N818AE

Part: ANTI-ICE VALVE — FAILED (RT WING) · airframe 38,039 hrs · 34,599 cycles

WG A/ICE FAIL ON DESCENT IN ICING CONDITIONS, QRH COMPLIED WITH, MESSAGE WENT AWAY-C/A-REMOVED AND REPLACED WING A/ICE VALVE 2. IAW AMM 30-11-01. NO DEFECTS NOTED. HIGH PWR RUN REQ'D. PERFORMED HIGH POWER RUN FOR WING 2 ANT ICE VALVE OPC. GOOD IAW EMB 140 AMM 30-00-00. NO DEFECTS NOTED.

Part: DOOR — LACK OF LUBE (MAIN CABIN) · airframe 37,625 hrs · 34,190 cycles

MAIN CABIN DOOR DIFFICULT TO CLOSE AND OPEN. INSPECTED ,CLEANED & LUBED MAIN DOOR ACTUATING & LOCKING MECHANISM IAW AMM 52-11-00 OPS CHECKS GOOD.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 37,210 hrs · 33,758 cycles

FA REPORTS MAIN DOOR DIFFICULT TO OPEN AND CLOSE. LUBRICATED MAIN DOOR ACTUATING AND LOCKING MECHANISM IAW EMB 140 AMM 52-18-00. OPC GOOD.

Part: FLASHLIGHT — MALFUNCTIONED (FWD CABIN) · airframe 37,076 hrs · 33,623 cycles

FWD FLASHLIGHT FLICKERS WHEN TURNED TO ON. REMOVED AND REPLACED FWD FLASHLIGHT ASSY IAW AMM 33-50-16 OPC GOOD

Part: DOOR — LACK OF LUBE (CABIN) · airframe 36,995 hrs · 33,543 cycles

FA UNABLE TO OPEN PAX DOOR FROM INSIDE. DOOR IS ABLE TO OPEN FROM THE OUTSIDE. C/A-APLIED LUBED TO PAX DOOR IAW AMM 52-10-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,983 hrs · 32,677 cycles

EMERGENCY LIGHT ABOVE FA SEAT FOUND TO BE INOP DURING PS2 CHECK-C/A-REMOVED AND REPLACED PANEL SIGN ASSEMBLY OF FWD EXIT SIGN IAW EMB140 AMM 33-50-14. OPC FAIL. ITEM REQUIRES FURTHER T/S. REMOVED AND REPLACED INVERTER FROM FWD CABIN CLOSET IAW EMB140 AMM 33-50-11. OPC OF EMERGENCY LIGHT ABOVE FA SEAT GOOD. NO DEFECTS NOTED. INVERTER P/N 7824-1

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 35,109 hrs · 31,798 cycles

MAIN PAX DOOR HANDLE BINDING, UNABLE TO OPEN THE DOOR. CLEANED, LUBRICATED, AND TESTED THE MAIN PAX DOOR IAW AMM 52-18-00. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: ENGINE — ODOR (RIGHT) · airframe 34,916 hrs · 31,572 cycles

WITH THE RT ENGINE RUNNING AT MAX POWER, THE NR 2 BLEED OPEN AND NR 1 PACK SELECTED, A STRONG ODOR WAS PRESENT IN THE COCKPIT. WITH THE RT ENGINE AT MAX POWER AND NR 1 BLEED OPEN, AND NR 1 PACK SELECTED, NO ODOR PRESENT, THE RT ENGINE IS PROCUDING A STRONG ODOR AT MAX POWER. AFTER COMPRESSOR WASH WAS COMPLIED WITH ODOR EVENT ETN-EM-72-034, NO ODORS DETECTED. PERFORMED A NR 2 ENGINE COMPRESSOR WASH IAW MM 72-00-00-100-801. OPS CHECKED GOOD IAW ETN-EM-72-034. NO ODORS DETECTED.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 34,873 hrs · 31,524 cycles

MAIN CABIN DOOR WILL STICH & NOT CLOSE OR OPEN. LUBRICATED MAIN DOOR ROLLERS AND OPS CHECKED GOOD IAW AMM 52-18-00.

Part: SUPPORT — LOOSE (AFT CARGO DOOR) · airframe 34,742 hrs · 31,382 cycles

CARGO DOOR OPENED AFTER TAKEOFF, NO PRESSURIZATION ISSUES. FOUND THE AFT CARGO DOOR SWITCH SUPPORT LEVER WITH A LOT OF PLAY. REMOVED AND REPLACED THE AFT CARGO DOOR SWITCH IAW AMM 52-76-01-04, OPS CHECKED IAW AMM 52-76-01-05, AND PRESSURIZED AIRCRAFT IAW AMM 21-31-00, COULD NOT DUPLICATE FAULT.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,685 hrs · 31,318 cycles

AFT EMERGENCY EXIT ROW 11 A, B, & C CENTER AISLE INOPERATIVE. CONNECTED THE AFT OVERHEAD EMERGENCY EXIT SIGN. OPS CHECKED GOOD.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 34,466 hrs · 31,095 cycles

NR 1 EMERGENCY LIGHT CONNECTOR FOUND BROKEN. REMOVED AND REPLACED THE CONNECTOR IAW SWPM 20-21-00.

Part: FRAME — CHAFED (FR 81) · airframe 34,466 hrs · 31,095 cycles

FRAME 81 HAS MULTIPLE CHAFES AT THE 6 O'CLOCK POSITION. ACCOMPLISHED A REPAIR IAW ERS-EM-53MR-3111.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 34,466 hrs · 31,095 cycles

SERVICE DOOR LOWER SILL IS CORRODED AROUND 2 SCREW HOLES. REMOVED CORROSION, SERVICE DOOR LOWER SILL AROUND 2 SCREW HOLES. IAW CPM 51-14-02. BLENDED AREA ON SERVICE DOOR LOWER SILL AROUND FWD SCREW HOLE FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-21-02.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 34,466 hrs · 31,095 cycles

CARGO DOOR CUT-OUT LOWER SILL CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02, AND 51-20-03.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 34,466 hrs · 31,095 cycles

CARGO DOOR CUT-OUT FWD ANGLE CORRODED ON LOWER END. REMOVED AND THE ANGLE IAW SRM 53-31-04, FIGURE 212.

Part: SKIN — CHAFED (RUDDER) · airframe 34,466 hrs · 31,095 cycles

RUDDER 1 HAS CHAFE ABOVE PANEL 326AL. REPAIRED THE SKIN IAW ERS-EM-55MR-633.

Part: FRAME — CHAFED (FRM 69) · airframe 34,466 hrs · 31,095 cycles

FRAME 69 CHAFED AT THE V-BAND CLAMP, STRINGER 19L. REPAIRED THE FRAME IAW SRM 53-00-04.

Part: LIGHT — UNKNOWN (CABIN) · airframe 34,407 hrs · 31,040 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. PERFORMED AN OPS CHECK, CHECKED GOOD IAW AMM TASK 33-50-00-700-801-A

Part: TANK UNIT — FAILED (LEFT) · airframe 33,992 hrs · 30,650 cycles

IMMEDIATELY AFTER TAKE OFF, RECEIVED A FUEL IMBALANCE. TANK 1 INDICATION DROPPED APROX. 900 LBS. BOTH QUANTITY INDICATIONS WERE ERRATIC AND BECAME UNRELIABLE. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. REMOVED AND REPLACED FUEL T/U NR 2 ON LT SIDE AND FUEL T/U NR 3 AND 4 ON RH SIDEIAW AMM 28-41-02 SYSTEM OPS CHECKS GOOD. FUEL TANK UNIT

Part: CONNECTOR — BROKEN (CABIN) · airframe 32,505 hrs · 29,238 cycles

FLOOR PROXIMITY STRIP LIGHT AT FLOORBOARD 251JF HAS A BROKEN CONNECTOR. REPAIRED FLOOR PROXIMITY STRIP LIGHT IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD.

Part: FILTER — DIRTY (BLEED AIR SYS) · airframe 32,092 hrs · 28,769 cycles

BLEED 1 OVERTEMP INFLIGHT. VISUALLY INSPECTED FAN AIR VLV LINES, NO DAMAGE FOUND. FOUND CLEAN FAN AIR VLV FILTER IAW AMM 36-11-03. PERFORMED OPERATIONS CHECK IAW AMM 36-00-00, DID NOT FIX REF ITEM 3. R & R FAN AIR VLV IAW AMM 36-11-03. OPERATIONS CHECKED GOOD IAW AMM 36-00-00.

Part: DETECTOR — FAILED (NR 1) · airframe 31,934 hrs · 28,612 cycles

AFTER TAKING RUNWAY FOR POSITION & HOLD RECEIVED ICE CONDITION ADVISORY MSG FOLLOWED BY A ICE CONDITION. ANTI-ICE WARNING MSG PRIOR TO TAKEOFF ROLL. AFTER A FEW MINUTES MSG'S WENT AWAY BUT CAME BACK AGAIN, ON TAXI BACK TO GATE. TROUBLESHOOT SYS FOUND NR 1 ICE DETECTOR FAIL. R & R NR 1 ICE DETECTOR IAW AMM 30-80-01. OPERATIONS CHECKED GOOD. NO MSG FOUND IAW AMM 30-80-00.

Part: WIRE — BROKEN (CABIN) · airframe 31,933 hrs · 28,610 cycles

LIGHT ELEMENT OF PROXIMITY LIGHT STRIP, NR 6 HAS A BROKEN WIRE. R & R NR 6 FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. SEE NRTC BOW 205943 FOR OPERATIONAL CHECK.

Part: WIRE — CHAFED (CABIN) · airframe 31,933 hrs · 28,610 cycles

PROXIMITY LIGHT STRIP NR 1 WIRE AT THE FLOORBOARD IS MISSING AN ELEC CONNECTOR & THE SAME WIRE IS CHAFED WITH BARE WIRE SHOWING. R & R ELEC CONNECTOR, MALE & ACFT SIDE, AT SPLICE SP9019 FOR THE NR 1 PROXIMITY LIGHT STRIP IAW SWPM 20-21-00, 20-50-00 & 20-50-01. OPERATIONAL CHECKED GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,933 hrs · 28,610 cycles

FRAME 23 IS CRACKED, BETWEEN STRINGER 15R - 16R. REPAIRED FRAME 23 AT STRINGER 16R IAW SRM 51-40-02 & EO EM-53MR-1808.

Part: CONNECTOR — MISSING (CABIN) · airframe 31,933 hrs · 28,610 cycles

EMERGENCY LIGHT STRIP WIRE AT SEAT LOCATION 13 A IS MISSING SPLICE CONNECTOR. REPAIRED & INSTALLED SERVICEABLE SPLICE CONNECTOR ON EMER LIGHT STRIP WIRE AT SEAT LOCATION 13A IAW SWPM 20-21-00. SEE BOW 205943 FOR OPERATIONS CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,931 hrs · 28,608 cycles

POSSIBLE CRACKS ON LT REAR FUSELAGE RIVETS FRAMES 77 - 79. REPAIRED LT UPPER FUSELAGE SKIN CRACK AT FRAME 77 & STRINGER 06L IAW ERS-EM-53MR-1795.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,931 hrs · 28,608 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 & ABOVE STRINGER 2R, CRACK IS APPROX 3/8" LONG. REPAIRED IAW ERS-EM-53MR-1793.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,931 hrs · 28,608 cycles

CENTER FLOORBEAM HAS CORROSION AFT OF THE CROSS MEMBER AT FRAME 27. REPAIRED CTR FLOORBEAM CORROSION AFT OF THE CROSS MEMBER AT FRAME 27 BY INSTALLED EXTERNAL ANGLE, FILLER & SHIMS IAW SRM 53-00-10, 51-40-02. CPM 51-21-06, ETN-EM-51-075 & ETN-EM-51-091.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,931 hrs · 28,608 cycles

LEFT OMEGA BEAM HAS CORROSION, FWD OF THE CROSS MEMBER AT FRAME 27. REPAIRED LT OMEGA BEAM CORROSION BY INSTALLING REPAIR DOUBLER IAW SRM 53-00-10 FIG 202 SHEET 2, CPM 51-21-05 & ETN-EM-51-075.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 31,931 hrs · 28,608 cycles

FORWARD SERVICE DOOR SILL IS CORRODED. REPAIRED FWD SERVICE DOOR SILL IAW ERS-EM-53MR-1792.

Part: CONNECTOR — MISSING (CABIN) · airframe 31,931 hrs · 28,608 cycles

EMERGENCY LIGHT STRIP WIRE AT SEAT LOCATION 13A IS MISSING SPLICE CONNECTOR. REPAIRED & INSTALLED SERVICEABLE SPLICE CONNECTOR ON EMER LIGHT STRIP WIRE AT SEAT LOCATION 13A IAW SWPM 20-21-00. SEE BOW 205943 FOR OPERATIONS CHECK.

Part: BOLT — LEAKING (FUEL SYSTEM) · airframe 31,911 hrs · 28,586 cycles

STRONG FUEL SMELL IN COCKPIT. REMOVED, REINSTALLED & RESEALED BOLT AT STRINGER 18R & FRAME 40 IAW AMM 20-10-01 & SRM 51-21-01. SEE NRWC 818-ABI-02100 FOR DETAILS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,595 hrs · 28,265 cycles

EMERGENCY LIGHT IN PSU PANEL AT SEAT 11A INOPERATIVE. REMOVED & INSTALLED SERVICEABLE LAMP IN PSU PANEL AT SEAT 11A IAW AMM 33-50-07. OPERATIONS CHECKED GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 31,338 hrs · 27,993 cycles

AFTER CLIMB OUT ACFT WAS NOT PRESSURIZING. WE CLIMBED UP TO 10000 FT & RETURNED. R & R AUTO DIGITAL CONTROL IAW AMM 21-21-01. OPERATIONS CHECKED GOOD. PERFORMED FUNCTIONAL AUTO PRESSURIZATION TEST IAW AMM 21-31-00. OPERATIONS CHECKED GOOD.

Part: BRAKE — CONTAMINATED (MLG) · airframe 30,985 hrs · 27,684 cycles

HYDRAULIC FLUID UNDER NR 1 BRAKE ASSEMBLY. VISUAL CHECK & OPERATIONAL OF NR 1 BRAKE ASSEMBLY NO LEAKS NOTED IAW AMM 32-41-00.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 30,935 hrs · 27,646 cycles

AT FL 310 IN & OUT OF WEATHER INCLUDING THUNDERS STORM CELLS IN VICINITY, STRONG ODOR OF SMOKE POSSIBLY ELEC IN COCKPIT & CABIN LASTING 2 - 3 MINUTES & DISSIPATED. ODOR IN CABIN LASTED UNTIL LANDING, NEVER SAW SMOKE ONLY SMELLED SMOKE. DECLARED EMER LANDING NORMALLY, DEPLANED. PERFORMED ETN EM-72-034, ODOR WAS DETECTED MOMENTARILY ON CONFIGURATION 3. AT FULL POWER E1 BLEED ON COCKPIT PACK MOPS ON, HOWEVER, SUBSEQUENT ATTEMPTS TO DUPLICATE ODOR UNDER SAME CONDITIONS FAILED. REFERENCE ITEM 1 LOG PAGE 3757459 FOR FCF.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 30,779 hrs · 27,512 cycles

CAPTAINS EMER FLASHLIGHT CRADLE BROKEN. R & R CAPTAINS EMER FLASHLIGHT CRADLE IAW TASK 33-50-16-000-801-A & TASK 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 30,491 hrs · 27,270 cycles

TRANSFERRED FROM NRWC 818-CMI-01732 ITEM 1. FWD CABIN FLASHLIGHT CRADLE BROKEN. FLIGHT ATTENDANT FWD FLASHLIGHT ASSEMBLY DEFERRED IAW MEL 25-53. FLIGHT ATTENDANT SPARE FLASHLIGHT STORED FWD ENTRY RT STORAGE. R & R CRADLE IAW AMM 25-61-02. OPERATIONS CHECKED GOOD. MEL RESTORED.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 30,389 hrs · 27,190 cycles

FLASHLIGHT IN FWD CABIN IS INTERMITTENT. R & R FWD CABIN FLASHLIGHT IAW AMM 33-50-16.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 30,389 hrs · 27,190 cycles

FLASHLIGHT IN THE AFT CABIN IS INOPERATIVE. R & R AFT CABIN FLASHLIGHT IAW AMM 33-50-16.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 30,158 hrs · 27,024 cycles

ACCESS DOOR OPEN ON EICAS & DOORS ON MFD SHOWS FWD AVIONICS DOOR OPEN AS GEAR CAME UP ON TAKEOFF. OPENED & CLOSED FWD ELEC COMPARTMENT DOOR. OPERATIONS CHECKED GOOD IAW AMM 52-71-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,120 hrs · 26,989 cycles

DURING PS 1 INSPECTION FOUND RT AFT EXTERNAL EMER LIGHT INOPERATIVE. R & R RT AFT EXTERNAL EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 29,139 hrs · 26,147 cycles

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

Part: CONTROL VALVE — MALFUNCTIONED (BRAKE SYS) · airframe 29,126 hrs · 26,136 cycles

DURING TAXI AFTER LANDING, RECEIVED SEVERAL BRAKE DEGRADED, WARNING MESSAGES ON EICAS. REPLACED RT INBD SHUTTLE VALVE. AMM ETN-EM-32-236 DID NOT FIX THE PROBLEM, BRAKE DEGRADE REMAINS. REMOVED AND REPLACED BRAKE CONTROL VALVE ELECTRICAL CONNECTOR IAW STD WIRING PRACT. MANUAL . OPS AND TAXI CHECKED GOOD IAW AMM 32-41-03.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 29,069 hrs · 26,086 cycles

WINDSHIELD ON FIRST OFFICER`S SIDE CRACKED TAXING IN. R & R FIRST OFFICER`S WINDSHIELD IAW AMM 56-10-01. OPERATIONS CHECK LEAK TESTED GOOD IAW ITEM NR 3 & NR 4 DEFERRALS.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 28,934 hrs · 25,953 cycles

FLIGHT ATTENDANT`S FWD FLASHLIGHT HOLDER BROKEN. R & R FLIGHT ATTENDANT`S FWD FLASHLIGHT HOLDER IAW AMM 35-50-00, OPERATIONS CHECKED GOOD.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 28,493 hrs · 25,550 cycles

HYDRAULIC 1 LOW QTY APPEARED ON EICAS IN CRUISE MONITORED HYD 1 QTY & IT WENT TO ZERO. NR 1 ELEC HYD PUMP MAY HAVE RUN UP TO 5 MINUTES WITH QTY AT ZERO. HYD 1 FAIL APPEARED ON EICAS AFTER ABOUT 20 MINUTES. COMPLIED WITH AOM VOLUME 1 ABNORMAL CHECK LIST. TRANSFERRED TO NRWC 818-ORD-01391. INSPECTED NR 1 HYD MANIFOLD BYPASS PINS, BYPASS PINS DO NOT SHOW BYPASS CONDITION. PERFORMED OPERATIONS CHECK OF NR 1 EMDP IAW MM 29-10-04, OPERATIONS CHECKED GOOD. R & R NR 1 HYD PUMP IAW AMM 29-10-03, OPERATION CHECK & LEAK CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,423 hrs · 25,477 cycles

FORWARD FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT CRADLE BROKEN. R & R FWD FLIGHT ATTENDANT`S FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO SMOKE) · airframe 27,715 hrs · 24,891 cycles

DURING FERRY FLIGHT, AT 1000 AGL FINAL, FULLY CONFIGURED, CREW RECEIVED A CARGO SMOKE INDICATION ALONG WITH CARGO SMOKE BOTTLE INOPERATIVE CAUTION MESSAGES. EXECUTED EMERGENCY PROCEDURE IAW AOM VOLUME 1 AND DECLARED AN EMERGENCY. NO FIRE INDICATION OBSERVED AFTER LANDING BY EITHER THE F/A THROUGH THE AFT SIGHT GLASS OR FIRE CREW ON GROUND. POST LANDING INSPECTION REVEALED AN EXCESS WATER AND MOISTURE DRIPPING FROM REAR FUSELAGE DUE TO THE LONG FLIGHT IN RAIN. PERHAPS MOISTURE WAS A CONTRIBUTING FACTOR TO THE ERRONEOUS INDICATION OF CARGO SMOKE. REMOVED AND INSTALLED NEW CARGO BAY BOTTLES IAW AMM 26-23-01. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 27,538 hrs · 24,706 cycles

FLIGHT 3427, CAPTAIN`S FLASHLIGHT NOT WORKING. REMOVED AND REINSTALLED THE ASSY AND RECONNECTED THE CONNECTOR. OPS CHECKED GOOD IAW AMM 33-50-16. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — ODOR (COCKPIT) · airframe 27,524 hrs · 24,698 cycles

ELECTRICAL ODOR SEEMS TO COME FROM COCKPIT AROUND CONTROLLER. FOUND GFC PANEL WITH ELECTRICAL ODOR. R & R FGC PANEL IAW AMM 22-11-01. OPS CHECKS GOOD. ACFT RVSM ELIGIBLE. ACFT IS COMPLIANT FOR CONTINUE CAT II OPERATIONS.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 26,893 hrs · 24,202 cycles

THE CREW REPORTED THAT ON THE LANDING ROLLOUT THEY RECEIVED A BAGGAGE SMOKE EICAS MESSAGE. UPON COMING TO A COMPLETE STOP AND SETTING THE PARKING BRAKE THE CREW RAN THE CHECK LIST PROCEDURE IAW AOM-1 AND THE EPC. THE CREW CALLED CRASH, FIRE AND RESCUE AND THEY FOUND NO EVIDENCE OF FIRE OR SMOKE. THE ACFT TAXIED TO THE GATE UNDER ESCORT. THE ACFT WAS REMOVED FROM SERVICE. R & R THE BAGGAGE COMPARTMENT FORWARD SMOKE DETECTOR IAW AMM 26-15-01. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 26,756 hrs · 24,080 cycles

FR 65 SHEAR TIE CORRODED IN FRONT OF CARGO DOOR SILL. REPAIRED SHEAR TIE IAW EO EM-53MR-1129, PART A.

Part: WIRE — BROKEN (CABIN) · airframe 26,841 hrs · 24,162 cycles

DURING MX INSPECTION, FOUND THE CABIN AISLE NR1 EMERGENCY LIGHT STRIP HAS BROKEN WIRES. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 1 PROXIMITY LIGHT STRIP IAW AMM 35-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 26,756 hrs · 24,080 cycles

FR 68 SHEAR TIE CORRODED AFT OF CARGO DOOR SILL. REPAIRED SHEAR TIE IAW EO EM-53MR-1129, PART B.

Part: WIRE — BROKEN (CABIN) · airframe 26,841 hrs · 24,162 cycles

DURING B INSPECTION, FOUND THE EMERGENCY EXIT OVERHEAD CEILING PANEL NR 253CLC HAS EMERGENCY LIGHT WIRE BROKEN. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED BROKEN WIRE ON CEILING PANEL NR 253CLC IAW SWPM 20-50-01. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,782 hrs · 23,220 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-09. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,530 hrs · 22,986 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR GUIDED EMERGENCY LIGHT AT ROWS 9 AND 10 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT STRIP AS PER AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUNRED TO SERVICE.

Part: DOOR — BINDING (MAIN PAX) · airframe 24,785 hrs · 22,303 cycles

FLIGHT 9807, CREW REPORTED MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN - MECHANICALLY 1ST STEP OPEN OK 2ND STEP DOOR BINDS MECHANISM. THE AIRCRAFT WAS REMOVED FROM SERVICE. RIGGED PASSENGER DOOR IAW AMM 52-18-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,769 hrs · 22,286 cycles

DURING B INSPECTION, FOUND THE FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,603 hrs · 22,121 cycles

DURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT BULB IAW EMB-145 AMM 33-50-06. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 24,356 hrs · 21,888 cycles

ON FLIGHT 2712 THE FLIGHT ATTENDANT REPORTED THAT WHEN PUSHING THE CABIN DOOR OPEN IT STICKS AND NEEDS TO BE JIGGLED. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN DOOR FRAME ROLLERS IAW EMB-140 AMM 53-21-02. THE FUNCTIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 24,137 hrs · 21,714 cycles

ON FLIGHT 2717 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN CABIN DOOR. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD PER AMM 52-18-00. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 23,974 hrs · 21,588 cycles

ON FLIGHT 2934 THE CREW REPORTED THE CABIN DOOR WAS VERY HARD TO OPEN-SEEMED TO HANG UP PART WAY. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN DOOR ACTUATING AND LOCKING MECH AND OPS CHECK IAW EMB 52-18-00. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 25,253 hrs · 21,414 cycles

ON FLIGHT 3969 THE FLIGHT ATTENDANT ADVISED THE FLASHLIGHT WAS MISSING FROM THE AFT CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW FLASHLIGHT IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: YOKE — DEFECTIVE (COCKPIT) · airframe 23,710 hrs · 21,395 cycles

FOR FLIGHT 3348 THE CAPTAIN'S YOKE WAS SMOKING FROM NUT PLATE BEHIND STEERING DISCONNECT SWITCH. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S CONTROL YOKE IAW EMB AMM 27-11-08-020-001-A00 STEP J1 AND 27-11-08-420-001-A00 STEPS I1, I13, I14, AND I15. OPERATIONAL CHECKED GOOD IAW EMB AMM 27-11-08-842-001-A00 STEPS J3-J14. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 23,551 hrs · 23,551 cycles

ON FLIGHT 3394 THE CREW REPORTED THE MAIN CABIN DOOR DIFFICULT TO OPEN FROM THE INSIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED LUBRICATION OF SIDE HINGED MAIN DOOR ACTUATING AND LOCKING SYSTEM IAW AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 22,867 hrs · 20,783 cycles

DURING MAINTENANCE INSPECTION FOUND THE COCKPIT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT IAW EMB 140 AMM33-50-05. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DME — INOPERATIVE (NAV SYSTEM) · airframe 22,570 hrs · 20,544 cycles

ON FLIGHT 4452 THE CREW REPORTED THE NAV 2 VOR AND NAV 2 LOC INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NAV ADF DME UNIT IAW EMB AMM 34-32-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN DOOR) · airframe 22,271 hrs

MAIN DOOR HARD TO OPEN. OPERATED DOOR SEVERAL TIMES IAW EMB MM 52-18-00, OPS CHECK GOOD. COULD NOT DUPLICATE.

Part: ICU — INOPERATIVE (VHF COMM) · airframe 21,646 hrs · 19,789 cycles

ON FLIGHT 3286 THE DURING CRUISE THE CREW REPORTED A DUAL TRANSPONDER FAILURE AFTER DEPARTURE. THE AIRCRAFT RETURNED TO BJX. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED NR 1 INTEGRATED COMMUNICATION UNIT VHF IAW AMM 23-00-01. THE OPERATIONAL CHECK WAS GOOD IAW AMM 34-52-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 21,276 hrs · 19,488 cycles

ON FLIGHT 4521 THE CREW REPORTED A HEAVY OIL ODOR THROUGHOUT THE AIRCRAFT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER 1 ENGINE PER AE WORKCARD 71-000-00. THE LEAK AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LANDING GEAR — MALFUNCTIONED · airframe 21,255 hrs · 19,469 cycles

ON FLIGHT 4469 THE CREW REPORTED THAT AFTER TAKE OFF DURING GEAR RETRACTION THE LANDING GEAR FAILED TO RETRACT FOLLOWED BY A LANDING GEAR LEVER DISAGREE MESSAGE. THE CAPTAIN ELECTED TO DIVERT TO IAD. CRASH, FIRE AND RESCUE WERE CALLED FOR THE LANDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR IAW AMM 32-32-02. THE OPERATIONAL CHECK WAS GOOD, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,822 hrs · 19,071 cycles

ON FLIGHT 4680 THE CREW REPORTED THAT DURING ALL PHASES OF FLIGHT NOTICED AN OIL ODOR IN THE CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT PER ETN: EM-72-034R4 AND FIM 21-20-00-810-801-A AND COULD NOT DUPLICATE THE ODOR. NO DEFECTS NOTED AT THIS TIME. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,019 hrs · 16,584 cycles

DURING MAINTENANCE BASE INSPECTION THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO HAVE CORROSION AT CARBON CROSS MEMBER. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE CENTER OMEGA BEAM AT FRAME 25 AT CARBON CROSS MEMBER IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — OUT OF POSITION (WINDSHIELD) · airframe 17,312 hrs · 15,999 cycles

ON FLIGHT 3645, CREW REPORTED CAPTAIN WINDSHIELD SEAL CAME OFF DURING CLIMB OUT SUSPECT INGESTED ENG NR 1. CABIN FILLED WITH FUMES NO SMOKE , NO INDICATION OF DAMAGE. RETURNED TO DEPARTURE AND SHUTDOWN AFTER LANDING. ACFT REMOVED FROM SERVICE. PERFORMED FOD INSPECTION, PERFORMED BOROSCOPE INSP/ENG RUNS NO ODORS PRESENT AT THIS TIME. ENGINE IS SERVICEABLE IAW SRM. ACFT RETURNED TO SERVICE.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 13,760 hrs · 12,258 cycles

CREW GOT A BLEED 2 VALVE FAIL AND RETURNED TO LAX FOR MTX. THE RETURN TO LAX WAS DUE TO ICING CONDITIONS ONLY. MTX REMOVED AND REPLACED H2 BLEED TWO VALVE IAW EMB 140 AMM 36-11-05, OPS CHECKS GOOD AT THIS TIME AIRCRAFT RETURN TO SERVICE.

Part: FAN — FAILED (ZONE 100) · airframe 13,415 hrs · 11,921 cycles

ELECTRICAL BURNING ODOR, TURNED SHED BUSSES OFF ODOR DISSIPATED. REMOVED AND REPLACED RECIRCULATION FAN IAW EMB AMM - OPERATIONAL CHECK GOOD - PERFORMED FUNCTIONAL; CHECK FLIGHT WITH NO DEFECTS NOTED - AIRCRAFT RETURNED TO SERVICE

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,149 hrs · 11,710 cycles

GALLEY HAT BEAM FOUND CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,149 hrs · 11,710 cycles

SERVICE DOOR SILL FOUND CORRODED. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-06, 51-20-03 AND 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,149 hrs · 11,710 cycles

LEFT OMEGA BEAM FRAME 20 CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,149 hrs · 11,710 cycles

LEFT OMEGA BEAM FRAME 20 CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (HYD SYSTEM) · airframe 11,862 hrs · 10,733 cycles

TOTAL LOSS OF NUMBER ONE HYDRAULIC SYSTEM FLUID. REMOVED AND REPLACED NUMBER ONE SYSTEM AILERON MANIFOLD AND RIGHT GROUND SPOILER ACTUATOR. PERFORMED OPERATIONAL CHECK WITH NO DEFECTS NOTED IAW EMB AMM, RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FS 25)

THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE LEFT OMEGA BEAM TO REMOVE CORROSION. FABRICATED A FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10 FIGURE 201. (M)

Part: FLOOR SUPPORT — CORRODED (FS 25)

THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 30 CHAPTER 53-00-10 FIGURE 203. (M)

Part: FLOOR SUPPORT — CORRODED (FS 20)

ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE PREVIOUS REPAIR AND CLEANED THE AREA. FABRICATED A REPAIR PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 30, CHAPTER 53-00-10 FIG 201. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED TWO REPAIR DOUBLERS, FOUR SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2777. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF OMEGA BEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS AND PLATE. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142, REV 22, CHAPTER 53-21-10, FIG 201 SHEET 1, CPM 51-61-00 AND STANDARD SRM PRACTICES. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

ORD - FLT 4371 - DURING FLIGHT CREW REPORTED THE FIRST OFFICERS WINDSHIELD BUBBLING AND ARCING WITH ANTI-ICING TURNED ON. CREW LEFT ICING CONDITONS AND CONTINUED TO ORIGINAL DESTINATIONS WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)