N813AE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,817 hrs · 34,434 cycles

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

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 37,413 hrs · 34,065 cycles

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

Part: ANTI-ICE VALVE — FAILED (RT ENGINE) · airframe 36,225 hrs · 32,844 cycles

E2 A ICE FAIL IN AUTO MODE WHILE IN ICE CONDITIONS. VALVE FAILED CLOSED-C/A-DEFFERED E2 ANTI ICE M PROCEDURE C/W. REMOVED AND REPLACED E2 ANTI-ICING VALVE IAW EMB 140 AMM 30-21-01, OPS CK GOOD, MEL RESTORED

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,946 hrs · 32,556 cycles

THE EMERGENCY LIGHT ON THE DOOR COVER IS INOP. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-10. OPC GOOD.

Part: TIRE — OUT OF ROUND (NLG) · airframe 35,926 hrs · 32,534 cycles

SIGNIFICANT VIBRATION ON NOSE GAER ABOVE 15 KTS TO 80 KTS WORSE 50-80 WENT AWAY WITH TILLER OR PEDAL STEERING INPUTS.ONLY HAPPPENS DEAD CENTER * REPEAT WRITE UP-C/A-FOUND NOSE TIRE TO BE OUT OF BOUND RAR LH NOSE LANDING GEAR WHEEL ASSY IAW CARD NO. 32-700-17

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 35,465 hrs · 32,108 cycles

ON DESENT A CABIN AND FLIGHT DECK ODOR OF ACRID RUBBER WAS NOTICED THE FLIGHT WAS IN IMC, MODERATE TURBULANCE BOTH PACKS ON AND IN AUTO AND IGNITION SELECTORS WERE ON THE SMELL LASTED ABOUT 30 SECONDS AND WENT AWAY WHEN IGNITION WAS BACK TO AUTO. -C/A-C/W ETN-EM-72-034 AND PERFORMED ENG RUN WITH CREW WITH NO FINDINGS AND NO SMELLS NOTED PERFORMED GVI OF LT AND RT RELAY PANELS NO DEFECTS NOTED AIRCRAFT OK FOR SERVICE.

Part: ENGINE — CONTAMINATED (LEFT) · airframe 35,411 hrs · 32,063 cycles

ON DESCENT DIRTY SOCK SMELL IN COCKPIT AND CABIN A SLIGHT HAZE WAS VISABLE IN THE AIR. -C/A-FOUND OIL IN LT ENG FLOWPATH PER RRMM 72-30-00-200-803-A, REMOVED AND REPLACED TURBO LT ENG IAW W/W 71-00-00 OPC/LEAK CHECK GOOD, COMPLIED WITH ODOR EVENT ETN-EM-72-034 NO FAULTS FOUND

Part: UNKNOWN — ODOR (CABIN) · airframe 35,154 hrs · 31,796 cycles

DURING INITIAL CLIMB, THERE WAS A MELTED PLASTIC ODOR DURING THE FIRST COUPLE THOUSAND FEET. REMOVED AND REPLACED COCKPIT RECIRCULATION FAN IAW AMM 21-24-01. OPS CHECKED GOOD. REMOVED AND REPLACED NR 2 PACK WATER COLLECTOR IAW AMM 21-51-05. OPS TESTED GOOD. REMOVED AND REPLACED LT WATER COLLECTOR IAW AMM 21-51-05. OPS TESTED GOOD. OPS CK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 34,863 hrs · 31,453 cycles

FA AFT FLASHLIGHT WILL NOT STAY SECURED IN BRACKET. REMOVED AND REPLACED FLASHLIGHT BASE IAW AMM 33-50-16. OPS CHK GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 34,702 hrs · 31,296 cycles

CARGO DOOR SILL CORRODED IN MULTIPLE PLACES BETWEEN FR65 AND 68. REMOVED AND REPLACED CARGO DOOR SILL BETWEEN FR65 AND 68 IAW SRM 51-40-02.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 34,702 hrs · 31,296 cycles

FRAME 23 CRACKED AT RIGHT FLOOR SILL. REPAIRED FR 23 BTW STR 15R AND 16R IAW SRM 51-40-02 AND EO EM-53MR-1808.

Part: RIB — CRACKED (LT WING) · airframe 34,702 hrs · 31,296 cycles

LT WING OUTBD RIB WEB CRACKED AT PCA ACCESS PANEL. PERFORMED CUTOUT FABRICATED AND INSTALLED DOUBLER, FILLER AND SHIM FOR REPAIR OF LT WING RIB 21 IAW SRM 57-20-02 ITEM 4.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,702 hrs · 31,296 cycles

MACHINED FITTING BETWEEN FRAMES 19 AND 20 AT STRINGER 3L CRACKED. REMOVED AND REPLACED MACHINED FITTING BETWEEN FRAMES 19 AND 20 AT STRINGER 3L CRACKED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,702 hrs · 31,296 cycles

53-20-11 CENTER OMEGA BEAM IS CORRODED AT FRAME 59. REPAIRED CENTER OMEGA BEAM AT FR 59 IAW EO-EM-53MR-1518.

Part: CONNECTOR — DEFECTIVE (EMERGENCY LIGHT) · airframe 34,202 hrs · 30,752 cycles

PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED MALE SPLICE CONNECTOR FOR PASSENGER DOOR EXTERNAL EMERGENCY LIGHT IAW SWPM 20-21-00 AND WM 33-50-50. PASSENGER DOOR EXTERNAL EMERGENCY LIGHT OPT IS GOOD IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,159 hrs · 30,710 cycles

SERVICE DOOR GROUND ILLUMINATION EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR EXTERNAL GROUND ILLUMINATION EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECK GOOD.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 33,776 hrs · 30,346 cycles

DURING FLASHLIGHT FUNCTIONAL CHECK, W/C 33-700-20. FOUND F/O'S FLASHLIGHT CRADLE CRACKED. R & R EMERGENCY FLASHLIGHT CRADLE IAW AMM 33-50-16, OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 32,624 hrs · 29,119 cycles

AFTER TAKEOFF CREW RECEIVED SPOILER FAIL MSG ON EICAS IN FLIGHT. COMPLIED WITH AOM VOL 1 PROCEDURES. DECLARED AN EMER & LANDED WITHOUT INCIDENT. PERFORMED SPOILER SYS OPERATIONS CHECK IAW AMM 27-63-01. OPERATIONS CHECKED GOOD AT THIS TIME. ACFT OK FOR SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,915 hrs · 28,413 cycles

FOUND CRACK & BUCKLING ON FRAME 22 & STINGER 18, INTERNAL DAMAGE. TRANSFERRED TO NRWC 813-MQT-01987. COMPLIED WITH PERMANENT REPAIR IAW ERS-EM-53MR-1490.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,673 hrs · 28,174 cycles

FOUND DURING PS 2 INSPECTION EXTERIOR AFT EMER LIGHT TO BE INOPERATIVE. R & R AFT EXTERIOR EMER LIGHT BULB IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 31,540 hrs · 28,041 cycles

FLIGHT ATTENDANTS NR 1 FLASHLIGHT ASSEMBLY BROKEN. R & R FLASH LIGHT & CRADLE ASSEMBLY WITH SERVICEABLE UNIT IAW MM CH 33-50-16. OPERATIONS CHECKED GOOD. MEL ITEM RESTORED.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 31,142 hrs · 27,698 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR MID SKIN TIP 145-27274-006. R & R RT ELEVATOR MID SKIN TIP 145-27274-006 IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 55-20-01, ETN EM-55-073R2 & EM-55-076. SEE NRTC E432536 FOR PAINT, WEIGHT & BALANCE.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 31,142 hrs · 27,698 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR UPPER CTR SKIN 145-27270-006. R & R RT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 55-20-01, 55-10-01 & ETN EM-55-073R2. FOR PAINT, WEIGHT & BALANCE SEE NRTC E432536.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 31,142 hrs · 27,698 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR MID SKIN TIP 145-27274-005. R & R LT ELEVATOR MID SKIN TIP 145-27274-005 IAW SRM 55-20-01, 51-20-01 03, 51-40-02 06 & ETN EM-55-073. SEE NRTC E432541 FOR PAINT, WEIGHT & BALANCE.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 31,142 hrs · 27,698 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR OTBD UPPER SKIN TIP 145-37534-001. R & R LT ELEVATOR OTBD UPPER SKIN TIP IAW SRM 51-20-03, 51-40-06, 51-40-02, 51-20-01, CPM 51-21-04 & ETNS EM-55-073. SEE NRTC E432541 FOR PAINT, WEIGHT & BALANCE.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 31,142 hrs · 27,698 cycles

HAIL DAMAGE EVENT. REPLACE LT ELEVATOR UPPER CTR SKIN 145-27270-005. R & R LT ELEVATOR UPPER CTR SKIN IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 55-20-01, 55-10-01 & ETNS EM-55-073R2. FOR PAINT, WEIGHT & BALANCE SEE NRWC E432541.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 31,142 hrs · 27,698 cycles

REPLACE RT ELEVATOR OTBD UPPER SKIN TIP 145-37534-002. R & R RT ELEVATOR OTBD UPPER SKIN TIP 145-37534-002 IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 55-20-01, ETN EM-55-073R2 & EM-55-076. SEE NRTC E432536 FOR PAINT, WEIGHT & BALANCE.

Part: SKIN SPLICE — CORRODED (FUSELAGE) · airframe 31,142 hrs · 27,698 cycles

SKIN SPLICE CORRODED BETWEEN FRAME 13 & 14, STRINGER 21R - 20R. PERFORMED REPAIR OF SKIN SPLICE IAW SRM 53-00-02. SEE WIPS & TASK FOR DETAILS.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 31,142 hrs · 27,698 cycles

LEFT BEAM OTBD SUPPORT IS CRACKED BETWEEN FRAME 47 & 48. R & R IAW SRM 53-23-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,142 hrs · 27,698 cycles

EXTERNAL FUSELAGE LT, CRACKED AROUND RIVET, FRAME 77. APPLIED REPAIR TO DAMAGED LT SKIN IAW ERS-EM-5300-0159.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,142 hrs · 27,698 cycles

EXTERNAL FUSELAGE LT, SKIN CRACKED AROUND RIVET, FRAME 79. APPLIED REPAIR TO DAMAGED LT SKIN IAW ERS-EM-5300-0159.

Part: SKIN SPLICE — CORRODED (FUSELAGE) · airframe 31,142 hrs · 27,698 cycles

EXTERNAL FUSELAGE LT SKIN CRACKED AROUND RIVET, FRAME 78. APPLIED REPAIR TO DAMAGED LT SKIN IAW ERS-EM-5300-0159.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,142 hrs · 27,698 cycles

EXTERNAL FUSELAGE RT, SKIN CRACKED AROUND RIVET, FRAME 77. APPLIED REPAIR TO DAMAGED RT SKIN IAW ERS-EM-5300-0158.

Part: SKIN SPLICE — CORRODED (FUSELAGE) · airframe 31,142 hrs · 27,698 cycles

EXTERNAL FUSELAGE RT SKIN CRACKED AROUND RIVET, FRAME 78. APPLIED REPAIR TO DAMAGED RT SKIN IAW ERS-EM-5300-0158.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 31,142 hrs · 27,698 cycles

RIGHT FWD AILERON TORQUE TUBE SUPPORT CORRODED BETWEEN FRAME 12 & 13. R & R IAW SRM 51-40-02. SEE TURNOVER FOR DETAILS.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,142 hrs · 27,698 cycles

STRINGER 21R CORRODED FRAME 13. R & R IAW SRM 51-40-02.

Part: RELAY — MALFUNCTIONED (STAB) · airframe 31,093 hrs · 27,659 cycles

ON DESCENT IN ICING CONDITIONS CREW RECEIVED STAB ANTI-ICE FAIL MSG. CREW COMPLIED WITH AOM VOL 1 PROCEDURES. DECLARED AN EMER & LANDED WITHOUT INCIDENT. R & R RELAY K0537 IAW AMM 30-11-00. OPS CHECKED GOOD IAW AMM 30-00-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 30,974 hrs · 27,562 cycles

ON TAKEOFF, WE RECEIVED A TAKEOFF CONFIG WARNING AROUND 60KTS, THE VOICE DID NOT ANNOUNCE THE COMPONENT THAT CAUSED THE WARNING. HOWEVER THE SPOILERS SHOWED OPEN WITH HANDLE CLOSED. TRANSFERRED TO NRWC 813-DFW-01817. FOLLOWED FIM 31-51-00-810-804 FOR NO TAKEOFF CONFIG ON EICAS & PERFORMED OPERATIONAL CHECK OF THE AURAL WARNING UNIT IAW AMM 31-51-00 & FOUND TO BE OK FOR SERVICE. SEE ITEMS BELOW FOR ADDITIONAL GVI & OPERATIONS CHECKS.

Part: CONTROL UNIT — FAILED (BRAKE SYSTEM) · airframe 30,426 hrs · 27,123 cycles

FLIGHT DISABLED ON TAXIWAY B JUST NORTH OF TAXIWAY A NEAR RUNWAY 04 WITH BRAKES LOCKED UP. PAX DEPLANED & BUSSED TO TERMINAL. ACFT TOWED TO GATE. ADVANCED THRUST LEVERS 70% N1 BRAKES 0 PLANE DID NOT MOVE. REMOVED AND REPLACED BRAKE CONTROL UNIT IAW AMM 32-41-02 OPS CHECK GOOD.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 30,359 hrs · 27,054 cycles

AFT CABIN EMER FLASHLIGHT ON & OFF SWITCH INTERMITTENT. R & R AFT CABIN FLASHLIGHT IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,868 hrs · 26,598 cycles

CAPTAIN`S FLASHLIGHT NOT INDICATING CHARGING WHILE PROPERLY SET IN CRADLE. R & R CAPTAIN'S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 29,158 hrs · 25,979 cycles

RT OVERWING AFT EMERGENCY LIGHT IS INOPERATIVE. R & R RT OVERWING AFT EMERGENCY LIGHT BULB IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 29,137 hrs · 25,957 cycles

AFTER TAKEOFF KGCK, SELECTED GEAR UP & HANDLE WOULD NOT MOVE. PRESSED DOWN LOCK REL BUTTON, HANDLE WENT UP BUT NLG SHOWED IN TRANSIT & WOULD NOT RETRACT. ABOUT THE SAME TIME GOT LG AIR & GND POST EICAS. SELECTED LG DOWN GEAR EXTENDED & GOT 3 GREEN INDICATION, DIVERTED TO AMA. ABOUT 20 MINUTES INTO FLT LA AIR & GND FAIL EICAS WENT AWAY. UNABLE TO DUPLICATE, SUSPECT ICE ON NLG PREVENTED FULL EXTENSION. VERIFIED WOW SYS, OPERATIONS CHECKED OK IAW AMM CH 32-63-00. VERIFIED NLG STRUT FULLY EXTENDS & NWS CTR CAM ENGAGES. VERIFIED LANDING GEAR EXTENSION & RETRACTION, OPERATIONS CHECKED OK IAW AMM CH 32-30-00 & RII 146777.

Part: HOSE — CHAFED (HYD SYSTEM) · airframe 28,280 hrs · 25,197 cycles

CREW REPORTED DURING CRUISE, RECEIVED AN EICAS HYD 2, LOW QTY MESSAGE FOLLOWED BY ENG 2 HYD FAIL MESSAGE. COMPLIED WITH AOM VOL 1, PROCEDURES AND DECLARED AN EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. SERVICED HYD TO LEVEL AFTER E2 PUMP CHANGE IAW AMM -12-13-01. R & R HYD 2, PUMP AND SYS FILTERS IAW AMM 29-10-03 AND 29-10-08. LEAK CHECK FAILED. FOUND HYD PRESSURE HOSE TO BE CHAFED. R & R THE HYD PRESSURE HOSE IAW AMM 20-10-03. OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — MALFUNCTIONED (COCKPIT) · airframe 28,154 hrs · 25,077 cycles

CAPTAINS FLASHLIGHT NOT SHOWING CHARGE STATUS LIGHT. R & R FLASHLIGHT IAW STANDARD & PRACTICES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,008 hrs · 24,940 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,271 hrs · 24,303 cycles

DURING MX PS2 INSP, FOUND THE LT SIDE CENTER FAIRING EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LIGHT BULB IAW AMM 33-50-10. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — BROKEN (COCKPIT) · airframe 27,226 hrs · 24,261 cycles

FLIGHT 4396, CREW REPORTED CAPTAIN’S FLASHLIGHT HOLDER BROKEN. ACFT REMOVED FROM SERVICE. R & R BROKEN FLASHLIGHT AND FLASHLIGHT HOLDER IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,007 hrs · 24,060 cycles

DURING PS-1 CHECK, FOUND FURTHEST AFT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50-08, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 26,943 hrs · 23,997 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD FLIGHT ATTENDANT FLASHLIGHT BASE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT BASE PER AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 26,807 hrs · 23,850 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT IN THE COCKPIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT EMERGENCY LIGHT BULB IAW EMB AMM 33-50-05-000-801-A AND 33-50-05-400-801-A.THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,809 hrs · 23,852 cycles

DURING MAINTENANCE INSPECTION FOUND THE BAGGAGE DOOR SILL HAS SEVERAL SPOTS OF CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SILL IAW EMBRAER STRUCTURAL REPAIR MANUAL 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,809 hrs · 23,852 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT FRAME 10 IS CRACKED BELOW DV WINDOW. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT FRAME 10 IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 23,852 hrs · 23,852 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OUTBOARD OMEGA BEAM FLOOR SUPPORT IS CRACKED BETWEEN FRAMES 48 & 49. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OMEGA BEAM FROM FRAMES 45 TO 52 IAW STRUCTUAL REPAIR MANUAL 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (RT WING) · airframe 26,809 hrs · 23,852 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT WING LOWER SKIN TO HAVE A 1" CRACK AT INBOARD EDGE OF RIB 5. REPAIRED SKIN IAW EO EM-57MR-675AND ETA-EM-5700-691. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — DAMAGED (CABIN) · airframe 26,831 hrs · 23,878 cycles

DURING MAINTENANCE INSPECTION FOUND NR 1, 2, 4, 6 7 PROXIMITY (EMERGENCY) LIGHT STRIP HOLDERS DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1, 2, 4, 6 7 PROXIMITY (EMERGENCY) LIGHT STRIP HOLDERS, HARDWARE & CONNECTION STRIPS IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,831 hrs · 23,878 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT TO HAVE A DEAD BATTERY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY FOR THE AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IAW EMB AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — MISSING (CABIN) · airframe 26,831 hrs · 23,878 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT CABIN EMERGENCY LIGHT STRIP WIRES (2) ARE MISSING WIRE CONNECTIONS. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW CONNECTORS AT SPLICE SP9502 AND SP9503 IAW SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,831 hrs · 23,878 cycles

DURING MAINTENANCE INSPECTION FOUND MOST OF THE AFT EMERGENCY FLOOR PROXIMITY LIGHT STRIPS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED MOST OF THE AFT EMERGENCY FLOOR PROXIMITY LIGHT STRIPS IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (BLEED AIR SYS) · airframe 26,657 hrs · 23,727 cycles

ON FLIGHT 3240 THE CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A NR 2 ENGINE BLEED LEAK MESSAGE. THE CREW FOLLOWED AOM VOL 1 PROCEDURES. THE MESSAGE DISAPPEARED AND THEN CAME BACK. THE CREW CONTINUED TO FOLLOW THE AOM PROCEDURES WHICH LEAD THEM TO SHUTDOWN THE NR 2 ENGINE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO GGG. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. VERIFIED LEAK 2 ILLUMINATED ON BLEED 2 WITH NO BLEED AIR PRESENT ON AIRCRAFT, FOUND WIRE W772-0001 BROKEN OFF S7263 AND SHORTED TO GROUND. RE-ATTACHED WIRE TO S7263. THE OPERATIONAL CHECK WAS OK IAW WM 36-21-50. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

RIGHT OVERWING EMERGENCY LIGHT LAMP INOP. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10, OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 25,842 hrs · 22,955 cycles

DURING B INSPECTION FOUND THE LEFT WING AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GROUND WIRE — DIRTY (CABIN) · airframe 25,777 hrs · 22,892 cycles

DURING B INSPECTION FOUND THE MAIN DOOR STAIR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT BULB IN REFERENCE WITH EMB AMM TASK: 33-50-10-000-801-A, AND 33-50-10-400-801-A. NO FIX. REMOVED EMERGENCY LIGHT ASSEMBLY AND FOUND GROUND WIRE HAD BAD CONNECTION CLEANED GROUND WIRE AND TESTED FOUND TO BE GOOD. RE-INSTALLED ASSEMBLY WITH NEW BULB. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 25,360 hrs · 22,495 cycles

DURING B INSPECTION FOUND THE AFT PASSENGER CABIN FLASHLIGHT BATTERY CONNECTOR CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,218 hrs · 22,367 cycles

DURING B INSPECTIONS FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-40-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,382 hrs · 21,583 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT FLOOR STRIP AT SEATS 7A AND 8A IS INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTING PROXIMITY STRIP AT 7A-8A IAW EMB 140 33-50-12. THE OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,183 hrs · 21,393 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT FLASHLIGHT INOPERABLE (NEXT TO PASSENGER DOOR). THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN'S FLASHLIGHT IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 22,539 hrs · 19,997 cycles

ON FLIGHT 4300 (ON FIRST FLIGHT OF THE DAY) THE CREW REPORTED THAT AT 17000 FEET WHILE PERFORMING THE ANTI ICE TEST RECEIVED A BLEED 2 OVER TEMPERATURE WARNING. WHEN THE CREW PUT THE OVERRIDE KNOB BACK TO AUTO THE EICAS WARNING MESSAGE WAS GONE. THE CREW REPEATED ONE MORE TIME AND GOT THE WARNING MESSAGE. THE CAPTAIN ELECTED TO DIVERT TO CMH. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE E2 FAN AIR VALVE IAW AMM 36-11-03. ACCOMPLISHED E2 AIR BLEED SYSTEM OPERATIONAL TEST IAW AMM 36-00-00. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,531 hrs · 19,990 cycles

DURING MANTENANCE BASE VISIT FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT OMEGA BEAM AT FRAME 20 IAW SRM 53-00-10 FIGURE 201. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,531 hrs · 19,990 cycles

DURING MANTENANCE BASE VISIT FOUND FRAME 23 TO BE CRACKED BETWEEN STRINGERS 15 RIGHT AND 16 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 IAW EO EM-53MR-1815. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 22,273 hrs · 19,755 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE FIRST OFFICERS FLASHLIGHT HOLDER BROKEN. THE AICRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE HOLDER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,524 hrs · 19,125 cycles

ON FLIGHT 4069 THE CREW REPORTED THE FLOOR PROXIMITY LIGHTS FROM ROW 11 TO ROW 16 TO BE INOPERABLE. THE AIRACRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FIRE LOOP — MALFUNCTIONED (LT NACELLE)

ON FLIGHT 4278 UPON LANDING CREW REPORTED, AN ENGINE 1 FIRE INDICATION. NO EMERGENCY DECLARED AND FIRE BOTTLE WAS NOT DISCHARGED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER 1 ENGINE FIRE DETECTION LOOP IAW EMB 140 AMM 26-11-01. FIRE DETECTION OPERATIONAL CHECK PERFORMED AND SYSTEM FUNCTIONS NORMALLY. AIRCRAFT RETURNED TO SERVICE. (A)

Part: COMPUTER — ODOR · airframe 13,773 hrs · 12,494 cycles

IC BUS FAIL, ILLUMINATED ON EICAS IC2 C/B POPPED. FLIGHT ATTENDANT SMELLED SMOKE FOR A BRIEF PERIOD OF TIME BUT IT DISSIPATED QUICKLY. REMOVED AND REPLACED IC-600 COMP IAW EMB140 AMM 31-42-01. PERFORMED OPS CHECK IAW EMB140 AMM 31-42-00. OPS CHECK GOOD. AIRCRAFT RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (UNKNOWN)

TOWER REPORTED WHITE VAPOR COMING FROM AIRCRAFT ON CLIMBOUT FROM DFW, RETURN TO DFW. (M)

Part: INVERTER — FAILED (EMERGENCY LIGHT)

SBP - FLT 3139 - FOUND CEILING EMERGENCY EXIT ROW 11 EXIT LIGHT INOPERATIVE. RAI INVERTER IAW AMM 33-50-11. OPS CHECK GOOD. RETURN AIRCRAFT TO SERVICE. (M)

Part: WIRE — LOOSE (EMERGENCY LIGHT)

LAX - FLT 3109 - CEILING EMERGENCY LIGHT EXIT AT ROW 11 INOPERATIVE. FOUND MID CEILING EXIT LOCATOR FORWARD WIRE SPLICE LOOSE, RESECURED WIRE AND PERFORMED OPS CHECK IAW EMB 140, AMM 33-50-00, OPS CHECK GOOD.

Part: TRIM SYSTEM — FAILED (UNKNOWN)

SJC - FLT 3141 - NOTIFIED BY THE CREW 30 SEC AFTER TAKEOFF MAIN PITCH TRIM FAILED. CAPT ELECTED TO RETURN TO FIELD. REPLACED TRIM CONTROL PANEL. OPS CHECK GOOD. REPLACED PILOT YOKE PITCH TRIM SWITCH. OPS CHECK GOOD. COMPLIED WITH REPEAT CONTROL WORK SCOPE. ALL OPS CHECK GOOD. TRIM CONTROL PANEL 13-34177-405 S/N OFF 57896. CAPTAIN PITCH TRIM SWITCH P/N 145/63000-401 S/N OFF L4632. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRUCTURE — VIBRATION (COCKPIT)

PILOT WROTE CONSTANT VIBRATION THROUGH THE COCKPIT FLOOR DURING CLIMB AND FLIGHT. PERFORMED ALL TASK ON THE VIBRATIONS W/C AND NO DEFECTS NOTED. PERFORMED FCF AND ALL PARAMETERS WERE OPS CHECK GOOD. TRIAD RELEASED THE A/C AND RETURNED TO SERVICE. (M)

Part: FAN — SEIZED (CABIN)

SJC - FLT 3158 - CREW REPORTED PLASTIC BURNING SMELL IN ENTIRE AIRCRAFT HAD TO DON OXYGEN MASKS. REPLACED NR 1 RECIRCULATION FAN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FIRE WARNING — FALSE INDICATION (CARGO BAY)

THE BAGGAGE COMPARTMENT EXTINGUISHER LIGHT ILLUMINATED. THE CAPTAIN DISCHARGED THE BAGGAGE COMPARTMENT FIRE BOTTLES AS A PRECAUTIONARY. THE FIRE DEPT INSPECTED THE CARGO AREA AND FOUND NO EVIDENCE OF SMOKE OR FIRE. RAI HIGH RATE BOTTLE AS PER EMB 140 AMM 26-23-01 AND METERING BOTTLE P/N 34600731, S/N 17924F1. ALL SYSTEMS OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FS 25)

THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 29, CHAPTER 53-00-10. (M)

Part: SILL — CORRODED (SERVICE DOOR)

THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE SERVICE DOOR SILL TO REMOVE THE CORROSION. FABRICATED A DOUBLER. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 29, CHAPTER 53-21-02 FIG 201 AND 203. (M)

Part: BEAM — CORRODED (GALLEY)

THE GALLEY CENTER BEAM WAS FOUND TO BE CORRODED UNDER THE FLOOR RAMP. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED EXTERNAL DOUBLER. REPAIR DONE IAW EMB SRM, SRM EMB145/1142 REV 29, CHAPTER 53-21-10 FIG 202 SHEET 2. (M)

Part: FRAME — CORRODED (FS 81)

ABI - FRAME 81 WAS FOUND GOUGED AT THE 6 O`CLOCK POSITION.

Part: FLOOR SUPPORT — CORRODED (FS 27)

THE LEFT OMEGA BEAM AT FRAME 27 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE OMEGA BEAM TO REMOVED THE CORROSION. FABRICATED AN EXTERNAL, DOUBLER, AND FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB145/1142 REV 29, CHAPTER 53-00-10, FIG 202. (M)

Part: FLOOR SUPPORT — CORRODED (FS 27)

ABI - THE CENTER OMEGA BEAM AT FRAME 27 WAS FOUND CORRODED. PERFORMED A CUT OUT OF BEAM TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB145/1142 REV 29, CHAPTER 53-00-10, FIG 203. (M)

Part: FLOOR SUPPORT — CORRODED (FR 20)

THE LT OMEGA BEAM AT FR 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER, PLATE, AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: STRINGER — CHAFED (STR 19R)

A PREVIOUS REPAIR ANGLE ON STRINGER 19R WAS FOUND CHAFED. REMOVED THE EXISTING REPAIR ANGLE AND CLEANED THE AREA. FABRICATED AN INSTALLED A NEW REPAIR ANGLE. REPAIR DONE IAW SRM. (K)

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB)

YYZ- FLT 4904 - DURING APPROACH WHEN AUTO PILOT WAS DISCONNECTED, PITCH TRIM 1-2 INOPERATIVE MESSAGE CAME ON EICAS. STAYED ON FOR A FEW SECONDS THEN WENT OUT. BOTH PITCH TRIM SWITCHES WORKED. LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE COMPLIED WITH ETN EB 27-022. THE HSCU WAS REMOVED AND REPLACED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)