N805AE

Part: RADIO ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 33,482 hrs · 29,855 cycles

TERRAIN WARNING AND PULL UP CALL OUTS AT ALTITUDE-C/A-FLIGHT CREW PLACARDED EGPWS MODES 1-4MEL 3421 AUTH #121081D-A MOC #680993. FLIGHT CREW PLACARDED EGPWS WINDSHEAR WARNING REF MEL 34-26 AUTH 010070D-B MOC 680820. FLIGHT CREW PLACARDED CAT II STATUS REF MEL 34-55 AUTH 010071D-A MOC 680820. REMOVED AND REPLACED RADIO ALTIMETER IAW EMB140 AMM 34-31-01. OPERATIONAL CHECKS GOOD. MEL 34-11 RESTORED. RESET RAD ALT CIRCUIT BREAKER. RADIO ALTIMETER REPLACED. MEL 34-55 REMAINS OPEN FOR MONITORING

Part: UNKNOWN — ODOR (CABIN) · airframe 33,271 hrs · 29,640 cycles

UPON LANDING WHEN SWITCHED TO THE APU BLEED AND SMELLED A STRONG EXHAUST SMELL . WE DISCONTINUED THE APU BLEED AND IT WENT AWAY-C/A-C/W FIM TASK 21-20-00-810-801-A NO FINDINGS NO SMELL. GVI OF APU COMPARTMENT NO DEFECTS NOTED C/W ETN-EM-72-034 NO SMELLS NOTED A/C OK FOR SERVICE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 32,693 hrs · 29,043 cycles

CABIN ALT INCREASED ABNORMALLY IN CONJUNCTION WITH INDICATED ALT. DIFFERENTIAL PRESS WAS 0-1 P.S.I. AIRCRAFT NEVER PRESSURIZED WHEN WE DID RESET THE PACKS.-C/A-REMOVED AND REPLACED ELECTROPNEUMATIC OUTFLOW VALVE IAW EMB 140 AMM 21-31-03. NO DEFECTS NOTED. REMOVED AND REPLACED DIGITAL CONTROLLER IAW EMB 140 AMM 21-31-01, FOR PRECAUTIONARY PURPOSES. PERFORMED MANUAL MODE PRESSURIZATION CHECK IAW EMB140 AMM 21-31-00. OPC GOOD OF MANUAL PRESSURIZATION. NO DEFECTS NOTED AT THIS TIME. PERFORMED PRESS TEST IAW EMB AMM 21-31-00 PRESS TEST GOOD NO DEFECTS NOTED.

Part: CRADLE — DEFECTIVE (FLASHLIGHT) · airframe 32,136 hrs · 28,547 cycles

FLASHLIGHT AT THE BACK IS INOP. C/A-DEFERRED AFT FLASHLIGHT AS PER MEL 25-53. AUTH # 050345-C. REMOVED AND REPLACED AFT FLASHLIGHT CRADLE ASSY IAW AMM 33-50-16 OPS CHECK GOOD MEL RESTORED.

Part: ROLLER — DIRTY (ENTRY DOOR) · airframe 31,845 hrs · 28,275 cycles

MAIN ENTRY DOOR HARD TO OPEN ESPECIALLY THE LAST INCH OF HANDLE TRAVEL. C/A-CLEANED & LUBRICATED THE MAIN DOOR FRAME ROLLER IAW ETN-EM 52-061. PERFORMED MAIN DOOR INTERNAL ACTUATING HANDLE TEST IAW AMM 52-18-00. OPC GOOD. NO DEFECTS NOTED @ THIS TIME.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 31,562 hrs · 28,004 cycles

UPON START UP OF NR 2 ENGINE CAPT DETECTED STRONG FUMES. FA ALSO DETECTED FUMES. CAPT SHUT OFF ENG AND FUMES DISSIPATED. C/W ENG ODOR EVENT IAW ETN-EM-72-034. RAN BOTH ENG NR 1 & NR 2 AT IDLE. NO STRANGE ODOR OR FUMES WERE NOTE. PERFORMED MAX PWR/ENG RUNS PER ETN-EM-72-034. NO DEFECTS FUMES/ODOR DETECTED. ALL CHECKS NORMAL PER ETN. MAX POWER RUN AND 75 TLA STILL REQUIRED FOR ITEM 3 TO 10.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,234 hrs · 27,699 cycles

AFT LH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED AFT LH OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 31,157 hrs · 27,631 cycles

MAIN CABIN DOOR IS HARD TO CLOSE-C/A-PERFORMED THE LUBRICATION OF THE MAIN DOOR FRAME ROLLERS IAW EMB 140 AMM 53-21-02. OPC GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 31,061 hrs · 27,512 cycles

BEFORE TAKEOFF ROLL TO CONFIG BUTTON INDICATED TO OK. TRIMS SET 8 UP. DURING ROLL ABOVE 80 KTS MASTER WARN TAKEOFF CONFIG TRIM. ABORTED TAKEOFF. CHECKED CONFIG BUTTON AGAIN AFTER PULLING OF RUNWAY AND IT INDICATED TO OK. C/A-PERFORMED CMC DOWNLOAD IN REF TO AMM 45-00-00, NO RELATED MAINT MSG FOUND ON CMC. AND ACP'D HORIZONTAL STAB ELEC OPS TEST IN REF TO AMM 27-40-00. TEST PASS & NO FAULT FOUND. ACFT OK TO RTN SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,943 hrs · 27,368 cycles

LT OMEGA BEAM IS CORRODED BETWEEN FRAMES 52 AND 54-C/A-REPAIRED LT OMEGA BEAM CORROSION BETWEEN FRAMES 52 AND 54 IAW ERS-EM-53MR-3430

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 30,943 hrs · 27,368 cycles

SERVICE DOOR CENTER SILL CORRODED-C/A-ACCOMPLISHED REPAIR ON SERVICE DOOR CENTER SILL IAW SRM 53-21-02.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 30,943 hrs · 27,368 cycles

FR 23 RT SPLICE REPAIR BTW STR 15R & STR 16R-C/A-REPAIRED FRAME 23 BETWEEN STRINGERS 16R-15R IAW EM-53MR-1808

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,943 hrs · 27,368 cycles

MACHINED FITTING AT FR 19-20 STR 3L CRACKED-C/A-REMOVED AND REPLACED MACHINED FITTING AT FR 19 STR 3L IAW SRM 51-40-02

Part: FITTING — CORRODED (FUSELAGE) · airframe 30,943 hrs · 27,368 cycles

FR 68 SHEAR CLIP CORRODED AT CARGO DOOR CUTOUT LOWER CORNER-C/A-REMOVED AND REPLACED WITH SERVICEABLE SECTION OF SHEAR CLIP AT FRAME 68 IAW SRM 53-31-04

Part: LIGHT — DAMAGED (CABIN) · airframe 30,943 hrs · 27,368 cycles

FOUND NR 6 FLOOR LIGHTS AND EXTRUSION DAMAGED.-C/A-REMOVED AND REPLACED NR 6 FLOOR LIGHT AND EXTRUSION IAW SWPM 20-21-00. FOUND DURING OPEN UP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,943 hrs · 27,368 cycles

LT FRAME 10 CRACKED AT UPPER END-C/A-REMOVED AND REPLACED LT FRAME 10 IAW SRM 51-40-02

Part: CONNECTOR — BROKEN (CABIN) · airframe 30,943 hrs · 27,368 cycles

FOUND NR 8 FLOOR PROXIMITY LIGHT WIRES BROKEN CONNECTORS-C/A-REPAIRED NR 8 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-21-00. FOUND DURING OPEN UP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,943 hrs · 27,368 cycles

RT FRAME 10 CRACKED AT UPPER END-C/A-REMOVED AND REPLACED RH FRAME 10 IAW SRM 51-40-02

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 30,943 hrs · 27,368 cycles

MACHINED FR 63 DOUBLER GOUGED AT STR 07R-C/A-PERFORMED REPAIR AT FR 63 STR 07R IAW EO EM-53MR-1212

Part: CONNECTOR — MISSING (CABIN) · airframe 30,943 hrs · 27,368 cycles

EMERGENCY LIGHT STRIP CONNECTOR MISSING AT 6A-C/A-COMPLETE:REPAIRED EMERGENCY LIGHT STRIP CONNECTOR AT 6A IAW SWPM 20-21-00. SEE BOW300995 FOR OPC

Part: WIRE — BROKEN (CABIN) · airframe 30,943 hrs · 27,368 cycles

EMERGENCY LIGHT STRIP NR 5 FROM FRONT OF CABIN HAS A BROKEN WIRE FROM LIGHT STRIP.-C/A-COMPLETE:INSTALLED SERVICABLE EMERGENCY LIGHT STRIP NR 5 FROM FRONT OF CABIN IAW AMM 33-50-12. SEE BOW300970 FOR OPERATIONAL CHECK OF EMERGENCY LIGHT STRIPS.

Part: CONNECTOR — MISSING (CABIN) · airframe 30,943 hrs · 27,368 cycles

EMERGENCY LIGHT STRIP CONNECTOR MISSING (AT OVER WING HATCH)-C/A-COMPLETE:REPAIRED EMERGENCY LIGHT STRIP CONNECTOR AT OVER WING HATCH IAW SWPM 20-21-00. SEE BOW300995 FOR OPC

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,943 hrs · 27,368 cycles

FOUND FWD RT EXTERNAL EMERGENCY LIGHT IN-OP.-C/A-COMPLETE: REMOVED AND REPLACED FWD RT EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 30,939 hrs · 27,363 cycles

MAIN CABIN DOOR VERY HARD TO LATCH. LUBE & OPERATIONS CHECKED MAIN CABIN DOOR IAW AMM 52-18-00. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 30,940 hrs · 27,364 cycles

FIRST OFFICER`S EMER FLASHLIGHT INOPERATIVE. R & R FIRST OFFICER`S EMER FLASHLIGHT & FLASHLIGHT BATTERY IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS AT THIS TIME.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 30,799 hrs · 27,244 cycles

CAPTAINS FLASHLIGHT HOLDER BROKEN. DEFERRED IAW MEL 25-53. INSTALLED NEW FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONAL CHECKED GOOD. MEL RESTORED.

Part: DOOR SEAL — DIRTY (PAX DOOR) · airframe 30,482 hrs · 26,974 cycles

FLIGHT ATTENDANT REPORTS THE MAIN PAX DOOR IS VERY DIFFICULT TO CLOSE & SOMEWHAT DIFFICULT TO OPEN. CLEANED & LUBRICATED MAIN DOOR RUBBER SEALS IAW AMM 52-18-00. OPENING & CLOSING GOOD.

Part: PRESSURE SWITCH — FAILED (AC BAY) · airframe 30,412 hrs · 26,914 cycles

NUMBER 1 PACK OVERLOAD CLIMBING THRU 30,000 FT. R & R OVER PRESS SW IAW AMM 21-51-06. OPERATIONS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 30,085 hrs · 26,582 cycles

AFTER TAKEOFF RETRACTED GEAR. NORMAL INDICATION ON EICAS OF GEAR RETRACTED, BUT FELT & HEARD THAT THE DOOR WAS STILL OPEN. RETURNED TO DFW. R & R NLG DOOR SEQUENCE PROXIMITY SWITCH IAW AMM 32-63-03. LG OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,491 hrs · 26,030 cycles

FLIGHT ATTENDANT`S FWD FLASHLIGHT INOPERATIVE. FLIGHT CREW PLACARDED IAW MEL 2553. R & R FWD FLIGHT ATTENDANT`S FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. MEL ITEM RESTORED.

Part: HINGE — DIRTY (CABIN DOOR) · airframe 29,436 hrs · 25,991 cycles

CABIN DOOR DIFFICULT TO CLOSE, HANDLE JAMS THE LAST FEW INCHES WHEN PUSHING DOWN HANDLE. CLEANED & LUBED CABIN DOOR ROLLER HINGE IAW AMM 53-21-02, OPERATIONS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,070 hrs · 25,668 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. R & R COCKPIT EMERGENCY LIGHT BULB IAW AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. OPS CHECK GOOD END.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,922 hrs · 25,545 cycles

FWD CABIN CEILING EMERGENCY LIGHT INOPERATIVE. R & R LAMP IN FWD AISLE EMERGENCY LIGHT IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,416 hrs · 25,082 cycles

DURING MX INSPECTION, FOUND THE F/O`S FLASHLIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT IAW 33-50-001. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 28,262 hrs · 24,937 cycles

CREW REPORTED A STRONG OIL ODOR DURING TAKEOFF AND THEN AGAIN WHEN THE ICING SYSTEM CAME ON AT ABOUT 24,000 FT. F/A ALSO COMPLAINED OF ODOR IN CABIN. ACFT REMOVED FROM SERVICE. ACCOMPLISHED FIM TASK 72-00-00-810-814, AND ETN-EM-72-034 WITH NO DEFECTS NOTED. ACFT RELEASED FOR FUNCTIONAL CHECK FLIGHT. FUNCTIONAL CHECK FLIGHT SATISFACTORY. ARICRAFT RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 28,190 hrs · 24,873 cycles

DURING MX INSPECTION, FOUND THE MAIN CABIN DOOR DIFFICULT TO OPERATE. THE ACFT WAS REMOVED FROM SERVICE. LUBED PASSENGER DOOR IAW AMM 52-18-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,755 hrs · 24,462 cycles

DURING MAINTENANCE INSPECTION FOUND THE AISLE EMERGENCY LIGHT [MIDDLE] INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AISLE EMERGENCY LIGHT BULB [MIDDLE] IAW EMB 140 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 27,720 hrs · 24,436 cycles

DURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW EMB-140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 27,216 hrs · 24,031 cycles

DURING PS-1 CHECK FOUND THE SECOND TO LAST ROW OF EMERGENCY FLOOR LIGHTING STRIPS TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. DURING REMOVAL OF LIGHTING STRIP, FOUND THE WIRE TO BE PULLED FROM THE BACK OF THE CONNECTOR. REMOVED AND REPLACED THE MALE CONNECTOR AND CONTACT IAW SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,166 hrs · 23,976 cycles

DURING B INSPECTION FOUND THE CARGO SILL HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO SILL IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 27,166 hrs · 23,976 cycles

DURING MAINTENANCE INSPECTION FOUND THE CABIN FLOOR EMERGENCY AISLE LIGHT SEGMENTS NR 1, 4, 6 & 7 PLASTIC EXTRUSION LIGHT CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1, 4, 6 & 7 PLASTIC EXTRUSION LIGHT IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — TORN (CABIN DOOR) · airframe 27,166 hrs · 23,976 cycles

DURING MAINTENANCE INSPECTION FOUND THE MAIN CABIN SEAL DOOR TORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN SEAL IAW AMM 52-18-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,992 hrs · 23,804 cycles

DURING B INSPECTION FOUND SEVERAL EMERGENCY LIGHTS INOPERABLE. SUSPECT NR 2 POWER SUPPLY FAULT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT EMERGENCY LIGHTING SYSTEM IN REFERENCE WITH W/M 33-50-50 ALL INOPERATIVE LAMPS POWERED BY NR 2 EPSU. REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY AND POWER SUPPLY UNIT IAW W/C 33-700-19 EMERGENCY LIGHTING SYSTEM OPC W/C 33-700-17 WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,830 hrs · 23,654 cycles

DURING B INSPECTION FOUND THE 2ND FROM FRONT CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE 2ND FROM FRONT AISLE CEILING EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,672 hrs · 23,494 cycles

DURING B INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM TASK 33-50-09-000-801-A AND 33-50-09-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MANIFOLD — DEFECTIVE (NLG STEERING) · airframe 26,625 hrs · 23,456 cycles

FOR FLIGHT 4206 THE CREW REPORTED, ABORTED TAKEOFF FOR MOD DUE TO HEAVY NOSE WHEEL SHIMMY AND AIRCRAFT VEERING RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT IAW EMB140 FIM 32-50-00-810-804-A. REMOVED AND REPLACED THE STEERING MANIFOLD IAW EMB140 TASK 32-50-04-000-801-A AND 32-50-04-400-801-A. PART NUMBER 3085701007, SERIAL NUMBER 0694. REMOVED AND REPLACED THE FEEDBACK UNIT POTENTIOMETER IAW TASK 32-50-07-000-801-A AND 32-50-07-400-801-A. PART NUMBER 1170A350001, SERIAL NUMBER 01205. REMOVED AND REPLACED THE NOSE LANDING GEAR WHEELS IAW W/C 32-700-17. PART NUMBER 31551, SERIAL NUMBERS 03060306 & 27242724. LUBRICATED FEEDBACK UNIT WITH AEROSHELL 33 GREASE ON THE GEARING. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,578 hrs · 23,408 cycles

DURING B INSPECTION FOUND THE FURTHEST AFT CEIING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT IAW EMB AMM TASKS 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (LH WING AFT) · airframe 26,421 hrs · 23,261 cycles

DURING MAINTENANCE INSPECTION, FOUND LEFT WING EXIT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT LT WING EXT EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,353 hrs · 23,191 cycles

DURING B INSPECTION, FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,970 hrs · 22,848 cycles

DURING B INSPECTION, FOUND THE EMERGENCY LIGHT AT SEAT 11B/C INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AISLE EMERGENCY LIGHT LAMP IAW AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,900 hrs · 22,794 cycles

DURING B INSPECTION, FOUND THE LEFT OVERWING LATERAL PANEL EXTERNAL EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT UPPER EXTERNAL EMERGENCY LIGHT LAMP RESEATED IAW AMM 33-50-07. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DEFECTIVE (FLASHLIGHT) · airframe 25,806 hrs · 25,806 cycles

ON FLIGHT 3384 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS NOT CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERYY FOR THE FIRST OFFICER’S FLASHLIGHT EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 25,386 hrs · 22,415 cycles

FOR FLIGHT 3285 THE CREW REPORTED THE MAIN CABIN DOOR WOULD NOT COMPLETELY CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED THE HINGED MAIN DOOR IAW AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 25,267 hrs · 22,335 cycles

ON FLIGHT 3417 THE CREW REPORTED THAT WHEN ANTI-ICE ACTIVATED DURING ICING CONDITIONS THERE WAS A BURNING ODOR. AFTER LANDING /PERFORMED PNEUMATIC ICE TEST ON ACTIVATION OF ICE DETECTION NR 2, THE BURNING ODOR WAS PRESENT AGAIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED NR 2 ANTI-ICING SYSTEM OPERATIONAL CHECK GOOD IAW EMB 140 AMM 30-00-00. NO SMELLS NOTED. FOUND BIRD INGESTED IN NR 2 COMPLIED WITH NR 2 ENGINE BOROSCOPE INSPECTION COMPRESSOR SECTION IAW ETN EM 72-026 NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — NOT SEATED (CABIN) · airframe 25,002 hrs · 22,138 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEATED EMERGENCY OVERWING LAMP. THE EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — NOT SEATED (CABIN) · airframe 24,972 hrs · 24,972 cycles

DURING B-INSPECTION FOUND THE LEFT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SEATED LAMP IN LEFT AFT OVERWING EMERGENCY LIGHT IAW EMB 140 AMM 33-50-10. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ADC — FAILED (NR 1) · airframe 24,041 hrs · 21,282 cycles

IAS- AMBER ON BOTH PFDS AT 80 KNTS ON T/O ROLL. ABORTED T/O. REMOVED AND REPLACED NR 1 ADC.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,512 hrs · 19,887 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT OMEGA BEAM AT FRAME 20 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT OMEGA BEAM AT FRAME 20 IAW SRM 53-00-10 FIG.202 SHEET 2. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,512 hrs · 19,887 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 23 CRACKED .75 INCH BETWEEN STRINGERS 15 RIGHT AND 16 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 IAW ENGINEERING ORDER EM-53MR-1750. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOSE — BLOWN (AC PACK) · airframe 21,931 hrs · 19,405 cycles

ON FLIGHT 2919 DURING THE CLIMB THE CREW REPORTED, RECEIVED A PACK 1 VALVE CLOSED MESSAGE ON EICAS. THE CREW RESET PER AIRCRAFT OPERATIONS MANUAL VOLUME 1 WHICH CLEARED. 5-10 MINUTES LATER THE CREW DETECTED A SMOKE ODOR FOLLOWED BY PACK 1 VALVE CLOSED MESSAGE. THE CREW ELECTED TO RETURN TO DFW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED A BLOWN OUT HOSE ON THE NR 1 PACK BETWEEN THE DUAL TEMPERATURE CONTROL VALVE AND THE PACK VALVE IAW EMB-140 AMM 21-51-01. THE OPERATIONAL CHECK WAS OK. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 18,515 hrs · 16,406 cycles

ON FLIGHT 4141, DURING A ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT FLOOR PROXIMITY STRIP (LEFT AFT) HAS BROKEN WIRES. ISSUED MEL. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 18,155 hrs · 16,406 cycles

ON FLIGHT 4141, DURING A ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT FLOOR PROXIMITY STRIP (LEFT AFT) HAS BROKEN WIRES. REMOVED AND REPLACED FLOOR PROX STRIP. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (MLG) · airframe 15,579 hrs · 13,926 cycles

ON FLIGHT 4820, CREW REPORTED UPON GEAR RETRACTION GOT 'LANDING GEAR HANDLE DISAGREE WITH GEAR DOWN AND UNSAFE INDICATION. CYCLED GEAR AND GEAR CAME UP. AIRCRAFT REMOVED FROM SERVICE. AFTER TROUBLESHOOTING DETERMINE LANDING GEAR HANDLE FOUND TO BE DEFECTIVE. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW AMM 32-32-02. PERFORMED SEVERAL OPERATIONAL SYSTEM CHECK IAW EMB AMM 32-30-00. OPERATIONAL CHECK GOOD, NO FURTHER DEFECTS NOTED AND NR 8194; AIRCRAFT RETURNED TO SERVICE.

Part: SQUAT SWITCH — WORN (MLG) · airframe 15,545 hrs · 13,890 cycles

ON FLIGHT 4915, CREW REPORTED JUST AFTER TAKEOFF WHEN SELECTING GEAR UP, GOT A LANDING LEVER DISAGREE ON EICAS. CYCLED GEAR AS PER AOM PROCEDURES. SAME MESSAGE. CYCLED LEVER DOWN GOT 3 GREEN AND NO LEVER DISAGREE MESSAGE. RETURNED TO CVG. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED HARNESS AND NOSE WOW SWITCH PER EMB AMM 32-63-05. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 14,780 hrs · 13,306 cycles

STRONG OIL ODOR IN BLEED SYSTEM AFTER TAKEOFF AND ON FINAL APPROACH. REMOVED AND REPLACED NR 1 ENGINE IAW EMB WORK CARD NR 71-000-00. GROUND RAN AND LEAK CHECKED IAW EMB WORK CARD 72-700-00. NO DEFECTS AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — FUMES · airframe 14,757 hrs · 13,282 cycles

TURBINE OIL FUMES ARE BEING INTRODUCED INTO THE CABIN AND COCKPIT THROUGH ENG BLEED 1. IF BOTH PACKS ARE DRIVEN FROM BLEED 2.

Part: SENSOR — MALFUNCTIONED (NR 3 BRAKE) · airframe 14,638 hrs · 13,157 cycles

IN CLIMB, RIGHT INBOARD BRAKE OVERHEAT EICAS MSG CON ON. TEMP CAME DOWN THEN TEMP WENT BACK UP TO TOP OF GAUGE THEN WENT BLANK THEN GAUGES NORMAL IN GREEN. RETURNED TO SJC. AFT LANDED BRAKE TEMP OVERHEAT EICAS MESSAGE APPEARED AGAIN. TEMP GAUGE TO MAX ON TAXI TO GATE GAUGE WENT TO FULL HOT TO NORM BACK TO HOT. LANDING VSI AT 300 FPM AND 40,500 LBS. NO MTX REQ FOR OVERWEIGHT LANDING. REMOVED AND REPLACED RIGHT HAND NR 3 BRAKE TEMP SENSOR IAW EMB AMM 32-47-01 OPERATIONAL CHECK GOOD AIRCRAFT RETURNED TO SERVICE

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 14,540 hrs · 13,047 cycles

STRONG OIL ODOR IN BLEED/PACK SYSTEM AFTER TAKEOFF. MEL ISSUED 21-29 WHEN PACK NR 1 WAS FOUND CAUSING ODOR. REMOVED AND REPLACED LT ZERO CARBON SEAL IAW EMB MM 72-25-25. PERFORMED OPS CHECK ON LT BLEED AIR SYS IAW EMB MM 21-20-00. NO OIL ODOR NOTED, AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — FAILED (PARKING BRAKE) · airframe 13,495 hrs · 11,893 cycles

ABORTED TAKEOFF, RECEIVED NO TAKEOFF CONFIGURATION WARNING ON EICAS, FLAPS AT 9 DEGREES, SPOILER CLOSED, TRIM AT 7 DEGREES AND TL AT 75 PERCENT. REMOVED AND REPLACED EMERGENCY PARKING BRAKE PRESSURE SWITCH IAW EMB AMM 32-44-07, PERFORMED CONFIGURATION OPERATIONAL CHECK IAW AMM 31-51-00 WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,051 hrs · 11,543 cycles

FOUND CARGO DOOR FRAME LOWER SILL CORRODED. REMOVED AND REPLACED LOWER SILL IAW EMB SRM 51-40-02. RESTORED PROTECTIVE FINISH, RETURNED AIRCRAFT TO SERVICE.

Part: STRINGER CLIP — CORRODED · corrosion level 2 · airframe 13,051 hrs · 11,543 cycles

FOUND SHEAR CLIP AT FRAME 68 CORRODED. PERFORMED CUTOUT OF DAMAGED AREA. FABRICATED REPAIR PIECES, INSTALLED REPAIR PIECES IAW EMB IC2007-145/00513A. RESTORED PROTECTIVE FINISH, RETURNED AIRCRAFT TO SERVICE.

Part: STRINGER CLIP — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 13,051 hrs · 11,543 cycles

FOUND STRINGER CLIP AT FRAME 65 TO BE CORRODED. PERFORMED CUTOUT OF DAMAGED SHEAR CLIP, FABRICATED REPAIR PIECES. INSTALLED REPAIR PIECES IAW EMB IC2007-145/00513A. RESTORED PROTECTIVE FINISH, RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,051 hrs · 11,543 cycles

FOUND LEFT OMEGA BEAM CORRODED AT FRAME 25. PERFORMED CUTOUT OF DAMAGE, FABRICATED REPAIR PIECES. INSTALLED REPAIR PIECES IAW EMB SRM 53-00-10. RESTORED PROTECTIVE FINISH. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,051 hrs · 11,543 cycles

FOUND CENTER FLOORBEAM CORRODED AT FRAME 24. PERFORMED CUTOUT OF DAMAGE, FABRICATED REPAIR PIECES. INSTALLED REPAIR PIECES IAW EMB SRM 53-00-10. RESTORED PROTECTIVE FINISH AND RETURNED AIRCRAFT TO SERVICE.

Part: UNKNOWN — NOISY (NLG) · airframe 12,630 hrs · 11,219 cycles

HEARD A NOISE IN THE NOSE GEAR AREA AFTER GEAR RETRACTION.

Part: UNKNOWN — VIBRATION (FUSELAGE) · airframe 12,606 hrs · 11,200 cycles

DISC - AIRFRAME SHUDDERED DURING FLIGHT SEVERAL TIMES. CREW REPORTED THAT IT FELT LIKE SEVERAL BIRDS HAD HIT THE LOWER FUSELAGE.

Part: INSULATION — DAMAGED (E/E BAY)

CLT - FLT 4495 - AFTER TAKEOFF HAD A STRONG ELECTRICAL SMELL IN THE COCKPIT, NO SMOKE NOTED RETURNED TO CLT, NO OTHER PROBLEMS. REMOVED THERMOACOUSTIC INSULATION PADS FROM AVIONIC FAN AND REPAIRED DAMAGED INSULATION PER ETN EM 25-120, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND AFT RIGHT SILL CORRODED IN NUMEROUS AREAS. REMOVED AND REPLACED RIGHT AFT SILL AS PER SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND FORWARD DOUBLER CORRODED TOP AND BOTTOM SURFACES. REMOVED AND REPLACED FORWARD DOUBLER AS PER SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND RIGHT FORWARD SERVICE DOOR SILL CORRODED IN NUMEROUS AREAS. REMOVED AND REPLACED SILL ASSEMBLY AS PER SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP INSPECTION, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20, FORWARD CABIN. COMPLIED WITH LEFT OMEGA SHAPED BEAM REPAIR IAW SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

SAW - FOUND DURING CPCP INSPECTION, FOUND CORROSION ON SERVICE DOOR SILL IN FORWARD CABIN GALLEY. REMOVED AND REPLACED SERVICE DOOR SILL IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FIREWALL — CRACKED (APU)

SAW - FOUND CRACKS ALONG APU FIREWALL WHEN INSTALLING APU. REPLACED APU FIREWALL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — MALFUNCTIONED (E/E BAY)

DFW - FLT 3574 - DURING LANDING ROLL CREW RECEIVED PITCH TRIM 1/2 INOPERATIVE MESSAGE AFTER A/P DISCONNECT. NO PROBLEMS WITH A/P SWITCH BEING STUCK. CREW DID NOT RESET C/B'S. MAINTENANCE REMOVED AND REPLACED THE HORIZ STABILIZER CONTROL UNIT IAW EMB MM AFTER COMPLYING WITH ETN EB-27-022. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)