N631AE

Part: UNKNOWN — ODOR (CABIN) · airframe 47,712 hrs · 45,176 cycles

ELECTRICAL SMELL IN CRUISE AND DESENT IN RAIN WITH W/S HEAT ON. OPS CHECKED W/S HEAT SYSTEM,WINDSHIELD WIPER SYSTEM, AND RAN APU AND PACKS PER AMM 20-42-00 AMM 21-00-00 AND AMM 30-41-00 RESPECTIVELY OPS CHECK OK NO FAULTS NOTED AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 48,828 hrs · 45,220 cycles

ABNORMAL SMELL AFTER TAKEOFF WITH PACK AND BLEED ON. R&R'D RECIRC FAN REF 21-24-011,OPS CHECK GOOD. R&R'D 3100 MUFFLER DUCT REF AMM21-24-02.CHANGED ALL 3 HEPA FILTERS REF PIEDMONT W/C 21-28-00 RAN AIRCRAFT OFF OF ENG #1 BLEED & #2 BLEED ON PACK #1 NO DEFECTS OR ODORS NOTED,GOOD FIX, OK FOR SERVICE. (BURNING BAGEL SMELL) AIRCRAFT IS CURRENTLY IN WORK AT MDT WILL UPDATE WHEN CLEARED

Part: ECS — ODOR (COCKPIT) · airframe 48,713 hrs · 45,107 cycles

PDIS 631 21-01 2533072 08APR21 ROA CLOSE AFTER TAKE OFF UPTO 6000FT WITH BOTH BLEEDS ON BURNT BAGEL SMELL IN COCKPIT. SMELL REAPPEARED ON SHORT FINAL FACT 08APR21 04:09 ROA BORESCOPED #1 ENG AND FOUND OIL ON BOLT HEADS IN THE FLOW PATH EXTENSION AREA. BORESCOPE #2 ENG, NO PROBLEMS FOUND. SEE HA-300 SEQ #1 FOR DMT TO R/R #1 ENGINE. ALL DONE IAW RR AMM 72-30-00-990-883.

Part: LOCALIZER — ERRATIC · airframe 48,473 hrs · 44,846 cycles

PDIS 631 34-32 2353451 13FEB21 MDT CLOSE LOCALIZER ERRATIC 12 MILES FROM CHO. GOT WORSE THE CLOSER TO RUNWAY 3. AUTO PILOT COUPLED TO CAPTS SIDE AND ISSUE PERSISTED WITH AUTO PILOT OFF FACT 14FEB21 00:10 MDT CHECKED #1 AND #2 NAV LOG SENS WITH NAV750B. #1 SHOWS -105 AND #2 SHOWS - 102. R&R #2 INTEG NAV REF PRIMUS II SR2 INTEG RADIO FOR SYSTEM SPECS AND C/WVOR/ILS, ADF, AND MB SYSTEM OP TESTS. REF EMB MM 34-32-01 OPS CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 48,273 hrs · 44,624 cycles

ONCE REACHING CRUISE CAPT NOTICED A BURNING SMELL FOR APPROXIMATELY 3 SECONDS, THEN DISSIPATED. ON ARRIVAL SMELL CAME BACK FOR APPROXIMATELY 10 SECONDS, THEN DISSIPATED. INSPECTED NR 1 AND 2 PACKS, LEFT AND RIGHT RELAYS PANELS, NO DEFECTS NOTED AT THIS TIME. RAN APU FOR 10 MINS, RAN BOTH ENGINES FOR 5 MINS, NO DEFECTS NOTED AT THIS TIME. UNABLE TO DUPLICATE THE NOTED DISCREPANCY. OPERATIONS CHECK GOOD. A/C OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 47,893 hrs · 44,193 cycles

HEAVY BURNING RUBBER ODOR IN FLT DECK DURING TAKE-OFF. ABORTED T/O. MAINTENANCE: PILOTS TAXIED TO RUNWAY 24 ROA AND REJECTED T/O AT 100 KTS. NO UNUSAUL SMELLS, SOUNDS, OR MSG'S OBSERVED. OK FOR SERVICE. INSP NWA, NO FAULTS FOUND AND OPS CHEECKED PACS, NO ABNORMAL SMELLS. OK FOR SERVICE AT THIS TIME.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 47,753 hrs · 44,034 cycles

DURING RON FOUND FLOOR LIGHTS AT ROW 7 TO 12 ARE INOP. RR NR 5 EMERGENCY LIGHT POWER INVERTER IAW 33-50-01. THIS SUPERSEDES PREVIOUS SDR REPORT. THE PREVIOUS SDR REPORT HAS A MISTAKE ON NATURE OF CONDITION COLUMN.

Part: UNKNOWN — UNKNOWN (AILERON) · airframe 47,382 hrs · 43,599 cycles

PDIS 631 27-11 2232271 17FEB20 MDT CLOSE ABOVE 250KNOTS A/C HAD SIGNIFICANT RIGHT ROLLING TENDENCY ALONG WITH MINIMAL ARTIFCIAL AILERON FEEDBACK. SLIGHT BANK INPUTS LED TO LARGE AIILERON BANK OUTPUT FACT 18FEB20 05:06 MDT PERFORMED OPS CHECK OF ARTIFICIAL FEEL UNIT IRT AMM 27-11-06-700-801 AND CHECKED AILERON DEFLECTION IRT AMM 27-10-00-700-801. ALL RIG PINS REMOVED. NO DEFECTS NOTED AT THIS TIME. PERFORMED EXTERNAL LEAK CHECK OF HYDRAULIC AILERON ACTUATORS IRT AMM 27-12-00-700-803A AND FUNCTION CHECKED IRT 27-12-01-700-801A. NO DEFECTS NOTED AT THIS TIME.

Part: INDICATOR — DEFECTIVE (COCKPIT) · airframe 46,528 hrs · 42,622 cycles

STAND-BY ATTITUDE INDICATOR NOT ERECT IN FLIGHT. FIX: R&RD STAND-BY ATTITUDE INDICATOR REF AMM 34-24-01. OPS CHECK GOOD IAW AMM 34-24-00. OK FOR SERVICE. NOTE: AIRCRAFT DIVERTED TO CLT FOR REPAIR.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 46,374 hrs · 42,446 cycles

CEILING EMERGENCY LIGHT AT ROW 12 DOES NOT ILLUMINATE. R & R THE CEILING EMERGENCY LIGHT BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,349 hrs · 42,418 cycles

RH AFT EXTERIOR EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE.... FIX: R&R D RH AFT EMERGENCY LIGHT,OPS CHCK GOOD IAW AMM TASK 33-50-10-000/400-801-A

Part: ACTUATOR — FAILED (NLG UPLOCK) · airframe 46,345 hrs · 42,414 cycles

NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. CYCLED PER QRH, NO CHANGE. RTF. INSPECTED CONNECTORS. NO DEFECTS NOTED. R & R THE NLG UNLOCK ACTUATOR IAW AMM 32-33-06. OPS & LEAK CHECKED GOOD, OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,058 hrs · 42,093 cycles

NDIS 631 33-51 0014870 23APR19 RIC CLOSE EMERGENCY LIGHT IN 12BC PSU INOP 27751 00 NGR FACT 23APR19 09:56 RIC R/R LIGHT LAMP IN PSU OVER SEATS 12BC IAW AMM 33-50-08-000-801-A/400-801-A P/N ON LAMP 1317 P/N OFF LAMP 1317

Part: WARNING MESSAGE — ILLUMINATED (ANTI ICE SYSTEM) · airframe 45,695 hrs · 41,683 cycles

PDIS 631 30-10 1867981 14FEB19 PHL ASSGN DURING A/I TEST IN FLIGHT, STAB A/I FAIL MSG APPEARED ON EICAS.

Part: RELAY — FAILED (STAB ANTI ICE) · airframe 45,691 hrs · 41,679 cycles

PDIS 631 30-10 1867972 13FEB19 PHL CLOSE STAB A/ICE FAIL MESSAGE APPEARED ON EICAS. RAN QRH B ROUGHT POWER LEVER UP INDICATION REMAINED ON. FACT 13FEB19 18:06 PHL FOLLOWED FIM TASK 30-12-00-810-803-A RNR K0552 RELAY AS REQUIRED GROUND RAN BOTH ENGINE WITH BLEEDS ON O PS CHECK PER AMM 30-80-00-700-801-A GOOD ON GROUND O K FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (HORIZONTAL STAB) · airframe 45,691 hrs · 41,679 cycles

PDIS 631 30-10 1867951 11FEB19 ALB CLOSE STAB ANTI ICE FAIL EICAS MESSAGE APPEARED DURING ANTI ICE PNEUMATIC TEST IN FLIGHT. FACT 11FEB19 02:59 ALB REMOVED AND REPLACED H-STAB ANTI-ICE VALVE IAW EMB145AMM 30-12-01. OPS CHECK GOOD . OK FOR SERVICE

Part: RELAY — MALFUNCTIONED (SPOILER) · airframe 42,848 hrs · 38,565 cycles

SPOILER FAIL EICAS MESSAGE DISPLAYED AFTER RETRACTION. EXTINGUISHED DURING TAXI. PERFORMED SPOILER OPS CHECK. NO DEFECTS NOTED. R & R THE RELAYS K0030 AND K0031 FOR POSITIVE MAINTENANCE ACTION. OPS CHECKED GOOD. OKAY FOR SERVICE IAW MM 27-63-01.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · airframe 42,819 hrs · 38,522 cycles

LEFT OMEGA BEAM IS CORRODED ON BOTTOM SIDE BELOW FRAME 59 CROSSMEMBER. ACCOMPLISHED A REPAIR IAW ERS.

Part: SKIN — DENTED (FRAMES 23-24) · airframe 42,819 hrs · 38,522 cycles

SKIN DENTED AFT OF FRAME 23 BETWEEN STRINGERS 9 - 10R. ACCOMPLISHED A REPAIR IAW ERS-EM-53MR-2796.

Part: FLOOR SUPPORT — CORRODED (FR 59) · airframe 42,814 hrs · 38,520 cycles

LEFT OMEGA BEAM IS CORRODED ON BOTTOM SIDE BELOW FRAME 59 CROSSMEMBER. ACCOMPLISHED A REPAIR IAW ERS-EM-53MR-2786.

Part: FLOOR SUPPORT — CORRODED (FRAMES 26-59) · airframe 42,814 hrs · 38,520 cycles

CENTER OMEGA BEAM IS CHAFED AND CORRODED BETWEEN FRAMES 26-59 ON SIDE WEB. ACCOMPLISHED A REPAIR IAW ERS-EM-53MR-2788.

Part: FLOOR SUPPORT — CORRODED (FRAME 38) · airframe 42,814 hrs · 38,520 cycles

CENTER OMEGA BEAM IS CORRODED AT FRAME 38. ACCOMPLISHED A REPAIR IAW SRM 53-00-10.

Part: FLOOR SUPPORT — CORRODED (FRAME 38) · airframe 42,814 hrs · 38,520 cycles

LEFT OMEGA BEAM IS CORRODED AT FRAME 38. ACCOMPLISHED A REPAIR IAW SRM 53-00-10.

Part: FLOOR SUPPORT — CORRODED (FRAMES 58-59) · airframe 42,814 hrs · 38,520 cycles

CENTER OMEGA BEAM IS CORRODED BETWEEN FRAMES 58-59. ACCOMPLISHED A REPAIR IAW ERS-EM-53MR-2784.

Part: FLOOR SUPPORT — CORRODED (FRAME 29) · airframe 42,814 hrs · 38,520 cycles

LEFT OMEGA BEAM IS CORRODED AT FRAME 29. INSTALLED A DOUBLER, FILLER, AND SHIMS ON THE OMEGA BEAM IAW SRM 53-00-10, AND 51-40-02.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 42,814 hrs · 38,520 cycles

CARGO DOOR SILL FOUND CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02, AND 51-20-03.

Part: FLOOR SUPPORT — CORRODED (FRAMES 33-34) · airframe 42,814 hrs · 38,520 cycles

CENTER OMEGA BEAM IS CORRODED BETWEEN FRAMES 33-34. REPAIRED CENTER OMEGA BEAM WITH A FABRICATED DOUBLER & FILLER IAW SRM 53-00-10, 51-00-10, AND 51-20-01.

Part: SHEAR TIE — CORRODED (CARGO DOOR) · airframe 42,814 hrs · 38,520 cycles

CARGO DOOR CUTOUT LATERAL L-SHAPE IS CORRODED AT PREVIOUSLY BLENDED AREA AT LWR CORNER OF CUTOUT. REPAIRED IAW SRM 53-31-04 , AND 51-40-02

Part: DOOR SILL — CORRODED (CABIN) · airframe 42,814 hrs · 38,520 cycles

SERVICE DOOR CENTER SILL IS CORRODED AT LOWER AFT CORNER. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02, SRM 51-20-03, AND SRM 51-40-09.

Part: YOKE — CRACKED (RT ENGINE) · airframe 42,814 hrs · 38,520 cycles

RIGHT ENGINE FWD LOWER YOKE IS CRACKED ON FWD SIDE. REPLACED THE FWD LOWER YOKE IAW EO EM-54MR-386.

Part: FLOOR SUPPORT — CORRODED (FRAME 29) · airframe 42,814 hrs · 38,520 cycles

CENTER OMEGA BEAM IS CORRODED AT FRAME 29. REMOVED CORROSION IAW SRM 51-10-03.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,897 hrs · 37,737 cycles

BOTH LT AND RT EMERGENCY LIGHTS UNDER OVERWING EXIT DOORS ARE INOPERATIVE. R & R THE NR 4 POWER SUPPLY AND BATTERY HOLDER ASSY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: BRAKE — OVERHEATED (NR 3) · airframe 41,703 hrs · 37,569 cycles

RIGHT BRAKE OVERHEAT INBD. REMOVED AND REPLACED THE NR 3 BRAKE ASSY IAW W/C 32-600-14.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 41,378 hrs · 37,232 cycles

RT OVERWING EMERGENCY LIGHT INOP. R&R RT OVERWING EMERGENCY LIGHT BULB, OPS GOOD IAW AMM 33-50-07.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 40,753 hrs · 36,644 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. PERFORMED MAIN CABIN DOOR LUBE IAW AMM 52-10-01. OPS CHECK GOOD.

Part: UNKNOWN — ODOR · airframe 40,252 hrs · 36,176 cycles

STRONG ELEC BURNING SMELL WITH NO SIGN OF SMOKE AFTER STARTING BOTH ENGS BEFORE TAXI. DEFERRED PACK ONE. PERFORMED OPERATIONS CHECK OF COOLING PACK SYS IAW AMM TASK 21-51-00-700-802-A. OPERATIONS CHECKED GOOD, PACK 1 SOUNDS, SMELLS & FUNCTIONS NORMALLY. MEL ITEM RESTORED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 39,099 hrs · 35,097 cycles

NUMBER 4 EMER LIGHT INVERTER INOPERATIVE. R & R NR 4 EMER LIGHT INVERTER IAW AMM 33-50-11. FOR OPERATIONS CHECK SEE BOW 202439.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,099 hrs · 35,097 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 & ABOVE STRINGER 2R. REPAIRED RT UPPER FUSELAGE SKIN IAW ERS-EM-53MR-1675.

Part: FRAME — GOUGED (FUSELAGE) · airframe 39,099 hrs · 35,097 cycles

FRAME 70 GOUGED, BETWEEN STRINGERS 11R - 12R. REPAIRED FRAME 70 IAW ERS-EM-53MR-1665.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,099 hrs · 35,097 cycles

LEFT UPPER FUSELAGE SKIN HAS 2 CRACKS AT FRAME 75 & ABOVE STRINGER 2L. REPAIRED LT UPPER FUSELAGE SKIN IAW ERS-EM-53MR-1676.

Part: MARKER — DETERIORATED (SERVICE DOOR) · airframe 39,099 hrs · 35,097 cycles

SERVICE DOOR FRAME LOCKING RED MARKS DETERIORATED. RESTORED SERVICE DOOR LOCKING RED MARKS TO THE TOP TWO FRAME STOPS IAW CPM 51-21-06, ETNS EM-51-109, GN-51-011R4, EM-51-075, EM-51-091R3 & GN-51-016R5.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 39,099 hrs · 35,097 cycles

CROSSBEAM AT FRAME 25 - 26 CORRODED. R & R CROSSBEAM, BETWEEN FRAME 25 - 26 IAW SRM 51-40-02 & ETN-EM-53-139 R4, SEE WIPS & TASK FOR DETAILS.

Part: DISPLAY — FAILED (COCKPIT) · airframe 38,365 hrs · 34,373 cycles

IN FLIGHT, CAPTAIN SIDE ALTIMETER RED X DISPLAYED. SELECTED REVERSIONARY ADC AS DIRECTED BY AOM VOL 1 PROCEDURE. REMOVED SMALL AMOUNT OF WATER FROM PITOT STATIC DRAIN VIA QUICK DISCONNECT IAW AMM 34-13-00. R & R NR 1 PFD BEZEL IAW AMM 34-22-02. OPERATIONS CHECKED GOOD IAW AMM 34-22-00 & 34-15-00.

Part: UPLOCK — FAILED (NLG) · airframe 37,715 hrs · 33,786 cycles

ON CLIMB OUT NOSE GEAR & GEAR DOOR WOULD NOT CLOSE UP. R & R NLG UPLOCK BOX IAW AMM 32-33-07. OPERATIONS & LEAK CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 37,366 hrs · 33,496 cycles

FIRST OFFICER`S FLASHLIGHT INOPERATIVE. R & R FIRST OFFICER`S FLASHLIGHT AS REQUESTED.

Part: TRUNNION — LACK OF LUBE (NLG) · airframe 37,274 hrs · 33,423 cycles

DURING TAKEOFF A LOUD RHYTHMIC THUMPING NOISE WAS HEARD DURING GEAR RETRACTION. A STRONG SMELL LIKE BURNING RUBBER OCCURRED AT THE SAME TIME. NO OTHER UNUSUAL INDICATIONS AFTER THAT. UPON LANDING POST FLIGHT INSPECTION FOUND THE LT MAIN STRUT AT LOW EXTENSION WITH ALMOST NO CHROME SHOWING. FOUND NLG TRUNIONS LACKING GREASE. LUBRICATED NLG IAW AMM 32-34-00. EXTENSION & RETRACTION CHECKS GOOD IAW AMM 32-30-00. IAW ITEM 3 LOG PG 3691568 FOR LT MAIN STRUT SERVICE, NO ODERS NOTED.

Part: SHUTOFF VALVE — FAILED (BRAKE SYSTEM) · airframe 37,123 hrs · 33,295 cycles

DURING LANDING ROLLOUT FELT LIKE PARTIAL LOSS OF BRAKING. AFTER EXITING THE RUNWAY RT OF BRAKE TEMP SPIKED INTO UPPER AMBER RANGE, LT OTBD LOWER AMBER, INBDS BOTH REMAINED AT THE BOTTOM OF THE GREEN RANGE. R & R THE BRAKE SOV IAW AMM 32-41-05. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 36,338 hrs · 32,551 cycles

LEFT AFT OVERWING EMER LIGHT FOUND INOPERATIVE IAW PS 2 INSPECTION. R & R LT AFT OVERWING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 36,080 hrs · 32,332 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R OF EMERGENCY LIGHT ASSEMBLY IAW TASK 33-50-09-000-802-A, A BROKEN WIRE WAS DISCOVERED, REPLACED FEMALE CONNECTOR & MALE PLASTIC COVER IAW WM 33-50-00. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKE SYS) · airframe 35,716 hrs · 31,989 cycles

AFTER TAKEOFF, RECEIVED A BRAKE DEGRADE MOMENTARILY ON EICAS & LT INBD BRAKE INDICATOR VANISHED AND BRAKE OVERHEAT SEVERAL MINUTES LATER. COMPLIED WITH AOM VOL I PROCEDURE FOR OVERHEAT & RETURN TO DEPARTURE. INBD INDICATOR NEVER RETURNED, ALL OTHER BRAKE INDICATORS GREEN. ACCOMPLISHED OPS CHECK OF BRAKE TEMP INDICATION SYSTEM IAW AMM 32-47-01-420-001-A00. OPS CHECKED GOOD.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 35,057 hrs · 31,475 cycles

DURING MBV INSPECTION ON ACFT 631AE QC FOUND FRAME 65 Z FRAME WITH SCREW DAMAGE BETWEEN STRINGERS 12R - 13R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON FRAME 65 Z FRAME BETWEEN STRINGERS 12R - 13R IAW ERS-EM-53MR-121. REPAIR DOUBLER AL2024T3 .050 INCHES.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,057 hrs · 31,475 cycles

DURING HMBV INSPECTION QC FOUND CORROSION BETWEEN FR 13 - 14, STRINGER 19R - 20R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. THE ACFT WAS REMOVED FROM SERVICE. CUT OUT DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW ERS-EM-53MR-080.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 35,057 hrs · 31,475 cycles

BACK LIGHTING AROUND EMERGENCY LIGHT SWITCH IS INOPERATIVE. R & R EMERGENCY LIGHT PANEL ILLUMINATED PLACARD ASSEMBLY IAW AMM 20-13-10, OPERATIONAL TEST GOOD.

Part: HANDLE — BINDING (MAIN CABIN DOOR) · airframe 34,735 hrs · 31,236 cycles

MAIN CABIN DOOR HANDLE BINDS HALF WAY THROUGH OPEN/LOCK CYCLE. PERFORMED OPEN AND CLOSED MAIN CABIN DOOR SEVERAL TIME NO DEFECTS OR NOISE IAW AMM 52-10-05.

Part: HANDLE — MALFUNCTIONED (PAX DOOR) · airframe 34,520 hrs · 31,060 cycles

F/A REPORTS MAIN DOOR HANDLE ROTATES TO CLOSED POSITION WHEN DOOR ABOUT HALF OF THE WAY TO FULL OPEN POSITION. LUBRICATED DOOR HANDLE MECHANISM. NO DEFECTS NOTED.

Part: FLASHLIGHT ASSY — INOPERATIVE (FO'S) · airframe 34,471 hrs · 31,021 cycles

F/O FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: LOCK — LACK OF LUBE (PAX DOOR) · airframe 34,148 hrs · 30,751 cycles

MAIN DOOR DIFFICULT TO OPEN. LUBRICATED MAIN DOOR LOCK MECHANISM IAW AMM 52-18-00.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 33,298 hrs · 30,065 cycles

DURING B INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT ON/OFF SWITCH BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IN REFERENCE WITH EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 33,262 hrs · 30,040 cycles

DURING PS-2 INSPECTION FOUND THE COCKPIT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT EMERGENCY LIGHT BULB IAW AMM 33-10-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 32,811 hrs · 32,811 cycles

DURING MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR DIFFICULT TO OPEN. FOUND FWD UPPER MAIN DOOR ROLLER TO BE OUT OF ADJUSTMENT, ADJUSTED IAW AMM 52-18-00-820-805-A. PERFORMED LOAD TEST OF MAIN PASSENGER DOOR FOUND TO OPEN WITH 30LB OF FORCE, CHECKED GOOD IAW AMM 52-18-00-820-801-A. AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 32,799 hrs · 29,655 cycles

ON FLIGHT 3959 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN PASSENGER DOOR ROLLERS PER AMM 52-18-00. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CLAMP — DEFECTIVE (BLEED AIR SYS)

ON FLIGHT 3973 THE CREW REPORTED THAT WHILE CLIMBING THROUGH 4000 FEET IN ICING CONDITIONS THEY RECEIVED A MASTER WARNING AND BLEED 1 LEAK MEASSAGE ON EICAS. THE CREW RAN THE CHECKLIST AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AFT CLAMP ON NR 1 ENGINE BLEED VALVE IAW EMB 145 AMM 36-11-05. PERFORMED BLEED SYSTEM OPS CHECK IAW AMM 36-00-00. THE OPERATIONAL CHECK AND LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CLAMP — DEFECTIVE (BLEED AIR SYS)

BLEED 1 LEAK. REMOVED AND REPLACED AFT CLAMP ON NR 1 ENGINE BLEED VALVE IAW EMB 145 AMM 36-11-05. PERFORMED BLEED SYSTEM OPS CHECK IAW AMM 36-00-00. OPS CHECK AND LEAK CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

SEAT 12A EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT LAMP AT SEAT 12A.

Part: FLAP — MALFUNCTIONED (WING) · airframe 31,736 hrs · 28,797 cycles

ON FLIGHT 3454 THE CREW REPORTED THAT DURING CLIMBOUT FROM MIA, RAISED FLAPS AND FLAPS STUCK AT 4 DEGREES. FLAPS WOULD NOT RETRACT, WOULD NOT LOWER. THE CREW REPORTED THE BEST COURSE OF ACTION WAS TO RETURN TO MIA AND DECLARED AN EMERGECNY DUE TO THE HIGH APPROACH SPEED. THE CREW REDUCED FLAP PROCEDURE PER AOM-1 (FLAP FAIL EICAS MSG). THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING IAW EMB 145 FIM 27-51-00, AND THE OPERATIONAL CHECK SYSTEM WORKED PROPERLY - STARTED FSA SERVICING PROCEDURE IAW EMB 145 W/C 27-600-03. FUNCTIONAL CHECK REQUIRED FOR FLAP FAIL WITH FLAP JAMMING AS PER ITEM NR 1 ON AML PAGE 3273332. THE AIRCRAFT WAS RELEASED FOR FUNCTIONAL CHECK FLIGHT PURPOSES ONLY. THE FUNCTIONAL CHECK FLIGHT WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,508 hrs · 28,631 cycles

DURING B INSPECTION, FOUND THE GALLEY SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY SERVICE DOOR EMERGENCY LIGHT IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. LIGHT STILL INOPERATIVE. FOUND BROKEN WIRE NR 799-8001-20, REPAIRED WIRE IAW AMM 20-21-00. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 30,693 hrs · 27,985 cycles

ON FLIGHT 3252 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO PUSH OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED ROLLERS ON AIRFRAME SIDE OF MAIN CABIN DOOR IAW EMB 145 AMM 20-20-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 30,643 hrs · 27,945 cycles

DURING B INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT HOLDER IAW EMB145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROFILE — CRACKED (AVIONICS DOOR) · airframe 30,463 hrs · 27,789 cycles

DURING MAINTENANCE INSPECTION FOUND THE REAR AVIONICS COMPARTMENT DOOR (272DR) INNER PROFILE IS CRACKED UNDER THE RETAINING PIN. AIRCRAFT REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-52MR-308. AIRCRAFT RETURNED TO SERVICE.

Part: RIB — CHAFED (LT WING) · airframe 30,463 hrs · 27,789 cycles

DURING MAINTENANCE INSPECTION FOUND LEFT WING RIB 21 CHAFED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-57MR-612. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER SPLICE — CORRODED (21 LEFT) · corrosion level 2 · airframe 30,463 hrs · 27,789 cycles

DURING MAINTENANCE INSPECTION, FOUND STRINGER 21 LEFT SPLICE BETWEEN FR13 AND FR14 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REPLACED STRINGER SPLICE IAW EO-EM-53MR-1559. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 30,279 hrs · 27,657 cycles

DURING B-INSPECTION FOUND THE OVERWING EMERGENCY LIGHTS AFT INOPERABLE ON BOTH SIDES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY UNIT POWER SUPPLY IAW WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 30,201 hrs · 27,597 cycles

DURING B-INSPECTION, FOUND BOTH AFT EMERGENCY WING LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY POWER SUPPLY BATTERY AND CHARGER IAW W/C 33-700-19. THE OPS CHECKED GOOD IAW W/C 33-700-17. AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 30,148 hrs · 27,558 cycles

FLIGHT 3398, FLIGHT ATTENDANT REPORTED MAIN CABIN DOOR WAS DIFFICULT TO OPEN. AIRCRAFT REMOVED FROM SERVICE. CLEANED AND LUBED MAIN CABIN DOOR ROLLERS IAW 52-10-00. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,063 hrs · 27,484 cycles

DURING B INSPECTION FOUND THE EMERGENCY EXTERIOR OVERWING LIGHT ON THE LEFT AND RIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND BATTERY POWER SUPPLY IAW MTX W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 30,063 hrs · 27,484 cycles

DURING B INSPECTION FOUND THE EMERGENCY FLOOR STRIP LIGHT NR 2 AND 3 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 INVERTER. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,063 hrs · 27,484 cycles

DURING B-INSPECTION FOUND THE SERVICE DOOR SIDE HINGED EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED GUILD AT SERVICE DOOR SIDE HINGE. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,063 hrs · 27,484 cycles

DURING B INSPECTION FOUND THE EMERGENCY FLOOR STRIP LIGHT NR 4,5 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 BATTERY AND BATTERY POWER SUPPLY IAW AE MTX W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 30,055 hrs · 27,473 cycles

DURING MAINTENANCE INSPECTION FOUND EMERGECNY LIGHT FLOOR STRIPS 2 AND 3 NOT LIGHTING. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LOOSE CONNECTORS ON FLOOR STRIPS 2 AND 3, RECONNECTED CONNECTORS IAW EMB AMM 33-50-12-400-801-A STEP 2. THE OPERATIONAL CHECK WAS GOOD IAW WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 30,062 hrs · 27,483 cycles

EMERGENCY LIGHTS WOULD NOT POWER OFF WHEN AIRCRAFT IS POWERED DOWN. DURING MAINTENANCE INSPECTION FOUND THAT AFTER DEPOWERSING AIRCRAFT NOTICED EMERGENCY LIGHTS ROW 8-12 AND OVERWING EMERGENCY LIGHTS ON. TURNED BOTH BATTERIES ON CYCLES EMERGENCY LIGHTS AND TURNED BOTH BATTERIES OFF AND EMERGENCY LIGHTS CONTINUED TO STAY ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTETM IAW AMM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,688 hrs · 27,225 cycles

DURING MAINTENANCE BASE VISIT FOUND BOTH AFT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND CHARGER ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW AE W/C 33-700-19. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 29,648 hrs · 27,196 cycles

DURING MAINTNEANCE BASE VISIT FOUND THE EMERGENCY STRIP LIGHTS 2 AND 3 ARE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHTING SYSTEM POWER SUPPLY IN THE GALLEY IAW AE-MTX-WC-33-700-19. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,620 hrs · 27,164 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT CABIN EMERGENCY CEILING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGECY CEILING LIGHT ON AFT CABIN IAW EMB-145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FUSE — BLOWN (NR 2 EPSU) · airframe 29,096 hrs · 26,783 cycles

ON FLIGHT 631 THE CREW REPORTED THE EMERGENCY FLOOR PROXIMITY LIGHTS STRIPS 2 AND 3 WERE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT POWER SUPPLY FUSES IAW EMB CMM 25-60-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,087 hrs · 26,776 cycles

ON FLIGHT 4357 THE CREW REPORTED THAT ON THE TAKEOFF ROLL THE CREW STARTED STEERING WITH THE RUDDER PEDALS IT FELT HARD IN STEERING RECEIVED GOT A "YAW DAMP FAIL" MESSAGE ON EICAS. THE CREW ABORTED THE TAKEOFF AND RETURNED TO GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED AN OPERATIONAL CHECK OF THE AUTOPILOT SYSTEM IAW AMM 22-11-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 28,452 hrs · 26,284 cycles

ON FLIGHT 3919 AT FLIGHT LEVEL 280 THE FLIGHT ATTENDANT REPORTED AN UNMISTAKABLE SMELL OF SMOKE. THE ODOR LASTED APPROXIMATLEY 5 MINUTES THEN DISSIPATED. THE CREW NEVER SAW SMOKE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTION FOUND THE CAPTAIN’S SIDE FLASHLIGHT HOT AND SMELLED BURNT. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT AND ASSEMBLY IAW EMB145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,747 hrs · 25,737 cycles

DURING MAINTENANCE BASE VISIT FOUND AFT LEFT OVERWING EMERGENCY LIGHT TO BE INOBERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT LEFT WING EMERGENCY LIGHT. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 25,502 hrs · 24,033 cycles

ON FLIGHT 3322 DURING THE DESCENT INTO DFW THE CREW RECEIVED A CARGO COMPARTMENT SMOKE DETECTION MESSAGE. THE CREW USED THE CARGO FIRE EXTINGUISHER SYSTEM. THE CREW DECLARED AN EMERGENCY AND LANDED AT DFW WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD AND AFT CARGO SMOKE DETECTORS. REMOVED AND REPLACED BAGGAGE COMPARTMENT HIGH RATE FIRE EXTINGUISHER BOTTLE IAW AMM 26-23-01. REMOVED AND REPLACED BAGGAGE COMPARTMENT METERING FIRE EXTINGUISHER BOTTLE IAW AMM 26-23-01. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,465 hrs · 24,005 cycles

DURING MAINTENANCE BASE VISIT FOUND THE NR 1 EMERGENCY LIGHT STRIP TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT STRIP IAW EMB AMM 145 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,465 hrs · 24,005 cycles

DURING MAINTENANCE BASE VISIT FOUND STRINGER 21 LEFT SPLICE BETWEEN FRAMES 13 AND 14 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1559. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,465 hrs · 24,005 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LAVATORY BUCKET TO BE CORRODED AROUND THE WASTE VALVE, WATER CONNECTION, AND RELEASE HANDLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1555. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WINDOW FRAME — CORRODED (COCKPIT) · corrosion level 2 · airframe 25,465 hrs · 24,005 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT DIVISION WINDOW FRAME LOWER BEAM HAS CORRODED WINDSHIELD SCREW HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICEABLE RIGHT DIVISION WINDOW LOWER BEAM IAW ETA-EM-53MR-157. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CRACKED (PYLON) · airframe 25,465 hrs · 24,005 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT YOKE FORWARD SPAR LOWER LINKAGE FITTING CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICEABLE LEFT YOKE FORWARD SPAR LOWER LINKAGE FITTING IAW EO EM-54MR-338. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,292 hrs · 22,296 cycles

LEFT EMERGENCY LIGHT INOP. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPC GOOD IAW AMM 33-50-00-700-801-A. ACFT RETURNED TO SERVICE. (ORIGINAL SUBMISSION DATE 7/18/2009, CONTROL NR CHANGE, SG)

Part: FIRE DETECTOR — FAILED (LEFT ENGINE) · airframe 18,174 hrs · 17,569 cycles

ENGINE ONE FIRE DETECT FAIL CAUTION MESSAGE ON TAKEOFF. REMOVED AND REPLACED NUMBER ONE ENGINE FIRE DETECTOR IAW EMB AMM 26-11-01 AND ENGINE PYLON FIRE DETECTOR IAW EMB 26-11-02. OPERATIONAL CHECKS GOOD ON BOTH COMPONENTS, RETURNED AIRCRAFT TO SERVICE.

Part: WIRE HARNESS — BURNED (LIGHTS)

ELECTRICAL SMOKE SEEPING OUT OF OVERHEAD SIDE WALL PANEL IN THE AREA OF OVERHEAD LIGHING RIGHT SIDE ROW 4. RAI HARNESS ASSEMBLY, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IMBV INSPECTION, FOUND RIGHT UPPER SEAT TRACK FROM FRAMES 36-47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IMBV INSPECTION, FOUND LEFT INBOARD FORWARD SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IMBV INSPECTION, FOUND RIGHT FORWARD BOTTOM SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IMBV INSPECTION, FOUND RIGHT UPPER SEAT TRACK FROM FRAMES 30-36 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IMBV INSPECTION, FOUND RIGHT FORWARD UPPER SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT RACK IAW AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IMBV INSPECTION, FOUND RIGHT UPPER SEAT TRACK FROM FRAMES 47-53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

IMBV INSPECTION, FOUND LEFT INBOARD SEAT TRACK CORRODED FROM FRAMES 42-43. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FCU — FAULTY (TE FLAPS)

DURING DESCENT, FLAPS STUCK AT 9 DEGREES EXTENSION. REPLACED FLAP ELECTRONIC CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE) · airframe 12,041 hrs · 12,308 cycles

DURING AN MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED, REMOVED EXISTING CENTER SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW SRM AND CORROSION PREVENTATIVE MANUAL.

Part: SWITCH — INOPERATIVE (LT MLG)

DURING TAKEOFF CREW REPORTED THE LANDING GEAR DID NOT RETRACT WHEN SELECTED UP. CREW NOTED A LDG AIR/GRD MESSAGE ON EICAS. CREW RETURNED TO DEPARTURE AIRPORT. MAINTENANCE DOWNLOADED CMC AND FOUND MULTIPLE FAILURES ON THE LT PROXIMITY SWITCH. THE LT WOW PROXIMITY SWITCHES 1 AND 2 WERE REPLACED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CREW REPORTED ALL OF FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. (M)

Part: STRINGER — GOUGED (FUSELAGE)

ABI - DURING A IMBV INSPECTION, MAINTENANCE FOUND THE RIGHT STRINGER 19 AT FRAME 52 GOUGED. BLENDED GOUGED AND PERFORMED AN NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED TWO DOUBLERS AND FOUR SHIMS. REPAIR DONE IAW EMB GST-3363/02 AND GST-3355/02. (M)

Part: STRINGER — GOUGED (FUSELAGE)

ABI - DURING A IMBV INSPECTION, MAINTENANCE FOUND THE LEFT STRINGER 19 AT FRAME 52 GOUGED. BLENDED GOUGE AND PERFORMED AN NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED TWO DOUBLERS AND FOUR SHIMS. REPAIR DONE IAW EMB GST-3363/02 AND GST 3355/02. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - DURING A IMBV INSPECTION, MAINTENANCE FOUND THE SERVICE DOOR CENTER SILL CORRODED BELOW SRM LIMITS. BLENDED CORRODED AREAS ON CENTER SILL. PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS NOTED. FABRICATED TWO REPAIR DOUBLER. REPAIR DONE IAW AE ETN NR EM-53-036 AND EMB SRM (SRM EMB-145.1142 REV 19) CHAPTERS 51-40-02, 51-20-03 AND 51-40-06. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING A IMBV INSPECTION, THE GALLEY AREA CENTER BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING BEAM AND INSTALLED NEW BEAM IAW EMB 145 SRM (EMB 145/1142 REV 19) CHAPTERS 51-40-02, 51-20-03 AND 51-40-06. (M)

Part: SUPPORT — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29964. RAMP SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING WAS DURING AN IMBV INSPECTION REFERENCE, CRIC NR 29955. SERVICE DOOR CENTER SILL CORRODED. INSTALLED DOUBLERS ON SERVICE DOOR CENTER SILL IAW EMB 145 ETN EM-53-026, STEP 1-7 AND SRM 51-40-02, 51-20-03, 51-40-06. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29956. SERVICE DOOR AFT SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02, 51-40-06 AND 51-20-03. (M)

Part: FLOOR SUPPORT — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29981. CARGO ENTRANCE LEFT BEAM GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-20-01, 51-20-03, 51-40-02, 51-40-02, 51-40-04, 51-40-06. (M)

Part: CROSSBEAM — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29962. CROSSBEAM PROFILE CORRODED. REMOVED AND INSTALLED SERVICEABLE CROSSBEAM AND PROFILE (P/N 14529150003) IAW EMB 145 SRM 51-40-02, 51-40-06, AND 51-20-03. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29956. SERVICE DOOR AFT SILL CORRODED. REMOVED AND INSTALLED SERVICABLE SILL IAW EMB 145 SRM 51-40-02, 51-40-06 AND 51-20-03. (M)

Part: FLOOR SUPPORT — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING WAS FOND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29957. GALLEY CENTER GUSSET BEAM CORRODED. REMOVED AND INSTALLED SERVICABLE BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29959. AFT GALLEY DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 51-40-02. (M)

Part: GUSSET — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29958. FORWARD GALLEY DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29961. LEFT GALLEY SIDE SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN IMBV INSPECTION REFERENCE CRIC NR 29953, LEFT OMEGA BEAM FORWARD SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK ON OMEGA BEAM IAW EMB 145 AMM 53-01-06. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING REPAIR AND CLEANED AREA. FABRICATED A FILLER, TWO SHIMS, PLATE AND EXTERNAL ANGLE. REPAIR DONE IAW EMB145 SRM (EMB 145/1142 REV 19) CHAPTER 53-21-10 FIG 201. (M)

Part: ENGINE — MALFUNCTIONED (LEFT)

ORD - FLT 4218 - DURING FLIGHT CREW REPORTED SMOKE IN COCKPIT. DUE TO REPEAT DISCREPANCY, ENGINEERING DIRECTED MAINTENANCE TO REPLACE THE LEFT ENGINE. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FUEL NOZZLE — MALFUNCTIONED (LT ENGINE)

ORD - FLT 4015 - DURING CLIMB, FLIGHT CREW REPORTED A SMOKE SMELL IN COCKPIT. AIRCRAFT WAS RETURNED TO ORD WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED ALL 16 FUEL NOZZLES ON LEFT ENGINE IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACTUATOR — INOPERATIVE (TAIL)

DISC-PITCH TRIM AUTO MSSG ON EICAS IN FLIGHT WITH AUTOPILOT ON THEN ALL PITCH TRIM SWITCHES FAILED. C/A MAINTENANCE REMOVED AND INSTALLED A NEW HORIZONTAL STABILIZER ACTUATOR.

Part: PIN — BENT (CONTROL HANDLE)

DFW - FLT 3745 - AFTER TAKEOFF, CREW REPORTED A LANDING GEAR DISAGREE MESSAGE ON EICAS. LANDING GEAR HANDLE WAS CYCLED SEVERAL TIMES WITH NO SUCCESS. AIRCRAFT WAS RETURNED TO DFW. MAINTENANCE FOUND AN REPOSITIONED LANDING GEAR POSITION SWITCH FROM DOORS TO NORMAL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. THE NEXT FLIGHT, DURING CLIMB-OUT THE LANDING GEAR HANDLE WOULD NOT MOVE. CREW DECLARED EMERGENCY AND RETURNED TO DFW. MAINTENANCE FOUND A BENT CONNECTOR PIN IN THE LANDING GEAR CONTROL HANDLE. LANDING GEAR CONTROL HANDLE WAS REMOVED AND REPLACED IAW EMB MM. OPERATIONAL CHECK AS GOOD AND AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK FLIGHT. FCF WAS SATISFACTORY AND AIRCRAFT WAS

Part: WINDSHIELD — FAILED (COCKPIT)

DFW - FLT 3766 - CAPTAIN'S WINDSHIELD SHATTERED IN FLIGHT. EMERGENCY WAS DECLARED. CAPTAINS WINDSHIELD WAS REMOVED AND REPLACED. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MSN - FLT 4044 - DURING PRE-FLIGHT INSPECTION, CREW REPORTED THE AFT FLOOR PROXIMITY EMERGENCY LIGHTS DID NOT ILLUMINATE. MAINTENANCE REPLACED THE AFT LIGHT STRIP IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DOOR — OPEN (GPU ACCESS)

ORD - FLT 4215 - CREW REPORTED AN AUDIBLE VIBRATION COMING FROM THE LEFT SIDE OF AIRCRAFT NOSE. MAINTENANCE FOUND THE GPU ACCESS DOOR TO BE OPEN. DOOR WAS DAMAGED AND WAS PUT ON CDL AT THIS TIME. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DUCT — DAMAGED (RT NACELLE)

XNA - FLT 3721 - ON TOUCHDOWN, THE CREW REPORTED THE NR 2 ENGINE FIRE WARNING INDICATION. THE CREW PULLED THE FIRE BOTTLE HANDLES AND RELEASED THE AGENT. AFTER THE AIRCRAFT WAS PARKED, THE CREW AND CRASH FIRE AND RESCUE WALKED AROUND AND FOUND NO VISIBLE EVIDENCE OF ACTUAL FIRE. NO PASSENGER INCIDENTS REPORTED. MAINTENANCE FOUND BLEED DUCT BLOWN OUT IN NR 2 ENGINE NACELLE AREA AND BLOWING DIRECTLY ON FIRE SENSING LOOP. MAINTENANCE REMOVED AND REPLACED BLEED DUCT ASSEMBLY. BOTH ENGINE FIRE BOTTLES WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M)