N614AE

Part: IGNITER — FAILED (NR 2 ENGINE) · airframe 45,818 hrs · 42,541 cycles

#2 ENG HUNG START AT 32% N2. FOLLOWE BY ODOR IN CABIN....FIX: R&RD B IGNITOR IAW MM 74-21-10 GROUND RUN A/C, OPS CHECK GOOD.OK FOR SERVICE

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 45,569 hrs · 42,247 cycles

NR 1 HYD LOW QTY MSG EICAS MSG IN FLIGHT. QTY CONTINUIOUSLY TRICKLED DOWN FOR WHOLE FLIGHT. R & R NR 1 ENGINE DRIVEN PUMP IAW AMM 29-10-01. PERFORMED A LEAK TEST IAW AMM TASK 29-10-00-860-801-A/200, OPS CHECKED GOOD, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,517 hrs · 42,183 cycles

NDIS 614 33-50 0013140 25SEP19 SBY CLOSE SERVICE DOOR EXTERNAL LIGHT IS INOP (EMERGENCY LIGHT) 27863 00 SSM FACT 25SEP19 10:34 SBY R+R SERVICE DOOR EXTERNAL LIGHT ASSY IAW AMM 33-50- 10 (EMERGENCY LIGHT

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 41,500 hrs · 27,625 cycles

SERVICE DOOR HINGE EMERGENCY EXIT LIGHT INOP.... FIX: R&R D SERVICE DOOR HINGE EMEGENCY LIGHT LAMP IAW AMM TASK 33-50-10-000/400-801-A.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 44,463 hrs · 40,944 cycles

614 21-01 2099092 20MAR19 PHL ASSGN DURING CRUISE CREW SMELLED ODOR IN COCKPIT, SELECTED W/S HEAT OFF, ODOR DISAPPEARED. UPON TURNING W/S HEAT BACK ON, NOTICED HIGHER THAN NORMAL ELECTRICAL DRAW ON W/S HEAT 2. MAINTENANCE R&R GLARESHIELD AND NUMBER 2 W/S TERMINAL COVER FOR INSPECTION PURPOSES MEL 20MAR19 16:45 PHL C07913 30-15 WINDSHIELD HEATING SYS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,369 hrs · 40,831 cycles

NDIS 614 33-51 0008490 05MAR19 RIC CLOSE SERVICE DOOR EMERGENCY LIGHT INOP 27625 00 NGR FACT 05MAR19 11:53 RIC R/R EMERGENCY LIGHT BULB ON SERVICE_DOOR IN REF TO AMM 33-50-09-000/400-801-A.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 43,953 hrs · 40,329 cycles

RT OVER WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT OVER WING EMERGENCY LIGHT LAMP IN REF TO AMM 33-50-10-000/400-801-A. OK FOR SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,685 hrs · 40,026 cycles

EMERGENCY EXIT SIGN BY THE MAIN DOOR WAS INOPERATIVE. R & R THE EMERGENCY EXIT SIGN, OPS CHECKED GOOD. COVER SECURED.

Part: A/C PACK — OUT OF ADJUST (AC BAY) · airframe 43,523 hrs · 39,837 cycles

PACK 1 O/L MESS. ADJUSTED TEMPERATURE SETTING, LIGHT EXTINGUISHED. OPERATED SYSTEM FOR 30 MINUTES, NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: DOOR SILL — CORRODED (FRAMES 65-67) · airframe 43,213 hrs · 39,494 cycles

CARGO DOOR SILL IS CORRODED IN SEVERAL PLACES BETWEEN FRAMES 65 AND 67. R & R THE DOOR SILL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT IN COCKPIT CEILING, LIGHT NR 7 IS INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD.

Part: LIGHT — MISINSTALLED (RT OVERWING) · airframe 39,777 hrs · 36,579 cycles

RIGHT OUTER OVERWING EMERGENCY LIGHT IS UPSIDE DOWN. CORRECTLY REPOSITIONED RT OUTER OVERWING EMERGENCY LIGHT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,486 hrs · 36,356 cycles

RIGHT WING OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT WING OVERWING EMERGENCY LIGHT BULB. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,429 hrs · 36,310 cycles

RIGHT AFT WING FUSELAGE FAIRING EXTERIOR FLOOD LIGHT IS INOPERATIVE. REPLACED THE LAMP RT AFT WING FUSELAGE FAIRING EXTERIOR FLOOD LIGHT. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,429 hrs · 36,310 cycles

SERVICE DOOR EXTERIOR FLOOD LIGHT IS INOPERATIVE. R & R SERVICE DOOR EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: LEAD — BROKEN (CABIN) · airframe 38,975 hrs · 35,930 cycles

NUMBER 8 EMER LIGHT STRIP HAS BROKEN LEAD. R & R NR 8 EMER LIGHT FLOOR STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: GUSSET — DAMAGED (FUSELAGE) · airframe 38,975 hrs · 35,930 cycles

LEFT FLOOR GUSSET UNDER COCKPIT FLOOR PANEL 221GF, FASTENER HOLE DAMAGED. REPAIRED LT FLOOR GUSSET UNDER COCKPIT FLOOR WHERE DAMAGED FASTENER HOLE WAS IAW ERS-EM-53MR-1677.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,975 hrs · 35,930 cycles

LEFT UPPER FUSELAGE SKIN CRACKED AT FIRST FASTENER BELOW STRINGER 2L ON FRAME 75. ACCOMPLISHED REPAIR OF LT REAR FUSELAGE I SKIN IAW ERS-EM-53MR-1689.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 38,975 hrs · 35,930 cycles

EMERGENCY FLOOR LIGHT STRIPS NR 2 & 3 INOPERATIVE. R & R NR 3 EMER ACFT INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,975 hrs · 35,930 cycles

EXTERNAL SKIN OF FUSELAGE HAS A LIGHTNING STRIKE AFT FRAME 19, BETWEEN STRINGER 18R & 19R. PERFORMED REPAIR TO EXTERNAL SKIN AFT FRAME 19, STRINGER 18R - 19R IAW SRM 53-21-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,975 hrs · 35,930 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED FIRST FASTENER BELOW STRINGER 2R. REPAIRED FRAME 75 IAW ERS-EM-53MR-1688.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,975 hrs · 35,930 cycles

FRAME 68, Z FRAME CRACKED UNDER CARGO DOOR HOLD OPEN ROD CUP BRACKET. PERFORMED REPAIR OF FRAME 68, Z FRAME IAW ERS-EM-53MR-16821.

Part: STOP FITTING — GOUGED (CARGO DOOR) · airframe 38,975 hrs · 35,930 cycles

CARGO DOOR AFT CONTINUOUS STOP IS GOUGED. R & R CARGO DOOR AFT CONTINUOUS STOP IAW ERS-EM-5200-440 & SRM 51-40-02.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 38,973 hrs · 35,928 cycles

EMERGENCY FLOOR LIGHT STRIPS NR 2 & 3 INOPERATIVE. R & R NR 3 EMER ACFT INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,973 hrs · 35,928 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AT 1ST FASTENER BELOW STRINGER 2R ON FRAME 75, APPROX 1/2" LONG. REPAIRED RT UPPER FUSELAGE SKIN AT 1ST FASTENER BELOW STRINGER 2R ON FRAME 75 IAW ERS-EM-53MR-1688.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,973 hrs · 35,928 cycles

FRAME 68, Z FRAME CRACKED UNDER CARGO DOOR HOLD OPEN ROD CUP BRACKET. PERFORMED REPAIR TO FRAME 68, Z FRAME UNDER CARGO DOOR HOLD OPEN ROD CUP BRACKET IAW ERS-EM-53MR-1681. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,973 hrs · 35,928 cycles

LEFT UPPER FUSELAGE SKIN CRACKED AT 1ST FASTENER BELOW STRINGER 2L ON FRAME 75, APPROX 3/8" LONG. EASI 8071 USED, 100-500 KHZ PROBE, FREQ=400, V-GAIN=78.5, H-GAIN= 65.0, LPF=100. REPAIRED LT UPPER FUSELAGE SKIN AT FIRST FASTENER BELOW STRINGER 2L ON FRAME 75 IAW ERS-EM-53MR-1689. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,973 hrs · 35,928 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 & ABOVE STRINGER 2R, APPROX 3/8" LONG. CRACK ON RT REAR FUSELAGE 1 EXTERNAL SKIN AFT OF FRAME 75 ABOVE STRINGER 2R WILL BE CUT OUT & REPAIRED WITH FILLER & DOUBLER, SEE NRTC E471752 FOR CORRECTIVE ACTION.

Part: WIRE — BROKEN (CABIN) · airframe 38,973 hrs · 35,928 cycles

BROKEN WIRE, W192-8630-22, ON EMER FLOOR LIGHT STRIP 1. REPAIRED WIRE, W192-8630-22, ON EMER FLOOR LIGHT STRIP 1 IAW SWPM 20-21-00. SEE BOW 202054 FOR OPERATIONS CHECK.

Part: LEAD — BROKEN (CABIN) · airframe 38,973 hrs · 35,928 cycles

EMERGENCY LIGHT STRIP NR 8 HAS BROKEN LEADS. INSTALLED EMER LIGHT STRIPS NR 8 IAW AMM 33-50-12. SEE BOW 202054 FOR OPERATIONS CHECK.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 38,864 hrs · 35,823 cycles

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

Part: WIRE — BROKEN (CABIN) · airframe 38,748 hrs · 35,697 cycles

AFT EMERGENCY LIGHT STRIP BROKEN WIRE ON AIRCRAFT SIDE OF STRIP, IN FRONT OF LAVATORY. REPAIRED FLOOR STRIP WIRE IAW SWPM 20-21-00.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 38,721 hrs · 35,664 cycles

RIGHT EMER LIGHT OVERWING INOPERATIVE. R & R RT EMER LIGHT OVERWING. OPERATIONS CHECKED GOOD IAW AMM 33-50-01.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,631 hrs · 35,576 cycles

RIGHT EXTERIOR OVERWING EMER LAMP INOPERATIVE. R & R RT EXTERIOR OVERWING EMER LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SKIN — DENTED (RT HORIZ STAB) · airframe 38,039 hrs · 35,023 cycles

REPLACE RT STAB UPPER SKIN. R & R RT STAB UPPER SKIN IAW SRM 55-10-01 SI, 51-40-02, 51-20-03, 51-40-06, CPM 51-21-04, 51-21--05, 51-21-06, ETN-EM-55-073R2, ETN-EM-55-074, ETN-GN-51-016 R5, ETN-EM-51-120 R1 & ETN-EM-51-091 R4.

Part: SKIN — DENTED (LT HORIZ STAB) · airframe 38,039 hrs · 35,023 cycles

HAIL DAMAGE EVENT. REPLACE LT STAB UPPER SKIN. R & R LT STAB UPPER SKIN IAW SRM 55-10-01SI, 51-20-01, 51-20-03, 51-40-02, 51-40-06, ETN-EM-55-074 & ETN-EM-51-118.

Part: SKIN — DENTED (RT HORIZ STAB) · airframe 38,039 hrs · 35,023 cycles

REPLACE RT STAB UPPER SKIN. R & R RT STAB UPPER SKIN IAW SRM 55-10-01 SI, 51-40-02, 51-20-03, 51-40-06 & CPM 51-21-04, 51-21--05, 51-21-06, ETN-EM-55-073R2, ETN-EM-55-074, ETN-GN-51-016 R5, ETN-EM-51-120 R1 & ETN-EM-51-091 R4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,938 hrs · 34,934 cycles

SECOND FROM THE REAR AISLE EMER LIGHT INOPERATIVE. R & R AISLE EMER LIGHT LAMP IAW AMM 33-50-08. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,658 hrs · 34,687 cycles

RIGHT EXTERIOR OVERWING EMER LAMP INOPERATIVE. R & R RT EXTERIOR OVERWING EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 37,365 hrs · 34,447 cycles

AFTER LANDING GEAR RETRACTION, THE NOSE GEAR DOORS DIDN`T FULLY CLOSE, CYCLED GEAR DOWN THEN UP, DID NOT FIX THE PROBLEM. RETURNED TO DEPARTURE. R & R WIRING HARNESS FOR PROXIMITY NR 3 NLG UPLOCK IAW 32-00-03 & PROXIMITY SWITCH NR 3 NLG IAW 32-63-03. OPS CHECKED GOOD IAW 32-30-00-700-801.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 37,314 hrs · 34,412 cycles

OVERWING EMER LIGHT RT WING INOPERATIVE. R & R OVERWING EMER LIGHT RT WING LAMP. OPERATIONS CHECKED GOOD IAW AMM 33-50-07.

Part: ELECTRICAL BOX — MALFUNCTIONED (E&E BAY) · airframe 37,198 hrs · 34,314 cycles

IAW NR 1 OF THIS LOG PAGE AFTER START ENG 1, DURING TAXI, STRONG ELEC BURNING SMELL IN COCKPIT & GALLEY AREA. PERFORMED GVI INSPECTION FOR SMOKE SMELL & BURNT EVIDENCE AT FWD AVIONICS & RT POWER CONTROL DISTRIBUTION BOX IAW AMM 24-65-01.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 37,198 hrs · 34,314 cycles

DURING TAXI, AFTER STARTING NR 1 ENG, STRONG ELEC BURNING SMELL IN COCKPIT & GALLEY AREA. BOTH ENGS RUNNING WITH APU FEEDING THE PACKS NO SMOKE OR FIRE VISIBLE. COMPLIED WITH ETN EM-72-034 FOR ENG ODOR EVENT TROUBLESHOOTING SUPPLEMENT. PERFORMED GVI OF MAIN CABIN & COCKPIT. OK FOR SERVICE SEE ITEM 4 OF THIS LOG PAGE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,976 hrs · 34,125 cycles

RIGHT EXTERIOR AFT OVERWING EMER LIGHT IS INOPERATIVE. LAMPED THE RT EXTERIOR AFT OVERWING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,976 hrs · 34,125 cycles

CABIN EMER LIGHTS INOPERATIVE. FLOOR PROXIMITY 4 & 5 LT EXIT IDENTIFIER & RT EXIT IDENTIFIER. R & R INVERTER NR 5 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 36,727 hrs · 33,925 cycles

FIRST OFFICER`S FLASHLIGHT ON & OFF SWITCH IS BROKEN. THE SWITCH FELL OFF THE LIGHT. R & R FIRST OFFICER'S FLASHLIGHT. OPERATIONS CHECKED GOOD IAW AMM CH 33-51-01.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 36,605 hrs · 33,812 cycles

RAMP PERSONNEL REPORTED A BURNING SMELL IN THE CARGO COMPARTMENT UPON OPENING THE CARGO DOOR. REF THIS LOG PAGE ITEM 2 FOR CORRECTIVE ACTION. R & R FWD & AFT SMOKE DETECTORS IAW AMM 26-15-01. FOUND DETECTORS DIRTY & SMELL BURNT. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,498 hrs · 33,718 cycles

BOTH LT & RT OVERWING INTERIOR EMER HATCH LIGHTS INOPERATIVE. R & R BULBS IAW MM 33-50-07. OPERATIONS TESTED GOOD IAW MM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,419 hrs · 33,665 cycles

SERVICE DOOR EMER STAIR LIGHT INOPERATIVE. R & R SERVICE DOOR EMER STAIR LIGHT BULB. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 36,268 hrs · 33,543 cycles

ELONGATED HOLE ON LT ELEVATOR LOWER INBD LE. PERFORMED REPAIR ON T ELEVATOR LOWER INBD LE IAW ERS-EM-55MR-129.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 36,422 hrs · 33,667 cycles

LEFT ELEVATOR HAS DENT WITH GOUGE ON BOTTOM MID SKIN. PERFORMED REPAIR ON LT ELEVATOR BOTTOM MID SKIN IAW ERS-EM-55MR-141.

Part: SKIN — DAMAGED (ELEVATOR) · airframe 36,268 hrs · 33,543 cycles

HAIL DAMAGE EVENT, REPLACE ELEVATOR MID SKIN. FABRICATED ELEVATOR MID SKIN IAW ERS-EM-55MR-126.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,675 hrs · 33,068 cycles

EMERGENCY BATTERY POWER SUPPLY NR 3 INOPERATIVE. R & R BATTERY ASSEMBLY & CHARGER FOR EMERGENCY BATTERY POWER SUPPLY NR 3 IAW WC 33-700-19. OPERATIONS CHECKED IAW WC 33-700-17.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 34,642 hrs · 32,247 cycles

COCKPIT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IN COCKPIT IAW AMM 33 50 16. OPERATIONS CHECKED GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,330 hrs · 31,973 cycles

INTERNAL SKIN CORRODED BETWEEN FRAMES 13 AND 14 AND STRINGERS 19L AND 18R. REPAIRED SKIN IAW EO EM-53MR-2224.

Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 34,330 hrs · 31,973 cycles

CARGO DOOR HAS CORROSION AROUND SCREW HOLES ON FWD SIDE. PERFORMED PERMANENT REPAIR OF CARGO DOOR IAW EO EM-52MR-380.

Part: LIGHT — CHAFED (CABIN) · airframe 34,330 hrs · 31,973 cycles

FOUND FLOOR PROXIMITY LIGHT WIRES AT FR 33 BETWEEN STRINGERS 15L AND 16L DAMAGED. REPAIRED 2 FLOOR PROXIMITY LIGHT WIRES CHAFED AT FRAME 33 BETWEEN STRINGERS 15L AND 16L IAW SWPM 20-21-00. FOUND DURING SHEET METAL REPAIR.

Part: SPAR — CRACKED (LT WING) · airframe 34,330 hrs · 31,973 cycles

LEFT WING SPAR III CRACKED. REPAIRED SPAR IAW EO EM-57MR-711.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,330 hrs · 31,973 cycles

FR 68, LT SHEAR TIE CORROSION ON LOWER PORTION ABOVE CARGO DOOR SILL. REPAIRED FR 68 SHEAR TIE IAW EO EM-53MR-1129, PART B.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,330 hrs · 31,973 cycles

EMERGENCY LIGHT AT FLOOR PANEL 251FF HAS A BROKEN WIRE AT FUSELAGE END. REPAIRED WIRE IAW SWPM 20-50-01.

Part: TUBE — CORRODED (LT ELEVATOR) · airframe 34,330 hrs · 31,973 cycles

LEFT ELEVATOR MASS BALANCE TUBE CORRODED. PERFORMED REPAIR IAW EO EM-5500-177, PART C .

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 33,138 hrs · 31,045 cycles

ON FLIGHT 2977 THE CREW REPORTED THAT DURING LANDING WHEN SELECTED FLAPS TO 9%. THE CREW RECEIVED A CAUTION MESSAGE FLAP FAIL AND EICAS INDICATION 0%. COMPLIED WITH AOM VO L 1 AND DECLARED AN EMERGENCY. THE CREW CALLED FOR CFR AS A PRECAUTIONARY MEASURE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AICRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT IAW EMB 145 AMM 27-53-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 32,553 hrs · 30,572 cycles

DURING B INSPECTION FOUND THE EMERGENCY FLOOR LIGHTING STRIP AT PANEL 241BF HAS BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (ANTI-ICE SYS) · airframe 32,499 hrs · 30,530 cycles

ON FLIGHT 4350 THE CREW REPORTED THAT WHILE DECENDING INTO ICING CONDITIONS THEY RECEIVED A WING ANTI-ICE FAIL MESSAGE FOLLOWED BY ICE COND ANTI- ICE INOPERABLE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED CMC = NO MESSAGES, PERFORMED OPERATIONAL CHECK IAW AMM 30-00-00-700-802-A, OPS CHECK OK (VERIFIED PRESSURES AT EACH EACH LOW PRESS MANIFOLD GREATER THAN 18 PSIG). THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,375 hrs · 30,423 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 INVERTER IAW EMB MM 33-50-11. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,375 hrs · 30,423 cycles

DURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR EMERGENCY EXIT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB AT THE SERVICE EMERGENCY EXIT DOOR IAW EMB MM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 31,882 hrs · 30,016 cycles

DURING MAINTENANCE INSPECTION FOUND THE UPPER AFT (LARGE) "EXIT" SIGN AT LEFT OVERWING EXIT IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK IAW 33-50-00-700-801-A AND THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CARGO BAY) · airframe 31,645 hrs · 29,825 cycles

DURING MAINTENANCE INSPECTION THE RAMP REPORTED A BURNED RUBBER ODOR IN THE CARGO AREA. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF CARGO COMPARTMENT AND LAV COMPARTMENT EMG NACELLES FOUND NO SMOKE OR BURNING OR BURNT ODORS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CRACKED (RT PYON) · airframe 31,396 hrs · 29,640 cycles

RT PYLON BOLT HOLE CRACKED. COMPLIED WITH PERMANENT REPAIR IAW EO EM-54MR-410, PART C.

Part: DISPLAY — UNSERVICEABLE (COCKPIT) · airframe 30,517 hrs · 28,927 cycles

FLIGHT 3541, CREW REPORTED EICAS BLANKED OUT AFTER ENGINES STARTED. REPORTED A STRONG ODOR OF BURNING PLASTIC. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EICAS DISPLAY UNIT IAW AMM 34-22-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,280 hrs · 28,749 cycles

DURING MAINTENANCE INSPECTION FOUND THE NUMBER 3 EMERGENCY FLOOR STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY FLOOR LIGHT STRIP LAMP IAW EMB 145 AMM 33-50-12-000-801-A AND 33-50-12-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 30,005 hrs · 28,532 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE NR 3 EMERGENCY LIGHT STRIP BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 30,006 hrs · 28,533 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE EMERGENCY LIGHT PROXIMITY STRIP NR 5 WIRES ARE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH OPERATIONAL CHECK IAW AMM 33-55-00 NO DEFECTS NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 30,020 hrs · 28,541 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 5 EMERGENCY LIGHT STRIP BY THE EMERGENCY EXIT HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT STRIP IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 29,369 hrs · 28,062 cycles

DURING MAINTENANCE BASE VISIT FOUND THE SERVICE DOOR SHROUD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. SERVICE DOOR EMERGENCY LIGHT LAMP NOT PROPERLY INSTALLED, REMOVED AND REINSTALLED SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRANSDUCER — FAILED (NR 3 WHEEL) · airframe 29,149 hrs · 27,899 cycles

ON TOUCHDOWN AND AFTER BRAKING APPLIED, IT FELT LIKE HALF OF THE BRAKING AUTHORITY WAS LOST. COULD FEEL IT GO FROM GOOD BRAKING TO MUSHY. AFTER GATE ARRIVAL NOTICED THAT BOTH OUTBOARD BRAKE TEMPS WERE MIDDLE OF THE AMBER SCALE AND BOTH I/B BRAKE TEMPS WERE IN MIDDLE OF GREEN SCALE. READ CMC AND FOUND BRK WHEEL SPD TRAX NR 3 FAIL, REMOVED AND REPLACED NR 3 BREAK WHEEL SPEED TRAX, AND PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM IAW FIM 32-41-00-810-816-A AND AMM 32-41-03-000-801-A.

Part: TIRE — SEPARATED (NR 4) · airframe 28,805 hrs · 27,617 cycles

ON FLIGHT 4328 THE CREW REPORTED THE NR 4 TIRE MISSING APPROXIMATLEY 2 FEET OF TREAD. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 MAIN WHEEL ASSEMBLY IAW WORK 32-700-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,508 hrs · 27,403 cycles

ON FLIGHT 4564 DURING CRUISE AT FLIGHT LEVEL 370 THE CREW REPORTED AN ELECTRICAL ODOR IN THE COCKPIT. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO SAV. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED COCKPIT, RAN ALL ELECTRICAL SYSTEMS. RAN APU AND BLEED SYSTEM AND HAD CREW RUN ENGS/BLD/PACK CHECKED ALL SYSTEMS WITH APU/GPU/BATT. NO DISCREPANCIES FOUND. PARTS REMOVED OR REPLACED. OK FOR SERVICE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,407 hrs · 27,325 cycles

FOR FLIGHT 4061 DURING THE PREFLIGHT INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-020-003-A00 AND EMB AMM 33-50-10-420-003-A00. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-00-700-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 27,227 hrs · 26,439 cycles

ON FLIGHT 3311 JUST PRIOR TO LANDING (ABOUT 200 FL AFL) RECEIVED BAGGAGE SMOKE MESSAGE ON EICAS AFTER CLEARING RUNWAY. PERFORMED EPC MEMORY ITEMS -FIRED BAGGAGE EXTINGUISHER. FLIGHT ATTENDANT CONFIRMED NO FIRE BY VISUAL INSPECTION. CRASH, FIRE AND RESCUE CONFIRMED NO HEAT BY INFRARED. TAXIED TO GATE SHORTLY PRESSING BAGGAGE SMOKE BUTTON. RECEIVED BAGGAGE EXTINGUISHER BOTTLE INOPERABLE MESSAGE ON EICAS. BAGGAGE SMOKE LIGHT THEN EXTINGUISHED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BAGGAGE UPPER FIRE EXTINGUISHER BOTTLE IAW AMM 26-23-01. THE OPERATIONAL CHECK WAS GOOD. REMOVED AND REPLACED THE BAGGAGE LOWER FIRE EXT BOTTLE IAW AMM 26-23-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,098 hrs · 26,350 cycles

FOR FLIGHT 4135 MAINTENANCE FOUND THE CAPTAINS FLASHLIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS EMERGENCY FLASHLIGHT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SLEEVE — DISCONNECTED (ACM) · airframe 25,425 hrs · 23,972 cycles

ON FLIGHT 2897 THE CREW REPORTED THAT BOTH PACKS FAILED INTERMITTENTLY DURING CLIMBOUT AND CONTINUED TO SO THROUGHOUT THE FLIGHT. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO FSM. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND SLEEVES BEHIND AIR CYCLE MACHINE DISCONNECTED, CONNECTED SLEEVES AND REMOVED AND REPLACED BOTH BLOWN SLEEVES ON THE LEFT AND RIGHT PACK IAW EMB 145 AMM 21-20-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAP — OUT OF ADJUST (CABIN DOOR) · airframe 25,271 hrs · 24,843 cycles

ON FLIGHT 3811 THE CREW REPORTED A LOUD WHISTLING SOUND FROM THE MAIN CABIN DOOR HEARD BETWEEN FLIGHT LEVEL 340 AND FLIGHT LEVEL 350 AND CONTINUOUSLY DURING CRUISE. NO SOUND WAS HEARD DURING THE CLIMB AND DESCENT. THE FLIGHT ATTENDANT REPORTED THE SOUND SEEMED TO BE EMANATING FROM THE TOP OF DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED THE UPPER DOOR FLAP IAW EMB AMM TASK 52-18-00-820-810-A. LEAK CHECKS WERE GOOD AT THIS TIME IAW EMB145 AMM 21-31-00-810-801-A ON GROUND. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 25,262 hrs · 24,837 cycles

ON FLIGHT 44262 DURING TAKEOFF THE CREW REPORTED FLAP FAIL AT 9 DEGREES. THE CREW ELECTED TO RETURN TO RDU. THE AIRCRAFT LANDED OVERWEIGHT BUT WAS UNDER THE 360 FEET PER MINUTE AT TOUCHDOWN, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOLLOWED FIM TASKS27-51-00-810-801A AND TASK 27-51-00-810-804A. PERFORMED FLAP RESET AND OPERATIONAL CHECK IAW AMM 27-51-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 25,098 hrs · 24,673 cycles

DURING THE MAINTENANCE BASE INSPECTION FOUND FRAME 65 HAS TOOLING MARKS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 65 IAW ENGINEERING ORDER EM-53MR-1473. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,098 hrs · 24,673 cycles

DURING MAINTENANCE CHECK FOUND A DENT IN THE RIGHT FORWARD FUSELAGE BETWEEN FRAMES 6-8. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH REPAIR IAW EO EM-53MR-1353 PART B. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,098 hrs · 24,673 cycles

DURING MAINTENANCE BASE INSPECTION FOUND CENTER OMEGA BEAM CORRODED AT FRAME 25. 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: FITTING — DAMAGED (AILERON) · airframe 25,098 hrs · 24,673 cycles

DURING MAINTENANCE BASE INSPECTION FOUND RIGHT AILERON ACTUATOR FITTING TO BE DAMAGED BEYOND LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED AILERON ACTUATOR FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,098 hrs · 24,673 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE INSPECTION FOUND LEFT OMEGA BEAM AT CARBON CROSS MEMBER TO BE CORRODED AT FRAME 54. 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 25,098 hrs · 24,673 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 33. 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: CONTROL LEVER — DEFECTIVE (COCKPIT) · airframe 24,141 hrs · 23,898 cycles

ON FLIGHT 4005 A LANDING GEAR DISAGREE WARNING ON EICAS APPEARED AFTER THE LANDING GEAR HANDLE WAS MOVED INTO THE UP POSITION AFTER TAKEOFF. ALL THREE LANDING GEAR INDICATOR LIGHTS INDICATED YELLOW. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IAW EMB-145 AMM 32-32-02. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN)

ON FLIGHT 3762 ON TAKEOFF CREW REPORTED A BURNING OIL ODOR. AIRCRAFT REMOVED FROM SERVICE. PERFORMED ETN EM-72-034R4, AND REMOVED AND REPLACED LT ENGINE PER WORK CARD 71-000-000 OPERATIONAL CHECKED GOOD. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. (A)

Part: FADEC — FAILED · airframe 20,264 hrs · 20,404 cycles

ON FLIGHT 3530 ,CREW REPORTED NUMBER 1 ENGINE FLAME OUT EN ROUTE AT 16,000 FT 310KTS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED 1A AND 1B FADEC IAW ROLLS ROYCE MM 73-22-01 AND REMOVED AND REPLACED LEFT ENGINE FPMU IAW ROLLS ROYCE MM 73-21-10. OPERATION CHECK GOOD. NO LEAKS NOTED. FOUND FADCU HARNESS AT CONNECTION P8 PIN A BURNED. REMOVED AND REPLACED NR 1 ENG BLUE FADEC A IAW ROLLS ROYCE MM 76-11-20. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 20,245 hrs · 20,388 cycles

AIRCRAFT WAS REMOVED FROM SERVICE. DURING MBV INSPECTION THE BAGGAGE DOOR OPENING LOWER CENTER SILL WAS FOUND CORRODED. REMOVED AND REPLACE WITH NEW SILL PN 145-25480-603 IAW EMB 145 SRM 51-40-02 AND 51-20-03. AIRCRAFT RETURNED TO SERVICE.

Part: O-RING — LEAKING (NR 1 BLEED) · airframe 19,772 hrs · 19,999 cycles

DURING CLIMB-OUT, NR 1 BLEED LEAK INDICATION EXTINGUISHED ONCE BLEED VALVE WAS CLOSED RETURNED TO DFW. REMOVED AND REPLACED BLEED LINE O-RING AT JOINTS 7, 9, 11, 17 AND JOINT ABOVE 17 FOR NR 1 BLEED IAW EMB-145-AMM 36-11-10, LEAK CHECK GOOD AIRCRAFT RETURNED TO SERVICE.

Part: HOSE — DAMAGED (HYD SYSTEM) · airframe 19,589 hrs · 19,812 cycles

IMMEDIATELY AFTER TAKEOFF WHEN GEAR LEVER HANDLE PLACED IN "UP" POSITION RECEIVED EICAS MESSAGES "LG LEVER DISAGREE "HYD SYS 1 FAIL" HYD SYS 1 INOP" HYD 1 LOW QTY" E1 HYD PUMP FAIL. DECLARED AN EMERGENCY AFTER A FLYBY CREW LANDED UNEVENTFULLY. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR UP HYDRALIC HOSE P/N 145-70242-401. REPLACED NR 1 EMDP P/N MPEV30086 S/N MS684677. REPLACED E1 HYD PUMP P/N 971808 MOD D S/N MX611193. REPLACED 3 HYD FILTERS P/N 31829-3. AIRCRAFT RETURNED TO SERVICE.

Part: HYDRAULIC SYSTEM — MULTIPLE FAIL · airframe 19,589 hrs · 19,812 cycles

IMMEDIATELY AFTER T/O WHEN GEAR LEVER HANDLE PLACED IN "UP" POSITION RECEIVED A MASTER WARNING EICAS MSG "LG LEVER DISAGREE". THE NOSE WHEEL SHOWED UP AND WHITE THE MAINS SHOWED DOWN AND RED. THE HYD FLUID INDICATED ZERO WITH NO PRESS ON THE LT HYD SYSTEM. CREW ALSO HAD ASSOCIATED EICAS MESSAGES "HYD SYS 1 FAIL" HYD SYS 1 INOP" HYD 1 LOW QTY" E1 HYD PUMP FAIL. CREW DECLARED AN EMERGENCY, CREW WAS ABLE TO GET THE LANDING GEAR DOWN AND LOCKED. AFTER A FLYBY CREW LANDED UNEVENTFULLY.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 18,685 hrs · 19,072 cycles

CABIN EMERGENCY LIGHT WILL NOT STAY ILLUMINATED. REMOVED AND REPLACED FOUR EMERGENCY POWER PACKS IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: ADC — FAILED (NR 1) · airframe 18,407 hrs · 18,813 cycles

NUMBER ONE AIR DATA COMPUTER FAILURE, DIVERTED TO LRD. PERFORMED PITOT LEAK CHECK IAW EMB AMM 34-13-00 WITH NO DEFECTS. OPERATIONAL CHECK GOOD IAW EMB AMM 34-15-00. RETURNED AIRCRAFT TO SERVICE.

Part: DUCT — BLOWN (BLEED AIR SYS) · airframe 17,728 hrs · 18,195 cycles

HEARD LOUD POP FOLLOWED BY EICAS BLEED 1 LEAK MESSAGE, LAVATORY SMOKE MESSAGE, BAGGAGE SMOKE MESSAGE, DISCHARGED BAGGAGE EXTINGUISHER - CABIN/FLIGHT DECK FILLED WITH SMOKE. EMERGENCY DECLARED AND RETURNED TO ORD. POST INSPECTION FOUND BLEED DUCT DISCONNECTED AND DAMAGE TO THE INSULATION UNDER CABIN FLOOR. REMOVED AND REPLACED DUCT, BLANKETS AND O-RINGS IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: FIREWALL — CRACKED (AFT FUSELAGE)

DURING 8 YEAR INSPECTION FOUND APU FIREWALL CRACKED AT LOWER RT MOUNT. INSTALLED NEW FIREWALL IAW SRM. (K)

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

DURING INSPECTION FOUND LT LWR SEAT TRACK FROM FRAMES 36-47 CORRODED. INSTALLED NEW SEAT TRACK IAW MM. AIRCRAFT RETURNED TO SERVICE. (K)

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

DURING IMBV INSPECTION, FOUND RT FWD IB SEAT TRACK FROM FRAMES 24-30 CORRODED. REMOVED AND INSTALLED NEW SEAT TRACK IAW MM. AC RETURNED TO SERVICE. (K)

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

DURING INSPECTION FOUND RT LWR SEAT TRACK FROM FRAMES 30-36 CORRODED. REPLACED SEAT TRACK IAW MM. AIRCRAFT RETURNED TO SERVICE. (K)

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

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

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

DURING HMBV INSPECTION FOUND LT LOWER SEAT TRACK FROM FRAME 36 TO 47 HAS CORRODED AREAS. INSTALLED NEW SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

DURING HMBV INSPECTION FOUND LT LOWER SEAT TRACK FROM FRAME 30 TO 36 CORRODED. REPLACED SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: SEAT TRACK — CORRODED (CABIN)

DURING HMBV INSPECTION, FOUND RT NR 3 SIDEWALL SEAT TRACK CORRODED. INSTALLED SERVICEABLE SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SEAT TRACK — CORRODED (CABIN)

DURING INSPECTION, FOUND NR 4 RT SIDEWALL SEAT TRACK IS CORRODED. REPLACED SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

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

DURING HMBV INSPECTION FOUND NR 2 RT SIDEWALL, SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: BEAM — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND OMEGA BEAM IS CORRODED AT CARBON CROSS BEAM ATTACHMENT AT FRAME 20. REPAIRED OMEGA BEAM BY INSTALING AN EXTERNAL DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

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

DURING HMBV INSPECTION FOUND SERVICE DOOR SILL CORRODED AROUND FASTENER HOLES. INSTALLED NEW SERVICE DOOR SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: CONTROL UNIT — INOPERATIVE (TAIL COMPARTMENT)

DURNG TAKEOFF AT 800 AGL CREW REPORTED PITCH TRIM ONE INOPERATIVE WITH CAS MESSAGE. WHEN AIRCRAFT WAS LEVELED BACKUP PITCH TRIM BECAME INOPERATIVE WITH NO MESSAGE. COMPLIED WITH APPROPRIATE CHECKLIST AND RECOVERED ALL PITCH TRIMS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT AND THE BACK UP TRIM SWITCH (P/N 145-34177-401) IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

FORWARD TWO EMERGENCY FLOOR STRIP LIGHTS INOPERATIVE AND BOTH FORWARD OVERHEAD EXIT SIGNS INOPERATIVE. RAI BATTERY POWER SUPPLY AND NR 1 EMERGENCY BATTERY POWER SUPPLY OFF, P/N 20131A AND S/N 65143, EMERGENCY BATTERY P/N 110049, S/N 13617. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING AN IMB MAINTENANCE, FOUND THE CARGO DOOR CUT OUT LOWER SILL CORRODED. 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: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV MAINTENANCE, FOUND CORROSION ON FORWARD DIGITAL. REMOVED CORROSION BY CUT OUT. FABRICATED A REPLACEMENT STRAP, TWO DOUBLERS AND SHIMS. REPAIRED IAW EMB 145 (SRM 145/1142 CHAPTER 53, REV 18) 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV MAINTENANCE, FOUND CORROSION ON GALLEY CENTER BEAM. REMOVED CORRODED GALLEY CENTER BEAM. INSTALLED NEW BEAM IAW EMB 145 (SRM 145/1142, CHAP 51 REV 18) 51-40-02, GST 1128/02, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMV MAINTENANCE, FOUND CORROSION ON LEFT OMEGA BEAM, PREVIOUS REPAIR, AT FRAME 20. REMOVED PREVIOUS REPAIR (CORROSION LIMITED TO PREVIOUS REPAIR). FABRICATED A DOUBLER ANGLE AND SHIMS AND FILLERS. REPAIR DONE IAW EMB145 (SRM 145/1142, CHAPTER 53, REV 17) 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV MAINTENANCE, FOUND CORROSION ON GALLEY RIGHT FLOORBEAM, THREE AREAS, BETWEEN FRAMES 20 AND 23. REMOVED CORROSION BY BLENDING. NDT PERFORMED, NO DEFECTS. FABRICATED THREE REPAIR DOUBLERS, REPAIR DONE IAW EMB GST-1491/02, AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN IMBV MAINTENANCE FOUND CORROSION ON LEFT HAND OMEGA BEAM BETWEEN FRAMES 20 AND 23. REMOVED CORROSION BY BLENDING. FABRICATED A REPAIR DOUBLER REPAIR DONE IAW SRM.

Part: SILL — CORRODED (FUSELAGE)

DURING AN IMBV MAINTENANCE FOUND CARGO DOOR LOWER SILL CORRODED. REMOVED SILL(BEAM). INSTALLED NEW SILL IAW SRM.

Part: FRAME — CHAFED (FUSELAGE)

ABI - DURING INSPECTION, FOUND FRAME 81 CHAFED ON LOWER EDGE. REPLACED CHAFED FRAME IAW EMB 145 SRM 145/1142 CHAPTER 51, REV 17, 51-40-02, AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — GOUGED (FUSELAGE)

ABI - DURING INSPECTION, FOUND STRINGER 19R GOUGED. BLENDED GOUGE. FABRICATED A DOUBLER ANGLE, AND TWO SHIMS IAW EMB GST-1448/02 ITEM 10 AND STANDARD SRM PRACTICES. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. GALLEY CENTER FLOOR SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT IAW EMB 145 SRM 51-20-01, 51-20-03, 51-40-01, 51-40-02, 51-40-04, 51-40-07. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. RIGHT BEAM GUSSET IN CARGO IS CORRODED. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. LEFT BEAM GUSSET IN CARGO IS CORRODED AT FRAME 61. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M)

Part: SKIN — DENTED (FUSELAGE)

DURING INSPECTION, FOUND DENT ON AFT LOWER FUSELAGE AFT OF FRAME 67, BETWEEN STRINGERS 20R AND 21R. REMOVED DAMAGED SKIN BY CUT OUT. FABRICATED A REPAIR DOUBLER, FILLER IAW EMB 145 SRM 145/1142, CHAPTER 53-21-01, EMB GST-1451/02, 2002 AND STANDARD SRM PRACTICES. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. LEFT FORWARD SILL IN CARGO IS CORRODED. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. RIGHT SILL IN CARGO IS CORRODED BETWEEN FRAME 68-71. REMOVED AND REPLACED RIGHT CARGO SILL IAW EMB 145 SRM 51-40-02. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE)

ABI - THIS IS A LEVEL 2 FINDING. RIGHT CROSSMEMBER IN CARGO IS CORRODED. REMOVED CORROSION AND PERFORMED NDT. FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. FORWARD AND AFT DIAMOND GUSSET ARE CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. RIGHT CABIN SILL CORRODED BETWEEN FRAMES 53 AND 55. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M)

Part: FRAME — CORRODED (FUSELAGE)

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

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

ABI - THIS IS A LEVEL 2 FINDING. RIGHT CABIN SILL CORRODED BETWEEN FRAMES 24 AND 28. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST 1491/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. RIGHT CABIN SILL BETWEEN FRAMES 28 AND 34 IS CORRODED. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. LEFT CABIN SILL CORRODED FROM FRAME 23 TO 26. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST 1491/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. CENTER GUSSET IN LAVATORY IS CORRODED. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. RIGHT SEAT TRACK PROFILE HAS CORROSION BETWEEN FRAMES 24 AND 29. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING. RIGHT GUSSET IN LAVATORY IS CORRODED. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491/02. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - THIS IS A LEVEL 2 FINDING. LAVATORY LEFT SILL IS CORRODED. BLENDED AND PERFORMED NDT, FOUND TO BE ACCEPTED AS IS IAW EMB GST-1491-02. (M)

Part: BATTERY — DISCHARGED (CABIN)

ORD - FLT 4370 - CREW REPORTED THAT DURING POST FLIGHT CHECK, THE EMERGENCY LIGHTS ON INSIDE OF SERVICE DOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY AND BATTERY CHARGER. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200127807. (M)

Part: MODULE — INOPERATIVE (CABIN)

TOL - FLT 4350 - CREW REPORTED THE CABIN EMERGENCY LIGHTS NOT CONTROLLABLE FROM THE FLIGHT ATTENDANTS PANEL. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANTS LIGHTING CONTROL MODULE IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DUCT — DAMAGED (AFT CARGO)

ORD - FLT 4262 - DURING FLIGHT, CREW REPORTED A NR 2 BLEED LEAK. AFTER LANDING CARGO FIRE WARNING LIGHT ILLUMINATED. CREW FIRED BOTTLES. MAINTENANCE FOUND A DAMAGED DUCT BEHIND AN AFT CARGO WALL. DUCT WAS REPLACED, OPS CHECK WAS GOOD. FIRE BOTTLES WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: MODULE — INOPERATIVE (GALLEY)

CMH - FLT 4008 - FLIGHT ATTENDANT EMERGENCY LIGHT CONTROL INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CONTROL MODULE IAW EMB MM. OPERATIONAL HECK GOOD AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL BOX — FAILED (SPOILERS)

MGM - FLT 3536 - DURING TAKEOFF ROLL, CREW NOTED SPOILER FAIL ACCOMPANIED WITH CONFIG WARNING. CREW ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. SPOILER CONTROL UNIT WAS REMOVED AND REPLACED, OPS CHECK GOOD. (M)

Part: LIGHT — CORRODED (OVERWING)

ORD - FLT 4022 - RIGHT AND LEFT EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. FOUND CORROSION ON LIGHT ASSY AND BULBS. CLEANED LIGHTS ASSY AND REMOVED AND REPLACED BULBS. OPS CHECK GOOD. (M)

Part: CONTROLLER — FAILED (COCKPIT)

ORD - FLT 4017 - AFTER TAKEOFF, CREW GOT A LANDING GEAR LEVER DISAGREE MESSAGE ON THE EICAS. GEAR WAS RECYCLED AND GOT THREE GREENS. AIRCRAFT RETURNED TO ORD WITHOUT FURTHER INCIDENTS. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)