N838AE

Part: FLASHLIGHT — UNSECURE (AFT CABIN) · airframe 37,078 hrs · 32,769 cycles

MEL 25-53 AUTH# 121051-C AFT FA FLASHLIGHT INOPREF LOG PAGE 4550081 ITEM 1 .-C/A-RESEATED FLASH LIGHT IN HOLDER AND LET CHARGE ALL NIGHT. OPC GOOD. MEL 25-53 RESTORED.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 37,074 hrs · 32,763 cycles

AFT FA FLASHLIGHT INOP-C/A-FLIGHT CREW PLACARDED AFT FA FLASHLIGHTAUTH 121051-CREF 25-53 MOC 696266. RESEATED FLASH LIGHT IN HOLDER AND LET CHARGE ALL NIGHT. OPC GOOD. MEL 25-53 RESTORED.

Part: THERMOSTAT — FAILED · airframe 36,981 hrs · 32,663 cycles

BLEED 1-2 VLV OVR TEMP IN FLIGHT WHILE IN ICING CONDITIONS DECLARED EMERGENCY AND AIR RETURN "TRANSFERRED TO NRWC 838-SGF-03378"-C/A-RAR LH AND RH FAN AIR CONTROL THERMOSTATS SEE NRWC 838-SGF-03378 FOR CORRECTIVE ACTION

Part: HANDSET — ODOR (FWD GALLEY) · airframe 36,880 hrs · 32,574 cycles

UPON LANDING FA REPORTED A BURNING SMELL IN GALLEY AREA-C/A-PERFORMED FIM TASK 21-20-00-810-801-A- FOUND FWD FA HAND MIC TO HAVE AN ELECTRICAL BURNT SMELL.CHECKED GENERAL CONDITION OF PLUG NO DEFECTS NOTED REMOVED AND REPLACED FWD FA HAND MIC IAW AMM 23-31-03. OPS CHECK GOOD.

Part: FLASHLIGHT — UNKNOWN (CABIN) · airframe 36,874 hrs · 32,569 cycles

AFT FA FLASH LIGHT INOP-C/A-FLT CREW PLACARD AFT FA FLASH LIGHT IAW MEL 2553 AUTH # 110372-C MOC # 624980. OPS CHECKED AFT FA FLASHLIGHT. OPS CHECKED GOOD. IAW CMM 25-60-14 MEL RESTORED

Part: WIRE — DAMAGED (CABIN) · airframe 36,601 hrs · 32,312 cycles

FLOOR PROXIMITY LIGHT STRIP LAST IN AISLE IS INOP-C/A-REPAIRED THE WIRING TO THE FLOOR PROXIMITY LIGHT STRIP LAST IN AISLE IAW EMB SWPM 20-20-00 OPS CHECK GOOD

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 36,366 hrs · 32,094 cycles

AIRCRAFT FAILED TO PRESSURIZE ABOVE 900 FT AT 13,000 FT. PERFORMED PRESSURIZATION CONTROL OPS TEST IN BOTH MANUAL & AUTOMATIC MODE IAW AMM 21-31-00. PERFORMED GROUND CONNECTION VALVE ADJUSTMENT TEST IAW AMM 21-22-04. OPS CHECK GOOD.NO OTHER DEFECTS NOTED.

Part: SKIN — DENTED (PAX DOOR) · airframe 36,350 hrs · 32,072 cycles

DENT FOUND ON LOWER EDGE OF PASSENGER DOOR. PERFORMED PERMANENT REPAIR IAW ERS-EM-52MR-1016 PART A

Part: STRUCTURE — DENTED (PAX DOOR) · airframe 36,334 hrs · 32,054 cycles

PERFORM PERMANENT REPAIR OF PAX DOOR DENT IAW ERS-EM-52DF-1006 PTD. MAJOR REPAIR. REPAIRED PAX DOOR IAW ERS-EM-52DF-1006R2 PART D AND ERS-EM- 52MR-1016. SEE NRWC 838-ABI-03210 FOR DETAILS TDMI 838T5263 IS RESTORED

Part: BATTERY — OVERHEATED (MASTER) · airframe 36,319 hrs · 32,040 cycles

BATT 2 OVTEMP ON SHORT FINAL APPROACH TURNED PER EPC OFF BAT 2, THEN RECIEVED PROPER EICAS BATT 2 OFF BUS. PRIOR TO POWERING DOWN A GATE, SAW BATT 2 TEMP OF 104, IT WAS 80 AFTER TAXIED OFF RUNWAY. FIRE DEPT CALLED AND DISCONNECTED BOTH MAIN BATTERIES. REMOVED AND REPLACED BATT #2 IAW AMM 24-36-01. OPS CHECK GOOD. BATTERY TEMP NORMAL. REMOVED AND REPLACED BATT #1 IAW AMM 24-36-01. OPS CHECK GOOD. BATTERY TEMP NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,786 hrs · 31,542 cycles

MOST AFT EMERGENCY LIGHT STRIP INOP. C/A-REMOVED AND REPLACED AFT FLOOR PROXIMITY LIGHT IAW AMM 33-50-12. OPC IS GOOD.

Part: A/C PACK — SMOKE (RIGHT) · airframe 35,546 hrs · 31,308 cycles

SMOKE IN CABIN REAR TO MIDDLE STRONG BURNING SMELL-C/A-FOLLOWED FIM TASK 21-20-00-810-801A FOUND RH ACM SEIZED RAR ACM #2 IAW AMM 21-51-03 PERFORMED GENERAL INSPECTION OF COOLING PACK SYS IAW AMM 21-51-00 OPS CHECK GOOD. NO SMELL NOTED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,325 hrs · 31,113 cycles

EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT 7A AND 8A INOP. C/A-DEFERRED EMERGENCY FLOOR PROXIMITY LIGHT AS PER MEL 33-30. REMOVED AND REPLACED EMERGENCY FLOOR PROX LIGHT IAW AMM 33-50-12. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. MEL RESTORED

Part: UNKNOWN — ODOR · airframe 35,120 hrs · 30,936 cycles

OILY SMELL FROM PACKS WHEN TO THRUST IS APPLIED. GOES AWAY AFTER A FEW MIN "TRANSFERRED TO NRWC 838-DFW-02889". C/A- PERFORMED ETN-EM-72-034. RUNS CHECKED GOOD. NO ODORS DETECTED. PER FIM 72-00-00-810-814, REMOVED AND REPLACED LT ENGINE FUEL NOZZLES 3,4,5,6,13 AND 14 IAW RRMM 73-11-10. .

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 34,733 hrs · 30,588 cycles

AUTOMATIC PRESSURIZATION SYSTEM FAILED AS WE BEGAN OUR CLIMB.-C/A-RAR CABIN PRESS. CONTROL SYSTEM DIGITAL CONTROLLER IAW AMM 21-31-01. PERFORMED PRESS. CONTROL SYSTEM FUNCTIONAL TEST IN AUTO MODE IAW AMM 21-31-00. OPERATIONAL CHECK GOOD NO FURTHER DEFECTS NOTED.

Part: DAU — FAILED (COCKPIT) · airframe 34,288 hrs · 30,162 cycles

DAU NR 2 FAILED. PERFORMED FIM TASK 31-40-00-810-809-A. FOUND TO BE TRANSITORT CONDITION OF THE IC-60 COMPUTER. OPS CHECK OF IC-600 GOOD REF AMM 31-42-00. AIRCRAFT OK FOR CONTINUED SERVICE. REMOVED AND REPLACED NR 2 DAU IAW AMM 31-41-01. OPS CHECK GOOD AIRCRAFT OK FOR SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 33,483 hrs · 29,411 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,483 hrs · 29,411 cycles

IN RFI AT FR 65, FRAME Z PN 145-25672-203 FOUND CORRODED AROUND ANCHOR NUT HOLES. IN RFI AT Z FR65 ON LT SIDE CORROSION BLENDED IAW SRM 51-10-03. AFTER FURTHER INVESTIGATION, Z FR 65 WAS FOUND TO BE OUT OF LIMITS AND REMOVED FOR REPLACEMENT IAW SRM 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 33,483 hrs · 29,411 cycles

CF2 FLOOR STRUCTURE RT GUSSET 1 BTW FR24 & FR31 CORRODED. CF2 FLOOR STRUCTURE RT GUSSET 1 BTW FR24 & FR31 CORRODED OUT OF LIMITS, REPLACED IAW SRM 51-40-02.

Part: RELIEF VALVE — FAILED (BRAKE SYSTEM) · airframe 33,483 hrs · 29,411 cycles

FNC OF THE EMERGENCY PARKING BRAKE SYS THERMAL RELIEF VALVE FAILED TEST. EMERGENCY PARKING BRAKE SYSTEM THERMAL RELIEF VALVE REPLACED IAW AMM 32-44-06.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 33,483 hrs · 29,411 cycles

CF2 FLOOR STRUCTURE LT SILL NR 3 BTW FR31 & FR35 CORRODED. CF2 FLOOR STRUCTURE LT SILL NR 3 OUT OF LIMITS AND REMOVED PER SRM 53-22-10 AND 51-40-20 AND INSTALLED A NEW PART WITH SOLID RIVET.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 33,483 hrs · 29,411 cycles

LT SILL NUMBER 5 CORRODED AT SEVERAL PLACES. LT SILL NUMBER 5 BLENDED IAW SRM 51-10-03 AND FOUND OUT OF LIMIT IAW SRM 5323-10 LT SILL NUMBER 5 REMOVED FOR REPLACEMENT IAW SRM 51-40-02. LT SILL NUMBER 5 INSTALLED IAW SRM 51-40-02.

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 33,439 hrs · 29,363 cycles

WHILE PERFORMING PS-1 INSPECTION FOUND EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY HOLDER ASSY AND CHARGER ASSY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: B-NUT — LEAKING (APU FUEL) · airframe 32,659 hrs · 28,561 cycles

WITH APU BLEED OPEN, GET A SRONG ODOR OF FUEL, POST FLIGHT INSPECTION REVEALS FUEL LEAKING FROM UNDER APU AREA. FOUND LOOSE B-NUT ON APU FUEL CONTROL INLET, ADJUSTED & OPS CHECK IAW AMM 49-31-01, FOUND SYS WORKING PROPERLY. OPERATIONS CHECKED, OPERATIONS CHECK APU BLEED SYS IAW AMM 21-00-00 SATISFACTORY.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 32,537 hrs · 28,463 cycles

IN CRUISE FLIGHT AT 320 THE BAGGAGE SMOKE WARNING MSG APPEARED MOMENTARILY & THE BAGGAGE EXTINGUISHER LIGHT ILLUMINATED & STAYED ON REST OF FLIGHT. PERFORMED SEVERAL TEST OF BAGGAGE SMOKE DETECTION SYS IAW AMM 26-15-00. OPERATIONS CHECKED GOOD. PERFORMED A GVI OF BOTH BAGGAGE SMOKE DETECTORS. NO DEFECTS NOTED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,130 hrs · 27,995 cycles

SECOND & THIRD EMER FLOOR STRIP LIGHTING INOPERATIVE. R & R NR 3 EMER LIGHT INVERTER IAW 33-50-11. OPERATIONS CHECKED GOOD.

Part: SWITCH — DIRTY (CARGO DOOR) · airframe 31,396 hrs · 27,179 cycles

ANTI-ICE LGA ACCT MX & BAGGAGE DOOR, OPEN INDICATION RIGHT AFTER TAKEOFF FLIGHT CONTINUED. CLEAN BOTH MICRO SWITCHES IAW 52-76-01. OPERATIONS CHECKED GOOD, NO FAULT INDICATION.

Part: ENGINE — SMOKE (NR 2) · airframe 31,363 hrs · 27,141 cycles

SMOKE COMING OUT OF ENG 2, AFTER SHUTDOWN WITH A STRONG SMELL OF BURNED OIL. COMPLIED WITH ETN-EM-79-015 STEPS 1 - 9. RETURNED ENG TO SERVICE. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: BRAKE — FAILED (TE FLAP XMSN) · airframe 30,128 hrs · 26,108 cycles

FLAP LOW SPEED EICAS MESSAGE ON APPROACH. M PROCEDURES COMPLIED WITH, NO CMC MESSAGE. R & R RT FLAP TRANSMISSION BRAKE IAW AMM 27-51-01. OPS CHECKED GOOD. PERFORMED WIRE CHECK IAW FIM 27-51-00-810-814-A. ALL FOUND OK.

Part: FLAP — MALFUNCTIONED (WING) · airframe 30,098 hrs · 26,080 cycles

FLAP FAIL ON FINAL AT 2000 FT ALL SET FOR 22 FAILED AT 11 ON GLIDE SLOPE SLOWING THROUGH 120 KT 450 FPM DESCENT. RESET & PERFORMED OPERATIONS CHECK OF FLAP SYS IAW AMM 27-51-00. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,737 hrs · 25,793 cycles

CAPTAIN'S FLASHLIGHT INOPERATIVE. R & R CAPTAIN'S FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 29,257 hrs · 25,360 cycles

FLIGHT ATTENDANT EMER FLASHLIGHT HOLDER BASE IS BROKEN. R & R FLIGHT ATTENDANT EMER FLASHLIGHT BRACKET IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: SWITCH — INOPERATIVE (AILERON SYS) · airframe 28,965 hrs · 25,119 cycles

AILERON SYS 1 INOPERATIVE IN FLIGHT. R & R AIL SYS NR 1 PUSH BUTTON IAW AMM 20-13-08. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: PROXIMITY SWITCH — OUT OF ADJUST (MLG) · airframe 28,836 hrs · 25,015 cycles

DOWN LOCK RELEASE BUTTON PRESSED FOR GEAR RETRACTION ON TAKEOFF. LG AIR & GND FAIL MSG AFTER GEAR SELECTED DOWN. FOUND PROXIMITY SWITCHES ON RT & LT MLGS OUT OF RANGE. ADJUSTED PROX SWITCHES IAW AMM 32-63-05 & PERFORMED EXT & RETRACTION OF GEARS IAW AMM 32-30-00. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,834 hrs · 25,013 cycles

LEFT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1L & 2L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75 BETWEEN STRINGERS 1L & 2L IAW ERS-EM-53MR-550.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,834 hrs · 25,013 cycles

RIGHT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1R & 2R. PERFORMED PERMANENT REPAIR OF RT REAR FUSELAGE I SKIN AT FRAME 75 BETWEEN STRINGERS 1R & 2R IAW ERS-EM-53MR-551.

Part: WIRE — BROKEN (CABIN) · airframe 28,834 hrs · 25,013 cycles

NUMBER 2 EMER PROXIMITY LIGHT STRIP HAS BROKEN & DAMAGED WIRES. R & R FWD GALLEY EMER LIGHT STRIP IAW AMM 33-50-12.

Part: FITTING — WORN (RT AILERON) · airframe 28,834 hrs · 25,013 cycles

RIGHT AILERON DAMPER FITTING WORN. REMOVED & INSTALL DAMPER FITTING IAW EO EM-27MR-112.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 28,834 hrs · 25,013 cycles

CIRCUMFERENTIAL SPLICE IS CORRODED BETWEEN FRAME 12 & 13, STRINGER 21L & 21R. COMPLIED WITH ERS-EM-5300-528 JUNCTION 02 CIRCUMFERENTIAL SPLICE CORROSION BETWEEN FRAME 12 & 13 & BETWEEN STRINGER 21L - 21R. PERMANENT REPAIR SEE TASK & WIPS FOR DETAILS.

Part: DOOR — GOUGED (CABIN) · airframe 28,834 hrs · 25,013 cycles

MAIN DOOR GOUGED ALONG LOWER EDGE, METAL MOVED, NOT PAINT DAMAGE ONLY. MAIN DOOR GOUGED ALONG LOWER EDGE FOUND TO BE ACCEPTED AS IS IAW ERS-EM-5200-159. SEE TASK & WIPS FOR DETAILS.

Part: DOOR — DENTED (CABIN) · airframe 28,834 hrs · 25,013 cycles

MAIN DOOR DENTED NEAR AFT EDGE, 9 INCHES ABOVE AFT LOWER CORNER. MAIN DOOR DENTED NEAR AFT EDGE, 9 INCHES ABOVE AFT LOWER CORNER FOUND TO BE ACCEPTED AS IS IAW ERS-EM-5200-159. SEE TURNOVER FOR DETAILS.

Part: WIRE — BROKEN (CABIN) · airframe 28,834 hrs · 25,013 cycles

TWO EMER LIGHT STRIP WIRES ARE BROKEN AT FLOOR PANEL 261BF. INSTALLED SERVICEABLE PINS ON TWO EMER LIGHT STRIP WIRES, AT FLOOR PANEL 261BF IAW WM 91-10-02, SWPM 20-00-03 & SWPM 20-21-00. SEE BOW 157401 FOR OPERATIONS CHECK.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 28,834 hrs · 25,013 cycles

BATTERY COMPARTMENT DOOR CUT OUT CRACKED, AFT EDGE MARKED. REPAIRED CRACK ON BATTERY COMPARTMENT DOOR CUT OUT AFT EDGE IAW ERS-EM-5300-527. SEE WIP & TASK ENTRIES FOR DETAILS.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 28,561 hrs · 24,769 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED MAIN PAX DOOR ROLLERS IAW MM 52-18-00, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: ISIS — FAILED (COCKPIT) · airframe 28,245 hrs · 24,507 cycles

STANDBY ATT FAIL DURING ROTATION, DIVERT BACK TO LGA. R & R ISIS IAW AMM 34-01-01. OPERATIONS CHECK & LEAK CHECKED GOOD IAW AMM 34-01-01.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 27,953 hrs · 24,254 cycles

MAIN CABIN ENTRY DOOR EXCESSIVE FORCE USED TO OPEN OR CLOSE DOOR USING INSIDE HANDLE. CLEANED & LUBED MAIN CABIN DOOR IAW MX STANDARD PRACTICES, OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,761 hrs · 24,089 cycles

OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD IAW WC 33-700-17.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 27,709 hrs · 24,050 cycles

RIGHT & LT AFT OVERWING EMERGENCY LIGHT IS INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY IAW EMB 140 AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 27,314 hrs · 23,727 cycles

AFT FLASHLIGHT IN CABIN NOT CHARGING. R & R AFT FLASHLIGHT, OPS GOOD AMM 33-50-16.

Part: WIRE — LOOSE (FLASHLIGHT) · airframe 26,814 hrs · 23,301 cycles

DURING B INSPECTION, FOUND THE AFT CABIN EMERGENCY FLASHLIGHT NOT CHARGING. FOUND A LOOSE WIRE ON SPLICE, REINSTALLED. THE OPS CHECKED GOOD IAW AMM 20-13-01. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,325 hrs · 22,839 cycles

DURING MX INSP. FOUND THE LT AFT EXTERIOR EMERGENCY LIGHT INOP. THE ACFT WAS PLACED ON MEL. REPLACED FUSE 1 AT BATTERY CHARGER NR 4 IAW RADIANT POWER CORP CMM 25-60-03. FUSE, PN: 276005. LIGHT EMERGENCY LT, PN: 30-2510-3. NR 4 BATTERY, EMERGENCY LIGHTING, PN: 2013-1A. SN: 68179. NR 4 BATTERY CHARGER ASSY, PN: 11-0049. SN: 19319. THE OPS CHECK WERE GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — SHORTED (EXTERIOR) · airframe 26,325 hrs · 22,839 cycles

DURING MX FOUND BOTH OVERWING EXTERIOR EXIT LIGHT ASSEMBLIES SHORTED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LT AND RT EXTERIOR EMERGENCY LIGHT ASSEMBLIES AT OVERWING POSITIONS IAW MM 33-50-10. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 26,224 hrs · 22,744 cycles

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

Part: WINDSHIELD WIPER — OUT OF POSITION (WINDSHIELD) · airframe 25,464 hrs · 22,073 cycles

FOR FLIGHT 3342 THE CREW REPORTED THE CAPTAIN’S WINDSHILD WIPER WOULD NOT MOVE WHEN TURNED TO LOW OR HIGHT COULD HEAR MOTOR RUNNING SMELLED MOTOR BURNING PULLED C/B 6-15 WIPER MOTOR WOULD NOT TURN OFF WHEN SLECTED TO OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPOSITION WIPER ARM OFF OF WIPER STOP. PERFORMED OPERATIONAL CHECK IAW AMM 30-41-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,449 hrs · 22,058 cycles

DURING MAINTENANCE INSPECTION FOUND THE GALLEY EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY EMERGENCY LIGHT IAW AMM 33-29-03. THE LIGHT OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED · airframe 25,310 hrs · 21,949 cycles

ON FLIGHT 2711 THE CREW REPORTED THAT WHILE IN CRUISE THEY RECEIVED A FLAP FAIL CAUTION MESSAGE ON EICAS. THE CREW COMPLIED WITH AOM VOL 1 CHECKLIST, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REACTIVATED NR 2 ENGINE ANTI-ICE VALVE IAW 30-21-01, OPS CHECK NR 2 ENGINE ANTI ICE VALVE IAW 30-21-00. THE OPERATIONAL CHECK WAS GOOD. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — WEAK (COCKPIT) · airframe 24,444 hrs · 21,070 cycles

DURING MAINTENANCE INSPECTION, FOUND THE FLIGHT DECK FLASHLIGHT DIM & NOT HOLDING A CHARGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT IAW MM 33-50-16. TESTED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — LOOSE (PAX DOOR) · airframe 24,285 hrs · 20,935 cycles

FLIGHT 2726, CREW REPORTED MAIN CABIN DOOR WOULD NOT OPEN FROM INSIDE. AIRCRAFT REMOVED FROM SERVICE. FOUND INTERIOR DOOR HANDLE LOOSE, TIGHTEN HANDLE. OPS CHECKED GOOD IAW AMM 140 52-00-00. AIRCRAFT RETURNED TO SERVICE.

Part: DUCT — SEPARATED (HEAT EXCHANGER) · airframe 24,234 hrs · 20,892 cycles

FLIGHT N2726, THE CREW REPORTED THAT ON TAKEOFF THEY LOST PACK 2 (PACK VALVE CLOSED) WOULD NOT RESET. DECLARED AN EMERGENCY & RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. INSTALLED DUCT ON NR 2 HEAT EXCHANGER. NR 2 PACK OPS CHECKED GOOD AMM 21-51-00. AIRCRAFT RETURNED TO SERVICE.

Part: GUSSET — CORRODED (LAVATORY) · airframe 24,181 hrs · 20,849 cycles

DURING MAINTENANCE BASE INSPECTION, FOUND THE LAVATORY LEFT BEAM GUSSET CORRODED AT THE FORWARD END. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW SERVICEABLE LAVATORY LEFT BEAM GUSSET IAW SRM 51-40-02, 51-20-03, 51-20-01, 51-40-09. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,181 hrs · 20,849 cycles

DURING MAINTENANCE BASE INSPECTION, FOUND THE EMERGENCY LIGHT NR 6 HAS A BROKEN WIRE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,181 hrs · 20,849 cycles

DURING MAINTENANCE BASE INSPECTION, FOUND THE RIGHT BEAM GUSSET CORRODED AT THE AFT END. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT BEAM GUSSET IAW EMB SRM 51-40-02 AND 51-20-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,091 hrs · 20,777 cycles

DURING MAINTENANCE INSPECTION FOUND THE FIRST FLOOR PROXIMITY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST FLOOR PROXIMITY LIGHT IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,014 hrs · 20,702 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,938 hrs · 20,631 cycles

DURING B INSPECTION, FOUND THE RIGHT EXIT ROW EMERGENCY DOME LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EXIT ROW EMERGENCY DOME LIGHT AND PRINTER CIRCUIT BOARD. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,874 hrs · 20,571 cycles

DURING B INSPECTION, FOUND SEAT 11A OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BULB IN 11A OVERHEAD EMERGENCY EXIT LIGHT IAW AMM 33-50-08-000-801-A/33-50-08-400-801-A . OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — ERODED (EXTERIOR) · airframe 23,846 hrs · 20,545 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND EXTERNAL LEFT OVERWING EMERGENCY LIGHT BULB TO BE MAKING INTERMITTENT CONTACT WITH SOCKET OF LIGHT ASSEMBLY DUE TO ELECTRODE EROSION OF BULB. REMOVED AND REPLACED LIGHT BULB AND CHECKED EMERGENCY LIGHT IAW EMB140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,811 hrs · 20,511 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT ABOVE SEAT 11A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-07-000-801-A AND 33-50-07-400-801-A PART NUMBER 1317. DID NOT FIX. TROUBLESHOT AND FOUND NO POWER AT SOCKET. REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY CHARGER ASSEMBLY AND BATTERY IAW WC 33-700-19. OPC IAW WC 33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,493 hrs · 20,200 cycles

DURING B-INSPECTION FOUND THE LEFT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW EMB140 AMM 33-50-17. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,444 hrs · 20,154 cycles

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

Part: LIGHT — INOPERATIVE (LT WING) · airframe 23,288 hrs · 20,041 cycles

DURING INSPECTION FOUND LEFT WING AFT EMERGENCY LIGHT IN OPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT WING AFT EMERGENCY LIGHT IAW EMB 140 AMM 33-50-10 OPERATIONAL CHECKS GOOD. THE AIRCRAFT RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,111 hrs · 19,910 cycles

DURING THE B-INSPECTION FOUND THE LEFT FUSELAGE EMERGENCY AFT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT EMERGENCY LIGHT AFT IAW EMB 140 AMM 33-50-55. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 22,839 hrs · 19,699 cycles

ON FLIGHT 2745 THE CREW REPORTED THE FLAP FAIL MASTER CAUTION CAME ON DURING APPROACH THEY FAILED AT 7 DEGREES. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED FIM IAW EMB 27-51-00-810-804-A. RECYCLED FLAP 1/2 CB, FLAP FAIL MESSAGE RESET. PERFORMED OPERATION CHECK OF FLAP CONTROL SYSTEM IAW AMM 27-51-00. THE OPERATIONAL CHECK WAS NORMAL. VISUAL INSPECTION, NO FAULTS FOUND.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,611 hrs · 19,508 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT EXTERNAL OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT BULB ON RIGHT OVERWING EMERGENCY LIGHT. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — LACK OF LUBE (MAIN DOOR) · airframe 22,573 hrs · 19,578 cycles

F/A REPORTS MAIN DOOR DIFFICULT TO OPERATE. MAY JUST NEED LUBRICATION. LUBRICATED THE ACTUATING EXTERNAL HANDLE IAW EMB 140 AMM 52-18-00 AND CLEANED SEAL FROM STICKERS. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,537 hrs · 14,067 cycles

FOR FLIGHT 4165 MAINTENANCE REPORTED THE SIDE HINGED MAIN DOOR EXTERNAL EMERGECNY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVCIE. REMOVED AND REPLACED THE SIDE HINGED MAIN DOOR EXTERNAL EMERGENCY LIGHT BULB IAW EMB AMM 33-50-10. THE OPERATIONAL C CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DUCT — BLOWN (AC BAY) · airframe 21,608 hrs · 18,653 cycles

ON FLIGHT 4104 THE CREW REPORTED THE NR 1 PACK FAILED AND THEY COULD NOT MAINTAIN CABIN PRESSURE DURING CLIMB TO 14,000 FEET. THE MASKS WERE DEPLOYED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFOMRED OPERATIONAL CHECK OF PACK NR 1 IAW EMB 140 AMM 21-51-00, THE CHECK WAS GOOD. COMPLIED WITH PRESSURIZATION AND LEAK CHECK IAW AMM 21-31-00, AND THE CHECK WAS GOOD. REMOVED AND REPLACED THE BLOWN DUCTS BETWEEN PACK VALVE AND DTCV IAW EMB 140 AMM 21-60-01. THE OPERATIONAL CHECK AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,537 hrs · 18,595 cycles

ON FLIGHT 4167 THE CREW REPORTED THE LEFT AFT EXTERIOR EMERGENCY LIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT EXTERIOR EMERGENCY LIGHT. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,226 hrs · 16,694 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT UPPER SEAT TRACK SUPPORT AT FRAME 50 TO HAVE CORROSION AT 2 SPOTS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT UPPER SEAT TRACK SUPPORT AT FRAME 50 IAW EO EM-53MR-1617. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 18,749 hrs · 16,337 cycles

FOR FLIGHT 2816 THE EMERGENCY EXIT LIGHT NEAR 11A WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. MAINTENANCE INSPECTED LIGHT AND DID AN OPERATIONAL CHECK PER 33-50-00. THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (NLG PROX SWITCH) · airframe 13,481 hrs · 10,969 cycles

ON FLIGHT 3006, CREW REPORTED AIR/GND FAIL MESSAGE WHEN RETRACTING THE LANDING GEAR. GEAR REMAINED DOWN WITH 3 GREEN LIGHTS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NOSE LANDING GEAR HARNESS IAW EMB140 AMM 32-61-02. PERFORMED OPERATIONAL CHECK ON LANDING G EXTENSION AND RETRACTION IAW EMB 140 AMM 32-30-00. OPERATION CHECK GOOD. FOUND PIN BROKEN ON NOSE NLG PROX SWITCH AND REMOVED AND REPLACED NOSE LANDING GEAR PROX SWITCH IAW EMB 140 AMM 32-68-02. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CORRODED (BS 258) · corrosion level 2 · airframe 18,475 hrs · 22,935 cycles

DURING A HMBV INSPECTION, THE GALLEY FLOOR FRAME AT STA 258 WAS FOUND CORRODED. REPAIRED CORRODED AREA IAW SAAB SRM 53-70-30 AND SRM 51-40-21. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (WARNING MESSAGE) · airframe 12,060 hrs · 9,942 cycles

RECEIVED ELECTRICAL EMERGENCY ABNORMAL MESSAGE, DIVERTED TO BUF, MESSAGE CLEARED ITSELF. NO CMC MESSAGE NOTED, RESET ELECTRICAL POWER PER EMB FAULT ISOLATION MANUAL TASK 24-60-00-810-820A.

Part: PRESSURE SWITCH — FAILED (NR 1 A/C PACK) · airframe 11,476 hrs · 9,466 cycles

PACK ONE OVERLOAD MESSAGE FOLLOWED BY PACK TWO OVERLOAD MESSAGE, EMERGENCY DECLARED. RETURNED TO ACT. PERFORMED FUNCTIONAL CHECK OF NUMBER ONE PACK WITH NO DEFECTS NOTED. REMOVED AND REPLACED NUMBER TWO PACK OVERPRESSURE SWITCH IAW EMB 21-51-06. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: ENGINE — SMOKE (NR 2)

CREW REPORTED LAV SMOKE WARNING MESSAGE AFTER TAKEOFF. THIS IS THE SECOND OCCURENCE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW AE W/C 72-000-00 OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACM — SEIZED (A/C BAY)

SYR - FLT 4320 - DURING CRUISE FLIGHT, THE FLIGHT ATTENDANT REPORTED LOUD NOISE UNDER THE FLOORBOARD FOLLOWED BY A BURNING SMELL AND SMOKE. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT AIR CYCLE MACHINE. OPERATIONAL CHECK GOOD. (M)