N605KS

Part: SWITCH — MALFUNCTIONED (BLEED LEAK) · airframe 50,267 hrs · 42,671 cycles

BLEED 2 LEAK. DECLARED EMERGENCY "TRANSFERRED TO NRWC 605-DFW-03237". C/A: REPLACED ENGINE START GROUND CONNECTION LEAK SWITCH S7263, PER MM 36-20-02. OPERATIONS CHECK GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 50,030 hrs · 42,459 cycles

FLIGHT ATTENDANT FORWARD EMERGENCY FLASH LIGHT INOPERABLE. MEL 2553-AUTH NR 110047-C. C/A: FOUND F/A'S FWD EMERGENCY FLASH LIGHT HOLDER BROKEN. R & R F/A'S FLASH LIGHT HOLDER. OPERATIONS CHECKED GOOD, IAW AMM 33-50-16. MEL ITEM RESTORED.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 49,889 hrs · 42,318 cycles

FWD RT EXTERIOR EMERGENCY LIGHT INOP. C/A: R&R EXTERNAL EMERGENCY LIGHT LAMP, IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD, IAW EMB 145 AMM 33-50-00.

Part: SIGN — UNSECURE (CABIN) · airframe 49,382 hrs · 41,835 cycles

EMERGENCY EXIT SIGN ON CEILING NEXT TO THE GALLEY IS FALLEN DOWN AND HANGING BY WIRES-C/A-SECURED EXIT SIGN IN PLACE, PERFORMED OPS CHECK. IAW AMM 33-50-00. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 49,199 hrs · 41,629 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED MAIN DOOR EXTERNAL EMERGENCY LIGHT IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 49,030 hrs · 41,472 cycles

EMERGENCY LIGHT AT LH EMERGENCY DOOR IS INOP-C/A-RAR BATTERY POWER SUPPY #3 IAW 33-50-04 AND REMOVED AND REPLACED LH EMERGENCY DOOR EXIT IDENTIFIER SIGN IAW 33-50-13 OPERATIONAL CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1ASMI S/N 73057

Part: SKIN — DENTED (FRAMES 4-5) · airframe 49,004 hrs · 41,438 cycles

DURING MBV INSPEECTION, QC FOUND A DENT BETWEEN FRAMES 4-5, STRINGERS 11R-14R-C/A-REPAIRED DENT BETWEEN FRAMES 4-5 AND STRINGERS 11R-14R IAW ERS-EM-53MR- 4022.

Part: PROFILE — CORRODED (PAX DOOR) · airframe 49,004 hrs · 41,438 cycles

DURING MBV INSPECTION, QC FOUND CORROSION ON THE PAX DOOR LOWER NUT PLATE HOLE.-C/A-REPAIRED CORROSION ON PAX DOOR LOWER NUT PLATE HOLE IAW EMB 145 SRM 52-10-02 AND ETN-EM-52-041 STEP 2. (REPAIR MATERIAL: DOUBLER 2024T3, 0.040")

Part: FLOOR SUPPORT — CORRODED (FRAMES 19-21) · airframe 49,004 hrs · 41,438 cycles

DURING MBV INSPECTION, QC FOUND THE GALLEY LH FLOOR BEAM CORRODED AT CARBON CROSS MEMBER AT FR 20.-C/A-REPAIRED GALLEY LH FLOOR BEAM AT CARBON CROSS MEMBER AT FR 20 IAW EMB 145 SRM 53-00-10RE ITEM 2. (REPAIR MATERIALS: EXTERNAL ANGLE 2024T3 0.050", FILLER 2024T3 0.050", SHIM 2024T3 0.090", PLATE 2024T3 0.125")

Part: CHANNEL — CORRODED (FRAMES 19A-22) · airframe 49,004 hrs · 41,438 cycles

DURING MBV INSPECTION, QC FOUND THE SERVICE DOOR CENTER SILL CORRODED AT PREVIOUS BLENDED AREAS.-C/A-REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 49,004 hrs · 41,438 cycles

DURING MBV INSPECTION, QC FOUND THE CARGO DOOR INNER BEAM ON VB4 BETWEEN HB3 AND HB4 CRACKED.-C/A-REMOVED AND REPLACED CARGO DOOR INNER BEAM ON VB4 BETWEEN HB3 AND HB4 IAW EMB 145 SRM 51-40-02 AND ERS-EM-5200-1051. (P/N INSTALLED: 145-25939-601)

Part: PROFILE — CORRODED (CARGO DOOR) · airframe 49,004 hrs · 41,438 cycles

DURING MBV INSPECTION, QC FOUND THE CARGO DOOR LOWER PROFILE NUT PLATE HOLES CORRODED.-C/A-REMOVED AND REPLACED CARGO DOOR LOWER PROFILE IAW EMB 145 SRM 51-40-02.

Part: WEB — GOUGED (CARGO DOOR) · airframe 49,004 hrs · 41,438 cycles

DURING MBV INSPECTION, QC FOUND 2 PREVIOUS REPAIR DOUBLERS ON CARGO DOOR INNER SKIN WEB WITH GOUGES-C/A-REMOVED AND REPLACED 2 PREVIOUS REPAIR DOUBLERS ON CARGO DOOR INNER SKIN WEB IAW EMB 145 SRM 52-30-01-RE ITEM #12. (REPAIR MATERIAL: DOUBLER 2024T3 0.050)

Part: SKIN — CRACKED (CRGO DOOR HANDLE) · airframe 49,004 hrs · 41,438 cycles

DURING MBV INSPECTION, QC FOUND THE CARGO DOOR HANDLE CUTOUT CRACKED AT AFT UPPER END.-C/A-CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER TO CARGO DOOR HANDLE CUTOUT IAW ERS-EM-52MR-1052. (REPAIR MATERIAL: 2024-T3, 0.050)

Part: LIGHT — DAMAGED (CABIN) · airframe 49,004 hrs · 41,438 cycles

8EA FLOOR PROXIMITY LIGHT PANELS DAMAGED-C/A-COMPLETE:REMOVED AND REPLACED ALL FLOOR PROXIMITY LIGHT PANELS IAW EMB 145 AMM 33-50-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,004 hrs · 41,438 cycles

EMERGENCY LIGHT UNDER PANEL 233BLC AND COCKPIT STEP UP PANEL INOP-C/A-COMPLETE:REMOVED AND REPLACED WARDROBE EMERGENCY LIGHTS DC/AC INVERTER IAW EMB 145 AMM 33-50-11. OPC GOOD.

Part: LIGHT — BROKEN (RH CABIN) · airframe 49,004 hrs · 41,438 cycles

RH CABIN FLOOR EMERGENCY LIGHT STRIPS BROKEN (5 EA)-C/A-COMPLETE:REMOVED AND REPLACED 5 RH FLOOR EMERGNCY LIGHT STRIPS AS REQUIRED.

Part: LIGHT — BROKEN (CABIN) · airframe 49,004 hrs · 41,438 cycles

LH ANGLE EMERGENCY LIGHT STRIP FOR PANEL 231FF IS BROKEN-C/A-COMPLETE:REMOVED AND REPLACED LH ANGLE EMERGECNY LIGHT STRIP FOR PANEL 231FF IAW EMB 145 AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,004 hrs · 41,438 cycles

#2, #4, #6, #7, AND #8 FLOOR PROXIMITY LIGHT STRIPS DAMAGED-C/A-COMPLETE:REMOVED AND REPLACED #2, #4 , #6, #7, AND #8 FLOOR PROX LIGHT STRIPS IAW EMB-145 AMM 33-50-12.

Part: ACM — FAILED (AC BAY) · airframe 48,698 hrs · 41,129 cycles

AT CRUISE FL 240 FA REPORTED PASSENGERS AT SEAT 11 B/C WERE REPORTING NOISES COMINF FROM LOWER RIGHT SIDE FOLLOWED BY CABIN SMOKE MERGENCY WAS DECLARED AND EMERGENCY PROCEDURES COMPLIED WITH DURING DESCENT SMOKE STOPPED IN CABIN LANDED SAFETY SAFELY IN CHS OVERWEIGHT LANDING AT 44900LBS SMOOTH NORMAL LANDING AT LESS THAN 100FPM-C/A-INSPECTED ACTF AND FOUND TO BE NUM 2 PACK SYS FOR CAUSE OF SMOKE NO OTHER DESCREPANCIES NOTED FLIGHT CREW PLACARDED #1 PACK MEL# 21-28 AUTH# 110034D-C MOC# 730088. CHANGED MEL 21-28 TO MEL 21-29 BOTH PACKS INOP AUTH 110034DM-C M PROCEDURES C/W AUTH 110034DM-C REF 21-29 NO OVERWEIGHT INSP REQUIRED DUE TO SINK RATE LESS THAN 360 FEET PER MIN. C/W EO# EM-2100-048 SATISFACTORY. COMPLETED #2 ACM INSTALLATION IAW AMM# 21-51-03-400-801-A. COMPLETED #2 PACK DUAL HEAT EXCHANGER INSTALLATION IAW AMM# 21-51-02-400-801-A. REPLACED #2 PACK CONDENSER MIXER IAW AMM 21-51-04. REMOVED AND REPLACED #2 PACK EXHAUST DUCT IAW AMM 21-51-02. C/W INSPECTION FUEL QUANTITY INDICATION HARNESS SATISFACTORY IAW AMM 28-41-00. REPLACED #2 RECIRCULATION FAN IAW AMM 21-24-01. CLEARED MEL 21-29. RH HEAT EXCHANGER P/N 816630-2 S/N 9801070; RH CONDERNSER/MIXER P/N 816650-2 S/N 9802122; REECIRCULATION_GASPER FAN P/N 4611028900 S/N 1823

Part: VALVE — FAILED (AC BAY) · airframe 48,695 hrs · 41,126 cycles

#1 PACK OVLD AND #1 PACK VALVE FAIL IN FLIGHT CLIMBING THROUGH FL340. QRH PROCEDURE FOLLOWED.-C/A-FLIGHT CREW PLACARDED #1 PACK. MEL# 21-28 AUTH# 110034D-C MOC# 730088. CHANGED MEL 21-28 TO MEL 21-29 BOTH PACKS INOP AUTH 110034DM-C M PROCEDURES C/W AUTH 110034DM-C REF 21-29. REMOVED AND REPLACED DUCT ON #1 PACK TO RAM AIR CONNECTION IAW AMM 21-51-03 AND REMOVED AND REPLACED # 1 PACK VALVE IAW AMM 21-51-01, OPC GOOD. REPLACED LH MUFFLER IAW AMM 21-24-01. C/W EO# EM-2100-048 SATISFACTORY. CLEARED MEL 21-29. PRIMARY INLET LH DUCT P/N 816618-1

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,689 hrs · 41,121 cycles

FWD MOST CENTER CEILING EMERGENCY LIGHT IN CABIN INOP-C/A-REMOVED AND REPLACED FWD MOST CENTER CEILING EMERGENCY LIGHT IN CABIN IAW AMM TASK 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END.

Part: DUCT — INOPERATIVE (NR 1 A/C PACK) · airframe 48,658 hrs · 41,090 cycles

PACK 1 OVRLD MESSAGE IN FLIGHT COMPLETED QRH, PAX NOTED NOISE & SMELL IN CABIN-C/A-REMOVED AND REPLACED DUCT IAW AMM TASK 21-51-01.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,347 hrs · 40,799 cycles

MAIN DOOR EXTERIOR EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED MAIN DOOR EXTERIOR EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD.

Part: FAN — FAILED (AFT RECIRC) · airframe 48,277 hrs · 40,728 cycles

STRONG FOUL ODOR COMING FROM RUNNING THE PACKS-C/A-FOUND STRONG ODOR COMING FROM GASPERFAN (PAX VENTS AND COCKPIT VENTS) DEFERED GASPER FAN AS PER MEL 21-4 (M) PROCEDURES C/W. REPLACED GASPER FAN IAW EMB 145 AMM 21-23-03 NORMAL OPERATION NOTED MEL 21-4 RESTORED

Part: SPAR — CRACKED (TE FLAP) · airframe 48,040 hrs · 40,517 cycles

CRACK IN AFT SPAR 6.1 INCHES LONG LT IB FLAP. C/A-REPAIRED IAW ERS-EM-57MR-1140 PART A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 47,486 hrs · 40,013 cycles

BLEED 2 LEAK IN CLIMBOUT. C/A-PERFORMED LEAK CHECK OF NR 2 BLEED SYSTEM IAW MM 36-00-00 AND ETNEM-36-063. OPS CK AND LEAK CHECK GOOD,

Part: WARNING LIGHT — FALSE INDICATION (NR 1 A/C PACK) · airframe 47,264 hrs · 39,790 cycles

PACK 1 OVERLOAD DURING T/O ROLL. T/S PACK 1 OVERLOAD PER FIM TASK EMB145 FIM 21-51-00-810-801A STEPS 1-3 FOUND TO BE A TRANSITORY CONDITION OF THE A/C SYSTEM. PERFORMED OP CK OF THE A/C SYSTEM IAW EMB 145AMM 21-51-00 NO DEFECTS NOTED

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,217 hrs · 39,754 cycles

RT FUSELAGE SKIN CRACKED AT FR 12A STR 6R. C/A-PERFORMED PERMANENT REPAIR RT FUSELAGE SKIN CRACKED AT FR 12A STR 6R IAW ERS-EM-53MR-3701.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,217 hrs · 39,754 cycles

RT WINDSHIELD LATERAL POST UPPER SKIN CRACKED BETWEEN WINDSHIELD AND DV WINDOW OPENING. C/A-PERFORMED PERMANENT REPAIR ON RT WINDSHIELD LATERAL POST UPPER SKIN CRACKED BETWEEN WINDSHIELD AND DV WINDOW OPENING IAW ERS-EM-53MR-3701.

Part: CONNECTOR — BROKEN (CABIN) · airframe 47,217 hrs · 39,754 cycles

EMERGENCY FLOOR LIGHT STRIP AT PANEL 241BF HAS BROKEN CONNECTORS. C/A-REPLACED BROKEN CONNECTORS ON EMERGENCY FLOOR LIGHT STRIP AT 241BF IAW SWPM 20-21-00 AND 20-00-03. CONNECTOR P/N M39029/32-248.

Part: FRAME — DENTED (FUSELAGE) · airframe 47,217 hrs · 39,754 cycles

FRAME 4 BENT BETWEEN STR 4R AND 6R. C/A-PERFORMED PERMANENT REPAIR ON FR 4 AND STR 4R-6R IAW ERS-EM-53MR-3690.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,217 hrs · 39,754 cycles

FWD FUSELAGE 1 RT SKIN HAS DENT AT FR 4 BETWEEN STR 4R-6R. C/A-PERFORMED PERMANENT REPAIR ON FWD FUSELAGE 1 RT SKIN AT FR 4 AND STR 4R-6R IAW ERS-EM-53MR-3690.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 47,217 hrs · 39,754 cycles

RT OMEGA BEAM INBD SUPPORT CRACKED AT FWD END OF REPLACEMENT PIECE BETWEEN FR47 AND FR48. C/A-REMOVED AND REPLACED RT OMEGA BEAM IAW SRM 53-23-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,217 hrs · 39,754 cycles

DENT FWD OF CARGO DOOR BUMPER. C/A-PERFORMED PERMANENT REPAIR OF THE DENT FWD OF CARGO DOOR BUMBER IAW SRM 53-31-01.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 47,217 hrs · 39,754 cycles

FR 3 FRAME AND SPLICE BELOW STR 11L HAS EXISTING #40 HOLE DAMAGE. C/A-PERFORMED PERMANENT REPAIR ON FR 3 AND SPLICE AT STR 11L IAW ERS-EM-53MR-3672.

Part: SHUNT — CORRODED (FUSELAGE) · airframe 47,217 hrs · 39,754 cycles

CORROSION ON APU CONNECTING BAR MOUNTING SUFACE SHUNT. C/A-PERFORMED PERMANENT REPAIR ON APU CONNECTING BAR SHUNT AND FR 80 IAW ERS-EM-53MR-3675.

Part: SPLICE — DEFECTIVE (EXIT LIGHT) · airframe 47,217 hrs · 39,754 cycles

COCKPIT STEP EMER LIGHT INOP. C/A-COMPLETE:REMOVED AND REPLACED SPLICE SP9016 AND SP9017 IAW SWPM 20-00-03, 20-21-00, 20-50-01, 20-50-00. EASI TOOL #102. OPERATIONAL CHECK GOOD.

Part: STRUCTURE — CRACKED (EXIT LIGHT) · airframe 47,217 hrs · 39,754 cycles

NR 4 FLOOR LIGHT STRIP EXTRUSION CRACKED. C/A-COMPLETE:REMOVED AND REPLACED NR 4 FLOOR LIGHT STRIP EXTRUSION IAW AMM 33-50-12.

Part: ENGINE — WARNING MESSAGE (NR 1) · airframe 47,110 hrs · 39,672 cycles

E1 OIL PRESSURE DECREASED TO AMBER RANGE IN FLIGHT. (CAPTAINS SAID IT HAPPENED 40 MINUTES INTO FLIGHT AT 35K FT, E1 OIL PRESSURE DECREASED INTO AMBER RANGE BUT NEVER TURNED RED.) FOLLWED QRH FOR LOW OIL PRESSURE WITH NI EICAS MSG PRESENT. STARTED WITH 12 QUTS OF OIL. GOT TO SDF WITH 10 QTS ON EICAS. REMOVED & REPLACED # 1 ENGINE, OPS CHECK GOOD.

Part: CLAMP — LOOSE (AC BAY) · airframe 46,633 hrs · 39,287 cycles

BLEED 2 LEAK. FOUND PACK VALVE CLAMP LOOSE. RESECURED CLAMP. FOUND NO FURTHER LEAKS. OPS CHECK GOOD. NO FURTHER EICAS MESSAGE.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 46,043 hrs · 38,744 cycles

BLEED 2 LEAK IN FLIGHT. ON GROUND MESSAGE WENT AWAY. FOUND AIR LEAKING IN ZONE 270 IN CARGO COMPARTMENT. REPLACED O-RINGS AND RESECURED COUPLINGS 272CRW AND 272BF. NO MORE LEAKS DETECTED. OPS CHECK GOOD

Part: WIRE — BROKEN (FLASHLIGHT) · airframe 45,524 hrs · 38,283 cycles

CAPTAIN`S EMERGENCY FLASHLIGHT HAS A BROKEN WIRE. REPAIRED THE WIRE. OPS CHECKED GOOD.

Part: CLAMP — LOOSE (NR 2 BLEED) · airframe 43,434 hrs · 38,212 cycles

BLEED 2 LEAK EICAS MESSAGE. SECURED THE CLAMPS ON THE PRSOV, OPS AND LEAK CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 45,099 hrs · 37,911 cycles

CARGO SMOKE ON EICAS ACCOMPANIED BY THE CARGO EXTINGUISH BUTTON ILLUMINATION. DEPLOYED FIRE BOTTLE IN THE CARGO BAY. R & R THE CARGO SMOKE DETECTOR. OPS CHECKED GOOD. R & R THE CARGO BAY FIRE EXTINGUISHER BOTTLES. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (FLOOD LIGHT) · airframe 44,608 hrs · 37,466 cycles

COCKPIT FLOOD LIGHT IS INOPERATIVE. R & R THE LAMP, OPS CHECKED GOOD.

Part: SKIN — CRACKED (FRAME 75) · airframe 44,123 hrs · 37,005 cycles

SKIN CRACKED ABOVE STRINGER 2L FRAME 75. CUTOUT DAMAGE AND APPLIED FILLER AND DOUBLER .

Part: SKIN — CORRODED (FRAME 13) · airframe 44,123 hrs · 37,005 cycles

AREA OF CORROSION ON FUSELAGE INNER SKIN AFT OF FRAME 13 BETWEEN STRINGER 19R AND 20R. PERFORMED CUTOUT TO REMOVE THE DAMAGED SECTION. FABRICATED AND INSTALLED REPLACEMENT SKIN SECTION AND SPLICE.

Part: LIGHT — UNKNOWN (CABIN) · airframe 43,611 hrs · 36,565 cycles

LARGE EMERGENCY EXIT LIGHT, AFT OF LT OVERWING EXIT IS INOPERATIVE. OPS CHECKED LARGE EMERGENCY EXIT LIGHT, AFT OF LH OVERWING EXIT(#23), OPS CHECK GOOD.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG) · airframe 42,395 hrs · 35,604 cycles

LANDING GEAR AIR TO GROUND ON EICAS AND E1-2 DISAGREE. REPLACED NOSE PROXIMITY SWITCH AND SERVICED NOSE STRUT, OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,313 hrs · 35,537 cycles

LEFT OVERWING EXIT MARKER NR 23 FAILS TO ILLUMINATE. AFTER CYCLING POWER ON LT OVERWING EXIT MARKER NR 23, OPS CHECK GOOD.

Part: MOUNT BRACKET — CRACKED (LT MLG WW) · airframe 40,561 hrs · 34,124 cycles

LEFT MLG WW PANEL 155QZ MOUNT BRACKET IS CRACKED ON THE TOP END. INSTALLED NEW BRACKET IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,561 hrs · 34,124 cycles

FRAME 10 BELOW DV WINDOW FRAME IS CRACKED APPROX 1 1/2 INCH, LT SIDE. INSTALLED NEW FRAME 10 SECTION BELOW LT DV WINDOW IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 40,561 hrs · 34,124 cycles

LEFT CARGO DOOR, HOLD OPEN SUPPORT BRACKET IS CRACKED, APPROX 1/2 INCH AT THE LOWER ATTACHMENT POINT. R & R LT CARGO DOOR HOLD OPEN SUPPORT BRACKET IAW SRM 51-40-02.

Part: FIREWALL — CRACKED (APU BAY) · airframe 40,561 hrs · 34,124 cycles

APU FIREWALL HAS TWO EACH CRACKS AT THE P274 MAIN ELECTRICAL CONNECTOR, INBD LOWER SCREW ATTACHMENT POINT. CRACKS ARE APPROX 3/8 INCH LONG EACH. REPAIRED AREA IAW SRM CH 53-32-13.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,561 hrs · 34,124 cycles

INNER FUSELAGE SKIN CORRODED AROUND DRAIN VLV BETWEEN STRINGERS 21LT & 21RT ON BOTH SIDES OF FRAME 67. REPAIRED FUSELAGE SKIN CORROSION AT FRAME 67, BETWEEN STRINGER 21LT & 21RT IAW ERS-EM-53MR-1266.

Part: LIGHT — CRACKED (CABIN) · airframe 40,561 hrs · 34,124 cycles

EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT POSITION NR 3 HAS EXPOSED WIRES & AT POSITION NR 7 CRACKED. REPAIRED WIRE W192-8678-22 AT POSITION NR 3, W192-8702-22 AT POSITION NR 4. REPLACED CONNECTOR FOR SP9114 AT POSITION NR 7 IAW SWPM 20-21-00. SEE BOW 186096.

Part: CONNECTOR — CRACKED (CABIN) · airframe 40,561 hrs · 34,124 cycles

NUMBER 6 EMER FLOOR LIGHT STRIP CONNECTOR IS CRACKED. R & R CRACKED QUICK DISCONNECT CONNECTOR ON THE NR 6 EMERGENCY FLOOR LIGHT STRIP IAW SWPM CHAPTER 20-21-00. REF BOW 186096 FOR OPERATIONAL CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 40,561 hrs · 34,124 cycles

NUMBER 2 EMER LIGHT STRIP WIRES ARE BROKEN. R & R NR 2 EMER LIGHT STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,561 hrs · 34,124 cycles

EMERGENCY EXIT LOCATOR SIGN IN CABIN AT EMER EXIT DOORS, HATCHES DO NOT ILLUMINATE ON AFT SIDE. R & R AFT EMER EXIT LOCATING LIGHT AT OVERWING EMER HATCH LOCATION IAW AMM33-50-15. OPERATIONS CHECKED GOOD.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 40,561 hrs · 34,124 cycles

FLOORBOARD CROSSBEAM IS CORRODED AT CTR OMEGA BEAM AT FRAME 20. REPAIR OF CROSSBEAM AT FRAME 20 HAS BEEN COMPLIED WITH IAW ETN-EM-53-241, SRM 51-10-03, CPM 51-21-04, CPM 51-21-05 & CPM 51-21-06.

Part: STRUCTURE — CRACKED (CABIN) · airframe 40,561 hrs · 34,124 cycles

CENTER CABIN FLOOR RT SIDE WALL EXTRUSIONS CRACKED & BROKEN AT POSITION NR 3 OF THE LONG ONES & THE VERY SHORT ANGLED ONE AT RT CORNER. INSTALLED CTR CABIN FLOOR RT SIDE WALL EXTRUSION AT POSITION NR 3 OF THE LONG ONES & THE VERY SHORT ANGLED ONE AT RT FRONT CORNER IAW AMM 33-50-12.

Part: LIGHT — BROKEN (CABIN) · airframe 40,561 hrs · 34,124 cycles

LEFT SIDE WALL EXTRUSIONS THAT HOLD FLOOR PROXIMITY EMER LIGHT STRIPS ARE BROKEN AT POSITIONS 1, 2, 5 & 7. THE EMER LIGHT STRIPS HAVE ALREADY REMOVED FROM THEM. R & R LT SIDE WALL EXTRUSIONS THAT HOLD FLOOR PROXIMITY EMER LIGHT STRIPS AT POSITIONS 1, 2, 5 & 7 IAW AMM 33-50-12. OPERATIONS CHECK OF EMER LIGHT STRIPS GOOD.

Part: HOT WATER POT — DEFECTIVE (GALLEY) · airframe 40,302 hrs · 33,881 cycles

HOT JUG BURNING SMELL FOR A FEW SECONDS, THEN WENT AWAY. INSTALLED NEW COFFEE & HUT JUG IN ORIGINAL, INBD, POSITION FOR 30 MINS & CURRENT POSITION, OTBD FOR 15 MINS WITH BOTH PACS RUNNING & RECIRCS ON & OFF WITH NO SMELLS AT THIS TIME.

Part: PITOT SYSTEM — CONTAMINATED · airframe 40,100 hrs · 33,713 cycles

DEPARTED IN HEAVY PRECIPITATION, EN ROUTE RECEIVED COMPARATOR ANNUNCIATION FOR AIRSPEED MULTIPLE TIMES 4 - 6 KNOT DIFFERENCE AT 360. THEN DESCENDING THROUGH 340 AIRSPEED DIFFERENCE OF APPROX 50 KTS BETWEEN CAPTAIN & FIRST OFFICER AIRSPEED, ALTITUDE DIFFERENCE OF OVER 200'. DRAINED WATER FROM PITOT SYSTEMS 1 - 2 DRAINS. PERFORMED PITOT STATIC LEAK CHECK & FUNCTIONAL CHECK IAW AMM 34-13-00 WITH NO FAULTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,576 hrs · 33,267 cycles

AFT AISLE EMER LAMP INOPERATIVE. R & R AFT AISLE EMER LIGHT LAMP IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.

Part: CARBON SEAL — FAILED (NR 2 ENGINE) · airframe 39,424 hrs · 33,099 cycles

DURING CLIMB OUT, LAVATORY SMOKE MESSAGE. AFTER 10 SECONDS MESSAGE EXTINGUISHED. RETURNED FOR LANDING. LAVATORY SMOKE OPS CHECKED GOOD IAW TASK 26-14-00-700-801-A. TROUBLESHOT ODOR IAW FIM 21-20-00-810-803-A. OIL FOUND IN NR 2 ENGINE FAN CASE. R & R NR 2 ENGINE CARBON SEAL ASSEMBLY IAW RRMM 72-25-25-000-801. OPERATIONS CHECK & LEAK CHECKED GOOD. COMPLIED WITH ETN72-034 ODOR EVENT WORK CARD. OPS CHECKED FAILED. R & R NR 2 ENGINE IAW WORK CARD 71-000-00 ODOR GONE.

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 39,402 hrs · 33,074 cycles

RECEIVED LAVATORY SMOKE WARNING SHORTLY AFTER TAKEOFF, GEAR RETRACTION. UPON INSPECTION FOUND NO TRACES OF FIRE OR SMOKE. SUSPECT FAULTY LAVATORY SMOKE DETECTOR. R & R SMOKE DETECTOR SENSOR IAW AMM 26-14-01. OPERATIONS CHECKED GOOD. NO SMOKE DETECTED AT THE TIME.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 39,330 hrs · 33,019 cycles

EMERGENCY FLOOR STRIP ON SEAT 10A & 11A INOPERATIVE. R & R BATTERY CHARGER ASSEMBLY & HOLDER ASSEMBLY BATTERY IAW AMM 33-50-04. OPERATIONS CHECK WAS GOOD AT THIS TIME. EMER LIGHTING BATTERY PN 2013-1A SN 108497.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 39,279 hrs · 32,972 cycles

EMERGENCY FLOOR LIGHT STRIPS 8A - 12A INOPERATIVE. R & R NR 5 INVERTER & NR 3 BATTERY IAW AMM 33-51-01 & 33-51-02. OPERATIONS CHECKED GOOD INVERTER PN 7824-1.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 38,999 hrs · 32,745 cycles

OVERWING EXIT EMER LIGHT INOPERATIVE. REMOVE & INSTALL INVERTER NR 6 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 38,675 hrs · 32,455 cycles

MAIN CABIN DOOR INOPERATIVE. LUBED MAIN CABIN DOOR IAW 52-18-00. OPERATIONS CHECKED GOOD.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 38,628 hrs · 32,416 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR ROOT SKIN LE. R & R RT ELEVATOR ROOT SKIN TIP IAW ETN-EM-55-073 & SRM 51-40-02.

Part: WIRE — CHAFED (CABIN) · airframe 38,629 hrs · 32,417 cycles

CHAFED WIRES AT MULTIPLE LOCATIONS BETWEEN FRAME 18 - 20 & STRINGER 2R - 3R & BETWEEN FRAME 13 - 14 & STRINGER 4R - 5R. REPAIRED WIRES W192-8035-20, W192-8036-20, W192-8559-20, W192-8560-20, W192-8584-22, W192-8593-20, W192-8627-20, W192-8628-22 & W192-8629-22, W192-8556-20, W192-8561-20, W192-8583-22 & W192-8630-22 IAW SWPM 20-21-00 STEP 8.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 38,628 hrs · 32,416 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR MID SKIN TIP. R & R RT ELEVATOR MID SKIN TIP IAW ETN-EM-55-073 & SRM 51-40-02.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 38,628 hrs · 32,416 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR SKIN TIP. R & R RT ELEVATOR SKIN TIP IAW SRM 51-40-02 & ETN-EM-55-073.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,628 hrs · 32,416 cycles

MULTIPLE HAIL DAMAGE EVENT. REPLACE RT CTR FUSELAGE 1. R & R RT CTR FUSELAGE 1 IAW SRM 51-40-02 & ETN-EM-53-262.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 38,628 hrs · 32,416 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR UPPER CTR SKIN. R & R RT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02 & ETN-EM-55-073.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 38,628 hrs · 32,416 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR SKIN TIP. R & R LT ELEVATOR TIP SKIN IAW SRM 51-40-02 & ETN-EM-55-073.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 38,628 hrs · 32,416 cycles

MULTIPLE HAIL DAMAGE EVENT. REPLACE LT ELEVATOR MID SKIN. R & R LT ELEVATOR MID SKIN IAW SRM 51-40-02 & ETN-EM-55-073.

Part: SKIN — DENTED (LT HORIZ STAB) · airframe 38,628 hrs · 32,416 cycles

MULTIPLE HAIL DAMAGE EVENT. REPLACE LT STABILIZER SKIN. R & R LT HORIZONTAL STAB TOP SKIN IAW SRM 51-40-02 & ETN ETN-EM-55-073.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 38,628 hrs · 32,416 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR OTBD TIP LE. R & R RT ELEVATOR OTBD TIP LE IAW SRM 51-40-02 & ETN-EM-55-073.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,628 hrs · 32,416 cycles

MULTIPLE HAIL DAMAGE EVENT. REPLACE LT CTR FUSELAGE 1. R & R LT CTR FUSELAGE 1 IAW SRM 51-40-02 & ETN-EM-53-262.

Part: SKIN — DENTED (RT HORIZ STAB) · airframe 38,628 hrs · 32,416 cycles

MULTIPLE HAIL DAMAGE EVENT. REPLACE RT STABILIZER SKIN. R & R RT HORIZONTAL STAB TOP SKIN IAW SRM 51-40-02 & ETN-EM-55-073.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 38,628 hrs · 32,416 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR UPPER CTR SKIN. R & R LT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02 & ETN-EM-55-073.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 38,172 hrs · 32,055 cycles

EMERGENCY EXIT LIGHT AT MAIN DOOR STAYS ON IN ARM POSITION. R & R FWD NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: PRESSURE SWITCH — UNSERVICEABLE (BRAKE SYSTEM) · airframe 37,740 hrs · 31,720 cycles

ON FLIGHT 3377 AT START OF TAKEOFF ROLL CREW REPORTED BRAKE ON LIGHT ILLUMINATED FOLLOWED BY MASTER WARNING & CONFIG ILLUMINATED ON EICAS. PERFORMED LOW SPEED ABORT NO UNUSUAL BRAKE PROBLEMS & BRAKE LIGHT ON, STAYS ILLUMINATED REGARDLESS OF BRAKE HANDLE POSITION. NO VOICE FOR TAKEOFF BRAKES HEARD. THE ACFT WAS REMOVED FROM SERVICE. R & R THE EMERGENCY PARKING BRAKE PRESS SWITCH IAW 32-44 07. R & R THE PRESS SWITCH CONNECTOR IAW SWPM 20-13-07, OPERATIONS TESTED GOOD.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 37,419 hrs · 31,469 cycles

HYDRAULIC 1, LOW QUANITY MESSAGE ON EICAS. NR 1 EDP LEAKING. R & R NR 1 EDP IAW AMM 29-10-03. PS-1 CHECK ACCOMPLISHED 11-6-13. ACCOMPLISHED OIL CHECK IAW OIL SERVICE CHECK CARD. FOUND OXYGEN PRESSURE TO BE 1800 PSI SERVICED TO 1850 PSI TEMP 65. IAW AMM 35-12-00.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 37,026 hrs · 31,139 cycles

F/A FLASHLIGHT CRADLE IS BROKEN. R & R F/A FLASHLIGHT CRADLE IAW AMM 33-50-165, OPS CHECKED GOOD.

Part: LIGHT — LOOSE (ROW 12BC) · airframe 36,843 hrs · 30,954 cycles

EMERGENCY EXIT PANEL LIGHT INOPERATIVE. AT ROW 12 BC. RESECURED EMERGENCY EXIT PANEL LIGHT 12 BC IAW AMM 33-50-08 AND OPS TESTED IAW AMM 33-50-00. TESTED SATISFACTORY.

Part: FLASHLIGHT — DAMAGED (COCKPIT) · airframe 36,059 hrs · 30,289 cycles

DURING B INSPECTION FOUND THE FOUND CAPTIAN'S FLASHLIGHT DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW EMM AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 36,028 hrs · 30,265 cycles

ON FLIGHT 3580 THE CREW REPORTED THAT ON LANDING APPROACH THEY NOTICED A STRONG ELECTRICAL ODOR IN THE COCKPIT. THE FLIGHT ATTENDANT SMELLED THE ELECTRICAL ODOR AS WELL IN THE FRONT OF THE AIRCRAFT BUT NOT IN THE BACK OF AIRCRAFT. THE ODOR WENT AWAY UPON REACHING THE GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED FLIGHT ATTENDANT FLASHLIGHT AND BASE INSPECTED & RE-INSTALLED PER EMB 33-50-16. REMOVED AND REPLACED NR 2 EMERGENCY POWER SUPPLY & BATTERY IAW 33-50-04 & 33-50-11. OCK IAW 33-50-00. INSPECTED FORWARD AVIONICS AREA & FANS IAW 21-26-00. CHECKED FOR ODOR BEHIND THE CAPTAIN’S & FIRST OFFICER’S SEAT BY POWER DISTRIBUTION BOXES. NO ODORS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,895 hrs · 30,170 cycles

FLIGHT 9806 CREW REPORTED, CLIMBING THRU FLT LEVEL 210 THEY NOTICED A SLIGHT ELECTRICAL BURNING ODOR IN COCKPIT, IT ESCALATED TO AN INTENSE ODOR. CREW DONNED O2 MASKS & DECLARED AN EMERGENCY AND LANDED AT VPS. AIRPORT FIRE & RESCUE INSPECTED AIRCRAFT. THEY DID NOT FIND ANY FIRE OR SMOKE. DEPLANED AND THE FLT ATTENDANT SMELLED THE ODOR STARTING FROM ROW 6 AND TOWARD THE COCKPIT. AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF NR 1 ENGINE AND NR 1 PACK SYSTEM IAW EMB AMM 21-00-00,72-00-00, AND PERFORMED OPERATIONAL CHECK OF BOTH BLEED SYSTEMS IAW EMB AMM 36-00-00. ALSO PERFORMED ETN# EM-72-034 AND NO SMELL DETECTED. CHECKED ALL CABIN LIGHTS IAW 33-21-00. CHECKED ALL COCKPIT LIGHTS IAW EMB AMM 33-11-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRANK ASSY — INOPERATIVE (F/R FLASHLIGHT) · airframe 35,890 hrs · 30,164 cycles

FLIGHT 3265. FIRST OFFICER’S FLASHLIGHT WAS NOT INDICATING IT WAS CHARGING. REMOVED AND REPLACED THE FIRST OFFICER’S FIASHLIGHT HOLDER IAW AMM-33-51-01. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 35,866 hrs · 30,143 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 5 EMERGENCY LIGHTSTRIP WIRES BROKEN OFF P/N 7881-2. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 EMERGENCY LIGHTSTRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,861 hrs · 30,138 cycles

DURING MAINTENANCE INSPECTION FOUND THE SKIN CRACKED NEAR RIVET HOLE ON FRAME 75 AND BETWEEN 1R/2R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-2114. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: YOKE — CRACKED (LT ENGINE) · airframe 35,861 hrs · 30,138 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT ENGINE FORWARD LOWER YOKE CRACKED FORWARD SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED A NEW SERVICEABLE LEFT ENGINE FORWARD LOWER YOKE IAW AEA EO EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CRACKED (STAB TO FUSELAGE) · airframe 35,861 hrs · 30,138 cycles

LT FWD VERTICAL STAB-TO-FUSELAGE REENFORCEMENT ANGLE CRACKED ON AFT END. REMOVED CRACKED LT FWD VERTICAL STAB-TO-FUSELAGE REINFORCEMENT ANGLE, PREPPED AND INSTALLED SERVICEABLE ANGLE IAW AEA EO EM-53MR-1281.

Part: LIGHT — DAMAGED (CABIN) · airframe 35,866 hrs · 30,143 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 6 LEFT EMERGENCY LIGHT FLOOR EXTRUSIONS DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 LEFT EMERGENCY LIGHT FLOOR EXTRUSIONS IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 35,866 hrs · 30,143 cycles

DURING MAINTENANCE INSEPECTION FOUND THE NR 6 CABIN EMERGENCY LIGHT STRIP BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHTSTRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 35,866 hrs · 30,143 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 3 HAS BROKEN PN-6636-7. THE AIRCRAFT WAS REMOVED FROM SERVICE. UPON FURTHER INVESTIGATION THE NR 3 EMERGENCY LIGHT STRIP WAS DETERMINED TO BE SERVICEABLE AND WAS RE-INSTALLED IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 35,866 hrs · 30,143 cycles

DURING B INSPECTION FOUND THE GALLEY CENTER BEAM GUSSET HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY CENTER BEAM GUSSET IAW EMB SRM 51-40-02 AND 51-20-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 35,861 hrs · 30,138 cycles

LT WING, RIB 5 CRACKED. R & R RIB IAW AEA EO EM-57-MR-594, R1 PART A.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 35,866 hrs · 30,143 cycles

DURING B INSPECTION FOUND THE GALLEY RIGHT AFT BEAM GUSSET HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT BEAM GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — MISSING (CABIN) · airframe 35,866 hrs · 30,143 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT FLOOR STRIP CONNECTIONS AT 12BC MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED SERVICEABLE CONNECTORS ON THE EMERGENCY LIGHT FLOOR STRIP AT 12BC IAW EMB-145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,758 hrs · 30,059 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT LENS BUSTED OUT AND LAMP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EMERGENY LIGHT ASSEMBLY IAW EMB AMM 33-50-09. THE OPERATIONAL CHECK WAS GOOD IAW EMB 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,464 hrs · 29,050 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IN THE SERVICE DOOR EMERGENCY LIGHT IAW EMB AMM TASKS 33-50-09-000-801-A AND 33-50-09-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,464 hrs · 29,050 cycles

DURING B INSPECTION FOUND THE 4TH FROM FRONT CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT LAMP IAW EMB AMM TASKS 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: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 34,128 hrs · 28,807 cycles

ON FLIGHT 4103, THE CREW REPORTED THAT DURING CLIMB AND DESCENT THERE WAS AN OILY ODOR IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH ETN EM-72-034 R4 AND DETERMINED OIL SMELL IN COCKPIT TO BE EMANATING FROM THE NR 1 ENGINE. DETERMINED THAT THE NR 0 CARBON SEAL WAS FAULTY AND THE CAUSE OF THE OILY ODOR. THE NR 0 CARBON SEAL WAS REMOVED AND REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,013 hrs · 28,706 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT AT SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR MOUNTED EMERGENCY LIGHT LAMP IAW EMB 145 AMM TASKS 33-50-10-000-801-A & 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,887 hrs · 28,607 cycles

DURING B INSPECTIONS FOUND THE FIRST EMERGENCY FLOOR PATH LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY FLOOR LIGHT STRIP IAW EMB 145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (MLG) · airframe 33,854 hrs · 28,580 cycles

ON FLIGHT 4333, THE CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION THEY HEARD AN UNUSUAL NOISE AND RECEIVED A CONTINUOUS LEFT MAIN GEAR IN TRANSIT INDICATION ON EICAS. THE CREW DECLARED AN EMERGENCY, COMPLETED AOM VOL 1 CHECKLIST AND RETURNED TO JFK. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PROXIMITY SWITCH IAW EMB-145 AMM 32-61-01. THE OPERATIONAL CHECK PER 32-63-05 WAS GOOD, NO DEFECT NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MOUNT — DAMAGED (RT ENGINE) · airframe 33,764 hrs · 28,517 cycles

DURING B INSPECTION, FOUND THE RIGHT ENGINE FORWARD LOWER MOUNT OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT ENGINE FORWARD LOWER MOUNT IAW AMM 71-20-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,764 hrs · 28,517 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT IN CEILING AT ROW 12 IS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP IN CEILING AT ROW 12 IAW AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: MOUNT — DAMAGED (RT ENGINE) · airframe 33,764 hrs · 28,517 cycles

DURING B INSPECTION, FOUND THE RIGHT ENGINE FORWARD UPPER MOUNT OUT OF LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT ENGINE FORWARD UPPER MOUNT IAW AMM 71-20-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,497 hrs · 28,312 cycles

DURING B-INSPECTION FOUND THE AFT CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT IN REFERENCE WITH AMM TASK 30-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,301 hrs · 28,121 cycles

ON FLIGHT 2786 THE CREW REPORTED THAT BOTH CABIN FLASHLIGHTS ARE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD CABIN FLASHLIGHT AND CHECK OK IAW MM 33-51-01. THE REAR FLASHLIGHT’S OPERATIONAL CHECK WAS GOOD. THE OPERATIONAL CHECK WAS GOOD FOR BOTH. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,199 hrs · 28,022 cycles

DURING MAINTENANCE INPSPECTION FOUND THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERABLE. PART WAS PLACED ON MEL. REMOVED AND REPLACED SERVICE DOOR EXTERNAL EMERGENCY LIGHT SOCKET. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-10. MEL 33-29. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,035 hrs · 27,903 cycles

DURING B-INSPECTION FOUND THE EMERGENCY CEILING AISLE LAMP INOPERABLE AT ROW 16. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 33,006 hrs · 27,880 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LIGHTS INOPERABLEAT ROW 10 A. THE AIRCRAFT WAS REMOVED FROM SERVICE. SOLDERING WIRES AT EMERGENCY LIGHT STRIP IAW AWM STD PRACT 20-30-00. THE OPERATIONAL TEST CHECK WAS GOOD IAW W/C 33-700-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 32,939 hrs · 27,829 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY AISLE FLOOR EMERGENCY FLOOR LIGHT STRIP HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 MM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — LEAKING (BLEED AIR SYS) · airframe 32,926 hrs · 27,817 cycles

ON FLIGHT 4318 THE CREW REPORTED THAT ON TAKEOFF THEY RECEIVED A BLEED NR 1 LEAK MESSAGE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED O-RINGS AND SLEEVES AT JOINT 17 IN CARGO COMP AS PER ETN-EM-36-048 IAW EMB-145 AMM 36-11-09. LEAK CHECK GOOD. ALSO REMOVED AND REPLACED THE BLEED NR 1 T TUBE ASSEMBLY AT JOINT 19 IAW EMB-145 AMM 36-11-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 32,841 hrs · 27,753 cycles

DURING MAINTENANCE INSPECTION FOUND THE LAST AFT FLOOR PROXIMITY LIGHT STRIP BROKEN ON REMOVAL TO FOM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP AS REQUIRED IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,646 hrs · 27,596 cycles

DURING MAINTENACE VIST FOUND THE EMERGENCY LIGHTS LEFT ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY NR 2, 3 & 4 IAW EMB-145 AMM 33-50-04. SERIAL NUMBERS: 96216, 109815, 85163. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,646 hrs · 27,596 cycles

DURING MAINTENACE VISIT FOUND THE EMERGENCY LIGHT LEFT ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGECNY POWER SUPPLY UNIT BATTERY NR 1 IAW EMB-145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR SEAL — OBSTRUCTED (EMERGENCY EXIT) · airframe 32,494 hrs · 27,470 cycles

ON FLIGHT 3931 THE CREW REPORTED THE EMERGECNY EXIT WINDOW-B/C (RT) SIDE WHISTLES IN FLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CONDUCTED A GENERAL VISUIAL INSPECTION OF THE RIGHT OVERWING EMERGENCY EXIT DOOR SEAL FOUND TAPE UNDER SEAL, REMOVED TAPE IAW STANDARD MAINTENANCE PRACTICES. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,231 hrs · 26,475 cycles

FOR FLIGHT 2773 DURING THE PREFLIGHT INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-09 STEPS 1-3. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SLEEVE — DEFECTIVE (TEMP CONTROL) · airframe 31,133 hrs · 26,409 cycles

ON FLIGHT 4088 THE CREW REPORTED THAT AT TAKEOFF AT 500 AGL, RECEIVED A BLEED 2 LEAK INDICATION ON EICAS. PERFORMED EPC CHECKLIST AND THE CAPTAIN DECLARED AN EMERGENCY. THE BLEED LEAK MESSAGE EXITING WHEN DESELECTED BLEED 2 VALVE. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SLEEVE ON THE DUEL TEMPERATURE CONTROL VALVE IAW EMB 145 AMM 21-60-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: O-RING — DEFECTIVE (BLEED AIR SYS) · airframe 30,000 hrs · 25,587 cycles

ON FLIGHT 3633 AFTER TAKEOFF THE CREW REPORTED A NUMBER 1 BLEED LEAK AT FLIGHT LEVEL 50 FOR APPROXIMATELY 3 TO 4 MINUTES. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED PNEUMATIC ENERGY THOUGHT ONE OF THE ENGINES IAW EMB 145 MM 36-00-00-808-801. THE OPERATIONAL CHECK WAS GOOD, NO LEAKS FOUND AT THIS TIME. REMOVED AND REPLACED O-RINGS AND COUPLING NR 23 AND NR 28 IAW AMM 36-11-10. REMOVED AND REPLACED TUBE ASSEMBLY IPC 36-17-00 FIG 20 ITEM 260 IAW EMB WORKCARD 36-11-10. REMOVED AND REPLACED COOPER GASKET ON APU BLEED CHECK VALVE IAW EMB 145 AMM 36-12-02. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 36-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 29,811 hrs · 25,423 cycles

ON FLIGHT 3655 THE FLIGHT ATTENDANT REPORTED SOME OF THE EMERGENCY LIGHTS ON IN CABIN ON PREFLIGHT. ALSO THE CREW REPORTED EMERGENCY LIGHTS WERE OFF IN COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND RELACED THE NR 3 AND NR 4 CHARGER AND BATTERY POWER SUPPLY IAW WC 33-700-19. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL LEVER — MALFUNCTIONED (MLG) · airframe 29,161 hrs · 24,908 cycles

ON FLIGHT 3932 GEAR RETRACTS NORMALLY AFTER T/O THEN 5 MIN LATER LOUD THUMP WAS FELT AND HEARD IN COCKPIT AND CABIN, A/C THEN PITCH UP ON AUTOPILOT. HYD PAGE INDICATES APPROPRIATE QTY AND PRESS BUT LEFT INBOARD BRAKE TEMP FLUCTUATING ERRATIC FULL SCALE. TWENTY MINUTES LATER BURNING RUBBER SMELL NOTED IN CABIN BY F/A. GEAR EXTENDED NORMALLY AND NORMAL LANDING. EMERGENCY WAS DECLARED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 32-52-02. REMOVED AND REPLACED LT INBOARD BRK TEMP IAW AMM 32-47-01 P/N 0132AFU-2 S/N H0382. REMOVED AND REPLACED SIDEWALL LIGHT HARNESS AT SEAT 1A IAW AMM 33-31-06, P/N 7287502-609. C/W FUNCTIONAL CHECK OF AUTO-PILOT SYS IAW AMM 22-11-00-700-803-A AND HORZ -STAB ELECTRONIC TEST IAW AMM 27-40-00-700-802-A. ALL OPS CHECKED GOOD. THE A/C RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (FLASHLIGHT) · airframe 28,891 hrs · 24,699 cycles

DURING PS-2 MAINTENANCE CHECK FOUND THE AFT EMERGENCY FLASHLIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 FLASHLIGHT AND CHARGER IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — DEFECTIVE (COCKPIT) · airframe 28,222 hrs · 24,129 cycles

ON FLIGHT 3905 DURING THE CLIMBOUT THE CREW REPORTED THAT THE PRIMARY FLIGHT DISPLAY ILLUMINATED AT 260 FEET AND THE PRIMARY FLIGHT DISPLAY 1 LOST POWER. THE CREW ALSO REPORTED, DETECTED SMOKE AND FUMES. THE CREW ELECTED TO RETURN TO PIT AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED THE PRIMARY FLIGHT DISPLAY NR 1 AND INSTALLED A SERVICEABLE UNIT AND SWAPPED THE MULTIFUNCTION DISPLAY 2 BACK TO THE ORIGINAL POSITION IAW EMB-145 AMM 34-22-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,781 hrs · 22,861 cycles

DURING PS-2 INSPECTION, FOUND LARGE EMERGENCY LIGHT EXIT MARKING SIGN ON THE RIGHT SIDE EMERGENCY EXIT HAD FAILED TO ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER IAW EMB 145 AMM 33-50-11. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COMPUTER — FAILED (NR 2) · airframe 26,758 hrs · 22,832 cycles

ON FLIGHT 4292 AT 20,000 FEET, THE CREW REPORTED A MASTER CAUTION IC BUS BAR FAILED. THE CREW SMELLED FUMES OF BURNING ELECTRONICS. THE FIRST OFFICER’S PRIMARY FLIGHT DISPLAY AND THE MULTI-FUNCTION DISPLAY FAILED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 2 IC 600 IAW EMB AMM 31-42-01. PERFORMED OPERATIONAL CHECK IAW EMB AMM 31-42-00 OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 26,306 hrs · 22,400 cycles

ON CONFORMITY CHECK, MAINTENANCE FOUND RIGHT OVERAWING EMERGENCY EXIT LIGHT INOPERATIVE. FOUND CONNECTOR TO BE LOOSE, TIGHTENED CONNECTOR IAW EMB 145 WM 20-50-00. REMOVED AND REPLACED BULB IAW EMB AMM 33-50-10. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — BENT (RT ELEVATOR) · airframe 26,306 hrs · 22,400 cycles

DURING IMBV INSPECTION, THE RIGHT ELEVATOR LOWER SKIN WAS FOUND BENT AT THE FAIL/SAFE ROD CUT OUT. PERFORMED A 2.25 INCH BY 1.5 INCH. CUT OUT TO REMOVE THE DAMAGE. FABRICATED A 8.625 INCH BY 6.5625 INCH DOUBLER. CLEANED, ALODINED, PRIMED AND INSTALLED DOUBLER IAW EMB SRM 55-20-01. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FR20) · corrosion level 2 · airframe 26,306 hrs · 22,400 cycles

DURING IMBV INSPECTION THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A 16.3 INCH BY 2.9 INCH CUT OUT TO REMOVE THE DAMAGE. FABRICATED A 19.3 INCH BY 3.6 INCH DOUBLER FROM EPNEM53-EP54701, A 16.2 INCH BY 3.0 INCH FILLER FROM EPNEM53-EP54703 AND TWO SHIMS FROM AL2024T3 0.090 INCH ONE 6.2 INCH BY 1.1 INCH AND THE OTHER 7.5 INCH BY 1.1 INCH. CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10 FIGURE 202. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,306 hrs · 22,400 cycles

DURING IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 32 WAS FOUND CORRODED. PERFORMED A 4.8 INCH BY 2.6 INCH. CUT OUT TO REMOVE THE DAMAGE. FABRICATED A 17.3 INCH BY 3.6 INCH DOUBLER, A 13.5 INCH BY 1.6 INCH FILLER AND TWO SHIMS AND THE OTHER 5.6 INCH BY 1.1 INCH. CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-00-10 FIGURE 202. AIRCRAFT RETURNED TO SERVICE.