N13903

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 38,868 hrs · 29,766 cycles

BOTH COFFEEMAKERS EMITTED SMOKE DURING FLIGHT. REMOVED AND REPLACED THE COFFEEMAKERS. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (SEATS 8 & 9A) · airframe 38,190 hrs · 29,214 cycles

DURING MX INSPECTION, THE FLOOR EMERGENCY LIGHT AT SEATS 8 & 9A WERE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT, AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 2) · airframe 36,163 hrs · 27,646 cycles

PILOT REPORTED SMOKE IN COCKPIT AND CABIN DURING FLIGHT. MAINTENANCE R & R THE NR 2 AIR CYCLE MACHINE WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,357 hrs · 25,423 cycles

BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 BATTERY CHASSIS ASSEMBLY TRAY. OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,049 hrs · 22,075 cycles

DURING 3A-CHECK INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 6L. MX REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A BUSHING REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02787, AND THE ACFT WAS RELEASED FOR SERVICE ON 07/11/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,049 hrs · 22,075 cycles

DURING 3A-CHECK INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 79 BELOW STRINGER 4L. MX REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A BUSHING REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02787, AND THE ACFT WAS RELEASED FOR SERVICE ON 07/11/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,049 hrs · 22,075 cycles

DURING 3A-CHECK INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 79 BELOW STRINGER 6R. MX REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A BUSHING REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02787, AND THE ACFT WAS RELEASED FOR SERVICE ON 07/11/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,049 hrs · 22,075 cycles

DURING 3A-CHECK INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77 BELOW STRINGER 5L. MX REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02787, AND THE ACFT WAS RELEASED FOR SERVICE ON 07/11/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,049 hrs · 22,075 cycles

DURING 3A-CHECK INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 79 BELOW STRINGER 5R. MX REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A BUSHING REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02787, AND THE ACFT WAS RELEASED FOR SERVICE ON 07/11/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,049 hrs · 22,075 cycles

DURING 3A-CHECK INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 75 ABOVE STRINGER 2L. MX REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS RELEASED FOR SERVICE ON 07/11/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,049 hrs · 22,075 cycles

DURING 3A-CHECK INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 6R. MX REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A BUSHING REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02787, AND THE ACFT WAS RELEASED FOR SERVICE ON 07/11/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,049 hrs · 22,075 cycles

DURING 3A-CHECK INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 5L. MX REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A BUSHING REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02787, AND THE ACFT WAS RELEASED FOR SERVICE ON 07/11/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,049 hrs · 22,075 cycles

DURING 3A-CHECK INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 75 ON STRINGER 2L. MX REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A DOUBLER REPAIR IAW CHANGE REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS RELEASED FOR SERVICE ON 07/11/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,049 hrs · 22,075 cycles

DURING 3A-CHECK INSPECTION THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 4L. MX REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A BUSHING REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02787, AND THE ACFT WAS RELEASED FOR SERVICE ON 07/11/13.

Part: DRAG ANGLE — CRACKED (STAB TO FUSELAGE) · airframe 29,049 hrs · 22,075 cycles

DURING 3A INSPECTION THE LT FWD VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE (SHAPE L ATACHMENT) WAS FOUND TO BE CRACKED APPROX 1.75" FROM THE AFT END. MX R & R THE AFFECTED DRAG ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/12/13.

Part: BULB — INOPERATIVE (FLASHLIGHT) · airframe 28,159 hrs · 21,390 cycles

CREW REPORTED CAPTAIN'S FLIGHT DECK FLASHLIGHT INOPERATIVE. MX REPLACED LAMP, OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CENTER FUSELAGE) · airframe 27,794 hrs · 21,116 cycles

ACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE LT SILL FROM FRAME 18 THRU 23. MX R & R THE SILL IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,794 hrs · 21,116 cycles

ACFT IS IN A C-CHECK, WHEN CORROSION WAS FOUND ON THE LT OTBD SEAT TRACK SUPPORT FROM FRAMES 46 THRU 50. MX BLENDED THE CORROSION AND WAS OUT OF LIMITS. REPLACED THE SUPPORT IAW SRM 53-00-11,AND EC 5320-01522, REV B. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 27,794 hrs · 21,116 cycles

ACFT IS IN FOR A C-CHECK WHEN THE CORROSION WAS FOUND ON THE LT AND RT SILL FRAME AT FRAMES 59 THRU 61. MX R & R THE SILLS IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (CENTER FUSELAGE) · airframe 27,794 hrs · 21,116 cycles

ACFT IN FOR A C-CHECK WHEN CORROSION WAS FOUND IN THE OMEGA BEAM AND GUSSET AT FRAMES 59 THRU FRAME 61. MX BLENDED OUT THE CORROSION AND HAD TO CUTOUT THE DAMAGE AND FABRICATE A NEW DOUBLER. INSTALL DOUBLER IAW ETD 2013-000636. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,794 hrs · 21,116 cycles

ACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE RT SILL FROM FRAME 44 TO FRAME 49. MX BLENDED THE CORROSION BEYOND THE LIMITS, THEY R & R THE SILL, RESTORED THE SURFACE PROTECTION IAW SRM 51-20-03 AND 51-40-02 AND CPM 51-21-06.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 27,794 hrs · 21,116 cycles

A/C IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE RT SILL FRAME AT FRAMES 28 THRU 33. MX R & R THE SILL IAW SRM 51-20-03 AND 51-20-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: DOUBLER — CORRODED (REAR FUSELAGE) · airframe 27,794 hrs · 21,116 cycles

DURING C-CHECK, CORROSION WAS FOUND ON THE LT WALL DOUBLER AT FRAME 61. MX R & R THE LT DOUBLER IAW SRM 51-40-02.

Part: SILL — CORRODED (CENTER FUSELAGE) · airframe 27,794 hrs · 21,116 cycles

ACFT IS IN A C-CHECK AT WHERE CORROSION WAS FOUND ON THE RT SILL AT FRAME 35 AND 36. MX R & R THE SILL IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SILL — CORRODED (CENTER FUSELAGE) · airframe 27,793 hrs · 21,116 cycles

DURING C-CHECK, CORROSION WAS FOUND ON THE RT SILL AT FRAME 53. MX BLENDED THE AREA AND WAS OUT OF LIMITS IAW SRM 51-10-03. R & R SILL IAW SRM 51-40-02-03.

Part: SILL — CORRODED (CENTER FUSELAGE) · airframe 27,794 hrs · 21,116 cycles

ACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND IN THE RT SILL BETWEEN FRAMES 36 TO FRAME 37. MX R & R A NEW SILL IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: PRESSURE SWITCH — FAULTY (RUDDER) · airframe 24,443 hrs · 18,410 cycles

CLE FLT 2866 THE CREW REPORTED A RUDDER SYSTEM 1 INOP MESSAGE DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE RUDDER 1 PRESSURE SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — DAMAGED (RT WING) · airframe 24,391 hrs · 18,370 cycles

TYS - A/C WAS FERRIED FROM ABE TO TYS AFTER A TUG STRUCK THE RT WING SUSTAINING DAMAGE TO THE AFT OUTBOARD SECTION. THE AILERON, SHROUDS, TIP FAIRING AS WELL AS SEVERAL UNDERLYING STRUCTURAL ELEMENTS WERE ALSO DAMAGED. MAINTENANCE REMOVED THE AILERONS, SHROUDS, TIP FAIRINGS, RIB 25 AND OUTBOARD LOWER ACCESS PANEL. CONTINUED WITH CUTTING AND REMOVING THE DAMAGED SECTIONS OF THE LOWER WING IAW IKARUS TECHNICAL INSTRUCTIONS TI 145-11-170 AND SRM CHAPTER 51. INSPECTION PERFORMED A NDI OF THE CUT AREAS IAW NDI MANUAL AND NO DISCREPANCIES FOUND. FAB ALL THE REPAIR PARTS IAW IKARUS TECHNICAL INSTRUCTIONS TI-145-11-170 AND SRM CHAPTER 51. APPLIED ALODINED AND EPOXY PRIMER TO THE REPAIRED PARTS. ALL 602'S WERE WRITTEN FOR FOM AND OTHER DISCREPANCIES. THIS A/C WILL BE REPO/TEST FLIGHT TO EWR FOR FINAL EVALUATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,799 hrs · 17,195 cycles

TYS - A/C IN FOR A C-CHECK WHEN INSPECTION FOUND THE VERTICAL STAB FIN SPAR 1 FRETTING AGAINST SKIN AT FRAME 73. MAINTENANCE REMOVED FR.75 FITTING, BLENDED THE AREA OF MINOR DAMAGE REPAIRED THE AREA WITH ALLODINED, PRIME AND PAINTED AND RE-INSTALL FITTING WITH SEALANT IAW EC 5310-01317. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: BATTERY — OVERTEMP (NR 2) · airframe 21,756 hrs · 16,404 cycles

NCI - FLIGHT 2643, DURING PREFLIGHT THE CREW REPORTED A BATTERY 2 OVERTEMP TO 92 DEGREES. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (AC BAY) · airframe 18,942 hrs · 14,317 cycles

CVG - FLIGHT 2772 - THE CREW REPORTED SMOKE IN THE CABIN /CKPIT IN CRUISE FLIGHT WITH THE SOURCE UNKNOWN. THE AIRCRAFT RETURNED TO CVG WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT TO FERRY TO IAH WHERE IT AGAIN LANDED WITHOUT INCIDENT. IAH MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COMPUTER — FAULTED (GPWS) · airframe 18,159 hrs · 13,745 cycles

FLIGHT 3047 - EWR - FLIGHT CREW REPORTED INTERMITTENT GPWS INOP IN EICAS, THRUST RATING CHANGE UNCOMMANDED, THRUST DOES NOT RESET IN ICING CONDITIONS. IAH MX RERACKED GPWS COMPUTER AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PRECOOLER — FAULTY (BLEED AIR SYS) · airframe 18,120 hrs · 13,718 cycles

CVG FLIGHT NR 2788 THE CREW REPORTED A BLEED 1 OVERTEMP MSG IN FLIGHT. THE ACFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR 1 PRECOOLER ASSEMBLY. OPS CHECKS WERE GOOD.

Part: HOUSING — DAMAGED (HORIZ STAB) · airframe 13,623 hrs · 10,571 cycles

TYS C-CHECK- DISCREPANCY- RT HORIZONTAL STAB. HINGE POINT HAS MIGRATED BUSHING AT IT'S FLANGE. REMOVED BUSHINGS REWORKED HOUSING TO 1ST OVERSIZE OF 1.664" AND INSTALLED NEW BUSHINGS IAW EMB 135/145 SRM 55-10-02.

Part: UPLOCK — INOPERATIVE (LT MLG) · airframe 10,306 hrs · 7,991 cycles

PNS - FLIGHT 2506, THE CREW REPORTED THAT ON THE FIRST GEAR EXTENSION, THE LEFT MAIN LANDING GEAR REMAINED RETRACTED, AFTER SEVERAL ATTEMPTS, THE LANDING GEAR EXTENDED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, INSTALLED THE GEAR PINS, AND THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK BOX, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DIODE — INOPERATIVE (FLASHLIGHT) · airframe 9,224 hrs · 7,149 cycles

SDF - REAR CABIN EMERGENCY FLASHLIGHT LED INOP. REMOVED AND REPLACED REAR CABIN FLASHLIGHT ASSY. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,872 hrs · 6,882 cycles

DURING C-CHECK, LT OMEGA BEAM HAS VARIOUS AREAS OF CORROSION BETWEEN FS 24 AND FS 32. MX REPAIRED LT OMEGA BEAM AT FRM 29 IAW EC 5320-01249. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,872 hrs · 6,882 cycles

DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FS 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FS 18 TO FS 23 IAW EMB 145 SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CHAFED (FUSELAGE) · airframe 8,872 hrs · 6,882 cycles

FRAME 81 FOUND CHAFED AT 6 O'CLOCK POSITION. MX REMOVED DAMAGED AREA AND INSTALLED NESTED DOUBLER REPAIR IAW EC5330-01472 AND EMB 145 SRM 51-40-03. ACFT RETURNED TO SERVICE.

Part: ENGINE — LEAKING (NR 2)

CREW REPORTED A LAV SMOKE WARNING AFTER TAKEOFF. AIRCRAFT RETURNED TO EWR WITHOUT INCIDENT. REPLACED THE NR 2 ENGINE AND AIRCRAFT RETURNED TO SERVICE.

Part: ELEVATOR — MALFUNCTIONED (FLIGHT CONTROL)

GRR FLIGHT NR 2584 THE CREW REPORTED ON SHORT FINAL APPROXIMATELY 500' ABOVE GROUND THE ELEVATORS COULD NOT BE MOVED FORWARD OR AFT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT IAW EMBRAER IC 2003-145/2694A. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS TEST FLOWN WITH NO DEFECTS REPORTED. AIRCRAFT RELEASED FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,113 hrs · 3,119 cycles

DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10 AND 51-21-04,05, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF INSPECTION

Part: ANGLE — CORRODED · airframe 4,113 hrs · 3,119 cycles

DURING A SCHEDULED INSPECTION THE CENTER RAMP ANGLE WAS FOUND TO CORRODED IN SEVERAL AREAS AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: DOOR — OUT OF ADJUST (NLG)

CLE FLIGHT 2104 THE CREW REPORTED NOSE VIBRATION IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE RIGHT NOSE GEAR DOOR OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE RIGHT NOSE GEAR DOOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS TEST FLOWN AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SIGN — FAULTY

BTV---CO3387, DURING SERVICE CHECK MAINTENANCE FOUND OVERWING EMERGENCY EXIT LOCATING LIGHT INOPERATIVE.....REMOVED AND REPLACED EMERGENCY EXIT LOCATING SIGN ASSEMBLY IAW EMB145 AMM #33-50-15. OPS.CHECKED GOOD.

Part: ODOR — DETECTED (COCKPIT)

SDF- DURING ICE TEST THE CREW NOTED A STRONG SMELL OF SMOKE IN THE COCKPIT AND FORWARD CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND THE AIRCRAFT WAS RELEASED IAW MEL. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE ICE DETECTION SYSTEM, NO SMOKE SMELL NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.