N632AE

Part: LINE — CRACKED (ENGINE BLEED) · airframe 48,109 hrs · 45,469 cycles

DURING FLIGHT. E2 A/I FAIL MESSAGE APPEARED. FOLLOWED QRH AND MESSAGE REMAINED. T/S IN REF TO FIM 30-11-00-810-801-A. INSPECTED ENG BLEED DUCTS ON #2 ENGINE. FOUND CRAK ON Y-PIPE BETWEEN ENGINE A/I VALVE AND HIGH STAGE VALVE. R&R'D ENG BLEED Y-PIPE IAW AMM 30-21-05-04. OPS CK GOOD. NO MESSAGES ON EICAS OR CMC. CLEAR MEL 30-7-1.

Part: LINE — CRACKED (ENG BLEED) · airframe 48,098 hrs · 45,457 cycles

DURING FLIGHT WING A/I FAIL MESSAGE APPEARED. FOLLOWED QRH AND MESSAGE REMAINED. HA300 FACTED OUT AS - T/S IN REF TO FIM 30-11-00-810-801-A. INSPECTED ENG BLEED DUCTS ON #2 ENGINE. FOUND CRACK ON Y-PIPE BETWEEN ENGINE A/I VALVE AND HIGH STAGE VALVE. R&R'D ENG BLEED Y-PIPE IAW AMM 30-21-05-04. OPS CK GOOD. NO MESSAGES ON EICAS OR CMC.

Part: WARNING MESSAGE — FALSE ACTIVATION (CONFIGURATION) · airframe 48,005 hrs · 45,342 cycles

PDIS 632 27-36 2379001 01JUN21 EVV CLOSE SPS 1-2 INOP, SPS ADANCE, NO TAKEOFF CONFIG DURING TAKEOFF MESSAGES CLEARED WHEN A/C STOPPING. FACT 01JUN21 10:52 EVV PERFORMED SPS OPS CHECK IAW AMM 27-36-00-700-801-A. OPS CHECK GOOD. NO SPS MSGS DISPLAYED ON EICAS, A/C OK FOR SERVICE AT THIS TIME.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (NR 2 ENGINE) · airframe 47,978 hrs · 45,310 cycles

DURING CLIMB AT 14000 FEET EICAS E2 A/ICE FAIL PRESENTED. RAN QRH MSG WAS INTERMITTENT WITH OVERRIDE KNOB SELECTED TO ALL. ENG AIR INLET 2 OPEN INSCRIPTION WAS ALSO INTERMITTENT. ENG A/ICE OVER PRESS EICAS ALSO PRESENTED. PERFORMED HIGH STAGE PRESSURE SWITCH FUNCTIONAL TEST AMM 36-11-07-700-801-A NO DEFECTS NOTED. R&R RELAYS K0112,K0527 &K0535 AS A MAINTENANCE PRECAUTION IN REF TO AMM 20-13-02-000/400-801-A. REMOVED ENGINE 2 A/I DUCT IN REF TO AMM TASK 30-21-05-000-801-A TO FOM AND REMOVED ENGINE 2 PRESSURE TRANSDUCER AND MANIFOLD IN REF TO AMM TASK A30-21- 06-000-801-A. PERFORMED BOROSCOPE ON PICOLLO TUBE NO DAMAGE FOUND. REINSTALLED #200 ENGINE A/I DUCT IN REF TO AMM TASK 30-21-05-400-801-A AND REINSTALLED #200 ENGINE PRESSURE TRANSDUCER AND MANIFOLD IN RE TO AMM TASK 30-21-06-400-801-A. R&R A/I CONTROL PANEL IN REF TO AMM20-13-01-000/400-801-A. PERFORMED ANTI-ICING SYSTEM OPS CHECK IN REF TO 30-00-00-700-802-A OPS CHECK GOOD.PERFORMED ENGINE ANTI ICING VALVE OPERATIONAL TEST IN REF TO AMM TASK 30-21-00-700-804-A. OPS CHECK GOOD. PERFORMED ENGINE THERMAL ANTI ICING SYSTEM OPS CHECK IN REF TO AMM TASK 30-21-00-700-803-A. OPS CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 47,674 hrs · 44,972 cycles

NDIS 632 27-00 0029100 24MAR21 PHF CLOSE FOR MIR PURPOSE: PILOT DID ABORTED TAKE OFF WHEN HE NOTED A POSSIBLE SPOILER DEPLOYMENT WITH FAIL MESSAGE.DIRECTED CA TO DO CONFIG TEST WITH TRIM INDICATION SHOWING. HAD HIM RECONFIG A/C AND DO TEST AGAIN WITH PASSING. NO HISTORY NOTED. SECOND TAKEOFF OK FACT 24MAR21 12:02 PHF FOR MIR PURPOSE ONLY

Part: SOLENOID VALVE — MALFUNCTIONED (NLG DOORS) · airframe 47,440 hrs · 44,724 cycles

AROUND 8000 FT NLG DOOR OPENED UNCOMMANDED. FOUND NLG DOOR NOT CLOSING WITH GEAR UP. T/S IN REF TO EMB145 FIM 32-32-00. R & R NLG DOOR SOLENOID VALVE, REF EMB145 AMM 32-33-02-04. PERFORMED EXTENSION/RETRACTION TEST, REF EMB145 AMM 32-30-00. OPERATIONS CHECK GOOD, NO LEAKS FOUND. OK FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (NR 2 ENGINE) · airframe 47,415 hrs · 44,701 cycles

E2 ANTI ICE FAIL AT 60 KNOTS ON TAKEOFF ROLL *NOTE* PASSED GROUND PNEUMATIC TEST, MESSAGE EXTINGUISHED WHEN THRUST LEVER RETURNED TO IDLE. REINSTALLED ORIGINAL A/ICE VALVE FOR E2, PER EMB 145 AMM 30-21-01. R & R E2 PRESSURE TRANSDUCER, PER EMB 145 AMM 30-21-06. OPERATIONS CHECKED, PER EMB 145 AMM 30-00-00. OPERATIONS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 46,813 hrs · 44,029 cycles

SMOKE IN CABIN OBSERVED. CLEARED UP WITH PACK 1 ON. SMOKE PERSISTED WITH PACK 2 ON. CREW NOTICED PACK 2 MAKING NOISE. R&R'D RT ACM IAW AMM 21-51-03-04. RAN PACK 2 WITH APU AND ENGINE BLEED. NO SMOKE OR OTHER DEFECTS NOTED AT THIS TIME. CLEAR MEL 21-13-1. NO BROKEN FAN BLADES NOTED ON REMOVED ACM.

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER) · airframe 45,859 hrs · 42,959 cycles

PDIS 632 29-10 1948251 06SEP19 CLT CLOSE RUDDER SYS 1/2 INOP MSG IN FLIGHT WEITH HYD SYSTEM 1 FAIL MSG INTERMITTENT. 27717 00 RNR HISTORY: NONE FACT 06SEP19 17:23 CLT R&R RUDDER PRESSURE SWITCH PER AMM 27-23-04 OPS + LEAK CHECK GOOD. OK FOR SERVICE.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 44,639 hrs · 41,566 cycles

PDIS 632 36-10 1856433 22JAN19 PHL CLOSE HS VLV 2 FAIL EICAS MSG DURING TAKE OFF ROLL HISTORY: FACT 22JAN19 20:17 PHL TROUBLESHOT WITH FIM 36-11-00-810-810-A UP TO BLOCK 7. R&R'D NR 2 HIGH STAGE VALVE IAW AMM 36-11-02. OPS CHECK GOOD. OKAY FOR SERVICE.

Part: CONNECTOR — DIRTY (FLASHLIGHT) · airframe 43,890 hrs · 40,710 cycles

PILOT'S EMERGENCY FLASHLIGHT WILL NOT ILLUMINATE. TRIED BATTERY, NO FIX. BATTERY BACK TO ORIGINAL. CLEANED AND RESEATED CONNECTORS IN REF TO SWPM 20-50-00, GOOD FIX. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 43,788 hrs · 40,576 cycles

EXAUST FUMES WERE DETECTED IN THE COCKPIT AFTER ENGINE START USING THE APU. APU EGT GOES TO AMBER DURING ENGINE START. EGT FLUCTUATES IN HIGH 600S WITH NO EICAS MESSAGE. RAN APU AND ENGINES FOR 30 MINUTES, NO EXHAUST FUMES OR OTHER DEFECTS NOTED. APU EGT REMAINED WITHIN ALLOWABLE PARAMETERS. OK FOR SERVICE.

Part: WIRE — BROKEN (START SYSTEM) · airframe 43,653 hrs · 40,427 cycles

NR 2 ENGINE FAILED TO START. NO ROTATION. ON APU BLEED. FOUND BROKEN WIRES ON PINS 10 AND 39 ON PNEUMATIC CONTROL PANEL CONNECTOR P7128. REPAIRED WIRES IAW SWPM. PERFORMED ENGINE CROSS START AND AIR BLEED CHECK IN REF TO AMM 36-00-00-200-803-A/500. OPS CHECK GOOD. OK FOR SERVICE.

Part: CONTROLLER — FAILED (WINDSHIELD HEAT) · airframe 42,026 hrs · 38,675 cycles

NR 1 WINDSHIELD HEAT FAIL EICAS MESSAGE DURING ICING CONDITIONS. CREW COMPLIED WITH QRH. DID NOT ATTEMPT TO REACTIVATE THE SYSTEM. R & R THE NR 1 WINDSHIELD TEMP CONTROLLER IAW AMM 30-42-01. OPS CHECKED GOOD. OK FOR SERVICE. CHECKED RESISTANCE OF WINDSHIELD TEMP SENSORS AND CONTINUITY OF HARNESS BETWEEN SENSORS AND CONTROLLER. NO DEFECTS NOTED.

Part: RELAY — FAILED (ZONE 100) · airframe 42,024 hrs · 38,673 cycles

DURING INSPECTION OF RELAY E FAIL STEP-11 IAW FCD1-30-16-0276. FOUND DAMAGE/BURNT PINS ON PITOT STATIC NR 3. RELAY K0058 PIN C2, RELAY SOCKET/BASE XK0058 PIN C2 AND CHARRED WIRE. BOTH RELAY K0058, RELAY SOCKET XK0058 AND PINS WERE R & R.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,021 hrs · 38,672 cycles

AREA EMERGENCY LIGHT ON GALLEY DOOR HINGE INTERMITTENT. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT ASSY IAW AMM 33-50-10. OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 41,958 hrs · 38,606 cycles

FA REPORTED MAIN CABIN DOOR HARD TO OPERATE. LUBRICATED THE MAIN DOOR FRAME ROLLERS IAW ETN-EN-52-061.

Part: LAMP — NOT SEATED (EMERGENCY LIGHT) · airframe 41,659 hrs · 38,310 cycles

SERVICE DOOR GROUND ILLUMINATION EMERGENCY LIGHT INOPERATIVE. RESEATED THE LAMP IAW AMM 33-50-09. OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 41,525 hrs · 38,190 cycles

PASSENGER DOOR WOULD NOT OPEN INSIDE OR OUTSIDE. CLEAN AND LUBED MAIN DOOR ROLLERS IAW AMM 52-21-01. OPS CHECKED GOOD.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,120 hrs · 37,824 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT PANEL ASSEMBLY IAW AMM 25-23-04. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,120 hrs · 37,824 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-09. OP CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (EXTERNAL) · airframe 41,085 hrs · 37,799 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-10-000-801, AND 33-50-10-400-801. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,063 hrs · 37,781 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP 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: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 41,063 hrs · 37,781 cycles

FWD CABIN EMERGENCY FLASHLIGHT CRADLE BROKEN. REMOVED AND REPLACED FWD FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A, AND 33-50-16-400-801-A OPS CHECKED GOOD.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 40,842 hrs · 37,574 cycles

AIRCREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN FROM THE OUTSIDE HANDLE. ADJUSTED THE DOOR IAW ETN EM-52-013R1.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 40,822 hrs · 37,557 cycles

MAIN CABIN DOOR VERY HARD TO GET OPEN WHEN HANDLE FULL UP. COMPLIED WITH PAX DOOR INSPECTION IAW AMM 52-11-00 LUBE AS REQUIRED CHECK GOOD OK FOR SERVICE

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 40,742 hrs · 37,496 cycles

FA REPORTS MAIN DOOR DIFFICULT TO OPEN. LUBRICATED MAIN DOOR FRAME ROLLER IAW AMM 53-21-02. OPS CHECKED GOOD.

Part: CLAMP — UNSECURE (NR 1 ENGINE) · airframe 40,730 hrs · 37,484 cycles

DURING CLIMB, CREW RECEIVED NR 1ENGINE BLEED LEAK MESSAGE. CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT INCIDENT. PERFORMED LEAK CHECK BLEED 1 SYSTEM JOINT NO LEAKS FOUND. DURING INSPECTION FOUND BLEED 1 PRECOOLER V CLAMP LEAKING. SECURED THE CLAMP IAW AMM 20-10-10. OPS AND LEAK CHECKED SATISFACTORY IAW AMM 36-00-00.

Part: SLEEVE — BLOWN (A/C PACK DUCT) · airframe 40,730 hrs · 37,484 cycles

NR 1 BLEED LEAK AFTER TAKE OFF, RAN CHECKLISTS AND BLEED LEAK INDICATION WENT OUT AFTER ABOUT 5 MINUTES. INSPECTED AND FOUND THE NR 1 PACK DUCTING SLEEVE TO BE BLOWN. REMOVED AND REPLACED THE SLEEVE IAW AMM 21-51-00. OPS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 40,678 hrs · 37,443 cycles

FWD FLASHLIGHT CRADLE BROKEN. REMOVED AND REPLACED THE FLASHLIGHT CRADLE ASSEMBLY. OPS CHECKED GOOD IAW AMM 33-50-16.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 40,437 hrs · 37,213 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN. LUBRICATED THE MAIN DOOR ROLLERS, OPS CHECKED GOOD IAW AMM 52-18-00-820-801-A.

Part: ROLLER — LACK OF LUBE (DOR FRAME) · airframe 40,389 hrs · 37,176 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN. LUBRICATE MAIN CABIN DOOR'S FRAME ROLLERS AND OPC, GOOD. REFER TO AMM 53-21-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (TAKEOFF CONFIG) · airframe 40,320 hrs · 37,110 cycles

TAKEOFF CONFIGURATION TRIM WARNING AT 100KTS. ABORTED TAKEOFF. PERFORMED OPS CHECK IAW AMM 27-40-00 OPS CHECKED GOOD. PERFORMED HIGHSPEED TAXI WITH CREW TAXI CHECKED GOOD. AIRCRAFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,144 hrs · 36,949 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R MAIN CABIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC GOOD AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,021 hrs · 36,821 cycles

RH INTERIOR CEILING MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RT INTERIOR CEILING MOUNTED EMERGENCY EXIT LIGHT BULB IAW AMM 33-50-08 OPS CHECK GOOD

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 40,006 hrs · 36,806 cycles

FA REPORTED MAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE. LUBRICATED THE ROLLERS ON FUSELAGE FRAME FOR MAIN CABIN DOOR IAW AMM 52-00-00. OPS CHECKED GOOD.

Part: DOOR SEAL — DIRTY (CABIN DOOR) · airframe 39,955 hrs · 36,758 cycles

F/A REPORTS MAIN ENTRANCE DOOR IS VERY HARD TO OPEN. CLEANED SEAL AND PERFORMED OPS CHECK OF MAIN CABIN DOOR IAW AMM 52-10-01, OPS CHECK GOOD.

Part: DOOR FRAME — DIRTY (FUSELAGE) · airframe 39,609 hrs · 36,421 cycles

MAIN DOOR DIFFICULT TO OPEN. CLEANED DEBRIS OUT OF DOOR FRAME IAW AMM 53-21-02. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,385 hrs · 36,223 cycles

NUMBER 3 EMER LIGHT BATTERY PACK NEEDS REPLACEMENT INOPERATIVE. R & R NR 3 EMER LIGHTING BATTERY PACK IAW AMM 33-50-04. TESTED SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,347 hrs · 36,182 cycles

MAIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: BULB — INOPERATIVE (FLASHLIGHT) · airframe 39,297 hrs · 36,140 cycles

CAPTAINS FLASHLIGHT INOPERATIVE. R & R CAPTAIN`S FLASHLIGHT BULB. OPS CHECKED GOOD IAW AMM 33-51-01.

Part: CONTACTOR — DEFECTIVE (APU) · airframe 39,273 hrs · 36,120 cycles

AT GATE PRIOR TO DEPARTURE, PUNGENT ACRID ODOR, SUGGESTIVE OF ELEC FIRE FILLED FLIGHT DECK. APU RUNNING, NO GND POWER, INSPECTED ACFT THERMALLY, NO SIGNIFICANT HOT SPOTS DETECTED INTERNAL OR EXTERNAL. SEE PRIOR WRITE UP FOR SMOKE PG 3998956 1. REF AML PAGE 3998982 ITEMS 1 -3. SHORTLY AFTER SMELL WAS REPORTED APU SHUTDOWN & WOULD NOT START. FOUND BATT BUS 2 FUSE F0140 BLOWN. REF LOG PAGE 3998985 ITEM 2, AMM 24-34-02, NO FIX, PAGE 3998982 2. R & R APU STARTER & GEN IAW AMM 24-34-01. OPERATIONS CHECKED GOOD. TROUBLE SHOT IAW FIM 24-36-00-810-802A. R & R APU START CONTACTOR IAW WM 24-36-50, APU OPERATIONS CHECKED GOOD IAW AMM 49-13-00, NO FAULTS. OK FOR SERVICE.

Part: SWITCH — FAILED (AC BAY) · airframe 39,217 hrs · 36,062 cycles

IN LEVEL CRUSE AT FL 250, FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN WITH SOME ORDER IN THE COCKPIT. DID NOT LOCATE THE SOURCE, SUBSIDED AFTER A FEW MINUTES, DIVERTED. INSPECTED ACFT & PERFORMED ETN-EM-72-034. FOUND PACK 1 TO BE INOPERATIVE WITH PNEUMATIC SOURCE. DEFERRED IAW MEL 21-27, CONFIRMED PACK 2 OVLD. R & R PACK 2 PACK OVER TEMPERATURE SWITCH IAW AMM 21-51-08. PERFORMED OPERATIONS CHECK IAW AMM 21-20-00. OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME. MEL ITEM RESTORED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,133 hrs · 35,976 cycles

DURING MBV INSPECTION, QA FOUND 2 CRACKS ON RT REAR FUSELAGE I SKIN AT FRAME 75, BELOW STRINGER 2R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON CRACKS IAW ERS-EM-53MR-1898. REPAIR MATERIAL, DOUBLER 2024-T3, 0.080, FILLER 2024-T3, 0.063, ANGLE 2024-T3, 0.050, SHIM 2024-T3-0.032.

Part: PROFILE — CORRODED (PAX DOOR) · airframe 39,133 hrs · 35,976 cycles

DURING MBV INSPECTION, QA FOUND CORROSION AROUND PAX DOOR LINER, 6TH FROM TOP AFT SIDE NUTPLATE HOLE. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIRED CORROSION AROUND PAX DOOR LINER 6TH FROM TOP AFT SIDE NUT PLATE HOLE IAW ERS-EM-53MR-1890. ACFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION.

Part: YOKE — CRACKED (LT ENGINE) · airframe 39,133 hrs · 35,976 cycles

DURING MBV INSPECTION, FOUND LT PYLON LOWER FWD ENG MOUNT SUPPORT YOKE CRACKED. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. R & R LT PYLON LOWER FWD ENG MOUNT SUPPORT YOKE IAW EO EM-54MR-386.

Part: WIRE — BROKEN (CABIN) · airframe 39,133 hrs · 35,976 cycles

EMERGENCY LIGHT ON CEILING PANEL 253CLC HAS A BROKEN WIRE. REPAIRED 2 CUT WIRES IAW SWPM 20-21-00. FOR OPERATIONS CHECK SEE BOW 208622.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,133 hrs · 35,976 cycles

RIGHT AFT FUSELAGE FRAME 75, BELOW STRINGER 2 SKIN CRACKED AT FASTENER MARKED, SETTINGS 400KHZ 135 V-65.0 H-75.0 FILTER LO 100. CRACKED FUSELAGE SKIN AT FRAME 75, STRINGER 2R AREA WILL BE CUT OUT & REPAIRED WITH FILLER & DOUBLER, SEE NRTC E487295 FOR ACCOMPLISHMENT OF REPAIR.

Part: WIRE — BROKEN (CABIN) · airframe 39,133 hrs · 35,976 cycles

PROXIMITY LIGHT 2 EACH WITH ARROWS, 1 EACH OVERWING EXIT & 1 EACH WITHOUT ARROWS HAVE BROKEN WIRES. R & R PROXIMITY LIGHTS IAW AMM 33-50-12. SEE NRTC BOW 208622 FOR FINAL INSTALL & OPERATIONS CHECKS.

Part: WIRE — BROKEN (CABIN) · airframe 39,133 hrs · 35,976 cycles

EMERGENCY EXIT LIGHT ON CEILING PANEL 233BLC HAS A BROKEN WIRE. REPAIRED CUT WIRE IAW SWPM 20-21-00. FOR OPERATIONS CHECK SEE BOW 208622.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 38,852 hrs · 35,737 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR UPPER CTR SKIN. R & R SKIN IAW SRM 51-20-01, 51-40-02, 51-20-03, 51-40-06, 55-20-01, ETN-EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,852 hrs · 35,737 cycles

HAIL DAMAGE EVENT. REPLACE LT CTR FUSELAGE 1 SKIN. R & R LT CTR FUSELAGE I UPPER SKIN IAW SRM 51-40-02, 53-21-01-SI, 51-20-01, 51-20-03, 51-40-06, ETN-EM-51-118, ETN-EM-53-262 & ERS EM-5300-1759.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 38,852 hrs · 35,737 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR INBD LE. R & R LT ELEVATOR INBD LE SKIN IAW SRM 51-20-01, 51-40-02, 51-20-03, 51-40-06, 55-20-01, ETN-EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 38,852 hrs · 35,737 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR MID SKIN TIP. R & R LT ELEVATOR MID SKIN TIP IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 55-20-01, ETN-EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 38,852 hrs · 35,737 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR UPPER CTR SKIN. R & R RT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02, 55-20-01, 51-20-01, 51-20-03, 51-40-06, ETN-ETM-EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 38,852 hrs · 35,737 cycles

HAIL DAMAGE EVENT. REPLACE LT STABILIZER UPPER SKIN. R & R LT HORIZONTAL STABILIZER UPPER SKIN IAW SRM 51-40-02, 55-10-01-SI, 51-20-01, 51-20-03, 51-40-06 & ETN EM-55-073R2

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 38,852 hrs · 35,737 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR MID SKIN TIP. R & R RT ELEVATOR MID SKIN IAW SRM 51-40-02, 55-20-01, 51-20-01, 51-20-03, 51-40-06 & ETN-ETM-EM-55-073R2 & ETN-EM-55-076.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 38,852 hrs · 35,737 cycles

HAIL DAMAGE EVENT. REPLACED RT STAB SKIN. R & R RT STAB UPPER SKIN IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 55-10-01SI & ETN EM-55-073R2 & ENT EM-55-074.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZ STAB) · airframe 38,442 hrs · 35,348 cycles

ON APPROACH ABOUT 700 FT OR SO, PTRIM MAIN INOPERATIVE. MASTER WARNING, DECLARED EMER & PERFORMED GO AROUND. RAN PRIMARY PITCH TRIM FAILURE CHECKLIST IN AOM -1. PERFORMED HORIZONTAL STAB OPERATIONAL TEST IAW AMM 27-40-00. RESET OF SYS & OPERATIONS CHECKED OK. ACFT OK FOR SERVICE.

Part: ACM — FAILED (AC BAY) · airframe 38,155 hrs · 35,084 cycles

SMOKE IN THE COCKPIT AT CRUISE, DECLARED EMER. ACCOMPLISHED FIM TASK 21-20-00-810-801, SEE LOG PAGE 3924161 ITEM 1 FOR DISCREPANCY. FOUND LT ACM NEARLY SEIZED CAUSING SMOKE IN COCKPIT. DEFERRED LT PACK INOPERATIVE. R & R ACM IAW MM 21-51-03. OPERATIONS CHECKED GOOD AT THIS TIME. MEL RESTORED.

Part: WASHER — MISSING (PAX DOOR) · airframe 38,150 hrs · 35,080 cycles

FLIGHT ATTENDANT REPORTS MAIN PAX DOOR IS HARD TO OPEN & CLOSE. TROUBLE SHOT IAW FIM 52-18-00. INSTALLED MISSING WASHER ON MAIN DOOR UPPER SUPPORT LINK ON NUT SIDE. PERFORMED MAIN DOOR LUBRICATION ON ALL INTERNAL ACTUATING & LOCKING MECHANISMS, ALSO PERFORMED PULL CHECK OF MAIN DOOR HANDLE IAW AMM 52-18-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 37,953 hrs · 34,902 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,943 hrs · 34,893 cycles

CABIN CEILING EMER AISLE LIGHT NEAR WING EXIT INOPERATIVE. R & R LAMP IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 37,880 hrs · 34,840 cycles

FORWARD FLIGHT ATTENDANT’S FLASHLIGHT INOPERATIVE. FLIGHT CREW PLACARDED IAW MEL 25-53. R & R FLIGHT ATTENDANT`S FWD FLASHLIGHT BATTERY IAW 145-EEL-08-12. OPERATIONS CHECKED GOOD. PLACARDS REMOVED & MEL RESTORED.

Part: CONNECTOR — BROKEN (CABIN) · airframe 37,409 hrs · 34,431 cycles

5TH FLOOR PROXIMITY LIGHT CONNECTOR BROKEN. REPAIRED CONNECTOR ON 5TH FLOOR PROXIMITY EMER LIGHT IAW SWPM 20-21-00 & AMM 33-50-00. OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,393 hrs · 34,418 cycles

3A FLOOR EMER LIGHT STRIP INOPERATIVE. R & R FLOOR EMER LIGHT STRIP 3A IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 37,230 hrs · 34,280 cycles

EMERGENCY LIGHT STRIP AT ROWS 5, 6 & 7A INOPERATIVE. REPAIRED EMERGENCY LIGHT CONNECTOR IAW SWPM 20-50-00. OPERATIONS CHECKED GOOD.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (WINDSHIELD) · airframe 36,963 hrs · 34,064 cycles

W/S 1 HEAT FAILED IN ICING CONDITIONS. SWAP SENSOR LEADS 3 & 4 TO 5 & 6 OF W/S 1 HEAT IAW MM 30-42-04. OPERATIONS GOOD IAW MM 30-42-0. NO W/S 1 HEAT FAIL MSG DISPLAY AT THIS TIME.

Part: FLASHLIGHT — MALFUNCTIONED (COCKPIT) · airframe 36,393 hrs · 33,514 cycles

FIRST OFFICER`S FLASHLIGHT INOPERATIVE. PERFORMED OPS CHECK OF F/O'S FLASHLIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,886 hrs · 33,037 cycles

MAIN DOOR EMER LAMP INOPERATIVE. R & R MAIN DOOR EMER LIGHT LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 35,815 hrs · 32,947 cycles

FORWARD CABIN EMER FLASHLIGHT HOLDER BROKEN. R & R FWD CABIN EMER FLASHLIGHT HOLDER IAW TASK 33-50-16-000-801-A & TASK 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 35,688 hrs · 32,813 cycles

SERVICE DOOR EXTERNAL EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EXTERNAL EMER LIGHT LAMP IAW TASK 33-50-10-000-801-A & TASK 33-50-10-400-801-A,OPERATION CHECK, NO FIX. CONFIRMED POWER IS GETTING TO ASSEMBLY THROUGH QUICK DISCONNECT WIRES. FOUND PIN PUSHED OUT AT PLUG P7198. REINSTALLED PIN IAW SWPM 20-50-0. OPERATIONS CHECKED GOOD IAW MM 33-50-00. MEL RESTORED & PLACARD REMOVED.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 35,657 hrs · 32,782 cycles

UPON ARRIVAL AT ACFT OPENED COCKPIT DOOR & NOTICED STRONG ELEC ODOR NO POWER ON ACFT. PERFORMED AMM TASK 21-20-00. AIR CONDITIONING DISTRIBUTION SMOKE & ABNORMAL SMELL IN COCKPIT, UNKNOWN SOURCE. FLIGHT ATTENDANT & CAPTAIN`S FLASHLIGHT ASSEMBLY BAD. R & R BOTH ASSEMBLIES IAW AMM 33-50-16. PN P2-07-0011-500, SN OFF 6323 & SN ON 691-3.

Part: IMPELLER — DAMAGED (NR 1 ACM) · airframe 35,573 hrs · 32,703 cycles

ELECTRICAL FUMES IN COCKPIT & CABIN DURING DESCENT. INSPECTED RECIRCULATION FANS & PERFORMED ENGINE RUNS, COULD NOT DUPLICATE ODOR. REMOVED & INSPECTED NR 1 ACM, FOUND ACM TO HAVE EXCESSIVE RESISTANCE IN IMPELLER.

Part: PRECOOLER — DAMAGED (BLEED AIR SYS) · airframe 35,554 hrs · 32,681 cycles

AFTER TAKEOFF ALT T 01 THRUST STRONG BURNING SMELL IN COCKPIT & CABIN. ALL PAXS SMELLED FROM ROW 1 ALL THE WAY TO ROW 15. TRANSFERRED TO NRWC 632-ORD-01841. R & R PRE COOLER NR 1 IAW AMM 36-11-04, OPERATIONS CHECKED GOOD. NO FURTHER ODOR OR SMOKE NOTED IAW NRWC 632-ORD-01841.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 34,895 hrs · 32,133 cycles

SERVICE DOOR EMERGENCY LAMP INOPERATIVE. R & R SERVICE DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 34,562 hrs · 31,885 cycles

MAIN DOOR WILL NOT CLOSE. LUBED MAIN PAX DOOR IAW AMM 52-18-00, OPERATIONS CHECKED GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 34,527 hrs · 31,861 cycles

NUMBER 1 FLAP FAIL CAUTION MESSAGE ON APPROACH FLAPS. CAME IN AT 0 AFTER SETTING FLAPS 9. ACFT REQUIRES INSPECTION FOR FERRY FLIGHT. THIS ACFT HAS BEEN INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLIGHT & FOUND TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT.

Part: FLAP — MALFUNCTIONED (WING) · airframe 34,518 hrs · 31,855 cycles

ON FLIGHT 3578 DURING NR 1 ON APPROACH CREW REPORTED FLAP FAIL MESSAGE ON EICAS. DECLARED EMERGENCY & RAN AOM VOL 1 PROCEDURE LANDED FLAP 0. ACFT REQUIRES INSPECTION FOR FERRY FLIGHT. ACFT HAS BEEN INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLIGHT & FOUND TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,497 hrs · 31,833 cycles

FORWARD FUSELAGE II SKIN CORROSION AT FRAME 13, STRINGER 18R - 21R. PERFORMED REPAIR IAW AEA ERS-EM-53MR-123.

Part: WIRE — DAMAGED (CABIN) · airframe 34,497 hrs · 31,833 cycles

EMERGENCY FLOOR PROXIMITY LIGHT STRIP NR 2 INOPERATIVE. REPAIRED WIRE W1928681-22 FOR EMERGENCY FLOOR PROXIMITY LIGHT STRIP NR 2 IAW 145 SWPM 20-21-00 STEP 4.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 34,497 hrs · 31,833 cycles

CRACK ON FWD AVIONIC DOOR OPENING AT FRAME 8. PERFORMED REPAIR IAW EO EM-53MR-2092.

Part: FRAME — GOUGED (FUSELAGE) · airframe 34,497 hrs · 31,833 cycles

FR 65 GOUGED ON AFT LOWER EDGE BETWEEN 2L - 3L. PERFORMED REPAIR IAW AEA ERS EM 53 MR 127.

Part: SPAR — CRACKED (RT WING) · airframe 34,497 hrs · 31,833 cycles

RIGHT SPAR 3 CRACKED AT WIRING HARNESS PASS THRU HOLE. PERFORMED REPAIR IAW AEA ERS-EM-57MR-041.

Part: CHARGER — FAILED (CABIN) · airframe 34,497 hrs · 31,833 cycles

BATTERY CHARGER ASSEMBLY FAILS CHECK. R & R BATTERY CHARGER ASSEMBLY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,497 hrs · 31,833 cycles

EMERGENCY LIGHTING SYS BATTERY CHARGER ASSEMBLIES FOR BATTERY NR 3 & BATTERY NR 4 ARE INOPERATIVE. R & R EMERGENCY LIGHTING SYS BATTERY POWER SUPPLIES & BATTERY PACKS FOR BATTERIES NR 3 & NR 4 IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 34,462 hrs · 31,803 cycles

ON FINAL APPROACH INTO AIRPORT FLAP FAIL MESSAGE ON EICAS RESULTING IN FLAPS FAILING AT 0. R & R FECU IAW EMB 145 AMM 27-53-02, OPERATIONS CHECKED GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 34,372 hrs · 31,736 cycles

DURING CRUISE, RECEIVED A CARGO SMOKE MESSAGE. COMPLIED WITH THE EPC AND DIVERTED. DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. CHECKED THE CARGO AREA FOR FIRE. NO FIRE FOUND. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED HIGH RATE AND METERING BOTTLES IAW 23-23-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,298 hrs · 31,682 cycles

SERVICE DOOR EMERGENCY EXIT IDENTIFIER INOPERATIVE. R & R DC/AC INVERTER. OPS CHECKED GOOD IAW AMM 33-50-11.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,129 hrs · 31,528 cycles

EMERGENCY LIGHTS INOPERATIVE. R & R BULBS IAW 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: ENGINE — ODOR (LEFT) · airframe 34,008 hrs · 31,444 cycles

THE CREW REPORTED THAT DURING THE TAKEOFF ROLL THE NOTICED A BURNING ODOR IN THE COCKPIT. THE CREW ABORTED THE TAKEOFF. CONFIRMED ODOR IN CABIN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LT ENGINE IAW WC 71-000-00. OPS AND LEAK CHECKED GOOD IAW MM 72-00-00 AND C/W ETN 72-034 FOR BURNING SMELL CHECKS GOOD. OPS AND LEAK CHECKED GOOD IAW MM 72-00-00 AND C/W ETN 72-034 FOR BURNING ODOR CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,004 hrs · 31,440 cycles

SERVICE DOOR UPPER EXIT LIGHT INOPERATIVE. R & R SERVICE DOOR UPPER EXIT LIGHT ASSY IAW AMM 33-50-14. OPS CHECKED GOOD IAW AMM 33-50-00-700-801-A.

Part: BATTERY — FAILED (FLASHLIGHT) · airframe 33,856 hrs · 31,299 cycles

JUST PRIOR TO OPENING MAIN DOOR. F/A WAS COMPLAING OF ELECTRICAL FUMES BETWEEN COCKPIT DOOR AND THE MAIN A/C DOOR. R & R CABIN FWD FLASHLIGHT POWER UNIT REF CMM 25-60-11 AND OPS CHECK GOOD AND NO ELECTRICAL FUMES NOTED AT THIS TIME.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,773 hrs · 31,222 cycles

NR 3 AC/DC INVERTER FOR EMERGENCY LIGHT IN GALLEY INOPERATIVE. R & R NR 3 INVERTER IAW AMM 33-50-11; OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,773 hrs · 31,222 cycles

GALLEY EMERGENCY LIGHT ON CEILING PANEL INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-50-14; OPS CHECKED BAD.

Part: STRUCTURE — CRACKED (E/E DOORWAY) · airframe 33,772 hrs · 31,222 cycles

CRACK ON FWD AVIONICS DOOR OPENING. PERFORMED DVI IAW EO-EM-53MR-2092 PTB. NO FURTHER DAMAGE NOTED.

Part: DOOR — DIRTY (CABIN) · airframe 33,244 hrs · 30,814 cycles

THE CREW REPORTED THE MAIN DOOR WAS HARD TO OPEN AND CLOSE. THE ACFT WAS REMOVED FROM SERVICE. CLEAN AND LUBED THE MAIN CABIN DOOR. THE OPS CHECK WAS GOOD IAW 52-11-00. THE ACFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,072 hrs · 30,691 cycles

DVI FWD FUSELAGE FRAME 8 LOWER AVIONIC DOOR OPENING CRACKED. PERFORM DVI FWD FUSELAGE FRAME 8 LOWER AVIONIC DOOR IAW EO EM-53MR-2092, PART B ONLY NO FUTHER DAMAGE NOTED CONTINUED ON TDMI63253083F.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,948 hrs · 30,579 cycles

DURING B INSPECTION FOUND THE GALLEY OVERHEAD EMERGENCY LIGHT WAS BURNED OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY OVERHEAD EMERGENCY LIGHT IAW EMB-145 AMM 33-50-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 32,948 hrs · 30,579 cycles

DURING B INSPECTION FOUND THE LEFT WING UPPER EMERGENCY LIGHT BURNED OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT WING UPPER EMERGENCY LIGHT IAW EMB-145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,711 hrs · 30,376 cycles

DURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (HATCH AREA) · airframe 32,436 hrs · 30,155 cycles

CHECKED RIGGING HATCH AREA AND A CRACK WAS FOUND ON FOWARD FRAME. REPAIRED IAW EO EM-53MR-2092 RI.

Part: FRAME — CRACKED (HATCH AREA) · airframe 32,426 hrs · 30,147 cycles

CHECKED RIGGING HATCH AREA AND A CRACK WAS FOUND ON FOWARD FRAME WHERE RIGGING HATCH FWD DRAW BOLTS HATCH TO 9 IN THE MIDDLE. REPAIRED IAW EO EM-53MR-2092 PT A.

Part: GENERATOR — LEAKING (NR 4) · airframe 32,313 hrs · 30,058 cycles

LEVEL IN CRUISE FLIGHT AT FL240 THEY NOTICED THE OIL PRESSURE WAS IN THE AMBER RANGE. CHECKED OIL QUANTITY AND IT WAS DOWN TO 4 QTS. A MINUTE LATER THEY GOT AN EICAS WARNING E (2) OIL LOW PRESSURE. THE CREW PERFORMED THE CHECKLIST AND WERE DIRECTED TO PERFORM A PRECAUTIONARY ENGINE SHUTDOWN. LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LEAK COMING FROM NR 4 MAIN GENERATOR. REMOVED AND REPLACED NR 4 MAIN GENERATOR AND CARBON SEAL IAW EMB 145 AMM 24-31-01 AND RR MM 72-63-10. SEAL ASSY, CARBON MAGNET FHA PART NUMBER: 42520-70. PACKING PART NUMBER M83248/1-113. THE OPERATIONAL CHECK, LEAK CHECK AND PRESSURE CHECK WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SCREW — MISSING (SERVICE DOOR) · airframe 32,151 hrs · 29,939 cycles

ON POSTFLIGHT FOR FLIGHT 3540 THE CREW REPORTED A SCREW WAS MISSING ON PANEL AFT OF EMERGENCY LIGHT ON RIGHT SIDE OF AIRCRAFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED MISSING SCREW IAW MM 52-45-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,093 hrs · 29,118 cycles

DURING B INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,053 hrs · 29,080 cycles

DURING B INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EXTERIOR EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (PITCH TRIM) · airframe 31,003 hrs · 29,049 cycles

DURING FLIGHT 3535, DURING CLIMB-OUT PITCH TRIM MAIN INOPERATIVE WARNING MESSAGE BACK UP TRIM WORKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED HSCU IAW AMM 27-40-00 ALL TESTS OK PITCH TRIM ALL TESTS OK. AIRCRAFT RETURN TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,793 hrs · 28,883 cycles

DURING B INSPECTION, FOUND THE CEILING EMERGENCY LIGHT IN THE COCKPIT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT LAMP IAW AMM 33-50-05. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,787 hrs · 28,877 cycles

DURING MAINTENANCE INSPECTION, FOUND THE PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE . AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LAMP IAW AMM 33-50-10. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 30,173 hrs · 28,402 cycles

ON FLIGHT 2914 THE CREW REPORTED THE FLIGHT ATTENDANT FLASHLIGHT NOT SNUG IN CRADLE RED LIGHT DOESN’T STAY ILLUMINATED UNLESS FLIGHT ATTENDANT PUSHES ON IT IN TURBULENCE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 30,100 hrs · 28,350 cycles

DURING B-INSPECTION FOUND THE PASSENGER DOOR SWING ARM EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR SWING ARM EMERGENCY LIGHT BULB IAW EMB AMM 33-50-06 AND IAW 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 30,085 hrs · 28,341 cycles

DURING MAINTENANCE INSPECTION FOUND THAT THE FIRST OFFICER’S FLASHLIGHT HAD BECOME VERY DIM, IT WAS NOT CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS SIDE FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 30,077 hrs · 28,336 cycles

ON FLIGHT 2878 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS WEAK - DIM OUTPUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACE BATTERY IN FIRST OFFICER’S FLASHLIGHT IAW EMB-145 MM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 29,937 hrs · 28,223 cycles

ON FLIGHT 3401, THE CREW REPORTED THE EXIT SIGN ABOVE FLIGHT ATTENDANT JUMPSEAT WAS BROKEN. AIRCRAFT REMOVED FROM SERVICE. INSTALLED SCREW IAW AMM 33-50-14. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — OBSTRUCTED (MAIN PAX) · airframe 29,896 hrs · 28,195 cycles

ON FLIGHT 2764, FLIGHT ATTENDANT REPORTED A VERY LARGE GAP ON THE MAIN CABIN DOOR. DOOR SHOWS CLOSED ON EICAS. AIRCRAFT REMOVED FROM SERVICE. INSPECTED MAIN DOOR FOUND CURTAIN BLOCKING DOOR FROM CLOSING, CLEARED & RELOCATED SAME. OPS CHECKED GOOD IAW 52-10-00. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 29,861 hrs · 28,175 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 69 BETWEEN STRINGER 12 RIGHT AND 13 RIGHT TO BE PUNCTURED IN RADIUS. THE AIRCRAFT WAS REMOVED FROM SERVICE. FABRICATED AND INSTALLED INTERNAL L- ANGLE IAW EO# EM-53MR=1940. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 29,861 hrs · 28,175 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 64 RT WAS FOUND WITH TOOLING MARKS BEYOUND SRM LIMITS DURING HEAVY CHECK. THE AIRCRAFT WAS REMOVED FROM SERVICE. MANUFACTURED AND INSTALLED L SHAPED DOUBLER OVER BLENDED AREA IAW EO# EM-53MR-1523. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 29,893 hrs · 28,193 cycles

DURING MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT FLOOR PANEL 231GF HAS ONE BROKEN WIRE. AIRCRAFT REMOVED FROM SERVICE. REPAIRED BROKEN WIRE IAW AWM 20-00--03. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,891 hrs · 28,192 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHTING BATTERY ASSEMBLY & BATTERY CHARGER INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHTING BATTERY ASSEMBLY & BATTERY CHARGER WC 33-700-19 #2 A3265. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BRACKET — CRACKED (PAX DOOR HANDLE) · airframe 29,891 hrs · 28,192 cycles

DURING HEAVY CHECK, FOUND PAX DOOR INTERNAL ACTUATING HANDLE FITTING BRACKET THAT ATTACHES TO WEB STRUCTURE, IS CRACKED. FOUND A REPAIR THAT APPEARS TO BE SATISFACTORY (SEE ETN EM52-037 AND EO EM-52MR-250) AT THE PAX DOOR INTERNAL ACTUATING HANDLE FITTING, BRACKET THAT ATTACHES TO WEB STRUCTURE. DID NOT FIND ANY NEW DISCREPANCY AND DID NOT SEE ANY CRACK MARKED.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 29,893 hrs · 28,193 cycles

DURING MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY LIGHT STRIP EXTRUSION AT PANEL 231GF DAMAGED, 241BF HAS DAMAGED WIRES, 251DF IS DAMAGED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP EXTRUSION AT PANEL 231GF IAW AMM 33-50-12. REPAIRED THE DAMAGED WIRES ON FLOOR PROXIMITY LIGHT STRIP AT PANEL 241BF IAW AWM 20-21-0. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP EXTRUSION AT PANEL 251DF IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FWD DOOR) · airframe 29,893 hrs · 28,193 cycles

DURING B-INSPECTION FOUND THE SERVICE DOOR FORWARD FLOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR FORWARD FLOOR SILL IAW EMB145SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 29,893 hrs · 28,193 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR PROXIMITY STRIP LIGHT WIRE AT FLOOR PANEL 251HF BROKEN. AIRCRAFT REMOVED FROM SERVICE. REPAIRED WIRE IAW AWM 20-00-03. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (COCKPIT) · airframe 29,450 hrs · 27,881 cycles

ON FLIGHT 2935 THE CREW REPORTED THE COCKPIT DOOR WAS UNACCEPTABLY DIFFICULT TO CLOSE AND LOCK IN FLIGHT. ISSUE REQUIRES ONE CREW MEMBER TO LEAVE SEAT TO SECURE. THIS CAUSES A SECURITY PROBLEM DUE TO DOOR BEING OPEN TOO LONG TO SECURE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED DOOR AS REQUIRED AND THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 52-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,450 hrs · 27,881 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE EXIT ROW INTERIOR FORWARD AISLE EMERGENCY EXIT CEILING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXIT ROW INTERIOR FORWARD AISLE EMERGENCY EXIT CEILING LIGHT ASSY, OPC BAD IAW EMB AMM 33-50-15. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,518 hrs · 27,235 cycles

FLIGHT ATTENDANT REPORTS EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE ON "A" SEAT SIDE AT THE OVERWING EXIT. REMOVED AND REPLACED EMERGENCY LIGHTING INVERTER NR 4 IAW EMB-145 AMM 33-50-11. OPERATIONAL TEST GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,108 hrs · 26,932 cycles

ON FLIGHT 4236 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT CRADLE HAD BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT HOLDER IAW EMB-145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — SATURATED (COCKPIT) · airframe 27,676 hrs · 26,595 cycles

FOR FLIGHT 4004 DURING TAXI THE CREW REPORTED THE EICAS DISPLAY SCREEN WENT OUT ASSOCIATED WITH A DISPLAY CIRCUIT BREAKER POPPING AND A SMELL OF AN ELECTRICAL ODOR. WATER WAS LEAKING FROM THE CENTER WINDSHIELD POST. THE AIRCRAFT WAS REMOVED FROM SERVICE. WATER HAD DRIPPED DOWN ON EICAS DISPLAY. WHEN POWERED ON IT SHORTED OUT THE EICAS DISPLAY. RETORQUED THE FIRST OFFICER’S WINDSHIELD AND SWAPPED THE DISPLAY OF THE FIRST OFFICER’S. VERIFIED THE ELECTRICAL ODOR WAS COMING FROM THE MFD DISPLAY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,814 hrs · 25,958 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW EMB 145 33-50-07. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 20,273 hrs · 16,869 cycles

DURING MAINTENANCE BASE VISIT FOUND THE COCKPIT OVERHEAD EMERGENCY LIGHT TO BE OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT OVERHEAD EMERGENCY LAMP IAW EMB 145 AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,273 hrs · 16,869 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY LAMP TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LAMP IAW EMB 145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,313 hrs · 25,575 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AFT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT OVER THE WING EMERGENCY LIGHT IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,914 hrs · 25,259 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT LAMP TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERWING EMERGENCY LIGHT LAMP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,781 hrs · 25,141 cycles

ON FLIGHT 4224 DURING THE INSPECTION FOUND THE RIGHT OVER WING EXTERNAL EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EXTERNAL OVERWING LIGHT BULB. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,622 hrs · 18,325 cycles

DURING MAINTENANCE FOUND RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. AIRCRAFT REMOVED FROM SERVICED. REMOVED AND REPLACED LIGHT BULB. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,332 hrs · 24,781 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT EMERGENCY FLOOR STRIP PARTIALLY LIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,173 hrs · 24,648 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FUSELAGE SKIN CRACKED IN THE UPPER AFT CORNER OF FIRST OFFICERS DV WINDOW CUTOUT. THE CRACK LENGTH IS 58 MM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED WINDOW CUTOUT WITH DOUBLER REPAIR IAW ENGINEERING ORDER EM 53MR 1536 PT. B. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 24,887 hrs · 24,413 cycles

DURING MAINTENANCE BASE VISIT FOUND RIGHT FRAME 64 HAS TOOLING MARKS BEYOND MANUAL LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED RIGHT FRAME 64 IAW EO-EM-53MR-1523. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,887 hrs · 24,413 cycles

DURING MAINTENANCE BASE VISIT FOUND FUSELAGE SKIN CRACKED IN UPPER AFT CORNER OF FIRST OFFICERS WINDOW CUT OUT. THE CRACK LENGTH WAS FOUND TO BE 58 MILLIMETERS IN LENGTH. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED SKIN WITH DOUBLER IAW EO EM-53MR-1536. THE AIRCRAFT WAS REMOVED FROM SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,887 hrs · 24,413 cycles

DURING MAINTENANCE BASE VISIT FOUND REAR FUSELAGE 1 LEFT PYLON ACCESS AREA SKIN DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED SKIN IAW EO EM-53MR-1525. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 24,887 hrs · 24,413 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT FRAME 64 HAD TOOLING MARKS BEYOND MANUAL LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 64 IAW ENGINEERING ORDER EM-53MR-1523. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — ODOR (NR 1) · airframe 24,202 hrs · 23,869 cycles

ON FLIGHT 4100 THE CREW REPORTED A LAVATORY SMOKE WARNING ON INITIAL CLIMBOUT AND COCKPIT FUMES PRESISITED WITH ELECTRICAL SMELL IN FORWARD CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 1 LEFT HAND ENGINE AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,492 hrs · 23,222 cycles

DURING FLIGHT 4319 THE CREW REPORTED A HOT SMELL IN THE CABIN DURING THE FLIGHT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED GROUND VISUAL INSPECTION OF THE CABIN AND GALLEY AREA WITH POWER ON AND OFF. RAN LEFT AND RIGHT PACKS FOR 15 MINUTES. INSPECTED HOT JUG SYSTEM AND FOUND NO ABNORMAL SMELLS AT THIS TIME. OPERATIONAL CHECK IS GOOD. THE AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,283 hrs · 23,048 cycles

DURING PS1 INSPECTION FOUND LEFT EXTERNAL OVERWING EMERGENCY LIGHT INOPERABLE. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LAMP IAW EMB AMM 33-30-10. OPERATIONAL CHECK GOOD IAW AMM 33-50-00-700-801-A. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 22,862 hrs · 22,644 cycles

CREW REPORTED AFTER TAKEOFF, F/A NOTIFIED CAPTAIN OF LAV FIRE ALARM GOING OFF. THERE WAS NO FIRE, NO ODOR, AND NO SMOKE NOTED. THERE WAS ALSO NO COCKPIT INDICATION OF SMOKE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED HIGH POWER RUN WITH FLIGHT CREW AND CHECK LAV FOR ANY SMOKE ODOR INDICATION, NO SMOKE OR ODOR NOTED, PERFORMED OPS CHECK OF LAV SMOKE DETECTION SYS, OPS CHECK NORMAL. ACFT RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 22,757 hrs · 22,526 cycles

RT AFT EMERGENCY LIGHT INOP. AIRCRAFT REMOVED FROM SERVICE. CHANGED INOP LIGHT BULB. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN)

ON FLIGHT 4343, CREW REPORTED SMOKE AFTER TAKEOFF ODOR AND SLIGHT HAZE IN AFT CABIN FOR APPROX TWO SECOND. CREW DECLARED A EMERGENCY AND RETURNED TO BLOCK. AIRCRAFT REMOVED FROM SERVICE. PERFORMED ETN EM-72-034, NO DEFECTS NOTED. EXAMINED DUCTS, NO DEFECTS. OPERATION CHECK GOOD OF PACK SYSTEM GOOD, NO SMELL NO SMOKE. NO PARTS CHANGED. AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — UNSERVICEABLE (CABIN LIGHTS) · airframe 22,078 hrs · 21,838 cycles

ON FLIGHT 3953 CREW REPORTED ELECTRICAL BURNING ODOR COMING FROM THE AREA OF THE CABIN LIGHT CONTROL PANEL AND FASTEN SEAT BELT SIGN ABOVE IT AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED PASSENGER CABIN LIGHTING CONTROL MODULE ASSEMBLY IAW EMB 145 AMM 33-21-01. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 19,993 hrs · 19,839 cycles

DURING A MBV INSPECTION, THE BAGGAGE DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND CLEANED THE AREA. POSITIONED NEW SILL AND MARKED AND DRILLED, COUNTERSUNK AND ALODINED PART. INSTALLED NEW PART. REPAIR DONE IAW EMBRAER 145 SRM (SRM EMB 145/1142 REV. 39) CHAPTERS 51-20-01, 03, 51-40-02, 04 AND 51-40-06. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 19,993 hrs · 19,839 cycles

DURING A MBV INSP, THE BAGGAGE DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND CLEANED THE AREA. POSITIONED NEW SILL AND MARKED AND DRILLED, COUNTERSUNK AND ALODINED PART. INSTALLED NEW PART. REPAIR DONE IAW EMBRAER 145 SRM (SRM EMB 145/1142 REV. 39) CHAPTERS 51-20-01, 03, 51-40-02, 04 AND 51-40-06. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 19,287 hrs · 19,199 cycles

AFTER LIFTOFF LAV SMOKE ON EICAS. SMOKE CONFIRMED BY FLIGHT ATTENDANT DECLARED EMERGENCY AND RETURNED FOR LANDING. FOLLOWED AOM PROCEDURES LANDED BELOW MAX LANDING WEIGHT. REMOVED AND REPLACED ENG 1 IAW W.C. 71-000-00. AIRCRAFT RETURNED TO SERVICE.

Part: RELAY — FAILED (NLG)

LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. EICAS DISPLAYED AMBER LANDING AIR/GRD FAIL MESSAGE. REPLACED NOSE AIR/GRD RELAY XK0352 IAW EMB MM 20-13-00, OPS CHECK GOOD.

Part: LANDING GEAR — LOCKED (LG SYS)

ORD - FLT 4072 - LANDING GEAR AIRGROUND FAIL MSG ON EICAS. COULD NOT MOVE LEVER TO RETRACT RETURNED TO LAND. MESSAGE WENT AWAY AFTER 5 MINUTES. AIRCRAFT RETURNED TO FIELD. INSPECTED NLG CAM CENTERING MECHANISM, MLG STRUT BACKLASH AGAINST PROX SWITCH ON GEAR LEGS WITH NO DEFECTS NOTED. INSPECTED COMPLIED WITH EMB 32-10-02 AND 32-10-01, RETURNED AIRCRAFT TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

DURING HMBV, RIGHT SIDEWALL SEAT TRACK BETWEEN FRAMES 47-53 IS CORRODED. REPLACED SEAT TRACK IAW EMB AMM 53-01-06 AND I/C 2006-145/3865. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: RIB — DAMAGED (RUDDER)

DURING HMBV, FOUND RUDDER 1 LIGHTNING HOLE FLANGE DAMAGED. REMOVED AND REPLACED RIB IAW SRM 57-40-03. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURNG HMBV, FOUND RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 30-36 CORRODED. REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING HMBV, FOUND RIGHT SIDEWALL SEAT TRACK BETWEEN FRAMES 24-30 CORRODED. REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

DURING HMBV, FOUND LEFT INBOARD FORWARD SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BEARING CAP — CORRODED (LT MLG)

SAW - DURING HMBV, FOUND FORWARD BEARING CAP LEFT MAIN LANDING GEAR CORRODED. REPLACED BEARING CAP IAW AMERICAN EAGLE WORK CARD 57-200-84. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

DURING HMBV, FOUND RIGHT SIDEWALL SEAT TRACK BETWEEN FRAMES 30-36 CORRODED. REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

DURING HMBV, FOUND RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 24-30 CORRODED. REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BEARING CAP — CORRODED (RT MLG)

SAW - DURING HMBV, FOUND FORWARD BEARING CAP RIGHT MLG CORRODED. REPLACED BEARING CAP IAW AMERICAN EAGLE WORK CARD 57-200-84. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

DURING HMBV INSPECTION, FOUND LEFT SIDEWALL SEAT TRACK BETWEEN FRAMES 47-53 CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING HMBV, FOUND RIGHT WALL SEAT TRACK BETWEEN FRAMES 36-47 CORRODED. RAI`D SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER CONTROL)

DFW - FLT 3359 - CREW REPORTED THE RUDDER SYSTEM 1-2 FAILED AFTER TAKEOFF AT BETWEEN 150-170 KNOTS. MECHANICAL REVERSION WAS CHECKED THROUGH RUDDER. DIDN’T SEEM OVERLY STIFF. COMPLETED AOM CHECKLIST AND RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED RUDDER SYSTEM 2 PRESSURE SWITCH IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, MAINTENANCE FOUND THE SERVICE DOOR SILL CORRODED. INSTALLED NEW SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE) · airframe 12,406 hrs · 12,475 cycles

DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD SILL AT SERVICE DOOR CORRODED UPPER SURFACE. INSTALLED FWD SILL AT SERVICE DOOR IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502484) (K)

Part: GUSSET — CORRODED (FUSELAGE)

DURING CPCP INSPECTION MAINTENANCE FOUND THE GUSSET ON HAT BEAM CORRODED IN NUMEROUS SPOTS. MAINTENANCE REPLACED THE GUSSET IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502484) (K)

Part: STRAP — CORRODED (FUSELAGE)

DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD STRAP AT FRAME 14 CORRODED ON THE UPPER SURFACE. REPAIRED SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502484) (K)

Part: SILL — CORRODED (GALLEY) · airframe 12,406 hrs · 12,475 cycles

DURING CPCP INSPECTION MAINTENANCE FOUND THE SERVICE DOOR, AFT SILL CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502484) (K)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED DAMAGED CENTER SILL. INSTALLED NEW SILL IAW EMB SRM, EMB 145/1142 REV 19, CHAPTER 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING IN IMBV INSPECTION, THE LEFT OMEGA BEAM AFT OF FRAME 24 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGED SECTION OF LEFT OMEGA BEAM AND TREATED BARE METAL EDGES. FABRICATED AN EXTERNAL ANGLE, TWO SHIMS AND FILLER. REPAIR DONE IAW EMB 145 SRM, EMB 145/1142 CHAPTER 53 REV 19, 53-21-10, FIG 202. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND TO BE CHAFED BEYOND SRM LIMITS AT SKIN JUNCTION 05. BLENDED CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142, CHAPTER 53, REV 19) 53-24-02, AND STANDARD SRM PRACTICES. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON A PREVIOUS REPAIR TO THE LEFT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR AND INSPECTION. THE UNDERLYING BEAM. NO ADDITIONAL DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142, CHAPTER 53, REV 19) 53-21-10 PARA 2 FIG 201 SHEET 1, AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. RIGHT AFT SILL HAS CORROSION. REMOVED CORRODED AFT SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. GALLEY AREA CENTER BEAM GUSSET HAS CORROSION. REMOVED BEAM AND INSTALLED SERVICEABLE BEAM IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. RIGHT FORWARD SILL HAS CORROSION. REMOVED CORRODED SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. SERVICE DOOR FORWARD SILL CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA AFT DIAMOND GUSSET HAS CORROSION. REMOVED CORRODED GUSSET AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING. GALLEY AREA LEFT SILL HAS CORROSION. REMOVED CORRODED SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, GALLEY AREA FORWARD DIAMOND GUSSET HAS CORROSION. REMOVED CORRODED DIAMOND GUSSET AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: CAP — CORRODED (NLG)

ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE NOSE LANDING GEAR RIGHT BEARING CAP. MAINTENANCE REPLACED THE NOSE LANDING BEARING CAP IAW EMB 145 MM 32-20-01-000-801-A AND 32-20-01-400-801-A. (M)

Part: CAP — CORRODED (LT MLG)

ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE LEFT MAIN LANDING GEAR LOWER FORWARD AND AFT BEARING CAPS. MAINTENANCE REPLACED THE CAPS IAW EMB145 MM 32-10-01-000-801-A AND 32-10-01-400-801-A. (M)

Part: CAP — CORRODED (LT MLG)

ABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE LEFT MAIN LANDING GEAR LOWER FORWARD AND AFT BEARING CAPS. MAINTENANCE REPLACED THE NOSE LANDING CAPS IAW EMB145 MM 32-10-01-000-801-A AND 32-10-01-400-801-A. REF SIMA200202310. (M)

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB)

MAF - FLT 3555 - DURING DESCENT, CAPTAINS YOKE PITCH TRIM SWITCH FAILED. AIRCRAFT WAS FERRIED TO ABI FOR REPAIR. HSCU WAS REMOVED AND REPLACED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ANTI-ICE VALVE — INOPERATIVE (TAIL)

HOU - FLT 3622 - CREW ABORTED TAKEOFF DUE TO WARNING INDICATION ON EICAS HOWEVER, THE CREW COULD NOT IDENTIFY WARNING. HAD THE CREW TO PERFORM PREFLIGHT COCKPIT CHECKS AND TEST TO SEE IF ANY OF THE SYSTEMS FAILED. NO SYSTEM FAIL CREW THEN PROCEEDED TO TRY TAKEOFF AGAIN. ONCE AGAIN HAD TO ABORT TAKEOFF DUE TO WARNING ON EICAS. WARNING WAS ENGINE 2 ANTI-ICE FAIL. MEL''D ENGINE ANTI-ICE SYSTEM. PENDING CLOSE OUT DUE TO MEL. MAINTENANCE REMOVED AND REPLACED THE NR 2 ANTI-ICE VALVE IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BEARING — FAILED (APU)

ORD - FLT 4062 - DURING CRUISE FLIGHT, LAVATORY SMOKE ILLUMINATED. CREW NOTED SOME KIND OF VAPOR OR MIST IN CABIN. MAINTENANCE TROUBLESHOT TO APU INTRODUCING VAPOR INTO THE APU BLEED WHICH ACTIVATED THE LAVATORY SMOKE DETECTOR. APU PUT ON MEL. REMOVED AND REPLACED APU. OPERATIONAL CHECK SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — FAILED (CABIN)

ORD - FLT 4045 - EMERGENCY FLOOR PROXIMITY LIGHTS AT ROWS 8 AND 9 DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT STRIP AT ROWS 8 AND 9. OPERATIONAL CHECK GOOD. (X)