N677AE

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 42,702 hrs · 38,047 cycles

RH OVERWING EXTERIOR AFT EMERGENCY LIGHT INOP. RAR LIGHT ASSY IAW AMM TASK33-50-10

Part: SLEEVE — FAULTED (HEAT EXCHANGER) · airframe 42,097 hrs · 37,380 cycles

IN FLIGHT PACK 2 VALVE CLOSED AND BLEED 2 VALVE CLOSED MSG ON EICAS . FOLLOWED QRH PROCEDURES MSGS CAME BACK FOLLOWED BY BLEED 2 LEAK. R/R LOWER 2.5 SLEEVE ON DUAL HEAT EXCHANGER IAW AMM 21-51-02 OPS CHECK GOOD AND LEAK CHECK GOOD AT THIS TIME. A/C OK FOR SERVICE.

Part: TRUNNION — GOUGED (ZONE 100) · airframe 41,845 hrs · 37,092 cycles

F035546 L/H MLG UPPER AFT TRUNNION INBD BOLT HOLE AT LOWER EDGE IS GOUGED. REPAIRED GOUGED L/H MLG UPPER AFT TRUNNION INBD BOLT HOLE AT LOWER EDGE IAW PIEDMONT EO1-57-25-0121 AND ETD2025-145-904528

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F035293 COCKPIT CO-PILOT L/H FLOOR BEAM GUSSET AT FR-14 AROUND NUT-PLATE HOLE HAS CORROSION. BLENDED CORROSION ON COCKPIT CO-PILOT L/H FLOOR BEAM GUSSET AT FR-14 AROUND NUT-PLATE HOLE IAW EMB 145 SRM 51-10-03. BLENDED AREA ACCEPTED PER PIEDMONT EO1-05-25-0116 AND ETD2025-145-904989

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F035290 COCKPIT CO-PILOT L/H FLOOR BEAM GUSSET BETWEEN FR-09/10 HAS CORROSION. BLENDED CORROSION ON COCKPIT CO-PILOT L/H FLOOR BEAM GUSSET BETWEEN FR-09/10 IAW EMB 145 SRM 51-10-03. BLENDED AREA ACCEPTED PER PIEDMONT EO1-05-25-0116 AND ETD2025-145-905000.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F035266 COCKPIT PILOT L/H FLOOR BEAM GUSSET BETWEEN COLUMN YOKE TO L/H RUDDER PEDAL HAS CORROSION. BLENDED CORROSION ON COCKPIT PILOT L/H FLOOR BEAM GUSSET BETWEEN COLUMN YOKE TO L/H RUDDER PEDAL IAW EMB 145 SRM 51-10-03. BLENDED AREA ACCEPTED PER PIEDMONT EO1-05-25-0116 AND ETD2025-145-905004

Part: BRACKET — CRACKED (ZONE 200) · airframe 41,845 hrs · 37,092 cycles

F035294 COCKPIT L/H LATERAL OVERHEAD BRACKET IS CRACKED. REMOVED AND REPLACED COCKPIT L/H LATERAL OVERHEAD BRACKET IAW EMB145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F035081 L/H UPPER SEAT TRACK #1 HAS CORROSION IN MULTIPLE AREAS. RAR THE L/H UPPER SEAT TRACK #1 IAW EMB 145 AMM 53-01-06

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 414,845 hrs · 37,092 cycles

F034875 LH # 2 FLOOR BEAM GUSSET CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED LH # 2 FLOOR BEAM GUSSET IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034852 1 RH #1 FLOOR SILL CORRODED IN MULTIPLE AREAS. RAR RH #1 FLOOR SILL WITH NEW SERVICEABLE FLOOR SILL IAW EMB145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034883 LH LOWER SEAT TRACK #2 CORRODED. REMOVED AND REPLACED LH LOWER SEAT TRACK #2 IAW EMB 145 AMM 53-01-06

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034887 RH LOWER SEAT TRACK #2 CORRODED. : REMOVED AND REINSTALLED SSI 53-20-11 RH LOWER SEAT TRACK #2 IAW EMB 145 AMM 53-01-06

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034886 RH LOWER SEAT TRACK #1 CORRODED. REMOVED AND REPLACED SSI 53-20-11 RH LOWER SEAT TRACK #1 IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034868 ) CENTER FLOOR BEAM GUSSET HAS MULTIPLE SPOTS OF CORROSION BETWEEN FR47 AND FR49. REMOVED AND REPLACED CENTER FLOOR BEAM GUSSET BETWEEN FR47 AND FR49 IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034889 RH LOWER SEAT TRACK #3 CORRODED. RAR RH LOWER SEAT TRACK #3 IAW EMB 145 AMM 53-01-06.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F035015 CORROSION ON SERVICE DOOR CENTER SILL. REMOVED AND INSTALLED NEW SERVICEABLE SERVICE DOOR CENTER SILL IAW EMB145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F035086 L/H UPPER SEAT TRACK #4 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED L/H UPPER SEAT TRACK #4 IAW EMB 145 AMM 53-01-06

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F035030 CENTER FLOOR OMEGA BEAM GUSSET BETWEEN FR-54/55 HAS CORROSION. REMOVED AND REPLACED THE CENTER FLOOR OMEGA BEAM GUSSET BETWEEN FR-54/55 IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034884 LH LOWER SEAT TRACK #3 CORRODED. BLENDED TO REMOVE CORROSION ON LH LOWER SEAT TRACK #3 IAW EMB 145 SRM 51-10-03. UPON EVALUATION, MEASURED AND FOUND BLENDED AREAS ON LH LOWER SEAT TRACK #3 TO BE WITHIN ALLOWABLE LIMITS IAW EMB145 SRM 53-00-11AD. APPLIED ALOIDINE TREATMENT TO BLENDED AREAS AS REQUIRED IAW EMB145 CPM 51-21-04. NO DEFECTS NOTED

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F035016 CORROSION ON DIAMOND GUSSET AT FRAME 20. RAR DIAMOND GUSSET AT FRAME 20 IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F035002 CORROSION ON LH INBD #1 SEAT TRACK. : REMOVED AND REPLACED L/H INBD SEAT TRACK #1 IAW EMB 145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 370,092 cycles

F034853 RH #2 FLOOR SILL CORRODED IN MULTIPLE AREAS. RAR R/H #2 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034876 LH # 3 FLOOR BEAM GUSSET CORRODED IN MULTIPLE AREAS. RAR WITH NEW SERVICEABLE LH # 3 FLOOR BEAM GUSSET. IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034869 CENTER # 2 FLOOR BEAM GUSSET CORRODED IN MULTIPLE AREAS. RAR CENTER FLOOR BEAM #2 GUSSET IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034870 CENTER FLOOR BEAM GUSSET HAS MULTIPLE SPOT OF CORROSION BETWEEN FR39 AND FR43. RAR CENTER FLOOR BEAM GUSSET BETWEEN FR39 AND FR43 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F035018 CENTER FLOOR BEAM GUSSET BETWEEN FR-59/61 HAS CORROSION. REMOVED AND RELACED CENTER FLOOR BEAM GUSSET AT FR 59/61 IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034871 RH LOWER SEAT TRACK #5 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED RH LOWER SEAT TRACK #5 IAW EMB 145 AMM 53-01-06.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F035019 LAV FLOOR POTABLE WATER FITTING SUPPORT HAS CORROSION ON UPPER SURFACE AND UNDERNEATH. RAR LAV FLOOR PORTABLE WATER FITTING SUPPORT IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (OZNE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034850 LH #3 FLOOR SILL CORRODED IN MULTIPLE AREAS. RAR R/H #3 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

LH FLOOR BEAM GUSSET HAS MULTIPLE SPOTS OF CORROSION BETWEEN FR48 AND FR53. REMOVED AND REPLACED THE LH FLOOR BEAM GUSSET BETWEEN FR48 AND FR53 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

LH #2 FLOOR SILL CORRODED IN MULTIPLE AREAS. R & R L/H #2 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F035082 L/H UPPER SEAT TRACK #2 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED L/H UPPER SEAT TRACK #2 IAW EMB 145 AMM 53-01-06.

Part: BEAM — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034731 LH CARBON BEAM WEB(BANANA PANEL) AT FR 61 CORRODED AT STR 16L. : RAR LH CARBON BEAM WEB(BANANA PANEL) IAW EMB 145 SRM 51-40-02

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034712 : FUSELAGE SKIN PREVIOUS REPAIR FILLER BETWEEN FR 67/68 STR21L/21R CORRODED. REPAIRED FUSELAGE SKIN PREVIOUS REPAIR FILLER BTW FR 67-68 AND BTW STR 21L-21R IAW PIEDMONT EO1-53-25-0119 AND EMB 145 SRM 53-31-01 RE ITEM C TYPE A, TABLE 209

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034700 CARGO LH SIDE FLOOR SILL CORRODED, IN LAVATORY AREA, BETWEEN FR 60/61. RAR CORRODED CARGO L/H SIDE FLOOR SILL BETWEEN FR 60/61 IN LAVATORY IAW EMB 145 SRM51-40-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F034758 : CARGO DOOR CUTOUT FR 65 SHEAR CLIP CORRODED BETWEEN STR16L/17L. REPAIRED CORROSION ON CARGO DOOR CUTOUT FR 65 SHEAR CLIP BETWEEN STR 16L/17L IAW PIEDMONT EO1-53-25-0114 AND EMB 145 SRM 53-31-04, ITEM 4D, FIG 212

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

CARGO DOOR CUTOUT LOWER SILL CORRODED. REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB 145 SRM 51-40-02.

Part: FRAME — CRACKED (ZONE 200) · airframe 41,845 hrs · 37,092 cycles

F034720 FRAME 66 CRACKED AT STR 16R. REMOVED CRACKED FR 66 LOWER FRAME SECTION AND INSTALLED SERVICEABLE FRAME 66 SECTION IAW EMB 145 SRM 51-40-02.

Part: BUSHING — MIGRATED (ZONE 300) · airframe 41,845 hrs · 37,092 cycles

F033969 RUDDER I LOWER HINGE FITTING UPPER DOUBLE HAT BUSHING LOWER HAT BUSHING MIGRATED. REAMED RUDDER 1 LOWER HINGE FITTING POSITION 2 HOLE, FABRICATED AND INSTALLED NEW DOUBLE HAT BUSHINGS IAW EMB 145 SRM 55-00-02 ITEM 3, FIG. 202 SHEETS 4,5,6 AND EO1-55-25-0113.

Part: FITTING — WORN (ZONE 600 AILERON) · airframe 41,845 hrs · 37,092 cycles

F033783 RH AILERON ACTUATOR ATTACHMENT FITTING WORN. REMOVED AND REPLACED WORN RH AILERON ACTUATOR ATTACHMENT FITTING IAW PIEDMONT EO1-57-25-0115 AND ETD2025-145-905221.

Part: TUBE — CORRODED (ZONE 500 ELEVATR) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F033428 LH ELEVATOR INBD AND OTBD MASS BALANCE TUBES CORRODED. REPAIRED CORROSION ON LH ELEVATOR INBD AND OTBD MASS BALANCE TUBES IAW PIEDMONT EO1-05-25-0116, IC2003-145-1934A AND SB145-55-0040 REV 1

Part: TUBE — CORRODED (ZONE 600 ELEVATR) · corrosion level 2 · airframe 41,845 hrs · 37,092 cycles

F033429 RH ELEVATOR INBD AND OTBD MASS BALANCE TUBES CORRODED. REPAIRED CORROSION ON RH ELEVATOR INBD AND OTBD MASS BALANCE TUBES IAW PIEDMONT EO1-05-25-0116, IC2003-145-1934A AND SB145-55-0040 REV 1

Part: SUPPORT BRACKET — DENTED (ZONE 800) · airframe 41,845 hrs · 37,092 cycles

F033509 CARGO DOOR LWR EDGE "L" SUPPORT BRACKET IS DENTED. REMOVED DENTED CARGO DOOR LWR EDGE "L" SUPPORT BRACKET AND INSTALLED SERVICEABLE SUPPORT BRACKET IAW EMB 145 SRM 51-40-02.

Part: SKIN — CHAFED (ZONE 800) · airframe 41,845 hrs · 37,092 cycles

F033507 CARGO DOOR INTERNAL LWR SKIN CHAFED BETWEEN VB3 AND HB4. : ACCOMPLISHED REPAIR ON CARGO DOOR INTERNAL SKIN BETWEEN VB3-HB4 IAW PIEDMONT EO1-52-25-0130 AND EMB 145 SRM 52-30-01, ITEM #12, FIGURE 213, 51-40-02.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 41,845 hrs · 37,092 cycles

F033051 NLG WHEEL WELL UPPER SKIN POSSIBLE CRACK JUST ABOVE THE RH NOSE SPIN BRAKE. PERFORMED DOUBLER REPAIR TO THE NLG WHEEL WELL UPPER SKIN AT THE RH NLG SPIN BRAKE IAW EMB 145 SRM 53-11-10RE, ITEM 2, FIG 201, SHEET 1 AND 2 AND EO1-53-25-0125.

Part: LAMP — INOPERATIVE (MAIN CABIN) · airframe 41,766 hrs · 36,984 cycles

MAIN CABIN DOOR GROUND ILUMINATION EMERGENCY LIGHT INOP-C/A-RAR LAMP AT MAIN CABIN DOOR GROUND ILUMINATION EMERGENCY LIGHT AND CLEANED GROUND AND SOCKET AT MAIN CABIN DOOR GROUND ILUMINATION EMERGENCY LIGHT IAW AMM 33-50-06 AND 20-13-21. OPC GOOD.

Part: LAMP — INOPERATIVE (COCKPIT) · airframe 41,766 hrs · 36,984 cycles

COCKPIT OVERHEAD EMERGENCEY LIGHT INOP-C/A-RAR LAMP AT COCKPIT OVERHEAD EMERGENCY LIGHT IAW AMM 33-50-05. OPC GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 41,662 hrs · 36,861 cycles

FA EMERGENCY FLASHLIGHT MOUNT BROKEN.MEL 25-32 - AUTH# 030213M-C. ORIGINAL LOG PG. 4809005-C/A-RAR AFT FA EMERGENCY FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16. OPC GOOD MEL RESTORED

Part: NONE — NONE · airframe 41,529 hrs · 36,706 cycles

ROW 12 CEILING EMERGENCY LIGHT INOP-C/A-RAR BATTERY POWER SUPPLY #3 IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A. NO FIX. RAR BATTERY PACK #3 IAW EMB AMM 33-50-04-000-802-A AND 33-50-04-400-802-A. NO FIX. RAR EMERENCY LIGHT INVERTER #4 IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPS CHECK GOOD. END.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 40,679 hrs · 35,726 cycles

DURING PS-2 FOUND EMERGENCY FLASHLIGHT ON TOLIET FORWARD PARTITION WOULD NOT CHARGE.-C/A-RAR EMERGENCY FLASHLIGHT ASSEMBY ON TOLIET FOWARD PATITION IAW EMB AMM 33-50-16. OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 40,456 hrs · 35,469 cycles

FWD CABIN EMERGENCY FLASHLIGHT NOT TAKING CHARGE-C/A-RAR FWD CABIN EMERGENCY FLASHLIGHT ASSY IAW ETN-33-059 OPS CHECK GOOD

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,358 hrs · 35,358 cycles

SEAT 12C WALL EMERGENCY SIGN INOP-C/A-T/S IAW WM 33-50-50-005 RAR #5 INNVERTER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,218 hrs · 35,200 cycles

ROW 12 CEILING EMERGENCY EXIT SIGN INOP-C/A-RAR #3 EMERGENCY BATTERY AND CHARGER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. NO FIX. RAR #4 INVERTER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPC GOOD. END.

Part: SIGN — INOPERATIVE (CABIN) · airframe 40,194 hrs · 35,168 cycles

EMERGENCY EXIT SIGN ON WALL JUST AFT OF RH OVER WING EMEGENCY EXIT INOP-C/A-TROUBLESHOT EMERGENCY EXIT SIGN. FOUND BAD [3] BATTERY POWER SUPPLY. RAR BATTERY POWER SUPPLY [3] IAW W/C 33-700-19 OPS CHECK GOOD

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,182 hrs · 35,153 cycles

CENTER CEILING EXIT SIGN INOP-C/A-RAR CENTER CEILING EMERGENCY EXIT SIGN OPC GOOD IAW AMM 33-50-15

Part: CHARGER — INOPERATIVE (EXTERIOR LIGHT) · airframe 40,160 hrs · 35,130 cycles

RH LWR EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR #2 EMERGENCY LIGHT BATT AND CHARGER OPC GOOD IAW W/C 33-700-19

Part: CLAMP — DAMAGED (FLASHLIGHT ASSY) · airframe 39,720 hrs · 34,647 cycles

AFT EMERGENCY FLASHLIGHT BRACKET CLAMP DAMAGED. C/A: R & R AFT EMERGENCY FLASHLIGHT SYSTEM ASSEMBLY, IAW EMB145 AMM 33-50-16. OPERATIONS CHECK GOOD.

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 39,272 hrs · 34,180 cycles

FA'S FLASHLIGHT HOLDER DAMAGED. C/A: R & R FA'S FLASHLIGHT HOLDER, IAW EMB 145 AMM 33-50-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,157 hrs · 34,061 cycles

FOUND EMERGENCY FLOOR LIGHT #3 INOP.

Part: FAN — FAILED (RECIRCULATION) · airframe 39,157 hrs · 34,061 cycles

CHEMICAL/RUBBERY SMELL NOTED IN COCKPIT. SMELL SEEMED TO DISAPATE WITH PACK 1 TURNED OFF. R & R COCKPIT RECIRCULATION FAN DUE TO LOUD HIGH PITCH WHINE. COMPLIED WITH ETN-EM-72-034 ENG ODOR EVENT TROUBLESHOOTING SUPPLEMENT NO ODORS DETECTED IN COCKPIT OR CABIN. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,157 hrs · 34,061 cycles

FOUND EMERGENCY FLOOR LIGHT NR 3 INOP. R & R CABIN EMERGENCY FLOOR PROXIMITY STRIP LIGHT NR 3 IAW AMM 33-50-12 AND ETN-EM-33-058. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,059 hrs · 33,940 cycles

EMERGENCY EXIT SIGN AT SEAT 3B INOPERATIVE. R & R THE NR 3 INVERTER IAW AMM 33-50-11-000-801-A, AND 33-50-11-400-801-A. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (MAIN DOOR) · airframe 38,762 hrs · 33,620 cycles

MAIN DOOR EMERGENCY LIGHT LAMP INOP-C/A-REMOVED AND REOLACED MAIN DOOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-06. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 38,635 hrs · 33,491 cycles

HIGH SPEED ABT 105KTS DUE TO STALL PROTECTION 1 AND 2 INOP WARNING ON TAKE-OFF ROLL- REJECTED TAKE OFF-C/A-REF NRWC 677-ORD-04250 FOR CMC DOWNLOAD FOUND SPC FAIL ON CMC.T/S IAW EMB 145 FIM 27-36-00.RAR SPC IAW EMB 145 AMM 27-36-02. / PERFORMED OPS CHECK OF STALL PROTECTION SYSTEM IAW EMB 145 AMM 27-36-00OPS CHECK GOODNO DEFECTS NOTED AT THIS TIME

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,568 hrs · 33,445 cycles

RH EMERGENCY LIGHT INOP (AFT)-C/A-REMOVED AND REPLACED RH EMERGENCY (AFT) LAMP IAW EMB 145 AMM 33-50-10 OPC O.K.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,262 hrs · 33,242 cycles

LH SIDE CENTER FAIRING EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR LH SIDE CENTER FAIRING EXTERNAL EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 37,808 hrs · 32,892 cycles

DURING INITIAL CLIMB AIRCRAFT DID NOT PRESSURIZED CABIN ALTITUD EQUALIZED AT 8000 FEET COMPLIED WITH PROCEDURES AND LANDED IN MIA.-C/A-REMOVED AND REPLACED PRESSURIZATION DIGITAL CONTROLLER IAW AMM 21-31-01. PERFORMED OPS CHK IAW AMM 21-23-00. OPS CHK GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 37,668 hrs · 32,767 cycles

RIGHT HAND OVER WING LARGE EXIT SIGN INOP-C/A-PERFORMED OPS CHECK PER EMB145 AMM 33-50-00-05 , OPS CHECK GOOD

Part: SKIN — CRACKED (FRAME 75) · airframe 37,582 hrs · 32,682 cycles

DURING HMBV INSPECTION, QC FOUND 2 CRACKS AROUND RIVETS ON RH REAR FUSELAGE I SKIN AT FR 75 BETWEEN STGR 1R AND 3R. -C/A-PERFORMED PERMANENT REPAIR TO CRACKS ON RH REAR FUSELAGE I SKIN AT FR 75 BETWEEN STGR 1R AND 3R IAW EMB 145 SRM 53-31-01-RE REPAIR #11. (REPAIR MATERIALS: DOUBLER ALCLAD 2024-T3, 0.080?, FILLER: ALCLAD 2024-T3, 0.063?, ANGLE: ALCLAD 2024-T3, 0.050?, SHIM ALCLAD 2024-T3, 0.032?)

Part: RIB — CRACKED (LT WING) · airframe 37,582 hrs · 32,682 cycles

DURING HMBV INSPECTION, QA FOUND THE LH WING RIB 21 CRACKED INSIDE 551CB-C/A-PERFORMED PERMANENT REPAIR ON LH WING RIB 21 IAW EMB 145 SRM 57-20-07 REPAIR 4. MATERIALS; FILLER- AL 2024T3 (0.040) DOUBLER; AL7475 T761 (0.050) / SHIM; AL2024T3 (0.032)

Part: FITTING — GOUGED (RT AILERON) · airframe 37,582 hrs · 32,682 cycles

DURING HMBV INSPECTION QC FOUND RH AILERON DAMPENER FITTING GOUGED. -C/A-REMOVED AND REPLACED RH AILERON DAMPENER FITTING IAW EO EM-27MR-112.

Part: WEB — GOUGED (CARGO DOOR) · airframe 37,582 hrs · 32,682 cycles

DURING HMBV INSPECTION, QA FOUND THE BAGGAGE DOOR INTERNAL WEB GOUGED ABOVE AND AFT OF THE VENT PANEL-C/A-PERFORMED PERMANENT REPAIR ON THE BAGGAGE DOOR INTERNAL WEB ABOVE AND AFT OF THE VENT PANEL IAW EMB 145 SRM 52-30-01 AND ETN-EM-52-043. REPAIR DOUBLER: 2024 T3 0.050?

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,582 hrs · 32,682 cycles

DURING HMBV INSPECTION, QC FOUND THE CARGO DOOR CUTOUT LWR SILL CORRODED. -C/A-REMOVED AND REPLACED CARGO DOOR LWR SILL IAW EMB 145 SRM 51-40-02 AND 51-20-03.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,582 hrs · 32,682 cycles

CABIN EMERGENCY PROXIMITY LIGHT STRIP WIRE BROKEN AT FR 58-C/A-COMPLETE:REPAIRED WIRE FOR CABIN EMERGENCY PROXIMITY LIGHT STRIP AT FR 58 IAW EMB 145 SWPM 20-21-00 AND AMM 33-50-12 CHECKS GOOD

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,582 hrs · 32,682 cycles

BROKEN WIRE ON THE AIRCRAFT SIDE OF THE #8 EMERGENCY LIGHT STRIP CONNECTOR.-C/A-COMPLETE:REMOVED AND REPLACED AIRCRAFT SIDE WIRE CONNECTOR AT EMERGENCY LIGHT STRIP #8 IAW EMB 145 SWPM 20-50-00. EASI# 102

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,582 hrs · 32,682 cycles

EMERGENCY FLOOR PROX LIGHTS # 6, 7 AND 8 INOP.-C/A-COMPLETE:REMOVED AND REPLACED #4 BATTERY AND BATTERY CHARGER, IAW ENVOY W.C 33-700-19

Part: LIGHT — INOPERATIVE (RT WING) · airframe 37,444 hrs · 32,544 cycles

RH WING FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED RH FWD EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A OPC GOOD

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 37,184 hrs · 32,290 cycles

SERVICE DOOR EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-000-801-A OPC GOOD AT THIS TIME NO FURTHER DEFECTS NOTED AT THIS TIME END.

Part: HOLDER — SMOKE (COCKPIT) · airframe 37,097 hrs · 32,218 cycles

SMOKE VISIABLE ON CAPTAIN`S YOKE CONTROL COLOUMN LEFT SIDE AROUND THE STEERING DISENGAGE BUTTON ELECTRICAL SMOKE ODOR AS WELL AS VISIABLE WHITE SMOKE. CONFIRM SMOKE SMELL FOUND CA CHART HOLDER WITH SPARKING MARKS BEHIND BULBS AND CB COCKPIT READING OPEN RAR CA CHART HOLDER IAW AMM 25-12-11 OPS CHECK GOOD IAW AMM 33-11-00 AIRCRAFT OK TO RETURN TO SERVICE

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 36,999 hrs · 32,118 cycles

CABIN RATE STARTED CLIMBING RAPIDLY AT AROUND 10,000 FT. CABIN RATE WENT TO DASHES. PRESN AUTO FAIL DISPLAYED ON EICAS.-C/A-DEFERRED AUTOMATIC AND MANUAL PRESSURIZATION CONTROL AS PER MEL 21-19 AUTH#060231DM-C DUE TO LACK OF PARTS. M PROCEDURES C/W. BOTH OUTFLOW VALVES HAVE BEEN LOCKED OPEN AS PER MEL. USING THE INFO IN THE KVA RAR THE PRESSURIZATION DIGITAL CONTROLLER IAW EMB AMM 21-31-01-000-801-A & 21-31-01-400-801-A RESTORED M-PROCEDURES FOR OPC, OPC FAIL, RECOMPLIED WITH M-PROCEDURES MEL REAMINS OPEN END. OPERATIONAL CHECK GOOD IAW EMB-145 AMM 21-31-00 MEL ITEM RESTORED C/W M-PROCEDURES REVERSE

Part: CHARGER — INOPERATIVE (CABIN) · airframe 36,938 hrs · 32,040 cycles

GALLEY EMER LIGHTS AND FLOOR STRIPS 1-3 INOP. C/A-REMOVED AND REPLACED #2 EMERGENCY BATTERY AND CHARGER IAW W/C 33-700-19. PERFORMED OPS CHECK IAW W/C 33-700-17. OPC GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 113277

Part: LIGHT — NOT REPORTED (EXTERIOR) · airframe 36,914 hrs · 32,015 cycles

EXTERNAL EMERGENCY LIGHTS OF THE RT SIDE FORWARD LOWER FAIRING - REMOVAL/ INSTALLATION. C/A-RAR EXTERNAL EMERGENY LIGHT IAW AMM TASK 33-50-10-04.

Part: HANDLE — LACK OF LUBE (PARKING BRAKE) · airframe 36,826 hrs · 31,906 cycles

PARKING BRAKE DIFFICULT TO SET. C/A-LUBED ON EMERGENCY AND PARKING BRAKE HANDLE REF AMM 32-44-10. OPS CHECK GOOD. OK FOR SERVICE.

Part: PROXIMITY SENSOR — FAILED (LT MLG) · airframe 36,234 hrs · 31,464 cycles

LG AIR GROUND FAIL IN AIR RETURN TO GATE. REMOVED & REPLACED LEFT MAIN GEAR FWD WOW PROXIMITY SWITCH, AND NOSE LANDING GEAR WOW PROXIMITY SWITCH IAW AMM 32-63-01. ACCOMPLISHED AMM LANDING GEAR PROX SWITCH ADJ/TEST IAW AMM 32-63-05, ACCOMPLISHED EXTENSION/ RETRACTION ADJ/TEST 4 CYCLES IAW AMM 32-30-00, OK FOR SERVICE.

Part: GASKET — DAMAGED (BLEED AIR SYS) · airframe 36,213 hrs · 31,448 cycles

E1 A/ICE FAIL MSG CLIMBING FL180. DEFERRED AS PER MEL 30-11 AUTH 020470DM-C C/W M PROCEDURES. MEL REFERENCE CHANGED FROM 30-11 TO 30-12 PER MOC 801520. M PROCEDURES FOR 30-11 REVERSED. REMOVED AND REPLACED GASKET AND CLAMP ON E1 UPPER CHECK VALVE IAW AMM 36-11-01. MEL RESTORED

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 35,490 hrs · 30,684 cycles

ON TAKE-OFF AT 700' ENGINE 2 BLEED LEAK. -C/A-FOUND BLEED LINE JOINTS IN AFT AVI AND CARGO LEAKING. REMOVED AND REPLACED NR 2 BLEED LINE O-RINGS AT JOINT LOCATIONS 14 AND 24 IAW AMM 36-11-10. LEAK CHECK GOOD. PERFORMED LEAK CHECK OF NR 2 BLEED LINE JOINT IN AFT AVIONICS LOCATION NR 24 IAW AMM TASK 36-11-10. LEAK CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (ANTI-ICE SYS) · airframe 35,308 hrs · 30,468 cycles

A/ICE FAIL WING ON DESCENT WHILE IN ICING CONDITIONS THRUST INCREASE AND RECYCLE OF BUTTON DID NOT CORRECT ISSUE. PERFORMED ANTI ICE OPS CK WITH CREW SYSTEM OPS NORMAL NO DEFECTS NOT A/C OK FOR SERVICE IAW AMM 30-00-00.

Part: CARBON SEAL — DAMAGED (NR 2 ENGINE) · airframe 35,057 hrs · 30,214 cycles

NR 2 ENG SMOKE ON SHUTDOWN. R&R OF SHAFT PLUG/ MAGNETIC CARBON BREATHER SEAL DEFERRED PER ETN-EM-79-015.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 34,931 hrs · 30,105 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED ROLLER IAW AMM. 52-10-01 & OPS CHK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,644 hrs · 29,836 cycles

DURING A PS-1 CHECK, FOUND THE EMERGENCY LIGHTS INOPERATIVE, COCKPIT FLOOD LIGHT, AISLE LIGHT 1 AND EXTERNAL WING TO FUSELAGE FAIRNG LIGHT. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY HOLDER ASSY AND NR 1 EMERGENCY BATTERY CHARGER ASSY IAW AMM 33-50-04. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. R & R EXTERNAL WING TO FUSELAGE EMERGENCY LIGHT IAW AMM 33-50-10. PERFORMED AN OPS CHECK IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,447 hrs · 29,634 cycles

FLOOR EMERGENCY LIGHTS AT THE EMERGENCY EXIT ROW INOPERATIVE. REMOVED AND REPLACED THE LIGHTS, OPS CHECKED GOOD IAW AMM 33-50-12.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,053 hrs · 29,243 cycles

DURING A CHECK, FOUND EMERGENCY EXIT SIGN IN THE FRONT OF SEAT 3B TO BE INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-13. OPS CHECKED IAW AMM 33-50-00, CHECKED GOOD. NO DEFECTS NOTED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 33,936 hrs · 29,159 cycles

FLOOR EMERGENCY LIGHTS FROM ROW 1 TO ROW 7 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW 33-50-04. AND PERFORMED AN OPS CHECK IAW WC 33-700-17. OPS CHECKED GOOD.

Part: LIGHT — CRACKED (CABIN) · airframe 32,887 hrs · 28,138 cycles

LT NR 8 EMERGENCY LIGHT STRIP IS CRACKED. REMOVED AND REPLACED LT NR 8 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,887 hrs · 28,138 cycles

SKIN CRACK LOCATED ON FR 78/ STR 4R-5R. INSTALLED REPAIR DOUBLER & FILLER, EXTERNAL FUSELAGE SKIN AT FR 78/ STR 4R-5R IAW SRM 53-32-01

Part: FRAME — CHAFED (FUSELAGE) · airframe 32,887 hrs · 28,138 cycles

FRAME 59 IS CHAFED AT STRINGER 8L. REMOVED CHAFED REINFORCEMENT AT FR 59 AND STR 8L, INSTALLED SERVICEABLE REINFORCEMENT IAW GPM 17-13, SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,887 hrs · 28,138 cycles

PAX DOOR EMERGENCY LIGHT INOP. RECONNECTED PAX DOOR EMERGENCY LIGHT AS REQUIRED. OPC GOOD.

Part: VALVE — FAILED (RT PACK) · airframe 32,096 hrs · 27,420 cycles

PACK VALVE CLOSED DURING CLIMB. INSPECTED NR 1 PACK DUCKS FOR LEAKS IAW AMM 21-51-14. FOUND THREE LEAKS AND REPLACED THREE SLEEVES IAW ETN-EM-21-056 AND R & R PACK VALVE NR 1 IAW AMM 21-51-01 OPS AND LEAK CHECKED GOOD

Part: CONNECTOR — DIRTY (NR 1 PACK) · airframe 32,095 hrs · 27,419 cycles

NR 1 & 2 PACK VALVE CLOSED. CLEANED AND RESECURED THE CONNECTOR ON PACK NR 1 VALVE AND OPERATIONAL CHECKED SATISFACTORY IAW AMM-21-51-00.

Part: SWITCH — INOPERATIVE (STAB TRIM) · airframe 31,932 hrs · 27,286 cycles

MAIN PITCH TRIM MAIN INOPERATIVE. PERFORMED OPS CHECK OF MAIN PITCH TRIM SYS IAW AMM 27-40-00. OPS CHECKED GOOD. REMOVED AND REPLACED FIRST OFFICER`S CONTROL YOKE TRIM SWITCH IAW AMM 27-40-03. OPS TESTED GOOD IAW AMM TASK 27-40-00-700-802-A/500.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 31,874 hrs · 27,233 cycles

PTRIM MAIN INOP BACKUP TRIM STILL FUNCTIONING SEE LOG BOOK PG 1404871 "TRANSFERRED TO NRWC 677-DFW-02513". REMOVED AND REPLACED HSCU IAW AMM 27-40-01. OPS CHECK GOOD. REF NRWC 677-DFW-02513 FOR CORRECTIVE ACTION.

Part: ACTUATOR — FAILED (PITCH TRIM) · airframe 31,875 hrs · 27,234 cycles

AT FL 30.3, RECEIVED A PTRIM MAIN INOPERATIVE, NON EICAS. USED BACKUP PITCH TRIM TO DIVERTED. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR IAW AMM 27-40-02. OPS CHECKED GOOD IAW AMM TASK 27-40-02-700-801-A/500.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,514 hrs · 26,901 cycles

RIGHT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,292 hrs · 26,656 cycles

UPPER RT WING EMERGENCY LIGHT IS INTERMITTANT. R & R THE LAMP. OPS TESTED OK IAW AMM 33-50-10.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 30,711 hrs · 26,170 cycles

PTRIM MAIN INOPERATIVE MESSAGE ON EICAS IN FLIGHT. NO AUTOPILOT MISTRIMS THIS TIME. R & R HSA IAW AMM 27-40-02. NO MESSAGE ON EICAS. OPS CHECK NORMAL.

Part: CONTROL UNIT — FAILED (HORIZ STAB) · airframe 30,710 hrs · 26,169 cycles

PTRIM MAIN INOPERATIVE, MESSAGE ON EICAS IN FLIGHT. ALSO, AP MISTRIM CAUTION MSG CAME ON. BUT EXTINGUISHED AUTO PILOT WAS DISCONNECTED. T/S CMC MESSAGE HORIZONTAL STABILIZER CONTROL UNIT FAILURE IAW FIM 27-43-00-810-801A. R & R THE HSCU IAW AMM 27-40-01 AND PERFORMED OP'S CHECK IAW AMM 27-40-00. OP'S CHECK IS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,656 hrs · 26,111 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R&R SERVICE DOOR EMERGENCY LIGHT IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS GOOD.

Part: SUPPORT BRACKET — CRACKED (FWD FUSELAGE) · airframe 28,128 hrs · 23,578 cycles

INSIDE FWD HYD COMPARTMENT HAS POSSIBLE CRACK ON AFT UPPER SUPPORT BRACKET. PERFORMED DOUBLER REPAIR TO HYD COMPARTMENT SUPPORT BRACKET IAW ERS-EM-53MR-1169. SEE TURNOVER FOR DETAILS.

Part: SUPPORT — CRACKED (FAIRING) · airframe 28,128 hrs · 23,578 cycles

LEFT OVERWING UPPER FAIRING SUPPORT AT FRAME 49 IS CRACKED. PERFORMED DOUBLER REPAIR FOR CRACK AT LT OVERWING UPPER FAIRING SUPPORT IAW ERS-EM-53MR-1177 & SRM 53-23-12.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 28,128 hrs · 23,578 cycles

FLOOR PROXIMITY LIGHT NR 2 CONNECTOR BROKEN ON ACFT SIDE, SP9038. R & R FLOOR PROXIMITY LIGHT NR 2 CONNECTOR, SP-9038, ON ACFT SIDE IAW SWPM 20-21-00. SEE BOW 182880 FOR OPERATIONS CHECK.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 28,128 hrs · 23,578 cycles

RIGHT OMEGA BEAM PREVIOUS REPAIR DOUBLER UNDER LAVATORY GUSSET CORRODED AT NUTPLATE HOLE. REPAIRED RT OMEGA BEAM PREVIOUS REPAIR DOUBLER IAW ERS-EM-53MR-1164.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,128 hrs · 23,578 cycles

EXTERNAL FUSELAGE LIGHTNING STRIKE DAMAGE BETWEEN FRAME 14 - 15 ON STRINGER 19R. REPAIRED EXTERNAL FUSELAGE LIGHTNING STRIKE DAMAGE IAW ERS-EM-53MR-1147.

Part: FRAME — CHAFED (FUSELAGE) · airframe 28,128 hrs · 23,578 cycles

FRAME 80 IS CHAFED BELOW APU FIRE BOTTLE MOUNT. REPAIRED FRAME 80 IAW ERS-EM-57MR-1146.

Part: BEAM — CORRODED (FUSELAGE) · airframe 28,128 hrs · 23,578 cycles

LEFT BEAM IS CORRODED NEAR CROSSBEAM BETWEEN FRAME 58 & 59. REPAIRED HAT BEAM IAW ERS-EM-53MR-1150.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · airframe 28,128 hrs · 23,578 cycles

SERVICE DOOR BOTTOM FRAME HAS 4 CORRODED NUTPLATE HOLES. REPAIRED SERVICE DOOR BOTTOM FRAME NUTPLATE HOLES IAW ERS-EM-52MR-304.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,128 hrs · 23,578 cycles

FUSELAGE EXTERNAL SKIN HAS 3 DENTS AFT OF FRAME 65 AT STRINGER 20L & 21L. REPAIRED 3 DENTS ON FUSELAGE SKIN IAW ERS-EM-53MR-1138.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,128 hrs · 23,578 cycles

FUSELAGE SKIN IS PITTED NEAR FRAME 60 STRINGER 21R. REPAIRED EXTERNAL SKIN PITTING NEAR FRAME 60 IAW ERS-EM-53MR-1148.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,128 hrs · 23,578 cycles

FUSELAGE EXTERNAL SKIN HAS 3 DENTS BETWEEN FRAME 65 - 66, STRINGER 19L. DENTED AREA ON FUSELAGE SKIN ACCEPTED AS IS IAW ERS-EM-53MR-1139.

Part: DOOR — DENTED (CABIN) · airframe 28,128 hrs · 23,578 cycles

MAIN DOOR HAS DENT BELOW HANDLE. DENTED AREA BELOW PAX DOOR HANDLE ACCEPTED AS IS IAW ERS-EM-52MR-301.

Part: LIGHT — CRACKED (CABIN) · airframe 28,128 hrs · 23,578 cycles

LEFT NR 7 EMER LIGHT STRIP IS CRACKING. R & R LT NR 7 EMER LIGHT STRIP IAW AMM 33-50-12. SEE BOW 182857 FOR FINAL INSTALL & OPERATIONAL TEST.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,128 hrs · 23,578 cycles

RIGHT FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 1 FASTENER ON FRAME 79 BELOW VERTICAL STAB. REPAIRED RT FUSELAGE EXTERNAL SKIN CRACK AROUND 1 FASTENER IAW ERS-EM-53MR-1151. SEE WIP & TASKS FOR DETAILS OF WORK PERFORMED.

Part: WIRE — BROKEN (CABIN) · airframe 28,128 hrs · 23,578 cycles

FLOOR PROXIMITY LIGHTING STRIP NR 1 WIRING BROKEN AT FLOOR STRIP. R & R FLOOR PROXIMITY LIGHTING STRIP NR 1 IAW AMM 33-50-12. SEE BOW 182880 FOR OPERATIONAL CHECK.

Part: CONNECTOR — BROKEN (CABIN) · airframe 28,128 hrs · 23,578 cycles

CABIN AISLE EMER LIGHT STRIP NR 5 ELEC CONNECTOR BROKEN. REPAIRED CABIN AISLE EMER LIGHT STRIP NR 5 CONNECTOR IAW SWPM 20-21-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,128 hrs · 23,578 cycles

LEFT FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 1 FASTENER ON FRAME 79 BELOW VERTICAL STAB. REPAIRED LT FUSELAGE SKIN CRACK AROUND FASTENER IAW ERS-EM-53MR-1151. SEE WIP & TASKS FOR DETAILS OF WORK PERFORMED.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 28,128 hrs · 23,578 cycles

EMERGENCY LIGHT STRIP WIRE HARNESS ON LT BEAM FRAME 54 HAS TORN INSULATION. REPAIRED EMER LIGHT STRIP WIRE HARNESS ON LT BEAM IAW SWPM 20-21-00.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 27,739 hrs · 23,274 cycles

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

Part: BLEED VALVE — FAILED (ENGINE) · airframe 27,397 hrs · 22,965 cycles

ON FINAL APPROACH EICAS PRESENTED BLD 1 OVERTEMP MASTER WARNING, 3 TIMES FAILED ASM 1 PROCEDURE. R & R ENG BLEED VLV IAW AMM 36-11-05-40-801-A. ENG BLEED VLV OPERATIONS CHECKED GOOD IAW AMM 36-00-00-700-803-A.

Part: HANDLE — MALFUNCTIONED (PARKING BRAKE) · airframe 27,004 hrs · 22,664 cycles

PARKING BRAKE VERY DIFFICULT TO OPERATE. COMPLIED WITH PARKING BRAKE HANDLE SERVICING IAW AMM 32-44-01. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,494 hrs · 22,215 cycles

AFT CABIN BULKHEAD FLASHLIGHT INOPERATIVE. REPLACED AFT FLASHLIGHT IAW 33-50-16.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 26,094 hrs · 21,890 cycles

ABORTED TAKEOFF DUE TO BLD 2 VLV FAIL MSG ON EICAS. DURING TAKEOFF AT 78 KNOTS, MAXIMUM BRAKING APPLIED. R & R NR 2 BLEED VLV IAW AMM 36-11-05.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 26,117 hrs · 21,914 cycles

DURING TAKEOFF ON FLIGHT 3153 CREW REPORTED BLEED 2 VLV FAIL MSG ON EICAS AT 78 KNOTS. MAXIMUM BRAKING APPLIED & ABORTED TAKEOFF. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 2 BLEED VLV IAW AMM 36-11-05. OPERATIONS CHECKED GOOD. THE ACFT RETURN TO SERVICE.

Part: SWITCH — INOPERATIVE (BLEED AIR SYS) · airframe 25,993 hrs · 21,813 cycles

BLEED 2 VLV FAIL. R & R BLEED 2 PUSH BUTTON IAW AMM 20-13-04, OPERATIONS CHECK OF E2 BLEED VLV GOOD IAW AMM 36-11-05.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 25,971 hrs · 21,795 cycles

ON TAKEOFF ROLL PRIOR TO 80 KNOTS HAD BLEED 2 VLV FAIL MSG ON EICAS. PERFORMED ENG 2 BLEED VLV OPERATIONAL CHECK WITH FLIGHT CREW IAW AMM 36-11-05-700-802-A. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,632 hrs · 21,534 cycles

COCKPIT STEP EMERGENCY LIGHT INOPERATIVE. R & R NR 1 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,632 hrs · 21,534 cycles

COCKPIT STEP EMERGENCY LIGHT INOPERATIVE. R & R BATTERY PACK NR 1 & CHARGER IAW AMM 33-50-04, OPERATIONS CHECK FAIL.

Part: SIGN — INOPERATIVE (CABIN) · airframe 25,632 hrs · 21,534 cycles

COCKPIT STEP EMERGENCY LIGHT INOPERATIVE. R & R EXIT SIGN IAW AMM 33-50-13. OPS CHECKED FAIL.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,971 hrs · 21,000 cycles

FIRST OFFICER`S FLASHLIGHT INOPERATIVE. INSTALLED NEW FLASHLIGHT IAW AMM 25-12-10, OPERATIONS CHECKED GOOD.

Part: TUBE — DISCONNECTED (ANTI-ICE SYS) · airframe 24,955 hrs · 20,990 cycles

ENTERED LIGHT RIME ICING DURING CLIMB OUT & RECEIVED ALL NORMAL ICING ADVISORY MESSAGES & 4 OPEN INSCRIPTIONS IN SWITCHES. APPROXIMATELY 10 SECONDS LATER EICAS INDICATED, WG ANTI-ICE FAIL, CAUTION MESSAGE FOLLOWED SHORTLY BY, ICE COND ANTI-ICE INOPERATIVE WARNING. MESSAGES REMAINED UNTIL EXITING ICING CONDITIONS AT WHICH TIME ALL MESSAGES EXTINGUISHED. COMPLIED WITH AOM VOL 1 PROCEDURES. FOUND TUBING TO RT PRESS REG VLV DISCONNECTED, RECONNECTED IAW AMM 20-10-03, OPERATIONS CHECKED IAW AMM 30-00-00, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,842 hrs · 20,897 cycles

DURING MAINTENANCE INSPECTION ON FLIGHT 2779 FOUND THE RT OF WING EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R BULB IAW EMB AMM 33-50-10. OPERATIONS CHECKED GOOD & NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,297 hrs · 20,440 cycles

LT FWD EXTERNAL EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT DOWN TO NR 1 BACK-UP BATTERY SUPPLY CHARGER. R & R BACKUP BATTERY CHARGER IAW AMM 33-50-04. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,254 hrs · 20,404 cycles

MAIN CABIN DOOR EMERGENCY LIGHT IN CEILING PANEL INOPERATIVE. R & R EMERGENCY LIGHT LAMP AT CEILING OF MAIN CABIN DOORWAY IAW AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECKED GOOD.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 23,893 hrs · 20,107 cycles

DURING MBV INSPECTION, BAGGAGE DOOR CUTOUT STRUCTURE HAS CORROSION ON INNER SKIN JUST FWD OF FRAME 68. REPAIRED BAGGAGE DOOR CUTOUT STRUCTURE AT FRAME 68 IAW EO EM-53MR-1129.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 23,893 hrs · 20,107 cycles

DURING MBV INSPECTION, FOUND RT HAT BEAM IN THE LAV BETWEEN FRAMES 59 AND 60 IS CORRODED. DAMAGED AREA CUT OUT AND REPAIRED IAW EO EM-53MR-2170.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 23,893 hrs · 20,107 cycles

DURING MBV INSPECTION, FOUND ANGLE BRACKET AT RIB 4 WHICH PANEL 155QZ ATTACHES TO IS CRACKED APPROX. 4". R & R ANGLE BRACKET AT RIB NR 4 WHICH 155QZ ATTACHES TO IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 23,893 hrs · 20,107 cycles

DURING MBV INSPECTION, FOUND AFT BELLY PANEL. SUPPORT L BRACKET IS CRACKED, LOCATED JUST INBD OF RT INBD FLAP. R & R AFT BELLY SUPPORT BRACKET ON LOWER SIDE JUST INBD OF RT INBD FLAP IAW EM-53-142 AND SRM 51-40-02.

Part: SUPPORT — CRACKED (CARGO CABLE DRUM) · airframe 23,893 hrs · 20,107 cycles

DURING MBV INSPECTION, FOUND CARGO DOOR CABLE DRUM SUPPORT AT FRAME 68 IS CRACKED IN 2 SPOTS, APPROX 1.5" TOTAL. R & R 2 DAMAGED DRUM SUPPORTS IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 23,893 hrs · 20,107 cycles

DURING MBV INSPECTION, FOUND SUPPORT BROKEN UNDER CARGO DOOR SUPPORT ROD RECEPTICLE (FRAME 68). R & R CARGO DOOR ROD RECEPTICLE SUPPORT IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FUSELAGE FRAME) · airframe 23,893 hrs · 20,107 cycles

DURING MBV INSPECTION, FOUND FRAME 73 HAS A CRACKED SHEAR CLIP AT STRINGER 10R.

Part: SHEAR TIE — CRACKED (FUSELAGE FRAME) · airframe 23,893 hrs · 20,107 cycles

DURING MBV INSPECTION FOUND FRAME 68 HAS A CRACKED SHEAR CLIP BETWEEN STRINGERS 5R AND 6R. R & R LT ANGLE FRAME 68 IAW SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 23,893 hrs · 20,107 cycles

BAGGAGE DOOR CUTOUT STRUCTURE HAS CORROSION ON INNER SKIN JUST FWD OF FRAME 68. CORROSION AT BAGGAGE DOOR CUTOUT REPAIRED AS REQUIRED IAW E/O EM-53MR-1129, PART B.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,893 hrs · 20,107 cycles

RT HAT BEAM IN LAV BETWEEN FR 59 AND 60 IS CORRODED. REPAIRED RT HAT BEAM IN LAV BETWEEN FR 59 AND 60 IAW EO EM-53MR-2170.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,267 hrs · 19,604 cycles

DURING B INSPECTION FOUND THE FORWARD CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 23,222 hrs · 19,567 cycles

ON FLIGHT 2804 THE FLIGHT ATTENDANT REPORTED THE AFT FLASHLIGHT WAS INOPERABLE. DEFERRED AS PER MEL 25-53 AUTH # 040579-C. REMOVED AND REPLACED THE FLIGHT ATTENDANT AFT FLASHLIGHT HOLDER ASSEMBLY. MEL RESTORED. THE OPERTIONAL CHECK WAS GOOD IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,054 hrs · 19,432 cycles

DURING B INSPECTION FOUND THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT IAW EMB AMM TASK 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: FAIRING — DAMAGED (LT WING) · airframe 23,048 hrs · 19,429 cycles

ON FLIGHT 2963 THE CREW REPORTED THAT DURING CRUISE THE LEFT WING TIP HAD LIGHTNING STRIKE DAMAGE AND THE FIRST OFFICER’S PFD SCREEN WAS MUTI COLORED AFTER LIGHTNING STRIKE. ALSO THE CAPTAIN’S CA'S MFD ' PFD & EICAS SHOWING MULTI COLORS DUE TO LIGHTNING STRIKE. LIGHTNING STRIKE BROKE THE FIRST OFFICER’S WINDSHIELD & THE RIGHT WINDSHIELD WIPER ARM WAS DAMAGED. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE FUSELAGE HAS SEVERAL LIGHTNING STRIKE BURN MARKS AND THE APU EXHAUST COWLING HAS LIGHTNING STRIKE DAMAGE. THE AOA VANE 1 HAD LIGHTNING STRIKE DAMAGE. REMOVED AND REPLACED LEFT HAND WING TIP IAW EMB 145 AMM 57-30-00. REMOVED AND REPLACED THE FIRST OFFICER’S PFD IAW AMM 34-22-01. REMOVED AND REPLACED EICAS, BOTH PFD'S, CA MFD IAW AMM 34-22-01, 31-41-02. PART NUMBER 7014300901, S/N 0204B345, PART NUMBER 7014300901, S/N 0205B411, PART NUMBER 7014300901, S/N 0211C182. REMOVED AND REPLACED F.O. COCKPIT WINSHEILD AS PER AMM 56-10-01 PART NUMBER NP15131112, S/N 03129H3636 AND REMOVED AND REPLACED THE RIGHT WINDSHIELD WIPER ARM IAW EMB 145 AMM 30-41-03 PART NUMBER 90-0183-12. PERFORMED INSPECTION AND REPAIR FUSELAGE LIGHTNING STRIKE BURN MARKS IAW SRM 53-00-01. REMOVED AND REPLACED APU EXHAUST SILENCER IAW AMM EMB145-53-32-00. PART NUMBER 4503801C, SN 0717. REMOVED AND REPLACED LEFT AOA VANE SENSOR IAW EMB 145 AMM 27-36-01. PART NUMBER 0861DT5, SN 2337. THE OPERATIONAL CHECKS WERE GOOD ON ALL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,882 hrs · 19,299 cycles

ON FLIGHT 3302 THE CREW REPORTED THE EMERGENCY CEILING LIGHT OVER 1A WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED AN ELECTRICAL RESET AND THE OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM IAW AMM 33-50-00, FOUND SYSTEM WORKING PROPERLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 22,659 hrs · 19,129 cycles

ON FLIGHT 2788 THE CREW REPORTED THE LUMINESCENT EXIT PANEL AT STEP OF COCKPIT ENTRY WAS NOT WORKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET POWER IAW EMB 145 AM 24-30-00. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — INOPERATIVE (TE FLAPS) · airframe 22,652 hrs · 19,124 cycles

FLIGHT 3354. ON FINAL, RECEVIED A FLAP FAILED MESSAGE ON EICAS. CONFIRNED FLAP REMAINED AT 0 DEGREES. ADVISED ATC. COMPLIED WITH ALL AOM PROCEDURES. EMERGENCY DECLARED. MADE A FLAPLESS LANDING WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLAP VELOCITY SENSOR IAW AMM 27-51-12. OPS CHECKED GOOD. FLAP FAIL MESSAGE NO LONGER DISPLAYED ON EICAS. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,362 hrs · 18,106 cycles

DURING B INSPECTION, FOUND THE AFT FLOOR PROXIMITY STRIP LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. PERFORMED OPS CHECK IAW WORK CARD 33-700-17, AND CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 20,425 hrs · 17,392 cycles

ON FLIGHT 3989 THE CREW REPORTED A STRONG ELECTRICAL FUME ODOR IN THE COCKPIT AND CABIN DURING FLIGHT AT FL200. AFTER ELECTRICAL SYSTEM FIRE OR SMOKE CHECK LIST ITEM "SHED BUSES KNOB OFF" THE FUMES SEEMED TO DISIPATE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO FWA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. ALL OF THE OPERATIONAL CHECKS WERE GOOD. NO DEFECTS NOTED ON ANY COMPONENT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,113 hrs · 17,146 cycles

DURING B-INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LAMP IAW EMB 145 AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 19,956 hrs · 17,037 cycles

DURING MAINTENANCE INSPECTION FOUND CAPTAIN'S FLASHLIGHT BUTTON BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAIN’S FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16. OPERATIONAL CHECKS GOOD. THE AIRCRAFT RETURN TO SERVICE.

Part: STRINGER — BENT (FUSELAGE) · airframe 19,295 hrs · 16,565 cycles

DURING MAINTENANCE BASE INSPECTION FOUND STRINGER 15 LEFT BETWEEN FRAMES 1A TO 2 I BENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED STRINGER 15L FROM FRAME 1A TO 4 IAW EMBRAER STRUCTURAL REPAIR MANUAL 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — BENT (FUSELAGE) · airframe 19,295 hrs · 16,565 cycles

DURING MAINTENANCE BASE INSPECTION FOUND STRINGER 15 LEFT BETWEEN FRAMES 1A TO 2 BENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED STRINGER 15L FROM FRAME 1A TO 4 IAW EMBRAER STRUCTUAL REPAIR MANUAL 51-40-02. THE AIRCRAFT WAS RETURNED TO SERIVCE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 19,295 hrs · 16,565 cycles

DURING MAINTENANCE BASE INSPECTION FOUND LEFT FORWARD FUSELAGE SKIN BIRD STRIKE DAMAGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH EO EM-53MR-1881 R1 PART C. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (ACCESS HATCH) · airframe 19,295 hrs · 16,565 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE COCKPIT UNDERFLOOR ACCESS HATCH SKIN HAS .5 INCH CRACK UNDER THE LOCK PIN BRACKET BETWEEN THE MOUNTING HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-52MR-239. THE AIRCRAFT WAS RETURNED TO SERIVCE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 19,295 hrs · 16,565 cycles

DURING MAINTENANCE BASE INSPECTION FOUND FRAME 2 DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DAMAGED FRAME 2 WITH NEW IAW EO EM-53MR-1881. THE AIRCRAFT WAS RETURNED TO SERIVCE.

Part: FITTING — GOUGED (RT AILERON) · airframe 19,295 hrs · 16,565 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE DAMPNER FITTING ON THE RIGHT AILERON GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DAMPNER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERIVCE.

Part: SKIN — CRACKED (ACCESS HATCH) · airframe 19,296 hrs · 16,565 cycles

COCKPIT UNDERFLOOR ACCESS HATCH SKIN HAS .5" CRACK UNDER THE LOCK PIN BRACKET. BETWEEN THE MOUNTING HOLES. REPAIRED IAW EO EM-52MR-239.

Part: SHEAR TIE — CORRODED · airframe 19,296 hrs · 16,565 cycles

SHEAR CLIP AT FR 65 AT CARGO SILL LEVEL CORRODED. REPAIRED SHEAR CLIP IAW EO EM-53MR-1129.

Part: WIRE — BROKEN (CABIN) · airframe 19,571 hrs · 16,759 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CABIN FLOOR EMERGENCY LIGHT STRIP NR 5 HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED CONNECTOR AT SPLICE SP9115 IAW SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 19,571 hrs · 16,759 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE EMERGENCY FLASHLIGHT MISSING FROM THE COCKPIT (BEHIND THE CAPTAIN’S SEAT). THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED FLASHLIGHT IAW EMB 145-EEL-06-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,705 hrs · 16,131 cycles

ON FLIGHT 3513 THE CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT WOULD NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW EMB 145 AMM 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — DAMAGED (STEERING CONTROL) · airframe 18,586 hrs · 16,046 cycles

AIR TURNBACK - NR 1 HYD SYS LOW QTY CAUTION, THEN SHORTLY AFTER GOT A NR 1 HYD PUMP FAIL WARNING MSG. CFR WAS CALLED. AC LANDED SAFELY WITHOUT INCIDENT. REMOVED AND REPLACED O-RING ON STEERING CONTROL UNIT IAW EMD 145 AMM 29-10-13, LEAK CHECK GOOD.

Part: BATTERY PACK — MALFUNCTIONED (CABIN) · airframe 17,632 hrs · 15,289 cycles

ON FLIGHT 3658 DURING TAXI THE 3 EMERGENCY LIGHT FLOOR PROXIMITY STRIPS WERE FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET TRANSIENT CONDITION OF BATTERY PACK NR 4. THE SYSTEM CHECKED GOOD IAW AMM 33-50-04. ALL EMERGENCY LIGHTS OPERATE AS REQUIRED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,247 hrs · 13,497 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT EMERGENCY DOOR EXIT SIGN TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED INVERTER NR 5 IAW EMB 145 AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,570 hrs · 12,938 cycles

DURING MAINTENANCE BASE INSPECTION FOUND LEFT OMEGA BEAM BETWEEN FRAMES 24-25 AT CROSS BEAM CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WITH A DOUBLER REPAIR IAW SRM CHAPTER 53-00-10 FIG 202. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,571 hrs · 12,938 cycles

DURING THE MAINTENANCE BASE INSPECTION FOUND THE SERVICE DOOR CENTER SILL IS CORRODED IN SEVERAL AREAS BETWEEN FRAMES 20 AND 22. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED SERVICE DOOR SILL WITH NEW, IAW WITH EMBRAER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,616 hrs · 12,205 cycles

SUPPLEMENTAL SDR - DURING MAINTENANCE INSPECTION THE NUMBER 4 AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE NUMBER 4 AFT EMERGENCY LIGHT CHARGERS AND BATTERY IAW EMB AMM 33-50-04. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 13,616 hrs · 12,205 cycles

DURING MAINTENANCE INSPECTION THE NUMBER 4 AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE NUMBER 4 AFT EMERGENCY LIGHT CHARGERS AND BATTERY IAW EMB AMM 33-50-04. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 13,616 hrs · 12,205 cycles

ON FLIGHT 3789 THE CREW REPORTED THAT THE NUMBER 4 AFT EMERGENCY LIGHT WAS INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE NUMBER 4 AFT EMERGENCY LIGHT CHARGER AND BATTERY IAW EMB AMM 33-50-04. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — MELTED (CABIN) · airframe 22,078 hrs · 21,528 cycles

ON FLIGHT 3509, AT CRUISE AND FL 360 PAX AND CREW DETECTED THE ODOR SOMETHING BURNING. AT THIS TIME BOTH VS INDICATION +4000 -4000 FPM AND 'ALT ON BOTH PFD AIRSPEED DECREASING. AT ABOUT FL 320 ALL SYSTEMS BACK TO NORMAL. AIRCRAFT REMOVED FROM SERVICE. REMOVED WATER FROM CAPT AND F/O PITOT-STATIC MOISTURE DRAIN/TRAPS IAW WC 34-600-01. CAPT AND F/O ADC INDICATIONS OP CHECK GOOD IAW AMM 34-15-00. FOUND AFT CABIN FLASHLIGHT WITH MELTED MARKS. REPLACED AFT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16 OPERATION CHECK GOOD NO BURNING ODOR AT THIS TIME. PRESSURIZATION OPERATION CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — SMOKE (LEFT) · airframe 11,617 hrs · 10,630 cycles

ON FLIGHT 3598, ON TAKEOFF CREW REPORTED SMOKE IN CABIN. CREW ABORTED TAKEOFF AND RETURNED TO BLOCK. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,667 hrs · 8,744 cycles

DURING IMBV, FOUND AFT BAGGAGE DOOR SILL TO BE CORRODED. REMOVED AND REPLACED SILL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — FAILED (GALLEY)

DFW - FLT 3599 - AFTER TAKEOFF FA AND PAX REPORTED SMELLING SOMETHING BURNING. AIRCRAFT RETURNED AFTER COMPLETING CHECKLIST, SMELL RETURNED ON GROUND, POSSIBLE OVERWEIGHT LANDING. RAI AFT GALLEY ELECTRICAL MODULE ASSY IAW C/D AEROSPACE CMM 25-31-98, OPS CHECK GOOD. PERFORMED ENGINE RUN ON BLEED SYSTEM IAW EMB AMM 36-00-00. NO DISCREPANCIES. OVERWEIGHT LANDING FOUND TO BE WITHIN LIMITS. SINK RATE LESS THAN 6 FPS IAW EMB 145, AMM 05-50-25. RETURNED AIRCRAFT TO SERVICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION AND FABRICATED A FILLER DOUBLER, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM. (K)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

LAVATORY SMOKE WARNING JUST AFTER TAKEOFF. INSPECTED LAVATORY FOUND NO EVIDENCE OF SMOKE OR DAMAGE. REPLACED THE LAVATORY SMOKE DETECTOR SENSOR IAW EMB AMM 26-14-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)