N843AE

Part: DUCT — UNSECURE (SEAT9BC) · airframe 36,225 hrs · 32,234 cycles

STRANGE ODOR OF DIRTY SOCKS COMING FROM PACKS WHILE RUNNING ON APU BLEED. SECURED RISER DUCT AT SEAT 9BC IAW AMM 21-20-04 . REMOVED AND REPLACED THE LT CONDENSER MIXER IAW AMM 21-51-04. OPS CHECKED GOOD. LEAK CHECKED GOOD. NO FURTHER DEFECTS NOTED. REMOVED AND REPLACED THE LT HEAT EXCHANGER IAW AMM 21-51-02. OPS AND LEAK CHECKED GOOD. REINSTALLED LT ACM IAW AMM 21-51-03. OPS AND LEAK CHECKED GOOD. C/W EO EM-2100-048 PART A. OPS AND LEAK CHECKED GOOD. REMOVED AND REPLACED THE RECIRCULATION MUFFLER DUCT IAW AMM 21-24-02. REMOVED AND REPLACED Y-DUCT ON LT PACK IAW AMM 21-60-01. OPS AND LEAK CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: BLEED VALVE — FAILED (NR 2) · airframe 35,992 hrs · 31,958 cycles

PACK VALVE AND BLD VALVE CLOSED INFLIGHT ON #2. PACK 2 VALVE C/B POPPED.-C/A-REMOVED AND REPLACED #2 PACK VALVE IAW AMM 21-51-01. OPERATIONAL CHECK GOOD. #2 BLD VALVE OPS CHECK GOOD IAW AMM 36-11-05.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 35,736 hrs · 31,709 cycles

COCKPIT EMERGENCY SIGN EXIT LIGHT INOP. C/A-REMOVED AND REPLACED EMERGENCY EXIT SIGN INVERTER 1 IAW AMM 33-50-11. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,628 hrs · 31,595 cycles

DURING INSPECTION, FOUND AISLE EMERGENCY LIGHT LAMP INOPERATIVE AT SEAT 11A. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP. OPS CHECKED GOOD IAW AMM 33-50-08.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 35,321 hrs · 31,331 cycles

FOUND AFT FLASHLIGHT HOLDER BROKEN. C/A-REMOVED AND REPLACED FLASHLIGHT, AFT HOLDER ASSEMBLY IAW AMM 33-50-16. OPC GOOD.

Part: SPLICE — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,584 hrs · 30,696 cycles

SUPPLEMENTAL FOUND EMERG. FLOOR STRIP LIGHT AT PAX SEAT 11 AND 12 DOES NOT ILLUMINATE. C/A-REMOVED AND REPLACED BATTERY AND CHARGER ASSY. IAW W/C # 33-700-19. DID NOT FIX. ITEM DEFERRED PER MEL 33-30, AUTH 030448-C. BATTERY CHARGER ASSY P/N 11-0049 S/N 15198. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 69972. REMOVED AND REPLACED EMERGENCY LIGHT STRIP BETWEEN SEATS 11 AND 12. DURING RAR FOUND BROKEN SPLICE CONNECTOR. SPLICED NEW CONNECTOR IAW STANDARD WIRING PRACTICES MANUAL 20-21-00. OPS CHECK GOOD. NO DEFECTS NOTED. MEL RESTORED.

Part: LIGHT — INOPERATIVE (SEATS 12A & 13A) · airframe 33,030 hrs · 29,286 cycles

FLOOR EMERGENCY LIGHT IN THE CABIN, ALONG SEATS 12A AND 13A DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Part: SWITCH — DIRTY · airframe 32,882 hrs · 29,157 cycles

LEFT WING LEADING EDGE DAMAGED, ACCESS DOOR OPEN MESSAGE. REAR AVIONICS DOOR INDICATION RED. CLEARED AFTER 5 MINUTES. CLEANED WARNING MICROSWITCH FOR REAR ELEC DOOR.AND OPS CHKED REAR ELEC DOOR HATCH WARNING INDICATION & MESSAGE OK IAW AMM 52-77-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,878 hrs · 29,154 cycles

WIRE FOR EMERGENCY LIGHT WAS BROKEN. REPAIRED EMERGENCY LIGHT WIRE IAW SWPM 20-21-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,878 hrs · 29,154 cycles

EMERGENCY LIGHT WIRE WAS BROKEN. REPAIRED WIRE IAW SWPM 20-21-00.

Part: SKIN — CRACKED (FRAMES 80-81) · airframe 32,878 hrs · 29,154 cycles

FUSELAGE SKIN UPPER SPLICE PLATE BETWEEN FRAMES 80 AND 81 WAS CRACKED. PERFORMED A PERMANENT REPAIR IAW SRM 51-40-02

Part: SHEAR TIE — CORRODED (FR 68) · airframe 32,878 hrs · 29,154 cycles

FRAME 68, FWD SHEAR TIE, AT THE CARGO DOOR CUTOUT HAD AN AREA OF CORROSION BETWEEN STRINGERS 15 - 16L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-31-04

Part: SKIN — CRACKED (FRAME 75) · airframe 32,878 hrs · 29,154 cycles

RIGHT UPPER FUSELAGE SKIN WAS CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R, THE CRACK WAS APPROXIMATELY 1 INCH LONG . PERFORMED A PERMANENT REPAIR IAW SRM 53-31-01, FIG 219

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 32,878 hrs · 29,154 cycles

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

Part: PROFILE — GOUGED (LT OVERWING EXIT) · airframe 32,878 hrs · 29,154 cycles

LEFT OVERWING EXIT LOWER PROFILE GOUGED IN THE RADIUS. REMOVED AND REPALCED LOWER FRAME PROFILE IAW SRM 51-40-02.

Part: SKIN — GOUGED (FUSELAGE) · airframe 32,878 hrs · 29,154 cycles

FUSELAGE EXTERNAL SKIN INSIDE PYLON PANEL 414DB GOUGED. FUSELAGE EXTERNAL SKIN INSIDE PYLON PANEL 414DB GOUGE REPAIRED IAW SRM 53-31-01 FIG 220.

Part: PROFILE — CORRODED (CARGO DOOR) · airframe 32,878 hrs · 29,154 cycles

CARGO DOOR LOWER FRAME PROFILE CORRODED AT NUTPLATE HOLES. REMOVED AND REPLACED CARGO DOOR LOWER FRAME PROFILE IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,878 hrs · 29,154 cycles

SSI 53-20-10 SERVICE DOOR CENTER SILL CORRODED AT FWD SCREW HOLE. REPAIRED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW SRM 53-21-02, FIGURE 201.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,878 hrs · 29,154 cycles

PERFORM PERMANENT REPAIR OF DENT(.5 X .5 X .028) WITH PAINT MISSING ON LT SIDE OF FUSELAGE BELOW CABIN WINDOW 1A IN RED STRIPE IAW SRM 53-21-01. PERFORMED PERMANENT REPAIR OF DENT(.5 X .5 X .028) WITH PAINT MISSING ON LT SIDE OF FUSELAGE BELOW CABIN WINDOW 1A IN RED STRIPE IAW SRM 53-21-01.

Part: FITTING — DAMAGED (LT AILERON) · airframe 32,878 hrs · 29,154 cycles

LT AILERON DAMPER FITTING GOUGED INSIDE FITTING. REMOVED AND INSTALLED LT AILERON DAMPER FITTING IAW EO EM-27MR-112 REPAIR.

Part: FRAME — CRACKED (FRM 66) · airframe 32,878 hrs · 29,154 cycles

FRAME 66 CRACKED, LOCATED BETWEEN STRINGERS 17L AND 18L. REPAIRED THE FRAME IAW ERS-EM-53MR-3279.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,878 hrs · 29,154 cycles

EMERGENCY LIGHT INOPERATIVE AT THE FA CEILING PANEL. REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT IAW AMM 33-50-08. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,878 hrs · 29,154 cycles

EMERGENCY EXIT ROW CEILING PANEL EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE BULB IN THE EMERGENCY LIGHT IAW AMM 33-50-08. OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (1 - 8) · airframe 32,878 hrs · 29,154 cycles

LEFT EMERGENCY LIGHT STRIP EXTRUSIONS NR 1 THRU 8 WERE DAMAGED. REMOVED AND REPLACED THE LT EMERGENCY LIGHT IAW AMM 33-50-12.

Part: STRINGER — CRACKED (FRAME 75) · airframe 32,878 hrs · 29,154 cycles

STRINGER 2R CRACKED AT FRAME 75. ACCOMPLISHED A REPAIR OF THE STRINGER IAW ERS-EM-53MR-3276.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 32,877 hrs · 29,151 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT.

Part: SWITCH — FAILED (FLASHLIGHT) · airframe 32,294 hrs · 28,550 cycles

F/A FWD FLASHLIGHT SWITCH CAME APART. REMOVED AND REPLACED THE FLASHLIGHT IAW STANDARD MAINTENANCE PRACTICES

Part: DISPLAY — FAILED (COCKPIT) · airframe 31,666 hrs · 27,974 cycles

FIRST OFFICERS MFD FAILED, ACCOMPANIED BY STRONG ELEC ODOR. NO EVIDENCE OF BURNED PINS OR WIRES. R & R FIRST OFFICERS MFD IAW AMM 34-22-01. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 31,055 hrs · 27,271 cycles

FIRST OFFICERS FLASHLIGHT HOLDER BROKEN. DEFERRED IAW MEL 25-53. R & R FIRST OFFICERS FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONAL CHECK GOOD & MEL RESTORED.

Part: SWITCH — FAILED (PARKING BRAKE) · airframe 30,417 hrs · 26,593 cycles

ABORTED TAKEOFF AT 80 KNOTS, WARNING TAKEOFF CONFIG BRAKES & SPOILER OPEN. R & R EMER PARKING BRAKE SWITCH IAW AMM 32-44-07. ALL CHECKED GOOD, OK FOR SERVICE. SPOILER DEPLOYMENT NORMAL. OPERATION FOR ACFT ON GND ON ABORTED TAKEOFF.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 30,069 hrs · 26,258 cycles

LEFT EMER EXIT DOOR, EXIT SIGN INOPERATIVE. R & R NR 5 EMER LIGHT INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,069 hrs · 26,258 cycles

OVERHEAD EMER LIGHT AT ROW 15 - 16 INOPERATIVE. RELAMPED CEILING EMER LIGHT AT ROW 15 - - 16 IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.

Part: INVERTER — MALFUNCTIONED (CABIN) · airframe 29,771 hrs · 25,942 cycles

LEFT CABIN EMER LIGHT AT LT OVERWING EMER EXIT MARKER SIGN INOPERATIVE. RESET EMER LIGHT INVERTER AT LT OVERWING EXIT IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 29,435 hrs · 25,642 cycles

CAPTAINS FLASHLIGHT CRADLE BROKEN. R & R CAPTAINS EMER FLASHLIGHT ASSEMBLY IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: BRAKE — DEFECTIVE (NR 2) · airframe 29,316 hrs · 25,554 cycles

AFTER LANDING WHEN TAXING ON TAXIWAY, THE LT BRAKE WAS MAKING UNUSUAL NOISE & FELT LIKE IT WAS CATCHING ALMOST LOCKING, COULD FEEL IT ON THE PEDAL. STOPPED ACFT & REQUESTED OPERATIONS TO TOW US IN. FLIGHT ATTENDANT ALSO REPORTED UNUSUAL LOUD NOISE. WITH LT GEAR ON AXLE JACK FOUND NR 2 WHEEL WOULD BIND DURING FWD ROTATION. R & R NR 2 BRAKE & WHEEL ASSEMBLY IAW WC 32-600-14 & 32-700-11. RESPECTIVE, LT MAIN WHEEL PN 31641 SN 32970234P.

Part: SKIN — CHAFED (RUDDER) · airframe 29,213 hrs · 25,467 cycles

RUDDER NR 1 LE IS CHAFED. REPAIRED IAW ERS EM-55MR-217.

Part: FITTING — LOOSE (RT AILERON) · airframe 29,213 hrs · 25,467 cycles

RIGHT AILERON PCA FITTING INBD LUG & OTBD HAT BUSHING IS LOOSE IN THE FITTING. R & R RT AILERON PCA FITTING IAW EO EM-27MR-112.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,213 hrs · 25,467 cycles

RIGHT OMEGA BEAM, SHOULD READ CTR, IS CORRODED BETWEEN FRAMES 57 - 59. REPAIRED RT OMEGA BEAM IAW ERS-EM-53MR-1011.

Part: HINGE FITTING — DAMAGED (RUDDER) · airframe 29,213 hrs · 25,467 cycles

RUDDER II UPPER HINGE FITTING, UPPER FLANGE BUSHING HOLE BEYOND LIMITS. INSTALLED NEW RUDDER II UPPER HINGE FITTING IAW SRM 55-40-02 & ETN EM-55-070.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,213 hrs · 25,467 cycles

HFEC INSPECTION INDICATES FLAW 3/4 INCHES LONG IN FUSELAGE SKIN, 3.5 INCHES FROM THE VERTICAL STAB BASE AT FRAME 75 BETWEEN STRINGERS 1 - 2 LT SIDE. COMPLETED REPAIR IAW ERS-EM-53MR-1020.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 29,213 hrs · 25,467 cycles

BLEED DUCT BRACKET IS COMPLETELY CRACKED THROUGH 2 INCHES AT FRAME 74 STRINGER 11R. R & R BLEED DUCT BRACKET AT RT SIDE FRAME 74 & INSTALLED AIR DUCT IAW SRM 51-40-02 & AMM 36-11-09.

Part: WEB — CRACKED (NLG WW) · airframe 29,213 hrs · 25,467 cycles

NLG UPLOCK BOX FWD WEB CRACKED. INSTALLED NEW NLG UPLOCK BOX FWD WEB IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 29,213 hrs · 25,467 cycles

CARGO DOOR HOLD OPEN CUP SUPPORT AT FRAME 68 FLOOR LEVEL IS CRACKED IN 2 AREAS. ONE INCH TOTAL LENGTH. INSTALLED NEW SUPPORT IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 29,213 hrs · 25,467 cycles

RIGHT OVERWING PANEL UPPER ATTACHMENT ANGLE HAS A 1 1/4 INCH CRACK AT THE RIVET ON FRAME 49. COMPLIED WITH REPAIR OF RT OVERWING PANEL UPPER ATTACHMENT ANGLE ON FRAME 49 IAW SRM 53-23-12.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,213 hrs · 25,467 cycles

RIGHT COCKPIT FRAME NR 10, BELOW THE DV WINDOW STRUCTURE, HAS A 1 1/2 INCH CRACK. R & R RT COCKPIT FRAME NR 10 BELOW DV WINDOW IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,213 hrs · 25,467 cycles

FRAME SHEAR CLIP IS CRACKED APPROX 1 INCH AT FRAME 79 BETWEEN STRINGERS 2R - 3R. R & R FRAME SHEAR CLIP AT FRAME 79 BETWEEN STRINGER 2R - 3R IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 29,213 hrs · 25,467 cycles

LEFT OVERWING PANEL LOWER ATTACHMENT ANGLE NR 3 HAS 1/2 INCH CRACK ON THE LE. R & R LT OVERWING PANEL LOWER ATTACHMENT ANGLE NR 3 IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 29,213 hrs · 25,467 cycles

RIGHT OMEGA BEAM ATTACH ANGLES ARE CRACKED BETWEEN FRAMES 47 - 48. COMPLIED WITH REPAIR OF RT OMEGA BEAM ATTACH ANGLES BETWEEN FRAMES 47 - 48 IAW SRM 52-32-02. CLIP PN 140-04213-603, CHANNEL PN 140-04213-607.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 29,213 hrs · 25,467 cycles

CARGO DOOR CABLE DRUM BRACKET AT FRAME 68 BETWEEN STRINGERS 4R - 5R HAS 3 CRACKS. 2.5 INCHES IN LENGTH TOTAL. REPLACED CARGO DOOR CABLE DRUM BRACKET AT FRAME 68 BETWEEN STRINGERS 4R - 5R IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 29,213 hrs · 25,467 cycles

STRINGER CLIP AT FRAME 80 TO STRINGER 8R HAS A 3/4 INCH CRACK. R & R STRINGER CLIP AT FRAME 80 TO STRINGER 8R IAW SRM 51-40-02. RESTORED SURFACE FINISH TO AFFECTED AREA OF EXTERNAL FUSELAGE IAW CPM 51-21-07, ETN -EM-51-91 & ETN-EM-51-120.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 29,213 hrs · 25,467 cycles

CARGO DOOR TORSION BRACKET AT FRAME 61 STRINGER 4R - 5R IS CRACKED .25 INCH. R & R CARGO DOOR TORSION BRACKET IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,213 hrs · 25,467 cycles

LEFT COCKPIT FRAME NR 10, BELOW THE DV WINDOW STRUCTURE, HAS A 1 1/2 INCH CRACK. INSTALLED NEW FRAME NR 10 BELOW DV WINDOW IAW SRM 51-40-02.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 28,291 hrs · 24,730 cycles

EICAS WINDSHIELD 1 HEAT FAIL MSG RECEIVED DURING CLIMB OUT. MSG WOULD CLEAR & REAPPEAR AOM VOL 1 PROCEDURES FOLLOWED. R & R WINDSHIELD TEMP CONTROLLER ON CAPTAINS SIDE IAW AMM 30-42-01. OPERATIONS & FUNCTION CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,769 hrs · 24,299 cycles

DURING TROUBLESHOOTING OF ITEM NR 1 THIS LOG PAGE FOUND NR 3 POWER SUPPLY BATTERY INOPERATIVE. R & R NR 3 POWER SUPPLY BATTERY IAW MM 33-50-04. EMERGENCY LIGHTS CHECKED GOOD IAW MM 33-50-00.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 27,763 hrs · 24,292 cycles

EMERGENCY LIGHTS, INTERNAL & EXTERNAL, FADE FROM BRIGHT TO OFF, REGARDLESS OF WHICH OPERATIONS CHECKED GOOD. PN 2013-1A NR 2, SN 109577, NR 3 SN 82488, NR 4 SN 103176. PN 11-0049 NR 2 SN 14891, NR 3 SN 18390, NR4 SN 18393.

Part: LIGHT — INOPERATIVE (SEAT 12 B/C) · airframe 26,258 hrs · 22,903 cycles

SEAT 12 B/C EMERGENCY OVERHEAD INTERNAL LIGHT INOPERATIVE. R & R EMERGENCY LIGHT LAMP IAW AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,153 hrs · 22,805 cycles

RT AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: ANTI-ICE VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 25,299 hrs · 22,111 cycles

ON FLIGHT 2733 THE CREW REPORTED THEY HAD AN ENGINE 1 ANTI-ICE FAIL DURING CLIMB IN NON-ICING CONDS: TAT +11C 9000 MSL. ICE DET1 FAIL MESSAGE ALSO ON. THE CREW FOLLOWED AOM PROCEDURES AND DID NOT REMEDY THE SITUATION. THE CREW DECLARED AN EMERGENCY AND REMAINED CLEAR OF ICING CONDITIONS. THE AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE 1 ANTI ICE VALVE IAW EMB-140 AMM 30-21-01. THE OPERATIONAL CHECK WAS GOOD IAW AMM 30-00-00-700-802-A. REMOVED AND REPLACED NR 1 ICE DETECTOR IAW EMB-140 AMM 30-80-01. PART NUMBER 0871HT31A, S/N 00728. THE OPERATIONAL CHECK WAS GOOD IAW AMM 30-80-00. NO FURTHER DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOUBLER — CRACKED (FUSELAGE)

DURING MBV INSPECTION, QC FOUND FRAME 23 REPAIR DOUBLER CRACKED BETWEEN STRINGERS 15R AND 16R. REMOVED PREVIOUS REPAIR PARTS, FABRICATED AND INSTALLED NEW REPAIR PARTS IAW EO EM-53MR-1808.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,347 hrs · 21,310 cycles

DURING B INSPECTION FOUND THE LEFT OVERWING FAIRING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY AND BATTERY CHARGER IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — DEFECTIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS NOT WORKING. REPLACED BATTERY HOLDER ASSY.

Part: WIRE — BROKEN (CABIN) · airframe 24,347 hrs · 21,310 cycles

DURING MAINTENANCE INSPECTION FOUND THE ELECTRICAL WIRE FOR THE NR 1 EMERGENCY LIGHT STRIP BROKEN AT CONNECTOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CONNECTOR FOR THE NR 1 EMERGENCY LIGHT STRIP IAW EMB 140 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,347 hrs · 21,310 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR CENTER SILL HAS CORROSION AROUND ALL 3 NUT PLATE HOLES (MARKED). THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR CENTER SILL WITH SERVICEABLE CENTER SILL AND RESTORED PROTECTIVE COATING IAW EMB SRM 51-40-02, CPM 51-21-05, CPM 51-21-06, AEA ETN-GN-51-016R2, ETN-EM-51-075 AND ETN-EM-51-091R2. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — CRACKED (CABIN) · airframe 24,347 hrs · 21,310 cycles

DURING B INSPECTION FOUND THE LEFT PROXIMITY LIGHT HOLDER 2EA AND RIGHT FLOOR TRIM 2EA CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT PROXIMITY LIGHT HOLDER 2EA AND RIGHT FLOOR TRIM 2EA IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 24,347 hrs · 21,310 cycles

DURING B INSPECTION FOUND THE PROXIMITY LIGHT IN GALLEY, ONE WITH ARROWS AND ONE WITH OUT ARROWS TO HAVE BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PROXIMITY LIGHT IN GALLEY, ONE WITH ARROWS AND ONE WITH OUT ARROWS IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,147 hrs · 21,124 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,069 hrs · 21,032 cycles

ON FLIGHT 3039 THE CREW REPORTED THAT BOTH FORWARD & AFT EMERGENCY FLASHLIGHT "CHARGE" LIGHTS [RED] WERE NOT ILLUMINATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD AND AFT EMERGENCY FLASHLIGHT ASSEMBLY IAW EMB 140 AMM CHAPT 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 23,535 hrs · 20,538 cycles

FLIGHT 2983, CREW REPORTED COURTESY LIGHTS OVER THE FLIGHT ATTENDANT AT ENTRY ARE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. PERFORMED MAIN DOOR EMERGENCY LIGHT TEST IAW AMM 33-50-00. OPS TESTED GOOD. NO PARTS REMOVED OR REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 22,900 hrs · 20,066 cycles

ON FLIGHT 2921 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED DOOR FRAME ROLLERS REF EMB-140 AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: NUT PLATE — MISSING (CABIN) · airframe 21,915 hrs · 19,314 cycles

LT AFT OVERWING EMERGENCY LIGHT LENS MISSING NUT PLATE. REMOVED AND REPLACED LT AFT OVERWING EMERGENCY LIGHT ASSY IAW EMBAMM 33-50-07.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,855 hrs · 19,276 cycles

LT AND RT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 4 BATTERY HOLDER ASSEMBLY / BATTERY CHARGER IAW AMM 33-50-04. OP CHECK GOOD.

Part: HOLDER — DEFECTIVE (CABIN) · airframe 21,855 hrs · 19,276 cycles

LT AND RT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 BATTERY HOLDER ASSEMBLY / BATTERY CHARGER IAW EMB 140 AMM 33-50-04. OP CK GOOD.

Part: SEAL — DIRTY (CABIN DOOR) · airframe 20,965 hrs · 18,557 cycles

ON FLIGHT 4238 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED DOOR SEAL IAW EMB 140 AMM 52-10-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,052,547 hrs · 18,196 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,234 hrs · 17,933 cycles

DURING PREFLIGHT INSPECTION FOR FLIGHT 4060 THE CREW FOUND THAT THE LEFT AND RIGHT OVERWING EXTERIOR LIGHTS FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND POWER SUPPLY IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 20,181 hrs · 17,886 cycles

ON FLIGHT 3918 THE CREW REPORTED THAT DURING THE CLIMBOUT THE AIRCRAFT PRESSURIZATION FAILED, CLIMBED TO 10,000FT, CABIN ALTITUDE AND SWITCHED TO MANUAL MODE, SYSTEM STABILIZED AND PRESSURIZATION STABILIZED, SHORTLY AFTER, CABIN ALTITUDE DISPLAY WENT BLANK (AMBER DASHES) THEN CABIN PRESSURIZED TO 7.9 PSID AT 8,000FT MSL. THE CAPTAIN DECLARED AN EMERGENCY AND RETURED BACK TO ORD. THE CREW TURNED OFF THE PACKS TO DEPRESSURIZE AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ELECTROPNEUMATIC OUTFLOW VALVE IAW AMM 21-31-03. REMOVED AND REPLACED THE MANUAL CONTROLLER IAW AMM 21-31-02. PERFORMED OUTFLOW VALVE FUNCTION IAW AMM 21-31-00. PERFORMED PRESSURE CONTROL SYSTEM FUNCTION TEST IN AUTOMATIC AND MANUAL IAW AMM 21-31-00, AMM 21-31-00. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 19,586 hrs · 17,378 cycles

ON FLIGHT 3974 THE CREW REPORTED THE UPPER BRACKET ON THE FLASHLIGHT CRADLE BEHIND THE CAPTAIN’S SEAT TO BE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT CRADLE IAW 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — VIBRATION (FLT CONTROL)

ON FLIGHT 4108 CREW REPORTED A FLUTTER/VIBRATION IN THE FLIGHT CONTROLS DURING ALL PHASES OF FLIGHT. STARTED AT 150KTS, VIBRATION FELT WITH GEAR IN UP OR DOWN POSITION. VIBRATION FELT WITH AUTO PILOT ON AND OFF, PACKS ON, CREW NOTED THE VIBRATION THROUGH FLIGHT CONTROLS AS A CONSTANT SHIMMY. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. AWAITING FOLLOW UP.

Part: COUPLING — BLOWN (CABIN DIST) · airframe 11,722 hrs · 10,191 cycles

AFTER DEPARTURE, NR 1 PACK VALVE FAIL FOLLOWED SHORTLY BY NR 1 BLEED VALVE CLOSED FOLLOWED CHECKLIST AND AFTER RESET ONCE. FUMES APPEARED IN COCKPIT. RETURNED TO BOS NO OTHER ABNORMALITIES NOTED. NO FUMES IN CABIN. FUMES DISSIPATED AS SOON AS BLEED VALVE CLOSED. FOUND COUPLING BETWEEN DUAL TEMP CONTROL AND NR 1 ACM TUBE BLOWN REMOVED AND REPLACED COUPLING IAW EMB AMM 21-60-01. RUN PACK OPS CHECK GOOD IAW AMM 21-51-00. AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN)

ALSO, F/A REPORTED AN OIL SMELL IN THE CABIN. THIS WAS DURING FLIGHT. NO EMERGENCY DECLARED AND A/C LANDED WITHOUT INCIDENT. RAI NR 2 ENGINE, OPS CHECK GOOD, FCF PASSED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE BEAM TO REMOVED CORROSION. FABRICATED A REPAIR DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTER 53-21-10 FIG 201. (M)

Part: SMOKE — DETECTED (CABIN)

SAN - FLT 3155 - AIR TURN BACK DUE TO SMOKE SMELL IN CABIN. DECLARED EMERGENCY. AIRCRAFT LANDED SAFELY WITHOUT INCIDENT. PERFORMED DETAIL INSPECTION AND PERFORMED OPERAITONAL CHECK OF AIR CONDITIONING SYSTEM. PERFORMED ENGINE RUNS IAW AMM. NO DEFECTS NOTED AT THIS TIME. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY)

FLT 3595 - CRP - CREW REPORTED DURING CRUISE FILGHT THE CARGO FIRE DETECTION LIGHT CAME ON CREW FOLLOWED AOM PROCEDURES AND FIRED THE CARGO FIRE BOTTLES. LIGHT EXTINGUISHED AFTER 60 SECONDS. AFTER AN INSPECTION SYSTEM WAS PUT ON MEL. S/D - MAINTENANCE REMOVED AND REPLACED TEH CARGO SMOKE DETECTORS IAW EMB MM. OPS CHECK AND AIRCRAFT WAS RETURNED TO SERVICE AFTER REPLACING THE CARGO FIRE BOTTLE. (M)