N616AE

Part: NONE — NONE · airframe 49,597 hrs · 45,166 cycles

FWD FA EMERGENCYFLASHLIGHT IS MISSING-C/A-RAR FWD FA EMERGENCY FLASHLIGHT. IAW E145 AMM 33-50-16

Part: NONE — NONE · airframe 49,526 hrs · 45,087 cycles

AFT EMERGENCY FLASHLIGHT MISSING MEL 25-32. AUTH #110026M-C. REF LOG PG 4676473/1.-C/A-RAR AFT EMEREGENCY FLASHLIGHT ASSY ON TOILET FWD PARTITION, BEHIND LAST DOUBLE SEAT IAW EMB 145 AMM 33-50-16. OPC GOOD. MEL ITEM RESTORED. (M) PROCEDURES REVERSED.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 BLEED SYS) · airframe 48,512 hrs · 43,965 cycles

BLEED 1 LEAK EICAS MSG IN AIR. HAPPENED AFTER OR DIRECTLY AFTER ENTERING ICING DID NOT DECLARE EMERGENCY-C/A-PERFORMED DUCT LINE INSPECTION AND CHECK IAW EMB 145 36-11-09 AND PERFORMED ENGINE BLEED VALVE OPERATIONAL CHECK IAW 36-11-05. OPS CHECK GOOD

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 48,276 hrs · 43,748 cycles

REAR CABIN EMERGENCY FLASHLIGHT MISSING-C/A-REPLACED CABIN CABIN FLASHLIGHT IAW ETN-EM-33-034 OPC GOOD NO FUTHER DEFECTS NOTED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,263 hrs · 43,731 cycles

LEFT FWD WING TO FUSELAGE FAIRING EMERGENCY LIGHT INOPERATIVE. C/A-REMOVED AND REPLACED NR 1 EMERGENCY BATTERY AND NR 1 EMERGENCY CHARGER ASSY IAW WORK CARD 33-700-19. OPERATIONAL CHECK GOOD. NO DISCREPANCIES NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,132 hrs · 43,584 cycles

RT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R RT OVERWING EMERGENCY LIGHT LAMP, IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPERATIONS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 47,576 hrs · 43,002 cycles

MAIN CABIN DOOR WOULDN'T OPEN FROM THE INSIDE.-C/A-LUB. THE MAIN DOOR FRAME ROLLERS AS REQUIRED.OPS. CHECK GOOD.NO DEFECTS NOTED AT THIS TIME.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 47,318 hrs · 42,746 cycles

SERVICE DOOR LOWER CENTER FLOOR SILL CORRODED-C/A-REPAIRED MIDDLE AND FWD NUTPLATE HOLES OF SERVICE DOOR CENTER SILL, IAW EMB 145 SRM 53-21-02.

Part: DOOR FRAME — GOUGED (CARGO DOOR) · airframe 47,318 hrs · 42,746 cycles

CARGO DOOR LWR OTBD FRAME FWD CORNER GOUGED-C/A-REMOVED AND REPLACED CARGO DOOR OTBD FRAME IAW EMB 145 SRM 51-40-02

Part: PROFILE — BENT (CARGO DOOR) · airframe 47,318 hrs · 42,746 cycles

CARGO DOOR LOWER PROFILE IS BENT NEAR FORWARD ROLLER-C/A-REMOVED AND REPLACED CARGO DOOR LOWER PROFILE IAW EMB 145 SRM 51-40-02

Part: FRAME — DENTED (FUSELAGE) · airframe 47,318 hrs · 42,746 cycles

FRAME 72 BETWEEN STRINGERS 15R AND 17R HAS A DENT-C/A-REMOVED AND REPLACED FRAME 72 IAW EMB 145 SRM 51-40-02

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 47,318 hrs · 42,746 cycles

CARGO DOOR LWR SIDE EDGE 4 NUTPLATE HOLES CORRODED-C/A-REMOVED AND REPLACED CARGO DOOR LWR INBD FRAME IAW EMB 145 SRM 51-40-02

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 47,318 hrs · 42,746 cycles

CARGO DOOR FWD SIDE EDGE NUTPLATE HOLE CORRODED OUT OF LIMITS-C/A-REPAIRED CARGO DOOR FWD FRAME CENTER HOLE IAW EMB 145 SRM 52-30-04RE

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 46,884 hrs · 42,320 cycles

MAIN DOOR EMERGENCY LIGHT INOP"TRANSFERRED TO NRWC 616-ORD-03398"-C/A-DEFERRED PER MEL 33-29. CLEANED MAIN DOOR EMERGENCY LIGHT ASSY ELECTRICAL CONNECTIONS IAW SWPM 20-50-00. OPS CHECK GOOD IAW EMB AMM 33-50-00. MEL RESTORED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,477 hrs · 41,905 cycles

ROW 12 B/C OVERHEAD EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED 12 B/C OVERHEAD EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-07-04. OPS CHECK GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (FWD CARGO) · airframe 46,276 hrs · 41,734 cycles

ON TAXI RECIEVED BAGG SMOKE INDICATION. REMOVED AND REPLACED FWD CARGO SMOKE DETECTOR IAW AMM 26-15-01 OPC GOOD

Part: ENGINE — FAILED (APU) · airframe 45,946 hrs · 41,490 cycles

POSSIBLE APU FIRE, SMOKE COMING FROM APU INTAKE. REMOVED AND REPLACED APU IAW W/C 49-800-05. OPS CHECK GOOD LEAK CHECK GOOD.

Part: CONTROL VALVE — FAILED (BRAKE SYSTEM) · airframe 45,725 hrs · 41,247 cycles

ON FINAL APPROCH WHEN LANDING REAR EXTENDED BRAKE DEGRADED MASTER CAUTION INDICATION APPEARED DID GO AROUND CAUTION DISAPPEARED WHEN LANDING GEAR RETRACTED + REAPPEARED ON 2ND LANDING NO BRAKING ACTION DEGRADATION ON LANDING. CAUTION DID NOT DISAPPEAR "TRANSFERRED TO NRWC 616-ORD-02975". C/A-REMOVED AND REPLACED BRAKE CONTROL VALVE IAW AMM 32-41-06 LEAK CHECK OPS CHECK GOOD NO FURTHER DISCREPANCIES NOTED AT THIS TIME.

Part: VALVE — FAILED (AC BAY) · airframe 45,457 hrs · 40,972 cycles

PAC 1 VALVE FAIL IN FLIGHT; PAC 1 & 2 OVLD IN FLIGHT; BURNING SMELL IN COCKPIT. SMELLED LIKE BURNT PLASTIC. NO COMPLAINTS OF BURNING SMELL IN CABIN. NO SMOKE OBSERVED IN COCKPIT. C/A-REMOVED AND REPLACED #1 PACK VALVE IAW AMM 21-51-01. PERFORMED OPERATIONAL TEST OF COOLING PACK SYSTEM IAW AMM 21-51-00. OPS TEST GOOD. NO DEFECTS NOTED. PERFORMED OPERATIONAL TEST OF COOLING PACK SYSTEM IAW AMM 21-51-00 WITH BLEED SOURCES: APU, ENG BLEED 1, AND ENG BLEED 2. OPS TEST GOOD. NO DEFECTS NOTED. PREFORMED LEAK ODOR EVENT TROUBLE SHOOOTING IAW ETN-EM-72-034. NO SMOKE OR ODOR NOTED. SUSPECT ODOR CAME FROM STATIC INVERTER. REMOVED AND REPLACED A/C STATIC INVERTER IAW AMM TASK 24-20-01-04. OPS CHECKED A/C GENERATION IAW TASK 24-20-00 SUCCESSFULLY. STATIC INVERTER P/N 816604-1 S/N 200104212.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 45,420 hrs · 40,935 cycles

AFT CABIN FLASHLIGHT CRADLE BROKEN. C/A-REMOVED AND REPLACED AFT FLASHLIGHT CRADLE IAW AMM TASK 33-50-16-000-801-A AND 33-50-16-400-801-A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,402 hrs · 40,912 cycles

FLOOR EMERGENCY LIGHT STRIP AT ROWS 6A/7A INOP. C/A-REMOVED AND REPLACED EMERGENCY LIGHT STRIP IAW AMM 33-50-12 OPS TEST GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,358 hrs · 40,864 cycles

DURING PS-2 FOUND LH EXT EMERGENCY LIGHT BURNED OUT. C/A-REMOVED AND REPLACED LT FWD EXT EMERGENCY LIGHT ASSY IAW 33-50-10. EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-50-00. EMERGENCY LIGHTING BATTERY NR 4 P/N 2013-1A S/N 103874 AND 79164, NR 1 109569. BATTERY CHARGER ASSY P/N 11-0049 S/N 13259.

Part: CONNECTOR — MISSING (CABIN) · airframe 44,372 hrs · 39,928 cycles

THE EMERGENCY LIGHT STRIP CONNECTOR THAT CONNECTS TO THE EMERGENCY LIGHT STRIP AT FLOOR PANEL 251BF HAS MISSING CONNECTOR. INSTALLED SERVICEABLE CONNECTOR ON EMERGENCY LIGHT STRIP AT FLOOR PANEL 251BF IAW SWPM 20-21-00.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 44,197 hrs · 39,779 cycles

NR 1 EMERGENGY LIGHT BATTERY HAD LOW VOLTAGE. R & R THE BATTERY, OPS CHECKED GOOD. THE BATTERY HAD A BLOWN FUSE.

Part: VALVE — DEFECTIVE (CABIN PRESSURE) · airframe 42,866 hrs · 38,631 cycles

A/C WOULD NOT PRESSURIZE AFTER TAKE OFF. R & R GROUND CONNECTION VALVE. PERFORMED OPS CHK OF PRESSURIZATION OPS CHECK GOOD.

Part: VALVE — DEFECTIVE (CABIN PRESSURE) · airframe 42,855 hrs · 38,621 cycles

UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKE OFF. R&R GROUND CONNECTION VALVE PERFORMED OPS CHECK OF PRESSURIZATION, OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 42,798 hrs · 38,573 cycles

F/O WINDSHIELD OUTER PLY SHATTERED. R & R F/O WINDSHIELD OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (STEERING SYSTEM) · airframe 42,182 hrs · 38,396 cycles

UNCOMMANDED STEERING SWERVED ON GROUND. REMOVED AND CLEANED FEEDBBACK POT CONNECTOR. RECONNECTED AND HAD CREW PERFORM TAXI OPS CHECK OF STEERING. NO DEFECT NOTED.

Part: SKIN — CRACKED (FRAME 75) · airframe 42,698 hrs · 38,491 cycles

RIGHT FUSELAGE EXTERIOR SKIN AT FR 75 HAS 3 POSSIBLE CRACKS - MARKED. PERFORMED REPAIR ON RH FUSELAGE EXTERIOR SKIN AT FR 75.

Part: LINE — FAILED (HYD SYSTEM) · airframe 40,036 hrs · 36,252 cycles

ON TAKEOFF, RECEIVED A LANDING GEAR DISAGREE MESSAGE AND HYD SYS 1 FAIL AND HYDRAULIC SYS 1 LOW QTY. INSPECTED AND FOUND LT MLG ACTUATOR HYDRAULIC LINE FAILED. R & R HYD LINE PERFORMED OPS CHECK OF GEAR. OPS AND LEAK CHECK GOOD.

Part: BUTTON — INOPERATIVE · airframe 39,953 hrs · 36,182 cycles

THRUST RATING PANEL CLIMB BUTTON WOULD NOT ENGAGE. R & R THRUST RATING PBA. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,413 hrs · 34,911 cycles

SERVICE DOOR, NR 2 SHROUDED EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 38,413 hrs · 34,911 cycles

COCKPIT STEP EXIT IDENTIFIER LIGHT NR 9 DOES NOT ILLUMINATE. MAINTENANCE REPLACED LIGHT, OPS CHECKED GOOD.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 38,413 hrs · 34,911 cycles

MAIN DOOR EMERGENCY FLOOD LIGHT NR 13 SWITCHED WITH COURTESY LIGHT. MAINTENANCE SWITCHED LIGHTS TO THE CORRECT POSITION, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,400 hrs · 34,899 cycles

FLOOR PROXIMITY EMER EXIT LIGHTS FROM EMER EXIT ROW TO THE FRONT DO NOT ILLUMINATE. OPERATED APU TO CHARGE EMER BATTERIES. TURNED ON EMER LIGHTS. PERFORMED OPERATIONS CHECK IAW AMM 33-50-00-700-801-A. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 38,400 hrs · 34,899 cycles

FLAP LOW SPEED ADVISORY APPEARED ON EICAS DURING CLIMB OUT. REINSTALLED FLAP DRIVE MOTORS IN ORIGINAL LOCATIONS IAW AMM 27-53-01. PERFORMED TAKEOFF FLAPS OPERATIONS CHECK IAW AMM 27-53-00-700-802-A. OPERATIONS CHECKED GOOD. CYCLED FLAPS MULTIPLE TIMES & COULD NOT DUPLICATE DISCREPANCY.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 38,399 hrs · 34,898 cycles

LOWER RT PARTITION DOUBLER ON FRAME 61 IS CORRODED BEYOND LIMITS. COMPLETED REPAIR TO RT PARTITION DOUBLER ON FRAME 61 IAW ERS-EM-53MR-1291.

Part: HINGE — DAMAGED (RUDDER) · airframe 38,399 hrs · 34,898 cycles

VERTICAL STAB TO RUDDER 1 LOWER HINGE SHACKLE HAS PLAY. INSTALLED NEW HINGE FITTING ASSEMBLY IAW SRM 51-40-02 & ERS-EM-5500-287.

Part: HINGE — RATCHETING (RUDDER) · airframe 38,399 hrs · 34,898 cycles

RUDDER 1 UPPER CONTROL ROD. BEARING ON VERTICAL STAB IS RACHETING. R & R RUDDER 1 UPPER CTR HINGE FITTING ASSEMBLY IAW SRM 51-40-02.

Part: BEARING — DISLODGED (RUDDER) · airframe 38,399 hrs · 34,898 cycles

RUDDER 1 LOWER CONTROL ROD BEARING ON VERTICAL STAB RETAINER RING IS DISLODGED. R & R RUDDER 1 LOWER HINGE FITTING ASSEMBLY IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,399 hrs · 34,898 cycles

FRAME 68 HAS A CRACK IN IT BETWEEN STRINGERS 14L & 15L. COMPLIED WITH PERMANENT REPAIR IAW ERS-EM-53MR-1271.

Part: HINGE FITTING — WORN (RUDDER) · airframe 38,399 hrs · 34,898 cycles

RUDDER NR 2 UPPER HINGE FITTING BORES WORN, CTR HINGE FITTING BORES WORN, LOWER CTR HINGE FITTING BORES WORN & LOWER HINGE FITTING BORES WORN. REPLACED ALL 4 FITTINGS IAW SRM 55-40--02 & ETN EM-55-070. FITTING PN 135-16841-601. UNDRILLED FITTING ASSEMBLY PN 135-16842-601.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 38,399 hrs · 34,898 cycles

CARGO DOOR HOLD OPEN ROD RETAINER SUPPORT IS CRACKED, AFT SIDE OF FRAME 68. R & R CARGO DOOR HOLD OPEN ROD RETAINER SUPPORT IAW SRM 51-40-02.

Part: FIREWALL — CRACKED (APU BAY) · airframe 38,399 hrs · 34,898 cycles

APU FIREWALL HAS 2 CRACKS AT LT UPPER ATTACH MOUNT POINT. REPAIRED APU FIREWALL CRACKS IAW EO EM 53AD-1883.

Part: ATTACH ANGLE — CRACKED (FRAME 50) · airframe 38,399 hrs · 34,898 cycles

RIGHT WING TO FUSELAGE UPPER ATTACHMENT ANGLE HAS 2 INCH CRACK AT FRAME. REMOVED & REPAIRED RT WING TO FUSELAGE UPPER ATTACHMENT ANGLE AT FRAME 50 IAW SRM 53-23-12 & 51-40-02.

Part: SPAR — CRACKED (RT WING) · airframe 38,399 hrs · 34,898 cycles

RIGHT WING SPAR NR 3 HAS APPROX 1 INCH CRACK PROTRUDING FROM THE WIRE HARNESS HOLE. COMPLIED WITH RT WING SPAR III CRACK, PERMANENT REPAIR IAW ERS-EM-57MR-438.

Part: SKIN — CRACKED (FRAME 75) · airframe 38,399 hrs · 34,898 cycles

LEFT FUSELAGE SKIN PANEL CRACKED AT FRAME 75 BETWEEN STRINGERS 1L- 3L. REPAIRED LT FUSELAGE SKIN AT FRAME 75 IAW ERS-EM-53MR-1268.

Part: SKIN — CORRODED (FUSELAGE) · airframe 38,399 hrs · 34,898 cycles

EM-53MR-1587 PTB CTR FUSELAGE I LOWER SKIN CORROSION. COMPLIED WITH EO EM-53MR-1587 PART B AS REQUIRED.

Part: WIRE — BROKEN (CABIN) · airframe 38,399 hrs · 34,898 cycles

CEILING PANEL 253CLC HAS A BROKEN EMER LIGHT WIRE. REPLACED CONNECTORS AT SP9124 & SP9125 IAW SWPM 20-21-00. SEE BOW 187014 FOR OPERATIONS CHECK OF EMER LIGHTS.

Part: SIGN — INOPERATIVE (CABIN) · airframe 38,399 hrs · 34,898 cycles

LEFT AFT EMER EXIT SIGN ON LT ESCAPE HATCH TRIM SHROUD PANEL 251CLW IS INOPERATIVE. R & R INOPERATIVE LT AFT EMER EXIT SIGN ON LT ESCAPE HATCH TRIM SHROUD PANEL 251CLW IAW AMM 33-50-14. OPERATIONS CHECKED GOOD. SEE ZONE 200 WC 06-400-24 FOR INSTALL OF PANEL 251.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 38,331 hrs · 34,831 cycles

EMERGENCY LIGHT ON AFT GALLEY WALL INOPERATIVE. R & R NR 3 EMER LIGHT INVERTER. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 37,522 hrs · 34,180 cycles

EICAS MSG, FLAP LOW SPEED, PRESENT IN CRUISE FLIGHT AT FL300 FLAP INDICATION IS BOXED YELLOW & DASHES REPEAT DISCREPANCY IAW LOG PAGES 3708414, 3708431, 3708444 & 3708449. R & R FECU IAW 27-53-02. OPERATIONS CHECKED GOOD IAW AMM TR 27-53-00.

Part: DRIVE UNIT — FAILED (TE FLAPS) · airframe 37,493 hrs · 34,159 cycles

PASSING THRU FL 200 BLUE ADVISORY FLAP LOW SPEED MSG ON EICAS. WHEN MAKING FINAL APPROACH & SELECTING FLAPS 9 STILL HAD FLAPS 0 INDICATING ON EICAS. RMU SHOWED FLAPS 9 & IT COULD BE FELT IN A/C CONTROLS. FLAPS WERE EXTENDED TO 22 WITH A VISUAL INSPECTION THAT THEY WERE IN CORRECT POSITION, NO FLAP FAIL MESSAGE PRESENTED. FOUND CHANNEL NR 1 INOPERATIVE. REPLACED THE FLAP POWER DRIVE UNIT IAW AMM 27-53-04.ACCOMPLISHED FLAP ZERO DEGREE RIGGING IAW AMM 27-53-04. FLAP SYSTEM OPS CHECKED GOOD.

Part: GAUGE — BROKEN (BRAKE SYSTEM) · airframe 37,102 hrs · 33,833 cycles

EMERGENCY PARKING BRAKE NITROGEN ACCUMULATOR GAUGE BROKEN & MISSING PARTS. R & R IAW AMM 32-44-04. TESTED SATISFACTORY.

Part: SOCKET — BURNED (CABIN) · airframe 36,882 hrs · 33,653 cycles

DURING TAXI FLIGHT ATTENDANT REPORTS BURNING SMELL IN GALLEY. INSPECTED GALLEY AREA & FOUND ALL LIGHTS & SYS WORKING PROPERLY. FOUND 1A CEILING LIGHT SOCKET BURNT. REMOVED LAMPS IAW AMM 33-21-06 & DEFERRED IAW MEL 33-2.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED SYS) · airframe 36,593 hrs · 33,435 cycles

NR 2 BLEED LEAK ON EICAS & BLEED. NR 2 BUTTON RED FOR 10 SEC DURING CLIMB OUT. PERFORMED OPS CHECKED GOOD IAW AMM 36-00-00-700-803-A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 36,591 hrs · 33,433 cycles

BLEED 2 LEAK ON EICAS WITH LEAK ILLUMINATED ON BLEED 2 BUTTON. OPERATIONS CHECKED GOOD IAW AMM 36-11-05. OK FOR SERVICE.

Part: CRADLE — DETACHED (COCKPIT) · airframe 36,437 hrs · 33,316 cycles

CAPTAIN'S FLASHLIGHT HOLDER ASSEMBLY FELL OFF. R & R CAPTAINS FLASHLIGHT & HOLDER ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 36,106 hrs · 33,012 cycles

FLAP FAIL, TROUBLE SHOT IAW FIM TASK 27-51-00-810-816-A. TRANSITORY COND OF FLAP CONTROL SYS. OPERATIONS CHECKED GOOD IAW AMM 27-51-00-700-801A.

Part: SENSOR — FAULTY (TE FLAP) · airframe 36,108 hrs · 33,013 cycles

FLAP FAIL, TRANSFERRED TO NRWC 616-ORD-02038. TROUBLE SHOT & FOUND LT FLAP VELOCITY SENSOR MOUNTING SCREWS LOOSE & ALSO FAILED WIRING CHECKS. R & R LT FLAP VELOCITY SENSOR IAW MM 27-51-12. OPERATIONS CHECKED GOOD IAW MM 27-51-00.

Part: STRAP — BROKEN (SMOKE GOGGLES) · airframe 35,971 hrs · 32,896 cycles

FIRST OFFICER`S SMOKE GOGGLE STRAP BROKEN. INSTALLED FIRST OFFICER'S SMOKE GOGGLE STRAP AS REQUIRED.

Part: UPLOCK — FAILED (NLG) · airframe 35,877 hrs · 32,819 cycles

AFTER TAKEOFF WE HEARD A BANGING CONTINUOUSLY, SOUND COMING FROM THE NOSE GEAR. SUSPECT NOSE TIRE OR GEAR DOOR, RECEIVED NOSE IN TRANSIT LIGHT INTERMITTENTLY. LG EXTENDED NORMALLY. R & R NLG UPLOCK BOX IAW AMM 32-33-07. PERFORMED OPERATIONAL CHECK OF LG EXTENSION & RETRACTION IAW 32-30-00, NO DEFECTS FOUND.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 35,807 hrs · 32,773 cycles

DURING CLIMB BETWEEN FL 270 & FL 350 BOTH CAPTAIN & FIRST OFFICER STARTED SMELLING WHAT APPEARED TO BE ELEC BURNING. CALLED FLIGHT ATTENDANT & SHE SMELLED IT TOO. AT FL 350 SMOKE STARTED COMING OUT OF THE FWD SIDE OF BOTH DV WINDOWS. THE ON SHORT FINAL BOTH RMU FAILED & COME BACK UP AGAIN. FLIGHT CONDITIONS AT ALTITUDE WERE BUMPY & IMC WITH SOME RAIN. PERFORMED ENG RUNS IAW AMM 71-00-01 & COMPLIED WITH ETN- EM-72-034, NO SMELL DETECTED IN THE COCKPIT AT THIS TIME. OPERATIONS CHECKED GOOD.

Part: HOLDER — LOOSE (FLASHLIGHT) · airframe 35,492 hrs · 32,535 cycles

CAPTAIN`S FLASHLIGHT LOOSE IN CHARGING CRADLE, FELL OUT UPON LANDING. R & R HOLDER ASSEMBLY IAW AMM 33-50-16, OPERATIONS CHECKED GOOD, NO DEFECT NOTED.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 35,475 hrs · 32,516 cycles

LAVATORY SMOKE WARNING OCCURRED IN DESCENT THRU 16000 FT NO SMOKE OR FIRE NOTED BUT WARNING STILL ILLUMINATED. FLIGHT CREW PLACARDED IAW MEL 26-2.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 35,365 hrs · 32,437 cycles

CABIN FLASHLIGHT AFT WILL NOT CLIP INTO HOLDER. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT AND HOLDER IAW EMB AMM 33-50-16 OPS CHECK GOOD MEL RESTORED

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 35,171 hrs · 32,290 cycles

FIRST OFFICER’S FLASHLIGHT INOPERATIVE. RELAMPED FIRST OFFICER`S FLASHLIGHT AS REQUIRED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,451 hrs · 31,692 cycles

THE CREW REPORTED THEY WERE UNABLE TO ROTATE ON TAKEOFF ROLL WITH YOKE FULL AFT. HIGH SPEED ABORT PERFORMED. THE ACFT WAS REMOVED FROM SERVICE. ELEVATOR DEFLECTION CHECK COMPLIED WITH IAW 27-31-00 ALSO OPS CHECK OF AURAL WARNING UNIT IAW AMM 31-51-00. ELEVATOR DEFLECTION CHECKED GOOD IAW AMM 27-31-00. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 34,350 hrs · 31,609 cycles

RIGHT WING AFT OVERWING EMERGENCY LIGHT FAILS TO ILLUMINATE. FOUND CORROSION ON BULB SOCKET AND WIRES. REPLACED RT WING AFT OVERWING EMERGENCY LIGHT IAW AMM 33-50-07-000/400-802-A. OPC GOOD IAW AE WC 33-700-17.

Part: SENSOR — INOPERATIVE (TE FLAPS) · airframe 34,249 hrs · 31,514 cycles

CREW REPORTED DURING DESCENT, EXPERIENCED A FLAP AND SPOILER MALFUNCTION. PERFORMED THE PROCEDURES IAW AOM VOL 1, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R THE LT & RT FLAP VELOCITY SENSOR IAW AMM 27-51-12. THE OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,237 hrs · 31,505 cycles

EMERGENCY LIGHT BATTERY CHARGER DOESN'T CHARGE. REMOVED BATTERY CHARGER.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,237 hrs · 31,505 cycles

BATTERY DID NOT CHARGE. REMOVED BATTERY.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,237 hrs · 31,504 cycles

CENTER FUSELAGE SKIN CORROSION, FRAME 17-19, STRINGERS 21L-21R. INSTALLED DOUBLER IAW EO-EM-53MR-2179.

Part: RIB — CRACKED (LT WING) · airframe 34,237 hrs · 31,504 cycles

LEFT RIB 5 CRACKED AT AFT LIGHTNING HOLE. RIB REPAIRED IAW EO EM-57MR-699.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 34,278 hrs · 31,541 cycles

EMERGENCY PROXIMITY FLOOR LIGHT WIRE NICKED AT FR 24 - 25 LT SIDE. REPAIRED WIRES IAW SWPM 20-21-00 SECTION 4A THRU B (2)D.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 34,278 hrs · 31,541 cycles

EMERGENCY LIGHT CONNECTOR AT FLOOR PLANEL 251DF BROKEN OFF. INSTALLED CONNECTOR IAW SWPM 20-21-00, STEP 5.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,278 hrs · 31,541 cycles

EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY AND CHARGER NR 3 IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,193 hrs · 31,466 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT ABOVE SEAT 7A INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE EMERGENCY LIGHT LAMP AT 7A IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 1A) · airframe 34,114 hrs · 31,402 cycles

DURING MX INSPECTION, FOUND SEAT 1A EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R SEAT 1A EMERGENCY LIGHT IAW AMM TASK 33-50-12. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED. ACFT RETURNED TO SERVICE.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 33,638 hrs · 31,025 cycles

ON FLIGHT 2788 THE CREW REPORTED A BURNING SMELL IN GALLEY. A PRONG ON THE BACK OF COFFEE JUG APPEARED BLACKENED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COFFEE JUG. THE OPERATIONAL CHECK WAS GOOD, NO SMELL NOTED AFTER REPLACED PER EMB CMM 25-32-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — DEFECTIVE (SPEED BRAKE) · airframe 33,553 hrs · 30,953 cycles

ON FLIGHT 4333 THE CREW REPORTED THAT DURING CLIMB ACCELERATING FROM 270KTS TO 300 KTS, A STRONG VIBRATION FELT THROUGH AIRFRAME, W COCKPIT AND THROUGH CONTROL WHEEL. AS A/C CLIMBED THROUGH APPROX 17,000 VIBRATION SLOWLY DECREASE TO MINIMAL VIBRATION AT CRUISE VIBRATION SLOWLY INCREASED DURING DESENT GETTING STRONGER AS AIRCRAFT DEPRESSURIZED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH VIBRATION DETAIL VISUAL INSPECTION IAW W/C 12-200-01. FOUND LEFT OUTBOARD SPOILER WITH PLAY FROM ACTUATOR TOP AREA. REMOVED AND REPLACED THE LEFT SPEED BRAKE ACTUATOR IAW EMB 27-62-02. THE OPERATIONAL CHECK AND LEAK CHECK WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LENS — CRACKED (EXTERIOR) · airframe 33,174 hrs · 30,658 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EXTERIOR EMERGENCY LIGHT LENS CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXTERIOR EMERGENCY LIGHT ASSEMBLY IAW EMB AMM TASK 33-50-09-000-802-A AND 33-50-09-400-802-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 32,718 hrs · 30,271 cycles

DURING MANITENANCE INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT CHARGER HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE FIRST OFFICER’S FLASHLIGHT CHARGER HOLDER IAW EMB145 AMM 33-50-16. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,585 hrs · 30,155 cycles

DURING MAINTENANCE INSPECTION FOUND THE EXIT LOCATING SIGN AT EMERGENCY EXIT ROW INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 INVERTER IAW EMB AMM 30-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,362 hrs · 29,955 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURN TO SERVICE.

Part: BLEED VALVE — FAULTY (NR 1 ENGINE) · airframe 32,168 hrs · 29,806 cycles

ON FLIGHT 3387 THE CREW REPORTED, RECEIVED A BLEED 1 VALVE FAIL DURING CLIMBOUT 17000 DISAPPEARED IN CRUISE REAPPEARED ON DESCENT AT 18700 ICING DURING CLIMBOUT, NO ICE DURING DESCENT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED SERVICEABLE NUMBER 1 ENGINE BLEED VALVE IAW EMB MM 36-11-05. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,019 hrs · 29,698 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT AT OVERHEAD MIDDLE AISLE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB ON MIDDLE AISLE OVERHEAD EMERGENCY LIGHTING IAW EMB145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 31,928 hrs · 29,617 cycles

DURING MAINTENANCE INSPECTION, FOUND THE RIGHT EMERGENCY LIGHT INOPERATIVE ON OVERWING LATERAL PANEL FORWARD SIDE. THE AICRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT EXTERNAL EMERGENCY LIGHT ASSEMBLY ON THE OVERWING LATERAL PANEL IAW AMM 33-50-10. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 31,928 hrs · 29,617 cycles

DURING B INSPECTION, FOUND THE RIGHT WING RIB NR 5 CRACKED AT CENTER LIGHTNING HOLE. COMPLIED WITH AEA EO EM-57MR-595. AIRCRAFT RETURNED TO SERVICE. "MAJOR REPAIR".

Part: LAMP — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 31,928 hrs · 29,617 cycles

DURING B INSPECTION, FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EMERGENCY LIGHT ON OVERWING LATERAL PANEL IAW AMM 33-50-10. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INTERMITTENT (FWD CABIN) · airframe 31,627 hrs · 29,369 cycles

ON FLIGHT 3242, THE CREW REPORTED THE FLIGHT ATTENDANT FORWARD FLASHLIGHT CHARGE LIGHT WORKED INTERMITTENTLY. TROUBLESHOT AND FOUND FLASHLIGHT LOOSE IN THE CRADLE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 31,378 hrs · 29,164 cycles

DURING B INSPECTION, FOUND EMERGENCY EXIT LIGHT ON AISLE AFT SIDE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT AND FOUND LOOSE WIRE ON SIGN, CONNECTED WIRE. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — DAMAGED (FWD CABIN) · airframe 31,362 hrs · 29,149 cycles

ON FLIGHT 3359, THE FLIGHT ATTENDANT REPORTED THE FORWARD FLASH LIGHT CRADLE WILL NOT HOLD THE FLASH LIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLASH LIGHT CRADLE IAW EMB CMM 25-61-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,036 hrs · 28,886 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LIGHT FLOOR STRIP AT EMERGENCY EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT EMERGENCY EXIT IAW EMB 145 AMM 33-50-12-000-801-A/33-50-12-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — INOPERATIVE (CABIN) · airframe 30,748 hrs · 28,656 cycles

DURING B-INSPECTION FOUND THE CABIN OVERWING EMERGENCY EXIT AFT CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RECONNECTED LOOSE CONNECTION ON CABIN CEILING EMERGENCY LIGHT AT EMERGENCY EXIT AFT SIDE IAW AMM 33-50-15. THE EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 30,657 hrs · 30,657 cycles

DURING FLIGHT 2816 THE CREW REPORTED THE AFT CABIN FLASHLIGHT CHARGE LIGHT INTERMITENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT HOLDER IAW EMB 145 AMM33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,598 hrs · 28,547 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BATTERY PACK NR 1 DRAINED. REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY ASSEMBLY IAW EMB-145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 30,347 hrs · 28,358 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT ON AFT GALLEY WALL INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD IAW AE W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,217 hrs · 28,271 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY EXIT SIGN LIGHTING IN FRONT OF SEAT 3B INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT SIGN IN FRONT OF SEAT 3B IAW EMB 145 AMM 33-50-14. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 29,929 hrs · 28,066 cycles

DURING MAINTENANCE VISIT FOUND THE EMERGENCY LIGHT SIGN INOPERABLE IN ROW 12 CEILING SIGN AFT OF SIGN. THE AIRCRAFT WAS REMOVED FROM SERVICE. TESTED EMERGENCY LIGHT IAW EMB AMM 33-50-00. NO DEFECTS FOUND. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 29,926 hrs · 28,064 cycles

ON FLIGHT 2794 THE CREW REPORTED THE NR 1 FUEL GAUGE GOES TO DASHES AND FUEL 2 LOW LEVEL WARNING DISPLAYS. THE AIRCRAFT WAS REMOVED FROM SERVICE. NR 1 FUEL QUANTITY DISPLAYED ON MFD AND PFD. NO MAINTENANCE REQUIRED AT THIS TIME. PERFORMED AN OPERATIONAL CHECK IN REFERENCE TO EMB 145 AMM 28-41-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: YOKE — CRACKED (LT PYLON) · airframe 29,905 hrs · 28,050 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT PYLON FORWARD LOWER YOKE CRACKED ABOVE LOWER ENGINE MOUNT FORWARD BOLT HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH EO EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 29,982 hrs · 28,105 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT STRIP REMOVABLE SPLICE CONNECTORS (A/C SIDE) AT POSTIONS 3 AND 6 DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED EMERGENCY LIGHT STRIP REMOVABLE SPLICE CONNECTORS (A/C SIDE) AT POSTIONS 3 AND 6 IAW EMB 145 WM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — INOPERATIVE (GALLEY) · airframe 29,871 hrs · 28,023 cycles

FOR FLIGHT 9301 THE CREW REPORTED THAT AS THEY PARKED AT GATE THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN GALLEY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT BALLAST RT8426 IAW AMM CH 33-21-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,634 hrs · 27,850 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AISLE EMERGENCY LAMP NR 3 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 3 AISLE EMERGENCY LAMP IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — SHORTED (APU) · airframe 29,452 hrs · 27,722 cycles

ON FLIGHT 2838 THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN COCKPIT AND CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED APU HARNESS DUE TO LIGHTNING STRIKE IAW EMB 145 AMM 24-34-00 REF NRWC 616-DFW-00583 FOUND APU HARNESS SHORTED DUE TO LIGHTNING STRIKE AFTER HARNESS CHANGE PERFORMED ETN EM-72-034R1 WITH NO DEFECTS OR ODORS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,027 hrs · 27,390 cycles

FOR FLIGHT 2712 MAINTENANCE REPORTED CENTER CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CENTER EMERGENCY LIGHT IAW EMB 145 AMM 33-50-08. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE — DISINTEGRATED (MLG) · airframe 26,455 hrs · 25,491 cycles

ON FLIGHT 3915 AFTER LANDING AND TAXIING TO THE GATE A RAMPER REPORTED TO MAINTENANCE THAT THE NR 3 BRAKE WAS ON FIRE. ON ARRIVAL BY MAINTENANCE TO THE AIRCRAFT THE BRAKE FIRE HAD EXTINGUISHED. THE BRAKE HAD DISINTEGRATED. ALSO THE BRAKE LINES BURNED AND HAD HEAT DAMAGED. CRASH, FIRE AND RESCUE WAS NOT CALLED. PASSENGERS HAD ALREADY DEPLANED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETE DETAILED INSPECTION OF THE RIGHT MAIN LANDING GEAR IAW EMB AMM 5-50-16. NO DEFECTS NOTED. REMOVED AND REPLACED THE NR 3 MAIN LANDING GEAR BRAKE ASSY IAW EMB CARD 32-600-14. REMOVED AND REPLACED THE NR 3 HYDRAULIC BRAKE HOSES IAW ELEB CMM 32-10-01. LEAK TEST GOOD. REMOVED AND REPLACED THE NR 3 MAIN LANDING WHEEL ASSY IAW EMB CARD 32-700-11. REMOVED AND REPLACED THE NR 4 BRAKE ASSEMBLY IAW W/C 32-600-14. REMOVED AND REPLACED THE NR 4 MLG WHEEL ASSEMBLY IAW W/C 32-700-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CABLE — LACK OF LUBE (PARKING BRAKE) · airframe 25,047 hrs · 24,384 cycles

PRIOR TO TAKEOFF FOR FLIGHT 3868 THE CREW DETERMINED THAT THE EMERGENCY PARKING BRAKE WOULD NOT ENGAGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED THE CABLE IN THE MECHANISM NOSE COMPARTMENT, LUBED THE PARKING BRAKE HANDLE IAW EMB 145 AMM 32-44-10. THE OPERATIONAL CHECK WAS GOOD, NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,924 hrs · 24,282 cycles

DURING MAINTENANCE BASE INSPECTION, FOUND LEFT OMEGA BEAM HAS CORROSION BETWEEN FRAMES 24 AND 25 AROUND CROSS MEMBER ATTACHMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM WITH A DOUBLER REPAIR IAW SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,924 hrs · 24,282 cycles

DURING MAINTENACE BASE INSPECTION, FOUND THE CARGO DOOR CUTOUT FORWARD "L" SHAPE NEAR THE BOTTOM LOWER CORNER TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM WITH A DOUBLER REPAIR IAW EMBRAER STRUCTURAL REPAIR MANUAL 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,924 hrs · 24,282 cycles

DURING THE MAINTENANCE BASE INSPECTION, FOUND THE LEFT OMEGA BEAM HAS CORROSION AT FRAME 20 AROUND CROSS MEMBER ATTACHMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM WITH A DOUBLER REPAIR IAW EMB STRUCTURAL REPAIR MANUAL 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,924 hrs · 24,282 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OMEGA BEAM HAS CORROSION AT FRAME 29 AROUND CROSS MEMBER ATTACHMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT OMEGA BEAM AT FRAME 29 WITH DOUBLER REPAIR IAW SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,924 hrs · 24,282 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CENTER OMEGA BEAM HAS CORROSION BETWEEN FRAMES 24 AND 25, AROUND CROSS MEMBER ATTACHMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE CENTER OMEGA BEAM WITH DOUBLER REPAIR IAW SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — NICKED (AILERON) · airframe 24,924 hrs · 24,282 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AILERON ACTUATOR FITTING TO HAVE SEVERAL NICKS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 24,924 hrs · 24,282 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 65 RIGHT TO HAVE TOOLING MARKS BEYOND STRUCTURAL REPAIR MANUAL LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED TOOLING MARKS IAW AEAI ENGINEERING ORDER EM-53MR-1449. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,728 hrs · 23,155 cycles

DISC - DURING PREFLIGHT FOR FLIGHT 4066 DAMAGE FROM LIGHTNING STRIKE. AIRCRAFT REMOVED FROM SERVICE. FOUND CORROSION AND CRACK IN FUSELAGE BETWEEN FRAME 13 AND 14 AND BETWEEN STRINGER 20R AND 21R. AIRCRAFT INSPECTED AND FERRIED TO MQT FOR PERMANENT REPAIR. MAINTENANCE REMOVED DAMAGED AREA AND REPLACED WITH NEW STRINGER 21R SPLICE AND SKIN PANEL IAW EMBRAER SRM 51-40-02, 53-00-03 AND AE ENGINEERING ORDER EM-53MR-1307. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,728 hrs · 23,155 cycles

DURING PREFLIGHT, DAMAGE FROM LIGHTNING STRIKE NOTED. MX CALLED TO PERFORM LIGHTNING STRIKE INSP, FOUND CORROSION AND CRACK IN FUSELAGE BETWEEN FRAME 13 AND 14 AND BETWEEN STRINGER 20R AND 21R. ACFT INSPECTED AND FERRIED FOR PERMANENT REPAIR.

Part: WIRE — FAILED (WINDOW DEICE)

ON FLIGHT 3401 ON DESCENT AT FL330, CREW REPORTED A ELECTRICAL BURNING ODOR AND SAW SMOKE COMING FROM 3 SPOTS ON THE WINDSHIELD. AIRCRAFT LANDED SAFELY. AIRCRAFT REMOVED FROM SERVICE. FOUND THE P LEAD ON THE FOS WINDOW INSULATION MELTED ISSUED MEL 3023.

Part: TERMINAL — DAMAGED (WINDSHIELD) · airframe 23,378 hrs · 22,848 cycles

ON FLIGHT 3401, ON DESCENT AT FL330, CREW REPORTED A ELECTRICAL BURNING ODOR AND SAW SMOKE COMING FROM 3 SPOTS ON THE WINDSHIELD. AIRCRAFT LANDED SAFELY. AIRCRAFT REMOVED FROM SERVICE. FOUND THE P LEAD ON THE FOS WINDOW INSULATION MELTED ISSUED MEL 3023. FOUND CONNECTOR AT WINDSHIELD (FO) DAMAGED REPLACED TERMINAL END ON POWER WIRE AT CONNECTOR P IAW EMB SPWM 20-50-01. OPS CHECK GOOD IAW EMB145 AMM 30-41-00. THIS RESTORED MEL 30-23. AIRCRAFT RETURNED TO SURVIVE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 22,360 hrs · 21,936 cycles

ON FLIGHT 3389 CREW REPORTED SMOKE IN THE COCKPIT WITH BURNING ELECTRICAL ODOR AT GATE WITH PASSENGERS LOADED. AIRCRAFT REMOVED FROM SERVICE. PERFORMED ABNORMAL ODOR/SMOKE CHECK, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: COWLING — OPEN (NR 1 ENGINE) · airframe 20,627 hrs · 20,401 cycles

ON FLIGHT 4154, CREW REPORTED ENGINE VIBRATION IN CRUISE FLIGHT. PASSENGER REPORTED HEARING A LOUD BOOM NOISE FROM THE ENGINE IN FLIGHT. UPON LANDING IN ORD, THE TOWER REPORTED THAT EAGLE SHOULD CHECK THE NR 1 ENGINE DUE TO OBVIOUS DAMAGE AS SEEN DURING TAXI IN TO ORD. UPON POST-FLT INSPECTION, IT WAS DISCOVERED THAT THE NR 1 ENGINE COWL HAD OPENED IN FLIGHT AND PARTS HAD SEPARATED THE AIRCRAFT AND DAMAGE TO THE ENGINE HAD OCCURRED.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 20,136 hrs · 19,929 cycles

STRONG PLASTIC MELTING OR BURNING SMELL COMING FROM GALLEY AREA. FOUND BALLAST OVER GALLEY GOING OUT REMOVED AND REPLACED BALLAST IAW EMB AMM 33-28-07. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — INOPERATIVE (BRAKE TEMP) · airframe 19,677 hrs · 19,579 cycles

ON TAKEOFF, CREW OBSERVED "BRAKE OVERHEAT" MESSAGE ON EICAS WITH THE NUMBER 2 BRAKE TEMP INDICATION INOP. CREW ABORT TAKEOFF AND RETURN TO THE GATE. C/A ISSUED MEL 32-03. MTX REMOVED AND REPLACED NR 2 BRAKE TEMP SENSOR IAW EMB 145 AMM 32-47-01. OP CK GOOD MEL 090962-C. RESTORED AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 19,677 hrs · 19,579 cycles

BRAKE OVERHEAT MESSAGE ON EICAS WITH THE NUMBER 2 BRAKE TEMP INDICATION INOP. CREW ELECTED TO ABORT TAKEOFF AND RETURN TO THE GATE. ISSUED MEL 32-03.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG) · airframe 19,269 hrs · 19,260 cycles

LANDING GEAR NO RETRACT, RETURNED TO DFW. FOUND PROXIMITY SENSOR OUT OF ADJUSTMENT. ADJUSTED RIGHT MAIN LANDING GEAR NUMBER ONE AND TWO WEIGHT ON WHEEL PROXIMITY SENSORS IAW EMB 32-63-05. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 18,623 hrs · 18,654 cycles

MAIN ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. RECONNECTED DOOR LIGHT IAW EMB AMM 33-50-06. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: ACTUATOR — FAULTY (NR 3)

ORD - FLT 9329 - FLAPS SELECTED FROM 9 DEGREE TO 22 DEGREE GOT `FLAP FAIL` EICAS MESSAGE AND INDICATOR REMAINED 9 DEGREE. FOLLOWED AOM PROCEDURES FOR LANDING, FLAPS WOULD NOT RETRACT FROM 9 DEGREE AFTER LANDING. REMOVED AND REPLACED FLAP DRIVE ACTUATOR, IAW EMB AMM 27-57-09. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LEVER — FAULTY (TE FLAPS)

FLAP FAIL MESSAGE ON APPROACH, PERFORMED UNEVENTFUL ZERO DEGREE FLAP LANDING. REMOVED AND REPLACED FLAP SELECTOR LEVER. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. (M)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS)

ORD - 4449 - SELECTED FLAPS TO 9 DEGREES RECEIVED FLAPS FAILED MESSAGE ON EICAS, EXECUTED AIRCRAFT OPERATING MANUAL CHECKLIST AND LANDED UNEVENTFUL WITH FLAPS ZERO. TROUBLESHOT PER FAULT ISOLATION MANUAL. RESET FLAP SYSTEM, OPERATIONAL CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: TIP CAP — FLUTTER (RT STABILIZER)

DFW - FLT 3538 - ELEVATOR TAIL FLUTTER AT 300KTS AND ABOVE, BETWEEN 10,000 AND 20,000. ALSO IN DESCENT SLOWING THROUGH 250 KTS. REPLACED UPPER AND LOWER RUDDER 1 ATTACHMENT HINGES, RIGHT HORIZONTAL STABILIZER TIP. COMPLETED ALL PARTS OF EO EM-55AD-207R4. ADJUSTED RUDDER DEFLECTION ECCENTRIC PIN TO ZERO POSITION ALONG WITH VIBRATION WORK CARD. FITTING P/N 120-38377-001, STABILIZER TIP P/N 145-35900-404, SPACER P/N 145-25626-001, BUSHING P/N 120-33582-005. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BUSHING — WORN (ELEVATOR)

ELEVATOR TAIL FLUTTER AT 300KTS AND ABOVE. BETWEEN 10,000 AND 20,000 ALSO IN DESCENT SLOWING THROUGH 250 KTS. REPLACED UPPER AND LOWER RUDDER 1 ATTACHMENT HINGES, RT STABILIZER TIP. COMPLETED ALL PARTS OF EO. ADJUSTED RUDDER DEFLECTION ECCENTRIC PIN TO ZERO POSITION ALONG WITH VIBRATION WORK CARD. 1(FITTING, PN 120-38377-001), 2(STABILIZER TIP, PN 145-35900), 3(SPACER, PN 145-25626-001), 4(BUSHING, PN 120-33582-005), 5(BUSHING, PN 120-33582-005). AC RETURNED TO SERVICE. (K)

Part: SILL — CORRODED (FWD SERVICEDOOR)

DURING CPCP INSPECTION FOUND SERVICE DOOR FWD SILL CORRODED. REPLACED FWD SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

DURING CPCP INSPECTION FOUND RT FWD IB SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

DURING CPCP INSPECTION FOUND LT FWD IB SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: GUSSET — CORRODED (CABIN)

DURING CPCP INSPECTION FOUND CORROSION ON GUSSET ON RT HAT BEAM AT FRAME 20. REPLACED GUSSET IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

DURING CPCP INSPECTION FOUND RT FWD OB SEAT TRACK IS CORRODED. REPLACED SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2

DURING CPCP INSPECTION FOUND RT IB SEAT TRACK FROM FRAME 36-47 CORRODED. REPLACED SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

DURING CPCP INSPECTION FOUND LT IB SEAT TRACK BETWEEN FRAMES 24-30 CORRODED. REPLACED SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

DURING CPCP INSPECTION FOUND RT OB SEAT TRACK BETWEEN FRAMES 30-36 IS CORRODED. REPLACED SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SILL — CORRODED (CABIN)

DURING CPCP INSPECTION FOUND SERVICE DOOR, FORWARD SILL PLATE CORRODED. INSTALLED NEW SILL PLATE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

DURING CPCP INSPECTION FOUND LT IB SEAT TRACK BETWEEN FRAME 30 AND 36 CORRODED. INSTALLED A NEW SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

DURING CPCP INSPECTION FOUND RT IB SEAT TRACK BETWEEN FRAME 30 AND 36 CORRODED. INSTALLED A NEW SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: FRAME — GOUGED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, FRAME 81 WAS FOUND GOUGED BELOW SRM LIMITS. BLENDED THE GOUGE AND PERFORMED NDT INSPECTION FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB STATEMENT IC2003-145/4017 DATED NOV 27, 2003. (M)

Part: SIGN — INOPERATIVE (CABIN)

DFW - DURING PHASE INSPECTION MAINTENANCE REPORTED THE EMERGENCY EXIT SIGN AT ROW 3BC TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN AT ROW 3BC IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

ORD - DURING FLIGHT CREW REPORTED THE BAGGAGE SMOKE LIGHT FLICKERED ON. CREW DISCHARGED FIRE BOTTLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. FIRE BOTTLE WAS ALSO REPLACED. (M)

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)

JAN - FLT 3479 - FLIGHT CREW REPORTED CABIN PRESSURE UNCONTROLABLE AT FL350. EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED DIGITAL CONTROLLER AND RESECURED THE RAM AIR DUCT IAW EMB MM. PERFORMED FCF WHICH WAS FOUND TO BE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING AN IMBV MAINTENANCE, FOUND CORROSION ON SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. PERFORMED NDT INSPECTION, NO DEFECTS NOTED. FABRICATED THREE REPAIR DOUBLERS. REPAIR DONE IAW EMB GST-1552/02M ITEM NR 4, AND STANDARD SRM PRACTICES. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - DURING IN IMBV MAINTENANCE, FOUND DENT ON LOWER FUSELAGE BETWEEN FRAMES 64 AND 65, AND STRINGERS 21L AND 21R. REMOVED DAMAGED SKIN BY CUT OUT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB 145 (SRM 145/1142, CHAPTER 53, REV 18, GST-1618/02, AND STANDARD SRM PRACTICES. (M)

Part: DOUBLER — CORRODED (AFUSELAGE)

ABI - DURING AN IMBV MAINTENANCE, FOUND CORROSION ON LEFT OMEGA BEAM, PREVIOUS REPAIR, AT FRAME 20. REMOVED PREVIOUS REPAIR, CORROSION LIMITED TO PREVIOUS REPAIR. FABRICATED A DOUBLER, PLATE AND SHIMS. REPAIR DONE IAW EMB145 SRM 145/1142, CHAPTER 53 REV 18, 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: BEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV MAINTENANCE, FOUND FOUR CORRODED NUTPLATES AT PILOTS WINDSHIELD LOWER OUTBOARD CORNER. REMOVED CORRODED NUTPLATES. REAMED BEAM BOLTS HOLES TO .313 INCH TO REMOVE CORROSION. REPAIR DONE IAW EMB GST-1578/02-B, EMB 145 (SRM 145/1142, CHAPTER 51 REV 18) 51-40-02, 51-20-03, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

DURING AN IMBV MAINTENANCE FOUND STRINGER 19L CHAFED. BLENDED CHAFE. PERFORMED NDT INSPECTION, NO DEFECTS. FABRICATED DOUBLER AND SHIMS. REPAIR DONE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV MAINTENANCE FOUND CORROSION ON GALLEY UNDER FLOOR CENTER BEAM. REMOVED CORRODED GALLEY CENTER BEAM. INSTALLED NEW CENTER BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV MAINTENANCE FOUND CORROSION ON FORWARD DIGITAL. REMOVED CORROSION BY CUT OUT. FABRICATED A REPLACEMENT STRAP, TWO DOUBLERS AND SHIMS. REPAIR DONE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (LAVATORY)

ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36132, CENTER BEAM GUSSET UNDER LAVATORY CORRODED. BLENDED CORROSION, ACCEPTED AS IS IAW EMB GST-1552/02. RESTORED PROTECTIVE FINISH IAW EMB145 CPM 51-21-04, 51-21-05, AND 51-21-06. (M)

Part: FLOOR SUPPORT — CORRODED (LAVATORY)

ABI - THIS IS A LEVEL 2 FINDING IN CRIC NR 36131, RIGHT BEAM GUSSET UNDER LAVATORY CORRODED. BLENDED CORROSION AND ACCEPTED AS IS IAW EMB GST-1552/02. (M)

Part: BEAM — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36129, RIGHT CENTER OMEGA BEAM HAS CORROSION FROM FRAME 23 TO 26. BLENDED CORROSION AND ACCEPTED AS IS IAW EMB GST-1552/02. (M)

Part: BEAM — CORRODED (GALLEY)

ABI - THIS IS FROM A LEVEL 2 FINDING ON CRIC NR 36128, LEFT OMEGA BEAM HAS CORROSION FROM FRAME 23 TO 26. INSPECTED AND ACCEPTED AS IS IAW EMB GST-1552/02. RESTORED PROTECTIVE COAT IAW CPM 51-21-06. (M)

Part: CROSSBEAM — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36125, GALLEY CROSSBEAM AND PROFILE CORRODED. INSTALLED NEW CROSSBEAM AND PROFILE IAW EMB145 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36126, GALLEY FORWARD DIAMOND GUSSET HAD CORROSION. INSTALLED NEW FORWARD DIAMOND GUSSET IAW EMB145 SRM 51-20-03, 51-40-02 AND 51-40-06. (M)

Part: GUSSET — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36127, GALLEY AFT DIAMOND GUSSET HAS CORROSION. INSTALLED NEW GUSSET IAW EMB145 SRM 51-20-03 AND 51-40-02. (M)

Part: FLOOR SUPPORT — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36118, GALLEY CENTER BEAM GUSSET HAS CORROSION. INSTALLED NEW GALLEY CENTER BEAM GUSSET IAW EMB145 SRM 51-40-02, 51-20-03, 51-40-06. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36123, LEFT SILL IN GALLEY AREA HAS CORROSION. INSTALLED NEW SERVICEABLE SILL IAW EMB145 SRM 51-20-03, 51-40-06, AND 51-40-02. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36120, GALLEY FORWARD RIGHT SILL HAS CORROSION. INSTALLED NEW SERVICEABLE SILL IAW EMB145 SRM 51-40-02, 51-20-03. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36122, GALLEY RIGHT FAT SILL HAS CORROSION. INSTALLED NEW SERVICEABLE SILL IAW EMB145 SRM 51-40-02. (M)

Part: SUPPORT — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 36119, GALLEY RAMP SUPPORT HAS CORROSION. INSTALLED NEW RAMP SUPPORT IAW EMB145 SRM 51-20-02, 51-40-02. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FOUND ROWS 4 AND 6 EMERGENCY FLOOR LIGHTING INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT STRIP IAW AMM. OPS CHECK GOOD. (M)

Part: SEAL — LEAKING (NR 2 BLEED)

DFW - FLT 3593 - DURING CRUISE FLIGHT, CREW REPORTED NR 2 BLEED LEAK. AIRCRAFT WAS RETURNED TO DFW. MAINTENANCE REPLACED THE BLEED DUCT SEALS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — FAILED (SPOILER)

ORD - FLT 4329 - DURING TAKEOFF AT APPROXIMATELY 150-155 KNOTS CREW REPORTED PITCH TRIM FAIL ON EICAS FOLLOWED BY BOTH BACK UP SWITCHES FAILING. AT APPROXIMATELY 220 KNOTS CAPTAIN WAS ABLE TO USE BACK UP SWITCHES, WHICH OPERATED THROUGH THE REMAINDER OF THE FLIGHT. PITCH TRIM 1 FAIL LIGHT REMAINED ON AFTER LANDING. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STAB CONTROL UNIT AND SPOILER CONTROL UNIT IAW EMB MM. FUNCTIONAL CHECK FLIGHT OF AIRCRAFT WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0275. (M)

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB)

ORD - FLT 4329 - DURING TAKEOFF AT APPROXIMATELY 150-155 KNOTS CREW REPORTED PITCH TRIM FAIL ON EICAS FOLLOWED BY BOTH BACK UP SWITCHES FAILING. AT APPROXIMATELY 220 KNOTS CAPTAIN WAS ABLE TO USE BACK UP SWITCHES, WHICH OPERATED THROUGH THE REMAINDER OF THE FLIGHT. PITCH TRIM 1 FAIL LIGHT REMAINED ON AFTER LANDING. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STAB CONTROL UNIT AND SPOILER CONTROL UNIT IAW EMB MM. FUNCTIONAL CHECK FLIGHT OF AIRCRAFT WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

ORD - FLT 4261 - COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP. OPS CHECK GOOD. (X)

Part: BLEED VALVE — FAILED (NR 1 & 2 ENGINES)

ORD - FLT 4053 - DURING CLIMB-OUT, BOTH LAVATORY AND BAGGAGE SMOKE INDICATION CAME ON. AIRCRAFT RETURNED TO ORD. NO FIRE PRESENT, SMOKE WAS SMELLED AREA. REMOVED AND REPLACED BOTH ENGINE (S/N 311069 LT, 311071 RT) DUE TO BLEED AIR SYSTEM VALVES. OPS CHECK GOOD. (M)

Part: SOCKET — FAILED (GALLEY)

DFW - FLT 3663 - FLIGHT ATTENDANT REPORTS MILD BURNING ODOR IN THE GALLEY AREA. PULLED ALL THREE GALLEY CIRCUIT BREAKERS AND THE ODOR WENT AWAY. REMOVED AND REPLACED ONE AIRCRAFT SIDE HOT JUG SOCKET. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — FAILED (ROW 3BC)

ORD - FLT 4031 - EMERGENCY EXIT LIGHT ON FORWARD BULKHEAD OF ROW 3BC DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. (X)