-10 AND RE-CONNECTED NR 7 COUPLER. PERFORMED LEAK CHECK ABOUT 15 MINS, IN REF TO AMM 36-11-09. NO LEAKING FOUND AT THIS TIME & NO MESSAGE NOTED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,389 hrs · 32,369 cycles

BROKEN EMERGENCY LIGHT STRIP WIRE AT FLOOR PANEL 231GL. C/A UPON FURTHER INVESTIGATION FOUND PANEL NUMBER TO BE 231GF. REPAIRED EMERGENCY LIGHT STRIP WIRE AT FLOOR PANEL 231GF, IAW EMB 145 SWPM 20-21-00 AND SYS CHK IAW EMB 145 AMM 33-50-00. CHECK GOOD.

Part: SPAR — CRACKED (LT WING) · airframe 37,389 hrs · 32,369 cycles

LT WING SPAR 1 LOWER FLANGE CRACKED AT SCREW HOLE JUST OUTBOARD OF RIB 9 THRU TO THE RADIUS OF THE SPAR FACE. C/A PERFORMED REPAIR OF LT WING SPAR 1, IAW EMB 145 SRM 57-20-05 STEP 3X.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 37,389 hrs · 32,369 cycles

EMERGENCY LIGHT STRIP NR 4 WIRE DAMAGED, ON LIGHT STRIP. FOUND ON OPEN UP. C/A, REMOVED AND REPLACED EMERGENCY LIGHT STRIP NR 4, IAW EMB 145 AMM 33-50-12. PERFORMED OPC, IAW EMB145 AMM 33-50-00. SYS CKS GOOD.

Part: FLOOR SUPPORT — CRACKED (FRAME 23) · airframe 37,389 hrs · 32,369 cycles

LT OMEGA BEAM CRACKED AT LOWER INBOARD RIVET AT FR 23. C/A PERFORMED REPAIR FOR LT OMEGA BEAM CRACKED AT LOWER INBOARD RIVET AT FR 23, IAW EMB ERS-EM-53MR-4187.

Part: SKIN — DENTED (LT WING LE) · airframe 37,389 hrs · 32,369 cycles

THE LT WING LEADING EDGE 2 IS DENTED IN THE POLISHED AREA 38" FROM THE OUTBOARD END, AS MARKED. C/A-ACCOMPLISHED PERMANENT REPAIR TO LT LEADING EDGE 2, IAW ENVOY ERS-EM-57MR-1264.

Part: FRAME — CRACKED (FRAME 72) · airframe 37,389 hrs · 32,369 cycles

FR 72 CRACKED STGR 16L AT RIVET BUCKTAIL. C/A PERFORMED REPAIR TO FR72 LT SECTION, IAW ERS-EM-5300-4180 AND EMB 145 SRM 53-00-04, ITEM 3, FIG.201.

Part: WEB — CORRODED (CARGO DOOR) · airframe 37,389 hrs · 32,369 cycles

CORROSION ON BAGGAGE DOOR LOWER FWD WEBBING. C/A INSTALLED REPAIR DOUBLER AND NUTPLATE ON BAGGAGE DOOR LOWER FWD WEBBING, IAW EMB145 SRM 51-40-02.

Part: DOOR FRAME — CORRODED (CARGO) · airframe 37,389 hrs · 32,369 cycles

SSI 52-30-08 CORROSION ON BAGGAGE DOOR FWD FRAME. C/A INSTALLED FABRICATED LOWER BAGGAGE DOOR FWD FRAME DOUBLER & FILLER, IAW EMB145 SRM 52-30-04RE.

Part: FLOOR SUPPORT — CRACKED (FRAMES 47-50) · airframe 37,389 hrs · 32,369 cycles

RH OMEGA BEAM INBD SUPPORT IS CRACKED BETWEEN FRAMES 47-48-C/A-REMOVED UNSERVICEABLE RH OMEGA BEAM INBD SUPPORT BETWEEN FRAMES 47-50 IAW EMB 145 SRM 51-40-02 AND INSTALLED SERVICEABLE RH OMEGA BEAM SUPPORT FROM FR 47-50 IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 53-23-02.

Part: ATTACH FITTING — DAMAGED (LT AILERON) · airframe 37,389 hrs · 32,369 cycles

LH AILERON PCA ATTACHMENT FITTING LUGS HAVE EDGE DAMAGE 3EA.-C/A-ACCOMPLISHED EO EM-27MR-112 ON LH AILERON PCA FITTING TORQUE WRENCH 7381

Part: FLOOR SUPPORT — CRACKED (FRAME 29) · airframe 37,389 hrs · 32,369 cycles

LT OMEGA BEAM SUPPORT COLUMN AT FRAME 29 IS CRACKED MARKED. C/A REMOVED AND REPLACED LT OMEGA BEAM SUPPORT COLUMN AT FRAME 29, IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 37,389 hrs · 32,369 cycles

SSI 53-30-48 CARGO DOOR CUTOUT LOWER DOOR SILL CORRODED.-C/A-REMOVED CORRODED CARGO DOOR CUTOUT LOWER DOOR SILL IAW EMB 145 SRM 51-40-02.INSTALLED SERVICEABLE CARGO DOOR CUTOUT LOWER SILL IAW EMB 145 SRM 51-40-02.

Part: FRAME — CRACKED (FRM 73) · airframe 37,389 hrs · 32,369 cycles

FR 73 CRACKED STGR 16R-17R. C/A REMOVED AND INSTALLED FR 73 SECTION, IAW EMB 145 SRM 51-40-02.

Part: FITTING — GOUGED (RT AILERON) · airframe 37,389 hrs · 32,369 cycles

RH AILERON DAMPER FITTING GOUGED.-C/A-ACCOMPLISHED EO# EM-27MR-112 TO RH AILERON DAMPER FITTING

Part: STRUCTURE — CORRODED (WASTE SERVICE) · airframe 37,389 hrs · 32,369 cycles

WASTE SERVICE DUMP VALVE HAS CORROSION BETWEEN VALVE AND BUCKET-C/A-RAR LAV WASTE BUCKET IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (FRAME 25) · airframe 37,389 hrs · 32,369 cycles

LT OMEGA BEAM SUPPORT COLUMN AT FRAME 25 IS CRACKED. REMOVED AND REPLACED LT OMEGA BEAM SUPPORT COLUMN AT FRAME 25 IAW EMB 145 SRM 51-40-02.

Part: LIGHT — BROKEN (CABIN) · airframe 37,389 hrs · 32,369 cycles

LT NR 5 EMERGENCY LIGHT STRIP EXTRUSION BROKEN. C/A COMPLETE: REMOVED AND REPLACED LT NR 5 EMERGENCY LIGHT STRIP EXTRUSION, IAW EMB 145 AMM 33-50-12.

Part: WIRE HARNESS — DEBONDED (EMERGENCY LIGHTS) · airframe 37,389 hrs · 32,369 cycles

LT NR 1 EMERGENCY LIGHT STRIP WIRE HARNESS DISBONDED. C/A COMPLETE: DUPLICATE DISCREPENCY, SEE NRWC NR E808485 FOR SIGN OFF AND DETAILS.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,389 hrs · 32,369 cycles

LT NR 4 EMERGENCY LIGHT STRIP EXTRUSION SCREW HOLE ELONGATED. C/A COMPLETE: REMOVED AND REPLACED LT NR 4 EMERGENCY LIGHT STRIP EXTRUSION, IAW EMB 145 AMM 33-50-12.

Part: LIGHT — BROKEN (CABIN) · airframe 37,389 hrs · 32,369 cycles

LT NR 1,NR 2, AND NR 3 EMERGENCY LIGHT STRIP EXTRUSIONS BROKEN. C/A COMPLETE: REMOVED AND REPLACED LT NR 1, NR 2, AND NR 3 EMERGENCY LIGHT STRIP EXTRUSIONS, IAW EMB 145 AMM 33-50-12.

Part: ACTUATOR — LACK OF LUBE (PARKING BRAKE) · airframe 37,197 hrs · 32,176 cycles

PARKING BRAKE STICKY TO SET IT RELEASE.-C/A-LUBED PARKING BRAKE ACTUATOR IAW EMB 145MM 32-44-10.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,068 hrs · 32,057 cycles

SUPPLEMENTAL AFT FLIGHT ATTENDEANT FLASHLIGHT INOP.-C/A-DEFERRED PER MEL 25-53. AUTH #030415-C. REMOVED AND REPLACED AFT FA FLASHLIGHT IAW AMM 33-50-16 AND ETN- EM-33-059. OPS CHECK GOOD. MEL ITEM RESTORED

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 37,000 hrs · 31,984 cycles

FWD CABIN EMERGENCY FLASHLIGHT BRACKET ASSEMBLY BROKEN.-C/A-REMOVED AND REPLCED FWD CABIN EMERGENCY FLASHLIGHT ASSEMBLY. OPS CHECKED GOOD IAW AMM 33-50-16.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,452 hrs · 31,415 cycles

DURING PS-1 CHECK, FOUND LH OVERWING EXTERNAL EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED OVERWING EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — SMOKE (GPU CONNECTOR) · airframe 36,330 hrs · 31,301 cycles

SMOKE REPORTED COMING FROM GPU CONNECTOR UPON DISCONNECTING FROM AIRCRAFT PORT NEEDS INSPECTION-C/A-INSP GPU CONNECTOR NO DEFECT FOUND IAW EMB 145 AMM 20-40-01 & 24-40-01 AC OK FOR SERVICE

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,700 hrs · 30,685 cycles

R/H EXT UPPER EMERGENCY LIGHT INOP-C/A-ADJUSTED EMERGENCY LIGHT IAW EMB 145 AMM 33-50-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,364 hrs · 30,367 cycles

RIGHT SIDE OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RIGHT SIDE OVER WING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,075 hrs · 30,071 cycles

REMOVED LH EXTERIOR EMERGENCY LIGHT ASSEMBLY AND SPACER PLATE ON FWD BELLY FAIRING TO FOM (REPAIR)-C/A-INSTALLED LH EXTERIOR EMERGENCY LIGHT ASSEMBLY AND SPACER PLATE ON FWD BELLY FAIRING IAW EMB145 AMM 33-50-10. OPC GOOD. SEE NRWC3 696-MQT-04135 FOR COMPLETION OF REPAIR MENTIONED IN TURNOVER.

Part: LIGHT — DAMAGED (COCKPIT) · airframe 35,075 hrs · 30,071 cycles

COCKPIT STEP RED EMERGENCY LIGHT IS BROKEN.-C/A-REPOSITIONED AND INSTALLED MISSING HARDWARE ON THE COCKPIT STEP COURTESY LIGHT IAW AMM33-26-06 OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,846 hrs · 29,878 cycles

EXT OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED NR 4 BATTERY CHARGER ASSEMBLY. OPS CHECK FAILED. DEFERRED AFT EXTERNAL EMERGENCY LIGHTS AS PER MEL 33-29 AUTH# 030740D-C. REMOVED AND REPLACED BATTERY CHARGER NR 4 DID NOT FIX. REMOVED AND REPLACED RT EXTERNAL EMERGENCY LIGHT ASSEMBLY, OPS CHECK GOOD IAW 33-50-10 MEL ITEM RESTORED. BATTERY CHARGER ASSY NR 4 P/N 11-0049 S/N 12569 S/N 15038.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,800 hrs · 29,842 cycles

DURING PS-1 CHECK FOUND BOTH AFT OVER THE WING EMERGENCY LIGHTS NOT WORKING. C/A-REMOVED AND REPLACED NR 4 EMERGENCY BATTERY PACK AND POWER SUPPLY IAW AMM 33-50-04, OPS CHECK IAW AMM 33-50-00-700-801-A. OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1ASMI S/N 798326.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,776 hrs · 29,826 cycles

EMERGENCY EXIT SIGN LEFT SIDE INOP (UPPER SIGN). C/A-REMOVED AND REPLACED #3 EMERGENCY LIGHTING BATTERY AND POWER SUPPLY IAW AMM 33-50-04 OPS CHECK GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 15185

Part: CHARGER — FAILED (CABIN) · airframe 34,627 hrs · 29,671 cycles

FOUND RT EMERGENCY OVER WING LIGHT INOP PER PS-2 CHECK. REMOVED AND REPLACED BATTERY CHARGER FOR BATTERY POWER SUPPLY 4 IAW AMM 33-50-04. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 34,498 hrs · 29,540 cycles

LT OVER WING EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED BULB ON LT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. OCK GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 34,498 hrs · 29,540 cycles

RT OVER WING EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED BULB ON RT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. OCK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,432 hrs · 29,467 cycles

REAR EXTERNAL EMERGENCY LIGHTS INOP. C/A-RAR EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-10. REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW AMM 33-50-04 AND 33-50-00. OPS CHECKS GOOD.

Part: LIGHT — ABNORMAL (CABIN) · airframe 34,329 hrs · 29,350 cycles

TRANSFER FROM LOG PG 4294014 ITEM #1 EMERGENCY LIGHTS FLICKERING + GALLEY LIGHTS WOULD NOT OFF IN FLIGHT ACCORDING TO FA-C/A-PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS IAW AMM 33-50-00. OPS CHECK GOOD. PERFORMED OPERATIONAL CHECK OF GALLEY LIGHT IAW AMM 33-29-00. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 34,193 hrs · 29,208 cycles

DURING PS-1 CHECK FOUND LH AND RH OVERWING EMERGENCY LIGHTS INOP-C/A-REMOVED LH AND RH O/W SIDE CENTER FAIRING EMERGENCY LIGHT IAW 33-50-10 SUBTASK 020-004-A AND TROUBLE SHOT LIGHTS IAW EMB-145 AMM 20-20-03. FOUND LH O/W EMERGENCY LIGHT TO BE SHORTED. RAR LH O/W EMERGENCY LIGHT AND REINSTALLED RH O/W EMERGENCY LIGHT IAW EMB-145 AMM 33-50-10 SUBTASK 020-004-A AND 420-004-A. OPS CHECK GOOD IAW 33-50-00-700-801.

Part: COMPUTER — FAILED (STALL WARNING) · airframe 33,950 hrs · 28,939 cycles

STALL PROTECTION TEST LIGHT STAYS ILLUMINATED AFTER TEST. NO AURAL WARNING DURING TEST. C/A-FOUND CMC MESSAGE SPC FAIL. REPLACED STALL PROTECTION COMPUTER IAW AMM 27-36-02-000-801-A & 27-36-02-400-801-A. OPERATIONAL TEST IAW WORK CARD 27-700-20 GOOD. NO FURTHER DEFECTS NOTED.

Part: FIRE BOTTLE — FAILED (CARGO BAY) · airframe 33,600 hrs · 28,602 cycles

SMOKE COMING OF BAG EXTINGISHER SYSTEM "TRANSFERRED TO NRWC 696-MIA-03681". C/A-REMOVED AND REPLACED BOTH BAGGAGE COMP EXT BOTTLES IAW AMM 26-23-04 OPT FOUND OK REFER NRWC 696-MIA-03681 FOR WORK PERFORMED. FIREEX BOTLE-630 CU.IN P/N 34600073-1 S/N 16935F1 LWR.

Part: FLASHLIGHT — CONTAMINATED (FWD CABIN) · airframe 32,997 hrs · 28,048 cycles

FOWARD CABIN FLASHLIGHT HAD WATER INSIDE LED AND MUST BE THUMPED TO GET IT TO WORK. R & R THE FWD FLASHLIGHT ASSY IAW AMM 25-60-00 OPS CHECKED GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 32,788 hrs · 27,880 cycles

DURING PS-1 INSPECTION, FOUND THE LEFT & RIGHT EXTERNAL OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED & REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY & BATTERY, OPS OK.

Part: ACTUATOR — FAILED (HORIZONTAL STAB) · airframe 32,425 hrs · 27,549 cycles

PITCH MAIN TRIM EICAS AT 36000 FT, RMR6 PROCEDURES FOLLOWED. RESET SYSTEM AND PERFORMED AN OPS CHECK OF PITCH TRIM SYSTEM IAW AMM 27-40-00-700-802-A. OPS CHECKED GOOD. REMOVED HORIZONTAL STABILIZER ACTUATOR IAW AMM 27-40-02-000-801-A. REPLACED THE HORIZONTAL STABILIZER ACTUATOR IAW AMM 27-40-02-400-801-A. OPS CHECKED GOOD IAW AMM 27-40-02.

Part: SKIN — GOUGED (FRAME 19) · airframe 32,401 hrs · 27,529 cycles

FUSELAGE SKIN UNDER FWD GPS ANTENNA FOUND GOUGED, AFTER ANTENNA REMOVAL. BLENDED THE GOUGES, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-01, AND 53-10-03, TABLE 101. REMOVED DAMAGED MATERIAL, AND PERFORMED HFEC INSPECTION IAW NDTM 51-00-00-916-801-A NO DEFECTS NOTED. FABRICATED, LOCATED, AND INSTALLED A FILLER AND DOUBLER IAW ETD-2018-145-013915, AND EM-53-071.

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 32,401 hrs · 27,529 cycles

CRACKED SHEAR TIE AT FRAME 68, BETWEEN STRINGERS 6R AND 7R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,401 hrs · 27,529 cycles

SERVICE DOOR FORWARD TRIM EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMEGENCY LIGHT IAW AMM 33-50-09, OPS CHECKED GOOD.

Part: SHEAR TIE — CRACKED (FRAME 66) · airframe 32,401 hrs · 27,529 cycles

CRACK IN THE SHEAR TIE AT FRAME 66, BETWEEN STRINGERS 6L AND 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06.

Part: SPLICE — MISSING (EMERGENCY LIGHT) · airframe 32,401 hrs · 27,529 cycles

FLOOR EMERGENCY LIGHT SPLICE AT FRAME 58 IS MISSING . REPLACED THE SPLICE IAW SWPM 20-21-00. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAME 38) · corrosion level 2 · airframe 32,401 hrs · 27,529 cycles

CORROSION ON INBD SIDE OF THE LT OMEGA BEAM AT CARBON CROSS MEMBER, FRAME 38. REMOVED CORROSION, PERFORMED HFEC INSPECTION, NO DEFECTS NOTED IAW SRM 51-10-03, AND NDTM 51-00-00-916-803-A, FABRICATED, LOCATED, DRILLED AND INSTALLED A REPAIR FILLER AND EXTERNAL ANGLE IAW SRM 53-00-00.

Part: FLOOR SUPPORT — CORRODED (FRAME 29) · corrosion level 2 · airframe 32,401 hrs · 27,529 cycles

CORROSION ON INBD SIDE OF THE LT OMEGA BEAM AT CARBON CROSSBEAM MEMBER AT FRAME 29. BLENDED CORROSION AND REMOVED DAMAGE IAW SRM 53-22-10, AND 53-00-10. PERFORMED NDT OF CUT OUT AREA IAW NDTM 51-00-00-916-801-A00 NO DEFECTS NOTED. FABRICATED A FILLER AND SHIMS, PERFORMED FPI OF REPAIR PARTS, NO DEFECTS NOTED, INSTALLED THE REPAIR AND APPLIED PROTECTIVE COATINGS IAW SRM 53-00-10, CPM 51-20-04, 51-20-05, AND 51-20-06

Part: STRAP — CHAFED (FUSELAGE) · airframe 31,534 hrs · 26,712 cycles

TEAR STRAP AT FR73 BETWEEN STR21L AND 21R CHAFED THROUGH. COMPLIED WITH ERS-EM-53MR-2877.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,534 hrs · 26,712 cycles

AISLE FLOOR LIGHT STRIPS NR 2 AND 3 INOPERATIVE. REMOVED AND REPLACED THE AC/DC INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,496 hrs · 26,671 cycles

EMERGENCY FLOOR LT STRIPS 2 AND 3 INOP. EMERGENCY BATTERIES CHARGED WITH GPU PER AMM 20-40-01-860-801-A. PERFORMED OPC OF EMERGENCY LIGHTING SYSTEM IAW AMM 33-50-00-700-801-A NO FAULTS FOUND.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 31,359 hrs · 26,525 cycles

LAV SMOKE WARNING ON EICAS AND SMOKE ALARM TONE IN GALLEY AT THE GATE. PERFORMED A LAV SMOKE TEST IAW AMM 26-14-00. OPS CHECKED GOOD WITH NO DEFECTS NOTED. NO ODORS OR SIGNS OF SMOKE. SUSPECT HIGH HUMIDITY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,963 hrs · 26,115 cycles

DISCOVERED EMERGENCY AISLE LIGHTS ON ROWS 3-6, DO NOT OPERATE. REMOVED AND REPLACED BATTERY POWER SUPPLY AND CHARGER IAW W/C 33-700-19. OPS CHECKED GOOD.

Part: ADC — MALFUNCTIONED (NR 1) · airframe 30,874 hrs · 26,024 cycles

AT 35,000 FT LOSS OF CA'S AIRSPEED INDICATOR, ALTIMETER, AND VERTICAL SPEED INDICATOR. RED X'S ON ALL SPS ADVANCED ON EICAS. TROUBLESHOT IAW FIM 34-22-00-810-812, AND FIM 34-22-00-810-813. R & R THE NR 1 AIR DATA COMPUTER IAW AMM 34-15-01. OPS CHECKED GOOD. ALSO, SPS ADVANCE MESS RELATED TO ADC FAIL IAW FIM 27-36-00-810-804. OPS CHECKED GOOD

Part: ELECTRONIC UNIT — FAILED (MLG) · airframe 30,265 hrs · 25,504 cycles

ON GEAR RETRACTION, HAD A LANDING GEAR LEVER DISAGREE WARNING ON THE EICAS. FOLLOWED AOM -1 LIST, CYCLING GEAR WITH THE SAME RESULTS. RETURNED TO DEPARTURE. REMOVED AND REPLACED LGEU IAW AMM TASK 32-32-01. OPS CHECKED GOOD.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 30,024 hrs · 25,284 cycles

NR 1 ENGINE ANTI ICE FAIL MESSAGE DURING PNEUMATIC INFLIGHT TEST. TURNED ICE DETECTION KNOB TO AUTO AND THE NR 1 ANTI ICE VALVE REMAINED OPEN. VALVE CLOSED AFTER SECOND ATTEMPT. SWITCHING ALL TO AUTO. PERFORMED CONTINUITY AND VOLTAGE TEST AND FUNCTIONAL TEST OF PRESSURE TRANSDUCER OF NR 1 ANTI-ICE SYSTEM IAW WM 30-20-50 AND AMM 30-21-00-700-801. NO DEFECTS NOTED. REMOVED AND REPLACED THE NR 1 ANTI ICE VALVE IAW AMM 30-21-01. OPS TESTED GOOD.

Part: DISPLAY — FAILED (COCKPIT) · airframe 29,922 hrs · 25,194 cycles

WHILE SITTING AT GATE ON APU PWR STRONG ELEC SMELL FROM CA SIDE THEN CA PFD WENT OFF. FEW MINUTES LATER PFD CAME BACK ON STRONG ODOR. SHUT OFF AC POWER TO AIRCRAFT. SWAPPED FO'S MFD AND CA PFD BACK TO ORIGINAL LOCATIONS. REMOVED AND REPLACED CA PFD IAW AMM 34-22-01. OPC GOOD. MEL RESTORED

Part: SHROUD — DEFECTIVE (CABIN) · airframe 28,844 hrs · 24,160 cycles

MAIN PAX DOOR EMER EXIT LIGHT INOPERATIVE. R & R PAX DOOR HINGE EMER LIGHT SHROUD IAW AMM 25-23-04 STEPS 3 I 1 F-I. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: SENSOR — FAILED (ANTI-ICE SYSTEM) · airframe 28,804 hrs · 24,113 cycles

DURING DESCENT IN ICING CONDITIONS, WING ANTI-ICE FAIL CAUTION MSG & ICE CONDITIONS, ANTI-ICE INOPERATIVE. WARNING MSG PRESENTED ON EICAS. WING ANTI-ICE SELECTION BUTTON SHOWED OPEN INSCRIPTION. R & R PITOT CURRENT SENSOR IAW AMM 30-31-00. OPERATIONS CHECKED GOOD.

Part: PRESSURE SWITCH — FAULTY (RUDDER) · airframe 28,398 hrs · 23,746 cycles

AT 28000 RUDDER 1 & 2 BECAME INOPERATIVE ON EICAS MSG ON & OFF, 25000 MSG REMAINED. TRANSFERRED TO NRWC 696-MIA-02571. REMOVED & INSTALLED BOTH RUDDER PRESS SWITCHES & OPERATIONS CHECKED. ALL CHECKS PASSED IAW 27-23-04.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,291 hrs · 23,657 cycles

AFT CABIN EMER FLASHLIGHT INOPERATIVE. R & R AFT CABIN FLASHLIGHT IAW AMM 25-60-00. OPERATIONS CHECKED GOOD AT THIS TIME. FLASHLIGHT BATTERY PN P4-01-1003-001.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,178 hrs · 23,569 cycles

AFT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW EEL. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,074 hrs · 23,483 cycles

FUSELAGE SKIN CRACK ON FRAME 78, BETWEEN STRINGERS 6R - 7R. FABRICATED & INSTALLED DOUBLER AT FRAME 78, BETWEEN STRINGER 6R & 7R IAW SRM 53-32-01.

Part: YOKE — DAMAGED (ENGINE MOUNT) · airframe 28,076 hrs · 23,484 cycles

ENGINE FWD LOWER YOKE REPAIR & REPLACEMENT. INSTALL OVERSIZE BUSHINGS, INSTALL GUSSET PLATE IAW EO-EM-54MR-386.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,074 hrs · 23,483 cycles

RIGHT OMEGA BEAM INBD SUPPORT IS CRACKED ON AFT END & NEAR FWD END. INSTALLED NEW SERVICEABLE RT OMEGA BEAM INBD SUPPORT, TWO PIECES, OVER WINGBOX AREA IAW SRM 51040-02 & SRM 53-23-02.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 28,074 hrs · 23,483 cycles

LEFT ENG FWD LOWER YOKE CRACKED BEHIND ENG MOUNT. R & R LT ENG LOWER FWD YOKE IAW EO EM-54MR-386.

Part: HINGE FITTING — CORRODED (LT WING) · airframe 28,074 hrs · 23,483 cycles

LEFT SPOILER CTR HINGE FITTING ON WING IS CORRODED. R & R LT SPOILER CTR HINGE FITTING ON WING IAW AMM 57-51-02.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 28,074 hrs · 23,483 cycles

FRAME 65 IS CORRODED NEAR CARGO DOOR LOWER STOP. REMOVED & INSTALLED NEW HALF FRAME & SHEAR CLIP AT FRAME 65 NEAR CARGO DOOR LOWER STOP IAW SRM 53-31-04 PG 204.

Part: DOOR — DENTED (CABIN) · airframe 27,868 hrs · 23,305 cycles

MAIN PAX DOOR HAS A DENT, LOCATED 16" AFT OF DOOR FWD EDGE & 13.5" UP FROM LOWER EDGE. DENT IS 1" L X 1.75" W X .012" D. ACCOMPLISHED PERMANENT REPAIR TO MAIN PAX DOOR DENT IAW ERS-EM-5200-468. DENT ENTERED INTO ADL 6960035.

Part: PROXIMITY SENSOR — FAILED (RT MLG) · airframe 27,534 hrs · 22,954 cycles

AFTER TAKEOFF LOUD BANGING NOISE HEARD IN ACFT RT MLG CYCLED FROM UP TO AMBER. GEAR EXTENDED NORMALLY. R & R RT UPLOCK BOX UPPER PROX SWITCH IAW AMM 32-61-01. PERFORMED GEAR EXTENSION & RETRACTION OPERATIONAL CHECK IAW AMM 32-30-00. OPERATIONS CHECKED SATISFACTORY.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,667 hrs · 22,215 cycles

CEILING EMER LIGHT AT EMER EXIT ON FWD SIDE INOPERATIVE. R & R BATTERY & POWER UNIT NR 4 IAW AMM 33-50-04, DID NOT FIX. REFER TO NRWC 696-DFW-02268. EMER LIGHTING BATTERY PN 2013-1ASMI SN 74445. R & R EMER LIGHT INVERTER AT NR 6 POSITION IAW AMM 33-50-11. OPERATIONS CHECKED GOOD. INVERTER PN 7824-1.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 26,478 hrs · 22,070 cycles

RIGHT WING AFT EMER LIGHT INOPERATIVE. R & R RT WING AFT EMER LIGHT BULB IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,322 hrs · 21,958 cycles

EMERGENCY FLOOR LIGHT STRIPS 4 & 5 & LT & RT SERVICE DOOR EXIT SIGNS INOPERATIVE. R & R EMER LIGHT AC DC INVERTOR NR 5. FLOOR STRIPS 4 & 5 & LT & RT SERVICE DOOR EXIT SIGNS. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,000 hrs · 21,670 cycles

DURING PS 1 INSPECTION FOUND MAIN DOOR EXIT SIGN INOPERATIVE. R & R NR 1 BATTERY & NR 1 CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 SN 14895.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,863 hrs · 21,520 cycles

DURING PS 1 INSPECTION FOUND EMER LIGHT AT MAIN ENTRANCE DOOR INOPERATIVE. R & R NR 1 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DIRTY (RMU) · airframe 25,686 hrs · 21,364 cycles

RMU NR 1 FROZE THEN WENT BRIGHT WHITE. IN CRUISE RMU NR 2 GOES TO COMPLETELY ALL DASHES, KICKED OFF NR 1 TRANSPONDER. REMOVED RMU NR 1 CLEANED CONNECTOR & REINSTALLED IAW AMM 23-81-01. OPERATIONS CHECKED GOOD AT THIS TIME IAW AMM 23-81-00-700-801-A. NO DEFECTS NOTED. REMOVED RMU NR 2, CLEANED CONNECTOR & REINSTALLED IAW AMM EMB 23-81-01. OPERATIONS CHECKED GOOD AT THIS TIME IAW AMM 23-81-00-700-801-A. NO DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,590 hrs · 21,250 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. R & R AFT CABIN FLASHLIGHT IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: GENERATOR — FAILED (NR 4) · airframe 25,536 hrs · 21,187 cycles

WHILE AIRBORNE APU GEN OFF BUS EICAS MSG OCCURRED. IAW MEL 24-5 FLIGHT REQUIRED AN APU GEN TO BE OPERATOR TO CONTINUOUS FLIGHT, RETURNED. APU GEN FUNCTION DEFERRED IAW MEL 24-8. R & R NR 4 ENG GEN IAW WC 24-800-00. OPERATIONS CHECKED GOOD. NO LEAKS NOTED. MEL RESTORED.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 25,277 hrs · 20,977 cycles

EMERGENCY LIGHTING STRIPS FROM 3A TO 7A INOPERATIVE. SECURED CONNECTOR FOR EMER LIGHTS IAW AMM 33-50-08.

Part: CONNECTOR — DIRTY (CABIN) · airframe 25,050 hrs · 20,773 cycles

OVERHEAD CEILING FWD EMER LIGHT BY EMER EXIT INOPERATIVE. REMOVED ELEC CONNECTIONS, CLEANED & REATTACHED CONNECTORS. OPERATIONS CHECKED GOOD IAW AMM 33-50-15.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,611 hrs · 20,328 cycles

LT & RT SIDE CTR FAIRING EMER LIGHTS ARE INOPERATIVE. R & R NR 4 BATTERY & CHARGER ASSEMBLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD AT THIS TIME. BATTERY CHARGER ASSEMBLY PN 11-0049 SN 15916.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,176 hrs · 19,961 cycles

LEFT EXTERNAL OVERWING EMERGENCY LAMP INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY & CHARGER IAW AE WC 33-700-17 & 33-700-19, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,144 hrs · 19,927 cycles

AFT LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE IAW PS-1 INSPECTION. R & R LT & RT OVERWING EMERGENCY LIGHTING BULBS IAW AMM 33-50-07, NO FIX. R & R NR 4 EMERGENCY BATTERY & POWER PACK IN OVERHEAD LT PAX COMPARTMENT. CLEANED LIGHT BULB CONTACTS, OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,028 hrs · 19,802 cycles

FOUND LT & RT EXTERIOR OVERWING EMERGENCY LIGHT NOT ON. R & R NR 4 EMERGENCY LIGHT BATTERY CHARGER & BATTERY PACK IAW AMM 33-50-04. R & R RT EXTERIOR OVERWING EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: BRACKET — CRACKED (FLASHLIGHT) · airframe 24,012 hrs · 19,791 cycles

CAPTAIN'S FLASHLIGHT BRACKET CRACKED. R & R CAPTAIN'S FLASHLIGHT IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: CUP — DAMAGED (EMERGENCY EXIT) · airframe 23,908 hrs · 19,734 cycles

RT EMERGENCY EXIT LOWER RECESS CUP DAMAGED. INSTALLED NEW RT EMERGENCY EXIT LOWER RECESS CUP IAW SUB TASK 25-23-03-420-001 STEP I 1 D PART TASK.

Part: SKIN — SCRATCHED (EMERGENCY EXIT) · airframe 23,907 hrs · 19,733 cycles

RT OVERWING EMERGENCY EXIT HAS SURFACE SCRATCHES ALONG UPPER OUTER SURFACE & AFT EDGE OUTER SURFACE. INNER LOWER OBSCURED HANDLE HAS LOWER SECTION BROKEN. REPAIRED OUTER SURFACE SCRATCHES OF RT EMERGENCY EXIT IAW CPM 51-21-07. NO FURTHER DEFECTS NOTED IAW NRWC 696-DFW-01736 FOR DAMAGED OBSCURED HANDLE, RECESS CUP.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 23,907 hrs · 19,733 cycles

MAIN CABIN AFT EMERGENCY FLASHLIGHT MISSING. DEFERRED AFT EMERGENCY LIGHT FLASHLIGHT IAW MEL 25-53 AUTH 030253-C. REINSTALLED AFT FLASHLIGHT & OPERATIONS CHECKED GOOD IAW AMM 33-51-01. MEL ITEM IS RESTORED.

Part: FAN — MALFUNCTIONED (COCKPIT) · airframe 23,907 hrs · 19,733 cycles

FLIGHT CREW DECLARED EMERGENCY LANDING FOR ELEC SMELL WITH SMOKE IN COCKPIT. FOUND COCKPIT RECIRCULATION FAN BURNED. R & R NR 1 RECIRCULATION FAN IAW AMM 21-24-01 & OPERATIONS CHECKED GOOD. PERFORMED ETN-EM-72-034 & NO ELEC SMELL OR SMOKE WAS FOUND.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,905 hrs · 19,730 cycles

ON SHORT FINAL APPROXIMATELY 30 SEC AFTER WE PUT THE GEAR DOWN WE STARTED SMELLING WHAT WE THOUGHT WAS ELEC SMOKE, BUT WE WERE NOT SURE ON THE LANDING ROLL OUT. THE FLIGHT ATTENDANT CALLED & SAID SHE SMELLED IT. NO SMELL WAS NOTED IN THE AFT CABIN AT ANY POINT. THE SMELL SUBSIDED SUBSTANTIALLY ON THE LANDING ROLL OUT. PERFORMED FIM TASKS IAW 21-20-00-810-803A. FOUND NO DEFECTS ALL LIGHTS WORK & ALL AVIONICS OPERATE NORMAL. PERFORMED ETN EM-72-034, FOUND NO DEFECTS & NOTICED NO SMELL IN COCKPIT OR CABIN.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 23,707 hrs · 19,567 cycles

DURING MBV INSPECTION FOUND FRAME SUPPORT CLIP AT FRAME 71, STRINGER 16L IS CRACKED. REMOVED AND REPLACED CRACKED FRAME SUPPORT CLIP AT FRAME 71, STRINGER 16L IAW SRM 51-40-02. RESTORED SURFACE FINISH TO AFFECTED AREA OF EXTERNAL FUSELAGE IAW CPM 51-21-07 AND ETN-EM-51-091.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 23,707 hrs · 19,567 cycles

DURING MBV INSPECTION FOUND FRAME SUPPORT CLIP AT FRAME 72, STRINGER 16L IS CRACKED. REMOVED AND REPLACED CRACKED FRAME SUPPORT CLIP AT FRAME 72, STRINGER 16L IAW SRM 51-40-02. RESTORED SURFACE FINISH TO AFFECTED AREA OF EXTERNAL FUSELAGE IAW CPM 51-21-07 AND ETN-EM-51-091.

Part: FIREWALL — CRACKED (APU BAY) · airframe 23,707 hrs · 19,567 cycles

DURING MBV INSPECTION FOUND APU FIRE WALL IS CRACKED AT THE UPPER RT ATTACHMENT POINT AS VIEWED FROM THE AFT SIDE. REPAIRED AS PER PART C OF EO EM-53AD-1883.

Part: LIGHT — CRACKED (CABIN) · airframe 23,707 hrs · 19,567 cycles

LEFT NR 1 & LEFT NR 2 EMERGENCY LIGHT STRIPS ARE CRACKED. R & R LT NR 1 & LT NR 2 EMERGENCY LIGHT STRIPS IAW AMM 33-50-12.

Part: LIGHT — BROKEN (CABIN) · airframe 23,707 hrs · 19,567 cycles

LEFT NR 7 EMERGENCY PROXIMITY LIGHT HAS A BROKEN WIRE. R & R LT NR 7 EMERGENCY PROXIMITY LIGHT IAW AMM 33-50-12.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 23,679 hrs · 19,543 cycles

DURING CLIMB ABOUT FL260 NI & ITT SPUN DOWN THEN INTERMITTENTLY WIND UP & DOWN. N1 APPEARED NORMAL AFTER IGNITERS ON BUT ITT STAYED LOW 300 ENG 1. PERFORMED ENG RUNS IAW RR MM 72-00-00. COULD NOT DUPLICATE THIS PROBLEM AT THIS TIME.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,656 hrs · 19,521 cycles

BOTH RT & LT EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & CHARGER ASSEMBLY IAW AMM 33050--04. OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 23,510 hrs · 19,409 cycles

BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R BOTH OVERWING EMERGENCY LIGHTS BATTERY CHARGER IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 23,474 hrs · 19,378 cycles

DURING MAINTENANCE INSPECTION ON FLIGHT 3005 FOUND FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT MISSING. THE ACFT WAS REMOVED FROM SERVICE. R & R FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT IAW EMB 145 AMM 25-51-00 & OPERATIONAL CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 23,474 hrs · 19,378 cycles

DURING MAINTENANCE INSPECTION ON FLIGHT 3005 FOUND LT & RT WING UPPER EMERGENCY LIGHTS INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 4 BATTERY CHARGER IAW EMB 145 AMM 33-50-04. OPERATIONS CHECKED GOOD MEL 33-50-04 AUTH 120368D-C IS RESTORED. THE ACFT WAS RETURNED TO SERVICE.

Part: NUT PLATE — BROKEN (EXTERIOR LIGHT) · airframe 23,472 hrs · 19,375 cycles

RIGHT EXTERIOR EMERGENCY OVERWING EMERGENCY LIGHT HAS A BROKEN NUTPLATE. R & R RT OVERWING EXTERIOR EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. CANNOT PERFORM OPERATIONS CHECK LIGHT IS MEL IAW AML.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,232 hrs · 19,207 cycles

NR 1 EMERGENCY LIGHT BATTERY INOPERATIVE. R & R BATTERY IAW MAINTENANCE W/C 33-700-19, OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,076 hrs · 19,091 cycles

EMERGENCY LIGHT ABOVE SERVICE DOOR INOPERATIVE. R & R NR 2 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD IAW WC 33-700-17.

Part: CONTROL UNIT — INOPERATIVE (TE FLAPS) · airframe 22,708 hrs · 18,795 cycles

CREW REPORTED THAT ON FINAL APPROACH, SELECTED FLAP 9 DEGREES. RECEIVED A FLAP FAIL MESSAGE ON EICAS AND THE FLAPS REMAINED AT 0 DEGREES. RAN THROUGH FLAP FAIL CHECKLIST AND DECLARED AN EMERGENCY . LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. ACTIVATED FECU IAW AMM 27-53-00. OPS CHECKED IAW AMM 27-53-00-700-801-A. R & R THE FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02. OPS CHECK GOOD. NO DEFECTS NOTED. PERFORMED FLAP FAIL/FLAP LOW SPEED OPS CHECK IAW WC 27-700-28. OPS CHECK GOOD. NO DEFECTS NOTED. MEL RESTORED. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DEFECTIVE (FLASHLIGHT) · airframe 21,589 hrs · 17,885 cycles

DURING B INSPECTION FOUND THE COPILOTS FLASHLIGHT INTERMITTENTLY CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT CRADDLE ASSEMBLY AND REMOVED AND REPLACED THE FLASHLIGHT BATTERY UNIT IAW EMB145 AMM 33-50-16-000-801A AND 33-50-16-400-801A AND 33-51-01-700-802A. PART # P4-01-1003-001. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,589 hrs · 17,885 cycles

DURING B INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT WILL NOT TURN ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S EMERGENCY FLASHLIGHT IAW EMB AMM 33-50-16-00-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,336 hrs · 17,680 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT AT FORWARD CEILING PANEL INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT AT FORWARD CEILING PANEL IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 21,267 hrs · 17,621 cycles

ON FLIGHT 3307 THE CREW REPORTED THAT ON FINAL APPROACH THEY NOTICED STRONG ELECTRICAL FUMES IN THE COCKPIT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ELECTRICAL SMELL COMING FROM AUTOFLIGHT GUIDANCE CONTROLLER. REMOVED AND REPLACED THE AUTOFLIGHT GUIDANCE CONTROLLER IAW AMM 22-11-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY PACK AND CHARGER ASSY.

Part: ACTUATOR — LEAKING (TE FLAP) · airframe 20,570 hrs · 17,065 cycles

ON FLIGHT 4009 THE CREW REPORTED THEY WERE CLEARED FOR AN ILS 27L INTO ORD AND RECEIVED A FLAP FAIL MESSAGE WHEN TRYING TO DEPLOY FLAPS 9, FLAPS STAYED AT 0. THE CREW PERFROMED THE AOM CHECKLIST AND ASKED FOR VECTORS OFF THE APPROACH AND DECLARED AN EMERGENCY. THE CREW RETURNED TO PIT AND LANDED WITHOUT INCIDENT. THE FLAPS NEVER DEPLOYED PAST 0. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND LEFT NR 3 FSA LEAKING. REMOVED AND REPLACED THE LEFT NR 3 ROOT FLAP ACTUATOR IAW EMB 145 AMM 27-51-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PDU — FAILED (TE FLAP) · airframe 20,477 hrs · 16,992 cycles

ON FLIGHT 4350 THE CREW REPORTED THAT ON APPORACH THE FLAPS FAILED IN THE ZERO POSITION. THE CREW COULD NOT OBTAIN ANY FLAPS ON LANDING. THE CREW DECLARED AN EMERGENCY AND RAN THE APPROPRIATE CHECKLIST. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT FLAP SYSTEM IAW EMB 145 AMM 27-51-00. REMOVED AND REPLACED THE FLAP POWER DRIVE UNIT IAW EMB 145 AMM 27-53-04. THE OPERATIONAL CHECK WAS GOOD, NO FURTHER DISCREPANCIES FOUND AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — LACK OF LUBE (TE FLAP) · airframe 20,457 hrs · 16,974 cycles

ON FLIGHT 4018 THE CREW REPORTED THAT THE FLAP FAILED WHEN SELECTING FLAP 9 ON APPROACH INTO ORD. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED FLAP SCREW JACK ACTUATOR GEAR - LUBRICATION IAW FIN REF 27-51-00. FOLLOWING FIM REF 27-51-00. FILLED ALL ACTUATORS. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (COCKPIT) · airframe 20,357 hrs · 16,891 cycles

DURING B INSPECTION FOUND THE CAPTAIN'S FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT CRADLE 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: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 19,324 hrs · 16,077 cycles

DURING COURTESY CHECK, FOUND THE FORWARD FLIGHT ATTENDANT’S FLASH LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASH LIGHT AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE FRAME) · airframe 19,236 hrs · 15,997 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 65 HAS OUT OF LIMITS WITH CORROSION AT LOWER STIKER PLATE NUTPLATES. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER PER ETD 2012-145-006915. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,499 hrs · 16,213 cycles

DURING SCHEDULED MAINTENANCE FOUND THE BAGGAGE DOOR SILL HAS CORROSION AT NUT PLATE (4 EACH). THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CARGO DOOR SILL, LOCATED & DRILLED NEW SILL BLENDED CORROSION ON EXISTING SILL REF SRM 51-10-03, 100 PERCENT MATERIAL LOSS, OUT OF LIMITS. INSTALLED NEW SILL PER SRM 51-40-02. PAINT: RE-STORED FINISH IAW SRM 51-21-06. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 19,492 hrs · 16,204 cycles

DURING SCHEDULED MAINTENANCE FOUND THE EMERGENCY LIGHT STRIP WIRES PULLED/BROKEN AT FERRULE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESOLDERED LEFT NR 1 EMERGENCY LIGHT WIRES REFERENCING EMB 145 SWPM 20-30-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (DOOR CUT OUT) · corrosion level 2 · airframe 19,237 hrs · 15,997 cycles

CARGO DOOR CUT OUT FWD LOWER CORNER CORROSION AT LOWER STRIKER PLATE AND RIVETS. REMOVED CORROSION ON FWD STRIKER PLATE REF SRM 51-20-00. REMOVED STRIKER PLATE FOM.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,237 hrs · 15,997 cycles

CORROSION ON FR68 "L" SHAPE AT THRESHOLD. REPAIRED FR 68 "L" SHAPE IAW EM-53MR-1129.

Part: FLOOR SUPPORT — CRACKED · airframe 15,997 hrs · 15,997 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT OUTBOARD OMEGA BEAM SUPPORT CRACKED AT FR47. AIRCRAFT REMOVED FROM SERVICE. REMOVED LEFT OUTBOARD OMEGA BEAM SUPPORT, LOCATED AND DRILLED NEW PART AND INSTALLED REF SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,236 hrs · 15,997 cycles

DURING MAINTENANCE INSPECTION, FOUND THE RIGHT FLOOR SILL CORRODED BETWEEN FRAMES 39 AND 44. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CORROSION REF SRM 51-10-03 NOMINAL .050 INCH REMAINING MATERIAL .032" OUT OF LIMITS OF SRM 53-23-10 FIGURE 101. REMOVED CORRODED SILL REF SRM 51-40-02, TRANSFERRED HOLES TO NEW SILL REF SRM 51-20-03 AND INSTALLED NEW SILL USING REF SRM 51-40-02. REMOVED FLOOR SILL FROM FR 36-41 REF SRM 51-410-02 LOCATED AND DRILLED NEW SILL USING REF SRM 51-20-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CORRODED (FUSELAGE) · airframe 19,499 hrs · 16,213 cycles

DURING SCHEDULED MAINTENANCE FOUND THE BAGGAGE DOOR CUTOUT FORWARD LOWER CORNER CORRODED AT NUT PLATE FOR TRIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED RIB DUE TO OUT OF LIMIT CORROSION. LOCATED & DRILLED NEW RIB IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 19,236 hrs · 15,997 cycles

DURING MAINTENANCE INSPECTION, FOUND A CRACK ON RIGHT BELLY PANEL SUPPORT FORWARD OF RIGHT INBOARD FLAP TQ BOX. AIRCRAFT REMOVED FROM SERVICE. REMOVED CRACKED BELLY PANEL SUPPORT RIGHT USING REF SUM 51-40-00. FABRICATED NEW ANGLE IAW SRM 51-40-02. TREATED AND PRIMED IAW CPM 51-23-04 AND CPM 51-28-05. INSTALLED NEW BELLY PANEL SUPPORT IAW SRM 51-40-02 AND TOP COATED IAW CPM 51-23-06. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 19,499 hrs · 16,213 cycles

DURING SCHEDULED MAINTENANCE FOUND THE RIGHT OUTBOARD OMEGA BEAM SUPPORT CRACKED AT FR47 AS MARKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED OUTBOARD OMEGA BEAM SUPPORT REF 51-40-02. LOCATED AND DRILLED NEW OUTBOARD OMEGA SUPPORT AT FRAME 47. INSTALLED NEW OUTBOARD OMEGA BEAM SUPPORT RIGHT SIDE FR47 REF SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,182 hrs · 15,953 cycles

DURING B-INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW AMM TASKS 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,084 hrs · 15,895 cycles

DURING MAINTENANCE INSPECTION FOUND THE FUSELAGE AFT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT CHARGER AND BATTERY IAW EMB WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (CABIN) · airframe 18,093 hrs · 15,136 cycles

ON FLIGHT 3933 THE CREW REPORTED THE REAR FLASHLIGHT HOLDER CLIP WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT HOLDER IAW EMB 145 AMM 33-50-16. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 16,819 hrs · 14,161 cycles

ON FLIGHT 2705 THE CREW REPORTED THAT DURING THE CLIMB AFTER TAKEOFF, RECEIVED A LAVATORY SMOKE WARNING. THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. THE PACKS BLEEDS AND RECIRCULATION FANS WERE TURNED OFF AND THE SMOKE CLEARED. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT ENGINE IAW W/C 71-000-00. THE OPERATIONAL CHECK WAS GOOD. NO LEAKS NOTED. NO SMOKE IN CABIN NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,664 hrs · 13,323 cycles

FOR FLIGHT 3637 IT WAS DISCOVERED THAT THE EMERGENCY LIGHTS AT ROW 8-12 AND THE OVERWING EMERGENCY LIGHTS WERE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY POWER SUPPLY AND BATTERY HOLDER ASSEMBLY AT LOCATION NR 3. THE OPERATIONAL CHECK WAS NORMAL IAW AMM 33-50-04 AND WORK CARD 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SOCKET — DAMAGED (CABIN) · airframe 14,897 hrs · 12,739 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY FLOOR PROXIMITY LIGHT NUMBER 4 HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW SOCKET ON FLOOR PROXIMITY LIGHT NR 4 IAW EMB SWP 20-50-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — FAULTY (NR 1) · airframe 14,081 hrs · 12,096 cycles

ON FLIGHT 3444 THE CREW REPORTED AN ODOR IN THE COCKPIT DURING TAKEOFF WITH THE PACKS ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 1 ENGINE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CD PLAYER — MALFUNCTIONED (CABIN) · airframe 13,966 hrs · 11,997 cycles

ON FLIGHT 4287 DURING CRUISE THE FLIGHT ATTENDANT REPORTED A BURNING ODOR FROM THE CD PLAYER. THE CREW PULLED CIRCUIT BREAKER J15AND THE ODOR WAS GONE. THE AIRCRAFT CONTINUED TO CMH AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CD PLAYER IAW EMB AMM 23-32-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BURNED (COCKPIT) · airframe 13,099 hrs · 9,745 cycles

ON FLIGHT 3505, CREW REPORTED THEY DECLARED AN EMERGENCY DUE TO ELECTRICAL ODOR IN THE COCKPIT DURING CRUISE. ODOR DISSIPATED DURING DECENT ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTS CHART HOLDER DUE TO LIGHT STAYS ON WHEN CLOSED AND MELTED AREA AROUND LIGHT BULB. IAW MM 25-12-11 CHART HOLDER OPS CHECK GOOD. NO BURNING SMELLS. ACFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND CARGO DOOR SILL UPPER AND LOWER SURFACES CORRODED. MAINT REPLACED CARGO DOOR SILL IAW SRM 51-40-02. ACFT WAS RETURNED TO SERVICE. (K)

Part: CARBON SEAL — FAULTY (NR 1 ENGINE) · airframe 8,174 hrs · 7,260 cycles

ON FLIGHT 3799, CREW REPORTED SMOKE IN CABIN AND COCKPIT WHEN POWER WAS APPLIED FOR TAKEOFF. ABORTED TAKEOFF AND EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO GATE UNEVENTFULLY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY IAW WORK CARD 71-000-00. REMOVED AND REPLACED THE NR 4 CARBON SEAL. UPON DISASSEMBLY THE NR 4 CARBON SEAL WAS NOTED WITH SEVERAL INDICATIONS IN THE CARBON SEALS. THE OUTER CARBON SEAL HOUSING WAS ALSO NOTED WITH OIL STAINING AND COKING DUE TO OIL LEAKING PAST THE CARBON SEAL SEGMENTS. OPERATIONAL CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 8,175 hrs · 7,260 cycles

ON FLIGHT 3731, CREW REPORTED UPON REACHING TAKEOFF SPEED NOTED SMOKE SMELL IN THE COCKPIT. CREW ABORTED TAKEOFF AND RETURNED TO GATE.

Part: ANTENNA — DEBONDED (COMMS) · airframe 7,695 hrs · 6,901 cycles

IN CLOUDS COMM 1 AND 2 BECOMES UNREADABLE AND UNLINK GOES NO COMM CREW ELECTED TO RETURN TO MQT. FOUND COMM 3 ANTENNA UNBOUNDED REBOUNDED COMM 3 ANTENNA. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 5,575 hrs · 4,493 cycles

LAVATORY SMOKE WARNING AFTER TAKEOFF. REMOVED AND REPLACED NUMBER TWO ENGINE IAW EMB AMM 72-00-00. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS, RETURNED AIRCRAFT TO SERVICE.

Part: HOLDER — DEFECTIVE (COCKPIT)

AIRCRAFT RETURNED TO FIELD FOR SMOKE SMELL IN COCKPIT COMING FROM CAPTAINS YOKE AREA. RAI CAPTAIN YOKE CHART HOLDER, IAW EMB 145 AMM 25-12-11, OPS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. (M)