N842AE

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,170 hrs · 27,539 cycles

EMERGENCY BATTERY NR 3 INOPERABLE. C/A REMOVED AND REPLACED NR 3 EMERGENCY BATTERY AND CHARGER ASSEMBLY, IAW AMM 33-50-04. OPERATIONAL CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,895 hrs · 27,241 cycles

REMOVED AND INSTALLED EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-50-04. OPS CHECKED GOOD. EMERGENCY LIGHT CHARGER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,736 hrs · 27,122 cycles

EMERGENCY LIGHTS INOPERATIVE ON MOST FWD AND MOST AFT CABIN CEILING PANELS. REMOVED AND REPLACED LIGHT BULBS ON THE FWD AND AFT MOST CEILING PANELS IAW AMM 33-50-08. OPERATIONAL CHECK GOOD.

Part: LAMP — INOPERATIVE (RT OVERWING) · airframe 31,297 hrs · 26,682 cycles

RH EXTERNAL OVERWING EMERGENCY LIGHT FAILS TO ILLUMINATE.-C/A-REMOVED AND REPLACED RH OVER WING EMERGENCY LIGHT LAMP IAW AMM 33-50-01. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,249 hrs · 26,636 cycles

L/H OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED L/H OVER WING EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD

Part: FAN — INOPERATIVE (RECIRCULATION) · airframe 31,209 hrs · 26,600 cycles

SMELL IN COCKPIT WHILE TAXING-C/A-UPON INSPECTION FOUND GRINDING NOISE TO BE COMING FROM RECIRC FAN. REMOVED RECIRC FAN 2 IAW EMB 140 AMM 21-24-01 AND FOUND TO BE BURNT. INSTALLED NEW RECIRC FAN IAW EMB 140 AMM 21-24-01. OPC IAW EMB 140 AMM 21-51-00. RAN PACKS FOR 30 MIN NO SMELL NOTED OPC GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,052 hrs · 26,459 cycles

AFT PAX EMERGENCY LIGHTS INCLUDING OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED BATTERY POWER SUPPLY & BATTERY PACK #4 IAW AMM 33-50-04 OPS CHK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 104912

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,963 hrs · 26,385 cycles

RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A OPC GOOD.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 30,856 hrs · 26,296 cycles

EMERGENCY LIGHTING BATTERY ASSY/ BATTERY CHARGER REPLACEMENT REQUIRED FOR BATTERY POWER SUPPLY #3-C/A-REMOVED AND REPLACED BATTERY POWER SUPPLY #3 IAW ENVOY W/C 33-700-19. OPC GOOD IAW ENVOY W/C 33-700-17. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 83000

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,818 hrs · 26,264 cycles

L/H CENTER FAIRING EXT EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED L/H CENTER FAIRING EXT EMERGENCY LIGHT BULB IAW EMB I45 AMM 33-50-10 OPS CHECK GOOD NO FURTHER DEFECTS NOTED

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 30,516 hrs · 25,941 cycles

MAIN CABIN DOOR VERY HARD TO OPEN. C/A-LUBRICATRED MAIN AIRFRAME ROLLERS CABIN DOOR IAW AMM 53-21-02.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 28,868 hrs · 24,370 cycles

LH OVERWING LIGHT INOP-C/A-REMOVED AND REPLACED LH OVERWING LIGHT IAW EMB 140 AMM 33-50-10 OPS CK GOOD

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,856 hrs · 24,357 cycles

CABIN EMERG LT IS ON-C/A-UPON THROUBLESHOOTING FOUND BATTERY POWER SUPPLY INOP, REMOVED AND REPLACED BATTERY POWER SUPPLY AND FOR PRECAUTIONARY PURPOSE RAR BATTERY PACK #4 IAW EMB 140 AMM 33-50-04. OPC GOOD NO DEFECTS NOTED AT THIS TIME. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 105997

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,814 hrs · 24,314 cycles

RT OMEGA BEAM OTBD SUPPORT IS CRACKED BETWEEN FRAMES 47-48. C/A-COMPLETE:ACCOMPLISHED REPAIR OF RT OUTBD OMEGA BEAM SUPPORT BETWEEN FR46 AND 50 IAW SRM 53-23-02.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 28,814 hrs · 24,314 cycles

CROSSBEAM BETWEEN FR 24-25 IS CORRODED. C/A-COMPLETE:REMOVED AND REPLACED ALUMINUM CROSSBEAM BETWEEN FR 24-25 IAW SRM 53-22-10 AND ETN-EM-53-139R4.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,814 hrs · 24,314 cycles

#4 LT EMERGENCY LIGHT STRIP EXTRUSION IS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #4 LT EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW301252 FOR OPC.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,814 hrs · 24,314 cycles

#5 LT EMERGENCY LIGHT STRIP EXTRUSION IS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #5 LT EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW301252 FOR OPC.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,814 hrs · 24,314 cycles

#7 LT EMERGENCY LIGHT STRIP EXTRUSION IS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #7 LT EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW301252 FOR OPC.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,814 hrs · 24,314 cycles

#1 AND #4 FLOOR EMERGENCY LIGHT STRIPS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #4 #1 FLOOR EMERGENCY LIGHT STRIP IAW AMM 33-50-12. SEE BOW301252 FOR OPC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,814 hrs · 24,314 cycles

RT FUSELAGE UPPER SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R, CRACK ENDS MARKED, APPROX. 1/2" LONG. EASI #6581 USED. 100-500 KHZ PROBE, FREQ=400KHZ, V-GAIN=77.0, H-GAIN=65.0, LPF=100, ANGLE=134. C/A-COMPLETE:ACCOMPLISHED REPAIR OF CRACKED SKIN AT FR75 ABOVE STRINGER 2R IAW SRM 53-31-01.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,814 hrs · 24,314 cycles

#3 LT EMERGENCY LIGHT STRIP EXTRUSION IS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #3 LT EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW301252 FOR OPC.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 28,814 hrs · 24,314 cycles

CROSSBEAM AT FR 20 IS CORRODED. C/A-COMPLETE:REMOVED AND INSTALLED SERVICEABLE CROSSBEAM AT FR 20 IAW ETN-EM-53-139 R4 AND SRM 53-21-10. NO FURTHER ACTION REQUIRED.

Part: STRUCTURE — DAMAGED (CABIN) · airframe 28,814 hrs · 24,314 cycles

RT FLOOR EXTRUSIONS #1 THRU #8 ARE DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED RT FLOOR ECTRUSIONS #1 THRU #8 IAW AMM 33-50-12.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,814 hrs · 24,314 cycles

EXTERNAL EMERGENCY LIGHT ON LT OVERWING PANEL INOP. C/A-COMPLETE:REMOVED AND REPLACED BULB ON EXTERNAL EMERGENCY LIGHT ON LT OVERWING PANEL IAW AMM 33-50-10 OPS CHECK GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,814 hrs · 24,314 cycles

#1 LT EMERGENCY LIGHT STRIP EXTRUSION IS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #1 LT EMERGENCY LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW301252 FOR OPC.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,814 hrs · 24,314 cycles

#5 EMERGENCY LIGHT STRIP IS DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED #5 FLOOR EMERGENCY LIGHT STRIP IAW AMM 33-50-12. SEE BOW 301252 FOR OPC.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 28,814 hrs · 24,314 cycles

FR 23 IS CRACKED AT RT OUTBD FLOOR SILL. C/A-COMPLETE:REPAIRED FR 23 AT RT OUTBD FLOOR SILL IAW EO#EM-53MR-1808 PART "A".

Part: SKIN — CORRODED (FUSELAGE) · airframe 28,814 hrs · 24,314 cycles

SSI 53-20-07 FUSELAGE INTERNAL SKIN IS CORRODED BETWEEN FR 37-38 STR 21L-21R.(MARKED). C/A-COMPLETE:PERFORMED REPAIR OF FUSELAGE INTERNAL SKIN IS CORRODED BETWEEN FR 37-38 STR 21L-21R IAW ERS-EM-5300-3455.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,814 hrs · 24,314 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 3 FASTNERS ON FR 79 RT SIDE BELOW VERITCAL STAB. C/A-COMPLETE:REPAIRED FUSELAGE EXTERNAL SKIN CRACK ON FRAME 79 RT SIDE BELOW VERTICAL STAB IAW SRM 53-32-01. SEE WIPS AND TASKS FOR DETAILS.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,814 hrs · 24,314 cycles

LT OMEGA BEAM FWD DIGITAL TO AFT DIGITAL INBD INTERCONNECT BRACKET IS CRACKED. C/A-COMPLETE:REMOVED AND REPLACED LT OMEGA BEAM FWD DIGITAL TO AFT DIGITAL INBD INTERCONNECT BRACKET IAW SRM 51-40-02.

Part: CONTROL UNIT — FAILED (PITCH TRIM) · airframe 28,740 hrs · 24,249 cycles

AT CRUISE ON FLIGHT 3211 CREW REPORTED WARNING MSG PITCH TRIM BACKUP INOPERATIVE. AUTOPILOT WAS ENGAGED & DECLARED EMERGENCY. THE ACFT WAS REMOVED FROM SERVICE. CORRECTIVE ACTION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,293 hrs · 23,854 cycles

LEFT EXTERIOR OVERWING EMERGENCY LAMP INOPERATIVE. R & R LT EXTERIOR OVERWING EMERGENCY LIGHT LAMPS IAW AMM TASK 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,272 hrs · 23,833 cycles

LT AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R LAMP AT LT AFT EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-10 & SMP, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,157 hrs · 23,741 cycles

ROW 14 EMERGENCY LIGHT INOPERATIVE. R & R ELECTROLUMINESCENT STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,855 hrs · 23,487 cycles

COCKPIT STEP EMERGENCY SIGN INOPERATIVE. R & R NR 1 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11 & OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 27,793 hrs · 23,425 cycles

FIRST OFFICER`S FLASHLIGHT HOLDER BROKEN. R & R FLASH LIGHT HOLDER IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: NUT — BENT (CRASH AXE) · airframe 27,713 hrs · 23,364 cycles

BUTTERFLY NUT THAT HOLDS CRASH AXE CLAMP CLOSED IS BENT OVER 90 DEGREES. UNABLE TO STOW OR USE CRASH AXE. INSTALLED IAW STANDARD PRACTICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,149 hrs · 22,920 cycles

EMERGENCY LIGHT ABOVE F/A SEAT INOPERATIVE. REPLACED INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: DISPLAY — FAILED (COCKPIT) · airframe 26,857 hrs · 22,664 cycles

AFTER DISCONNECTING GPU, DETECTED SMOKE IN COCKPIT, NOTICED EICAS BLANK AND MFD DISPLAYED AN AMBER "CHECK EICAS" MESSAGE. R & R EICAS DISPLAY UNIT IAW AMM 34-22-01, OPS GOOD, SMELL SMOKE WAS FROM FAULTY EICAS DISPLAY.

Part: WIRE HARNESS — FAILED (NLG) · airframe 26,855 hrs · 22,662 cycles

CREW REPORTED THAT DURING TAKEOFF, RECEIVED AN AIR GROUND FAIL MESSAGE WITH ASSOCIATED REV DISAGREE MESSAGE ON EICAS. DECLARED EMERGENCY, RETURNED AND LANDED WITH OUT INCIDENT. VR 300' IAW MINUTE AT LANDING. ACFT REMOVED FROM SERVICE. R & R NLG WOW HARNESS IAW AMM 32-00-03 & PROXIMITY SENSOR. PERFORMED OPS TEST 32-63-00 AND 32-30-00. THE OPS CHECKED GOOD. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (NLG) · airframe 26,857 hrs · 22,664 cycles

THE CREW REPORTED THAT DURING TAKEOFF THEY FELT A VIBRATION FROM THE NOSE GEAR AND HEARD A THUMP AFTER ROTATION. THE TOWER CONFIRMED RUBBER ON THE RUNWAY. THE CREW DECLARED AN EMERGENCY AND COMPLIED WITH AOM VOL 1 PROCDURES AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. NR 3, R & R RT AND LT NLG WHEEL ASSY AND PERFORMED TIRE TREAD FAILURE INSPECTION/CHECK IAW AMM 05-50-15. R & R ND REPLACED 7 DEGREE SWITCH IAW AMM 32-50-06. OPS CHECK NORMAL. PN 8-527-01, SN 8-527-01 & 80-057-01. R & R THE NLG RT STEERING ACTUATOR HYD LINE IAW CMM 32-21-10. THE ACFT WAS RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,764 hrs · 22,587 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-50-07. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,465 hrs · 22,360 cycles

DURING MX INSPECTION, FOUND EMERGENCY POWER BATTERY UNIT NR 3 INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R BATTERY UNIT. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 26,260 hrs · 22,173 cycles

DURING B INSPECTION, FOUND THE LT OVER WING EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE BULB IN OVER WING EMERGENCY LIGHT IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 26,209 hrs · 22,115 cycles

DURING B INSPECTION, FOUND THE LT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LT AFT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 25,972 hrs · 21,887 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OVER WING AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB FOR THE LEFT AFT OVER WING EMERGENCY LIGHT IAW EMB MM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 25,652 hrs · 21,606 cycles

ON FLIGHT 3226 THE CREW REPORTED THAT AT CRUISE THE FLIGHT CREW DETECTED TOXIC FUMES IN THE COCKPIT. THE FLIGHT ATTENDANT SMELLD FUMES IN THE FORWARD CABIN. THE FLIGHT ATTENDANT SAID THAT FUMES WERE CONCENTRATED IN THE FORWARD PART OF CABIN. THE CREW PERFORMED AN EMERGENCY LANDING IN SAT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THERE WERE NO FUMES DETECTED AFTER LANDING. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ETN-EM-72-034. ISOLATED LEFT PACK AIR CYCLE MACHINE MAKING BURNING METAL ODOR. REMOVED AND REPLACED LEFT PACK AIR CYCLE MACHINE REF EMB 140 AMM 21-51-03. THE OPERATIONAL CHECK AND LEAK CHECK WERE GOOD. PERFORMED ETN-EM-72-034, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — LOOSE (EXTERIOR) · airframe 25,545 hrs · 21,500 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT REAR WING/FUSELAGE FAIRING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED EXISTING LAMP IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — BIRD INGESTION · airframe 25,451 hrs · 21,399 cycles

FOR FLIGHT 3582 THE CREW REPORTED THAT ON TAKEOFF AFTER V1 MANY SUSPECTED BIRD STRIKES. THE SMELL ENTERED THE CABIN OF COOKED BIRD. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED THOROUGH INSPECTION OF A/C IAW EMB WORKCARD 05-200-07 BIRD STRIKE INSPECTION. PERFORMED VISUAL INSPECTION OF BOTH ENGINES AND FAN BLADES IAW RR MM 05-50-00-200-804. NO ABNORMALITIES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,295 hrs · 21,250 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OVER WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW ERJ 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — MISSING (FLASHLIGHT)

CAPTAINS FLASHLIGHT IS MISSING PLASTIC ON/OFF SWITCH. REMOVED BROKEN FLASHLIGHT BEHIND PILOT SEAT AND INSTALLED SERVICEABLE FLASHLIGHT IN REFERENCE WITH EMB 140 AMM 33-50-16-000-801-A AND 33-50-16-400-801-A.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,573 hrs · 20,538 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FORWARD CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IN FORWARD CABIN IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-51-01. AIRCRAFT IS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 24,507 hrs · 20,489 cycles

FOR FLIGHT 3259 - THE RAMP PERSONNEL REPORTED ON TAXI IN SMOKE WAS COMING FROM NR 1 ENGINE. SMOKE SMELLED SOMETHING LIKE BURNING ELECTRIC WIRING. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF LEFT ENGINE IAW AE3007A MM 72-00-00. SMOKE OBSERVED ON SHUTDOWN. REMOVED AND REPLACED SHAFT PLUG O-RING ON LEFT ENGINE IAW ROLLS ROYCE MM 72-59-15. THIS AIRCRAFT HAS BEEN INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLIGHT AND FOUND TO BE IN SAFE CONDITION FOR A FERRY FLIGHT. REMOVED AND REPLACED LEFT HAND ENGINE IAW WORK CARD 71-000-00. THE LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 24,377 hrs · 20,389 cycles

DURING MAINTENANCE INSPECTION, NOTICED A STRONG ODOR IN COCKPIT WHILE APU BLEED WAS RUNNING. AIRCRAFT REMOVED FROM SERVICE. RAN APU IAW AMM 49-13-00. SUPPLIED APU BLEED AND FOUND NO ODOR NOTED. OPS CHECKED GOOD. FOUND APU OIL OVER SERVICED REF NRWC NR 842-DFW-00901. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,232 hrs · 20,276 cycles

DURING B INSPECTION, FOUND THE RIGHT FORWARD OVERWING EMERGENCY LIGHT OUT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CRACKED (EMERGENCY EXIT) · airframe 24,167 hrs · 20,223 cycles

DURING MAINTENANCE, FOUND BEAM 3 IN THE RIGHT OVERWING EMERGENCY EXIT CRACKED .250 INCHES IN LENGTH NEAR THE AFT CORNER. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BEAM IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,211 hrs · 20,257 cycles

DURING B INSPECTION, FOUND THE LEFT NR 1 EMERGENCY LIGHT HAS A BROKEN WIRE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH CONNECTORS ON THE LEFT NR 1 EMERGENCY LIGHT IAW SWPM 20-21-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 23,714 hrs · 19,861 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY EXIT LIGHT ABOVE FLIGHT ATTENDENTS SEAT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED EMERGENCY LIGHT SYSTEM OPERATIONAL CHECK IAW EMB 140 AMM 33-50-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,259 hrs · 19,417 cycles

DURING MAINTENANCE INSPECTION FOUND RIGHT EXTERIOR OVERWING FORWARD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT IAW EMB 140 AMM 33-50-10, OPERATIONAL WAS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE.

Part: OXYGEN BOTTLE — DEFECTIVE (CABIN) · airframe 22,753 hrs · 18,997 cycles

ON FLIGHT 4387 THE CREW REPORTED A PASSENGER’S PORTABLE OXYGEN BOTTLE WAS OPERATING AT AT 1100 PSI. THE CREW ELECTED TO DECLARE AN EMERGECNY AND DIVERT TO CRW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER PORTABLE O2 BOTTLE IAW EMB 140 EEL-06-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — DEFECTIVE (COCKPIT) · airframe 22,564 hrs · 18,839 cycles

ON FLIGHT 4003 THE CREW REPORTED THE FLASHLIGHT HOLDER BEHIND THE CAPTAIN DOES NOT HOLD THE FLASHLIGHT. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REMOVED AND REPLACED THE FLASHLIGHT HOLDER ASSEMBLY IAW EMB-140AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,419 hrs · 18,704 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OVER THE WING EMERGENCY LIGHT OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVER THE WING EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE ASSY — MALFUNCTIONED (LT MLG) · airframe 21,666 hrs · 18,086 cycles

ON FLIGHT 2900 THE CREW REPORTED UPON LANDING AND TAXIING, RECEIVED A MESSAGE ABOUT THE LEFT INBOARD BRAKE OVERHEATING. THE CREW DECLARED AND EMERGENCY AND CRASH, FIRE AND RESCUE WERE DISPATCHED. FIRE DEPT TOOK A READING OF 1200. THEY ALSO HAD A NR 1 TIRE FLAT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 MAIN LANDING GEAR BRAKE ASSEMBLY W/C NR 32-700-11. THE LEAK CHECK AND OPERATIONAL CHECKS WERE GOOD. REMOVED AND REPLACED THE BRAKE CONTROL VALVE IAW EMB-140 AMM 32-41-06 THE LEAK CHECK WAS GOOD, TAXI CHECK GOOD IAW EMB AMM 32-41-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,354 hrs · 17,854 cycles

FOR FLIGHT 2721 DURING THE PREFLIGHT INSPECTION FOUND THE MAIN DOOR LINER EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR LINER EMERGENCY ASSEMBLY IAW EMB 140 AMM 33-50-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (COCKPIT) · airframe 19,254 hrs · 16,175 cycles

ON FLIGHT 3707 DURING THE CLIMBOUT THE CREW REPORTED, RECEIVED AN AIR/GROUND FAIL MESSAGE ON EICAS THAT REMAINED ON FOR DURATION OF FLIGHT. THE CREW ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC CONTROL UNIT IAW EMB AMM 32-32-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — FAULTY (NR 2) · airframe 18,857 hrs · 15,848 cycles

ON FLIGHT 3275 DURING CLIMB THE CREW REPORTED THE RUDDER SEEMED TO BE HALFWAY INOPERABLE IN FLIGHT. THE CREW COMPLIED WITH THE AIRCRAFT OPERATING MANUAL. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 PRESSURE SWITCH IAW EMB 140 AMM 27-23-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE)

DURING MBV THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. REMOVED DAMAGED SILL AND INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (A)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING MBV A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THAT EXISTING REPAIR DOUBLER AND CLEANED THE AREA. POSITIONED, MARKED, DRILLED, TREATED AND INSTALLED NEW REPAIR DOUBLER PN EPNEM53EP54701. REPAIRS PERFORMED IAW SRM 53-00-10. AC RETURNED FOR SERVICE. (K)

Part: PRESSURE SWITCH — MALFUNCTIONED (MLG BRAKES) · airframe 12,920 hrs · 10,903 cycles

ON FLIGHT 3485, FLIGHT CREW NOTICED BRAKE ON LIGHT. CREW DECLARED EMERGENCY AND LANDED SAFELY IN SJT. REMOVED AND REPLACED PARK BRAKE PRESS SWITCH AND CLEANED CONNECTOR, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — FAILED (ZONE 200) · airframe 12,077 hrs · 10,340 cycles

RECEIVED ELECTRICAL EMERGENCY ABNORMAL MESSAGE, RETURNED TO ORD. REMOVED AND REPLACED ELECTRICAL CONTROL PANEL IAW EMB 24-00-01. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (HORIZONTAL STAB) · airframe 11,383 hrs · 9,827 cycles

PITCH TRIM INOP MESSAGE ON TAKEOFF, BACKUP SYSTEMS FUNCTIONED NORMAL. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR IAW EMB AMM 27-40-02. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 9,814 hrs · 8,723 cycles

RECEIVED ELECTRICAL ABNORMAL MESSAGE, DIVERT TO BDL.

Part: SENSOR — FAULTY (LT TE FLAP)

FLAP FAIL MESSAGE ON DESCENT THROUGH 16,000 WITH VMC-ICING CONDITIONS. NO EMERGENCY DECLARED. THE FLAPS DID NOT MOVE WHEN 9 DEGREES POSITION WAS SELECTED. RMU AND EICAS BOTH INDICATED ZERO, ONLY MESSAGE WAS FLAP FAIL. COMPLIED WITH AMERICAN EAGLE DOCUMENT EM-27-010. TROUBLESHOT, IAW FIM 27-51-00-810-516-A. REMOVED AND REPLACED LEFT FLAP VELOCITY SENSOR IAW EMB AMM 27-51-13. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: LINE — LOOSE (HYD SYSTEM)

AFTER TAKEOFF FROM LGA HYDRAULIC SYSTEM 2 FLUID DROPPED TO `0` QUANTITY FOLLOWED BY ENGINE 2 HYDRAULIC PUMP FAILURE AND HYDRAULIC 2 LOW QUANTITY MESSAGE. FOUND LOOSE ENGINE 2 HYDRAULIC PUMP CASE DRAIN HYDRAULIC LINE. TIGHTEN NUT AND PERFORMED ENGINE DRIVEN PUMP INSPECTION CHECK, IAW AMM 29-10-03. SERVICED HYDRAULIC SYSTEM 2 RESERVOIR IAW AMM 12-13-01. BLEED HYDRAULIC 2 SYSTEM IAW AMM 29-00-00. LEAKED AND OPERATIONAL CHECK GOOD IAW MM 29-10-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CHAFED (FUSELAGE)

SAW - DURING IMBV INSPECTION, FOUND STRINGER 19 LEFT BETWEEN FRAMES 52-53 IS CHAFED. REPAIRED STRINGER IAW EMB SRM 53-24-00 BY CUTTING OUT DAMAGED PORTION OF STRINGER AND INSTALLING A DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M)

Part: GUSSET — CORRODED (FLOORBEAM)

DURING IMBV INSPECTION, FOUND GUSSET CONNECTING RIGHT HAT BEAM TO FLOORBEAM 20 CORRODED. REMOVED AND REPLACED GUSSET, IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING IMBV INSPECTION, FOUND RIGHT UPPER FLOORBEAM AT FRAME 23 IS CORRODED. REMOVED AND REPLACED FLOORBEAM, IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: TERMINAL — BURNED (HEAT CONTROLLER)

LAX - FLT 3121 - DURING CLIMB, THE FLIGHT ATTENDANT REPORTED A SMOKE ODOR IN THE CABIN. NO VISIBLE SMOKE NOTED. CREW ELECTED TO RETURN TO LAX AND DECLARED EMERGENCY. MAINTENANCE FOUND THE CAUSE TO BE THE NR 1 WINDSHIELD HEAT CONTROLLER TERMINALS WERE BURNED. THE CONTROLLER AND THE TERMINALS WERE REPLACED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WINDSHIELD — CRACKED (CABIN) · airframe 5,141 hrs · 4,781 cycles

ON CLIMB OUT AT 11,000 FL CAPTAINS WINDSCREEN SHATTERED RETURNED TO AIRPORT, LANDED SAFELY. NO LOSS OF CABIN PRESSURIZATION. REPLACED CAPTAIN WINDSHIELD. AC RETURNED TO SERVICE. (SW21200503048) (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 4,877 hrs · 4,546 cycles

DURING AN MBV INSPECTION OF AIRCRAFT. THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUTOUT A SECTION OF THE DAMAGED OMEGA BEAM AND TREATED THE BARE METAL EDGES. FABRICATED A REPAIR ANGLE .050 IN, REPAIR PLATE .125 IN, SHIMS AND A FILLER. REPAIR DONE IAW SRM. (SW21200501808) (K)