N12528

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 25,840 hrs · 26,816 cycles

DURING C-CHECK, GALLEY CENTER OMEGA BEAM CORRODED AT FRAME 20. R & R CENTER OMEGA BEAM BETWEEN FRAMES 17-24 IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 25,840 hrs · 26,816 cycles

DURING C-CHECK, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FRAMES 61-62) · airframe 21,927 hrs · 21,929 cycles

CARGO INTERIOR SKIN CORRODED BEYOND LIMITS AT FRAME 61-62 BETWEEN STRINGER 17-18R. R & R SKIN PANEL.

Part: FLOOR SUPPORT — CORRODED (FRAMES 24-25) · airframe 21,927 hrs · 21,929 cycles

DURING A C-CHECK, INSPECTION FOUND CENTER ASILE RT SIDE FLOOR SUPPORT BETWEEN FRAMES 24 AND 25 CORRODED. MAINTENANCE R & R OMEGA BEAM IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 23-32) · airframe 21,927 hrs · 21,929 cycles

DURING C-CHECK, INSPECTION FOUND THE RT FLOOR SUPPORT PITTED FROM FRAME 23 THRU 32. R & R IAW SRM 51-40-02.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,798 hrs · 21,741 cycles

DURING PREFLIGHT INSPECTION, CREW REPORTED THAT THE FIRST THREE EMERGENCY AISLE PATH LIGHTS WOULD NOT ILLUMINATE. MX R & R POWER SUPPLY, OPS TESTED WITH NO DEFECTS, AND AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — SMOKE (CABIN) · airframe 21,796 hrs · 21,738 cycles

THE READING LIGHT AT 11B WAS REPORTED AS SMOKING WHEN IT WAS TURNED ON. MX R & R THE AFFECTED READING LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — SMOKE (CABIN) · airframe 21,796 hrs · 21,738 cycles

READING LIGHT AT 11B WAS REPORTED AS SMOKING WHEN IT WAS TURNED ON. MX R & R THE AFFECTED READING LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,585 hrs · 21,415 cycles

DURING SCHEDULED MX, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — INOPERATIVE (WX RADAR SYS) · airframe 21,168 hrs · 20,828 cycles

THE CREW REPORTED AN ELECTRICAL ODOR IN IMC WITH THE RADAR ON, AND THAT IT WENT AWAY WHEN THE F/O'S RADAR CONTROLLER WAS OFF. THE ACFT LANDED WITHOUT INCIDENT. MX R & R WEATHER RADAR CONTROLLER, OPS TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — MULTIPLE FAIL · airframe 21,164 hrs · 20,825 cycles

IN FLIGHT, MISCOMPARE FLAG, NOTICED A HOT ELECTRICAL ODOR. SPS ADVANCD MESSAGE APPEARED, F/O POSITION IAS FROZE AT 225KTS WITH AIRSPEED CHANGES VARIABLE ON CA SIDE AND STBY IAS. THE ODOR WAS INTENSE ENOUGH TO WARRANT WEARING MASKS. ON LEAVING, ALL ERRORS AND ODOR CLEARED AFTER 2-3 MINUNTES. ACFT LANDED WITHOUT INCIDENT. INSPECTED THE ACFT, DRAINED PITOT LINES, VERIFIED NORMAL OPS OF STALL PROTECTION SYS, ALL WITH NO DEFECTS NOTED AND UNABLE TO DUPLICATE THE ODOR THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 17,190 hrs · 15,375 cycles

DURING INSPECTION THE NR 2 FLOOR PROXIMITY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE TO THE LIGHT. THE WIRE WAS SPLICED IN ACCORDANCE WITH EMB 135 SWPM 20-21-00.

Part: PROXIMITY SWITCH — BROKEN (NLG) · airframe 16,087 hrs · 13,924 cycles

CREW REPORTED A LG AIR/GND FAIL EICAS MESSAGE DURING CRUISE. IT WAS FOLLOWED BY AN E1/E2 REV DISAGREE MESSAGE. THE QRH WAS FOLLOWED AND IT WAS DECIDED TO RETURN TO FNT DUE TO ICING CONDITIONS AT THE DESTINATION. THE MESSAGE APPEARED INTERMITTENTLY DURING DESCENT AND CLEARED AFTER GEAR EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE PROX SWITCH TO HAVE A PIN BROKEN OFF IN THE CONNECTOR. THE PIN WAS EXTRACTED FROM THE CONNECTOR AND THE PROX SWITCH WAS REPLACED WITH NO FURTHER DEFECTS NOTED.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 15,125 hrs · 12,580 cycles

FLIGHT 1205, MKE TO IND. AFTER CLIMBING THROUGH 1,500FT THE CREW RECEIVED A MASTER CAUTION BAGGAGE DOOR OPEN INDICATION. THE QRH WAS COMPLETED AND THE AIRCRAFT RETURNED TO MKE AND LANDED WITHOUT INCIDENT. THE BAGGAGE DOOR WAS CONFIRMED CLOSED AND LOCKED AND THE INDICATION WAS PLACED ON DEFERRAL. THE DEFERRAL WAS CLEARED ON 9/5/2009 IN IND WHEN THE FORWARD MICRO SWITCH WAS ADJUSTED AND THE INDICATION SYSTEM OPERATED NORMALLY.

Part: CONTROL UNIT — INOPERATIVE (T/E FLAP) · airframe 14,844 hrs · 12,317 cycles

IAH-FLIGHT 2411, THE CREW REPORTED THAT THE FLAPS FAILED CLIMBING THROUGH 15000 FEET AT 0 DEGREES. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FECU (FLAP ELECTRONIC CONTROL UNIT). OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: FLAP — OUT OF ADJUST (RT WING) · airframe 14,676 hrs · 12,185 cycles

IAH - FLIGHT 2460, THE CREW REPORTED A FLAP FAIL MESSAGE IN FLIGHT AND PERFORMED AN EMERGENCY DESCENT AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RT HAND INBOARD FLAP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 13,861 hrs · 11,516 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS VARIOUS AREAS OF CORROSION AT FR24-28. MX REPAIRED FR 24-28 IAW EMB145 53-00-10 FIG 202. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,861 hrs · 11,516 cycles

SHV - DURING C-CHECK EMERGENCY LIGHT ON RIGHT FWD PNL 191 INOP. MX REMOVED AND REPLACED RIGHT FWD EMERGENCY LIGHT ASSY ON 191 PNL IAW EMB 135 AMM 33-50-10, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: LIGHT — INOPERATIVE · airframe 13,861 hrs · 11,516 cycles

SHV - DURING C-CHECK EMERGENCY LIGHT ON RIGHT FWD PNL 191 INOP. MX REMOVED AND REPLACED RIGHT FWD EMERGENCY LIGHT ASSY ON 191 PNL IAW EMB 135 AMM 33-50-10, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: ATTACH FITTING — DAMAGED (RT AILERON) · airframe 13,861 hrs · 11,516 cycles

SHV - DURING C-CHECK RIGHT AILERON TO PCA BRACKET HAS AN ELONGATED BUSHING HOUSING. MX REMOVED AND REPLACED RIGHT AILERON TO PCA FITTING IAW EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: REPAIR — CORRODED (FUSELAGE) · airframe 13,861 hrs · 11,516 cycles

SHV - DURING C-CHECK LEFT OMEGA BEAM PREVIOUS REPAIRED AT FR 20 HAS CORROSION. MX REPAIRED LEFT OMEGA BEAM PREVIOUS REPAIRED IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,231 hrs · 10,216 cycles

IAH - DURING A-CHECK INSPECTION THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS AND SEVERAL CABIN EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY EXIT LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,888 hrs · 7,600 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAMES 20-23. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-00-10, SECTION 2, FIG 201, SHEET 2 AND EMB 135 SRM 53-21-10, SECTION 7, FIG 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 8,888 hrs · 7,600 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AFT OF FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,888 hrs · 7,600 cycles

SHV - DURING C-CHECK THE BAGGAGE DOOR LOWER CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEVEL GEAR — FAILED (ENGINE) · airframe 8,242 hrs · 7,132 cycles

FLT 3251 - AT FL350 ENGINE NR 1 FAILED WITH NO INDICATIONS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE ASSY, COMPLIED WITH OPERATIONAL CHECKS AND ACFT WAS RELEASED TO SERVICE. *S/D* TEARDOWN REPORT: CAUSE OF THE UNCOMMANDED IN FLIGHT SHUTDOWN WAS A BEVEL GEAR FAILURE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,359 hrs · 5,647 cycles

IAH- DURING MAINTENANCE INSPECTION, THE NUMBER TWO CEILING EMERGENCY LIGHT AND EXTERIOR RIGHT HAND FORWARD EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE LOOP — DIRTY (NR 1 ENGINE) · airframe 6,286 hrs · 5,597 cycles

IAH - FLIGHT 3439, MEM TO IAH, THE CREW REPORTED THAT THE ENGINE ONE FIRE LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT AT LOW POWER SETTINGS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. DISCONNECTED, CLEANED AND RE-CONNECTED THE NUMBER ONE ENGINE FIRE LOOP. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 5,052 hrs · 1,047 cycles

TYS - DURING A SCHEDULED INSPECTION THE OVERHEAD EMERGENCY LIGHT ASSEMBLE AT AISLE 9 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB IAW EMB MM 33-50-08, THE OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 4,192 hrs · 3,923 cycles

DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,192 hrs · 3,923 cycles

SHV- DURING C-CHECK THE INBOARD BUTTSTRAP BETWEEN FRAMES 14 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,192 hrs · 3,923 cycles

SHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED T-FRAME 18. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,192 hrs · 3,923 cycles

SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,192 hrs · 3,923 cycles

SHV-DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT NR 3217 THE CREW REPORTED THE EMERGENCY LIGHT OVERHEAD OF EXIT ROW IS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BULB ON THE OVERHEAD EMERGENCY LIGHT AT EXIT ROW 9. OPERATIONAL CHECKS WERE GOOD.

Part: COFFEEMAKER — FAULTY · airframe 2,502 hrs · 2,329 cycles

CLE---CO2162, CREW REPORTED, " STRONG BURNING SMELL IN GALLEY WITH AND WITHOUT GALLEY POWER ON." INSPECTED AND REPLACED HOT JUG AS REQUIRED. (OPS.CHECKED NO BURNING SMELL NOTED, AIRCRAFT RETURNED TO SERVICE.)

Part: WINDSHIELD — CRACKED (COCKPIT)

CLE FLIGHT 3237 THE CREW REPORTED THE CAPTAINS WINDSHIELD SHATTERED DURING CLIMBOUT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS WERE GOOD.

Part: VALVE — LEAKING (FORWARD FUSELAGE)

CLE FLIGHT#2980 THE CREW REPORTED A SLIGHT VIBRATION AND SAID IT SOUNDED LIKE THE NOSE GEAR DOORS WERE NOT FULLY CLOSING.MAINTENANCE REPLACED THE NOSE GEAR SOLENOID VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.