N14173

Part: NONE — NONE · airframe 36,826 hrs · 25,499 cycles

OVERWING EMERGENCY EXIT COVERS ARE LOOSE. RESECURED EMERGENCY EXIT COVERS

Part: NONE — NONE · airframe 36,718 hrs · 25,405 cycles

ROW 18 EMERGENCY LIGHTS DO NOT COME ON WHEN SWITCH IS ACTIVATED. CHARGED EMERGENCY LIGHT BATTERIES USING AC POWER. OPS CHECK OF EMERGENCY LIGHTS SAT. NO OTHER DEFECTS NOTED.

Part: LIGHT — UNSECURE (CABIN) · airframe 36,157 hrs · 24,911 cycles

EMERGENCY PATH LIGHTING STRIP NEAR 1A IS DISLODGED. SECURED IN PLACED EMERGENCY PATH LIGHTING STRIP NEAR 1A WITH TAPE.

Part: FAN — ODOR (CABIN) · airframe 35,864 hrs · 24,661 cycles

PLASTIC BURNING SMELL NEAR ROW 18, WITH VISIBLE SMOKE COMING FROM FLOOR VENT IN THE ISLE. FOUND CONDENSATION COMING FROM DISCONNECTED FAN #2 HOSE. RECONNECTED FAN #2 HOSE. NO SMOKE AND SMELL NOTED. OPS CHECK SAT.

Part: INSTRUMENT PANEL — MULTIPLE FAIL · airframe 35,780 hrs · 24,588 cycles

AVIONICS MASTER 2 LIGHTED WHILE PRESSED IN, CA MFD INOPERATIVE, FO PFD INOPERATIVE, #2 FMS INOPERATIVE, #2 RMU INOPERATIVE. R&R AVIONICS MASTER #2 PUSH BUTTON. PERFORMED AVIONICS MASTER SWITCH TEST. OPS CHECK SAT

Part: SEALANT — MISSING (LT MLG) · airframe 35,687 hrs · 24,507 cycles

REMOVED SEALANT AROUND THE RH AND LH MLG LOWER SIDE STRUT BEARING FLANGE. APPLIED SEALANT AROUND RH AND LH MLG LOWER SIDE STRUT BEARING.

Part: LIGHT — MISINSTALLED (EXTERIOR) · airframe 35,520 hrs · 24,358 cycles

LH AND RH EXTERIOR OVER-WING EMERGENCY EXIT LIGHTS ARE INSTALLED UPSIDE DOWN. REMOVED AND REINSTALLED LH AND RH EXTERIOR OVER-WING EMERGENCY LIGHT EXIT PANELS.

Part: SKIN — CHAFED (RUDDER) · airframe 35,403 hrs · 24,255 cycles

LT SIDE RUDDER 1, FRONT SPAR SKIN CHAFED ON 2 PLACES BETWEEN RIB ZV 2601.0 AND RIB ZV 3179.0. LT SIDE RUDDER 1, FRONT SPAR SKIN CHAFED ON 2 PLACES BETWEEN RIB ZV2601 AND ZV3179 BLENDED AREA FOR INVESTIGATION, CUT OUT DONE. LT SIDE RUDDER 1, FRONT SPAR SKIN REPAIRED.

Part: DOUBLER — CORRODED (CARGO BAY) · corrosion level 2 · airframe 35,403 hrs · 24,255 cycles

CARGO AREA UNDER FLOOR CORROSION FOUND RAD ALT ANTENNA. CORROSION LEVEL 2: AT REAR FUSELAGE RADIO ALT ANTENNA, DOUBLER AND LOUVER FOR INVESTIGATION CUT OUT DONE. CARGO AREA UNDER FLOOR RAD ALT ANTENNA REPAIR CARRIED OUT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 35,403 hrs · 24,255 cycles

CORROSION ON AFT SHEAR CLIP OF CARGO DOOR, AT FR 68 BETWEEN STR 15L-16L. ON AFT SHEAR CLIP OF CARGO DOOR, AT FR 68 BETWEEN STR 15L-16L CORROSION BLENDED OUT OF LIMITS. ON AFT SHEAR CLIP OF CARGO DOOR, AT FR 68 BETWEEN STR 15L-16L CUT. ON AFT SHEAR CLIP OF CARGO DOOR, AT FR 68 REPAIR CARRIED OUT.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 35,403 hrs · 24,255 cycles

RT OMEGA BEAM CORRODED ON TOP SURFACE (AFTER REMOVAL OF GUSSET) CORROSION LEVEL 2. RT OMEGA BEAM CORRODED ON TOP SURFACE BLENDED OUT OF LIMIT AT TWO PLACES. RT OMEGA BEAM DOUBLER REPAIRED PART LOCALLY FABRICATED. RT OMEGA BEAM CUT OUT AFT OF FR 59 AMD FWD OF FR 61. BOTH LOCATIONS REPAIRED.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 35,403 hrs · 24,255 cycles

CENTER OMEGA BEAM CORRODED ON TOP SURFACE (AFTER REMOVAL OF GUSSET) CORROSION LEVEL 2. CENTER OMEGA BEAM CORRODED ON TOP SURFACE BLENDED OUT OF LIMIT AT TWO PLACES. CENTER OMEGA DOUBLER REPAIRED PART LOCALLY FABRICATED. CENTER OMEGA BEAM AFT OF FR 59 AND FWD OF FR 61. CUT OUT PERFORMED. BOTH LOCATIONS REPAIRED.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 35,403 hrs · 24,255 cycles

LOWER FUSELAGE ANTENNA RAD ALT NO 1 INTERNAL DOUBLER CORRODED. CUT OUT DONE. DOUBLER HOLES PATTERN DRILLED ON SKIN. DOUBLER INSTALLED WITH FILLER.

Part: FLOOR SUPPORT — DAMAGED (FRAME 23) · airframe 35,403 hrs · 24,255 cycles

DAMAGE ON LT CENTER FUSE 1 BETWEEN FR 23 JUNCTION 03 AND BETWEEN STR 19L-20L. DAMAGE ON LT CENTER FUSE 1 BETWEEN FR 23 JUNCTION 03 AND BETWEEN STR 19L-20L, AREA STRIPPED FOR INVESTIGATION. AN EXISTING BLEND IS FOUND ON LT CENTER FUSE 1 BETWEEN FR 23 - JUNCTION 03 AND BETWEEN STR 19L-20L BLEND SENT FOR ENGINEERING REVIEW CUT OUT CARRIED OUT ON LT CENTER FUSE 1 BETWEEN FR 23 JUNCTION 03 AND BETWEEN STR 19L-20L SKIN REPAIRED.

Part: SPAR — CRACKED (PYLON) · airframe 35,403 hrs · 24,255 cycles

LT AND RT PYLON SPAR II 2X CRACK (ONE EACH SIDE) ON RIVET HOLE. 1 BUSHING (FLUSH-PYLON) LOCALLY FABRICATED, 1 BUSHING (PYLON) LOCALLY FABRICATED. DAMAGED HOLES ON LT + RT PYLON SPAR II AT ENGINE ATTACHMENT FITTINGS REPAIRED.

Part: DOUBLER — DAMAGED (FWD PRESS BLKHD) · airframe 35,403 hrs · 24,255 cycles

PRESS BULKHEAD DOUBLER REPAIR EVALUATION FWD PRESS BULKHEAD AND REMOVE THE DOUBLER INSTALLED ON THE FORWARD PRESSURE BULKHEAD. DOUBLER REMOVED FOR REPAIR EVALUATION. NEW DOUBLER FABRICATED. INSTALLED NEW DOUBLER. NTD INSPECTION C/OUT BT MAGNIFYING GLASS X30.

Part: SKIN — CORRODED (CARGO DRAIN AREA) · corrosion level 2 · airframe 35,403 hrs · 24,255 cycles

CARGO AREA UNDER FLOOR FR 67 AROUND WATER DRAIN SKIN SHOW SIGN OF CORROSION, CORROSION LEVEL 2. CARGO AREA UNDER FLOOR FR 67 AROUND WATER DRAIN SKIN SHOW SIGN OF CORROSION OUT OF LIMITS REMOVED BY CUT OUT. REPAIR PARTS FAB, REPAIR CARRIED OUT. FOR SKIN REPROTECTION AT CARGO AREA UNDER FLOOR FR 67 AROUND WATER DRAIN. CARGO AREA UNDER FLOOR FR 67 BETWEEN STR 21L-21R SHEAR CLIP FOUND CORRODED OUT OF LIMITS AND REPLACED.

Part: RIVET — MISSING (DOOR TRACK) · airframe 35,403 hrs · 24,255 cycles

BAGGAGE DOOR FWD TRACK RIVET MISSING LOWER END. AFTER INVESTIGATION BAGGAGE DOOR FWD TRACK FOUND CORRODED AND BLENDED OUT OF LIMITS AT RIVET HOLE LOCATION & 1 ANCHOR NUT HOLES BAGGAGE DOOR FWD 2 FRAME 65 REPAIRED.

Part: SKIN — CRACKED (FRM 75.7) · airframe 35,403 hrs · 24,255 cycles

RF 1 LT FUSELAGE SKIN AT FR 75.700 BELOW STGR 2L 2 CRACK FOUND AT ONE RIVET LOCATION. ON RF1 LT FUSELAGE SKIN AT FR 75.700 BELOW STGR 2L CUT OUT DONE. ON RF1 LT FUSELAGE SKIN AT FR 75.700 BELOW STGR 2L SKIN REPAIRED.

Part: FLOOR SUPPORT — CRACKED · airframe 35,403 hrs · 24,255 cycles

CF3, LT OMEGA BEAM OUTBD ANGLE CRACKED. CF3, LT OMEGA BEAM OUTBD ANGLE REPAIRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,186 hrs · 24,064 cycles

ISLE PATH EMERGENCY PHOTO-LUMINESCENT INCORRECT AT 1A WITH EMERGENCY RED MARKS. R&R PHOTO-LUMINESCENT FLOOR STRIP LIGHT. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,135 hrs · 24,015 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R SERVICE DOOR EXTERNAL EMERGENCY LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,893 hrs · 23,803 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT FLICKERS. REMOVED AND REPLACED EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: SIGN — UNSECURE (EMERGENCY LIGHTS) · airframe 33,572 hrs · 22,569 cycles

EXIT SIGN AT ROW 18 UNSECURED. RE-SECURED EXIT SIGN ON ROW 18. OPS CHECK SAT.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 33,442 hrs · 22,458 cycles

WHEN FLAP HANDLE WAS PLACED TO 0, FLAPS 9 INDICATED ON EICAS. R&R FLAP SELECTOR LEVER.

Part: ACM — SEIZED (AC BAY) · airframe 33,398 hrs · 22,421 cycles

SMOKE IN THE COCKPIT AND CABIN. FOUND NR 1 ACM SEIZED. REMOVED AND REPLACED ACM. OPS CHECK OF NR 1 ACM SAT.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 33,003 hrs · 22,096 cycles

BOTH OVER WING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY FOR OVER WING EXTERIOR EMERGENCY LIGHTS. OPS CHECK SAT.

Part: CRADLE — DEFECTIVE (CABIN) · airframe 32,972 hrs · 22,069 cycles

LT AND RT EXTERNAL EMERGENCY LIGHTS ON CENTER FAIRINGS INOPERATIVE. R&R NR 4 EMERGENCY BATTERY CRADLE. OPS CHECK SAT.

Part: SKIN — CORRODED (FRAMES 80-81) · airframe 32,855 hrs · 21,973 cycles

AIRCRAFT DATA PLATE FORWARD RIGHT RIVET IS LOOSE AND SKIN AREA AT FORWARD SIDE HAS SURFACE CORROSION. CORROSION EXTENDS 100% THROUGH SKIN AND REQUIRES CUT-OUT AND REPAIR. PERFORMED CUT-OUT AND FABRICATED DOUBLER OUT OF ALCLAD 2024T3, 040" AND FILLER OUT OF ALCLAD 2024T3, 032". PERFORMED HFEC INSPECTION OF CUTOUT. NO CRACKS DETECTED. TREATED AND PRIMED REPAIR DOUBLER, FILLER, AND CUT OUT. INSTALLED DOUBLER AND FILLER IN THE INSTALLATION POSITIONS AND RELOCATED NAME PLATES AT ADJACENT BAY.

Part: STRUCTURE — CORRODED (VERTICAL STAB) · airframe 30,472 hrs · 20,479 cycles

A/C IS IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LT VERTICAL STAB WITH CORROSION. MAINTENANCE REMOVED THE CORROSION OF THE VERTICAL STAB IAW SRM 55-30-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: STRUCTURE — CORRODED (VERTICAL STAB) · airframe 30,472 hrs · 20,479 cycles

A/C IS IN A C-CHECK STATUS WHEN INSPECTION FOUND THE RT VERTICAL STAB WITH CORROSION. MAINTENANCE REMOVED THE CORROSION IAW WITH SRM 55-30-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 30,742 hrs · 20,479 cycles

CARGO DOOR CUT-OUT AT FRAME 65 LOWER SHEAR TIE CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SHEAR TIE.

Part: PROFILE — DAMAGED (CARGO DOOR) · airframe 30,742 hrs · 20,479 cycles

CARGO DOOR LOWER PROFILE IS DAMAGED ON FORWARD LOWER CORNER. REMOVED AND REPLACED LOWER PROFILE, PRIMED AND PAINTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,013 hrs · 19,281 cycles

EMERGENCY LIGHTS OPERATING OFF THE NR 2 EMERGENCY LIGHT BATTERY ARE INOP. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY. OPS CHECK GOOD.

Part: CARBON SEAL — LEAKING (ENGINE) · airframe 29,013 hrs · 19,281 cycles

WHEN OPERATING ON ENGINE BLEEDS WITH PACKS ON, THERE WAS A SMELL OF OIL IN THE FLIGHT DECK WHEN AT LOW POWER SETTINGS. REMOVED AND REPLACED CARBON SEAL. OPS AND LEAK CHECKED GOOD. THIS AIRCRAFT WAS OUT OF SERVICE FROM 12/5/16 TO 12/18/16

Part: ACM — FAILED (NR 1) · airframe 27,839 hrs · 18,430 cycles

THE CREW REPORTED SMOKE IN COCKPIT AND CABIN. MAINTENANCE INSPECTED AND REPLACED THE PACK NR 1 ACM. OPS CHECKS WERE GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,161 hrs · 17,950 cycles

DURING MAINTENANCE INSPECTION THE CEILING EMERGENCY LIGHTS ABOVE ROW 12 AND LT/RT OVERWING EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE R & R NR 4 EMERGENCY LIGHT BATTERY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,553 hrs · 17,539 cycles

DURING MAINTENANCE INSPECTION, THE NR 3 EMERGENCY LIGHT BATTERY WAS DISCOVERED INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT BATTERY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,038 hrs · 17,183 cycles

DURING ROUTINE MAINTENANCE THE LT SERVICE DOOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 25,402 hrs · 16,712 cycles

DURING MAINTENANCE INSPECTION, THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R A BLOWN FUSE IN THE NR 4 EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED THE LIGHTS WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FRAME 65-68) · airframe 24,788 hrs · 16,281 cycles

CARGO LOWER BEAM CORRODED BETWEEN FRAMES 65-68. R & R CARGO DOOR LOWER CUTOUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FRAMES 20-22) · airframe 24,788 hrs · 16,281 cycles

SERVICE DOOR SILL CORRODED BETWEEN FRAMES 20-22. R & R DOOR SILL IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — ODOR (LAVATORY) · airframe 24,177 hrs · 15,837 cycles

THE CREW REPORTED AN ELECTRICAL BURNING ODOR FROM THE LAVATORY LIGHT AFTER THE LATCH WAS CLOSED. THE ACFT LANDED WITHOUT INCIDENT. R & R THE LIGHT BALLAST, OPS TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,854 hrs · 15,617 cycles

DURING MAINTENANCE INSPECTION, BOTH AFT EXTERIOR OVERWING EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER ASSY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 23,842 hrs · 15,606 cycles

CREW REPORTED A LAVATORY SMOKE WARNING ON EICAS AFTER TAKEOFF. ACFT PERFORMED AN AIR TURN BACK WHERE IT LANDED WITHOUT INCIDENT. NR 2 ENGINE WAS R & R AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 20,889 hrs · 13,696 cycles

DURING 2A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 79 BELOW STRINGER 05R. MX REMOVED THE DAMAGE AROUND THE RIVET AND PERFORMED A BUSHING REPAIR IAW DER APPROVED TECHL DISPOSITION ETD2013-145-029290, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 08/15/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 20,889 hrs · 13,696 cycles

DURING 2A INSPECTION, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77 BELOW STRINGER 03L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW DER APPROVED TECH DISPOSITION ETD2013-145-029290, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 08/15/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 20,889 hrs · 13,696 cycles

DURING 2A INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE A CRACK AT A RIVET ON FRAME 77 BELOW STRINGER 08L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW DER APPROVED TECH DISPOSITION ETD2013-145-029290, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 08/15/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 20,889 hrs · 13,696 cycles

DURING 2A INSP THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE 2 EA CRACKS TOTALING 3.01MM (.118") IN LENGTH AT A RIVET ON FRAME 79 BELOW STRINGER 06L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW DER APPROVED TECH DISPOSITION ETD2013-145-029290, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 08/15/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 20,889 hrs · 13,696 cycles

DURING 2A INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE 3 EA CRACKS TOTALING 6.74MM (.026") AT A RIVET ON FRAME 79 BELOW STRINGER 05L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW DER APPROVED TECH DISPOSITION ETD2013-145-029290, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 08/15/13.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,951 hrs · 13,075 cycles

DURING SCHEDULED MX INSPECTION EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. MX R & R BATTERY CHARGER ASSY, OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,487 hrs · 12,767 cycles

DURING ROUTINE MX, BOTH LT AND RT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED THE NR 4 BATTERY SUPPLY CHARGER. OPS CHECKED GOOD.

Part: CONNECTOR — BURNED (NR 2 SPOILER) · airframe 12,667 hrs · 19,317 cycles

THE RT SPOILER DEPLOYED DURING FLIGHT, UNCOMMANDED. ACFT LANDED WHERE MX R & R THE RT INBD PROX SWITCH CONNECTOR PLUG IAW SWPM20-50-00. PERFORMED SPOILER OPS CHECKS IAW AMM 27-63-01. OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,249 hrs · 12,619 cycles

DURING MX INSP THE LT AND RT OVERWING EMERGENCY EXIT LIGHTS WERE FOIUND TO BE INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH FITTING — GOUGED (LT AILERON) · airframe 19,074 hrs · 12,497 cycles

DURING C-CHECK, LT AILERON INBD PCA ATTACHMENT FITTING GOUGED. MX R & R LT AILERON INBD PCA ATTACHMENT FITTING IAW EC5750-01177. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,074 hrs · 12,497 cycles

DURING C-CHECK BAGGAGE DOOR CUTOUT CENTER SILL CORRODED. MX R & R BAGGAGE DOOR CUT OUT CENTER SILL LOWER BEAM FOR CARGO DOOR IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (ZONE 900) · corrosion level 2 · airframe 19,074 hrs · 12,497 cycles

DURING C-CHECK, TOILET WASTE VALVE SUPPORT CORRODED. MX R & R WASTE DRAIN DUMP SUPPORT ASSY IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (LT SPOILER) · airframe 19,074 hrs · 12,497 cycles

DURING C-CHECK, LT SPOILER INBD HINGE OTBD HAT BUSHING MIGRATED. MX REMOVED LT SPOILER INBD HINGE OTBD HAT BUSHING, MEASURED HOLE AND REINSTALLED HAT BUSHING IAW EC5740-01152. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: NUT PLATE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 19,074 hrs · 12,497 cycles

DURING C-CHECK, MAIN DOOR LOWER STRUCTURE NUTPLATE HOLES CORRODED. MX PERFORMED REPAIR OF MAIN DOOR LOWER STRUCTURE NUTPLATE HOLES IAW EC5210-01154. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (RT SPOILER) · airframe 19,074 hrs · 12,497 cycles

DURING C-CHECK, RT GROUND SPOILER OTBD HINGE INBD HAT BUSHING MIGRATED. MX R & R GROUND SPOILER OTBD HINGE INBD HAT BUSHING IAW EC5740-01152, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (RT SPOILER) · airframe 19,074 hrs · 12,497 cycles

DURING C-CHECK, RT GROUND SPOILER INBD HINGE, OTBD HAT BUSHING MIGRATED. MX R & R RT GROUND SPOILER INBD HINGE, OTBD HAT BUSHING IAW EC5740-01152, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DRAIN VALVE — CORRODED (ZONE 900) · corrosion level 2 · airframe 19,074 hrs · 12,497 cycles

DURING C-CHECK WASTE DRAIN VALVE HOUSING CORRODED AROUND DUMP VALVE AND TEE HANDLE. MX R & R WASTE DRAIN DUMP SUPPORT ASSY IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (RT SPOILER) · airframe 19,074 hrs · 12,497 cycles

DURING C-CHECK, RT SPEED BRAKE ACTUATOR UPPER INBD HAT BUSHING MIGRATED. MX R & R RT SPEED BRAKE ACTUATOR UPPER INBD HAT BUSHING IAW EC5740-01152, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — DAMAGED (CARGO DOOR) · airframe 19,074 hrs · 12,497 cycles

DURING C-CHECK, BAGGAGE DOOR INTERNAL FRAME HAS TOOLING MARKS AROUND NUTPLATE HOLES. MX REPAIRED BAGGAGE DOOR INTERNAL FRAME TOOLING MARKS AROUND NUTPLATE HOLES IAW SRM 51-10-03. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (ZONE 600) · airframe 19,074 hrs · 12,497 cycles

DURING C-CHECK, RT GROUND SPOILER ACTUATOR UPPER INBD HAT BUSHING MIGRATED. MX R & R RT GROUND SPOILER ACTUATOR UPPER INBD HAT BUSHING IAW EC5740-01152, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,856 hrs · 11,679 cycles

THE CREW REPORTED A BURNING ODOR WITH APU START, IN COCKPIT. MX INSPECTED THE ACFT WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAL — DAMAGED (PAX DOOR) · airframe 17,015 hrs · 11,139 cycles

MAIN CABIN (PAX) DOOR HARD TO OPEN AND CLOSE. R & R PAX DOOR FRAME SEAL. OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 27,197 hrs · 20,633 cycles

RT OMEGA BEAM CAP FROM FRM 59 TO 61 CORRODED. R & R GUSSET.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 15,988 hrs · 10,405 cycles

THE CREW REPORTED NR 2 ENGINE HAD A HUNG START WITH A STRONG FUEL SMELL IN THE CABIN WITH WHITE SMOKE COMING FROM THE ENGINE. MAINTENANCE CONTROL HAD THE CREW PERFORM A SYSTEM RESET AND OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — FAULTY (CABIN) · airframe 14,002 hrs · 9,109 cycles

DURING ROUTINE MAINTENANCE THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD.

Part: GCU — FAULTY (COCKPIT) · airframe 21,663 hrs · 16,177 cycles

CLE FLT 5839 THE CREW REPORTED AN APU GENERATOR OFF BUS MESSAGE ON TAKEOFF. MAINTENANCE REPLACED THE APU GENERATOR CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: FUSE — BLOWN (CABIN) · airframe 12,447 hrs · 7,632 cycles

LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED NR 4 BATTERY TRAY FUSES IAW CMM 25-60-05, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 12,168 hrs · 7,359 cycles

ORD FLT 5779 THE CREW REPORTED A NR 1 HYDRAULIC SYSTEM FAIL MESSAGE AFTER LANDING. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,958 hrs · 6,228 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND NR 2 EMERGENCY LIGHT BATTERY LIGHTS DIM. RIC MX REMOVED AND REPLACED NR 2 BATTERY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BRAKE ASSY — DRAGGING (NR 3)

DEN - FLIGHT 7790 - AFTER TAKEOFF PERFORMED AIR RETURN DUE TO LANDING GEAR LEVER DISAGREE - RT MAIN LANDING GEAR WOULD NOT RETRACT DUE TO BLOWN TIRE. MAINTENANCE REMOVED AND REPLACED THE NR 3 BRAKE ASSEMBLY IAW EMB 145XR AMM 32-49-03, NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES, RT MLG AUXILLARY BRACE STRUT AND DOWNLOCK ACTUATOR/MOUNT BRACKET/HARNESS/PROXIMITY SWITCH, AND VARIOUS LINES AND BRACKETS IN THE WHEEL WELL. THE RT ENG REQUIRED 3 FAN BLADES AND 14 OUTER BYPASS VANES REPLACED FOR FOD DAMAGE. THE ACFT WAS APPROVED FOR FERRY FLIGHT TO SHV FOR FURTHER MAINTENANCE. MAINTENANCE AT SHV REMOVED AND REPLACED THE RT INBOARD FLAP, FLAP SHROUD, AND REPAIRED MINOR SKIN DAMAGE TO THE RT WING LOWER SURFACE. RT ENG VIBRATION CHECKS WERE ALSO PERFORMED. THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 8/06/08 AT 0200. (S)

Part: BRAKE ASSY — DRAGGING (NR 3)

AIR RETURN DUE TO LANDING GEAR LEVER DISAGREE-RT MAIN GEAR NOT RETRACTING DUE TO BLOWN TIRE. (S)

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 9,624 hrs · 5,353 cycles

SHV - DURING C-CHECK IT WAS FOUND THAT THE CARGO DOOR THRESHOLD WAS CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRESHOLD IAW EMB 145XR SRM 51-40-02 AND CONTINENTAL EXPRESS EC 5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 7,288 hrs · 3,927 cycles

IAD - DURING ROUTINE MAINTENANCE, MX FOUND RIGHT OVERWING EMERGENCY LIGHT EXIT INOP. MX PROCEED WITH TROUBLESHOOTING AND FOUND INVERTER INOP. MX REMOVED AND REPLACED INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,716 hrs · 2,516 cycles

SHV-DURING C CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145XR SRM 53-00-10, FIG. 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.