N857AE

Part: LIGHT — INOPERATIVE (ROW 10) · airframe 32,393 hrs · 29,179 cycles

ROW 10 FLOOR EMERGENCY LIGHT STRIP DAMAGED. C/A RAR ROW 10 FLOOR EMERGENCY LIGHT STRIP IAW EMB 140 AMM 33-50-12. OPERATIONS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,278 hrs · 29,046 cycles

1ST LT EMERGENCY LIGHT STRIP INOPERATIVE. R & R THE EMERGENCY LIGHT STRIP IAW AMM 140 33-50-12. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,275 hrs · 29,043 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. DID NOT FIX. REPLACED #1 EMERGENCY BATTERY AND #1 CHARGER IAW EMB W/C 33-700-19 AND W/C 33-700-17. DID NOT FIX. REQUIRES FURTHER TROUBLESHOOTING.

Part: HANDLE — MALFUNCTIONED (PARKING BRAKE) · airframe 32,091 hrs · 28,865 cycles

PARKING BRAKE HANDLE CANNOT BE SET. REMOVED AND REPLACED EMERGENCY/PARKING BRAKE HANDLE IAW AMM 32-44-11. OP CHECKED GOOD.

Part: GUIDE — DIRTY (PAX DOOR) · airframe 32,038 hrs · 28,819 cycles

FLIGHT ATTENDANT STILL REPORTING PAX DOOR STICKY & DIFFICULT TO OPEN, 2ND WRITE UP ON ISSUE. CLEANED DOOR GUIDES AND LUBED ROLLERS, PERFORMED DOOR OPEN AND CLOSE IAW AMM 52-18-00 SEVERAL TIMES. DOOR IS OPERATING AS REQUIRED, DOES NOT STICK, ACFT RELEASED FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,937 hrs · 28,723 cycles

SKIN DENTED 5" AFT OF FR 19 AND 2.350" BELOW STR 1`2L.-C/A-DENTED FUSELAGE SKIN 5.000 "AFT OF FR 19 AND 2.350 BELOW STR RL 12L REPAIRED IN ACCORANCE WITH ETD 2020-145-012727 REV B. REPAIR DOUBLER RECORDED UENDER ADL 8570011. REPROTECTION (TOP COAT) COVER ON WC 53-2366 ITEM #10.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 31,937 hrs · 28,723 cycles

CORROSION ON FR 80 APU SHUNT AREA-C/A-CORROSION BLENDED OUT OF LIMIT ON FR 80 APU SHUNT AREA. ON FR 80 APU SHUNT AREA REPAIR PARTS ARE FABRICATED AS PER SRM 53-32-04 FIG 203. ON FR 80 APU SHUNT AREA, FR 80 REPAIR PART INSTALLED WITH SOLID RIVET IAW SRM 53-32-04. BONDING TEST OF BRACKET REINFORCEMENT FR 80 APU SHUNT AREA.DONE IAW AMM 2-13-21. FOUND SERVICEABLE. SEE ATTACHED NDT REPORT. APU SHUNT REMOVAL/INSTALLATION COVER ON TASK 35.

Part: PROFILE — CRACKED (VERTICAL STAB) · airframe 31,937 hrs · 28,723 cycles

VERT.STAB., AFT SPAR3, L/H PROFILE CRACKED ABOVE RUDDER 1 TOP CENTER HINGE FITTING.-C/A-VERT.STAB., AFT SPAR 3, L/H PROFILE ABOVE RUDDER 1 TOP CENTER HINGE FITTING REPAIRED AS PER ETD 2020-145-013336.

Part: SKIN — GOUGED (PAX DOOR) · airframe 31,937 hrs · 28,723 cycles

GOUGE ON PAX DOOR SKIN, ON AFT EDGE AND 10.00" ABOVE LOWER EDGE.-C/A-ON PAX DOOR SKIN GOUGE AREA STRIPED FOR INVESTIGATION. GOUGE ON PAX DOOR SKIN AT AFT EDGE AREA, 10'000" ABOVE LOWER EDGE REPAIRED IN ACCORDANCE WITH ETD2020-145-014040 REV C. PAINT COVER ON WC: 53-2366 ITEM 1 PASSENGER DOOR TRIM SEAL REMOVED FROM BOTTOM AFT CORNER ON 24" FOR ACCESS IAW AMM 52-18-04. PASSENGER DOOR TRIM SEAL BOTTOM AFT CORNER INSTALLED BACK IN ITS CHANNEL ON 24" IAW AMM 52-18-04. REPAIR DOUBLER ADDED TO ADL #8570078.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,937 hrs · 28,723 cycles

CHERRY MAX FOUND ON SKIN AT FR 25 BTW FR 18-19LH.-C/A-PAINT STRIPPED SKIN AT FR 75 BTW FR 18-19 L/H AS PER CPM 51-21-01. CHERRY MAX REMOVED AND CUT OUT PERFORMED ON SKIN TO REMOVE DAMAGE. L/H FUSELAGE SKIN AT FRAME "25 BTW STRINGER "18 & 19, REPAIRED IAW. ETD2020-145-014121 SEE ATTACHED NDT REPORT TORNGATS WO #14067 REPAIR DOUBLER ADDED TO ADL #8570079, PAINT COVERED AS WC 53-2366 ITEM #13.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,937 hrs · 28,723 cycles

CHERRY MAX FOUND ON SKIN AT FR 28 AND STR 17 LH.-C/A-PAINT STRIPPED SKIN AT FR 28 AND STR 17 L/H AS PER 51-21-01. AIR CONDITIONING DUCTS BETWEEN WINDOW L/H #4-5 REMOVED FOR ACDCESS IAW AMM 21-20-04. BUSHING FABRICATED IAW ETD 2020-145-014213 AND SRM 51-10-07 (FREEZE PLUG). L/H FUSELAGE SKIN AT FRAME #28 AND STRINGER #17, REPAIRED IAW ETD 2020-145-014213. PAINT COVER AS WC 53-2366 ITEM #12 REPAIR ADDED TO ADL #8570083. AIR CONDITIONING DUCTS BTW WINDOW L/H #4, 5, INSTALLED IAW AMM 21-20-04.

Part: TIRE — VIBRATION (NLG) · airframe 31,904 hrs · 28,684 cycles

EXCESSIVE NLG SHIMMY VIBRATION BETWEEN 20-40 KNOTS WITH STEERING CNTERED. NO VIBRATION OFF CENTER-C/A-REMOVED AND REPLACED LEFT NLG TIRE IAW WC 32-700-17

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 31,868 hrs · 28,645 cycles

FWD CABIN EMERGENCY EXIT SIGN AT SEAT 3BC LIGHT INOP-C/A-REMOVED AND REPLACED FWD CABING EMERGENCY EXIT SIGN LIGHT AT SEAT 3BC IAW EMB 140 AMM 33-50-13. OPS CHECK GOOD.

Part: CONTROL MODULE — FAILED (EMERGENCY LIGHTS) · airframe 31,372 hrs · 28,149 cycles

EMERG LT NOT ARMED CAUTION MSG ON TAKE OFF AT APPROX 100 KIAS. THEN INTERMITTENTLY APPROX EVERY 3 MIN IN FLIGHT.-C/A-UPON FUTHER INSPECTION FOUND C/P FOR COCKPIT EMER LT SWITCH TO BE LOOSE. RESECURRED C/W. VERIFIED NORMAL OPERATION. REF EMB 140 SWPM 20-50-00. NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED EMERG/OVHD PNL LT SWITCH PANEL IAW EMB 140 AMM 20-13-10. OPC GOOD IAW EMB 140 AMM 35-50-00. REMOVED AND REPLACED CONTROL MODULE IAW AMM 33-21-01. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 30,953 hrs · 27,770 cycles

DURING FLIGHT IN ICING CONDITIONS STAB A/ICE FAIL MESSAGE APPEARED, FOLLOWED BY ICE-COND - A/I INOP WARNING-C/A-CMC FAULT CODE 30-IPM75. FLIGHT CREW PLACARDED STAB ANTI-ICE SYSTEM. MEL 30-5 AUTH 090895D-C MOC 437847

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 29,785 hrs · 26,596 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN. C/A-PERFORMED GVI OF MAIN DOOR FOUND TWO AFT ROLLERS NOT MOVING CLEAN AND LUB ROLLERS AS PER AMM 53-21-02 OPC GOOD.

Part: SKIN — DENTED (FRAMES 22A-23) · airframe 29,173 hrs · 26,029 cycles

TRANSFERRED FROM AML 4424546 ITEM 3, FOUND LARGE DENT WITH GAUGE BETWEEN STGR 12R & 14R AND BETWEEN FR 22A & 23. W=4.875IN, L=9.125IN, DEPTH=0.218IN. THIS IS A MAJOR REPAIR-C/A-REPAIRED DENT IAW ERS-EM-53MR-3545

Part: STRINGER — CRACKED (FRAMES 22-23) · airframe 29,173 hrs · 26,029 cycles

STR 13R IS CRACKED BETWEEN FR 22A-23.-C/A-REMOVED AND REPLACED STR 13R BETWEEN FR 22A-23 IAW SRM 51-40-02

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,901 hrs · 24,872 cycles

FLOOR EMERGENCY LIGHT BETWEEN ROWS 7 AND 8 FOUND INOPERATIVE.

Part: PUMP — FAILED (NR 1 HYD SYSTEM) · airframe 27,901 hrs · 24,871 cycles

NR 1 ENGINE HYD PUMP FAILED. REMOVED AND REPLACED THE HYD PUMP IAW AMM 29-10-03.

Part: UPLOCK — FAILED (LT MLG) · airframe 27,599 hrs · 24,544 cycles

DURING RETRACTION, LEFT MLG DID NOT INDICATE UP INDICATION FOLLOWED BY LG LEVER DISAGREE WARNING MESSAGE REMOVED AND REPLACED LT MLG UPLOCK BOX IAW AMM 32-33-10. OPS CHECKED GOOD.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 27,552 hrs · 24,488 cycles

NR 1 ENGINE ANTI-ICE VALVE CYCLING OPEN & CLOSED. SHOULD REMAIN OPEN. EICAS MESSAGES WOULD COME AND GO AS WELL. PUTTING ICE DETECTION KNOB TO ENGINE OR ALL E1 STILL WOULD NOT OPEN ALSO RECIEVED ENG1 ANTI ICE OVERPRESSURE ADVISORY MESSAGE. DURING CYCLING OF ANTI-ICE VALVE. REMOVED AND REPLACED THE ENGINE ANTI-ICE VALVE IAW AMM 30-21-01. LEAK TESTED GOOD. REMOVED AND REPLACED ANTI-ICE TRANSDUCER IAW AMM 30-21-06. LEAK TESTED GOOD. PERFORMED AN ANTI-ICE SYSTEM OPERATIONAL TEST IAW AMM 30-00-00. OPS CHECKED GOOD.

Part: DAU — FAILED (NR 1) · airframe 27,425 hrs · 24,370 cycles

DAU NR 1A FAILED. TROUBLESHOOT IAW FIM 31-41-00. REMOVED AND REPLACED THE NR 1 DAU IAW AMM 31-41-00, OPS CHECKED GOOD, NO DFECTS NOTED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,335 hrs · 24,256 cycles

COCKPIT STEP EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11 OPC GOOD.

Part: DOOR FRAME — CORRODED (CARGO) · airframe 27,152 hrs · 24,001 cycles

CARGO DOOR FWD FRAME CORRODED AT 4 NUTPLATE HOLES. REPAIRED THE DOOR FRAME IAW ERS EM-52MR-822.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 27,152 hrs · 24,001 cycles

LEFT NR 3 EMERGENCY LIGHT HAS BROKEN WIRES. R & R THE WIRES IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 27,152 hrs · 24,001 cycles

LH FORWARD LOWER FAIRING EMERGENCY LIGHT HAS A BROKEN WIRE. REPAIRED THE WIRE IAW SWPM 20-21-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 27,152 hrs · 24,001 cycles

LT NR 1 EMERGENCY LIGHT HAS BROKEN WIRES. R & R THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 27,152 hrs · 24,001 cycles

EMERGENCY LIGHT NR 6 HAS A BROKEN WIRE. R & R THE EMERGENCY LIGHT CONNECTOR IAW SWPM 20-21-00. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,906 hrs · 23,826 cycles

COCKPIT STEP EMER LIGHT INOPERATIVE. R & R NR 1 EMER BATTERY & CHARGER IAW WC 33-700-19. REF ITEM 2 THIS NRWC FOR OPERATIONS CHECK. EMER LIGHTING BATTERY PN 2013-1A SN 85712.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 26,460 hrs · 23,480 cycles

FIRST OFFICER`S EMER FLASHLIGHT CRADLE BROKEN. R & R IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 26,075 hrs · 23,178 cycles

STRONG SMELL OF JET FUEL IN COCKPIT & CABIN WHILE TAXIING IN WITH ENGS SUPPLYING PACKS. SMELL WENT AWAY WITH APU RUNNING & SUPPLYING PACKS. COMPLIED WITH AE ETN EM-72-034. NO ODOR EVENT NOTED AT THIS TIME.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 25,704 hrs · 22,819 cycles

EMERGENCY FLASHLIGHT CRADLE ABOVE FLIGHT ATTENDANT SEAT BROKEN. R & R FLIGHT ATTENDANT FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A, OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 25,264 hrs · 22,402 cycles

COCKPIT FLASHLIGHT CRADLE BROKEN, CAPTAIN`S SIDE. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,264 hrs · 22,402 cycles

FLIGHT ATTENDANT FLASHLIGHT WAS DISCOVERED IN LAVATORY & INOPERATIVE. DEFERRED IAW MEL 25-53. INSTALLED FLIGHT ATTENDANT FLASHLIGHT IAW CMM 25-60-11. OPERATIONAL TEST GOOD. THIS ACTION RESTORED MEL.

Part: HANDLE — OUT OF POSITION (CABIN DOOR) · airframe 25,264 hrs · 22,402 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN. REPOSITIONED HANDLE BACK ON SPLINE IAW AMM 52-18-05. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,255 hrs · 22,394 cycles

FLIGHT ATTENDANT FWD JUMP SEAT FLASHLIGHT IS INOPERATIVE. REPLACED FLASHLIGHT IAW CMM 25-60-11.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 24,570 hrs · 21,779 cycles

LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. C/A R & R LT AFT OVERWING EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-07, OPERATIONS CHECKED GOOD.

Part: LINE — LEAKING (APU FUEL) · airframe 3,239 hrs · 21,248 cycles

FUEL ODOR IN FLIGHT DECK AFTER APU & NR 1 ENGINE START. RETURNED TO GATE, R & R APU "OUT" FUEL LINE AT FUEL CONTROL, REF AMM 49-32-01. OPS CHECKED GOOD, NO LEAKS NOTED OR FUEL ODOR IN COCKPIT. FOUND GROUND CONNECTION VALVE SPRING BROKEN REF AMM 21-22-04. SUSPECT LEAKING THRU AIR DUCTS. R & R CONNECTION VALVE SPRING REF AMM 21-22-04. OPS ARE GOOD.

Part: ACM — ODOR (LEFT) · airframe 23,795 hrs · 21,049 cycles

INTERMITTENT OIL ODOR AT VARIOUS TIMES DURING PACK OPERATION. ODOR WOULD OCCUR THEN VERY QUICKLY DISSIPATE. R & R LT ACM, OPS CHECKED GOOD IAW AMM 21-51-03 AND 21-51-00. PACKS WERE OPERATED UNTIL RESIDUAL ODOR WAS ELIMINATED. AIRCRAFT RETURNED TO SERVICE.

Part: ACM — ODOR (LEFT) · airframe 23,795 hrs · 21,049 cycles

SITTING AT GATE WITH PCA CONNECTED, STARTED TO SMELL EXTREMELY STRONG OIL ODOR. MX STARTED APU, DISCONNETED PCA, TURNED NR 2 AND SAME ODOR RETURNED IN COCKPIT NOT IN CABIN. R & R LT PACK ACM AND OPS CHECKED GOOD IAW AMM 21-51-03 AND 21-51-00. PACKS WERE OPERATED UNTIL RESIDUAL ODOR WAS ELIMINATED.

Part: ENGINE — FAILED (NR 1) · airframe 23,772 hrs · 21,028 cycles

DURING CRUISE FL 330, NOTICED OIL LEVEL WAS 7 QTS ON NR 1 ENGINE. NR 1 ENGINE ITT WENT INTO CAUTION SO THEY PULLED TL BACK HALFWAY. ITT CAME DOWN THEN SHOT INTO RED. NR 1 ENGINE SHUTDOWN ON ITS OWN AND THE COCKPIT FILLED WITH SMOKE. NO ENGINE FIRE INDICATION PRESENT. NO N2 ROTATION. DECLARED AN EMERGENCY, DIVERTED AND LANDED WITHOUT INCIDENT. WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE. ALL LEAK CHECKS, FUNCTIONAL CHECKS AND OPS CHECKS COMPLIED WITH, NO DEFECTS NOTED IAW WC 71-00-00. AIRCRAFT RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 23,490 hrs · 20,777 cycles

THE CREW REPORTED THE FOWARD CABIN FLASHLIGHT HOLDER HAS A BROKEN RETAINING CLIP. ITEM DEFERRED IAW MEL 25/23, AUTH 060617-C. R & R THE FLIGHT F/A FLASHLIGHT HOLDER IAW AMM 33-50-16. THE OPS CHECK WAS GOOD. MEL RESTORED. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,917 hrs · 20,230 cycles

FLIGHT 3260, EMERGENCY LIGHTS WERE DISCOVERED TO BE ON DURING THE NIGHT, EMERGENCY LIGHTS WERE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY PACK IAW AMM 23 50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR SEAL — WORN (PAX DOOR) · airframe 22,538 hrs · 19,944 cycles

DURING MAINTENANCE INSPECTION FOUND THE PASSENGER DOOR SEAL WORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR SEAL IAW EMB 140 AMM 52-18-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 22,538 hrs · 19,944 cycles

DURING B INSPECTION FOUND THE LEFT NR 8 EMERGENCY LIGHT STRIP HAS BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 8 EMERGENCY PROXIMITY LIGHT STRIP IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 22,538 hrs · 19,944 cycles

DURING B INSPECTION FOUND A BROKEN WIRE AT NR 6 EMERGENCY LIGHT STRIP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 6 EMERGENCY LIGHT STRIP IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,362 hrs · 19,807 cycles

ON FLIGHT 2832 THE CREW REPORTED THE EMERGENCY LIGHT BELOW THE COCKPIT DOOR WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY IAW AMM 33-50-04. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DEFECTIVE (FLASHLIGHT) · airframe 22,283 hrs · 19,735 cycles

ON FLIGHT 3340 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS EXTREMELY DIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT BULB CMM 25-60-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — UNSERVICEABLE (RT ENGINE) · airframe 22,138 hrs · 19,621 cycles

DURING MAINTENANCE DETERMINED THAT AN OIL SMELL APPEARED TO BE COMING FROM THE NR 2 ENGINE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE ZERO CARBON SEAL IAW RRMM 72-25-25 PERFORMED ENGINE RUNS IAW RRMM 72-00-00 AND ETN EM -72-034. THE LEAK AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 22,013 hrs · 19,486 cycles

ON FLIGHT 3007 THE CREW REPORTED THAT WHEN SELECTING PACK NR 2, PACK NR 2 DID NOT COME ON AND THERE WAS A SLIGHT BURNING SMELL. DEFERRED NR 2 PAC (AIR CONDITIONING) SYSTEM PER MEL 21-29. REMOVED AND REPLACED THE RIGHT AIR CYCLE MACHINE IAW EMB 140 AMM 21-51-03. THE OPERATIONAL CHECK WAS IAW EMB 140 AMM 21-51-00. NO SMELL NOTICED. MEL CLOSED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (FWD CABIN) · airframe 21,429 hrs · 18,838 cycles

FLIGHT 3809, THE CREW REPOTRED THE FLIGHT ATTENDANT'S FORWARD FLASHLIGHT DOES NOT INDICATE CHARGING WHEN STOWED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT'S FORWARD FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,268 hrs · 18,650 cycles

ON FLIGHT 3058 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAILED (LT MLG) · airframe 3,608 hrs · 18,372 cycles

ON FLIGHT 4608 THE CREW REPORTED THAT AFTER TAKEOFF RECEIVED EICAS 'LG AIR/GND FAIL." THE LANDING GEAR COULD NOT BE RETRACTED. IN THE AIR RECEIVED NUMEROUS ALERTS FOR 'TAKEOFF, TRIM' AND ''TAKEOFF FLAPS". THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE CREW REPORTED THAT AFTER LANDING THE STEERING AND BRAKES FUNCTIONED NORMALLY. STICK SHAKER WAS ACTIVATED DURING THE TAXI IN ALONG WITH NUMEROUS OTHER ALERTS. THE AIRCRAFT WAS REMOVED FROM SERVICE. DURING TROUBLESHOOTING FOUND CMC MSG 'LG LEFT WOW PROX SWITCH FAIL." AND "LG RIGHT WOW PROX SWITCH FAIL. REMOVED AND REPLACED LEFT GEAR NR 2 PROX SWITCH & RIGHT GEAR NR 2 PROX SWITCH (WOW) IAW EMB 140 AMM 32-63-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 20,977 hrs · 18,321 cycles

ON FLIGHT 3061 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT. THE CREW RECEIVED A LANDING /AIR GROUND FAIL MESSAGE ON ECIAS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED (LGEU) IAW ERJ-140 AMM 32-32-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 20,774 hrs · 18,087 cycles

FLIGHT 3008, CREW REPORTED A LIGHTNING STRIKE ON APPROACH INTO LAX AT 8000 FT. ON EICAS SPS ADVANCE AND STICK PUSHER FAIL MESSAGE. ALL PFD'S, MFD'S AND EICAS WENT BLANK FOR 2 SECONDS. ALL SCREENS ARE NOW DISCOLORED. PASSENGERS REPORT LIGHTING EXITED AT ROW 16. UNKNOWN WHERE IT ENTERED. THE CREW DETECTED A SLIGHT ODOR OF BURNED WIRING. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED LIGHTNING STRIKE INSPECTION IAW WORK CARD 05-200-00. REMOVED AND REPLACED RIGHT, LEFT PFD SCREEN AND LEFT MFD SCREEN IAW AMM 34-22-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,542 hrs · 17,838 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. DURING TROUBLESHOOTING FOUND BATTERY POWER SUPPLY 1 NOT WORKING. REMOVED AND REPLACED THE BATTTERY POWER SUPPLY 1 IAW EMB 140 AMM 33-50-04. THE OPERATIONAL TEST WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — DEFECTIVE (COCKPIT) · airframe 20,273 hrs · 17,531 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE FLASHLIGHT FALLS OUT OF CAPTAINS FLASHLIGHT HOLDER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FAULTY FLASHLIGHT HOLDER IAW EMB140 AMM:30-50-16. THE OPERATIONAL CHECK WAS GOOD IAW EMB140 AMM: 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 19,883 hrs · 17,086 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT FLIGHT ATTENDANT FLASHLIGHT MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED MISSING FLASHLIGHT IAW EMB 140 AMM CHAPT 33-50-16. THE OPERATIONAL CHECK WAS GOOD IAW AMM CHAPT 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,884 hrs · 15,027 cycles

DURING MAINTENANCE BASE INSPECTION FOUND FRAME 23 TO BE CRACKED BETWEEN STRINGER 14 RIGHT AND 15 RIGHT. AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CRACK IAW ETD2011-145/00240 REV 1. AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — FAILED (ANTI-ICE SYSTEM) · airframe 17,923 hrs · 14,971 cycles

ON FLIGHT 2751 DURING CLIMB ABOVE 10,000 FEET, DURING ANTI ICE TEST THE CREW RECEIVED A WING ANTI ICE FAIL MESSAGE. DUE TO WEATHER IN AREA THE CREW ELECTED TO RETURN TO SGF. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT WING ANTI-ICING LOW PRESS TRANSDUCER IAW EMB AMM 30-11-11 AIR FOIL ANTI-ICING SYSTEM. THE OPERATIONAL TEST WAS GOOD IAW EMB AMM 30-10-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,598 hrs · 11,720 cycles

DURING MBV THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. CUT OUT CORRODED AREA. FABRICATED A 3.6 X 15.1 INCH DOUBLER FROM AL2024T3 0.050 INCH, A 11.5 X 2.5 INCH FILLER FROM AL2024T3 0.050 INCH AND 2 SHIMS, ONE 3.6 X 1.1 INCH AND THE OTHER 4.5 X 1.1 INCH, FROM AL2024T3 0.040 INCH. PREPPED, CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,662 hrs · 7,856 cycles

OMEGA BEAM CORRODED AT FRAME 20. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (BLEED SYSTEM) · airframe 8,582 hrs · 7,022 cycles

BLEED ONE LEAK WARNING MESSAGE, DECLARED AN EMERGENCY. RETURNED TO MIA. PERFORMED ENGINE RUNS IAW FAULT ISOLATION TASK 36-20-00-810-801-A WITH NO LEAKS NOTED OR FAULTS NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (FR 20-22)

SAW - DURING CPCP INSPECTION, FOUND SERVICE DOOR SILL IS CORRODED BETWEEN FRAMES 20 AND 22. MAINTENANCE INSTALLED A NEW SERVICE DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)