N601DW

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 46,848 hrs · 40,506 cycles

BLEED 1 VALVE CLOSED ADVISORY DISPLAYED AFTER T/O WITH VERY LOW BLEED TEPERATURE. RAN ENGINE 1 ON GROUND AT DIFFERENT THRUST SETTINGS AND PERFORMED ENG BLEED VALVE OPERATIONAL CHECK IAW AMM 36-11-05. NO ISSUES NOTED. OKAY FOR SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,340 hrs · 39,921 cycles

FLOOR EMERGENCY LIGHTS INOPERATIVE AT THE EMERGENCY EXIT. R & R THE INVERTER IAW AMM 33-50-11.

Part: FAN — FAILED · airframe 46,312 hrs · 39,883 cycles

BOTH BLEEDS OVERTEMP WARNINGS AT 16K, AFTER ICE PROTECTION HAD BEEN ON FOR 5 MINUTES. APU WAS NOT ON. REMOVED AND REPLACED THE NR 1 & 2 THERMOSTAT FAN A/C AND THERMOSTAT MOUNT TUB ASSY IAW SB 145-36-0028.

Part: TUBE — FAILED (BLEED SYSTEM) · airframe 46,290 hrs · 39,854 cycles

BLEED 1 LEAK EICAS MESSAGE DISPLAYED DURING CLIMBOUT. REMOVED AND REPLACED THE TUBES IAW AMM 36-13-00. PERFORMED A BLEED AIR LEAK CHECK IAW AMM 36-00-00. PERFOMED AN EBV FUNCTIONAL CHECK IAW AMM 36-11-05. LEAK AND OPS CHECKED GOOD. OK FOR SERVICE.

Part: INDICATOR — MALFUNCTIONED (ALTIMETER) · airframe 46,131 hrs · 39,673 cycles

DURING CRUISE ALTITUDE, THE STBY ALTIMETER WAS INDICATING 1800 FEET LOWER THAN ADC AND THE STBY AIRSPEED INDICATOR WAS 25 KNOTS SLOWER THAN ADC. R & R THE STANDBY ALTIMETER IAW AMM 34-11-01. OPS CHECKED GOOD.

Part: LANDING GEAR — UNKNOWN (NOSE) · airframe 45,999 hrs · 39,530 cycles

AT WHEELS UP, TWO LOUD THUMPING NOISES WERE HEARD COMING FROM NOSE AREA, ALONG WITH A HISSING SOUND. NO ABNORMAL INDICATIONS NOTED. EVALUATION FLIGHT SATISFACTORY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,975 hrs · 39,507 cycles

OVERHEAD EMERGENCY LIGHT AT THE PAX DOOR WAS FOUND INOPERATIVE. R & R THE BULB.

Part: BRAKE — LEAKING (MLG) · airframe 45,308 hrs · 38,827 cycles

LEFT BRAKES APPEAR TO BE SMOKING ON LANDING. NR 2 HYD QTY APPEARED TO BE DROPPING. FOUND THE LEFT MAIN BRAKE INBD LEAKING WHEN HYD PRESSURE IS APPLIED. R & R THE MAIN BRAKE ASSY IAW AMM 32-49-03. OPS CHECKED GOOD, OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 2 PITOT) · airframe 44,935 hrs · 385,419 cycles

DURING NR 2 ENGINE START, NR 2 PITOT INOPERATIVE CAUTION MESSAGE CAME INTO VIEW. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (ENGINE) · airframe 44,932 hrs · 38,414 cycles

LOW PRESSURE COMPRESSION INDICATION AT HIGHEST POINT IN THE YELLOW RANGE. CLEANED THE FADEC 1A & 1B CONNECTORS IAW MM 70-00-00, RAN ACFT, NO DEFECTS NOTED.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 44,710 hrs · 38,182 cycles

FIRST OFFICER`S ALTITUDE INDICATION MISSING ON PFD. TURNED OFF AVIONCIS AND PDU FOR 15 MIN. OPS CHECKED GOOD.

Part: RIB — CRACKED (LT WING) · airframe 44,303 hrs · 37,761 cycles

LT WING RIB 5 CRACKED. REPLACED LT RIB 5 IAW ERS EO EM-57MR-764.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,303 hrs · 37,761 cycles

FRAME 60 -61 PROTRUSION AT STRINGER 17L. ACCOMPLISHED REPAIR TO FRAME 60 - 61 AT STRINGER 17L IAW ERS-EM-53MR-2555.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 44,303 hrs · 37,761 cycles

VERTICAL STAB LT DRAG ANGLE CRACKED AFT OF FR 75 PREVIOUS REPAIR. PERFORMED PERMANENT REPAIR OF VERTICAL STAB LT DRAG ANGLE AFT OF FR 75 IAW SRM 51-40-02.

Part: FRAME — GOUGED (FUSELAGE) · airframe 44,303 hrs · 37,761 cycles

FRAME 65 PREVIOUS REPAIR GOUGED BTW STR 12R - 13R. PERFORMED PERMANENT REPAIR ON FR 65 BTW STR 12R-13R IAW ERS-EM-53MR-2545.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,303 hrs · 37,761 cycles

LT FLOORBEAM WEB CORRODED AT CENTER AISLE CROSSMEMBER AT FR 29. PERFORMED PERMANENT REPAIR OF CENTER AISLE CROSSMEMBER AT FR 29 IAW ERS-EM-53MR-2552

Part: SKIN — CANNING (FUSELAGE) · airframe 44,303 hrs · 37,761 cycles

FUSELAGE SKIN HAS PROTRUSION AND OIL CANNING BETWEEN FRAMES 7 AND 8 STR 13L - 15L. PERFORMED PERMANENT REPAIR OF FR 7-8 STR 13L-15L IAW ERS-EM-53MR-2522.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,303 hrs · 37,761 cycles

LT FLOORBEAM WEB CORRODED AT CENTER AISLE CROSSMEMBER AT FR 38. PERFORMED PERMANENT REPAIR OF CENTER AISLE CROSSMEMBER AT FR 38 IAW SRM 53-00-10 ITEM 3 FIG 202 SHEET 1.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 44,253 hrs · 37,727 cycles

EMERGENCY LIGHT ABOVE SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED THE INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 44,131 hrs · 37,622 cycles

CABIN FLASHLIGHT HAS NO RED CHARGE LIGHT. REMOVED AND REPLACED CABIN FLASH LIGHT IAW STANDARD MTX PRACTICES.

Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKES) · airframe 43,472 hrs · 37,031 cycles

ON PUTTING GEAR DOWN FOR FINAL APPROACH, EICAS MESSAGE BRAKE DEGRADE. WENT AROUND DID AOM1 CHECKLIST. DECLARED EMERGENCY AND LANDED WITHOUT INCINDENT. PERFORMED MAIN BRAKE FUNCTIONAL CHECK IAW AMM 32-41-00. FNC FAILED AT STEP J.2.H. CONTINUED FROM AMM 32-41-00. STEP J2H, PASS FNC OF MAIN BRAKE SYSTEM. UTILIZE BRAKE FIELD ANALYZER IAW 32-41-00. NO FAULT NOTED. PERFORM HIGH SPD TAXI WITH FLT CREW. NO MESSAGE NOTED.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 43,271 hrs · 36,861 cycles

EMERGENCY LIGHT IN THE SERVICE DOOR INOPERATIVE. REPAIRED WIRE FOR SERVICE DOOR AT SPLICE SP7376 IAW SWPM 20-21-00, EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-50-00.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 42,811 hrs · 36,440 cycles

FIRST OFFICERS FLASHLIGHT NOT SECURE TO FLASHLIGHT BASE. R & R FIRST OFFICERS FLASHLIGHT BASE IAW AMM 33-50-16.

Part: HYDRAULIC LINE — CRACKED (HYDRAULIC SYS) · airframe 42,577 hrs · 36,209 cycles

EMERGENCY HYD BRAKE LINE, UNDER COCKPIT FLOOR CRACKED & LEAKING. REPAIRED EMER HYD BRAKE LINE IAW AMM 20-10-03. LEAK & OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 42,502 hrs · 36,132 cycles

FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER IS BROKEN & DOES NOT HOLD FLASHLIGHT PROPERLY. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16, NO DEFECT NOTED.

Part: CRADLE — INOPERATIVE (AFT FLASHLIGHT) · airframe 42,399 hrs · 36,040 cycles

AFT FLASHLIGHT INOPERATIVE. CHANGE FLASHLIGHT HOLDER.

Part: SPLICE — DEFECTIVE (CABIN) · airframe 42,150 hrs · 35,809 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. R & R REMOVABLE SPLICE AT SERVICE DOOR EMER EXTERNAL LIGHT IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER) · airframe 41,591 hrs · 35,284 cycles

YAW DAMP FAIL. R & R RUDDER SYS 2 PRESS SWITCH IAW AMM 27-23-04. PERFORMED LEAK CHECK, LEAK CHECKED GOOD. PERFORMED OPERATIONS CHECK RUDDER SYS 2 IAW AMM 27-263-00. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 41,544 hrs · 35,247 cycles

CAPTAINS FLASHLIGHT NOT CHARGING. R & R CAPTAINS FLASHLIGHT IAW AMM 33-50-16. 0PERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 40,837 hrs · 34,588 cycles

MULTIPLE CABIN EMER LIGHTS INOPERATIVE. SUSPECT PROBLEM WITH EPSU NR 3. R & R NR 3 EMER LIGHT BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 40,831 hrs · 34,582 cycles

COCKPIT STEP EMER LIGHT INOPERATIVE. R & R EMER LIGHT DC & AC INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,767 hrs · 34,527 cycles

EMERGENCY LIGHT STRIP ON FLOOR BY 6A INOPERATIVE. R & R EMER LIGHT STRIP BY 6A IAW AMM 33-50-12. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 40,741 hrs · 34,506 cycles

FIRST OFFICERS FLASHLIGHT INOPERATIVE. TROUBLE SHOT FIRST OFFICERS FLASHLIGHT, FOUND LAMP BURNED OUT. R & R LAMP IAW CMM 25-60-11.

Part: BATTERY — DISCHARGED (CABIN) · airframe 40,699 hrs · 34,463 cycles

1/2 OF EMER LIGHTING NOT WORKING. R & R NR 4 EMER BATTERY ASSEMBLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 40,466 hrs · 34,267 cycles

ESCAPE PATH EMER LIGHTING ON LT SIDE ROWS 7 - 15 OTS. R & R NR 4 AC TO DC INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,349 hrs · 34,170 cycles

CABIN NR 5 FLOOR PROXIMITY STRIP LIGHT INOPERATIVE. R & R CABIN NR 5 FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: SLEEVE — BLOWN (AC BAY) · airframe 40,330 hrs · 34,150 cycles

WHILE RUNNING PROCEDURES FOR ITEM NR 1, RECEIVED PACK 2 OVLD, FOLLOWED BY BURNING SMELL. FOUND BLOWN SLEEVE FWD OF D C V CAUSING BURNING SMELL. R & R SLEEVE AMM 21-60-01. LEAK CHECK & OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CLAMP — FAILED (NR 1 A/C PACK) · airframe 40,329 hrs · 34,149 cycles

DURING CLIMB CREW RECEIVED PACK 1 OVLD MSG FOLLOWED BY PACK 1 OVLD MSG. CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMER & RETURNED WITHOUT INCIDENT. FOUND BROKEN CLAMP AT PACK 1 VALVE. R & R CLAMP IAW AMM 21-51-01. LEAK & OPS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,068 hrs · 33,941 cycles

FRAME 75 SKIN AT FASTENER AREA CRACKED ABOVE STRINGER 2R. ACCOMPLISHED FRAME 75 ABOVE STRINGER 2R SKIN REPAIR IAW ERS-EM-53MR-984.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,068 hrs · 33,941 cycles

FRAME 75 FASTENER SKIN AREA CRACKED BELOW STRINGER 2L. ACCOMPLISHED FRAME 75 BELOW STRINGER 2L SKIN REPAIR IAW ERS-EM-53MR-984.

Part: SPAR — CRACKED (LT WING) · airframe 40,068 hrs · 33,941 cycles

CRACK ON LT WING SPAR III AT HOLE FOR MLG HARNESS AT APPROX THE 7 O'CLOCK POSITION BETWEEN RIBS 3 & 4. ACCOMPLISHED REPAIR ON LT WING SPAR III AT HOLE FOR MLG HARNESS IAW ERS-EM-57MR-349. FOUND DURING EO-EM-5700-662.

Part: SPAR — CRACKED (RT WING) · airframe 40,068 hrs · 33,941 cycles

CRACK ON RT WING SPAR III AT HOLE FOR MLG HARNESS AT APPROX THE 4 O'CLOCK POSITION BETWEEN RIBS 3 & 4. ACCOMPLISHED REPAIR ON RT WING SPAR III AT HOLE FOR MLG HARNESS IAW ERS-EM-57MR-350. FOUND DURING EO-EM-5700-662.

Part: CONNECTOR — MISSING (CABIN) · airframe 40,065 hrs · 33,940 cycles

WIRE FOR FLOOR PROXIMITY LIGHT STRIP NR 8 IS MISSING CONNECTOR WHERE IT PASSES THRU THE FLOORBOARD. INSTALLED CONNECTOR TO NR 8 PROXIMITY LIGHT STRIP IAW SWPM 20-21-00. FOUND DURING OPEN UP.

Part: SUPPORT — CRACKED (ENGINE MOUNT) · airframe 40,065 hrs · 33,940 cycles

LEFT PYLON FWD LOWER YOKE FWD ENG MOUNT SUPPORT IS CRACKED. ACCOMPLISHED REPAIR TO LT PYLON FWD LOWER YOKE FWD ENG MOUNT SUPPORT IAW EO-EM-54MR-386 PART A.

Part: CONNECTOR — MISSING (CABIN) · airframe 40,065 hrs · 33,940 cycles

WIRE FOR FLOOR PROXIMITY LIGHT STRIP NR 4 IS MISSING CONNECTOR WHERE IT PASSES THRU THE FLOORBOARD. INSTALLED CONNECTOR TO NR 4 PROXIMITY LIGHT STRIP IAW SWPM 20-21-0. FOUND DURING OPEN UP.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 40,065 hrs · 33,940 cycles

SERVICE DOOR FRAME CORRODED BELOW AFT LOWER ROLLER. PERFORMED SERVICE DOOR FRAME CORROSION REPAIR IAW ERS EM -53MR-971.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,040 hrs · 33,918 cycles

LAVATORY CTR OMEGA BEAM HAS MULTIPLE CORRODED AREAS. REPAIRED LAVATORY CTR BEAM AT AFFECTED RIVET HOLE, 2.4 INCHES FWD OF FRAME 60 IAW ERS-EM-53MR-963.

Part: SUPPORT — CRACKED (ENGINE MOUNT) · airframe 40,040 hrs · 33,918 cycles

LEFT PYLON FWD LOWER YOKE FWD ENG MOUNT SUPPORT IS CRACKED. ACCOMPLISHED REPAIR TO LT PYLON FWD LOWER YOKE FWD ENG MOUNT SUPPORT IAW EO-EM-54MR-386 PART A.

Part: SPAR — CRACKED (LT WING) · airframe 40,040 hrs · 33,918 cycles

CRACK ON LT WING SPAR III AT HOLE FOR MLG HARNESS AT APPROX THE 7 O'CLOCK POSITION BETWEEN RIBS 3 & 4. ACCOMPLISHED REPAIR ON LT WING SPAR III AT HOLE FOR MLG HARNESS IAW ERS-EM-57MR-349.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,040 hrs · 33,918 cycles

FRAME 75 FASTENER SKIN AREA CRACKED BELOW STRINGER 2L. ACCOMPLISHED FRAME 75 BELOW STRINGER 2L SKIN REPAIR IAW ERS-EM-53MR-984.

Part: TRUNNION — CRACKED (LT MLG) · airframe 40,040 hrs · 33,918 cycles

LEFT MLG AFT UPPER TRUNNION OTBD LOWER MOUNT FLANGE HAS CRACK INDICATION. R & R LT MLG AFT UPPER TRUNNION IAW ERS-EM-5700-344. SEE TURN OVER FOR DETAILS.

Part: SPAR — CRACKED (RT WING) · airframe 40,040 hrs · 33,918 cycles

CRACK ON RT WING SPAR III AT HOLE FOR MLG HARNESS AT APPROX THE 4 O'CLOCK POSITION BETWEEN RIBS 3 & 4. ACCOMPLISHED REPAIR ON RT WING SPAR III AT HOLE FOR MLG HARNESS IAW ERS-EM-57MR-350.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,040 hrs · 33,918 cycles

FRAME 75 SKIN AT FASTENER AREA CRACKED ABOVE STRINGER 2R. ACCOMPLISHED FRAME 75 ABOVE STRINGER 2R SKIN REPAIR IAW ERS-EM-53MR-984.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 39,947 hrs · 33,841 cycles

CAPTAINS FLASHLIGHT SWITCH BROKEN. REPLACED IAW AMM-33-51-01.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 39,012 hrs · 33,031 cycles

FLIGHT ATTENDANT INFORMED CAPTAIN & MX THAT THE MAIN CABIN DOOR IS DIFFICULT TO OPERATE. PERFORM ADJUSTMENT OF PAX MAIN DOOR, IAW AMM 52-18-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,960 hrs · 32,985 cycles

EMERGENCY FLOOR LIGHTING STRIP 3RD FROM FRONT FOUND INOPERATIVE. R & R EMER FLOOR LIGHTING STRIP 3RD FROM FRONT IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 38,208 hrs · 32,310 cycles

CAPTAIN`S FLASHLIGHT HOLDER WILL NOT CHARGE FLASHLIGHT. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: SENSOR — FAILED (NR 2 ENGINE) · airframe 38,162 hrs · 32,272 cycles

AT 190 IN CRUISE VIB HP NR 2 JUMPED INTO YELLOW RANGE. REDUCED THRUST TO IDLE & ARROW RETURNED TO GREEN. HOWEVER EVEN WITH THRUST LEVER IN IDLE ARROW INTERMITTENTLY WENT OUT OF LIMITS. UPON INITIAL DESCENT ARROW PEGGED FULL OUT OF LIMITS AT THAT TIME PERFORMED A PRECAUTIONARY SHUTDOWN. R & R ENG NR 2 HP COMPRESSOR VIBRATION SENSOR IAW RR MM 77-41-10. OPERATIONAL CHECK OK.

Part: DUCT — CRACKED (RT BLEED) · airframe 37,373 hrs · 31,672 cycles

RIGHT BLEED DUCT FLANGE CRACKED. R & R BLEED DUCT, OPS CHECKED GOOD IAW AMM 36-11-09.

Part: CONTROLLER — FAILED (WINDSHIELD HEAT) · airframe 37,108 hrs · 31,428 cycles

EICAS MESSAGE "W/S 2 HEAT FAIL" RESET IAW AMM AOM, VOL 1 BUT IT FAILED AGAIN. ODOR SIMILAR TO SOMETHING GETTING WARM/HOT WAS DETECTED. THAT WENT AWAY WITH W/S 2 OFF. R & R NR 2 WINDSHIELD TEMP CONTROLLER IAW AMM 30-42-01. OP'S CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: STEERING SYS — FAILED · airframe 36,620 hrs · 31,006 cycles

LANDED, AT A HIGH SPEED TURNOFF ACFT SWERVED AND NOSE STEERING WENT INOPERATIVE . UNABLE TO RE-ENGAGE NOSE STEERING . TAXIED CLEAR OF RUNWAYS WITH DIFFERENCIAL THRUST. INSPECTED NLG ASSY AND PERFORMED ACFT TAXING AMM 9-20-00. NO EICAS MSG AT THIS TIME. ACFT OK FOR SERVICE.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 36,020 hrs · 30,543 cycles

ON FLIGHT 2850 THE CREW REPORTED THE MAIN PASSENGER DOOR WOULD NOT OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DEBRIS AND CYCLED DOOR SEVERAL TIMES. NO DEFECTS NOTED AMM1 52-10-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,938 hrs · 30,475 cycles

DURING MAINTENANCE INSPECTION FOUND MAIN DOOR EMERGENCY LIGHT INOPERABLE. C/W REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-06-000-802-A AND 33-50-06-400-802-A, OPERATION CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE.

Part: TRUNNION — CRACKED (RT WING) · airframe 35,455 hrs · 30,085 cycles

DURING MAINTENANCE INSPECTION WHILE DOING INSTALLATION OF THE RIGHT WING RIB 5QC FOUND THE RIGHT MAIN LANDING GEAR AFT TRUNNION CRACKED AT HI-LOK HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION. REMOVED AND REPLACED THE RIGHT AFT TRUNNION IAW EO EM-57MR-671. THE AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF THE HMBV CHECK.

Part: FRAME — GOUGED (FUSELAGE) · airframe 35,455 hrs · 30,085 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 70 GOUGED AT STRINGER 13 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-2075. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 35,455 hrs · 30,085 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 65 GOUGED AT STRINGER 13 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-2077. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 35,455 hrs · 30,085 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT WING RIB 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WING RIB 5 IAW EO EM-57MR-595. THE AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF THE HMBV CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 35,472 hrs · 30,099 cycles

DURING B INSPECTION FOUND THE 2EA PROX LIGHTS HAVE BROKEN WIRES AT PROX LIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE 2EA PROX LIGHTS IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (CARGO DOORWAY) · airframe 35,455 hrs · 30,085 cycles

CARGO DOOR CUT-OUT LOWER FWD SECTION CORRODED. REPAIRED CARGO DOOR CUT-OUT FWD SECTION IAW EO EM-53MR-1129.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,455 hrs · 30,085 cycles

DURING HEAVY CHECK, FOUND FUSELAGE INNER SKIN CORRODED BETWEEN FR 13-14, STR 20R-19R. PERFORMED PERMANENT REPAIR IAW EO-EM-53MR-2079.

Part: SILL — CORRODED (FUSELAGE) · airframe 35,472 hrs · 30,099 cycles

DURING MAINTENANCE INSEPCTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED INSTALLATION OF CARGO DOOR SILL AND RE-INSTALLED CARGO RAMP SUPPORT AT FR66 AND FR67 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 35,455 hrs · 30,085 cycles

FLIGHT 2910, CREW REPORTED AT 30,000 FT, HEARD A LOUD BANG. ALL INSTURMENT INDICATIONS NORMAL & A SMOOTH CRUISE CONDITION NOTED. UNABLE TO POSITIVELY IDENTIFY NOISE & SUSPECTED THAT A TIRE MAY HAVE BURST IN THE WHEEL WELL. DECLARED AN EMERGENCY & PERFORMED TIRE DAMAGE CHECKLIST. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED BOROSCOPE INSPECTION OF RT ENGINE COMPRESSOR FORWARD AND AFT SECTIONS AND OF RT ENGINE TURBINE SECTION IAW MM 72-50-00-200-801 NO ABNORMAL CONDITIONS NOTED. ACCOMPLISHED RT ENGINE PERFORMANCE RUNS IAW MM 72-00-00. PERFORMED RETRACTION & EXTENSION OF MLG IAW AMM 32-30-00. NO DEFECTS NOTED. ACCOMPLISHED RT ENGINE VIBRATION CHECK IAW MM 72-50-00, OPS CHECKED NORMAL. FDR DATA DOWNLOAD IAW 31-700-05. RT ENGINE FAN CASE ASSY HAS SCRATCHES & GOUGES FROM ELEVEN TO ABOUT ONE O'CLOCK POSITIONS I AREA C PERFORMED BLEND OF RT ENGINE FAN CASE IAW MM 72-25-30. AIRCRAFT RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 35,179 hrs · 29,877 cycles

ON FLIGHT 4368 THE CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT WOULD NOT HOLD CHARGE. REMOVED & REPLACED THE FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL TEST WAS GOOD. NO FURTHER DEFECTS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TUBE — DEFECTIVE (BLEED AIR SYS) · airframe 33,937 hrs · 28,896 cycles

ON FLIGHT 4197 THE CREW REPORTED THAT DURING CLIMB THROUGH 9000 FEET, RECEIVED A NR 1 ENGINE 1 BLEED LEAK MESSAGE ON EICAS. THE CREW PERFORMED THE EPC/AOM VOL 1 CHECK LIST AND DECLARED AN EMERGENCY. AFTER ACCOMPLISHING EMERGENCY CHECKLIST, THE LIGHT WENT OUT. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BLEED TUBE ASSEMBLY AT FR 69 IAW EMB-145 AMM 36-11-09. THE LEAK CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 33,638 hrs · 28,640 cycles

DURING MAINTENANCE INSPECTION, FOUND THE FORWARD CABIN EMERGENCY FLASHLIGHT ASSEMBLY HOLDER CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM TASK 33-50-16-000-801/33-50-16-400-801. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 32,964 hrs · 28,126 cycles

FLIGHT 2826, THE CREW REPORTED THE F/O’S FLASHLIGHT WAS INOPERATIVE, AIRCRAFT REMOVED FROM SERVICE. REPLACED FLASHLIGHT BATTERY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ROLL PIN — BROKEN (CAPTAIN SEAT) · airframe 31,494 hrs · 26,997 cycles

ON FLIGHT 4343 THE CREW REPORTED THAT ON THE START OF DESCENT THE CAPTAIN TRIED TO BRING HIS SEAT FORWARD INTO LANDING POSITION AND WAS UNABLE. THE CAPTAIN NOTICED THE RIGHT SIDE SEAT TRACK PIN WAS BROKEN. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TOWED TO THE GATE DUE TO THE CAPTAIN WAS NOT ABLE TO REACH THE RUDDER PEDALS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REINSTALLED ROLL PIN ON SEAT LOCK PIN IAW CMM 25-11-71. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LINKAGE — CRACKED (RT ENGINE) · airframe 30,609 hrs · 26,320 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT ENGINE FORWARD LOWER YOKE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE RIGHT ENGINE LOWER YOKE IAW EO EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,052 hrs · 25,125 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT FORWARD OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RECORDER — ODOR (COCKPIT FDA) · airframe 28,747 hrs · 24,880 cycles

ON FLT 3224 DURING CRUISE THE CREW REPORTED AT FLIGHT LEVEL 360 ENCOUNTERED A 10 SECOND DURATION OF SEVERE TURBULENCE. THE CREW ALSO NOTICED A BURNING ELECTRICAL ODOR AFTER THE TURBULENCE. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO DIVERT TO GGG. THE FLIGHT ATTENDANT AND 5 PASSENGERS WERE INJURED. THE FLIGHT ATTENDANT WAS UNABLE TO COMPLETE DUTIES. THE SEAT BELT SIGN WAS ON AND A PUBLIC ANNOUNCEMENT WAS MADE PRIOR TO ENTERING TURBULENCE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED SEVERE TURBULENCE OR BUFFETING CONDITION INSPECTION IAW W/C 05-200-03. PERFORMED DIGITAL FLIGHT DATA RECORDER DOWNLOAD W/C 31-700-05. R & R THE DIGITAL FLIGHT DATA RECORDER ASSEMBLY. OPS TESTED GOOD IAW AMM 31-31-00. R & R COCKPIT VOICE RECORDER IAW AMM 23-71-01. ALSO FOUND AVIONICS MASTER 2 PUSH BUTTON LAMPS TO ALL BE BURNED OUT. R & R LAMPS IAW AMM 20-13-04. THE OPERATIONAL CHECK WAS GOOD. THE SMOKE ODOR DID NOT RETURN DURING INSPECTION. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (BRAKE SYSTEM) · airframe 28,435 hrs · 24,648 cycles

FOR FLIGHT 2757 THE CAPTAIN REPORTED THAT AFTER LANDING DURING BRAKING THERE WAS AN AGGRESSIVE TO VIOLENT BRAKE GRABBING. REGARDLESS OF HOW SOFT THE BRAKES WERE APPLIED, THE BRAKES GRABBED HARD AND ERRATIC. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BRAKE CONTROL UNIT PER EMB MM 32-41-02. THE OPERATIONAL TAXI CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — ODOR · airframe 27,400 hrs · 23,823 cycles

AFTER LANDING THE CREW OF FLIGHT 3762 REPORTED A STRONG ELECTRICAL SMELL IN THE COCKPIT. AFTER ENGINE RUNS A STRONG OIL SMELL WAS PRESENT IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ENGINE RUN PER THE GROUND HANDLING CHECKLIST AND FOUND IT TO BE AN OIL BURNING SMELL. ACCOMPLISHED INTERNAL AND EXTERNAL OIL LEAKS PER RRMM 79-37-00. NO LEAKS NOTED. FOUND ENGINE TO BE CHANGED ON 12-18-09 AT CMH. SMELL WAS DETERMINED TO BE CAUSED BY ENGINE BREAK IN. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS OK’ED FOR SERVICE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CLAMP — DEFECTIVE (BLEED AIR SYS) · airframe 27,256 hrs · 23,699 cycles

ON FLIGHT 4113 THE CREW REPORTED ENCOUNTERED ICE ON CLIMBOUT AT 8000 FEET AND RECEIVED BLEED 1-2 LEAK WARNING ON EICAS. THE CREW ALSO REPORTED A FOUL SMELL IN THE COCKPIT AND CABIN. THE CREW ELECTED TO RETURN TO CHM AT A NORMAL DESCENT RATE. LANDING WEIGHT WAS OKAY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED GAMMA CLAMP LOCATED BETWEEN FRAMES 60 AND 70 IAW AMM 36-11-09. PERFORMED OPERATIONAL CHECK 36-00-00. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 26,680 hrs · 23,176 cycles

ON FLIGHT 3252 THE CREW REPORTED A STALL PROTECTION SYSTEM ADVANCED FLAP LOW SPEED EICAS MESSAGE PRESENT IN FLIGHT. EICAS INDICATED FLAPS AS AMBER BOX AND AMBER DASH. AMBER DASH FLAP INDICATIONS WERE ON BOTH DISPLAYS. AN EMERGENCY WAS DECLARED UPON ARRIVAL INTO DFW. AIRCRAFT LANDED WITH NO INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BLOWN FUSE F0098. REMOVED AND REPLACED LEFT FLAP DRIVE MOTOR UNIT. REMOVED AND REPLACED FLAT ELECTRONIC CONTROL UNIT. ALL WORK PERFORMED IAW EMB 145 AMM 20-13-08, 27-53-01 AND 27-53-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,457 hrs · 22,106 cycles

DURING IMBV, THE GALLEY FLOOR CENTER BEAM WAS FOUND CORRODED. REMOVED DAMAGED BEAM. PREPPED, CLEANED, ALODINED, PRIMED AND INSTALLED NEW BEAM IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,094 hrs · 21,180 cycles

ON FLIGHT 4481, MAINTENANCE REPORTED THE LEFT OVER WING EXIT MARKER AFT INOPERATIVE DURING A PS CHECK. REMOVED AND REPLACE INVERTER. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,633 hrs · 22,278 cycles

DURING IMBV THE GALLEY CENTER FLOORBEAM WAS FOUND CORRODED. REMOVED CORRODED FLOORBEAM, ALODINED AND PAINTED FASTENER HOLES AND INSTALLED NEW FLOORBEAM IAW EMB SRM 51-40-02 AND 51-40-03. ACFT RETURNED TO SERVICE.