N611AE

Part: NONE — NONE · airframe 49,459 hrs · 45,275 cycles

MEL 21-20 AUTH# 120348DM-C. ELECTRO PNEUMATIC OUTFLOW VALVE INOP DUE TO MEL 21-17 RETURN TO FIELD..PRESSURIZATION ISSUES..DECLARED EMRG AND LANDED WITHOUT FURTHER INCIDENT-C/A-REACTIVATED ELECTROPNEUMATIC OUTFLOW VALVEAS PER AMM 21-31-03-440-801A.OPS CHECK GOOD AS PER AMM 21-31-00. MEL ITEM RESTORED

Part: NONE — NONE · airframe 49,010 hrs · 44,758 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOT EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 48,802 hrs · 44,530 cycles

MEL 2532 - AUTH# 080401M-C ORIG. AML PG. 4734772 ITEM #1 AFT CABIN FA EMERGENCY FLASHLIGHT INOP-C/A-RAR AFT CABIN EMERGENCYFLASHLIGHT IAW AMM 33-50-16. OPC GOOD. MEL ITEM RESTORED.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 48,798 hrs · 44,526 cycles

CABIN AFT FA EMERGENCY FLASHLIGHT INOP.-C/A-FLIGHT CREW PLACARDED CABIN AFT FA EMERGENCY FLASHLIGHT. M PROCEDURES C/W. MEL 25-32 AUTH# 080401M-C MOC# 737389 CC# 696266

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,324 hrs · 44,007 cycles

RH UPPER OVER WING EMERGENCY LIGHT INOP-C/A-RAR RH UPPER OVER WING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10. OPC GOOD.

Part: FAN — ODOR (RECIRCULATION) · airframe 47,772 hrs · 43,429 cycles

BRIEFLEY ON TAKEOFF AND INTERMITTENTLY IN FLIGHT AN ODD SMELL WOULD COME UP IN THE COCKPIT/CABIN SMELL WAS SIMILAR TO ELECTRICAL BURNING. TRANSFERRED TO NRWC 611-DFW-03584. C/A: R & R NR 1 RECIRCULATION FAN, PER AMM 21-22-05. OPERATIONAL CHECK GOOD SWEE NRWC 611-DFW-03584 FOR ACTION TAKEN.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,735 hrs · 43,390 cycles

RT OVERWING EXIT AFT EMERGENCY LIGHT INOPERABLE. C/A: REMOVED AND INSTALLED LIGHT BULB, IAW EMB AMM 33-50-10. OPERATIONS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,686 hrs · 43,337 cycles

CABIN AFT AISLE EMERGENCY LIGHT INOPERABLE. C/A: REMOVED AND REPLACED AFT AISLE EMERGENCY LIGHT LAMP, IAW EMB 145 AMM 33-50-08. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,558 hrs · 43,208 cycles

EMERGENCY FLOOR LIGHT STRIP AT SEAT 8 INOPERABLE. C/A: R & R SEAT 8 EMERGENCY FLOOR LIGHT STRIP, IAW AMM 33-50-12. OPERATIONS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,455 hrs · 43,115 cycles

DURING PS-2 CHECK FOUND RIGHT HAND CENTER FAIRING EMERGENCY LIGHT OUT. C/A: R & R RT CENTER FAIRING EMERGENCY LIGHT LAMP, IAW EMB AMM 33-50-10. OPERATIONS CHECK GOOD.

Part: YOKE — CRACKED (LT ENGINE) · airframe 47,015 hrs · 42,666 cycles

LEFT ENGINE FORWARD YOKE LOWER CLEVIS HAS POSSIBLE CRACK IN RADIUS. REPLACED LT ENG FWD LWR YOKE FITTING IAW ERS-EM-54MR-698.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 47,015 hrs · 42,666 cycles

SUPPORT ON THE AFT SIDE OF FRAME 68 FOR CARGO DOOR HOLD OPEN STRUT HAS A 3/4" CRACK.-C/A-REMOVED AND INSTALLED NEW SUPPORT IAW SRM 51-40-02.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 47,015 hrs · 42,666 cycles

FORWARD CARGO DOOR TORSION BAR BRACKET AT FRAME 61 HAS A 1/8" CRACK. INSTALLED NEW BRACKET IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 47,015 hrs · 42,666 cycles

RIGHT OMEGA BEAM INBOARD LOWER SUPPORT "L" ANGLE IS CRACKED APPROXIMATELTY 1 1/2" ON THE FORWARD END BETWEEN FRAMES 47-48-C/A-REMOVED AND REPLACED RH OMEGA BEAM INBD LOWER SUPPORT L ANGLE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,015 hrs · 42,666 cycles

LEFT OMEGA BEAM AFT OF CROSSBEAM 24 HAS CORROSION.-C/A-REMOVED AND REPLACED PREVIOUS REPAIR DOUBLER ON LH OMEGA BEAM IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 47,015 hrs · 42,666 cycles

RIGHT OMEGA BEAM OUTBOARD LOWER SUPPORT "L" ANGLE IS CRACKED APPROXIMATELTY 1 1/2" ON THE FORWARD END BETWEEN FRAMES 47-48.-C/A-REMOVED AND REPLACED RH OMEGA BEAM OUTBD LOWER SUPPORT L ANGLE IAW SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 79) · airframe 47,015 hrs · 42,666 cycles

LEFT FUSELAGE SKIN AT FRAME 79 HAD SMALL CRACKS PROTRUDING FROM A RIVET. REPAIRED IAW SRM 53-32-01.

Part: SKIN — CRACKED (FRAME 77) · airframe 47,015 hrs · 42,666 cycles

RIGHT FUSELAGE SKIN AT FRAME 77 HAD SMALL CRACKS PROTRUDING FROM TWO RIVETS. REPAIRED IAW SRM 53-32-01.

Part: STRIP — TORN (CABIN) · airframe 47,015 hrs · 42,666 cycles

NR 8 EMERGENCY LIGHT STRIP IS TORN. REMOVED AND REPAIRED THE NR 8 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (SERVICE DOOR) · airframe 46,940 hrs · 42,590 cycles

SERVICE DOOR EMERGENCY LIGHT WIRE BROKEN-C/A-REPAIRED SERVICE DOOR EMERGNCY LIGHT BROKEN WIRE IAW AWM33-50-50, AND AMM 20-21-00. OPT GOOD IAW AMM 33-50-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,600 hrs · 42,281 cycles

LH SIDE CENTER FAIRING EMERGENCY LIGHT INOP-C/A-RAR LH SIDE CENTER FAIRING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-10 OPS CHECK GOOD.NO FURTHER DEFECT DETECTED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,508 hrs · 42,183 cycles

12C OVERHEAD EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED 12C OVERHEAD EMERGENCY LIGHT LAMP IAW EMB AM AND 33-50-08-400-801-A. OPC GOOD.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 46,481 hrs · 42,157 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. ADJUSTED THE LEFT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,295 hrs · 42,003 cycles

ROW 12 B/C OVERHEAD EMERGENCY LIGHT INOP-C/A-RAR ROW 12 B/C OVERHEAD EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECK GOOD. END

Part: UNKNOWN — ODOR (COCKPIT) · airframe 46,237 hrs · 41,938 cycles

EXTREMELY STRONG ODOR IN COCKPIT ON DESCENT FROM 8000 TO 5000 FEET.WET SOCK SMELL.APU OFF.ENGINE BLEEDS POWERING PACKS LASTED 2 -3 MINUTES-C/A-STARTED ENGINES AND RAN PACKS IAW EMB AMM 21-51-00 AND AMM 71-00-00. NO ODER NOTICED.C/W ETN-EM-72-034 .NO OTHER ODER NOTICED

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 45,473 hrs · 41,267 cycles

SERVICED DOOR EMERGENCY LIGHT INOP. C/A-RAR SERVICE DOOR EMERGENCY LAMP IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECK GOOD. END.

Part: TUBE — DAMAGED (NR 1 A/C PACK) · airframe 45,313 hrs · 41,120 cycles

PACK 1HAD STRONG DIRTY SOCK ODOR OM TAKE OFF & CLIMBOUT AND CRUISE. C/W ETN EM-72-034. NO OILY/SOCK SMELL NOTICED. WHILE PERFORMING ETN FOUND THE NR 1 PACK DUAL TEMP. CONTROL VALVE Y DUCT WARPED, REMOVED AND REPLACED THE Y DUCT IAW AMM 2160-01. OPS CHECK GOOD DURING ENGINE RUN UP AND AT TAKE OFF POWER. FCF FOUND SATISFACTORY

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 45,190 hrs · 40,980 cycles

WHILE PARKED AT GATE, EICAS "PRESN AUTO FAIL" PRESENTED. WHITE SMOKE NEAR THRUST LEVERS AND ELECTRICAL BURNING SMELL. FOUND "PRESS CONTROL" F8 BREAKER POPPED. (ENGINES WERE NOT RUNNING)-C/A-FOUND SMELL AND WHITE SMOKE COMING FROM AUTO PRESSURIZATION DIGITAL CONTROLLER. RESET BREAKER (F8) REMOVED AND REPLACED DIGITAL CONTROLLER IAW EMB-145 AMM 21-31-01, OPS CHECK GOOD. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,135 hrs · 40,921 cycles

MAIN DOOR EMERGENCY LIGHT INOP. C/A-RAR MAIN DOOR EMERGENCY LT LAMP IAW AMM 33-50-06-000-801-A AND AMM 33-50-06-400-801-A. OPC GOOD. NO MORE DEFECTS NOTED AT THIS TIME. END.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 44,438 hrs · 40,221 cycles

SUPPORT BRACKET AT FRAME 80 IS CRACKED (LT SIDE). C/A-INSTALLED NEW BRACKET IAW SRM 51-40-02..

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,438 hrs · 40,221 cycles

IN REFERANCE TO TSA DAMAGE ID 145-00074-00006-001 FORWARD FUSELAGE SKIN JUST ABOVE BATTERY COMPARTMENT BETWEEN FRAMES 4 AND 5. C/A-COMPLETED REPAIR IAW ERS EM-5300-3623 AND ERS EM-53MR-3816. REF NWRC E685453. SKIN P/N 123-06513-009. SPLICE PLATE P/N 123-10953-001.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 44,438 hrs · 40,221 cycles

RT UPEER WING/FUSELAGE SUPPORT IS CRACKED APROX. 3/4" BETWEEN THE RIVETS. JUST AFT OF FRAME 50. C/A-INSTALLED NEW RT UPPER WING/FUSELAGE SUPPORT IAW SRM 51-40-02.

Part: UNKNOWN — ODOR (COCKPIT)

POST TAKE OFF AT 1800 TO 200 FL, AN ELECTRICAL BURNING SMELL DETECTED ON FLIGHT DECK. (PILOTS FOUND SMELL COMING FROM PACK NR 1). OPS CHECK AC PACK 1 AND PACK 1 DISTRIBUTION SYSTEM. OPS CHECK GOOD. INSPECTED ALL ELECTRONICS IN FLIGHT DECK. NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 43,839 hrs · 39,686 cycles

POST TO AT 180 TO 200FL AN ELECTRICAL BURNING SMELL DETECTED ON FLIGHTDECK. DEFERRED NR 1 AC PACK ON DMI 2151001. MORE INFORMATION SENT WHEN AVAILABLE.

Part: MOTOR — BINDING (WINDSHIELD WIPER) · airframe 45,539 hrs · 39,420 cycles

FIRST OFFICER'S WINDSHIELD WIPER STOPPED MID WIPE. REMOVED AND REPLACED THE WINDSHIELD WIPER MOTOR. OPS CHECKED GOOD. OPEN.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 42,149 hrs · 38,195 cycles

CARGO DOOR SILL IS CORRODED AT THE FORWARD END. R & R THE DOOR SILL.

Part: LENS — CRACKED (EMEGENCY LIGHT) · airframe 42,103 hrs · 38,153 cycles

EMERGENCY LIGHT LENS CRACKED. R & R THE LENS. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,762 hrs · 3,729 cycles

EMERGENCY LIGHT AT ROWS 8 - 11, FOUND INOPERATIVE. REPAIRED THE WIRING. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,762 hrs · 37,029 cycles

EMERGENCY LIGHT IN CEILING BY SERVICE DOOR IS INOPERATIVE. R & R THE BULB, EMERGENCY LIGHT OPS CHECKED GOOD.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 39,280 hrs · 35,832 cycles

ACFT WILL NOT PRESSURIZE ON AUTO OR MANUAL MODE IN THE AIR ACFT RETURNED FROM FLIGHT. COMPLIED WITH REACTIVATION PROCEDURE. OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 38,963 hrs · 35,566 cycles

RIGHT OVERWING EMERGENCY EXIT MARKER NR 24 INOPERATIVE. RESEATED GRAND CONNECTOR OF EMERGENCY LIGHT. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,771 hrs · 35,408 cycles

PASSENGER DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R PAX DOOR EMERGENCY FLOOD LIGHT NR 1. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,771 hrs · 35,408 cycles

LEFT FWD EXTERIOR EMERGENCY FLOOD LIGHT NR 3 INOPERATIVE. R & R FWD EXTERIOR EMERGENCY FLOOD LIGHT NR 3. OPS CHECK GOOD.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 38,593 hrs · 35,267 cycles

GRADUAL LOSS OF PRESSURIZATION AT FL 370. OPEN

Part: SKIN — GOUGED (FUSELAGE) · airframe 38,481 hrs · 35,179 cycles

SURROUNDING EXTERIOR STRUCTURE AT PAX WINDOW 4BC IA GOUGED. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-1464.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,481 hrs · 35,179 cycles

RIGHT REAR FUSELAGE I, SKIN CRACKS AT FRAME 75 BETWEEN STRINGERS 1R & 3R. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR1462.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,480 hrs · 35,178 cycles

LEFT REAR FUSELAGE I SKIN BETWEEN FRAME 74 - 75 & STRINGER 20L BURN MARK. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN IAW ERS-EM-53MR-1463.

Part: SKIN — BURNED (FUSELAGE) · airframe 38,481 hrs · 35,179 cycles

LEFT REAR FUSELAGE I SKIN BETWEEN FRAME 74 - 75 & STRINGER 20L, BURN MARK. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-1463.

Part: FITTING — CRACKED (RT NACELLE) · airframe 38,480 hrs · 35,178 cycles

DURING MBV INSPECTION, FOUND RT ENG FWD LOWER YOKE FITTING CRACKED. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER INSPECTION. PERFORMED PERMANENT REPAIR ON RT ENG FWD LOWER YOKE FITTING IAW EO-EM-54MR-386. REPLACEMENT FITTING PN 145-29426-003.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,480 hrs · 35,178 cycles

FUSELAGE SKIN CRACK AT THREE RIVETS ON FRAME 75 BETWEEN STRINGERS 1R & 2R, END OF CRACKS MARKED. REPAIRED FUSELAGE EXTERNAL SKIN CRACKS AT FRAME 75 & STRINGER 1R - 3R IAW ERS-EM-53MR-146.

Part: PROXIMITY SWITCH — MALFUNCTIONED (LT SPOILER) · airframe 38,247 hrs · 34,976 cycles

ON LANDING AT APPROX 110 KTS DURING ROLLOUT GOT, SPOILER FAIL, EICAS MSG WITH OPEN INDICATION MSG WENT AWAY APPROX 10 SECONDS AFTER CLEARING RUNWAY & THEN INDICATED CLOSED. TRANSFERRED TO NRWC 611-ORD-02360. REF NRWC 611-ORD-02360 R & R LT INBD SPOILER PROX SWITCH IAW AMM 27-63-04 & ADJUSTED GAP IAW ETN-EM-27-132. OPERATIONS CHECKED GOOD. PROXIMITY SENSOR PN 80-057-01 SN 38824.

Part: CONTACT — NOT SEATED (EXIT SIGN) · airframe 37,754 hrs · 34,536 cycles

ROW 12C UPPER SIDEWALL EMER EXIT SIGN INOPERATIVE. RESEATED ELEC CONTACTS ON THE UPPER SIDEWALL EMER EXIT SIGN AT SEAT 12C IAW AMM TASKS 33-50-13-000-801-A & 33-50-13-400-801-A. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 36,698 hrs · 33,725 cycles

LEFT OVERWING EMER LIGHT IS INOPERATIVE. FOUND CONNECTOR LOOSE. TIGHTEN CONNECTOR AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 36,658 hrs · 33,685 cycles

MAIN DOOR EMER LIGHT WORKS INTERMITTENTLY. R & R MAIN DOOR EMER LIGHT ASSEMBLY IAW AMM 33-50-06.

Part: UNKNOWN — ODOR (CABIN) · airframe 36,605 hrs · 33,643 cycles

AFTER TAKEOFF AT 200 FEET AGL FLIGHT ATTENDANT CALLED & NOTIFIED FLIGHT CREW THAT SHE WAS SMELLING ELEC SMOKE & SOMETHING BURNING. COMPLIED WITH AOM ELECT SMOKE & MEMORY ITEM PROCEDURES. IMMEDIATE RETURN TO FIELD & DECLARED EMER. THE ACFT WAS REMOVED FROM SERVICE. TURNED APU OFF, CROSS BLEED AUTO, ENGS 1 & 2 BLEEDS OPEN, PACK 1 & 2 WAS CONFIGURED WITH NO VISIBLE INDICATION OF SMOKE OR FIRE. NO ODOR OF ELEC SMOKE IN COCKPIT. TURNED ON ALL COCKPIT & CABIN LIGHTS FOR OVER FOUR HOURS & COMPLIED WITH ETN-EM-72-034 R9 WITH NO EVIDENCE OF ANY ELEC, OIL, OR PLASTIC ODORS. CANNOT DUPLICATE SMELLS OR ODORS. THE ACFT RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 36,501 hrs · 33,567 cycles

FIRE DETECTION TEST NOT TESTING CORRECTLY, BAGG EXTINGUISHER BUTTON NOT ILLUMINATED. R & R CARGO SMOKE DETECTOR 1 IAW AMM 26-15-01. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,432 hrs · 33,494 cycles

EMERGENCY LIGHTS INOPERATIVE. R & R NR 1 EPSU BATTERY & CHARGER. OPERATIONS CHECKED GOOD IAW AMM 33-50-04. BATTERY CHARGER ASSEMBLY PN 11-0049 SN 19737.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 36,202 hrs · 33,301 cycles

SPS 2 INOPERATIVE ON EICAS UPON LANDING STICK SHAKER ACTIVATED. R & R STALL PROTECTION COMPUTER IAW AMM 27-36-02. OPERATIONS CHECKED GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 35,434 hrs · 32,658 cycles

RIGHT EXIT ROW UPPER DOOR SIGN INOPERATIVE. R & R EXIT ROW UPPER DOOR SIGN IAW AMM 33-50-14, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,330 hrs · 32,570 cycles

RT AFT EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. R & R LAMP IN RT AFT EXTERNAL EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 35,175 hrs · 32,434 cycles

RIGHT OVERWING EXIT SIGN INOPERATIVE. R & R RT EXIT SIGN IAW AMM 33-50-14, OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (THRUST REVERSER) · airframe 35,151 hrs · 32,413 cycles

E2 REV DISAGREE. DEFERRED IAW MEL 78-02 AUTH 021215M-C. M PROCEDURES COMPLIED WITH.

Part: DOOR — FROZEN (CABIN) · airframe 34,887 hrs · 32,208 cycles

MAIN PAX DOOR FROZEN SHUT. TOOK ACFT TO A HEATER HANGAR & LET IT THAW. ONCE DOOR OPENED, FOUND WATER & ICE ON DOOR SEAL. WIPED DOOR SEALS DOWN TO DRY & LUBRICATED THEM IAW AMM TASK 52-18-00-600-801-A STEP 2 J 3. NO FURTHER DEFECTS NOTED, DOOR OPENS & CLOSES NORMALLY.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,143 hrs · 31,630 cycles

ALL EMERGENCY LIGHTS ON POWER SUPPLY NR 1 INOPERATIVE. R & R NR 1 EMERGENCY POWER SUPPLY BATTERY PACK AND CHARGER ASSY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: DOOR — DAMAGED (EMERGENCY EXIT) · airframe 34,104 hrs · 31,589 cycles

RT EMERGENCY EXIT HANGS WHEN OPENING. REPOSITIONED RT EMERGENCY EXIT SHROUD IAW AMM 25-23-08.

Part: SPAR — CRACKED (LT WING) · airframe 34,123 hrs · 31,610 cycles

LT WING SPAR III CRACKED. REPAIRED LT SPAR III CRACK IAW EO EM-57MR-711. FOUND DURING EO EM-5700-662, ACCOMPLISHMENT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,103 hrs · 31,588 cycles

EXTERNAL SKIN CORRODED BETWEEN FRAMES 13-14, STR 20L-19R. REPAIRED IAW AEA EO EM-53MR-2198.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,103 hrs · 31,588 cycles

FR 68L SHAPE CORROSION ON LOWER PORTION ABOVE CARGO DOOR SILL. REPAIRED FR 68 SHEARCLIP IAW AEA EO EM-53MR-1129, PART B.

Part: FITTING — DAMAGED (LT AILERON) · airframe 34,103 hrs · 31,588 cycles

LT AILERON PCA FITTING DAMAGED. REMOVED AND INSTALL PCA FITTING IAW EO EM-27MR-112.

Part: SKIN — CRACKED (E/E DOOR) · airframe 34,103 hrs · 31,588 cycles

REAR ELECTRONICS DOOR 272DR SKIN CRACKED AROUND ANGLE RIVETS. REPAIRED IAW AEA EO EM-52MR-371.

Part: FRAME — GOUGED (FUSELAGE) · airframe 34,123 hrs · 31,610 cycles

FRAME 70 BETWEEN STR 12-13R GOUGED. REPAIRED IAW AEA EO EM-53MR-2193.

Part: WIRE HARNESS — FRAYED (EMERGENCY LIGHT) · airframe 34,103 hrs · 31,588 cycles

LEFT EMERGENCY LIGHT BRAIDED HARNESS BEHIND OVERWING PANEL FRAYED. REPAIRED THE LT EMERGENCY LIGHT BRAIDED HARNESS BEHIND OVERWING PANEL THAT WAS FRAYED IAW AWM 20-21-00, STEP 7.C.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,103 hrs · 31,588 cycles

EMERGENCY LIGHT STRIP NR 2 HAS A BROKEN WIRE ON FUSELAGE SIDE. REPAIRED THE EMERGENCY LIGHT STRIP NR 2 THAT HAD A BROKEN WIRE ON FUSELAGE SIDE IAW AWM 20-00-03.

Part: SPAR — CRACKED (LT WING) · airframe 34,103 hrs · 31,588 cycles

LT SPAR 3 CRACKED BETWEEN RIB 3 AND 4. LT SPAR 3 CRACKED BETWEEN RIB 3 AND 4. REPAIRED IAW EO EM-57MR-711.

Part: CONNECTOR — MISSING (EMERGENCY LIGHT) · airframe 34,103 hrs · 31,588 cycles

FR 38 CONNECTOR FOR EMERGENCY LIGHT STRIP IS MISSING. REPAIRED THE FR 38 CONNECTOR FOR EMERGENCY LIGHT STRIP THAT WAS MISSING IAW AWM 20-00-03, PAGE 65. SEE BOW 137540 FOR OPS CK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,103 hrs · 31,588 cycles

2 EA CABIN EMERGENCY LIGHT STRIP WIRES BROKEN. R & R NR 7 AND NR 8 CABIN EMERGENCY FLOOR LIGHT STRIPS IAW AMM 33-50-12 SEE NRTC NR BOW137540 FOR OPS TEST.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,007 hrs · 31,512 cycles

EXTERNAL MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM TASKS 33-50-10-000-801-A/33-50-10-400-801-A. OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (MLG) · airframe 33,869 hrs · 31,405 cycles

ON GEAR RETRACTION, NOTICED A LOUD BANGING NOISE COMING FROM NOSE GEAR WELL. CONTINUED FLIGHT. AN EMERGENCY WAS DECLARED AND ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF GEAR. ACCOMPLISHED CHECK OF GEAR WOW PROXIMITY SWITCHES, NLG DOOR SEQUENCE SWITCH, UPLOCK SWITCHES, AND DOWNLOCK HARNESSES IAW MM 32-63-05. RT MLG UPLOCK "B" SHOWED FAULTY . WHEN RT UPLOCK BOX HOOK IS TRIPPED, "B" SENSOR NEVER SHOWS TARGET NEAR. SWAPPED HARNESSES "A" TO "B" AND VERIFIED SENSOR IS WORKING. PROBLEM IS HARNESS. R & R THE RT MLG UPLOCK BOX IAW AMM 32-33-10. PROXIMITY SENSOR, OPS & LEAK CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: SOLENOID VALVE — DEFECTIVE (RT MLG) · airframe 33,559 hrs · 31,150 cycles

THE CREW REPORTED THAT DURING GEAR RETRACTION THE RT MAIN GEAR WOULD NOT FULLY RETRACT. A CONSTANT THUMPING NOISE WAS NOTICED. THE GEAR CYCLED DOWN AND ALL 3 SHOWED GREEN. THE CREW ELECTED TO RETURN TO DEPARTURE AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. FOUND BAD LANDING GEAR SOLENOID VALVE AND INSTALLED SERVICABLE VALVE IAW AMM 32-33-04. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 33,476 hrs · 31,078 cycles

THE CREW REPORTED THAT DURING CLIMB AT 8000 FT, THEY RECEIVED AN EICAS BLEED 2 LEAK MESSAGE AND BLEED 2 PUSHBUTTON. THE CREW COMPILED WITH THE AOM VOL 1 PROCEDURES AND THE LIGHT EXTINGUISHED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R O-RING, PN: 403039-20. TYWRAP, PN: PLT4S-M76. INSULATION SLEEVE, PN: 713463-11. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: COVER — DAMAGED (MAIN DOOR) · airframe 33,244 hrs · 30,873 cycles

DURING MAINTENANCE INSPECTION FOUND MAIN DOOR SIDE ARM COVER HAS HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/W REMOVED AND REPLACED MAIN DOOR SIDE ARM COVER IAW 25-23-05 STEPS 2J(7) AND 3I(1). OPS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (CABIN) · airframe 33,244 hrs · 30,873 cycles

DURING MAINTENANCE INSPECTION FOUND UPPER SIDEWALL EMERGENCY EXIT LIGHT AT SEAT12BC NOT WORKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/W REMOVED RIGHT SIDEWALL EMERGENCY EXIT LOCATOR SIGN. CLEANED ELECTRICAL CONNECTIONS AND RE-INSTALLED. LIGHT WORKS NORMALLY IAW EMB-145 AMM 33-50-14. OPC IAW EMB-145 AMM 33-50-0. THE AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 33,151 hrs · 30,785 cycles

DURING B INSPECTION FOUND THE COCKPIT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IN THE COCKPIT EMERGENCY LIGHT ASSEMBLY IAW EMB145 AMM 33-50-05. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (FLASHLIGHT) · airframe 33,096 hrs · 30,750 cycles

DURING MAINTENANCE INSPECTION, FOUND THE FIRST OFFICER’S FLASHLIGHT HOLDER/CHARGER BROKEN. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. DID NOT FIX. REMOVED AND REPLACED THE WIRE HARNNES EXTENTION ASSEMBLY FROM J1871 TO SP3553 TO SP3554 IAW WM 20-21-00. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 32,820 hrs · 30,529 cycles

ON FLIGHT 4324 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IAW EMB-145 AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: APU — FAILED · airframe 32,810 hrs · 30,523 cycles

FLIGHT 3557, CREW REPORTED A STRONG ODOR OF FUEL IN CABIN & COCKPIT WITH PACKS ON. APU FUEL SHUT OFF VALVE. REMOVED AND REPLACED APU. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 32,708 hrs · 30,461 cycles

FLIGHT 9809. CREW REPORTED AN ELECTRICAL BURNING ODOR AFTER TAKEOFF IN COCKPIT. DECLARED AN EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT FORWARD LOWER FAIRING EXTERNAL 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: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,703 hrs · 30,456 cycles

DURING B INSPECTION FOUND THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD EXTERIOR EMERGENCY LAMP. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CARGO BAY) · airframe 32,685 hrs · 30,437 cycles

DURING MAINTENANCE INSPECTION A BAGGAGE HANDLER REPORTED SUSPECT SMOKE ODOR IN CARGO COMPARTMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED BLEED SYSTEM LINES CHECK INSIDE CARGO COMP WITH APU AIR IAW AMM 36-00-00. FIRE DEPARTMENT PERFORMED SMOKE & HEAT CHECK. NO ODOR OR SMOKE DETECTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,640 hrs · 30,398 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AND RIGHT WING AFT EMERGENCY LIGHTS NOT COMING ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED NR 4 BATTERY CHARGER AND BATTERY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

NR 3 BATTERY EMERGENCY LIGHT SYSTEM INOP AND POWER SUPPLIES. REMOVED AND INSTALLED NEW NR 3 EMERGENCY LIGHT SYSTEM POWER SUPPLIES AND BATTERY IAW EMB-145 WORKCARD 33-700-19 AND OPS CHECK WORKCARD 33-700-17 GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

NR 4 BATTERY EMERGENCY LIGHTING SYSTEM INOP AND POWER SUPPLIES. REMOVED AND INSTALLED NEW NR 4 EMERGENCY LIGHTING SYSTEM POWER SUPPLIES AND BATTERY IAW EMB-WORKCARD 33-700-19 AND OPS CHECK WORKCARD 33-700-17 GOOD.

Part: CABLE — OUT OF ADJUST (ENTRY DOOR)

MAIN CABIN ENTRY DOOR COULD NOT BE OPENED ARRIVING AT AIRCRAFT FOR FIRST FLIGHT; DOOR HANDLE BINDING WHEN POP FROM OUTSIDE. ADJUSTED AFT SIDE LOCK BOX CABLE IAW EMB 145 AMM 52-18-00, OPS CHECKS GOOD.

Part: FLASHLIGHT — FAULTY (CABIN) · airframe 32,235 hrs · 30,080 cycles

ON FLIGHT 3372 THE CREW REPORTED A SULFER SMELL IN THE REAR OF THE AIRCRAFT DURING FLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,988 hrs · 29,878 cycles

DURING B INSPECTION FOUND THE RIGHT AND LEFT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AND LEFT OVERWING EMERGENCY LIGHT BULBS IAW EMB145 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,909 hrs · 29,812 cycles

DURING B INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW EMB AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,654 hrs · 29,617 cycles

DURING B INSPECTION FOUND THE LEFT DURING B INSPECTION FOUND THE LEFT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT EXTERIOR OVERWING EMERGENCY EXIT LAMP IAW EMB AMM TASK 33-50-10-000-801/33-50-10-400-801. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. EMERGENCY LIGHT INOPERABLE.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 31,530 hrs · 29,518 cycles

DURING B INSPECTION, FOUND THE FLIGHT ATTENDANT FORWARD FLASHLIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD FLASHLIGHT. OPS CHECKED GOOD IAW AMM 33-50-11. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,375 hrs · 29,403 cycles

DURING B INSPECTION, FOUND THE RIGHT EXTERIOR LATERAL-TO-FUSELAGE OVER WING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 31,244 hrs · 29,289 cycles

DURING B INSPECTION, FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD IAW AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (FLASHLIGHT) · airframe 31,108 hrs · 29,183 cycles

DURING B INSPECTION, WHILE PERFORMING FUNCTIONAL CHECK OF THE EMERGENCY FLASHLIGHTS WC 33-700-20, FOUND THE AFT FLASHLIGHT LIGHT BATTERY TO LIGHT CONNECTOR DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT ASSEMBLY. OPS CHECKED GOOD IAW AMM 33-50-16. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 30,949 hrs · 29,052 cycles

DURING B INSPECTION FOUND THE RIGHT AFT WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP FOR THE RIGHT AFT WING EMERGENCY LIGHT ASSEMBLY IAW EMB145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,682 hrs · 28,838 cycles

DURING B INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW EMB AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,489 hrs · 28,676 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT PER EMB MM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BELLCRANK — DEFECTIVE (CABIN DOOR) · airframe 30,232 hrs · 28,451 cycles

ON FLIGHT 3432 THE CREW REPORTED THE MAIN CABIN DOOR HANDLE WOULD NOT OPEN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/A: REMOVED AND REPLACED THE MAIN CABIN DOOR BELLCRANK IAW AMM 52 18-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CLAMP — LEAKING (ANTI ICE VALVE) · airframe 30,001 hrs · 28,287 cycles

FLIGHT 2957, CREW REPORTED THAT ON CLIMBOUT RECEIVED A "BLEED 1 LEAK" WARNING. FOLLOWED AOM PROCEDURES AND DESELECTED BLEED 1. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEAKING CLAMP AT HORIZONTAL STABILIZER ANTI-ICING VALVE. TORQUED PER AMM 30-12-01. NO LEAKS NOTED, THE OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DEFECTIVE (FLASHLIGHT) · airframe 29,711 hrs · 28,070 cycles

ON FLIGHT 2816 THE CREW REPORTED THE CAPTAINS FLASHLIGHT WORKS INTERMITTANTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED BATTERY AND OPERATIONAL CHECK WAS GOOD IAW EMB 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 29,553 hrs · 27,952 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT WING RIB 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT RIB 5 IAW EO-EM-57MR-595 R1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PIN — BROKEN (FIRE BOTTLE) · airframe 29,386 hrs · 28,824 cycles

FOR FLIGHT 4174 THE CREW REPORTED THE SAFETY TIE FLIGHT DECK FIRE EXTINGUISHER PIN WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED SAFETY TIE ON COCKPIT FIRE EXTINGUISHER IAW EMB 145 AMM STANDARD MTX PRACTICES. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (MAIN) · airframe 28,368 hrs · 27,083 cycles

FOR FLIGHT 3457 MAINTENANCE REPORTED, ARRIVING AT THE AIRCRAFT FOUND BATTERIES NR 1 AND NR 2 ON AUTO. THE GROUND POWER UNIT WAS AVAILABLE BUT NOT SELECTED. A STRONG "ACRID" ODOR WAS PRESENT. SHEDS OVRD, EMERGENCY LIGHTS ARMED AND ILLUMINATED FUEL PUMPS ON, APU SWITCH ON WITH THE AUXILIARY POWER UNIT NOT RUNNING SBY ATT UN-CAGGED, S/B SIGN ON. THE BATTERIES APPEARED TO BE DEAD. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE NR 1 & NR 2 BATTERIES IAW EMB-145 WORK CARD 24-600-00. THE OPERATIONAL CHECK WAS OK AS PER AMM 24-36-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,234 hrs · 26,974 cycles

FOR FLIGHT 4123 DURING PREFLIGHT INSPECTION THE CREW FOUND THE RIGHT EMERGENCY EXIT ROW DOME LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW EMB AMM TASKS 33-50-08-000-801-A AND 33-50-08-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — DEFECTIVE (CABIN) · airframe 28,210 hrs · 26,952 cycles

ON FLIGHT 4349 AT CRUISE FLIGHT LEVEL 370 THE FLIGHT ATTENDANT ADVISE OF A BURNING ODOR IN CABIN AS WELL AS A HAZE WAS FORMING IN THE CABIN. THE CREW WENT TO AOM NR 1 FIRE SMOKE IN CABIN CHECKLIST AND ELECTED TO LAND IN YYZ. THE CABIN LIGHTING WAS TURNED OFF. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE ODOR REMAINED THROUGH LANDING BUT GRADUALLY DISSIPATED AFTER DOOR WAS OPENED. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF CABIN INTERIOR LIGHTING INCLUDING CEILING, SIDEWALL AND PASSENGER SERVICE UNITS IAW EMB AMM 33-21-00 AND 33-25-00 AND FOUND NO DEFECTS. PERFORMED OPERATIONAL CHECK OF CABIN RECIRCULATION FAN IAW EMB AMM 21-20-00 AND FOUND IT TO BE NOT FUNCTIONING. PERFORMED GENERAL VISUAL INSPECTION OF CABIN RECIRCULATION FAN REF EMB AMM 21-24-01 AND FOUND IT TO BE THE SOURCE OF THE HAZE AND BURNING ODOR. REMOVED AND REPLACED THE CABIN RECIRCULATION FAN IAW EMB 145 AMM 21-24-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — ODOR (COCKPIT) · airframe 27,645 hrs · 26,531 cycles

ON FLIGHT 4149 DURING HEAVY RAIN AND LIGHTNING A PASSENGER REPORTED A BURING ODOR IN THE CABIN. THE CREW ALSO DETECTED A BURNING ODOR IN THE COCKPIT FOR 3 TO 4 MINUTES. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS BEZEL UNIT MAIN FLIGHT DISPLAY IAW EMB AMM 34-22-02. REMOVED AND REPLACED THE FIRST OFFICERS MAIN FLIGHT DISPLAY UNIT IAW EMB AMM 34-22-01. PERFORMED LIGHTNING INSPECTION. NO LIGHTNING STRIKE INDICATIONS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SOCKET — LOOSE (CABIN) · airframe 2,703,605 hrs · 26,053 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AFT OVERWING EMERGENCY LIGHT WILL NOT STAY LIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AND FOUND THE BULB SOCKET LOOSE. REMOVED AND REPLACED THE RIGHT AFT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10-000-801-A. THE OPERATIONAL CHECK WAS NORMAL AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,036 hrs · 26,053 cycles

FOR FLIGHT 4374 PRIOR TO FLIGHT THE CREW FOUND THE EMERGENCY SIGN NEAR RIGHT EMERGENCY WINDOW TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT CHARGER ASSEMBLY IAW EMB 145 AMM CH 33-50-04-000-802-A/33-50-04-400-802-A. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM CH 33-50-04-000-801-A/33-50-04-400-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (LT WING) · airframe 25,880 hrs · 25,158 cycles

DURING MAINTENANCE BASE VISIT FOUND DAMAGE TO LEFT WING LOWER SKIN AND ANGLE DUE TO TIRE STRIKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR OF DAMAGE TO LEFT WING LOWER SKIN AND ANGLE IAW EO-EM-57MR0488R3. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — DAMAGED (LT WING) · airframe 25,880 hrs · 25,158 cycles

DURING MAINTENANCE BASE VISIT FOUND DAMAGE TO LEFT WING LOWER SKIN AND ANGLE DUE TO TIRE STRIKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR OF DAMAGE TO LEFT WING LOWER SKIN AND ANGLE IAW EO-EM-57MR0488R3. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,826 hrs · 25,116 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OVERWING AFT EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TIRE — FAILED (NR 2) · airframe 25,789 hrs · 25,093 cycles

ON FLIGHT 3634 AFTER TAKEOFF THE CREW WAS NOTIFIED BY THE CONTROL TOWER OF A POSSIBLE BLOWN TIRE. DID A FLY BY ON THE MIA TOWER AND WAS TOLD THE NR 2 TIRE HAD BLOWN. CREW DECLARED AN EMERGENCY. UPON LANDING THE TIRE CAME APART DAMAGING THE LEFT INBOARD FLAP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 & 2 TIRES IAW EMB 32-700-11. REMOVED AND REPLACED THE LEFT INBOARD FLAP ASSEMBLY IAW 27-400-01. REMOVED AND REPLACED THE NR 4 MAIN LANDING GEAR WHEEL ASSEMBLY IAW 32-700-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,729 hrs · 25,040 cycles

DURING MAINTENANCE BASE VISIT THE LEFT FORWARD OVERWING AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT WING UPPER AFT EXTERNAL EMERGENCY EXIT LAMP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (MLG) · airframe 17,376 hrs · 16,589 cycles

ON FLIGHT 4154 CREW REPORTED ON TAKEOFF LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LGEU, ADJUSTED GAP ON LEFT NR 2 AND RIGHT NR 1 WOW PROX SWITCHES OPERATIONAL CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.

Part: FMU — MALFUNCTIONED (NR 1 ENGINE)

ON FLIGHT 3576 CREW REPORTED ENGINE 1 POWER FLUX N1 ITT, N2, IGNITION A&B AUTO RELIGHT AND FADEC TRANSFER IN FLIGHT FOR ABOUT 30 SECONDS. THRUST SURGED UP/DOWN CONTINUED FROM ABOVE TRUST LEVERS AT FLT IDLE. ENGINE 1 STABILIZED NO ABNORMAL INDICATIONS AFTERWARDS. NO EICAS MSGS. ACFT REMOVED FROM SERVICE. C/A R&R FPMU AND OPS CHECKED GOOD. FSF PASSED. ACFT RETURNED TO SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE)

ON FLIGHT 3748, CREW REPORTED ON TAKEOFF GOT AN OIL BURN OR DIRTY SOCK ODOR IN COCKPIT. ODOR DISSIPATED ON CLIMBOUT BETWEEN 10,000 FEET AND 15,000 FEET. NO EMERGENCY DECLARED. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. ACCOMPLISHED ETN EM 72-034R4 AND REPLACED ZERO CARBON SEAL ON LT ENG. OPERATIONAL CHECK GOOD. NO ODOR IN COCKPIT OR CABIN. ACFT RETURNED TO SERVICE. (S)

Part: UPLOCK — INOPERATIVE (RT MLG) · airframe 20,291 hrs · 20,219 cycles

ON FLIGHT 4104, CREW REPORTED RIGHT MAIN LANDING GEAR DID NOT SHOW UP AND LOCKED ONLY IN TRANSIT. CREW RETURNED TO MQT WITH NO FURTHER INCIDENTS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR UPLOCK BOX IAW EMB AMM 32-33-10 AND NR 8194;AND NR 8194;AND NR 8194; AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (HYD SYSTEM) · airframe 17,770 hrs · 18,036 cycles

HYDRAULIC SYSTEM 1 QUANTITY LEVEL WENT TO AMBER WITH LOW QUANTITY MESSAGE, ENGINE 1 HYDRAULIC SYSTEM PUMP FAIL MESSAGE, INTERMITTENT HYDRAULIC 1 FAIL MESSAGE, EMERGENCY DECLARED. POST INSPECTION FOUND HYDRAULIC FLUID ON NUMBER 1 ENGINE COWL.

Part: UNKNOWN — ODOR (COCKPIT)

AFTER TAKEOFF CREW SMELLED OIL ODOR IN COCKPIT. RETURNED TO DFW. (M)

Part: ENGINE — OVERTEMP (NR 1)

UNCOMMANDED NR 1 ENGINE SHUTDOWN IN FLIGHT, ITT WAS OVER 1000 DEGREES. (M)

Part: ENGINE — MALFUNCTIONED (NR 1)

LRD - FLT 3636 - UNCOMMANDED NR 1 ENGINE SHUTDOWN IN FLIGHT, ITT WAS OVER 1000 DEGREES. DOWNLOADED FLIGHT DATA RECORDER, IAW WORK CARD 31-700-05 AND DOWNLOADED CMC IAW WORK CARD 45-900-00. REMOVED AND REPLACED NUMBER 1 ENGINE, IAW AE WORK CARD 72-000-00. ALL OPS AND LEAK CHECKS COMPLIED WITH NO DISCREPANCIES NOTED. RETURNED AIRCRAFT TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING CPCP INSPECTION FOUND PROFILE ON TOP OF CENTER OMEGA BEAM BETWEEN FRAMES 59-60 HAS SPOTS OF CORROSION. REPAIRED PROFILE IAW IC 2005-145/6986. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (FUSELAGE)

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING CPCP INSPECTION FOUND CENTER HAT BEAM UPPER PROFILE HAS SPOTS OF CORROSION FROM FRAMES 19 TO 23. REPLACED GUSSET IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING CPCP INSPECTION FOUND OMEGA BEAM DOUBLER AT FRAME 20 IS CORRODED. REPLACED DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING HMBV INSPECTION FOUND AFT CARGO FLOOR SUPPORT AT FRAME 71 RT HAS CORROSION. INSTALLED NEW FLOOR SUPPORT IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING CPCP INSPECTION, FOUND CARBON CROSS MEMBER AT FRAME 24-25 CENTER OMEGA BEAM ATTACHMENT IS CORRODED. REPAIRED OMEGA BEAM BY INSTALLING AN EXTERNAL DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: CONTROL UNIT — FAILED (E/E BAY)

YUL - FLT 4759 - DURING APPROACH CREW REPORTED A MAIN AND BACKUP PITCH TRIM FAIL ON EICAS. SYSTEM WAS RESET AS PER THE MANUAL AND AICRAFT WAS LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECKS WERE SATISACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (GALLEY)

DURING AN MBV INSPECTION, FOUND CORROSION ON LEFT FLOORBEAM, PREV REPAIR, AT FRAME 20. REMOVED PREVIOUS REPAIR, CORROSION LIMITED TO UPPER DOUBLER ANGLE OF PREVIOUS REPAIR. FABRICATED A DOUBLER ANGLE. REPAIR DONE IAW EMB 145, SRM 145/1142 REV 23, CHAPTER 53-21-10 AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (GALLEY SERV DOOR)

DURING MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED SERVICE CENTER DOOR SILL. INSTALLED NEW SILL IAW EMB SRM, SRM EMB 145-1142 REV 23, CHAPTERS 51-40-02, 04, 05, 06, 07, 51-20-01 AND 51-20-03. (M)

Part: CLAMP — LOOSE (BLEED AIR SYS)

CLE - FLT 4383 - DURING APPROACH, THE CREW RECEIVED A BLEED ONE LEAK WARNIGN IN ICING CONDITIONS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS LANDED SAFELY IN CLE WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE INSPECTED ALL BLEED LINES AND RESECURED LOOSE CLAMPS AND COUPLINGS IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY CENTER FLOOR SUPPORT BEYOND SRM LIMITS AFTER BLENDING. REMOVED CORRODED GALLEY CENTER FLOOR SUPPORT. INSTALLED NEW GALLEY CENTER BEAM. WORK DONE IAW EMB 145, SRM 145/1142 CHAPTER 51, REV 17, 61-20-01, 51-20-03, 51-40-04, CPM 51-21-04, GST 1014/02, ITEM 10, AND STANDARD SRM PRACTICES. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIGHT HAT BEAM BETWEEN FRAMES 17 AND 19. REMOVED CORROSION BY BLENDING OUT. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED DOUBLER. WORK DONE IAW EMB GST-1014/02, ITEM 14, AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND LOWER CARGO DOOR SILL CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL (BEAM). INSTALLED NEW BEAM IAW EMB 145 (SRM 145/1142, CHAPTER 51, REV 17) 51-40-02, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — GOUGED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19L GOUGED. BLENDED GOUGE. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIRED IAW EMB GST-1002/02 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND GALLEY AREA FORWARD DIGITAL (RIGHT SIDE) CORRODED. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED DOUBLER. WORK DONE IAW EMB GST-1014/02, ITEM 4A, AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE SERVICE DOOR CENTER SILL. BLENDED CORROSION. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIRED IAW EMB GST-1014/02, ITEM 3, AREA NR 3, AND STANDARD SRM PRACTICES. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIGHT HAT BEAM BETWEEN FRAMES 23 AND 24. REMOVED CORROSION BY BLENDING OUT. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED DOUBLER. WORK DONE IAW EMB GST-1014/02, ITEM 7 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND GALLEY AREA FORWARD DIGITAL, LEFT SIDE, CORRODED. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. REPAIRED IAW EMB GST -1014/02 ITEM 4B, AND STANDARD SRM PRACTICES. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM PREVIOUS REPAIR AT FRAME 20. REMOVED PREVIOUS REPAIR. FABRICATED A DOUBLER ANGLE, FILLER, A PLATE, AND SHIMS. REPAIRED IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 17 REV 17 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

ABI - THIS IS A LEVEL 2 FINDING. LEFT GUSSET UNDER PILOTS CONTROL YOKE AND LEFT SEAT TRACK CORROSION FOUND. TREATED CORROSION IAW EMB 145 CPM 51-21-04, 51-21-05, 51-21-06. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LEFT GUSSET UNDER COPILOTS CONTROL COLUMN AND LEFT SEAT TRACK IS CORRODED. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1031/02, RETREATED AREA IAW EMB145 CPM 51-21-04, 51-21-05. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, FOUND DENT ON LEFT FUSELAGE AFT OF FRAME 20 BELOW STRINGER 11L. REMOVED DENT BY CUT OUT. FABRICATED A DOUBLER AND FILLER IAW EMB 145 SRM 145/1142 CHAPTER 53 REV 17, 53-21-01, AND STANDARD SRM PRACTICES. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LEFT SILL CORRODED BETWEEN FRAMES 31-36. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST 1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, CENTER BEAM GUSSET IS CORRODED AT FRAME 26. REMOVED CORROSION IAW EMB GST-1014/02. TREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. RIGHT SILL CORRODED BETWEEN FRAMES 23 AND 37. REMOVED CORROSION AND ACCEPTED AS IS IAW EMB GST-1014/02. RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LEFT BEAM GUSSET CORRODED BETWEEN FRAMES 31 AND 33. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LEFT SILL CORRODED BETWEEN FRAMES 29 AND 30. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LEFT BEAM GUSSET IS CORRODED BETWEEN FRAMES 25 AND 26. REMOVED CORROSION IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LEFT GUSSET IN LAVATORY HAS CORROSION. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02. RETREATED AREA IAW EMB 145 CPM 51-21-02, 51-21-05. (M0

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL FLOORBOARD SUPPORT CORRODED AT FRAME 51-54. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST 1014/02. RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

THIS IS A LEVEL 2 FINDING, LEFT SILL CORRODED BETWEEN FRAMES 29 AND 30. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, CENTER BEAM GUSSET IS CORRODED BETWEEN FRAMES 30 AND 34. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02. TREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LEFT SILL CORRODED BETWEEN FRAMES 43 AND 44. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, TREATED AREA IAW EMB 145 CPT 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL IS CORRODED AT FRAME 39. REPAIRED RIGHT SILL AT FRAME 39 IAW EMB 145 GST-1014/02. (M)

Part: GUSSET — CORRODED (FUSELAGE)

ABI - THIS IS A LEVEL 2 FINDING. RIGHT GUSSET UNDER PILOTS CONTROL COLUMN AND RIGHT SEAT SEAT TRACK IS CORRODED. TREATED CORROSION ON RIGHT GUSSET AND RIGHT SEAT TRACK IAW EMB 145 CPM 51-21-04, 51-21-05, 51-21-06. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL CORRODED BETWEEN FRAMES 48 AND 49. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST 1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 58 AND 59. REMOVED CORRODED, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, LEFT SILL CORRODED AT FRAME 49. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL CORRODED BETWEEN FRAMES 43 AND 44. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST 1014/02. RETREATED AREA IAW EMB145 CPM 51-21-04 AND 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT CROSSMEMBER CORRODED AT FRAME 59. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02. TREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL CORRODED AT FRAME 20. REMOVED CORROSION AND FOUND TO BE ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, CENTER GUSSET IN LAVATORY HAS CORROSION. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT GUSSET IN LAVATORY HAS CORROSION. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02. RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. CROSS BEAM PROFILE AT FRAME 23 CORRODED. REMOVED AND REPLACED CROSS BEAM PROFILE IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. CABIN FLOOR CROSS BEAM AT FRAME 23 END BRACKET AT RIGHT SILL CORRODED. REMOVED AND REPLACED CROSS BEAM IAW EMB 145 SRM 51040-02. (M)

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

THIS IS A LEVEL 2 FINDING. LEFT HAT BEAM GUSSET IS CORRODED BETWEEN FRAMES 65 AND 68. INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, RIGHT HAT BEAM IN GALLEY CORRODED BETWEEN FRAMES 17 AND 19. REPAIRED RIGHT HAT BEAM IN GALLEY BETWEEN FRAME 17 AND 19 IAW GST-1014/02. (M)

Part: SILL — CORRODED (FUSLEAGE)

THIS IS LEVEL 2 FINDING. SERVICE DOOR AFT SILL CORRODED. REMOVED AND REPLACED DOOR SILL IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. GUSSET CORRODED AT FRAME 19 ON RIGHT HAT BEAM. BLENDED OFF CORROSION IAW EMB 145 CPM 51-41-02. REPAIRED IAW EMB GST 1014/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDNG, LEFT SILL CORRODED BETWEEN FRAMES 20-22. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02. RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

Part: SILL — CORRODED (FUSELAGE)

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

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

ABI - THIS IS A LEVEL 2 FINDING. RIGHT SILL IS CORRODED AT FRAME 39. REPAIRED RIGHT SILL AT FRAME 39 IAW EMB 145 GST-1014/02. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE)

ABI - THIS A LEVEL 2 FINDING. CABIN FLOOR CROSS BEAM CORRODED AT FRAME 23. REMOVED AND REPLACED CROSS BEAM IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. LEFT SILL IS CORRODED BETWEEN FRAMES 61 AND 62. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)

Part: O-RING — DAMAGED (BLEED AIR SYS)

ORD - FLT 4263 - DURING CLIMB-OUT, CREW NOTED RIGHT ENGINE BLEED LEAK INDICATION. CREW RETURNED TO FIELD IN ORD AND DECLARED AN EMERGENCY. REPLACED O-RING IN BLEED DUCT IAW EMB 145 AMM. NO FURTHER LEAKS NOTED. (M)

Part: CONNECTOR — DAMAGED (ANTI-ICE SYSTEM)

DFW - FLT 3951 - CREW REPORTED BLEED LEAK 1 AND WING 1 ANTI-ICE FAIL ON EICAS. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY FOR THE BLEED PROBLEM. GROUND RAN AIRCAFT WITH NO DEFECTS NOTED. MAINTENANCE REMOVED AND REPLACED CANNON PLUG FOR LEFT WING BURST SWITCH. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL BOX — MALFUNCTIONED (COCKPIT)

CID - FLT 4239 - DURING CLIMB CREW SELECTED GEAR UP AND RECIEVED LANDING GEAR AIR/GROUND AND LANDING GEAR MESSAGE ILLUMINATED ON EICAS. RIGHT MAIN LANDING GEAR DID NOT INDICATE UP AND LOCKED AND CREW REPORTED AIRCRAFT YAW WHILE PROBLEM WAS OCCURING. CREW RETURNED TO FIELD SAFELY WITH NO FURTHER INCIDENTS WERE OCCURRING. CREW RETURNED TO FIELD SAFELY WITH NO FURTHER INCIDENTS WERE REPORTED. REMOVED AND REPLACED LGEU IAW AMM. OPS CHECK GOOD. (M)

Part: HYDRAULIC SYSTEM — LACK OF LUBE (NR 1)

CRP - FLT 3827 - FLIGHT CREW DECLARED EMERGENCY REPORTING AN OVERHEAT INDICATION ON THE NR 1 HYDRAULIC SYSTEM. MAINTENANCE SERVICED HYDRAULIC RESERVOIR. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 3,278,353 hrs

CID - FLT 4248 - EMERGENCY FLOOR LIGHTING ROWS 1 THROUGH 7 INITIALLY COME ON AND SLOWLY FADE TO OFF. C/A 6-13-00 MAINTENANCE REMOVED AND REPLACED THE NR 2 POWER SUPPLY BATTERY. OPS CHECKED GOOD. (X)

Part: WARNING LIGHT — ACTIVATED (RT MLG)

ORD - FLT 4055 - DURING TAKEOFF, CREW NOTED LANDING GEAR DISAGREE MESSAGE AND RIGHT MAIN NOT UP AND LOCKED. FOUND LARGE AMOUNTS OF ICE AND SNOW ON GEAR. REMOVED SAME. PERFORMED RETRACTION TEST IAW AMM 32-30-00-700-801. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY)

JAN - FLT 3683 - AFTER LANDING ON TAXI, CARGO SMOKE LIGHT CAME ON. CREW DISCHARGED CARGO FIRE BOTTLES. AREA CHECKED, NO SIGNS OF FIRE OR SMOKE. REMOVED AND REPLACED BOTH SMOKE DETECTORS IN CARGO AREA. OPS CHECK GOOD. (M)

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY)

JAN - FLT 3683 - AFTER LANDING ON TAXI, CARGO SMOKE LIGHT CAME ON. CREW DISCHARGED CARGO FIRE BOTTLES. AREA CHECKED, NO SIGNS OF FIRE OR SMOKE. REMOVED AND REPLACED BOTH SMOKE DETECTORS IN CARGO AREA. OPS CHECK GOOD. (M)

Part: CONNECTOR — CONTAMINATED (MLG)

MSN - FLT 9120 - DURING TAKEOFF, RIGHT LANDING GEAR DID NOT SHOW UP AND LOCKED. CREW FOLLOW QRC PROCEDURES, PROBLEM STILL PERSIST. CREW RETURNED TO MSN SAFELY. FOUND DE-ICER FLUID HAD BEEN SPRAYED ON LANDING GEAR AREA. CLEANED CANNON PLUG AND CONTACTS ON PROXIMITY SWITCHES. SWUNG GEAR, OPS CHECK GOOD. (M)

Part: FIRE DETECTOR — INOPERATIVE (CARGO BAY)

ORD - FLT 4266 - BAGGAGE SMOKE WARNING INDICATOR ILLUMINATED AFTER LANDING. VISUALLY CONFIRMED NO SMOKE. BAGGAGE EXTINGUISHER BOTTLES WERE DISPENSED. NO FURTHER INCIDENTS. REMOVED AND REPLACED SMOKE DETECTOR AND BOTH EXTINGUISHERS. PERFORMED OPS CHECK OF SYSTEM, OPS CHECK GOOD. (M)

Part: FIRE BOTTLE — DISCHARGED (CARGO BAY)

ORD - FLT 4266 - BAGGAGE SMOKE WARNING INDICATOR ILLUMINATED AFTER LANDING. VISUALLY CONFIRMED NO SMOKE. BAGGAGE EXTINGUISHER BOTTLES WERE DISPENSED. NO FURTHER INCIDENTS. REMOVED AND REPLACED SMOKE DETECTOR AND BOTH EXTINGUISHERS. PERFORMED OPS CHECK OF SYSTEM, OPS CHECK GOOD. (M)

Part: FIRE BOTTLE — DISCHARGED (CARGO BAY)

ORD - FLT 4266 - BAGGAGE SMOKE WARNING INDICATOR ILLUMINATED AFTER LANDING. VISUALLY CONFIRMED NO SMOKE. BAGGAGE EXTINGUISHER BOTTLES WERE DISPENSED. NO FURTHER INCIDENTS. REMOVED AND REPLACED SMOKE DETECTOR AND BOTH EXTINGUISHERS. PERFORMED OPS CHECK OF SYSTEM, OPS CHECK GOOD. (M)

Part: SEALS — FAILED (CARGO BAY)

GRR - FLT 4286 - BLEED LEAK INDICATED ON EICAS. BAGGAGE SMOKE WARNING ALSO CAME ON DURING FLIGHT. DISCHARGED FIRE EXTINGUISHER. REMOVED AND REPLACED BLEED SEALS AT COUPLING IN CARGO BAY FOR NR 1 BLEED SYSTEM. AIRCRAFT FERRIED TO ORD FOR FIRE EXTINGUISHER REPLACEMENT AND FURTHER TROUBLESHOOTING AND THEN RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ORD - FLT 4233 - AFT EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT LOCATION NR 4. OPERATIONAL CHECK GOOD. (M)

Part: SMOKE DETECTOR — FAILED (CARGO COMPT)

DFW - FLT 3502 - BAGGAGE SMOKE LIGHT CAME ON. USED BOTH FIRE EXTINGUISHERS. VERIFIED EVENT AS A FALSE WARNIGN. REMOVED AND REPLACED FIRE EXTINGUISHERS. REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTORS. FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — FAILED (CARGO COMPT)

DFW - FLT 3502 - BAGGAGE SMOKE LIGHT CAME ON. USED BOTH FIRE EXTINGUISHERS. VERIFIED EVENT AS A FALSE WARNIGN. REMOVED AND REPLACED FIRE EXTINGUISHERS. REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTORS. FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

ORD - FLT 4115 - FIRST OFFICER'S MAP LIGHT SOCKET SHORTED OUT AND CAUSED SMOKE IN THE COCKPIT. MEL'D COCKPIT LIGHTING. REMOVED AND REPLACED MAP LIGHT ASSEMBLY AND RHEOSTAT. OPERATIONAL CHECK GOOD. CLEARED MEL. REF: OPER CONTROL NR 98ZZZX4101. (X)

Part: RHEOSTAT — INOPERATIVE (COCKPIT)

ORD - FLT 4115 - FIRST OFFICER'S MAP LIGHT SOCKET SHORTED OUT AND CAUSED SMOKE IN THE COCKPIT. MEL'D COCKPIT LIGHTING. REMOVED AND REPLACED MAP LIGHT ASSEMBLY AND RHEOSTAT. OPERATIONAL CHECK GOOD. CLEARED MEL. REF: OPER CONTROL NR SIMA982662.

Part: FADEC 1A — FAILED (LEFT ENGINE)

ORD - FLT 4033 - THROUGH 13,000 FEET, LEFT ENGINE FLAMED OUT. TRIED TO RESTART, BUT AT LIGHT OFF, THE RAM AIR ADVISORY LIGHT CAME ON. DISCONTINUED START. REMOVED AND REPLACED FADEC 1A AND FADEC 1B. OPERATIONAL CHECKED WITH NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FADEC 1B — FAILED (LEFT ENGINE)

ORD - FLT 4033 - THROUGH 13,000 FEET, LEFT ENGINE FLAMED OUT. TRIED TO RESTART, BUT AT LIGHT OFF, THE RAM AIR ADVISORY LIGHT CAME ON. DISCONTINUED START. REMOVED AND REPLACED FADEC 1A AND FADEC 1B. OPERATIONAL CHECKED WITH NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)