N809AE

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 39,634 hrs · 35,034 cycles

MAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED MAIN DOOR EXTERNAL EMERGENCY LIGHT IAW EMB140 AMM 33-50-10. REPAIRED WIRE W717-0003-20 IAW EMB140 SWPM 20-21-00. OPC GOOD.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 39,630 hrs · 35,030 cycles

FLAP FAIL WHEN FLAP LEVER MOVED TO 9, EICAS SHOWED FLAPS 0. REMOVED AND REPLACED FECU IAW EMB 140 AMM 27-53-02. OPC FAIL. REMOVED AND REPLACED FVS IAW AMM 27-51-12. OPC GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,585 hrs · 34,979 cycles

11 B/C INTERIOR OVERHEAD EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED 11 B/C INTERIOR OVERHEAD EMERGENCY LIGHT IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,477 hrs · 34,883 cycles

RH OVERWING EMERGENCY LIGHT INOP.-C/A-REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10. OPS CHECK GOOD AT THIS TIME.

Part: CONTROL HANDLE — LACK OF LUBE (PARKING BRAKE) · airframe 39,464 hrs · 34,872 cycles

PARKING BRAKE HARD TO RELEASE-C/A-LUBRICATED EMERGENCY PARKING BRAKE CONTROL IAW ENVOY WIC 32-600-12. OPC GOOD AT THIS TIME. NO DEFECTS NOTED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 38,399 hrs · 33,926 cycles

VERY STRONG JET FUEL SMELL IN THE COCKPIT AND CABIN AFTER E2 HUNG START WAS ABORTED. FOLLOWING FIM# 72-00-00 AND FIN#21-20-00.INSPECTED ENG.FOR LEAKS & OIL LEVEL & NO DEFECTS FOUND .PERFORMED ENG. STARTING PROCEDURES IAW AMM71-00-00 NO HUNG START AT THIS TIME & NO FUEL OR OIL SMELL IN COCPIT OR CABIN,ALSO NO CMC MESSAGE OR FAULT CODE.AIR CONDITIONING WORKING PROPERLY IAW 21-50-00.

Part: DRAIN LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 38,205 hrs · 33,734 cycles

UNRELIABLE AIRSPEED. IAS MSG DISPLAYED ON BOTH PFD'S. FO AND STANBY INSTRUMENTS WERE SHOWING CONSISTENT AIRSPEED. EMERGENCY DECLARED. DIVERTED TO OKC. NOT OVERWEIGHT LDG. C/A-REMOVED WATER FROM CA AND FO PITOT DRAIN LINES IAW AMM 34-13-00. PERFORMED OPC AND FUNC OF FO ADC IAW AMM 34-15-00. OPC AND FUNC GOOD. FO PITOT STATIC SYS LEAK CHECK GOOD IAW AMM 34-13-00. PERFORMED OPC AND FNC OF ISIS. OPC AND FNC GOOD IAW AMM 34-01-01. LEAK CHECK GOOD IAW AMM 34-13-00. REMOVED AND REPLACED CA ADC IAW AMM 34-15-01. OPC GOOD. SEE ITEM 1 AML PG 4466921 FOR LEAK CHECK.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,042 hrs · 33,593 cycles

AFT CEILING EXIT SIGN AND LH EXIT DOOR SIGN INOP-C/A-REMOVED AND REPLACED #3 EMERG BATTERY AND POWER SUPPLY IAW AMM 33-50-04 OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1ASMI S/N 73049

Part: CONNECTOR — UNSECURE (CABIN) · airframe 37,920 hrs · 33,475 cycles

FWD CEILING EXIT LIGHT INOP. C/A-RESECURED CONNECTOR ON NR 6 EMERGENCY LIGHT INVERTER OPS CHECK GOOD IAW AMM 33-50-11.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,454 hrs · 33,059 cycles

FOUND BROKEN WIRE GOING TO SERVICE DOOR EMERGENCY EXTERNAL LIGHT. C/A-REPAIRED WIRE AT SPLICE SP7376 IAW SPWM 20-21-00.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,450 hrs · 33,055 cycles

EXIT ROW CEILING EXIT MARKER LIGHT FWD FACE DOES NOT ILLUMINATE-C/A-RAR #2 EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK IAW AMM 33-50-04. OPS CHECK GOOD

Part: WIRE — DAMAGED (CABIN) · airframe 37,450 hrs · 33,055 cycles

SUPPLEMENTAL SERVICE DOOR GROUND ILLUMINATION EMERGENCY LIGHT INOP-C/A- "TRANSFERRED TO AML PAGE 4420955 ITEM 2". DEFERRED PER MEL 33-29. REMOVED AND REPLACED EMER. LIGHT BATTERY PACK NR 2 IAW AMM 33-50-04. DID NOT FIX. REPAIRED WIRE AT SPLICE SP7376 IAW SPWM 20-21-00. OPC GOOD OF EMERGENCY LIGHTING SYSTEM IAW AMM 33-50-00. MEL ITEM RESTORED.

Part: ECU — FAILED (TE FLAP) · airframe 37,358 hrs · 32,963 cycles

SUPPLEMENTAL FLAP FAIL EICAS MESSAGE. FLAPS FAILED AT 0 DEGREES ON APPROACH. C/A-CMC FAULT MSG RH FLAP SENSOR FAIL HAD TO RESTORE FCU TO RESET FLAPS IAW FIM 27-51-00-810-817-A STEP 1 ITEM 2. RESTORED FCU BACK TO ORIGINAL CONDITION FOR MEL 27-09. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02. OPS CK GOOD IAW AMM 27-53-00. NO MESSAGE AT THIS TIME

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,344 hrs · 32,951 cycles

SERVICE DOOR HINGE COVER EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR HINGE COVER EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-09. OPC GOOD

Part: FLASHLIGHT — NOT REPORTED (CABIN) · airframe 37,092 hrs · 32,708 cycles

FLASHLIGHT HOLDER OVER FLIGHT ATTENDANT STATION. FLIGHT CREW PLACARDED FWD FA FLASHLIGHT HOLDER. SUPPLEMENTAL -C/A-FLIGHT CREW PLACARDED FWD FA FLASHLIGHT HOLDER MEL AUTH 100545-C REF 25-53 MOC 628765. REMOVED AND REPLACED F/A FLASHLIGHT ASSY IAW AMM 33-50-16. OPC GOOD. MEL RESTORED.

Part: DISPLAY — FAILED (COCKPIT) · airframe 36,725 hrs · 32,399 cycles

FO MFD FAILED IN FLIGHT WITH ELECTRICAL ODOR. CAPTAIN PULLED THE CIRCUIT BREAKER. RESET THE CIRCUIT BREAKER . REMOVED AND REPLACED THE FIRST OFFICER`S MFD IAW 34-22-01. OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: MODULE — MALFUNCTIONED (CABIN PRESSURE) · airframe 36,556 hrs · 32,254 cycles

AIRCRAFT FAILNG TO PRESSURIZE NO "CABIN ALT" INDICATION NO "CABIN RATE" INDICATION EMERGNECY DECLARED. R&R CPAM IAW AMM 21-32-01. OPC GOOD. PITOT STATIC LEAK CHECK GOOD.

Part: TIRE — FAILED (MLG) · airframe 36,315 hrs · 32,007 cycles

DURING TAXI IN AFTER LANDING, THE PLANE STARTED VIBRATING. PULLED OVER TO FIND TWO RIGHT MAIN TIRES FLAT. FOUND THE NR 3 MLG TIRE FLAT. REMOVED AND REPLACED THE MLG WHEEL ASSY IAW WC 32-700-11. REMOVED AND REPLACED THE NR 4 MLG WHEEL ASSY IAW WC 32-700-11.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 35,397 hrs · 31,002 cycles

#2 FLOOR EMERGENCY LIGHT STRIP HAS BROKEN WIRE-C/A-REPAIRED #2 FLOOR PROXIMITY LIGHT WIRE IAW EMB 145 SWPM 20-50-00.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 35,397 hrs · 31,002 cycles

EMERGENCY PATHWAY LIGHT ON SERVICE DOOR INOP-C/A-REPAIRED EMERGENCY PATHWAY LIGHT ON SERVICE DOOR WIRE TO P7198 PIN C IAW EMB 145 SWPM 20-21-00.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,397 hrs · 31,002 cycles

EMERGENCY FLOOR LIGHTING FROM 3A TO 6A INOP-C/A-REMOVED AND REPLACED #2 BATTERY HOLDER AND BATTERY CHARGER ASSEMBLY IAW EMB 145 AMM 33-50-04

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 35,397 hrs · 31,002 cycles

RH EMERGENCY LIGHT HAS BROKEN WIRES (WIRE# P8560) ON FUSELAGE FAIRING-C/A-REPAIRED RH 2 EMERGENCY LIGHT WIRES (WIRE# P8560) IAW EMB 140 SWPM 20-00-03 AND 20-21-00

Part: SKIN — DENTED (FRAME 19-20) · airframe 35,397 hrs · 31,002 cycles

2 DENTS AND 1 PROTRUSION BTW FR 19-20 STR 11-12L-C/A-REPAIRED 2 DENTS AND 1 PROTRUSION BTW FR 19-0 STR 11-12L IAW ERS-EM-53MR-3029

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 35,397 hrs · 31,002 cycles

#3 EMERGENCY LIGHT STRIP WIRES DAMAGED FROM ASSEMBLY-C/A-REMOVED AND REPLACED #3 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12.

Part: SKIN — NICKED (FRAMES 13-14) · airframe 35,397 hrs · 31,002 cycles

SKIN NICKED FWD OF FR 14 BTW STR 20-21L-C/A-PERFORMED REPAIR TO SKIN FWD OF FR 14 BTW STR 20-21L IAW EMB 140 SRM 53-21-01 FIG. 206

Part: FRAME — CRACKED (FR 78) · airframe 35,397 hrs · 31,002 cycles

CRACKS AROUND RIVETS ON L/H FRAME 78. REPAIRED CRACKS AROUND RIVETS ON LH FRAME 78 IAW ERS-EM-53MR-3020

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 35,397 hrs · 31,002 cycles

CARGO DOOR SILL IS CORRODED-C/A-RAR CARGO DOOR SILL IAW EMB 145 SRM 51-40-02

Part: FRAME — CRACKED (FRM 10) · airframe 35,397 hrs · 31,002 cycles

PILOT'S SIDE FRAME 10 CRACKED BELOW DV WINDOW TRACK-C/A-REMOVED AND REPLACED PILOT'S SIDE FRAME 10 IAW EMB 145 SRM 51-40-02

Part: FRAME — CRACKED (FRM 10) · airframe 35,397 hrs · 31,002 cycles

CO PILOT'S SIDE FRAME 10 CRACKED BELOW DV WINDOW TRACK-C/A-REMOVED AND REPLACED CO PILOT'S SIDE FRAME 10 IAW EMB 145 SRM 51-40-02

Part: FITTING — CRACKED (FRAMES 19-20) · airframe 35,397 hrs · 31,002 cycles

MACHINED FITTING BETWEEN FRAMES 19 AND 20 AT STRINGER 3L CRACKED-C/A-REMOVED AND REPLACED MACHINED FITTING BETWEEN FRAMES 19 AND 20 AT STRINGER 3L CRACKED IAW EMB140 SRM 51-40-02

Part: FRAME — CRACKED (FRM 23) · airframe 35,397 hrs · 31,002 cycles

FRAME 23 CRACKED AT RH OTBD FLOOR SUPPORT-C/A-REPAIRED FRAME 23 CRACK BETWEEN STRINGERS 15R - 16R AT RH OTBD FLOOR SUPPORT IAW EM-53MR-1808

Part: FITTING — CRACKED (LT PYLON) · airframe 35,397 hrs · 31,002 cycles

L/H PYLON LOWER FWD ENGINE YOKE FITTING CRACKED-C/A-REMOVED AND REPLACED L/H PYLON LOWER FWD ENGINE YOKE FITTING IAW EO EM-54MR-386.

Part: FLOOR SUPPORT — CORRODED (FR 57-59) · airframe 35,397 hrs · 31,002 cycles

SSI; 53-20-11 LEFT OMEGA BEAM IS CORRODED BTW FR 57-59-C/A-REPAIRED LEFT OMEGA BEAM BTW FR 57-59 IAW EO-EM-53MR-1518 REV 3

Part: FLOOR SUPPORT — CORRODED (FRAME 30) · airframe 35,397 hrs · 31,002 cycles

SSI 53-20-11; LEFT OMEGA BEAM IS CORRODED AT FR 38-C/A-REPAIRED LEFT OMEGA BEAM AT FR 38 IAW EMB 140 SRM 53-00-10, FIG 202 SHEET II

Part: SUPPORT — CORRODED (WASTE VALVE) · airframe 35,397 hrs · 31,002 cycles

SSI 53-20-29; LAV EXTERNAL WASTE VALVE SUPPORT IS CORRODED-C/A-REMOVED AND REPLACED LAV EXTERNAL WASTE VALVE SUPPORT IAW EMB 140-SRM 51-40-02

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 35,397 hrs · 31,002 cycles

LH #2 CABIN FLOOR PROXIMITY LIGHT WIRE BROKEN-C/A-REMOVED AND REPLACED LH #2 CABIN FLOOR PROXIMITY LIGHT IAW EMB 140 AMM 33-50-12-04

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 35,397 hrs · 31,002 cycles

EMERGENCY LIGHT HAD WIRE INSULATION DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 35,397 hrs · 31,002 cycles

LEFT CABIN FLOOR, FIVE EMERGENCY LIGHT EXTRUSIONS CRACKED. R & R THE LIGHTS IAW AMM 33-50-12-04.

Part: SIGN — INOPERATIVE (CABIN) · airframe 34,152 hrs · 29,723 cycles

EXIT MARKER SIGN ON LT EMER EXIT DOOR INOPERATIVE. R & R EXIT MARKER SIGN IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.

Part: HYDRAULIC LINE — NOT REPORTED (LT MLG) · airframe 34,024 hrs · 29,591 cycles

DURING FLIGHTS NOTICED HYD 1 LO QTY, AFTER LG EXTENSION, 3 DOWN, GOT ENG 1 HYD PUMP FAIL. COMPLIED WITH CHECKLIST. TRANSFERRED TO NRWC 809-DFW-02349. R & R LT MLG ACTUATOR EXT HOSE AMM 32-33-08. SEE ITEM 3 FOR GEAR EXTENSION & RETRACTION & LEAK CHECK. REF TO NRWC 809-DFW-02349 SERVICED NR 1 HYD SYS IAW AMM 12 13 01. SEE LOG PAGE 4065424 ITEM 1 FOR E1 HYD PUMP FAILED.

Part: DISPLAY — FAILED (COCKPIT) · airframe 33,525 hrs · 29,030 cycles

STRONG ELEC ODOR IN COCKPIT. REPLACED CAPTAINS MFD IAW AMM 34-22-01. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,373 hrs · 28,845 cycles

EMERGENCY LIGHTS ON FLOOR MID-WAY IN CABIN INOPERATIVE. R & R NR 3 EMER LIGHT BATTERY CHARGER & BATTERY IAW WC 33-700-17 & 33-700-19. OPERATIONS CHECKED GOOD. CHARGER ASSEMBLY BATTERY, PN BA5-0933-901 & SN C02266.

Part: CHARGER — FAILED (CABIN) · airframe 33,098 hrs · 28,531 cycles

EMERGENCY LIGHTS, FWD AISLE STRIP, GALLEY SERVICE DOOR & FWD EXTERNAL RT EMER LIGHT FLICKERS OFF AFTER ABOUT A SECOND AFTER BEING TURNED ON. ALL ARE POWERED BY NR 2 EMER BATTERY POWER SUPPLY. R & R NR 2 BATTERY CHARGER & BATTERY IAW MCM WC 33-700-19. OPERATIONS CHECKED GOOD IAW MCM WC 33-700-17. EMER LIGHTING BATTERY PN 2013-1A & SN 104844.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,387 hrs · 27,831 cycles

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

Part: UNIVERSAL — MALFUNCTIONED (COCKPIT TEMP) · airframe 32,306 hrs · 27,754 cycles

UNABLE TO CONTROL TEMP IN COCKPIT. TEMP CLIMBING THROUGH FL 190 DROPPED TO +7C IN COCKPIT. R & R NR 1 DIGITAL TEMP CONTROLLER IAW AMM-21-60-04. DID NOT FIX, SEE ITEM NR 2 THIS LOG PAGE.

Part: FCU — FAILED (FUEL SYSTEM) · airframe 32,273 hrs · 27,724 cycles

ON TAKEOFF ROLL, RECEIVED FUEL 1 - 2 LO LEVEL WARNING & BOTH FUEL QTY GAUGES SHOWED DASHES, TAKEOFF ABORTED. R & R FCU IAW AMM 28-41-01. OPERATIONS CHECK FOUND SATISFACTORY IAW AMM 28-41-0.

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER) · airframe 31,959 hrs · 27,453 cycles

AT ALT 240 RECEIVED YD & AP FAIL FOLLOWED BY RUDDER SYS 1 - 2 INOPERATIVE. EXAMINED AFCS EVENT CODES, CODE 271 PREVIOUS FLIGHT & LAST NIGHT, RUDDER HYD MON. AFCS FUNCTION CHECK OK IAW AMM 22-11-00 SEE ITEM 2. R & R NR 2 RUDDER PRESS SWITCH IAW AMM CH 27-23-04. OPERATIONS CHECKED OK IAW AMM CH 27-23-00.

Part: CONNECTOR — BROKEN (CABIN) · airframe 31,702 hrs · 27,239 cycles

FOUND NR 3 FLOOR PROXIMITY LIGHT WIRES BROKEN CONNECTORS. REPAIRED NR 3 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-00-03. FOUND DURING OPEN UP. NR 3 CONNECTOR PN M39029 32-248.

Part: CONNECTOR — BROKEN (CABIN) · airframe 31,702 hrs · 27,239 cycles

FOUND NR 6 FLOOR PROXIMITY LIGHT WIRES BROKEN CONNECTORS. REPAIRED NR 6 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-00-0. FOUND DURING OPEN UP. NR 6 CONNECTOR M39029 32-248.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 31,702 hrs · 27,239 cycles

BAGGAGE DOOR FWD FRAME CORRODED AT LOWER 2 SCREW HOLES. PERFORMED PERMANENT REPAIR IAW ERS-EM-52MR-275.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,702 hrs · 27,239 cycles

REAR FUSELAGE II EXT SKIN IS CRACKED AROUND A RIVET AT FRAME 79 BETWEEN STRINGERS 5L - 6L. CUT OUT CRACK ON REAR FUSELAGE II EXT SKIN AROUND A RIVET AT FRAME 79 BETWEEN STRINGERS 5L - 6L. INSTALLED REPAIR IAW ERS-EM-5300-1038.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,702 hrs · 27,239 cycles

REAR FUSELAGE II EXT SKIN IS CRACKED AROUND A RIVET AT FRAME 79 BETWEEN STRINGER 5R - 6R. CUT OUT CRACKS ON REAR FUSELAGE II EXT SKIN AROUND A RIVET AT FRAME 79 BETWEEN STRINGERS 5R - 6R. INSTALLED REPAIR FILLER & DOUBLER ON REAR FUSELAGE II EXT SKIN IAW ERS-EM-5300-1027.

Part: ACM — SEIZED (AC BAY) · airframe 31,628 hrs · 27,173 cycles

PASSENGER REPORTED AFTER LANDING SMELLING ELEC BURNING SMELL & A WISP OF VAPOR FROM A PSU OVER ROW 8 & 9. COMPLIED WITH FIM CH 21-20-00-810-801 NO SMELL OR DEFECTS NOTED IN CABIN AREA. FOUND NR 1 ACM INOPERATIVE. COMPLIED WITH ETN EM-72-034 FOUND NR 1 PACK ACM SEIZED. R & R LT ACM IAW AMM 21-51-03. LEAK CHECKED FAILED. MEL REMAINS OPEN. ACM OPERATIONS CHECKED GOOD. R & R FLEX RUBBER DUCT GOING FROM DUEL TEMP CONTROL VLV TO Y DUCT IAW AMM 21-60-01. OPERATIONS CHECK & LEAK CHECKED GOOD. NO DEFECTS NOTED. MEL ITEM RESTORED. SECURED LOOSE COUPLING ON NR 2 PACK IAW MM CH 21-50-01 MEL ITEM RESTORED ON LEAKS NOTED.

Part: CONTROL VALVE — FAILED (NR 1) · airframe 31,419 hrs · 26,984 cycles

AUTO MODE PRESS FAIL IN FLT. CONDUCTED PROCEDURES IAW AOM VOL 1 DEFERE IAW MEL 21-18. M PROCEDURES COMPLIED WITH. AUTO & MANUAL INOPERATIOMS. CORRECTIVE ACTION: PERFORMED OPERATIONS CHECK OF PRESS SYSTEM IN MAN & AUTO IAW AMM 21-31-00. OPERATIONS CHECKED MEL RESTORED. TEMP CONTROL VLV. R & R E 1 FAIL MSG ON THE CMC. R & R TEMP CONTROL VLV NR 1 IAW AMM 21-60-01. OPERATIONS CHECKED GOOD.

Part: ISIS — MALFUNCTIONED (COCKPIT) · airframe 31,101 hrs · 26,703 cycles

ABORTED TAKEOFF 70 KTS ISIS FAIL, DISPLAY READS ATT GAUGE. R & R INTEGRATED STANDBY INST SYS DISPLAY IAW AMM 34-01-01. PERFORMED LEAK TEST. OPERATIONS CHECKED GOOD. ACFT IS CAT 2 COMPLIANT.

Part: FLASHLIGHT — INSTALLED (COCKPIT) · airframe 30,897 hrs · 26,532 cycles

FIRST OFFICER'S FLASHLIGHT INOPERATIVE. R & R FIRST OFFICER`S FLASHLIGHT AS REQUIRED.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 30,434 hrs · 26,027 cycles

FLIGHT ATTENDANT REPORTS MAIN DOOR HARD TO OPEN. LUBRICATED MAIN DOOR FRAME ROLLER & CHECKED OK IAW MM 53-21-02.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 30,322 hrs · 25,923 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. LUBRICATED MAIN CABIN DOOR IAW AMM 52-18-00. OPERATIONS CHECKED SATISFACTORY.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 29,458 hrs · 25,158 cycles

CAPTAIN'S FLASHLIGHT CRADLE BROKEN. R & R CAPTAIN'S FLASH LIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,345 hrs · 25,069 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-10. OPERATIONS CHECKED GOOD IAW EMB AMM 33-50-00.

Part: WIRE — BROKEN (ANTI-ICE VALVE) · airframe 29,250 hrs · 24,991 cycles

ON FLIGHT 3269 DURING THE CLIMB IN ICING CONDITIONS CREW RECEIVED AN EICAS WING A/I FAIL MESSAGE & A NO ICE/AI ON MESSAGE. THE CREW COMPLIED WITH AOM VOL 1 PROCEDURES & CONTACTED SOC/MOC. AN EMERGENCY WAS DECLARED, DUE TO EN ROUTE WEATHER THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED 3 BROKEN WIRES AT WING 1 ANTI-ICE VLV WIRE 122-0124-20, W122-0121-24 & W122-0126-20 IAW SWPM 20-21-00 & WIRE M 30-10-50. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (MAIN CABIN DOOR) · airframe 29,056 hrs · 24,843 cycles

F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. SERVICED MAIN DOOR ROLLERS IAW AMM 52-18-00.

Part: WARNING LIGHT — FALSE ACTIVATION (SPOILERS) · airframe 29,040 hrs · 24,833 cycles

DURING CRUISE FLIGHT, RECEIVED AN EICAS CAUTION SPOILER FAIL MESSAGE. RAN APPROPRIATE CHECKLIST IAW AOM. PERFORMED OPS TEST OF THE SPOILER SYS IAW AMM 27-63-01. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,650 hrs · 24,520 cycles

EMERGENCY LIGHT FWD OF THE LT WING IS INOPERATIVE. R & R BULB ON EMERGENCY LIGHT FWD OF THE LT WING IAW AMM 33-50-10, OPS CHECKED GOOD.

Part: ENGINE — ODOR (NR 1) · airframe 28,495 hrs · 24,386 cycles

CREW REPORTED DURING DESCENT FROM 4000' MSL, AN OILY ODOR ENTERED COCKPIT AND F/A STATION, DISSAPATED AFTER A FEW MINUTES. R & R NR 1 ENGINE IAW 71-000-00. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,427 hrs · 24,324 cycles

DURING PS-2 CHECK, FOUND LT EXTERIOR OVER WING EMERGENCY LIGHT TO BE OUT. R & R LAMP IAW MM 33-50-10. OPS CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 28,362 hrs · 24,260 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED MAIN DOOR FRAME ROLLER IAW AMM 53-21-02.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 27,984 hrs · 23,940 cycles

THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE ACFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN CABIN DOOR ROLLER AND PERFORMED OPS CHECK IAW MM 52-10-00. THE ACFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 27,817 hrs · 23,790 cycles

ON FLIGHT 2963 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED LUB TO CABIN MAIN DOOR AND OPS CHECK TO INTERNAL ACTUATING MECHANISM PER EMB AMM 52-18-00-820-801 AND 52-18-00-600-801, FOUND WITHIN LIMITS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 27,616 hrs · 23,642 cycles

FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN PASSENGER DOOR FRAME ROLLERS IAW EMB 140 AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 27,355 hrs · 23,398 cycles

ON FLIGHT 4390 THE CREW REPORTED THE FLASHLIGHT HOLDER BEHIND THE CAPTAIN’S SEAT WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 27,321 hrs · 23,367 cycles

DURING B INSPECTION FOUND THE COCKPIT CEILING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMPS IAW EMB 140 AMM 33-50-05-000-801-A AND 33-50-05-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,317 hrs · 23,360 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,199 hrs · 23,253 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT AT ROW 11 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LAMP IN CEILING AT ROW 11 IAW EMB AMM TASK 33-50-08-000-801-A AND TASK 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PUMP — MALFUNCTIONED (NR 2 ENGINE) · airframe 27,175 hrs · 23,235 cycles

ON FLIGHT 9806 THE CREW REPORTED THE ENGINE NR 2 PULSING ON DESCENT THROUGH 11,000 RETURNED TO NORMAL ON LEVEL OFF OCCURED AGAIN ON APPROACH. THE CREW DECLARED AN EMERGECNY AND LANDED WITHOUT INCIDNET. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 ENG FPMU IAW RR AMM 73-21-10. THE OPERATIONAL CHECK AND LEAKS CHECKS WERE GOOD. ALSO REMOVED AND REPLACED-- O-RING, PART NUMBER: AS3209-239. GASKET, PART NUMBER: MS27196-16. PACKING, PART NUMBER: AS3085-111. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 27,172 hrs · 23,232 cycles

DURING MAINTENANCE CHECK FOUND THE FORWARD LEFT VERTICAL STAB TO FUSELAGE ANGLE HAS A CRACK APPROX 1" LONG. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD VERTICAL STAB TO FUSELAGE ANGLE IAW EO EM-53MR-2062. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,172 hrs · 23,232 cycles

DURING MAINTENANCE CHECK FOUND THE LEFT OMEGA BEAM SUPPORT CRACKED BETWEEN FRAMES 48-49. THE AIRCRAFT WAS REMOVED FROM SERVICE. OMEGA BEAM SUPPORT REPAIRED AS REQUIRED IAW SRM 53-23-02 AND ETA-EM-5300-2652. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,172 hrs · 23,232 cycles

DURING MAINTENANCE CHECK FOUND THE RIGHT OMEGA BEAM SUPPORT CRACKED BETWEEN FRAMES 47-48. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED RIGHT HAND OMEGA BEAM SUPPORT ANGLE IAW SRM 53-23-02 AND REINSTALLED OMEGA BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 27,190 hrs · 23,245 cycles

DURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT ON THE HINGE ASSEMBLY NOT WORKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND WIRE W716-007-02 BROKEN. SPLICED WIRE IAW SWPM 20-21-00. THE OPERATIONAL TEST WAS GOOD IAW AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,173 hrs · 23,232 cycles

RT FR 23 IS CRACKED AT FLOOR LEVEL NEAR STR. 15 RT. REPAIRED FRAME RT 23 IAW SRM 51-40-02 AND GUIDELINES FROM EO EM-53MR-1791.

Part: BATTERY — WEAK (CABIN) · airframe 27,172 hrs · 23,232 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY BATTERY HAD LOW VOLTAGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 27,190 hrs · 23,245 cycles

DURING MAINTENANCE INSPECTION FOUND WIRED BROKEN OFF OF EMERGENCY FLOOR PROXIMITY LIGHT 251BF & 231GF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED BROKEN WIRES TO EMERGENCY FLOOR PROXIMITY LIGHT 251BF & 231GF IAW EMB SWPM 20-21-00. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — MISINSTALLED (FLASHLIGHT) · airframe 27,190 hrs · 23,245 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT AFT CLOSET FLASHLIGHT NOT CHARGIING. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND WIRES FOR THE FLASHLIGHT HOOKED UP BACKWARDS. RECONNECTED WIRES CORRECTLY IAW AMM 33-50-16. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRIP — CRACKED (CABIN) · airframe 27,190 hrs · 23,245 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT NR 7 & 8 EMERGENCY FLOOR PROXIMITY STRIPS CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 7 & 8 EMERGENCY FLOOR PROXIMITY STRIPS IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 27,173 hrs · 23,232 cycles

REAR FUSELAGE SKIN HAS A CRACK APPROX .2500" LONG AT FRAME 75, STR 2L. REPAIRED CRACK AT FR75, STR 2L IAW EO EM-53MR-2062.

Part: ANGLE — CRACKED (STAB TO FUSELAGE) · airframe 27,173 hrs · 23,232 cycles

FWD LT VERTICAL STAB TO FUSELAGE ANGLE HAS A CRACK APPROX 1" LONG. RAR FWD LT VERT STAB TO FUSELAGE ANGLE IAW EO EM-53MR-2062.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 27,173 hrs · 23,232 cycles

REAR FUSELAGE SKIN HAS A CRACK APPROX .2500" LONG AT FRAME 75, S2R. REPAIRED SKIN IAW EO EM-53MR-2062, PART B.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,301 hrs · 22,388 cycles

FLIGHT 4293, CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 26,132 hrs · 22,226 cycles

FLIGHT 4298, CREW REPORTED FLASHLIGHT BEHIND THE CAPTAIN’S SEAT WAS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY AS PER MM 33-51-06. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — LEAKING (FUEL SYSTEM) · airframe 25,798 hrs · 21,891 cycles

FLIGHT 4074, THE CREW REPORTED DURING THE CLIMB, LIQUID (FUEL) STREAMING FROM LEFT WING. CREW ELECTED TO DIVERT AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ON THE GROUND, FUEL WAS FOUND ON THE UNDERSIDE OF WING NEAR BOTH FUEL VENTS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAL AND FLAP VALVE AT RIB 19 IAW AMM 28-11-04. THE LEAK CHECKED WAS GOOD. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,762 hrs · 21,859 cycles

DURING MAINTENANCE INSPECTION, FOUND THE FOUND BATTERY PACKS DISCHARGED. SOME EMERGENCY LIGHTS WOULD NOT EXTINGUISH. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY PACKS IAW AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COVER — CRACKED (MAIN DOOR) · airframe 25,391 hrs · 21,533 cycles

DURING MAINTENANCE INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT COVER ASSEMBLY CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT COVER ASSEMBLY IAW EMB 140 AMM 25-23-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (FWD CABIN) · airframe 25,265 hrs · 21,422 cycles

DURING MAINTENANCE INSPECTION, FOUND THE FLIGHT ATTENDANT FORWARD FLASHLIGHT MISSING. AIRCRAFT REMOVED FROM SERVICE. INSTALLED FORWARD FLIGHT ATTTENDANT FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ADC — FAULTY (NR 1) · airframe 25,260 hrs · 21,419 cycles

ON FLIGHT 3975 THE CREW REPORTED THAT AT FLIGHT LEVEL 360 AUTO PRESSURE FAILED ON EICAS, O2 MASKS DEPLOYED AND USED. THE CREW DECLARED AN EMERGECNY AND DIVERTED TO STL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AIR DATA COMPUTER NR 1 AND NR 2 IAW EMB 140 34-15-01 SYS. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SREVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,807 hrs · 21,007 cycles

DURING PS-2 MAINTENANCE CHECK FOUND THE EXTERIOR EMERGENCY AFT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT LEFT EXTERIOR EMERGENCY LAMP IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,290 hrs · 19,673 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FLOOR PROXIMITY LIGHTING STRIP HAD THE WIRE TERMINAL BOTTOM OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHTING STRIP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 22,835 hrs · 19,294 cycles

DURING MAINTENANCE BASE VISIT FOUND COCKPIT FUSELAGE CENTER WINDSHIELD CUTOUT STRUCTURE CRACKED .375 INCH BY THE NUT PLATE FOR COCKPIT HANDLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED COCKPIT FUSELAGE CENTER WINDSHIELD CUTOUT STRUCTURE IAW ETN EM-53-145. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 22,835 hrs · 19,294 cycles

DURING MAINTENANCE BASE VISIT FOUND CARGO DOOR TORSION BAR FORWARD BRACKET HAS .125 INCH CRACK ON THE FORWARD END WHERE IT ATTACHES TO FRAME 61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,835 hrs · 19,294 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 23 CRACKED BETWEEN STRINGER 15 RIGHT AND 16 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 IAW EO EM-53MR-1789. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,835 hrs · 19,294 cycles

DURING MAINTENANCE BASE VISIT FOUND "T" FITTING ON FRAME 66 FOR CARGO DOOR RAMP HAS .375 INCH CRACK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FITTING AS REQUIRED IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — FAILED (COCKPIT) · airframe 21,306 hrs · 18,044 cycles

ON FLIGHT 3286 THE CREW REPORTED A FLAP FAIL ON APPROACH AND DECLARED AN EMERGENCY. A ZERO FLAP LANDING WAS PERFORMED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. THE EICAS MESSAGE DID NOT RETURN, WORK DONE IAW AMM 27-53-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,527 hrs · 18,198 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT ON THE FRAME TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT ON THE FRAME IAW EMB AMM 33-50-000-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — FAILED (NR 1) · airframe 21,215 hrs · 17,987 cycles

ON FLIGHT 2758 THE CREW EXPERIENCED AN UNCOMMANDED ENGINE SHUTDOWN IN FLIGHT DURING CLIMB THROUGH TO FLIGHT LEVEL 277. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO DIVERT TO AEX. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 1 ENGINE IAW AEA WC 71-000-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 19,621 hrs · 16,605 cycles

DURING 3A PHASE CHECK FOUND THE EMERGENCY LIGHT AT THE SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB AT THE SERVICE DOOR. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,362 hrs · 16,375 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT’S AFT FLASHLIGHT TO BE DIM. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT’S AFT FLASHLIGHT BATTERY. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A PS CHECK, MAINTENANCE FOUND SERVICED DOOR LOWER EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LOWER SERVICED DOOR EMERGENCY LIGHT IAW 33-50-09. OPERATIONAL CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,330 hrs · 15,549 cycles

DURING MBV INSP, FOUND FWD DIGITAL TO BE CORRODED AROUND A NUTPLATE HOLE. REPAIRED DIGITAL IAW EO EM-53MR-1283. ACFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,330 hrs · 15,549 cycles

DURING HMBV FOUND LT OMEGA BEAM CORRODED BETWEEN FRAMES 26-27. REPAIRED LT OMEGA BEAM BETWEEN FRAMES 26 AND 27 IAW SRM 53-00-10 FIGURE 202 SHEET 2. ACFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,330 hrs · 15,549 cycles

DURING HMBV FOUND CTR OMEGA BEAM CORRODED BETWEEN FRAME 26 AND 27. REPAIRED CENTER OMEGA BEAM BETWEEN FRAME 26 AND 27 IAW SRM 53-00-10 ACFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,330 hrs · 15,549 cycles

DURING HMBV INSPECTION FOUND LT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25. REPAIRED OMEGA BEAM IAW SRM 53-00-10. ACFT WAS RETURNED TO SERVICE..

Part: SWITCH — FAILED (FUEL QTY INDI)

AT CRUISE CREW REPORTED TANK 1 FUEL QUANTITY WENT FROM DASHES TO 0 IN FLIGHT. CREW DECLARED FUEL EMERGENCY TO GET PRIORITY HANDLING. ACFT REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING IN REF TO FIM 27-43-0-810-802-A REMOVED AND REPLACED BACK UP SYSTEM CUT OUT SWITCH. OPS CHECK GOOD IAW AMM 27-40-00. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (K)

Part: VALVE — FAILED (BRAKES)

ON FLIGHT 4600 CREW REPORTED UPON TOUCHDOWN ALL FOUR BRAKES LOCKED AND ALL FOUR TIRES BLEW OUT. THE WHEEL RIMS WERE GROUND AWAY AND CAUSED A LOT OF SPARKS AND FLAMES. THE TOWER CALLED CRASH, FIRE RESCUE AND REPORTED AN ACFT FIRE. THE PASSENGERS PERFORMED AN EMERGENCY EVACUATION ON THE ACTIVE RUNWAY. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED FOUR MAIN LANDING GEAR TIRES AND BRAKE ASSEMBLIES. REMOVED AND REPLACED BRAKE VALVE. ACCOMPLISHED HIGH DRAG AND SIDE LOAD INSPECTIONS, PERFORMED FUNCTIONAL CHECKS OF MAIN BRAKE AND FREE FALL SYSTEM. FUNCTIONAL CHECKS GOOD. RE-INSTALLED RT AND LT EMERGENCY EXIT DOORS AND RESET CIRCUIT BREAKERS. ACFT RETURNED TO SERVICE. (S)

Part: WIRE HARNESS — CORRODED (MLG) · airframe 15,336 hrs · 13,162 cycles

ON FLIGHT 3823, CREW REPORTED AT CRUSE AT FL360 A LOUD BANG WAS FELT AND HEARD, APPROX 5 MIN LATER ANOTHER BANG FELT AND HEARD FOLLOWED BY LOUD BUFFETING FELT THROUGHOUT AIRCRAFT. NOISE AND VIBRATION CEASED ON DESCENT THROUGH FL320 NOISE AND BUFFET FELT LIKE NOSE LANDING GEAR DOORS HAD OPENED AT LEAST PARTIALLY BUT NO EICAS. AIRCRAFT REMOVED FROM SERVICE. WHILE PERFORMING TROUBLESHOOTING, FOUND NOSE LANDING GEAR RIGHT DOWN LOCK PROX SENSOR HARNESS NOT LOCKING PROPERLY ONTO PROX SENSOR AND FOUND CORROSION IN CONNECTOR. REMOVED AND REPLACED HARNESS ASSEMBLY AND PROX SENSOR IAW EMB 140 AMM 32-00-03. PERFORMED OPERATIONAL CHECK GOOD OF LANDING GEAR. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN)

DURING PREFLIGHT INSPECTION CREW FOUND THAT 3 LT AISLE EMERGENCY LIGHT STRIPS WERE INOPERATIVE. TIGHTENED LOOSE CONNECTION AT LIGHT STRIP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)

Part: CHANNEL — CORRODED

DURING INSPECTION, FOUND SERVICE DOOR CHANNEL HAS CORROSION AROUND NUT PLATES. REPLACED SERVICE DOOR CHANNEL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: DOUBLER — CORRODED (STA 22, 23)

DURING INSPECTION, FOUND FWD CABIN FLOOR DOUBLER HAS CORROSION AROUND NUT PLATES. INSTALLED NEW FORWARD CABIN FLOOR DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING INSPECTION, FOUND FWD CABIN FLOOR OMEGA SHAPE HAS CORROSION AT FRAME 20. INSTALLED NEW DOUBLER IAW SRM. AC WAS RETURNED TO SERVICE. (K)

Part: STRUCTURE — CHAFED

DURING INSPECTION, FOUND STRINGER 19 LT CHAFED BETWEEN FRAMES 52, 53. REPLACED DAMAGED STRINGER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: SILL — CORRODED

DURING INSPECTION, FOUND FORWARD CABIN SILL LT HAS SMALL AREA OF CORROSION ON UPPER FORWARD SIDE. REMOVED AND REPLACED LT SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING AN MBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT A 4 INCH SECTION OF DAMAGE FLOORBEAM AND TREATED THE BARE METAL. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21, CHAPTERS 53-21-10 FIGURE 201 SHEET 1. (M)

Part: STRINGER — CHAFED (FUSELAGE)

DURING AN MBV INSPECTION, FOUND STRINGER 19L CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED AN NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21, CHAPTER 53-24-01 FIGURE 201. (M)

Part: SWITCH — FAILED (YOKE)

CLE - FLT 4248 - DURING CRUISE FLIGHT, A GUST LOCK FAIL WARNING. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS DIVERTED TO CLE. MAINTENANCE REMOVED AND REPLACED THE CONTROL YOKE POSITION SWITCH AND ADJUSTED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FAN — INOPERATIVE (CARGO BAY)

DFW - FLT 3477 - DURING CLIMB, CREW REPORTED THE CARGO SMOKE LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY AND BLEW BOTTLES. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE FOUND THE VENTALATION FAN TO BE INOPERATIVE. FAN WAS REMOVED AND REPLACED IAW EMB MM OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISLODGED (CABIN)

CLE - FLT 4334 - DURING PREFLIGHT CRWE REPORTED, THE FORWARD EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE FOUND THE FORWARD BATTERY PACK TO BE DISLODGED. THE SAME BATTERY PACK WAS REINSTALLED IAW THE EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)