N837AE

Part: PUMP — FAILED (HYD SYSTEM) · airframe 32,168 hrs · 29,073 cycles

LO HYD 1 LO QTY DURING FLT IT DROPPED TO BOTTOM OF LEVEL AND GND OPS REPORT LEAKING FROMUNDER # 1 ENGINE FLUID-C/A-FOUND E1 LOWER COWLING WITH HYD FLUID COMING FROM EDAP REMOVED AND REPLACED E1 EDHP PER EMB AMM 29-10-*03 OPC AND LEAK CK GOOD SVCED HYD # 1 PER ETN-EM-29-023

Part: PUMP — FAILED (HYD SYSTEM) · airframe 32,168 hrs · 29,073 cycles

LO HYD 1 LO QTY DURING FLT IT DROPPED TO BOTTOM OF LEVEL AND GND OPS REPORT LEAKING FROMUNDER # 1 ENGINE FLUID-C/A-FOUND E1 LOWER COWLING WITH HYD FLUID COMING FROM EDAP REMOVED AND REPLACED E1 EDHP PER EMB AMM 29-10-*03 OPC AND LEAK CK GOOD SVCED HYD # 1 PER ETN-EM-29-023

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 32,132 hrs · 29,041 cycles

AFT FA FLASHLIGHT INOP-C/A-FLIGHT CREW PLACARDED AFT FA FLASHLIGHT MEL 25-53 AUTH 110212-C MOC 056048. REMOVED AND REPLACED AFT FA FLASHLIGHT IAW AMM 33-50-16 OPC GOOD MEL ITEM RESTORED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,970 hrs · 28,883 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LAMP IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.

Part: SEAL — DAMAGED (MAIN DOOR) · airframe 31,628 hrs · 28,537 cycles

AIRCRAFT UNABLE TO MAINTAIN PRESSURIZATION. REMOVED AND REPLACED MAIN DOOR RUBBER TRIM SEAL IAW AMM 52-18-04 AND PERFORMED FUNCTIONAL TEST FOR CABIN LEAKAGE WITH AIR BLEED FROM APU IAW AMM 21-31-00 LEAK CHECK GOOD. APPLIED SEALANT ON TOP FWD AND AFT CORNER OF SERVICE DOOR IAW AMM 52-00-01

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,848 hrs · 27,779 cycles

COCKPIT EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. OPC GOOD NO FURTHER DEFECTS NOTED. END.

Part: SOLENOID VALVE — FAILED (LANDING GEAR) · airframe 30,752 hrs · 27,690 cycles

LDG GEAR LEVER DISAGEE ON RETRATION WITH 3 RED GEAR INDICATION RECYCLED GEAR IAW QRH PROCEDUR, 3 GREEN DOWN INDICATION PREFORMED OVERWEIGHT LANDING "TRANSFERRED TO NRWC 837-CMI-02469". C/A- REMOVED AND REPLACED OF LG SOLENOID VALVE IAW AMM 32-33-04-000-801-A/32-33-04-400-801-A GEAR SWING OPC/LEAK CHECK GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 30,268 hrs · 27,275 cycles

DURING COURTESY CHECK FOUND EMERGENCY EXIT MARKING SIGN ABOVE FLIGHT ATTENDANT SEAT INOP. REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-11 OPC GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 30,231 hrs · 27,243 cycles

RH EXTERIOR EMERGENCY LIGHT ON OVERWING INOP.-C/A-RAR EXTERNAL EMERGENCY LIGHT RH LAMP IAW EMB 140 AMM 33-50-10. OPC GOOD.

Part: BOLT — MISSING (PARKING BRAKE) · airframe 29,595 hrs · 26,673 cycles

EMERGENCY PARKING BRAKE IS DIFFICULT TO SET. OPENED PARKING BRAKE MECHANISM AND FOUND BOLT MISSING. REMOVED AND REPLACED IAW AMM 32-44-11. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: FIRE DETECTOR — FALSE ACTIVATION (FWD CARGO) · airframe 28,855 hrs · 25,947 cycles

CAPTAIN REPORTED A CARGO FIRE WARNING DURING SHORT FINAL, CARGO FIRE BOTTLES DISCHARGED, AN EMERGENCY WAS DECLARED. FIRE DEPT INSPECTION REVEALED NO EVIDENCE OF FIRE. REMOVED AND REPLACED THE FWD CARGO FIRE DETECTOR IAW AMM 26-15-01. OPS CHECKED GOOD IAW W/C 26-200-06.

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER) · airframe 28,828 hrs · 25,918 cycles

RUDDER OVERBOOST AFTER TAKE OFF. RETURNED TO DEPARTURE. PERFORMED TROUBLESHOOTING IAW FIM 27-22-10, FOUND THE NR 1 RUDDER PRESSURE SWITCH INOPERATIVE. REMOVED AND REPLACED THE PRESSURE SWITCH IAW AMM 27-23-04. OPS AND LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,820 hrs · 25,904 cycles

EMERGENCY LIGHT NR 8 NOT WORKING. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12 . OPS CHECKED GOOD

Part: SKIN — CRACKED (FRAME 81) · airframe 28,820 hrs · 25,904 cycles

SKIN PLATE CRACKED AT FRAME 81 BETWEEN STRINGERS 1L - 2R. REPAIRED THE SKIN IAW SRM 51-40-02

Part: FITTING — CRACKED (FRAME 19) · airframe 28,820 hrs · 25,904 cycles

FITTING AT FRAME 19 STRINGER 3L CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 75) · airframe 28,820 hrs · 25,904 cycles

RIGHT REAR FUSELAGE SKIN CRACKED AT FRAME 75, BETWEEN STRINGERS 1R AND 2R. REPAIRED THE SKIN IAW SRM 53-31-01.

Part: SUPPORT — GOUGED (SERVICE DOOR) · airframe 28,820 hrs · 25,904 cycles

SERVICE DOOR LOWER VERTICAL SUPPORT GOUGED. REPAIRED THE VERTICAL SUPPORT IAW ERS-EM-52MR-869.

Part: SKIN — DENTED (FRAMES 19-20) · airframe 28,820 hrs · 25,904 cycles

FUSELAGE SKIN DENTED BETWEEN FRAMES 19 - 20, STRINGERS 20R - 21R. THE SKIN WAS REPAIRED IAW SRM 53-21-01, TYPE A1.

Part: SUPPORT — CRACKED (EMERGENCY EXIT) · airframe 28,820 hrs · 25,904 cycles

CORRODED AND CRACKED LT EMERGENCY EXIT LOWER LOWER WEB SUPPORT. REMOVED AND REPLACED THE WEB SUPPORT IAW SRM 51-40-02.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 28,820 hrs · 25,904 cycles

RIGHT ELEVATOR EXTERNAL UPPER SKIN IS CRACKED AT THE OUTBD AFT CORNER. REPAIRED THE ELEVATOR SKIN IAW EO EM-53MR-XXXX.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 28,820 hrs · 25,904 cycles

RIGHT ELEVATOR EXTERNAL LOWER SKIN IS CRACKED AT THE OUTBD AFT CORNER. REPAIRED THE ELEVATOR SKIN IAW EO EM-55MR-660.

Part: CONNECTOR — MISSING (EMERGENCY LIGHT) · airframe 28,820 hrs · 25,904 cycles

EMERGENCY LIGHT, NR 1 CONNECTOR MISSING. INSTALLED THE CONNECTOR IAW SWPM 20-21-00.

Part: FLOOR SUPPORT — CORRODED (FRAME 60) · airframe 28,820 hrs · 25,904 cycles

RIGHT OMEGA BEAM IN THE LAVATORY CORRODED AT FRAME 60. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-3214

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 28,820 hrs · 25,904 cycles

RIGHT OVERWING EXIT FWD FRAME CRACKED AT UPPER END. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02

Part: DOOR SILL — CORRODED (FR 66) · airframe 28,820 hrs · 25,904 cycles

CARGO DOOR CENTER SILL CORRODED. REMOVED AND REPLACED CARGO CUTOUT CENTER SILL IAW EMB 140 SRM 51-40-02.

Part: PROFILE — CORRODED (FRM 65) · airframe 28,820 hrs · 25,904 cycles

FRAME 65 L-SHAPE PROFILE LWR END AT CARGO DOOR CUTOUT HAS AN AREA OF CORROSION. REMOVED AND REPLACED WITH SERVICEABLE SECTION OF THE PROFILE IAW SRM 53-31-04 ITEM 4

Part: FRAME — CRACKED (FRM 10) · airframe 28,820 hrs · 25,904 cycles

FRAME 10 UNDER COPILOTS WINDOW IS CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.

Part: FITTING — DAMAGED (RT AILERON) · airframe 28,820 hrs · 25,904 cycles

RIGHT AILERON DAMPER FITTING DAMAGED. REMOVED AND REPLACED THE RT DAMPER FITTING IAW EO EM-27MR-112.

Part: FITTING — DAMAGED (LT AILERON) · airframe 28,820 hrs · 25,904 cycles

LEFT AILERON DAMPER FITTING DAMAGED. REMOVED AND REPLACED THE DAMPER FITTING IAW EO EM-27MR-112.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,820 hrs · 25,904 cycles

FOUR LT EMERGENCY LIGHT STRIP EXTRUSIONS ARE DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHTS IAW AMM 33-50-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,440 hrs · 25,567 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. R & R LAMP WITH NEW OPERATIONS CHECK GOOD ALL WORK IAW MM CH 33-50-10.

Part: ENGINE — FAILED (NR 2) · airframe 28,337 hrs · 25,493 cycles

IAW ITEM NR 1 ON LOG PAGE 3529025 OIL FOUND NR 2 ENG DURING BORESCOPE INSPECTION. R & R NR 2 ENG IAW WC 71-000-00. OPERATIONS CHECKED GOOD & LEAK CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 28,337 hrs · 25,493 cycles

LAVATORY SMOKE ON EICAS. COMPLIED WITH ETN-EM-72-034. BORESCOPE ON BOTH ENGS REQUESTED.

Part: UNKNOWN — SMOKE (CABIN) · airframe 28,337 hrs · 25,493 cycles

FLIGHT ATTENDANT REPORTED SMOKE COMING FROM LAVATORY, PAX COUGHING ALONG WITH FLIGHT ATTENDANT. COMPLIED WITH ETN-EM-72-034. BORESCOPE ON BOTH ENGS REQUESTED.

Part: BALLAST — BURNED (CABIN) · airframe 28,334 hrs · 25,490 cycles

SMOKE IN CABIN FROM MULTIPLE PSU'S. DURING TROUBLESHOOTING FOUND PSU BALLAST BETWEEN SEATS 14A - 15A BURNED. R & R BALLAST IAW AMM 33-21-05. OPERATIONS CHECKED OK.

Part: SHROUD — INOPERATIVE (TE FLAP) · airframe 28,108 hrs · 25,285 cycles

AFTER LANDING DURING FLAP RETRACTION, FLAP FAILED MSG & FLAPS STUCK AT 12 DEGREES. R & R LT INBD FLAP DRIVER SHROUD TIP IAW SPM. FLAPS SYS OPERATIONS CHECKED GOOD IAW AMM 27-51-00.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 27,917 hrs · 25,084 cycles

DURING FLIGHT 3352 FOUND CAPTAIN`S FLASHLIGHT HOLDER BROKEN. THE ACFT WAS REMOVED FROM SERVICE. CORRECTIVE ACTION R & R CAPTAIN'S FLASHLIGHT HOLDER ASSEMBLY IAW AMM 33-51-01. OPERATIONS CHECKED GOOD, THE ACFT RETURN TO SERVICE.

Part: CRADLE — BROKEN (FWD CABIN) · airframe 27,650 hrs · 24,826 cycles

FLIGHT ATTENDANT FWD FLASHLIGHT CRADLE IS BROKEN. REMOVED AND REPLACED FWD FLASHLIGHT CRADLE IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 27,572 hrs · 24,757 cycles

FLASHLIGHT BRACKET OVER FLIGHT ATTENDANT`S JUMP SEAT IS BROKEN. R & R WITH SERVICEABLE FWD FLIGHT ATTENDANT’S HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 27,578 hrs · 24,761 cycles

EMERGENCY LIGHT ON FLIGHT DECK INOPERATIVE. R & R FLT DECK EMERGENCY LAMP IAW AMM 33-50-05. LIGHT OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 27,572 hrs · 24,757 cycles

FLASHLIGHT BRACKET OVER FLIGHT ATTENDANT`S JUMP SEAT IS BROKEN. R & R WITH SERVICEABLE FWD FLIGHT ATTENDANT’S FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,269 hrs · 24,477 cycles

LEFT EXTERIOR FWD EMERGENCY LIGHT INOPERATIVE. R & R LT FWD EXTERIOR EMERGENCY LAMP IAW TASK 33-50-10-000-801-A & TASK 33-50-10-400-801-A END.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,681 hrs · 23,980 cycles

EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-50-12, OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,250 hrs · 23,527 cycles

F/A REPORTS BURNING ODOR AT ROW 15. PERFORMED OPS CHECK IAW 33-21-00 OF PASSENGER CABIN LIGHTS. NO ODOR NOTED NO FURTHER DEFECT AT THIS TIME, OPS GOOD.

Part: MECHANISM — LACK OF LUBE (MAIN DOOR) · airframe 26,008 hrs · 23,220 cycles

THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE ACFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN PAX DOOR LOCKING AND UNLOCKING MECHANISM IAW AMM 52-18-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 25,322 hrs · 22,570 cycles

ON FLIGHT 4057 THE CREW REPORTED THEY RECEIVED INITIALLY HYD 1 LOW QTY MESSAGE THEN ROUGHLY FORTY MINUTES LATER HYD SYS 1 FAIL THEN AIL SYS 1 INOPERABLE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO GRR. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 EDP IAW ERJ 145 29-10-03. RAN NR 1 ENGINE AT TAKEOFF POWER FOR MIN 3 MINUTES. CHECKED FOR LEAKS NONE NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 25,077 hrs · 22,339 cycles

ON FLIGHT 4233 THE CREW REPORTED THE RETENSION LATCH ON THE FIRST OFFICER'S FLASHLIGHT HOLDER WOULD NOT HOLD THE FLASHLIGHT IN POSITION TO CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER'S FLASHLIGHT 33-50-16 AMM EMB-140. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 24,988 hrs · 22,255 cycles

DURING B INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT HOLDER BRACKET BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT HOLDER BRACKET IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT)

FLASHLIGHT BEHIND CAPTAINS SEAT INOP. REPLACED FLASHLIGHT.

Part: FLASHLIGHT — WEAK (COCKPIT)

F/O'S FLASHLIGHT DIM. REPLACED FLASHLIGHT AND CRADLE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,352 hrs · 21,720 cycles

FRAME 23 CRACKED BELOW STRINGER 15R. REPAIRED CRACKED FRAME 23 BELOW STRINGER 15R IAW AEA EO EM-53MR-1808.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 24,353 hrs · 21,721 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR AFT FLOOR SILL AFT SUPPORT BRACKET CRACKED UNDER FLOOR SILL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR AFT FLOOR SILL AFT SUPPORT BRACKET UNDER FLOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,353 hrs · 21,721 cycles

DURING B INSPECTION FOUND THE CABIN RIGHT FLOOR SILL CORRODED AT FRAME 53. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CABIN THE RIGHT FLOOR SILL AT FRAME 53 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — CRACKED (CABIN) · airframe 24,353 hrs · 21,721 cycles

DURING B INSPECTION FOUND THE LEFT (5 EACH) AND RIGHT (3 EACH) PROXMITY LIGHT HOLDERS TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT & RIGHT PROXMITY LIGHT HOLDERS IAW EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 24,352 hrs · 21,720 cycles

LAVATORY BEAM HAS CORROSION AROUND NUT PLATE HOLE. ACCOMPLISHED EO EM-53MR-2032 LAVATORY RT FLOORBEAM CORROSION REPAIR.

Part: WIRE — BROKEN (CABIN) · airframe 24,353 hrs · 21,721 cycles

DURING B INSPECTION FOUND THE NR 8 AND THE OVERWING PROXIMITY LIGHTS TO HAVE BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 8 AND THE OVERWING PROXIMITY LIGHTS IAW EMB 140 AMM 33-50. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 24,231 hrs · 21,627 cycles

ON FLIGHT 3245 THE CREW REPORTED THE SWITCH ON THE COCKPIT FLASHLIGHT WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT FLASHLIGHT IAW MM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — INOPERATIVE (HORIZONTAL STAB) · airframe 23,905 hrs · 21,363 cycles

DURING MAINTENANCE INSPECTION LEVELING AT FL 220 WITH AUTO PILOT ENGAGED GOT PITCH TRIM MAIN INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED STAB ACTUATOR IAW AMM 27-40-02. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,879 hrs · 21,343 cycles

DURING MAINTENANCE INSPECTION, FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT REAR OVERWING EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-07. OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.

Part: O-RING — CUT (FLASHLIGHT) · airframe 23,592 hrs · 21,118 cycles

DURING B INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT SYSTEM O-RING CUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BOTTOM CAP O-RING IAW CMM DME CORPORATION 25-60-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,388 hrs · 20,942 cycles

DURING B INSPECTION, FOUND LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LAMP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,248 hrs · 20,807 cycles

ON FLIGHT 4113 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,241 hrs · 20,796 cycles

DURING B INSPECTION FOUND THE LEFT WING AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 22,904 hrs · 20,472 cycles

DURING MAINTENANCE INSPECTION FOUND THE UPPER LEFT WING EMERGENCY LIGHT BULB INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB ON LEFT WING UPPER POSITION REF 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,749 hrs · 20,352 cycles

DURING B-INSPECTION FOUND THE LEFT AFT OVER THE WING ROOT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT OVERWING ROOT EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 22,535 hrs · 20,190 cycles

ON FLIGHT 2980 THE CREW REPORTED THE OVERHEAD AISLE ROW 11 EMERGENCY HANGING FROM WIRES, VISIBLE FROM REAR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED OVERHEAD EMERGENCY LIGHT AT ROW 11 REF AMM 33-50-13. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,363 hrs · 20,065 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR EMERGENCY EXIT LIGHT IAW CMM 33-30-35. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 21,963 hrs · 19,796 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT AT 3B SIDE WALL INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESECURED CONNECTOR IAW AMM 20-00-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-20-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 21,808 hrs · 19,682 cycles

ON FLIGHT 2861 THE CREW REPORTED THAT ON DESCENT RECEIVED A "BAGG SMOKE WARNING". THE FLIGHT ATTENDANT COULD NOT SEE THROUGH THE PEEPHOLE TO VERIFY ANY SMOKE, A BAG WAS AGAINST IT . CRASH, FIRE AND RESCUE CAME OUT AND OPENED THE CARGO DOOR. NO SMOKE OR FIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD BAGGAGE SMOKE DETECTOR. THE OPERATIONAL CHECK WAS GOOD IAW ERJ 140 AMM 26-15-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 21,726 hrs · 19,612 cycles

ON FLIGHT 3085 THE CREW REPORTED THAT ON APPROACH TO LAX AT 2500 FEET THEY RECEIVED A BAGGAGE SMOKE MESSAGE ON EICAS. THE CREW DECLARED AN EMERGENCY AND LANDED AT LAX. CRASH, FIRE AND RESCUE WERE CALLED. THE CREW REPORTED THE INDICATION CAME BACK ON SEVERAL TIMES AFTER LANDING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AFT NR 2 CARGO SMOKE DETECTOR IAW ERJ 140 AMM #26-15-01-000-801-A AND #26-15-01-400-801-A. THE OPERATIONAL CHECK WAS GOOD IAW ERJ 140 AMM #26-15-00-700-804-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — DIRTY (CARGO BAY) · airframe 21,659 hrs · 19,536 cycles

ON FLIGHT 3055 ON TAXI AFTER LANDING THE CREW REPORTED, RECEIVED A SPURIOUS BAGGAGE SMOKE EICAS MESSAGE AND ILLUMINATION OF THE BAGGAGE EXTG BUTTON. THE MESSAGE WENT AWAY, LIGHT IN BUTTON DID NOT. THE CREW DECLARED AND EMERGENCY. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED EMB 140 FIM TASK 26-15-00-810-805A FOUND TO BE TRANSITORY CONDITION. UPON GENERAL VISUAL INSPECTION OF SMOKE DETECTORS 1 & 2, FOUND 1 TO BE EXTREMELY DIRTY. ALSO FOUND CAGE DAMAGED. REMOVED AND REPLACED SMOKE DETECTOR 1 IAW EMB 140 AMM 26-15-01. REMOVED AND REPLACED CAGE IAW EMB 140 AMM 26-15-0. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — SMOKE (RIGHT) · airframe 19,666 hrs · 17,608 cycles

ON FLIGHT 3060 THE CREW REPORTED THAT DURING TAKEOFF THE LAVATORY SMOKE DETECTOR WENT OFF. THE CREW RAN A CHECKLIST THEN ELECTED TO RETURN TO LAX. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT ENGINE IAW AEWC#71-000-00. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — DEFECTIVE (ENGINE) · airframe 19,943 hrs · 17,577 cycles

ON FLIGHT 3024 THE CREW REPORTED THE LAVATORY SMOKE WARNING CAME ON AFTER LIFT OFF. THE WARNING WENT OUT AFTER APPROXIMATELY 3 MINUTES. THE FLIGHT ATTENDANT TESTED THE SMOKE DETECTOR AND SYSTEM TESTED AS OK. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO LAX. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 2 CARBON SEAL ASSEMBLY IAW RRMM 72-25-25. PERFORMED ENGINE RUNS IAW RRMM 72-00-00. THE LEAK CHECK WAS GOOD. THE VIBRATION CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (GALLEY) · airframe 19,670 hrs · 17,225 cycles

ON FLIGHT 3104 AT WHEELS UP ON TAKEOFF THE CREW RECEIVED A LAVATORY SMOKE DETECTOR MESSAGE ON EICAS. THE HORN WENT OFF IN GALLEY. THE FLIGHT ATTENDANT CHECKED AND FOUND NO VISABLE SMOKE OR SMOKE ODOR. HOWEVER, THE FLIGHT ATTENDANT WAS ADVISED BY PASSENGER’S THAT THEY SMELLED SMOKE IN THE CABIN. THE CAPTAIN ELECTED TO RETURN TO LAX. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SMOKE DETECTOR PANEL FORWARD OF THE GALLEY IAW EMB 140 AMM 26-14-02. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR IAW AMM 26-14-01. PERFORMED GROUND RUNS IAW RRMM 72-00-00. NO ODOR OF SMOKE NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — WORN (AILERON) · airframe 19,365 hrs · 16,925 cycles

DURING HEAVY MAINTENANCE BASE VISIT FOUND RIGHT AILERON POWER CONTROL ACTUATOR BUSHING BORES WORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FITTING IAW EO EM-27MR-112. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 18,936 hrs · 16,581 cycles

ON FLIGHT 4145 WHILE ON THE GROUND THE FIRST OFFICER REPORTED, F/O FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW EMB140 CMM 25-60-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — JAMMED (LAVATORY) · airframe 18,195 hrs · 15,941 cycles

ON FLIGHT 4620 DURING PREFLIGHT INSPECTION THE FLIGHT ATTENDANT COULD NOT ACCESS THE DOOR TO THE LAVATORY FIRE EXTINGUISHER AS THE DOOR WAS JAMMED. LAVATORY SMOKE DETECTOR TEST PERFORMED AS REQUIRED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FIRE EXTINGUISHER TOILET PAPER DOOR ASSEMBLY IAW EMB 140 AMM25-40-01. OPEN TEST GOOD, NO FURTHER DEFECT NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE)

DURING MBV INSPECTION THE CENTER BEAM AT FRAME 25 WAS FOUND CORRODED. DAMAGE WAS CUT OUT. FABRICATED A REPAIR DOUBLE AL2024T3 .071 FILLER AND 2 SHIMS. DRILLED, CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW EMB SRM 51-00-10. ACFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING MBV INSPECTION THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. DAMAGE WAS CUT OUT. FABRICATED A REPAIR DOUBLE (AL2024T3.050), FILLER (AL2024T3.050) AND 2 SHIMS (AL2024T3.040). DRILLED, CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW EMB SRM 51-00-10. ACFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A MBV INSPECTION. A PREV REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. FABRICATED A DOUBLER, FILLER, PLATE AND TWO SHIMS. MARKED, DRILLED AND CLEANED REPAIR PARTS. REPAIR DONE IAW SRM145/1142, REF 40, CHAPTER 53-00-10, FIGURE 201. (K)

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 12,851 hrs · 11,403 cycles

ON FLIGHT 4376, CREW REPORTED RECEIVED HYDRAULIC 2 LOW QUALITY, SOON FOLLOWED BY HYDRAULIC 2 FAIL MESSAGE. CREW DECLARED EMERGENCY GOING INTO ORD. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER 2 EDMP. REMOVED AND REPLACED NUMBER 2 HYDRAULIC SYSTEM PRESSURE HYDRAULIC LINE. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (NLG) · airframe 12,482 hrs · 11,173 cycles

DISC-LND AIR/GND FAIL MESSAGE ON EICAS DURING GEAR EXTENSION. REMOVED AND REPLACED LGEU IAW EMB 140 AMM 32-21-01. RESECURED CONNECTOR ON LEFT MLG DOWN LOCK FWD PROX SWITCH 32-61-02. AIRCRAFT RETURN TO SERVICE.

Part: HOSE — DEFECTIVE (A/C BAY) · airframe 12,429 hrs · 11,129 cycles

PACK 1 FAIL EICAS MSG DID NOT HAVE ENOUGH FUEL TO CONTINUE ON TO CVG ELECTED TO DO AN AIR RETURN TO DFW DISC-SHORTLY AFTER TAKEOFF, NR 2 BLEED AND PACK VALVE CLOSED ANNUNCIATED ON THE EICAS. PER AOM; CYCLED BLEED VALVE AND PACK SEVERAL TIMES. UNSUCCESSFULLY. NR 2 PACK VALVE WOULD NOT STAY OPEN. REMOVED AND REPLACED BLEED HOSE AT DUAL TEMP CONTROL VALVE PACK OPS CK GOOD IAW EMB 140 AMM 21-20-00. AIRCRAFT RETURNED TO SERVICE.

Part: HOSE — WORN (FUEL SYS) · airframe 12,428 hrs · 11,128 cycles

ON FLIGHT 3502 PACK 2 FAIL EICAS MESSAGE DID NOT HAVE ENOUGH FUEL TO CONTINUE ON TO CVG ELECTED TO DO AN AIR RETURN TO DFW DISC-SHORTLY AFTER TAKEOFF, NR 2 BLEED AND PACK VALVE CLOSED ANNUNCIATED ON THE EICAS. PER AOM; CYCLED BLEED VALVE AND PACK SEVERAL TIMES. UNSUCCESSFULLY. NR 2 PACK VALVE WOULD NOT STAY OPEN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BLEED HOSE AT DUAL TEMP CONTROL VALVE PACK OPERATION CHECK GOOD IAW EMB 140 AMM 21-20-00. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — LEAKING (ZONE 400) · airframe 10,937 hrs · 9,986 cycles

"SUP" LAVATORY SMOKE DETECTOR GOING OFF ON TAKEOFF, VISIBLE SMOKE IN CABIN - RETURNED TO DFW. REMOVED AND REPLACED NUMBER 2 ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. ALL OPERATIONAL AND LEAK CHECKS COMPLIED WITH NO DEFECTS NOTED, RETURNED AIRCRAFT TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 9,124 cycles

DISC - FOUND GUSSET OVER RIGHT HAT BEAM BETWEEN FRAMES 59 TO 61 CORRODED. REMOVED AND REPLACED GUSSET IAW EMB IC2006-145/8562. AIRCRAFT RETURNED TO SERVICE

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 9,124 cycles

DISC - FOUND SERVICE DOOR SILL CORRODED. REMOVED AND REPLACED SILL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 9,124 cycles

DISC - FOUND GUSSET OVER LEFT HAT BEAM BETWEEN FRAMES BETWEEN 59 TO 60 CORRODED. REMOVED AND REPLACED GUSSET IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 9,124 cycles

DISC - FOUND GUSSET OVER LEFT HAT BEAM BETWEEN FRAME 59 TO 61 CORRODED. REMOVED AND REPLACED GUSSET IAW EMB IC2006-145/8562. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,753 hrs · 9,124 cycles

DISC - FOUND LEFT LOWER FORWARD SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 4,975 hrs · 4,532 cycles

DURING AN MBV INSPECTION THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM. (K)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

FOUND FORWARD BULKHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED NR 3 POWER SUPPLY. OPS CHECK GOOD. AIRCAFT RETURNED TO SERVICE. (M)

Part: DAMPER — BROKEN (RT AILERON)

DURING PHASE 4 INSPECTION, THE RT AILERON DAMPER CONTROL ROD WAS FOUND TO BE BROKEN CAUSING DAMAGE MOUNTING BRACKET ON THE AILERON. RAI RT AILERON DAMPER IAW AMM 27-12 & RAI RT AILERON IAW AMM 27-12. FCF PERFORMED AND FOUND TO BE SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)