N845AE

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 36,207 hrs · 33,120 cycles

AFT CABIN FLASHLIGHT INOP-C/A-DEFFERED AS PER MEL 25-53. REMOVED AND REPLACED AFT CABIN FLASHLIGHT ASSEMBLY IAW AMM-33-50-16. OPS CHECK GOOD. MEL RESTORED.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 36,049 hrs · 32,980 cycles

MAIN PAX FOOR GETS JAMMED AFTER CLOSING MAKING IT VERY DIFFICULT TO OPEN IT-C/A-LUBRICATED MAIN DOOR IAW EMB 140 AMM 52-11-00. NO FURTHER DEFECTS NOTED. OPC GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,670 hrs · 32,640 cycles

11 B/C OVERHEAD EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED OVERHEAD 11 B/C EMERGENCY LIGHT IAW AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. OPC GOOD. END.

Part: BRAKE — FAILED (NR 3) · airframe 35,514 hrs · 32,497 cycles

BRAKE DEGRADED UPON GEAR EXTENSION.-C/A-FOUND #3 BRAKE NOT OPERTING PROPERLY AND NO INDICATION OF TEMP ON EICAS REMOVED AND REPLACED #3 MAIN BRAKE ASSY IAW W/C 32-600-14, OPS CHECK GOOD. REMOVED AND R EPLACED #3 MAIN BRAKE TEMP SENSOR IAW AMM 32-47-01 OPS CHECK GOOD. BRAKE TEMPERATURE SENSOR P/M 0132AFU-1 S/N D8645

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 35,127 hrs · 32,137 cycles

LANDING GEAR AIR/GROUND FAIL. CMC FAULT CODE 32-LGM14. PERFORMED GVI OF ALL AIR/GROUND PROXIMITY SWITCHES AND AIR/GROUND OPS CHECK IAW AMM 32-63-00-700-801-A. OPS CHECKED GOOD. NO DISCREPANCIES NOTED.

Part: MUFFLER — ODOR (NR 1 A/C PACK) · airframe 35,110 hrs · 32,117 cycles

ON LANDING MUSTY SOCK SMELL IN COCKPIT. TURNED PACKS OFF ON GROUND AND SMELL WENT AWAY. REMOVED AND REPLACED #1 PACK RECIRC SYSTEM MUFFLER IAW AMM 21-24-02 OPC GOOD IAW AMM 21-20-00 MEL ITEM RESTORED

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 34,133 hrs · 31,205 cycles

SUPLEMENTAL WE WERE CLIMBING THROUGH FL180, WHEN WE PERFORMED ANTI-ICE/PNEUMATIC TEST WE NOTICED CAB ALT WENT VERY RAPIDLY TO AMBER AROUND 6,000FT CAB/ALT AT THAT POINT WE STARTED THE EMERGENCY DESCENT AND DECLARE EMERGENCY, CABIN ALT WENT TO 11,8000FT WITH CABIN WARNING "RED" IN EICAS WHILE DESCENDING. C/A-DEFERRED AS PER MEL 21-19. AUTH# 010446DM-C M-PROCEDURES C/W. PERFORMED OPC OF PRESSURIZATION CONTROL SYS. IAW AMM 21-31-00-700-801-A & 21-31-00-700-801-A. OPC GOOD. NO DEFECTS NOTED. MEL RESTORED.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 33,317 hrs · 30,502 cycles

SERVICE DOOR CEILING EMERGENCY LIGHT AND FWD BULKHEAD EXIT LOCATOR LIGHT INOPERATIVE. SECURED THE CONNECTOR P8525 ON SERVICE DOOR CEILING PANEL IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 32,827 hrs · 30,081 cycles

DURING CLIMB, RECEIVED A SPOILER FAIL MESSAGE. COMPLIED WITH QRH, DECLARED AN EMERGENCY AND CONTINUED TO DESTINATION. PERFORMED FIM 27-63-00. FOUND TO BE TRANSITORY CONDITION. OPS CHECKED SPOILERS IAW AMM 27-63-01. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: PITOT TUBE — DAMAGED (CAPTAIN'S SIDE) · airframe 32,666 hrs · 29,926 cycles

DURING CLIMB, IAS COMPARITOR FOLLOWED BY ALT COMPARITOR AND SPS ADVANCE. NRWC 845-DFW-02603 FOUND CO-PILOT`S STATIC TUBE DAMAGED UNDER COCKPIT FLOOR RIGHT SIDE. REPAIRED PITOT TUBE IAW AMM 20-10-03, AND PERFORMED A PITOT-STATIC LEAK CHECK AND OPERATIONAL CHECKED IAW IAW AMM 34-13-00.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT CARGO) · airframe 32,617 hrs · 29,876 cycles

CARGO SMOKE EICAS WITH LIGHT BUTTON, NO SMOKE OR FIRE DETECTABLE IN CABIN. RESET POWER IAW AMM 24-42-00. PERFORMED FIRE DETECTION SYSTEM OPS CHECK IAW AMM 26-10-00. OPS CHECKED. GOOD. REMOVED AND REPLACED THE AFT CARGO SMOKE DETECTORS IAW AMM 26-15-01. OPS CHECKED GOOD IAW AMM 26-15-00.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 32,611 hrs · 29,873 cycles

FWD SHEAR TIE AT FRAME 65 CORRODED. THE SHEAR TIE WAS REPAIRED IAW SRM 53-31-04.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 32,611 hrs · 29,873 cycles

IN BAGGAGE COMPARTMENT; AFT SMOKE DETECTOR MAINTENANCE LED FAILED TO COME ON DURING TEST.-C/A-BAGGAGE COMPARTMENT SMOKE DETECTOR REPLACED IAW AMM 26-15-01. / BAGGAGE COMPARTMENT SMOKE DETECTION SYSTEM OPERATIONAL TEST DONE IAW AMM 26-15-00. NO FAULT FOUND.

Part: STRAP — CRACKED (BODY FAIRING) · airframe 32,611 hrs · 29,873 cycles

LT BODY TO BODY FAIRING STRAP CRACKED 6 INCH AFT OF FR 49. -C/A- LT WING TO BODY FAIRING STRAP 6 INCH AFT OF FR 49 REPAIRED IAW SRM 53-23-12 TYPE II. AFTER INVESTIGATION EXISTING DRILL RUN FOUND UNDER REPAIR STRAP, SKIN REPAIRED IAW SRM 53-23-01, TABLE 108 WITH PLUG RIVETS.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 32,611 hrs · 29,873 cycles

CF2, LT GUSSET NR 2 CORRODED -C/A-CF2, LT GUSSET NR 2 CORROSION BLENDED IAW SRM 51-10-03 & FOUND TO BE OUT OF LIMIT IAW SRM 53-22-10 MAT'L THICKNESS = .050" MAT'L LOSS = .045" REMAINING MAT'L .005" & LESS CF2 LT GUSSET NR 2 REPLACED IAW SRM 51-40-02 SEAT TRACK REINSTALLED IAW AMM 53-01-06-400-8001-A SEAT TRACK REMOVED TO GAIN ACCESS IAW AMM 53-01-06.

Part: THERMOSTAT — FAILED (RIGHT) · airframe 32,526 hrs · 29,770 cycles

"BLEED 2 OVERTEMP" IN FLIGHT, REMOVED AND REPLACED NR 2 FAN AIR CONTROL THERMOSTAT IAW AMM 36-11-06, OPS CHECK GOOD. THERMOSTAT FAN AIR CONTROL, ENGINE P/N 816624-13 S/N 9911083

Part: LIGHT — INOPERATIVE (EXTERNAL) · airframe 32,354 hrs · 29,615 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT PANEL ASSEMBLY IAW AMM 25-23-04.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,354 hrs · 29,615 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. IPC 33-50-10-25 FOR LOCATION. R & R MAIN-DOOR EMERGENCY LIGHT PANEL ASSY IAW AMM 25-23-04, FOR OPS CHECK.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 31,620 hrs · 28,836 cycles

FIRST OFFICER EMER FLASHLIGHT CRADLE IS BROKEN. R & R FIRST OFFICERS EMER FLASHLIGHT CRADLE. CHECKED OK IAW AMM 33-50-16.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 30,787 hrs · 27,904 cycles

FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. R & R FLIGHT ATTENDANT FLASHLIGHT & CRADLE ASSEMBLY. OPERATIONS CHECKED GOOD IAW AMM 33-50-16. MEL ITEM RESTORED.

Part: MUFFLER — DISCONNECTED (RECIRC SYS) · airframe 30,712 hrs · 27,829 cycles

PASSENGER AT 9A REPORTED SMOKE & STEAM WITH BURNING SMELL NEXT TO SEAT. TURNED ON NR 1 PACK & OBSERVED CONDENSATION COMING FROM UNDER SEAT 9A. FOUND NR 1 RECIRCULATION SYS MUFFLER DISCONNECTED. SECURED MUFFLER IAW MM 21-24-02, NO BURNING SMELL, SMOKE OR STEAM OBSERVED AFTER TURNING ON NR 1 PACK. OPERATIONS CHECKED GOOD.

Part: ACM — SEIZED (NR 2) · airframe 30,376 hrs · 27,477 cycles

ODOR OF SMOKE IN THE COCKPIT AFTER TAKEOFF. EMERGENCY LANDING. FOUND NR 2 ACM SEIZED. R & R NR 2 ACM IAW AMM 21-51-03. OPS CHECKED GOOD IAW AMM 21-51-00-700-802-A. NO SMELL OF SMOKE NOTED IN COCKPIT OR CABIN. NO NR 2 PACK OVERHEAT MESSAGES NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,419 hrs · 26,556 cycles

NUMBER 1 BLEED VLV FAIL ON EICAS IN ICING CONDITIONS WITH THRUST LEVERS IN DETENT. TROUBLE SHOT IAW FIM 36-11-00. PERFORMED OPERATIONAL CHECK OF ICING SYS IAW 30-10-00 & 30-80-00, & 36-11-05. ACFT OK FOR SERVICE AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 28,812 hrs · 26,071 cycles

BLD 1 VLV FAIL AT 2200 FT IN ICING CONDITION. PERFORMED LT ENG BLD VLV OPERATIONAL CHECK IAW AMM 36-11-05-700-802-A. OPERATIONAL CHECKED GOOD.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 28,762 hrs · 26,028 cycles

CLIMBING FROM FL 300 TO FL 330, ACFT CABIN DELTA P JUMPED TO 8.0 PSI EXCEEDING AUTO MODE NORMAL MAXIMUM DIFFERENTIAL PRESSURE. DELTA P 8.0 PSI UNTIL DESCENT & DIVERT WHILE OPERATING IN NORMAL AUTO MODE CABIN DIFFERENTIAL PRESSURE EXCEEDED DELTA LIMIT 7.8 PSI & INDICATED 8.0 PSI CABIN DIFFERENTIAL PRESSURE. REMOVED AND REPLACED ELECTROPNEUMATIC OUTFLOW VALVE IAW AMM 21-31-03. OUTFLOW VALVES PASSED IAW AMM 21-31-00-700-804A AND AUTO MODE PASSED IAW AMM 21-31-00-700-802A.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 28,656 hrs · 25,944 cycles

CAPTAIN`S SIDE FLASHLIGHT BUTTON BROKE. R & R CAPTAIN`S SIDE FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (FLASHLIGHT) · airframe 28,502 hrs · 25,808 cycles

CAPTAIN'S FLASHLIGHT CHARGER INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD NO FURTHER DEFECTS NOTED MEL RESTORED.

Part: WIRE — DAMAGED (CABIN) · airframe 28,253 hrs · 25,576 cycles

EMERGENCY LIGHTING SYS FLOOR PROXIMITY STRIP INOPERATIVE, BROKEN WIRE LT AFT CABIN. DEFERRED IAW MEL 33-30. REPAIRED WIRE IAW SWPM 20-21-00 + 33-50-12. OPERATIONS CHECKED GOOD IAW MM 33-50-00. MEL ITEM RESTORED.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 28,111 hrs · 25,443 cycles

RIGHT OVERWING EMER LIGHT INOPERATIVE. R & R OVERWING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,110 hrs · 25,442 cycles

RIGHT CABIN FRAME NR 23 AT STRINGER 15 IS CRACKED. REPAIRED RT CABIN FRAME NR 23 IAW EO EM-53MR-1808.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,110 hrs · 25,442 cycles

RIGHT CABIN FRAME NR 23, AT STRINGER 15 IS CRACKED. REPAIRED IAW EO EM-53MR-1808.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 28,110 hrs · 25,442 cycles

LEFT OMEGA BEAM SUPPORT, OTBD FLANGE IS CRACKED BETWEEN FRAMES 47 - 48. R & R IAW SRM 53-23-01 & 51-40-02. CHANNEL PN 140-04213-611, SHEAR CLIP PN 140-04214-605 & 140-04214-611.

Part: DOOR SEAL — CORRODED (FUSELAGE) · airframe 28,110 hrs · 25,442 cycles

CARGO DOOR SILL HAS EVIDENCE OF CORROSION. REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,110 hrs · 25,442 cycles

RIGHT OTBD FLOOR SUPPORT BETWEEN FRAMES 35 - 50 IS CORRODED. REPAIRED IAW SRM 53-23-10.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 28,110 hrs · 25,442 cycles

STRINGER 21L BETWEEN FRAMES 12 & 13 IS PITTED BEYOND LIMITS NEXT TO SEVERAL RIVETS THAT GO THROUGH THE SKIN. REPAIRED IAW SRM CH 53-00-03.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 28,110 hrs · 25,442 cycles

CROSSBEAM AT FRAME NR 20 IS CORRODED. REPAIRED IAW ETN-EM-53-241.

Part: RIB — CRACKED (RUDDER) · airframe 28,110 hrs · 25,442 cycles

FORWARD RIB BY UPPER MIDDLE HINGE POINT ON RUDDER 1 HAS A 1/8 INCH CRACK. R & R IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,110 hrs · 25,442 cycles

RIGHT OTBD FLOOR SUPPORT BETWEEN FRAMES 52 - 53 IS CORRODED. REPAIRED RT OTBD FLOOR SUPPORT BETWEEN FRAMES 52 - 53 IAW SRM 53-23-10.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,110 hrs · 25,442 cycles

LEFT FWD EMER LIGHT STRIP DAMAGED. REPLACED LT FWD EMER LIGHT STRIP. REFERENCE BOW 160084 FOR INSTALLATION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,110 hrs · 25,442 cycles

RIGHT OTBD FLOOR SUPPORT BETWEEN FRAMES 25 - 35 CORRODED. REPAIRED IAW SRM 53-22-10.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 27,360 hrs · 24,749 cycles

AFT FLASHLIGHT HOLDER BROKEN. R & R AFT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 27,325 hrs · 24,725 cycles

FLIGHT ATTENDANT AFT EMERGENCY FLASHLIGHT MISSING. INSTALLED NEW EMERGENCY FLASHLIGHT AFT CABIN IAW AMM 25-60-00.

Part: HOLDER — WORN (FLASHLIGHT) · airframe 27,198 hrs · 24,597 cycles

REAR FLASHLIGHT HOLDER WORN. R & R REAR FLASHLIGHT HOLDER ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: HOLDER — LOOSE (FLASHLIGHT) · airframe 27,198 hrs · 24,597 cycles

REAR FLASHLIGHT HOLDER LOOSE. SECURED REAR FLASHLIGHT IAW STANDARD MX PRACTICES.

Part: DRAIN — CONTAMINATED (PITOT STATIC) · airframe 26,693 hrs · 24,161 cycles

CLIMBING THROUGH 3000 FT, ALTIMETERS WERE OFF BY APRROX 700 FT, AND INCREASING ALTITUDE WAS OFF BY 1200 FT, DURING RETURN FOR LANDING. DURING APPROACH GPWS STARTED GOING OFF PULL UP TERRAIN ETC. INCREASED LANDING TOUCH DOWN SPEED AS PRECAUTION. DRAINED WATER FROM DRAINS PERFORMED LEAKAGE TEST IAW AMM 34-13-00 IS GOOD. GPWS OP CHECKS GOOD IAW AMM 34-43-00. ACFT IS RVSM ELIGIBLE. ACFT IS COMPLIANT FOR CAT II OPERATIONS.

Part: ENGINE — SMOKE (RIGHT) · airframe 25,780 hrs · 23,419 cycles

CREW RECEIVED A "LAV SMOKE" EICAS MESSAGE. F/A REPORTED SMOKE IN THE CABIN AND A WARNING AND HORN ON THE FIRE PANEL IN THE GALLEY. F/A REPORTED THE REAR OF CABIN FILLED WITH SMOKE. DECLARED AN EMERGENCY AND RAN THE AOM VOL 1 CHECKLIST. DIVERTED AND LANDED WITHOUT INCIDENT. ON ARRIVAL, FOUND NO EVIDENCE OF FIRE/SMOKE OUTSIDE OR INSIDE ACFT. ACFT REMOVED FROM SERVICE. R & R RIGHT HAD ENGINE IAW 72-000-00. THE OPS AND LEAK CHECKED NORMAL. COMPLIED WITH ENGINE ODOR EVENT TROUBLESHOOTING IAW ETN EM-72-034. OPS CHECKED GOOD. NO FINDINGS AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — OVERHEATED (FLASHLIGHT) · airframe 25,727 hrs · 23,374 cycles

DURING MX INSPECTION FOUND F/O EMERGENCY FLASHLIGHT CRADLE SHOWS EVIDENCE OF OVERHEATING. ACFT REMOVED FROM SERVICE. R & R F/O FLASHLIGHT CRADLE IAW W/C33-700-20. AMM 33-51-01. ACFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 25,642 hrs · 23,304 cycles

THE CREW REPORTED THE REAR FLASHLIGHT CRADLE WAS BROKEN. FLASHLIGHT WOULD NOT REMAIN IN CRADLE. ACFT REMOVED FROM SERVICE. R & R REAR FLASHLIGHT CRADLE IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 25,181 hrs · 22,909 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — DIRTY (CABIN) · airframe 24,671 hrs · 22,472 cycles

ON FLIGHT 3928 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR WAS VERY DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED DOOR IAW EMB 140 AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,521 hrs · 22,332 cycles

ON FLIGHT 4029 THE FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHT AT 16A WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW EMB 140 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,363 hrs · 22,187 cycles

DURING PS-1 CHECK FOUND THE NR 1 CEILING EMERGENCY LIGHT BULB INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AISLE EMERGENCY LIGHT IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

RIGHT AFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 4 EPSU BATTERY AND CHARGER ASSEMBLY.

Part: FLAP — MALFUNCTIONED (WING) · airframe 24,142 hrs · 21,973 cycles

ON FLIGHT 3567 THE CREW REPORTED THAT AFTER LANDING THE FLAPS WOULD NOT RETRACT STUCK IN FLAP 22 WITH FLAP FAIL ON EICAS. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED FLAPS AND AREA.RESET FLAP SYSTEM. THE OPERATIONAL CHECK WAS GOOD IAW AMM 27-51-00. FOUND TO BE INTRANSITORY CONDITION. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 23,469 hrs · 21,354 cycles

DURING B INSPECTION, FOUND THE RIGHT BEAM GUSSET TO HAVE CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT BEAM GUSSET IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CORRODED (LAVATORY) · corrosion level 2 · airframe 23,456 hrs · 21,340 cycles

LAVATORY RT BEAM HAS CORROSION AT FWD AND AFT NUT PLATE. ACCOMPLISHED EO-EM-53MR-2015 REPAIR OF LAV RT BEAM AT FWD AND AFT NUT PLATE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 23,469 hrs · 23,469 cycles

DURING B INSPECTION, FOUND THE RIGHT AFT BEAM DIAMOND GUSSET TO HAVE CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT AFT BEAM DIAMOND GUSSET IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 23,469 hrs · 23,469 cycles

DURING B INSPECTION, FOUND THE LAV CENTER BEAM GUSSET TO HAVE CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAV CENTER BEAM GUSSET IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 23,469 hrs · 21,354 cycles

DURING B INSPECTION, FOUND THE SERVICE DOOR ENTRANCE FORWARD SILL TO HAVE CORROSION. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SILL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUELAGE) · airframe 23,469 hrs · 21,354 cycles

DURING B INSPECTION FOUND THE LAV LEFT BEAM GUSSET TO HAVE CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAV LEFT BEAM GUSSET IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,469 hrs · 21,354 cycles

DURING MAINTENANCE INSPECTION, FOUND THE MAIN ENTRANCE CEILING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,456 hrs · 21,340 cycles

DURING MAINTENANCE INSEPCTION, FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGECNY LIGHT BATTERY POWER SUPPLY IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 23,469 hrs · 21,354 cycles

DURING B INSPECTION, FOUND GALLEY FRAME 18 LEFT CROSSBEAM TO HAVE CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-09. AIRCRAFT RETURNED TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 23,469 hrs · 23,469 cycles

DURING B INSPECTION, FOUND GALLEY FRAME 20 CROSSBEAM TO HAVE CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-09. AIRCRAFT RETURNED TO SERVICE.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 23,022 hrs · 20,973 cycles

FLIGHT 4427, CREW REPORTED A STRONG ACRID ODOR IN THE CABIN DURING DESCENT. AIRCRAFT LANDED WITHOUT INCIDENT AND REMOVED FROM SERVICE. FOUND OIL LEAKING OUT OF AIR TURBINE STARTER FROM NR 1 ENGINE. REMOVED AND REPLACED THE MAGNETIC CARBON SEAL FROM ACCESSORY DRIVER GEARBOX IAW ROLL ROYCE MM 72-63-10. REPLACED RELEVANT O-RINGS OF SEAL AND STARTER. PERFORMED IDLE ENGINE RUN IAW GHC AND PERFORMED ETN: EM72034R4 FOR ODOR TROUBLESHOOTING. NO ODORS NOTED AT IDLE RUN. PERFORMED HIGH-SPEED ENGINE RUN IAW ETN: NO ENGINE ODOR NOTED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — MISINSTALLED (PAX DOOR) · airframe 22,955 hrs · 20,907 cycles

FLIGHT 4450, CREW REPORTED THEY WERE UNABLE TO OPEN THE MAIN CABIN DOOR FROM INSIDE THE CABIN. USED EXTERNAL HANDLE TO OPEN DOOR. AIRCRAFT REMOVED FROM SERVICE. CORRECTLY INSTALLED MAIN DOOR INTERIOR OPERATING HANDLE IAW AMM 52-18-05, MAIN DOOR FUNCTIONAL CHECKED GOOD. NO FURTHER DEFECT NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: HOLDER — BROKEN (CABIN) · airframe 22,745 hrs · 20,704 cycles

DURING B-INSPECTION FOUND THE FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT CABIN FLASHLIGHT HOLDER IAW EMB 140 AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DAMAGED (COCKPIT) · airframe 22,304 hrs · 20,259 cycles

ON FLIGHT 3070 THE CREW FOUND THE CAPTAIN’S FLASHLIGHT HOLDER DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAIN'S FLASHLIGHT ASSY IAW ERJ 140 AMM CHAPTER 33-50-16 OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,534 hrs · 19,683 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE AISLE CEILING EMERGENCY LIGHT AT ROW 16 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERHEAD AISLE EMERGENCY LAMP AT ROW 16 IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 21,456 hrs · 19,613 cycles

FOR FLIGHT 4167 THE CREW REPORTED THE AFT EMERGENCY FLASHLIGHT SWITCH WORKS INTERMITTENTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT AS REQUIRED IAW AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CORRODED (RT ENGINE) · corrosion level 2 · airframe 18,493 hrs · 16,801 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT ENGINE FRONT FRAME BOLT HOLES HAVE CORROSION. REMOVED CORROSION DEFERRED AND PERMANENT REPAIR REQUIRED AT OR BEFORE 200 FLIGHT HOURS IAW PART B OF EO EM-72MR-115. REMOVED AND REPLACED THE NR 2 ENGINE. THE OPERATIONAL CHECKS WERE GOOD NO LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 17,939 hrs · 16,391 cycles

ON FLIGHT 3059 AFTER TAKEOFF THE CREW REPORTED A "LANDING AIR / GROUND FAIL" MESSAGE ON EICAS. THE CREW PERFORMED AIRCRAFT OPERATING MANUAL PROCEDURES AND ALL INDICATIONS WERE GOOD FOR A LANDING. THE CREW DECLARED AN EMERGENCY. CRASH, FIRE, AND RESCUE WERE CALLED OUT AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED CLEARANCE GAP ON RIGHT NR 2 PROXIMITY SWITCH IAW EMB 140 AMM 32-63-05. PERFORMED FUNCTIONAL CHECK OF PROXIMITY SWITCHES IAW EMB 140 AMM 32-63-05. THE OPERATIONAL CHECKS WERE GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — LEAKING (NR 2 ENGINE) · airframe 16,918 hrs · 14,858 cycles

ON FLIGHT 3064 RIGHT AFTER TAKEOFF THE CREW REPORTED, RECEIVED A LAV SMOKE INDICATION MESSAGE ON EICAS. THE FLIGHT ATTENDANT REPORTED, SMELLED A STRANGE ODOR IN THE CABIN. THE CREW DECLARED AN EMERGENCY. THE FLIGHT DECK CREW DONNED OXYGEN MASK AND RETURNED TO SAN. NO SMOKE WAS VISIBLE ANYWHERE IN COCKPIT, LAV OR CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT. CRASH AND FIRE RESCUE CREW CAME IN AND COULD NOT FIND ANY HOT SPOTS OR ANYTHING THAT HAD SIGNS OF SMOKE OR ODOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE NUMBER 2. FOUND EVIDENCE OF THE NUMBER 4 CARBON SEAL LEAKING. REMOVED AND REPLACED THE NUMBER 4 CARBON SEAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 16,728 hrs · 14,540 cycles

DURING A PHASE INSPECTION AN EMERGENCY LIGHT LOCATED ON THE CEILING AT ROW 3 FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND THAT THE EMERGENCY LAMP ON THE CEILING AT ROW 3 WAS NOT SECURE IN THE SOCKET. THE LAMP WAS SECURED AND THE OPERATIONAL TEST WAS GOOD. NO PARTS WERE REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ECU — FAILED (TE FLAP) · airframe 16,554 hrs · 14,268 cycles

DURING FLIGHT 3115 THE CREW REPORTED, RECEIVED A STALL PROTECTION COMPUTER ADVANCE WARNING AND AN AMBER BOX WARNING FLAP INDICATION. THE CREW WAS UNABLE TO VERIFY FLAP INDICATION. THE CREW DECLARED AN EMERGENCY AND LANDED WITH NO INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. PERFORMED OPERATIONAL CHECK IAW EMB AMM 27-53-00. OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 14,573 hrs · 11,885 cycles

CREW REPORTED ON FLIGHT 4247 EMERGENCY LIGHT AT MAIN CABIN DOOR INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY AS PER EMB AMM 33-50-04 OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 11,137 hrs · 9,261 cycles

RUBBER BURNING ODOR COMING FROM GALLEY, HOT JUG SYSTEM TURNED OFF. FOUND BURNT WIRES IN HOT JUG SYSTEM MEL ISSUED. AIRCRAFT RETURNED TO SERVICE.

Part: DUCT — CRACKED (NR 1 ENGINE) · airframe 10,322 hrs · 8,617 cycles

NUMBER ONE ENGINE ANTI-ICE VALVE FAIL MESSAGE, RETURNED TO ORD. REMOVED AND REPLACED ANTI-ICING DUCT IAW EMB AMM 30-21-25. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: DUCT — DISCONNECTED (CABIN AIR) · airframe 10,404 hrs · 8,667 cycles

CABIN WOULD NOT COOL AND SMOKE REPORTED IN CABIN. RESECURED DUCT UNDER FLOOR IAW EMB AMM. PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: ANTI-ICE VALVE — FAILED (NR 1 ENGINE) · airframe 10,308 hrs · 8,608 cycles

ENGINE ONE ANTI-ICE MESSAGE, ATC DIVERSION, EMERGENCY DECLARED FOR LOW FUEL. REMOVED AND REPLACED ENGINE ONE ANTI-ICE VALVE IAW EMB AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DRIVE UNIT — INOPERATIVE (TE FLAPS)

DURING LANDING, CREW DECLARED AN EMERGENCY DUE TO FLAP FAIL. FLAPS WERE AT 9 DEGREES AND NO INDICATION WAS SEEN IN COCKPIT. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT FOR FLAPS. OPERATIONAL CHECK WAS GOOD IAW MM AND AIRCRAFT WAS RETURNED TO SERVICE. (SW212004046965)