N655AE

Part: HYDRAULIC LINE — LEAKING (ZONE 400) · airframe 53,527 hrs · 50,418 cycles

ENGINE HYD 1 PUMP FAIL & HYD 1 LOW QTY. PERFORMED GVI INSPECTION ENG #1 DUE TO SUSPECTED ENG #1 HYD LEAD. FOUND ABUNDACE OF HYD FLUID IN COWLING. SUSPECTED HYD RETURN LINE. FURTHER TROUBLESHOOTING REQUIRED. R & R NR 1 EDHP IRW AMM 29-10-03. OPS & LEACH CHECK GOOD.

Part: FUEL NOZZLE — FAULTED (NR 2 ENGINE) · airframe 52,800 hrs · 49,568 cycles

HUNG START ON NO.2 FOLLOWED BY FUEL SMELL IN A/C. PERFORMED GVI OF ENG 2 NO OBVIOUS DEFECTS NOTED OTHER THAN POOLED FUEL. DRY MOTORED ENG TO CLEAR OUT FUEL. DURING DRY MOTOR CONSTANT FUEL SPRAY WAS NOTED AT THE 6 OCLOCK POSITION WITH A 0 FUEL FLOW INDICATION ON THE EICAS SUSPECT FUEL LEAK INSIDE THE ENGINE. UNABLE TO CONTINUE T/S AT THIS TIME. FOUND FUEL NOZZLE 9 LEAKING R/RD FUEL NOZZLE 9 IAW RRMM 73-11-10 OPS AND LEAK CHECK GOOD.

Part: FUSE — LEAKING (ZONE 400) · airframe 52,672 hrs · 49,434 cycles

HYD 2 QTY IS EMPTY. HYD 2 WAS FULL AT PUSH BACK EMPTY BY GATE RETURN. FOUND #400 HYDRAULIC FUSE LEAKING. R&R #400 HYDRAULIC FUSE IAW AMM 32-41-07. LEAK CHECK AND OPS CHECK GOOD.

Part: NONE — NO DISCREPANCY (NONE)

BIRD STRIKE ON LH SIDE OF NOSE. PERFORMED BIRDSTRIKE INSPECTION IRW AMM 05-50-08. NO DAMAGE NOTED. A/C OK FOR SERVICE.

Part: THERMOSTAT — FAULTED (NR 2 ENG FAN AIR) · airframe 51,160 hrs · 47,776 cycles

BLD 2 VLV CLSD AFTER TAKEOFF MSG CLSD AFTER LANDING. FACT 09JUL24 00:03 PHL T/S IRW FIM 36-00-810-808-A DUE TO CMC PRECOOLER 2 TEMP CTL SYS FAIL MSG. R/R E2 FAN AIR CONTROL THERMOSTAT IAW AMM 36-11-06 R/R E2 BLD VLV IAW AMM 36-11-05 PERFORMED OPS CHECK IAW AMM 36-00-05 OPS/ LEAK CHECK GOOD OK FOR SERVICE AT THIS TIME

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 51,128 hrs · 47,731 cycles

PRESSURIZATION RISING DURING CLIMB WHILE RUNNING QRH PRESSURIZATION GOR HIGHER AND NORMALIZED AT 10,500 FT. PERFORMED OPERATIONAL CHECK IN AUTO AND MANUAL IAW 21-31-02 CND. R & R DIGITAL CONTROLLER IAW MM 21-31-01, OPS CK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,146 hrs · 46,592 cycles

FO W/S COMPLETED CRACKED DURING CLIMBOUT. R&R WINDHIELD IAW AMM 56-10-01.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 50,118 hrs · 46,555 cycles

00160 CABIN FLOOR SUPPORT ANGLE LOCATED AT FRM 20 Y 0.0 @ Y-479.0 IS CORRODED. REMOVED AND INSTALLED NEW FLOOR SUPPORT ANGLE P/N 145-20600-603 AT FR 20 Y-479 IAW EMB-145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 50,118 hrs · 46,555 cycles

00161 RHS CABIN FLOOR SUPPORT DOUBLER LOCATED AT FR 22 Y 479.O IS CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE R/H CABIN FLOOR SUPPORT DOUBLER P/N 145-22461-011 LOCATED AT FRAME 22 Y 479.0 IAW EMB 145 SRM 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 50,118 hrs · 46,555 cycles

00162 LHS CABIN FLOOR SILL IS CORRODED AT FRM 40, REMOVED AND REPLACED L/H CABIN FLOOR SILL P/N 145-25800-009 AT FRAME 40 IAW EMB 145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 49,733 hrs · 46,106 cycles

DAU 1B FAIL AFTER TAKE OFF, R & R DAU 1 IAW ANN 31-41-01. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: UNKNOWN — UNKNOWN · airframe 48,768 hrs · 45,060 cycles

BRAKE OVER TEMP AMBER IND WITH ASSC EICAS MSG ON O/B R/H BRAKE AFTER T/O FACT 11MAR23 12:24 R+R BRAKE CONTROL UNIT IAW EMB 145 MM 32-41-02 AS REQUIRED REF LP 280707 SEQ 3 FOR EVAL FLIGHT FACT 11MAR23 14:27 EVAL FLIGHT SATISFACTORY

Part: STARTER — FAILED (NR 1 ENGINE) · airframe 48,475 hrs · 44,762 cycles

ON NR 1 ENGINE START, ENGINE SHOWED NO ROTATION. AND EXCESS SMOKE WAS SEEN. GROUND CREW SIGNALED ENGINE FIRE BUT DID NOT USE FIRE BOTTLE. NO RELEVANT MESSAGES ON EICAS. REMOVED AND REPLACED THE NR 1 ENG AIR TURBINE STARTER IAW AMM 80-10-01 OPS CHECK OF ENG 1 MULTIPLE TIMES OPS CHECK GOOD OK FOR SERVICE

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,407 hrs · 43,508 cycles

NDIS 655 33-50 0030050 29MAY22 RIC CLOSE LEFT AND RIGHT EXTERNAL EMERGENCY LIGHT ABOVE THE WINGS ARE INOPERATIVE. FACT 29MAY22 11:49 RIC UPON FURTHER INSPECTION FOUND #400 EMERGENCY BATTERY CHARGER ASSY. WAS NOT PROVIDING VOLTS. REMOVED & REPLACED #400 EMERGENCY BATTERY CHARGER ASSY. IAW AMM 33-50-04-400-801-A. OPS CHECK GOOD. OK FOR SERVICE.

Part: NOT REPORTED — NOT REPORTED · airframe 46,890 hrs · 42,942 cycles

PDIS 655 21-31 2754131 14FEB22 CLT CLOSE AUTO PRESSURIATYION CONTROL INOP IN FLIGHT. MANUAL OPS NORMAL. DEACTIVATED OUTFLOW VALVE IAW 21-31-03-040-801-A. P/C C/B F-8 FACT 14FEB22 05:39 SBY REACTIVATED VALVES IAW AMM 2131-03-440-801-A, R&R ELECTRO- PNEUMATIC OUTFLOW VALVE IAW 21-31-03-400-801-A. OPS CHECK GOOD. CLEAR MEL 21-12-1

Part: NONE — NONE · airframe 46,766 hrs · 42,797 cycles

PDIS 655 05-51 2711371 14JAN22 SBY ASSGN BIRD STRIKE CAPTS SIDE OF NOSE FWD OF WIPER DURING ROTATION. (NO ENGINE OR AIRSPEED ISSUES) HISTORY: NO AIRCRAFT CURRENTLY RECEIVING STRUCTURAL REPAIR TO DENTED AREA UNDER THE GUIDANCE OF EMBRAERS ETD2022-145-001261

Part: ACM — FAILED (NR 1) · airframe 46,246 hrs · 42,250 cycles

IN CRUISE ODOR OF SMOKE PRESENT IN BOTH CABIN AND COCKPIT. ONCE ON GROUND COCKPIT TEMP INCREASED REGARDLESS OF TEMP CONTROLLER POSITION. INSPECTED PACK 1 AND FOUND ACM TO BE EXTREMELY HOT AND SEIZED. SMOKE SMELL CAME FROM PACK 1 ACM SEIZING AND NOW PACK 1 WILL NOT OPERATE. SEE SAME LP SEQ 2 FOR NEW WRITE UP AND MEL.

Part: SHEAR TIE — CORRODED (FRM 65) · airframe 45,705 hrs · 41,674 cycles

FR 65 SHEAR CLIP CORRODED AT CARGO DOOR LOWER SILL. CUT, POSITIONED, DRILLED AND INSTALLED SPLICE REPAIR ON FR 65 SHEAR CLIP AT CARGO DOOR LOWER SILL IAW ETD2021--145-019276 REV A AND EO1-53-21-0147.

Part: FLOOR SUPPORT — CORRODED (FRMS 29-30) · airframe 45,705 hrs · 41,674 cycles

L/H FLOOR SILL #3 IS CORRODED AT A PREVIOUS BLEND BETWEEN FRAMES 29-30. REMOVED AND INSTALLED SERVICEABLE LH #3 FLOOR SILL IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 45,705 hrs · 41,674 cycles

CARGO DOOR CUTOUT LOWER FLOOR SILL CORRODED. REMOVED AND PERFORMED INSTALLATION OF SERVICEABLE CARGO DOOR CUTOUT LOWER SILL IAW EMB 145 SRM 51-40-02.

Part: GUSSET — CORRODED · airframe 45,705 hrs · 41,674 cycles

RH OMEGA BEAM GUSSET #3 CORRODED. REMOVED AND REPLACED RH OMEGA BEAM GUSSET #3 IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 45,705 hrs · 41,674 cycles

LH #7 FLOORBOARD SILL CORRODED. REMOVED AND INSTALLED NEW LH #7 FLOORBOARD SILL IAW EMB 145 SRM 51-40-02.

Part: GUSSET — CORRODED (CENTER LAV) · airframe 45,705 hrs · 41,674 cycles

CENTER LAV OMEGA BEAM GUSSET CORRODED AT AFT END. REMOVED AND REPLACED CENTER LAV OMEGA BEAM GUSSET EMB 145 SRM 51-10-02.

Part: GUSSET — CORRODED (RIGHT) · airframe 45,705 hrs · 41,674 cycles

RH OMEGA BEAM GUSSET #2 CORRODED. REMOVED AND REPLACED R/H OMEGA BEAM GUSSET #2 IAW EMB 145 SRM 51-40-02.

Part: PANEL — CORRODED (RT LAVATORY) · airframe 45,705 hrs · 41,674 cycles

RH LAV BANANA PANEL CORRODED AT LOWER END. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE R/H LAV BANANA PANEL IAW EMB 145SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · airframe 45,705 hrs · 41,674 cycles

RH #3 FLOORBOARD SILL CORRODED. REMOVED AND REPLACED #3 FLOORBOARD SILL IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRMS 63-65) · airframe 45,705 hrs · 41,674 cycles

CARGO RH OUT BOARD FLOOR SILL CORRODED BETWEEN FRAMES63-65. REMOVED CORRODED CARGO RH OUT BOARD FWD FLOOR SILL, POSITIONED DRILLED AND INSTALLED SERVICEABLE FLOOR SILL IAW EMB 145 SRM 51-40--02, 51-20-03, APPLIED PAINT TOP COAT IAW EMB 145CPM 51-21-06 PIEDMONT BULLETIN CPM 51-03.

Part: GUSSET — CORRODED (RT LAVATORY) · airframe 45,705 hrs · 41,674 cycles

RH LAV OMEGA BEAM GUSSET CORRODED AROUND NIPPLES. REMOVED UNSERVICEABLE RH LAV OMEGA BEAM GUSSET & INSTALLED SERVICEABLE R/H LAV OMEGA BEAM GUSSET IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · airframe 45,705 hrs · 41,674 cycles

RH #2 FLOORBOARD SILL CORRODED. REMOVED AND REPLACED RH #2 FLOORBOARD SILL IAW EMB 145 SRM 51-20-03.

Part: PROXIMITY SWITCH — MALFUNCTIONED (NLG) · airframe 45,307 hrs · 41,273 cycles

LOUD NOISE FROM NOSE LANDING GEAR AREA HEARD AFTER GEAR RETRACTION, RAN QRH, CYCLED GEAR NOISE PERSISTED.(CAPT SAID GEAR LOCKED DOWN AND HE RETURNED BACK TO FIELD WITH AIRCRAFT) R&R'D NOSE DOOR SEQUENCE PROX SWITCH IAW 32-63-05-700-803-A AMM. SWUNG GEAR 8 TIMES GEAR DOORS CLOSED. OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (CARGO DOOR) · airframe 46,475 hrs · 43,524 cycles

BAG BAY DOOR INDICATED OPEN ON TAKE OFF ROLL. R & R CONNECTOR P7216, IAW 20-50-00. OPERATIONS CHECK GOOD, CLEAR MEL.

Part: UNKNOWN — FIRE (NR 1 ENGINE) · airframe 44,424 hrs · 40,256 cycles

RAMP AGENT REPORTED FLAMES FROM #1 ENG EXHAUST AT SHUT DOWN. MAINTENANCE: INSPECTED IAW RRMM 05-50-00. NO EVIDENCE OF OIL POOLING OR FIRE DAMAGE. STARTED #1 ENGINE AND SHUTDOWN WITH NO FIRE OR ABNORMAL SMOKE EXHAUST. OK FOR SERVICE

Part: PRESSURE SWITCH — FAILED (NR 1 A/C PACK) · airframe 43,575 hrs · 39,302 cycles

PDIS 655 21-01 1886972 27OCT19 PHL CLOSE PACK 1 OVRLOAD FOLLOWED BY BURNING RUBBER SMELL NOTI CED IN CABIN AND COCKPIT. SMELL WENT AWAY WHEN PACK 1 WAS TURNED OFF. FACT 27OCT19 23:54 PHL R&R'D #1 PACK OVERPRESSURE SWITCH IN REF TO AMM 21-5 1-06 OPS CHECK #1 PACK SEVERAL TIMES USING APU AND E NG #1 AND #2, NO DEFECTS NOTED AT THIS TIME. OK FOR

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,201 hrs · 36,218 cycles

RT OVERWING EMERGENCY LIGHT DOES NOT ILLUMINATE. REPLACED OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-50-10-000/400-801-A. OPS CHECK GOOD

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 43,201 hrs · 38,868 cycles

EMERGENCY LIGHT AT SEAT 16A HAS BROKEN CONNECTOR. REPLACED EMERGENCY FLOOR LIGHT AT ROW 16A IAW AMM 33-50-12-000/400-801-A, OS CHECK GOOD

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,168 hrs · 38,834 cycles

R/H LATERAL PANEL EMERGENCY LIGHT INOP. R & R LIGHT BULB FOR RH LATERAL PANEL EMERGENCY LIGHT

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,809 hrs · 38,431 cycles

LEFT EMERGENCY EXIT ON THE TOP OF EXIT IS NOT WORKING. REMOVED AND REPLACED LIGHT

Part: SIGN — INOPERATIVE (LT OVERWING) · airframe 42,726 hrs · 38,338 cycles

AFT EXIT SIGN FOR LH OVER THE WING ESCAPE HATCH DOES NOT ILLUMINATE. R & R AFT EXIT SIGN FOR LT OVERWING ESCAPE HATCH AT SEAT 12A IAW AMM 33-50-12-000/400-801-A, OPS CHECKED GOOD. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 42,462 hrs · 38,011 cycles

655 21-01 1854861 09APR19 PHF CLOSE ELECTRICAL BURNING SMELL IN COCKPIT IN FLIGHT AND ON THE GROUND. HISTORY: . FACT 09APR19 23:52 PHF MX INSP BOTH RELAY SUPPORT PANELS AND T/S IAW FIM 21 -20-00-810-801-A. NO ABNORMAL SMELLS OR DEFECTS NOT. OKAY FOR SERVICE AT THIS TIME.

Part: WHEEL — FAILED (DISCONNECT LINK) · airframe 42,153 hrs · 37,663 cycles

PDIS 655 27-12 2012781 31JAN19 PHL CLOSE WITHOUT CREW INPUT AIRCRAFT EXPERIENCED AILERON DISCONNECT ON SHORT FINAL AUDIBLE CLICK WAS HEARD JU ST PREVIOUS TO DISCONNECT. FACT 31JAN19 00:48 PHL R&R AILERON DISCONNECT LINK WHEEL IAW AMM 27-15-00 O PS CHECK GOOD OK FOR SERVICE

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 42,115 hrs · 37,620 cycles

PDIS 655 05-50 2012692 23JAN19 PHL CLOSE ON APU POWER SMOKE WAS OBSERVED COMING OUT FROM ABOVE F/O RADAR CONTROLLER, BUT BELOW GLARESHIELD. PULLED ALL CARDS OUT AND SAW NO DAMAGE, STRONG ODOR AND SMOKE CONTINUED. PACK 2 WAS ON WITH CROSS BLEED OPEN. POWERED DON AIRCRAFT, SMOKE STOPPED. FACT 23JAN19 16:48 PHL RNR FO WX RADAR CONTROL PANEL PER AMM 34-42-02 OPS PER AMM TASK 34-42-00-700-801-A GOOD OK FOR SERVICE. INSP BOTH PACKS NO DEFECTS NOTED RAN PACKS FOR 30 MINS INDIVIDUALLY AND TOGETHER PACKS OPS NORMAL NO SMOKE NOTED OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,221 hrs · 36,658 cycles

RT EXTERNAL OVERWING EMERGENCY LIGHT WILL NOT ILLUMINATE. R&R RT EXTERNAL OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-50-10 OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,088 hrs · 36,555 cycles

ICU PANEL CABIN AND CABIN EMERGENCY LIGHTS WERE BURNED OUT. R & R THE CABIN AND CABIN EMERGENCY LIGHTS IAW AMM 20-13-04.

Part: SEALANT — FAILED (WNG-BDY FAIRING) · airframe 41,068 hrs · 36,530 cycles

DURING CLIMB, THE FLIGHT ATTENDANT REPORTED A LOUD NOISE COMING FROM THE RIGHT SIDE OF THE FUSELAGE. RETURNED TO DEPARTURE. INSPECTED THE AIRCRAFT AND FOUND THE RT WING TO FUSELAGE SEALANT HANGING DOWN. APPLIED SEALANT TO FORWARD WING TO FUSELAGE FAIRING IAW SRM 51-10-01.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 40,012 hrs · 35,523 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R THE LIGHT IAW AMM 33-50-10-000-801. OPS CHECKED GOOD

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 39,843 hrs · 35,355 cycles

FLIGHT ATTENDANT FLASHLIGHT CRADLE CRACKED. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT CRADLE BASE IN REFERENCE WITH AMM 33-50-16-000-801-A & 33-50-16-400-801-A.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,374 hrs · 34,855 cycles

DURING PS-1 INSPECTION FOUND OVERBOARD EMERGENCY LIGHT ON RT AND LT WING TO BE INOPERABLE. REMOVED AND REPLACED THE RT OVERWING EMERGENCY LIGHT ASSEMBLY AND LT OVERWING EMERGENCY LIGHT BULB IAW AMM TASK 33-50-10.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,339 hrs · 34,823 cycles

WHILE PERFORMING PS-1 CHECK, FOUND RT OVERWING EMERGENCY LIGHT LAMP NOT WORKING. R & R THE LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,184 hrs · 34,665 cycles

FOUND EXTERIOR RT OVERWING EMERGENCY LIGHT INOPERATIVE IAW PS-1 INSPECTION. R & R THE LAMPS IAW AMM 33-50-10, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,997 hrs · 34,489 cycles

MAIN DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-06-000-801-A, & 33-50-06-400-801-A. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,884 hrs · 34,394 cycles

RIGHT CENTER FUSELAGE FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10.

Part: CONNECTOR — SHORTED (NLG) · airframe 38,655 hrs · 34,217 cycles

DURING DESECENT, HAD A LANDING GEAR AIR GROUND FAIL MESSAGE ILLUMINATE ON THE EICAS, AS WELL AS A NR 1 & 2 ENGINE REVERSER DISAGREE, FOLLOWED THE EMERGENCY ABNORMAL CHECKLIST, THERE WAS NO INDICATION OF REVERSERS OPEN. FOUND THE AIR / GROUND CIRCUIT BREAKER OPEN AND WILL NOT RESET DUE TO INTERNAL SHORT OF NLG WOW SWITCH CONNECTOR P2834. REMOVED AND REPLACED THE CONNECTOR IAW SWPM 20-50-05, FUNCTIONAL CHECKED OK IAW AMM 32-63-05.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,493 hrs · 34,081 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A, OPS CHECKED GOOD.

Part: CLAMP — LOOSE (BLEED VALVE) · airframe 38,451 hrs · 34,043 cycles

PASSING THROUGH 10,000 FT, BLEED 2 LEAK. FOUND A LEAK AT THE NR 2 ENG BLEED VALVE CLAMPS. REINSTALLED CLAMP IAW AMM 36-11-05. OPS CHECKED GOOD, LEAK CHECKED GOOD IAW 36-00-0-700-803.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 38,066 hrs · 33,686 cycles

AFTER GEAR SELECTED UP 'LG AIR/GND FAIL' PRESENTED ON EICAS-C/A-REMOVED AND REPLACED FWD WOW PROXIMITY SWITCH ON THE RT MLG IAW AMM 32-63-01 ALSO ADJUST AFT PROX BRACKET IAW AMM 32-63-05 OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,004 hrs · 33,636 cycles

RH OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPC GOOD. NO OTHER DEFECTS NOTED.

Part: WIRE — BROKEN (DOOR WARNING) · airframe 37,529 hrs · 33,193 cycles

SERVICE DOOR SHOWED OPEN ON MFD AND EICAS ON T/O ROLL. HIGH SPEED ABORT AT APPROXIMATELY 100 KTS. SERVICE DOOR WARNING SYS WRITTEN UP 7 TIMES SINCE 09/01. PERFORMED HIGH ENERGY STOP INSPECTION IAW AMM 05-50-16. NO DEFECTS NOTED. DEFERRED DOOR WARNING SYS, MEL 52-04 AUTH NR 090214-B. T/S SERVICE DOOR MICRO SWITCH IAW FIM 52-70-00-801-803-A SUSPECTED MICRO SWITCH S7245 BAD, R & R MICRO SWITCH IAW AMM 52-74-01-000-801-A AND 52-74-01-400-801-A, NO FIX, FOUND 2 BROKEN WIRES NEAR CONNECTOR REPAIRED IAW SWPM 20-21-00, OPC GOOD IAW AMM 52-74-01, END.

Part: SUPPORT — DAMAGED (FRAME 50) · airframe 37,482 hrs · 33,155 cycles

FWD SUPPORT AT FRAME 50, BETWEEN STRINGERS 13-14R, HAS MISDRILLED HOLES. REPAIRED THE SUPPORT IAW ERS-EM-53MR-2251-R1.

Part: FLOOR SUPPORT — CORRODED (FRAME 22) · airframe 37,482 hrs · 33,155 cycles

LEFT OMEGA BEAM GUSSET HAS CORROSION AT FRAME 22. ACCOMPLISHED REPAIR TO THE OMEGA BEAM IAW ERS-EM-53MR-2244.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 37,482 hrs · 33,155 cycles

EMERGENCY LIGHT WIRES ARE DAMAGED AT FRAME 19 BETWEEN STRINGERS 1 - 2R. REPAIRED THE WIRES IAW SWPM 20-21-00

Part: SPAR — CRACKED (LT WING) · airframe 37,482 hrs · 33,155 cycles

LEFT WING SPAR 1 LOWER LEADING EDGE ATTACHMENT CRACKED AT RIB 9. REPAIRED THE SPAR 1 LOWER LEADING EDGE ATTACHMENT CRACKED AT RIB 9 IAW ERS-EM-74-MR-681-R1.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 37,482 hrs · 33,155 cycles

ONE WIRE FOUND DAMAGED FOR EMERGENCY LIGHTS BETWEEN FRAMES 15-16 BEHIND THE RT OTBD GALLEY FLOOR SUPPORT. REPAIRED THE WIRE IAW SWPM 20-21-00.

Part: WIRE — DAMAGED · airframe 37,482 hrs · 33,154 cycles

WIRES ARE DAMAGED AT FRAME 19 BETWEEN STRINGERS 1 - 2R. REPAIRED THE WIRES IAW SWPM 20-21-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 37,482 hrs · 33,154 cycles

ONE WIRE DAMAGED FOR THE EMERGENCY LIGHTS BETWEEN FRAMES 15-16 BEHIND RT OTBD GALLEY FLOOR SUPPORT. REPAIRED THE WIRE IAW SWPM 20-21-00.

Part: GUSSET — CORRODED (FRAME 22) · airframe 37,482 hrs · 33,154 cycles

LEFT OMEGA BEAM GUSSET HAS CORROSION AT FRAME 22. REPAIRED THE OMEGA BEAM GUSSET IAW ERS-EM-53MR-2244.

Part: FRAME — CORRODED (FRM 65) · airframe 37,482 hrs · 33,154 cycles

FRAME 65 CORRODED BETWEEN STRINGERS 16-17L AROUND DOOR GUIDE. REPAIRED THE FRAME IAW SRM 53-31-04 "E", 4

Part: LIGHT — DAMAGED (CABIN) · airframe 37,482 hrs · 33,154 cycles

NR 1 LEFT EMERGENCY LIGHT DAMAGED. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12.

Part: SPAR — CRACKED (LT WING) · airframe 37,482 hrs · 33,154 cycles

LEFT WING SPAR NR 1 LOWER LEADING EDGE ATTACHMENT CRACKED AT RIB 9. REPAIRED IAW ERS-EM-74-MR-681-R1

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,482 hrs · 33,154 cycles

NR 3 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12..

Part: BATTERY PACK — NOT REPORTED (EMERGENCY LIGHTS) · airframe 37,482 hrs · 33,154 cycles

REMOVE AND REPLACE NR 1 EMERGENCY LIGHTING BATTERY ASSY/ BATTERY CHARGER. REMOVED AND REPLACED BATTERY ASSY AND CHARGER IAW WC 33-700-19

Part: FRAME — CORRODED (FR 68) · airframe 37,482 hrs · 33,154 cycles

FRAME 68 CORRODED BETWEEN STRINGERS 16 - 17L. REPAIRED THE FRAME IAW ERS-EM-5300-2231.

Part: TRUNNION — CRACKED (LT MLG) · airframe 37,482 hrs · 33,154 cycles

LEFT MLG AFT UPPER TRUNNION CRACKED. CRACK VERIFIED BY HFEC INSPECTION. REMOVED AND REPLACED THE TRUNNION IAW ERS-EM-57MR-679.

Part: SHEAR TIE — GOUGED (FRAME 65) · airframe 37,482 hrs · 33,154 cycles

CARGO DOOR CUTOUT FRAME 65 SHEAR TIE GOUGED AT STRINGER 15L. REPAIRED THE SHEAR TIE IAW ERS-EM-57MR-2241.

Part: SHEAR TIE — CORRODED (FRAME 68) · airframe 37,482 hrs · 33,154 cycles

FRAME 68 SHEAR TIE CORRODED BETWEEN STRINGERS 16 - 18L. REPAIRED THE SHEAR TIE IAW SRM 53-31-04.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,482 hrs · 33,154 cycles

NR 5 AND 6 EMERGENCY LIGHTS HAVE BROKEN WIRES. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT IAW AMM 33-50-12. REPAIRED THE NR 5 EMERGENCY LIGHT IAW SWPM 20-21-00.

Part: FLOOR SUPPORT — CORRODED · airframe 37,482 hrs · 33,154 cycles

CENTER FUSELAGE NR 1 LT OMEGA BEAM HAS CORROSION. REMOVED DAMAGE, IAW SRM 53-21-10, INSTALLED A FILLER AND DOUBLER IAW SRM 53-21-10. INSTALLED METAL STRIP IAW SRM 51-40-02

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 37,482 hrs · 33,154 cycles

FRAME 65 SHEAR TIE CORRODED BETWEEN STRINGERS 16 - 18L. REPAIRED THE SHEAR TIE IAW ERS-EM-53MR-2241.

Part: TRUNNION — CRACKED (RT MLG) · airframe 37,482 hrs · 33,154 cycles

RT MLG AFT UPPER TRUNNION CRACKED. CRACK VERIFIED BY HFEC INSPECTION. REMOVED AND REPLACED THE MLG AFT UPPER TRUNNION IAW ERS-EM-57MR-678.

Part: LIGHT — DAMAGED (CABIN FLOOR) · airframe 37,482 hrs · 33,154 cycles

NR 5 LT EMERGENCY LIGHT IS DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: SKIN — CHAFED (FUSELAGE) · airframe 37,482 hrs · 33,154 cycles

FUSELAGE EXTERNAL SKIN CHAFED INSIDE RT PYLON PANEL 424DB FWD OF CONNECTOR J0816. PERFORMED REPAIR OF THE SKIN AREA IAW SRM 53-31-01.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,314 hrs · 33,022 cycles

AFT CABIN EMERGENCY FLASHLIGHT IS INTERMITTENT. R & R AFT CABIN EMERGENCY FLASHLIGHT IAW CMM 25-60-02. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 37,297 hrs · 33,007 cycles

RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPS CHECK GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 37,180 hrs · 32,901 cycles

RT OVERWING EMERGENCY LT INOPERATIVE. RELAMPED RT OVERWING EMERGENCY LIGHT IAW AMM 33-50-07-000-801 AND 33-50-07-400-801. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,891 hrs · 32,648 cycles

RIGHT OVERWING UPPER AFT EXIT LIGHT INOPERATIVE. R & R OVERWING UPPER AFT EXIT LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,685 hrs · 32,455 cycles

RIGHT OVERWING EMER LAMP INOPERATIVE. R & R RT WING EXTERNAL OVERWING EMER LIGHT IAW AMM 33-50-10-000-801 33-50-10-400-801. OPERATION CHECKED GOOD.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 36,491 hrs · 32,275 cycles

ANTI-ICE DUE FLAPS FAIL ON EICAS, DECLARED AN EMERGENCY. R & R RT FLAP VELOCITY SENSOR IAW MM 27-51-12. OPERATIONS CHECKED GOOD. IAW NRWC-655-02425 & NRWC-655-0246.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,246 hrs · 32,049 cycles

RIGHT EXTERNAL OVERWING EMER LIGHT INOPERATIVE. R & R RT EXTERNAL OVERWING EMER LAMP IAW AMM 33-50-10-000-801 & 33-50-10-400-801. OPERATIONS CHECKED GOOD.

Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 35,950 hrs · 31,776 cycles

ON TAKEOFF CREW RECEIVED PACK 1 CLOSED MSG. NR 1 PACK CLOSE WILL NOT OPEN. CREW COMPLIED WITH AOM VOL 1 PROCEDURES & RETURNED WITHOUT INCIDENT. FLIGHT CREW PLACARD NR 1 PACK MEL 2129.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,784 hrs · 31,630 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,784 hrs · 31,630 cycles

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

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,764 hrs · 31,613 cycles

STRONG SMELL OF ELEC FUMES IN COCKPIT. OPERATED PACKS IAW GHC, OPERATED COCKPIT LIGHTING SYS IAW MM CH 33. OPERATIONS CHECKED OF W/S ONE & TWO HEAR GOOD IAW MM 30-42-01. PERFORMED GENERAL OLFACTORY INSPECTION OF COCKPIT, NO ABNORMAL SMELL OF ANY KIND NOTED.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 35,691 hrs · 31,547 cycles

INFLIGHT, LOSS OF ALTITUDE INDICATOR WITH RED X, LOSS OF ALTIMETER SETTING, ALT CAPTURE, & AIRSPEED CAPTURE FOLLOWED BY, VERTICAL MODE OFF, INDICATIONS. INDICATIONS CAME BACK AFTER 60 SECONDS & VERTICAL MODE OFF, EXTINGUISHED UPON LANDING ALL ON FIRST OFFICERS SIDE. COMPLIED WITH AMM 34-22-00, NO FAULTS FOUND. NO ASSOCIATED CMC MSGS & NO PREVIOUS HISTORY.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 35,485 hrs · 31,299 cycles

DEPARTING OUT WOULD NOT PRESSURIZE. THEN CABIN ALT REACHED 10100 FT. R & R PRESSURIZATION MANUAL CONTROLLER IAW AMM 21-31-02. ALSO COMPLIED WITH AUTO PRESSURIZATION FUNCTIONAL TEST IAW AMM 21-31-00-700-802-A. FOUND SATISFACTORY AT THIS TIME.

Part: HOLDER — CRACKED (FLASHLIGHT) · airframe 35,226 hrs · 31,024 cycles

AFT CABIN EMER FLASHLIGHT HOLDER ARM CRACKED. R & R AFT CABIN EMER FLASHLIGHT HOLDER. OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: FLASHLIGHT — DIM (CABIN) · airframe 34,494 hrs · 30,330 cycles

REAR CABIN FLASHLIGHT CHARGING BUT VERY DIM. REMOVED & INSTALLED AFT CABIN FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 34,013 hrs · 29,870 cycles

DURING PS 2 CHECK FOUND RT OVERWING EMER LIGHT INOPERATIVE. R & R RT OVERWING EMER LIGHT BULB IAW AMM 33-50-07. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,923 hrs · 28,870 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AT FRAME 75 FASTENER BELOW STRINGER 2R APPROX 1/4 INCHES LONG. INSTALLED DOUBLER, SHIM, FILLER & L-ANGLE IAW ERS-EM-53MR-580.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,923 hrs · 28,870 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75, ABOVE STRINGER 2L. CRACK IS APPROX 1 INCH IN LENGTH. INSTALLED DOUBLER, SHIM, FILLER & L ANGLE IAW ERS-EM-53MR-579.

Part: WIRE — BROKEN (CABIN) · airframe 32,923 hrs · 28,870 cycles

NUMBER 6 EMER LIGHT STRIP HAS BROKEN WIRE. R & R NR 6 PROXIMITY LIGHT IAW AMM 33-50-12.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 32,923 hrs · 28,870 cycles

STRINGER 21L IS CORRODED FWD OF FRAME 13. DAMAGE IS ACCEPTABLE AS IS. RESTORED PROTECTIVE FINISH IAW ERS-EM-5300-555. SEE TURNOVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,923 hrs · 28,870 cycles

INVESTIGATE SKIN CRACK AT FASTENER LOCATED AT FRAME 77 BETWEEN STRINGER 04R. INSTALLED DOUBLER & FILLER AT FRAME 77 & STRINGER 05R IAW ERS-EM-5300-578 & SRM 53-32-01.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 32,923 hrs · 28,870 cycles

MAIN PAX DOOR CUT OUT FWD LOWER SUPPORT BRACKET IS CRACKED. R & R BRACKET AT MAIN PAX DOOR CUT OUT, FWD, LOWER SUPPORT IAW SRM 51-20-03, 51-40-02 & CPM 51-21-06 & ETN EM-51-091.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,923 hrs · 28,870 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 ABOVE STRINGER 2L CRACK IS APPROX 1 INCH IN LENGTH. REPAIRED LT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 ABOVE STRINGER 2L IAW ERS-EM-53MR-579.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,923 hrs · 28,870 cycles

INVESTIGATE SKIN CRACK AT FASTENER LOCATED AT FRAME 77 BETWEEN STRINGER 08R & 09R, CRACKS FOUND. REMOVED DAMAGE & INSTALLED BUSHING, ONE EACH IAW ERS-EM-5300-578, SEE TURNOVER FOR DETAILS.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,923 hrs · 28,870 cycles

RIGHT BEAM CRACKED AT OTBD SUPPORT AT FRAME 47. R & R RT OTBD OMEGA BEAM SUPPORT FROM FRAME 47 TO 52 IAW SRM 53-23-02, 51-20-03, 51-40-02 & CPM 51-21-06. SEE WIP ENTRIES FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,923 hrs · 28,870 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AT FRAME 75 FASTENER BELOW STRINGER 2R APPROX 1/4 INCHES LONG. REPAIRED RT UPPER FUSELAGE SKIN CRACKED AT FRAME 75 FASTENER BELOW STRINGER 2R IAW ERS-EM-53MR-580.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,923 hrs · 28,870 cycles

LEFT BEAM CRACKED AT OTBD SUPPORT AT FRAME 47. R & R LT OTBD OMEGA BEAM SUPPORT FROM FRAME 47 TO 52 IAW SRM 53-23-02, 51-20-03 & 51-40-02. SEE WIP ENTRIES FOR DETAILS.

Part: SKIN — DENTED (PAX DOOR) · airframe 32,923 hrs · 28,870 cycles

THE PAX DOOR EXTERNAL SKIN IS DENTED NEAR THE BOTTOM CTR. THE PAX DOOR EXTERNAL SKIN DENT NEAR THE BOTTOM CTR ACCEPTED AS IS IAW ERS-EM-5200-164. ADL 6550065 ADDED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,923 hrs · 28,870 cycles

CARGO INTERIOR SKIN BETWEEN FRAME 61 - 62 & STRINGER 21L - 21R HAS MULTIPLE SPOTS OF CORROSION. DAMAGE ON THE CARGO INTERIOR SKIN BETWEEN FRAME 61 - 62 & STRINGER 21L - 21R ACCEPTED AS IS IAW ERS-EM-5300-556. SEE WIPS & TASKS FOR DETAILS.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 32,320 hrs · 28,374 cycles

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

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,302 hrs · 28,355 cycles

EMERGENCY EXIT SIGN LOCATED ABOVE SEAT 3BC ON FWD BULKHEAD WALL INOPERATIVE. R & R INVERTER ASSEMBLY FOR EMERGENCY EXIT SIGN, OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: PRESSURE SWITCH — FAILED (BLEED AIR SYS) · airframe 32,069 hrs · 28,178 cycles

AFTER TAKEOFF, HS VLV FAIL. WHEN PULLING THRUST BACK MSG WENT AWAY, WHEN THRUST WAS UP MSG REAPPEARED. THERE ALSO SOME FUMES SMELLED AFTER TAKEOFF NOT SURE IF THEY WERE ASSOCIATED. BOTH BLEED TEMPS REMAINED VERY LOW. R & R HIGH STAGE NR 2 PRESS SWITCH IAW 36-11-07 , OPERATIONS CHDCKED GOOD.

Part: SIGN — LOOSE (ROW 12C) · airframe 31,238 hrs · 27,557 cycles

ROW 12C SEAT, EMERGENCY EXIT SIGN FRAME LOOSE. REPLACED MISSING SCREW ON EMERGENCY EXIT SIGN AT 12C IAW AMM 33-50-07.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 30,863 hrs · 27,253 cycles

RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT OVERWING EMERGENCY LIGHT IAW AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,630 hrs · 27,072 cycles

NR 2 PACK IN AUTO MODE, F/A AND PASSENGERS REPORTED A BAD ODOR AND EXCESSIVE HEAT TOWARDS BACK OF ACFT. PERFORMED OPS CHECK OF NR 2 PACK IAW AMM 21-51-00. OPS CHECK GOOD AT THIS TIME COULD NOT DUPLICATE ODOR AND CABIN COOLING PROPERLY.

Part: FLASHLIGHT ASSY — INOPERATIVE (FWD CABIN) · airframe 30,458 hrs · 26,938 cycles

THE CREW REPORTED THE FWD FLASHLIGHT IN CABIN WAS INOPERATIVE. ACFT OK FOR SERVICE. R & R FLASHLIGHT AND CRADLE ASSY. OPS CHECKED GOOD IAW AMM 33-50-16. ACFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 30,319 hrs · 26,832 cycles

F/A FLASHLIGHT CRADLE BROKEN. R & R CRADLE IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,063 hrs · 25,850 cycles

DURING B INSPECTION FOUND THE CABIN CEILING EMERGENCY LIGHT 2 FROM THE FRONT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN CEILING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,141 hrs · 25,075 cycles

DURING B INSPECTION FOUND THE AFT CEILING EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 AC/DC INVERTER IAW EMB145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — FAILED (CABIN) · airframe 28,049 hrs · 25,002 cycles

DURING B INSPECTION FOUND THE 1, 2, 3 & 4 EMERGENCY BATTERIES FAILED CHECK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERIES AND THE BATTERY CHARGER ASSEMBLIES. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,044 hrs · 24,997 cycles

DURING B INSPECTION FOUND THE CABIN AREA EMERGENCY LIGHT STRIPS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 INVERTER IAW EMB-145 AMM 33-50-11. REMOVED AND REPLACED CONNECTOR ON FIRST AND LAST FLOOR EMERGENCY LIGHT STRIPS IAW EMB-145 SWPM 20-21-00, AND REPLACED EMERGENCY LIGHTING POWER SUPPLIES #1-4I AW MNTC WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 28,044 hrs · 24,997 cycles

DURING MAINTENANCE INSPECTION NOTICED THE FLIGHT ATTENDANT EMERGENCY FLASHLIGHT WAS MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THE MISSING FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 27,204 hrs · 24,359 cycles

ON FLIGHT 2878 THE FLIGHT ATTENDANT REPORTED THE FORWARD FLASHLIGHT IS WEAK AND DOESN'T CHARGE DISPITE RED LIGHT OF CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 3,421 hrs · 24,157 cycles

ON FLIGHT 3421 THE CREW REPORTED THAT AFTER FLAP 45 WAS SELECTED AND INDICATED " FLAP FAIL" MESSAGE APPEARED ON EICAS FLAP DID NOT RETRACT AFTER LANDING. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORM OPERATIONAL CHECK ON FLAP SYSTEM FROM 0 TO 45 ABOUT 20 TIMES. THE OPERATIONAL CHECK WAS GOOD PER AMM 27-53-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,820 hrs · 24,047 cycles

DURING B-INSPECTION FOUND THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVER THE WING EMERGENCY LAMP IAW EMB 145 AMM 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 SREVICE.

Part: FAN — FAILED (COCKPIT) · airframe 25,361 hrs · 22,942 cycles

STRONG ODOR SIMILAR TO BURNING RUBBER EMANATING FROM COCKPIT AREA DURING DESCENT. NO SMOKE NOTED NOTHING OBSERVED OTHERWISE. REMOVED AND REPLACED RT EXHAUST FAN PER 21-26-02. OPS CHECK GOOD. PASSED FCF.

Part: UNKNOWN — MALFUNCTIONED (FIRE DETECTION) · airframe 25,343 hrs · 22,930 cycles

DURING PREFLIGHT INSPECTION FOUND THE BAGGAGE EXTINGUISHER LIGHT DOES NOT ILLUMINATE DURING FIRE TEST. THE LIGHT DID NOT ILLUMINATE AND STAYED ON AFTER TEST. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH OPERATIONAL CHECK OF FIRE DETECTION SYSTEM IAW AMM 26-10-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,999 hrs · 22,678 cycles

ON FLIGHT 3579 DURING THE CLIMB THE FLIGHT ATTENDANT REPORTED SHE SMELLED SMOKE AND SAW SMOKE COMING FROM AROUND THE MAIN PASSENGER DOOR. THE ODOR WENT AWAY AFTER A COUPLE OF MINUTES. THE CREW ELECTED TO RETURN AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ENGINE RUN'S NO ODOR OR SMOKE ANY WHERE IN AIRCRAFT NO DISCREPANEY NOTICE IAW AMM EMB 145 71-00-06. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,174 hrs · 21,334 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AILERON PULLY SUPPORT AT FRAME 15 AND STRINGER 21 LEFT TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED SUPPORT BY INSTALLING A DOUBLER IAW AE EO EM-5300-1704 PART B. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,174 hrs · 21,334 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CENTER FUESLAGE 1 LEFT SHEAR CLIPS AT FRAME 15 AND FRAME 16 BETWEEN STRINGER 21 LEFT AND 21 RIGHT TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED BY BLENDING OUT CORROSION AND RESTORING PROTECTIVE COATING IAW AE EO EM-5300-1704 PART A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,174 hrs · 21,334 cycles

DURING MAINTENANCE BASE VISIT FOUND STRINGER 21 RIGHT FORWARD OF FRAME 13 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED STRINGER 21 RIGHT WITH NEW STRINGER 21 RIGHT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CHAFED (FUSELAGE) · airframe 23,174 hrs · 21,334 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 19 CHAFED AT STRINGER 3 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR IAW EO-EM-53MR-1698. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,174 hrs · 21,334 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AILERON FORWARD RIGHT HAND TORQUE TUBE INBOARD MOUNT BEARING HOUSING SUPPORT CHORDED AT LOWER INBOARD FLANGE TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SUPPORT WITH NEW SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (ELEVATOR) · airframe 23,174 hrs · 21,334 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT ELEVATOR UPPER SKIN DAMAGED BY A LIGHTNING STRIKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED BY INSTALLING DOUBLER AND FILLER IAW EO EM-55MR-327 PT B. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,432 hrs · 20,755 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE RIGHT OVERHEAD WING EMERGENCY EXIT LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,432 hrs · 20,755 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT AT 12A TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP ABOVE SEAT 12A IAW EMB 145 AMM 33-50-08-000-801-A/33-50-08-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 21,893 hrs · 20,342 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CEILING OVERHEAD EMERGENCY EXIT LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE WIRE CONNECTOR. THE OPERATIONAL CHECK WAS GOOD IAW WIRING MANUAL 20-00-03 AND AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE WARNING — MALFUNCTIONED (LAVATORY) · airframe 21,068 hrs · 19,707 cycles

ON FLIGHT 3654 DURING CRUISE THE CREW REPORTED A "LAV SMOKE" MASTER WARING MESSAGE. CIRCUIT BREAKER E11 & E12 WAS PULLED PER AIRCRAFT OPERATING MANUAL VOL 1 AND THE FIRST OFFICER INVESTIGATED THE LAVATORY. NO EVIDENCE OF FIRE ANYWHERE. THE LAVATORY WAS THEN LOCKED DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED TEST OF THE LAVATORY SMOKE DETECTION SYSTEM PER EMB 145 AMM 26-11-00. THE OPERATIONAL CHECK WAS GOOD, NO DEFECTS NOTED. NO PARTS WERE REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL CABLE — WORN (AILERONS) · airframe 13,348 hrs · 12,921 cycles

FOUND LEFT INBOARD AILERON CABLE WORN AT FRAME 25 FAIRLEAD. REMOVED AND REPLACED AILERON CABLE IAW EMB AMM 27-11-01. OPERATIONAL CHECK GOOD, RETURNED TO SERVICE.

Part: CONTROL CABLE — WORN (AILERONS) · airframe 13,348 hrs · 12,921 cycles

FOUND RIGHT OUTBOARD AILERON CABLE WORN AT FRAME 35 FAIRLEAD. REMOVED AND REPLACED AILERON CABLE IAW EMB AMM 27-11-01. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: CONTROL CABLE — WORN (AILERONS) · airframe 13,348 hrs · 12,921 cycles

FOUND LEFT OUTBOARD AILERON CABLE WORN AT FRAME 35 FAIRLEAD. REMOVED AND REPLACED AILERON CABLE IAW EMB AMM 27-11-01. OPERATIONAL CHECKED GOOD - RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,348 hrs · 12,921 cycles

FOUND ANGLE ON LEFT OMEGA BEAM CORRODED AT FRAME 20. REMOVED AND REPLACED ANGLE IAW EMB SRM 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,348 hrs · 12,921 cycles

FOUND CORROSION BEYOND LIMITS ON FORWARD SERVICE DOOR SILL. REPAIRED SILL IAW SRM 53-21-10, FIGURE 204, PAGE 216. INSTALLED NEW DOUBLER IAW EMB IC2007-145/00685, AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

MAINTENANCE DISCOVERED RIGHT OVERWING EMERGENCY HATCH LIGHT INOPERATIVE. REPLACED NUMBER THREE EMERGENCY BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SIGN — FAILED (EMERGENCY EXIT)

MSN - FLT 4242 - OVERWING EMERGENCY EXIT LOCATION SIGN FAILS TO ILLUMINATE. REPLACED THE CEILING EMERGENCY EXIT LOCATION SIGN IAW EMB 145 AMM 33-5-15. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

FOUND THE RIGHT OVERWING AND INSIDE CABIN EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 2 AND 4 EMERGENCY BATTERY SUPPLIES IAW EMB 145MM 33-50-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED AN EXTERNAL DOUBLER, FILLER, THREE SHIMS AND PLATE. REPAIR DONE IAW EMB SRM, SRM EMB-145/1142 REV 28, CHAPTER 53-21-10. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, STRINGER 19R WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/1147 PARA 8 DATED MARCH 3, 2005. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING INSPECTION OF THE AIRCRAFT, FOUND THE SERVICE DOOR CENTER SILL CORRODED. BLENDED THE CENTER SILL TO REMOVED THE CORROSION AND PERFORMED NDT INSPECTION. FABRICATED THREE REPAIR DOUBLERS, REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 28, CHAPTERS 53-21-02. (M)

Part: AILERON — LIGHTNING STRIKE (LT WING)

DFW - FLT 3473 - DURING CLIMB-OUT, AIRCRAFT WAS STRUCK BY LIGHTNING. AFTER INSPECTION REPLACED LEFT AILERON AND RIGHT ELEVATOR TRIM TAB. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

ORD - FLT 4286 - AFTER TAKEOFF WHEN CREW SELECTED WINDSHIELD HEAT ON THE WINDSHIELD STARTED TO BUBBLE AND THEN SHATTERED. CREW DECLARED AN EMERGENCY AND RETURNED TO ORD WITH NO OTHER INCIDENTS. (M)