N14198

Part: UNKNOWN — ODOR (CABIN) · airframe 39,942 hrs · 28,016 cycles

FOUL AIR SMELL COMING FROM AIR CONDITIONING IN CABIN AND FLIGHT DECK THROUGHOUT THE FLIGHT (OILY SMELL). INSPECTED E1, E2 AND APU FOR OIL LEAKS. NO OIL LEAKS NOTED. FOUND DEBRIS IN GROUND AIR INTAKE DUCT. CLEANED AND RAN BOTH PACKS. NO SMELL NOTED AT THIS TIME.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 39,609 hrs · 27,675 cycles

LH LOWER EMERGENCY EXIT DOOR SIGN INOPERATIVE. REMOVED AND REINSTALLED EMERGENCY EXIT MARKING SIGN AT LH LOWER CABIN ESCAPE HATCH. OPS CHECK SAT.

Part: SKIN — DENTED (ZONE 100) · airframe 39,449 hrs · 27,524 cycles

DENTS ON RH CENTER FUSE I SKIN, BTW SKIN JUNCTION 02 AND FR 15 AND BTW STR 16R-17R. REPAIR DOUBLER ON RH CENTER FUSE I SKIN, BTW FR 14-15 AND BTW STR 16R-17R

Part: REPAIR — DAMAGED (ZONE 200) · airframe 39,449 hrs · 27,524 cycles

REPAIR DOUBLER ON LH CENTER FUSE I SKIN, BTW FR 19-20 AND BTW STR 14L-15L. REPAIR DOUBLER REMOVED TO INVESTIGATE ON LH CENTER FUSE I SKIN BTW FR19-20 AND BTW STR 14L-15L. LH CENTER FUSE I SKIN REPAIR.

Part: SKIN — DAMAGED (ZONE 300) · airframe 39,449 hrs · 27,524 cycles

MIDDLE OF RUDDER II, LH SKIN, RIVETS HOLES ELONGATED ON ANCHOR NUT FOR RUDDER DEFLECTION TOOL INSTALLATION. REPAIR DOUBLER ON LH RUDDER II SKIN BTW RIB ZV2067-ZV2357

Part: RIVET — LOOSE (ZONE 300) · airframe 39,449 hrs · 27,524 cycles

MIDDLE OF RUDDER I, LH SKIN RIVETS LOOSE ON ANCHOR NUT FOR RUDDER DEFLECTION TOOL INSTALLATION. REPAIR DOUBLER ON LH RUDDER I SKIN BTW RIB ZV2312-ZV2601

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,449 hrs · 27,524 cycles

CARGO DOOR ENTRY, LOWER BEAM FOUND CORRODED. LOWER BEAM REMOVED AND REPLACED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 39,449 hrs · 27,524 cycles

REAR FUSELAGE I, FRAME 66, BTW STR 6L-7L, SHEAR CLIP FOUND CRACKED. RF I, FR66 BTW STR 6L-7L SHEAR CLIP REMOVED FOR REPLACEMENT. SHEAR CLIP FR66 MADE REPAIR PART, LOCALLY FABRICATED. REAR FUSE I, FR66 BTW STR 6L-7L, SHEAR CLIP FABRICATED INSTALLED.

Part: REPAIR — DAMAGED (ZONE 200) · airframe 39,449 hrs · 27,524 cycles

REPAIR DOUBLER ON LH CENTER FUSE I SKIN BTW FR20-21 AND BTW STR 13L-14L. LH CENTER FUSE I, SKIN BTW FR 20-21 AND BTW STR 13L - 14L DOUBLER REMOVED. SKIN REPAIRED BTW FR20-21 AND BTW STR 13L-14L

Part: PANEL — CRACKED (COCKPIT) · airframe 39,449 hrs · 27,524 cycles

HORIZONTAL - OVERHEAD PANEL IN COCKPIT FOUND CRACKED IN 2 PLACES. AFTER NDT INVESTIGATION, ONLY 1 CRACK FOUND ON RH SIDE. RH SIDE CRACK CUTOUT. RH SIDE REPAIRED.

Part: SKIN — DENTED (ZONE 200) · airframe 39,449 hrs · 27,524 cycles

EXTERNAL CENTER FUSELAGE, SKIN DENTED BTW FRAME 19-20 AND BTW STR 11L-12L. EXTERNAL CENTER FUSE, BTW FR 19-20 AT STR 11L. EXISTING RIVET REMOVED FOR REPAIR DOUBLER. EXTERNAL CENTER FUSELAGE I, SKIN BTW FR19-20 AND BTW 11L-12L DENT REPAIRED.

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,449 hrs · 27,524 cycles

CF IV, CENTER BEAM FOUND CORRODED BTW FR 59-61. CF4, CENTER BEAM BTW FR59-61 CORRODED OUT OF LIMIT. CF4, CENTER BEAM BTW FR 59-61 CUTOUT (2X) PERFORMED. CENTER BEAM BTW FR59-61 (2X) REPAIR DONE

Part: SPAR — CRACKED (ZONE 300) · airframe 39,449 hrs · 27,524 cycles

VERT STAB AFT OF REAR SPAR 3, LH SKIN UPPER AND LOWER PROFILE CRACKED. REMOVED AND REPLACED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 39,449 hrs · 27,524 cycles

IN REAR FUSELAGE, AT BULKHEAD 80, SHEAR CLIP CRACKED ON LH SIDE BETWEEN STRINGER 5L AND STRINGER 7L. IN REAR FUSELAGE AT BULKHEAD 80, SHEAR CLIP BTW STR 5L-7L PARTIALLY REMOVED. IN REAR FUSELAGE AT BULKHEAD 80, SHEAR CLIP BTW STR 5L AND 7L REPLACED

Part: FAIRING — CRACKED (ZONE 100) · airframe 39,449 hrs · 27,524 cycles

AFT BODY FAIRING ON THE RH SIDE, ONE RIB IS CRACKED. AFT BODY FAIRING ON THE RH SIDE, ONE RIB REMOVED AND REPLACED

Part: GUSSET — CORRODED (ZONE 200) · airframe 39,449 hrs · 27,524 cycles

CENTER FUSELAGE IV, CENTER GUSSET BTW FRAME 59-61 FOUND CORRODED. CF4, CENTER GUSSET BTW FR 59-61 CORRODED OUT OF LIMITS. GUSSET REMOVED FOR REPLACEMENT. GUSSET CENTER BTW FR 59-61 REPLACED

Part: SKIN — CRACKED (ZONE 200) · airframe 39,449 hrs · 27,524 cycles

CRACK FOUND AROUND RIVET ON LH REAR FUSE II SKIN AT FR 79 STR 7L-8L. CRACK AROUND RIVET AT SKIN FR79 BTW STR 7L-8L REPAIRED

Part: TEE ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,449 hrs · 27,524 cycles

REAR FUSELAGE 1, LH T-POST AT FR61 FOUND CORRODED. RF1, LH T-POST AT FR61 BLENDED OUT OF LIMITS. LH T-POST AT FR61 REMOVED FOR REPLACEMENT. LH T-POST NEW PART INSTALLED.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,449 hrs · 27,524 cycles

CENTER FUSELAGE 1, AT FRAME 14 AND STR 16L, REINFORCEMENT ANGLE FOUND CRACKED. AT CF1, AT FR 14 STR 16L REINFORCEMENT ANGLE REMOVED FOR REPLACEMENT. AT CF1 AT FR14 STR 16L REINFORCEMENT ANGLE REPLACED

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,449 hrs · 27,524 cycles

REAR FUSELAGE I, LH SILL BTW FRAME 61-65 FOUND CORRODED. LH SILL BTW FR 64-65 BLENDED OUT OF LIMIT. REAR FUSELAGE I, LH CARBON BULKHEAD REMOVED FOR ACCESS. RF I, L SILL BTW FR 61-65 REMOVED FOR REPLACEMENT. RF1, LH SILL BTW FR61-65 INSTALLED. RD1, LH CARBON BULKHEAD REINSTALLED

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,449 hrs · 27,524 cycles

CENTER FUSELAGE II, RH SILL BTW FRAME 29-35 FOUND CORRODED. CENTER FUSELAGE II, RH SILL BTW FR 29-35, CORROSION BLENDED OUT OF LIMIT. RH SILL BTW FR 29-35 REMOVED FOR REPLACEMENT. AT CF2, RH SILL BTW FR29-35 REPLACED

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,449 hrs · 27,524 cycles

CENTER FUSELAGE III, RH SILL BTW FRAME 35-41 FOUND CORRODED. RH SILL BTW FR 35-41 BLENDED OUT OF LIMITS. RH SILL BTW FR 35-41 REMOVED FOR REPLACEMENT. ON CF III, RH SILL BTW FR 35-41 REPLACED

Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · airframe 39,449 hrs · 27,524 cycles

CENTER FUSELAGE III, LH OMEGA BEAM BTW FRAME 50-46, OUTBD ANGLE, SURFACE BARE METAL. AFTER BEING CLEANED, FOUND TO BE CRACKED, REMOVED AND REPLACED.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 39,449 hrs · 27,525 cycles

REAR FUSELAGE I, BTW FRAME 67-68 AT BTW STR 4R-5R, SUPPORT FOUND CRACKED. REAR FUSELAGE I, BTW FRAME 67-68 BTW STR 4R-5R, SUPPORT REMOVED FOR REPLACEMENT. REAR FUSELAGE I, BTW FR 67-68 AT BTW STR 4R-5R SUPPORT REPLACED WITH NEW PART.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 39,095 hrs · 27,215 cycles

LH OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,764 hrs · 26,916 cycles

SERVICE DOOR UPPER EXIT SIGN EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR UPPER EXIT SIGN EMERGENCY LIGHT. OPS CHECK FAIL. REMOVED AND REPLACED INVERTER ASSEMBLY. OPS CHECK SAT

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,104 hrs · 26,306 cycles

SERVICE DOOR CEILING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPS CHECK SAT.

Part: SHAFT — LOOSE (MAIN CARGO DOOR) · airframe 36,131 hrs · 24,521 cycles

MCD WONT OPEN FROM INSIDE. INSPECTED AND FOUND MCD INTERNAL HANDLE LOOSE IN SHAFT, TIGHTENED HANDLE BOLT. OPS CHECK GOOD, NO ADJUSTMENTS MADE.

Part: NONE — UNKNOWN · airframe 36,066 hrs · 24,465 cycles

FUMES IN THE CABIN AND COCKPIT. SMOKE IN THE CABIN. REMOVED AND REPLACED #1 WS TEMP CONTROLLER. NO FURTHER FAULTS FOUND. FOUND DAMAGE ON #1 WS TEMP CONTROLLER. REPLACED THERMAL END ON #1 WS TEMP CONTOLLER. INSPECTED #3 PITOT AND RELAYS. NO DAMAGE FOUND. COMPLIED WITH WINDSHIELD HEATING SYSTEM. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE · airframe 35,826 hrs · 24,254 cycles

PHOTOLUMINESCENT STRIP NEAR GALLEY LOOSE. RESECURED PHOTOLUMINESCENT STRIP

Part: LAMP — INOPERATIVE · airframe 35,688 hrs · 24,129 cycles

EMERGENCY LIGHT AT CELING PANEL 243DLC INOP. R/R EMERGENY LIGHT LAMP AT CELING PANEL 243DLC

Part: LAMP — INOPERATIVE · airframe 35,688 hrs · 24,129 cycles

EMERGENCY LIGHT OVER SEAT 18A INOP. R/R EMERGENCY LIGHT LAMP OVER SEAT 18A. OPS CHECK SAT.

Part: BATTERY — OVERTEMP · airframe 35,232 hrs · 23,715 cycles

BATT 2 OVERTEMP EICAS MESSAGE. REPLACED #2 MAIN BATTERY AND OPS CHECKED GOOD,

Part: STRAP — MISSING · airframe 35,161 hrs · 23,651 cycles

FLOOR EMERGENCY LIGHT STRIP MISSING BY GALLEY. REPLACED EMERGENCY LIGHT STRIP.

Part: NONE — NONE · airframe 34,911 hrs · 23,432 cycles

LH AND RH OVERWING EXTERNAL EMERGENCY EXIT LIGHTS ARE INSTALLED UPSIDE DOWN. REMOVED AND REINSTALLED EXTERNAL EMERGENCY LIGHTS.

Part: STRAP — MISSING · airframe 34,790 hrs · 23,315 cycles

EMERGENCY EXIT LIGHTING STRIP MISSING BY 1A. R&R EMERGENCY EXIT LIGHTING STRIP.

Part: NONE — NONE · airframe 34,740 hrs · 23,269 cycles

NICKS FOUND ON TOP SKIN AROUND EXISTING REPAIR DOUBLER BTW FR 54 TO 55 AND STR 1R TO 1L IN CENTER FUSE IV AREA. ON TOP SKIN AROUND EXISTING REPAIR DOUBLER BTW FR 54 TO 55 AND STR 1R-1L, NICKS FOUND OUT OF LIMITS. ON TOP FUSE BTW FR 54 TO 55 AND STR 1R TO 1L SKIN REPAIRED

Part: NONE — NONE · airframe 34,740 hrs · 23,269 cycles

2 DENT FOUND SKIN BTW FR 6 AND JUN 1 BTW STR 13-15 LH. ON LH FWD FUSE 1 SKIN, BTW FR 6-7 AND BTW STR 13L-15L DENTS (2X) ARE OUT OF LIMITS. PERFORMED CUT OUT AND FABRICATED REPAIR DOUBLER AND QTY 2 FILLERS. INSTALLED REPAIR DOUBLER & 2 FILLERS ON SKIN BTW FR56 AND JUNCTION 1 AND BTW STR 13-15

Part: NONE — NONE · airframe 34,740 hrs · 23,269 cycles

AS PER CUSTOMER REQUEST, REPAIR DOUBLER ON RH CENTER FUSE 1 BTW FR 22A-23 AND BTW STR 13R-14R, NEED TO BE REMOVED FOR INVESTIGATION. REMOVED REPAIR DOUBLER ON RH CENTER FUSE 1 BTW FR 22A-23 & BTW STR 13R-14R FOR INVESTIGATION. CUT AWAY DAMAGE ON RH CENTER FUSE 1 BTW FR 22A-23 AND BTW 14R-15R. SKIN ON RH CENTER FUSE 1 BTW FR 22A-23 AND BTW STR 13R-14R REPAIRED

Part: NONE — NONE · corrosion level 2 · airframe 34,740 hrs · 23,269 cycles

CORROSION FOUND ON LH AFT L-SHAPE CARGO DOOR SURROUND STRUCTURE AT FR68 BTW STR 15-17. AT FR 68 BTW STR 15 AND 17 SHEAR CLIP BLENDED AND FOUND OUT OF LIMIT. "L" SHAPE AT FR68 BTW STR 15-17 LOCALLY FABRICATED. RPAIR PARTS INSTALLED ("L" SHAPE) AT CARGO DOOR FR68

Part: NONE — NONE · airframe 34,740 hrs · 23,269 cycles

SMALL DENT FOUND IN BOTTOM CORNER OF MAIN DOOR. CUT OUT PERFORMED, FILLER AND DOUBLER FABRICATED. DENT ON BOTTOM AFT CORNER OF THE MAIN DOOR REPAIRED.

Part: NONE — NONE · airframe 34,740 hrs · 23,269 cycles

CF1, BTW FR 13-14 AND BTW STR 10R-11R, SKIN DAMAGED DURING RIVET REPLACEMENT. BTW FR 13-14 AND BTW STR 10-11 RH REPAIR ON SKIN PERFORMED

Part: NONE — NONE · airframe 34,740 hrs · 23,269 cycles

DENT FOUND ON EXTERNAL SKIN BTW FR 79-80 AND BTW STR 11LH - 12LH. ON LH REAR FUSE 2 SKIN, AFTER INVESTIGATION, DENT IS LOCATED BTW FR80-81 AND BTW STR 11L-13L. DENT IS OUT OF LIMITS. PAINT STRIPPED FOR INVESTIGATION AT DENT LOCATION. DENT ON EXTERNAL SKIN BTW FR80-81 AND BTW STR 11L-13L REPAIRED.

Part: NONE — NONE · airframe 34,740 hrs · 23,269 cycles

CRACK FOUND ON LH FRAME 59 BTW STR 15L-16L IN CF IV AREA. LH FRAME 59 REPAIR FRAME SEGMENT AND SPLICE FABRICATED. LH FRAME 59 REPAIR PERFORMED BTW STR 14L-18L WITH NEW FABRICATED FRAME SEGMENT AND SPLICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,765 hrs · 22,397 cycles

SERVICE DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. SWAPPED EMERGENCY BATTERY CHARGER ASSEMBLY AND BATTER POWER SUPPLY 1 & 2 FOR TROUBLESHOOTING PURPOSES. OPERATIONS CHECK FAILED. SLAVED EXIT SIGN PANEL. OPERATIONS FAILED. R & R EMERGENCY LIGHT INVERTER. OPERATIONS CHECK SATISFACTORY. RETURNED EMERGENCY BATTERY/CHARGER ASSEMBLY AND EXIT SIGN PANEL ASSEMBLY TO ORIGINAL POSITIONS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,585 hrs · 22,232 cycles

MAIN CABIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT ASSEMBLY. OPERATIONS CHECK SATISFACTORY.

Part: STRUCTURE — CORRODED · airframe 33,585 hrs · 22,232 cycles

CORROSION AROUND A/C DATA PLATE LOCATED AT AFT EXTERIOR OF A/C. PERFORMED HFEC INSPECTION OF SKIN CUTOUT AT DATA PLATE AREA. NO INDICATIONS NOTED. PERFORMED CUT OUT AFFECTED AREA AND REMOVED DATA PLATED. FABRICATED DOUBLER, FILLER AND APPLIED CHEMICAL CONVERSION COMPOUND INCLUDING REWORKED AREA. COMPLETED REPAIR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,219 hrs · 21,928 cycles

MAIN DOOR HINGE EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R MCD EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,740 hrs · 21,518 cycles

LH EMERGENCY ROW LIGHT INOPERATIVE. R&R LH OVER WING EMERGENCY LIGHT BULB. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,488 hrs · 21,262 cycles

MAIN DOOR HINGE EMERGENCY LIGHT INOPERATIVE. R&R EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,488 hrs · 21,262 cycles

SERVICE DOOR UPPER EMERGENCY LIGHT INOPERATIVE. R&R SERVICE DOOR EXIT MARKING SIGN ASSEMBLY. OPS CHECK SAT.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,014 hrs · 20,815 cycles

OVHD EMER EXIT SIGN ABOVE SERVICE DOOR INOPERATIVE. R&R OVHD EMERGENCY EXIT SIGN ABOVE SERVICE DOOR. OPS CHECK SAT.

Part: ELECTRONIC UNIT — MALFUNCTIONED (MLG HANDLE) · airframe 31,027 hrs · 19,922 cycles

LG/LEVER DISAGREE MESSAGE ON EICAS DURING APPROACH. SHOWED ALL 3 RED LIGHTS. RECEIVED GREEN INDICATIONS AFTER TOUCHDOWN. R&R LGEU. OPS CHECK SAT. OCF REQUIRED. INSPECTED THE OPS CHECK OF LANDING GEAR. OPS CHECK SAT OF LANDING GEAR SWING AND FREE FALL.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 30,054 hrs · 18,980 cycles

EMERGENCY LIGHTS FLICKERING ON UNCOMMANDED. FOUND FUSE F0004 BLOWN. R & R THE FUSE F0004. OPS CHECK GOOD.

Part: FRAME — CORRODED (FRM 65) · corrosion level 2 · airframe 29,996 hrs · 18,922 cycles

DURING A C-CHECK, CORROSION WAS FOUND AT FRAME 65 CARGO DOOR CUTOUT, LOWER SIDE.

Part: FLOOR SUPPORT — CORRODED (FRAME 22) · airframe 29,996 hrs · 18,922 cycles

DURING C-CHECK, CORROSION WAS FOUND AT THE FWD WET AREA RT OMEGA BEAM HAT SECTION AT FRAME 22.

Part: SUPPORT — CRACKED (FRAMES 10-12) · airframe 29,996 hrs · 18,922 cycles

DURING C-CHECK, A CRACK WAS DISCOVERED IN THE OVERHEAD PANEL FRAME ON THE PILOTS SIDE ABOVE THE DV WINDOW. PART WAS 98% COMPROMISED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 29,585 hrs · 18,518 cycles

FIRST OFFICER`S WINDSHIELD CRACKED. R & R THE WINDSHIELD IAW AMM 56-10-01, OPS AND LEAK CHECKED GOOD.

Part: LIGHT — UNKNOWN (CABIN) · airframe 29,462 hrs · 18,384 cycles

CABIN EMERGENCY LIGHTS OUT. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS SYSTEM OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,309 hrs · 18,217 cycles

FWD CABIN BULKHEAD EMERGENCY LIGHT WILL NOT ILLUMINATE. PERFORMED OPS CK IRW AMM 33-50-00.

Part: LIGHT — MISSING (CABIN) · airframe 29,219 hrs · 18,134 cycles

CABIN EMERGENCY LIGHT STRIP HAS A SEGMENT MISSING. REPLACED CABIN EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,192 hrs · 18,112 cycles

CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED, CHARGED, AND REINSTALLED TH EEMERGENCY BATTERIES. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: LIGHT — MALFUNCTIONED (ROW 18) · airframe 28,249 hrs · 17,239 cycles

ROW 18 EMERGENCY LIGHTS INOPERATIVE. CHECKED SPLICES 9124, 9125, 9126 & 9127. NO DEFECTS NOTED. OPS CHECK PERFORMED. OPS CHECK GOOD.

Part: BATTERY PACK — UNSECURE (EMERGENCY LIGHT) · airframe 28,091 hrs · 17,105 cycles

CEILING EMERGENCY LIGHT AT ROW 7 INOPERATIVE. RESEATED EMERGENCY EXIT BATTERY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,085 hrs · 17,099 cycles

GALLEY EMERGENCY LIGHT INOPERATIVE. ADJUSTED THE LIGHT BULB. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,085 hrs · 17,099 cycles

EMERGENCY LIGHT AT ROW 18 INOPERATIVE. ADJUSTED THE BULB. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,997 hrs · 17,008 cycles

GALLEY EMERGENCY LIGHT AND OVERHEAD EMERGENCY LIGHT AT ROW 18 INOPERATIVE. CHARGED BATTERY POWER SUPPLY. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,969 hrs · 16,980 cycles

EMERGENCY LIGHT AT ROW 22 IS INOP. REMOVED AND REPLACED BULB.

Part: SKIN — DENTED (FRAMES 19-20) · airframe 27,565 hrs · 16,566 cycles

DENT WAS DISCOVERED BETWEEN FRAMES 19 - 20 AND STRINGERS 15 - 16L. MAINTENANCE REPAIRED DENT IAW SRM 53-21-01.

Part: SKIN — DENTED (FRAMES 20-21) · airframe 27,565 hrs · 16,566 cycles

DENT WAS DISCOVERED BETWEEN FUSELAGE FRAMES 20/21 AND STR 13/14L. SHOWS SIGNS OF OIL CANNING. MAINTENANCE REPAIRED DAMAGE IAW SRM 53-21-01.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,519 hrs · 15,792 cycles

DURING MAINTENANCE INSPECTION THE RT EMERGENCY EXIT WINDOW "EXIT MARKER" WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 5 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,519 hrs · 15,792 cycles

DURING MAINTENANCE INSPECTION, THE COCKPIT ENTRANCE EMERGENCY MARKER WOULD NOT ILLUMINATE. MAINTENANCE R & R THE AFFECTED EXIT IDENTIFIER, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,271 hrs · 15,609 cycles

DURING ROUTINE MAINTENANCE THE AFT CEILING EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: SHEAR TIE — CORRODED (FRAME 68) · corrosion level 2 · airframe 25,970 hrs · 15,397 cycles

DURING C-CHECK THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 16L-17L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-31-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 25,970 hrs · 15,397 cycles

DURING C-CHECK THE SHEAR TIE AT FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16L-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-31-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 25,970 hrs · 15,397 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: DRAG ANGLE — CRACKED (VERICAL STAB) · airframe 25,970 hrs · 15,397 cycles

DURING C-CHECK, THE LT DRAG ANGLE AT THE BASE OF THE VERTICAL STABILIZER WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE ANGLE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COUPLING — BLOWN (ZONE 100) · airframe 25,872 hrs · 15,325 cycles

ON SHORT FINAL THE F/A REPORTED AN ODOR AND A NOISE PRIOR TO THE ODOR. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE SECURED THE NR 1 DUCT TO ACFT LINE, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: A/C PACK — SMOKE (NR 1) · airframe 25,529 hrs · 15,059 cycles

THE CREW REPORTED THAT AFTER ICE TEST, AND ONCE PACKS WERE SELECTED ON THEY HAD NOTICEABLE SMOKE AND PARTICLES STATING TO FLOOD THE COCKPIT. BOTH PACK AND BLEED 1 WERE SHUTOFF TO CONTINUE THE FLIGHT. THE ACFT LANDED IN WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT AND PLACED PACK 1 ON MEL 21-51-00-3, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. R & R THE NR 1 ACM, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — WORN (LT RAM AIR) · airframe 25,296 hrs · 14,938 cycles

DURING CLIMB, FL220, REPORTED SMOKE IN THE COCKPIT AND SMELLING ELECTRICAL SMOKE, F/A CALLED REPORTING SMOKE IN THE CABIN, CREW WENT ON OXYGEN, RAN THE QRH, AND RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 1 ACM TO BE FROZEN AND DAMAGED. R & R THE NR 1 ACM, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. DISCREPANCY REPEATED. FOUND NR 1 RAM AIR VALVE ASSY WITH WORN BUSHING AND IT WAS REPLACED.

Part: ACM — SEIZED (LEFT) · airframe 25,229 hrs · 14,892 cycles

FLIGHT 6104 THE CREW REPORTED SMOKE IN THE CABIN AND FLIGHT DECK DURING CLIMBOUT IN ICING CONDITIONS. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND R & R THE NR 1 ACM, OPS CHECKS WERE PERFORMED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 18,348 hrs · 10,405 cycles

CREW REPORTED LAVATORY SMOKE MESSAGE ON EICAS TWICE DURING CRUISE, NO SMOKE NOTED. MX R & R THE SMOKE DETECTOR SENSOR WITH OPS CHECKED SUCCESSFUL AND PERFORMED ENGINE RUNS AT HIGH POWER WITH NO SMOKE NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — FAULTY (EXTERNAL) · airframe 17,070 hrs · 9,544 cycles

MX REPORTED THE SERVICE DOOR EMERGENCY LIGHT WAS INTERMITTENT. MX REPLACED THE EXTERNAL EMERGENCY LIGHT ASSY. OPS CHECKED GOOD.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 15,616 hrs · 8,507 cycles

IAH FLIGHT 3122, DURING CLIMB THE CREW REPORTED THAT THE MANUAL AND AUTO PRESSURIZATION WERE INOPERATIVE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE DIGITAL PRESSURIZATION CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 15,103 hrs · 8,234 cycles

IAH - FLIGHT 3131, THE CREW REPORTED A LAV SMOKE EICAS MESSAGE EN ROUTE FROM GDL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT OPERATIONALLY TESTED THE LAV SMOKE DETECTION SYSTEM ALL WITH NO DEFECTS/EVIDENCE OF SMOKE NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 14,906 hrs · 8,123 cycles

IAH - CREW REPORTED, RECEIVED ERRONIOUS LAV SMOKE MESSAGE. WENT AWAY AFTER A MINUTE. MAINTENANCE DETERMINED NR 2 ENGINE CREATED IRREGULARITY. REMOVED AND REPLACED NR 2 ENGINE IAW TASK CARD 6271001. AIRCRAFT RETURNED TO SERVICE.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 14,892 hrs · 8,115 cycles

DURING THE FLIGHT THE CREW REPORTED A FUEL SYSTEM CONFIGURATION DISAGREE MESSAGE ON THE EICAS DISPLAY. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE THE VENTRAL TANK TRANSFER SYSTEM WAS OPERATIONALLY CHECKED. ALL CHECKS WERE SUCCESSFUL AND THE DISCREPANCY WAS CLEARED.

Part: BATTERY — OVERTEMP (NR 1) · airframe 11,998 hrs · 6,379 cycles

IAH - FLIGHT 2809, THE CREW REPORTED A BATTERY ONE OVERTEMP DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE MAIN BATTERY NOTING THAT IT WAS COOL TO THE TOUCH, OPERATIONALLY TESTED WITHOUT DEFECT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 11,506 hrs · 6,107 cycles

ORD FLT 2983 THE CREW REPORTED AT FL360 COULD NOT MAINTAIN CABIN PRESSURE IN AUTO/MANUAL MODE UNTIL BELOW FL190. MAINTENANCE INSPECTED AND REPLACED THE PNEUMATIC OUTFLOW VALVE AND DIGITAL CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 10,619 hrs · 5,617 cycles

ATL - FLIGHT 2715, THE CREW REPORTED SMOKE IN THE COCKPIT DURING FLIGHT. THE AIRCRAFT DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FIM TASK 21-20-00, RAN UP ALL SYSTEMS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (NR 1 INLET) · airframe 9,825 hrs · 5,174 cycles

NR 1 ENG INLET HAS CORROSION INSIDE FASTENER HOLES. REAMED HOLES TO REMOVE CORROSION AND INSTALLED BUSHINGS IAW EC5420-01158B. AIRCRAFT STILL IN C-CHECK.

Part: STRIP — DAMAGED (CABIN) · airframe 8,879 hrs · 4,669 cycles

TYS - DURING A ROUTINE INSPECTION, MAINTENANCE FOUND THE EMERGENCY LIGHT STRIP AT THE GALLEY AREA DAMAGED. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP IAW EMB 145XR MM33-50-12, OPS CHECK GOOD.

Part: VALVE — LEAKING (FUEL TANK) · airframe 2,595 hrs · 1,384 cycles

CLE FLIGHT 2697, THE CREW REPORTED AFTER TAKEOFF THE TOWER REPORTED FUEL STREAMING FROM THE RIGHT WING TIP. A 400 LB FUEL IMBALANCE WITH RIGHT TANK FUEL QUANTITY DECREASING RAPIDLY. THE AIRCRAFT RETURNED AND LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT WING FUEL VENT VALVE. OPERATIONAL CHECKS WERE GOOD.