N24128

Part: LAMP — BURNED OUT (ZONE 200) · airframe 49,841 hrs · 32,998 cycles

MCD EXTERNAL EMERG LIGHT INOP. REMOVED AND REINSTALLED MCD EMERG LIGHT. OPS CHECK SAT.

Part: SWITCH — MISSING (ZONE 800) · airframe 49,237 hrs · 32,398 cycles

DOOR OPEN INDICATION WHEN MAIN DOOR CLOSED. PRESSURIZED AIRCRAFT. NO DEFECTS NOTED. FOUND FWD LOWER MCD MICROSWITCH TO BE MISSING ITS ARM AND NOT ACTIVATING. REMOVED AND REPLACED FWD LOWER MCD MICROSWITCH ARM AND ADJUSTED MICROSWITCH. OPS CHECK SAT.

Part: DOOR — UNSECURE (ZONE 800) · airframe 49,228 hrs · 32,389 cycles

MAIN CABIN DOOR SHOWING CLOSED BUT NOT FULLY SEALED. CYCLED MCD, FOUND SEAL NOT SEATED CORRECTLY. CLOSED DOOR SECURELY. NO FURTHER DEFECTS NOTED.

Part: FITTING — LOOSE (RT AILERON) · airframe 49,186 hrs · 32,349 cycles

AT RH AILERON, MANY LOOSE RIVETS AT DAMPER FITTING. BUSHINGS REPAIR ON RH AILERON LOWER SKIN, AT DAMPER FITTING.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 49,186 hrs · 32,349 cycles

AT CARGO ENTRY FR66 T FLOOR SUPPORT AND LOWER BRACKET FOUND CRACKED. FR66 T FLOOR SUPPORT REPLACED AND LOWER BRACKET REPLACED WITH MADE REPAIR PART, LOCALLY FABRICATED.

Part: SHEAR TIE — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,186 hrs · 32,349 cycles

LH SHEAR CLIP AT CARGO ENTRY FR 65 FOUND CORRODED. SHEAR CLIP SPLICE REPAIR ON LH REAR FUSE I FRAME 65, BTW STR 15L-16L CARRIED OUT

Part: SHEAR TIE — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,186 hrs · 32,349 cycles

LH SHEAR CLIP AT CARGO ENTRY FR 68 FOUND CORRODED. SHEAR CLIP SPLICED ON LH REAR FUSE I FRAME 68, BTW STR 15L-16L CARRIED OUT.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,186 hrs · 32,349 cycles

CF4, FRAME 59 FOUND CORRODED BTW STR 21L-20R. REPAIR ANGLE ON CENTER FUSE IV FRAME 59 BTW STR 21L-21R CARRIED OUT.

Part: SKIN — CRACKED (ZONE 800) · airframe 49,186 hrs · 32,349 cycles

CARGO DOOR, SKIN AROUND HANDLE CRACKED. REPAIR DOUBLER ON CARGO DOOR EXTERNAL SKIN, AROUND HANDLE HOUSING CUTOUT

Part: FRAME — CHAFED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

CHAFING ON RH CF2 FR34 BTW STR 9R-10R AND ON RH CF3 FR37 BTW STR 7R-8R. ANGLE REPAIR ON RH CENTER FUSE III FRAME 37, BTW STR 7R-8R CARRIED OUT AND FABRICATION OF L SHAPED SPLICE WITH AN ALTERNATE MATERIAL

Part: FRAME — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

FRAME 59 CRACKED BTW STR 15L-16L. EXTENDED SPLICE REPAIR ON LH CENTER FUSE IV FRAME 59, BTW STR 14L-16L CARRIED OUT.

Part: SKIN — DENTED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

CF3 LH UPPER SKIN DENT FOUND ON FR 39, BTW STR 3L-4L. REPAIR DOUBLER ON LH CENTER FUSE III SKIN AT FR39 BTW STR 3L-4L CARRIED OUT.

Part: FRAME — CRACKED (ZONE 100) · airframe 49,186 hrs · 32,349 cycles

FR 66 CRACKED AT LEVEL OF STR 18L. SPLICE REPAIR ON LH REAR FUSE I FRAME 66, BTW STR 18L-19L CARRIED OUT. SPLICE AND NEW FRAME SECTION FABRICATED WITH AN ALTERNATE MATERIAL

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,186 hrs · 32,349 cycles

CF3 ON CENTER OMEGA BEAM LOWER FLANGE BTW FR 46-52 FOUND CORRODED. REPAIR DOUBLER ON CF III ENTER OMEGA BEAM ON LH HORIZONTAL FLANGE BTW FR 51-52 CARRIED OUT

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

TAIL COMPARTMENT AT FR80 BTW STR 5R-7R SHEAR CLIP CRACKED. TAIL COMPARTMENT AT FR80 BTW STR 5R-7R SHEAR CLIP REPLACED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

TAIL COMPARTMENT FR80 BTW STR 4R-5R SHEAR CLIP CRACKED. TAIL COMPARTMENT FR80 BTW STR 4R-5R SHEAR CLIP REMOVED AND REPLACED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

TAIL COMPARTMENT FR80 BTW STR 5L-7L SHEAR CLIP CRACKED. TAIL COMPARTMENT FR80 BTW STR 5L-7L SHEAR CLIP REMOVED AND REPLACED

Part: SKIN — DENTED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

DENT FOUND ON EXT SKIN BTW FR 53-54 STR 4-5 LH. REPAIR DOUBLER ON LH CENTER FUSE IV SKIN, AT FR 54 AND BTW STR 4L-5L CARRIED OUT.

Part: SKIN — DENTED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

DENT FOUND ON EXTERNAL SKIN BTW FR 21-22 AND STR 11L-12L. REPAIR DOUBLER ON LH CENTER FUSE I SKIN, BTW FR 21-22 AND BTW STR 11L-12L CARRIED OUT

Part: SKIN — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

RF2, RH EXTERNAL SKIN, CRACK SUSPECTED BTW FR 77-78 AND BTW STR 5R-8R. REPAIR DOUBLER ON RH REAR FUSE II SKIN, AT FR78 BTW STR 5R-7R CARRIED OUT.

Part: RIB — CRACKED (ZONE 300) · airframe 49,186 hrs · 32,349 cycles

RUDDER II, FWD ON FRONT SPAR, UPPER RIB CRACKED AT UPPER MID HINGE FITTING. RUDDER II, FWD OF FRONT SPAR UPPER MID HINGE FITTING UPPER RIB REPLACED.

Part: SKIN — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

RF2, LH EXTERNAL SKIN, SEVERAL CRACKS SUSPECTED AT FR 77, 78, 79, 80 AND BTW STR 3L-7L. 2 REPAIR DOUBLER ON LH REAR FUSE II SKIN. DOUBLER #1 IS LOCATED AT FR77 BTW STR 3L-5L. DOUBLER #2 IS LOCATED AT FR 78 BTW STR 5L-7L

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

SHEAR CLIP FOUND CRACKED AT FR68 BTW STR 6R-10R. AT FR67 TO 68 STR 7 RH QTY 4 GROUND CABLES DISCONNECTED FOR ACCESS. RH SIDE CARGO INTERNAL AND LATERAL BLEED AIR T-DUCT AT FR68-69 6R-9R REMOVED FOR METAL ACCESS. SHEAR CLIP AT FR68 BTW STR 6R-10R REPLACED. RH SIDE CARGO INTERNAL AND LATERAL BLEED AIR T-DUCT AT FR68-69 6R-9R REINSTALLED. ELECTRONICAL BONDING TEST OF 4 GROUND STUD TESTED SERVICEABLE

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

LH OMEGA BEAM FOUND CRACKED AT FR21 AND 22. REPAIR DOUBLER ON LH CENTER FUSE I OMEGA BEAM, ON INBD VERTICAL FLANGE AT FR 21 AND 22 CUT OUT

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,186 hrs · 32,349 cycles

LH OMEGA BEAM FOUND CRACKED AT FR 24, 25, 27, 28 AND CORRODED BTW FR 24-28. LH OMEGA BEAM BTW FR 24-29 REMOVED. CORROSION OUT OF LIMITS.LH OMEGA BEAM BTW FR 24-29 REMOVED AND REPLACED.

Part: SKIN — DENTED (ZONE 100) · airframe 49,186 hrs · 32,349 cycles

FF2 LH LOWER SKIN DENT FOUND UPPER EXTERNAL POWER RECEPTACLE. ON FF2 LH LOWER SKIN UNDER EXTERNAL RECEPTACLE PAIN STRIPPED. FF2 LH LOWER SKIN UNDER EXTERNAL POWER RECEPTACLE REPAIRED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

LH OMEGA BEAM #3 FOUND CRACKED AT FR 29, 30, 31, 33, AND 35. ON CETNER FUSE II LH OMEGA BEAM, CRACKED CONFIRMED BY NDT ON INBD VERTICAL FLANGE AT FR29, 30, 31, AND 33. NO CRACK AT FR35. CRACKS ON LH OMEGA BEAM FR 30, 31, 33 CUT OUT DONE. LH OMEGA AT FR 30, 31, AND 33 REPAIRED

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

CENTER OMEGA BEAM FOUND CRACKED AT FR31. ON CENTER FUSE II CENTER OMEGA BEAM, CRACK CONFIRMED BY NDT ON LH VERTICAL FLANGE AT FR31. ON CENTER OMEGA BEAM FR31, CUTOUT AND LAYOUT PERFORMED. ON CENTER OMEGA BEAM FR31 REPAIRED.

Part: STRUCTURE — MECHANIC ERROR (ZONE 800) · airframe 49,186 hrs · 32,349 cycles

AT CARGO DOOR LOWER EDGE, DAMAGE FOUND WHILE REMOVING SEAL. AT CARGO DOOR LOWER EDGE REMOVED FOR INVESTIGATION. CARGO DOOR LOWER, EDGE INVESTED AND FOUND DAMAGE, CRACKED CARGO DOOR LOWER EDGE REPLACED.

Part: ANGLE — CRACKED (RT WNG-BDY) · airframe 49,186 hrs · 32,349 cycles

CF3 RH TOP WING TO BODY FAIRING ANGLE FOUND CRACKED AT FR47. AT CF3 RH TOP WING TO BODY FAIRING AT FR47, ANGLE REPLACED.

Part: SUPPORT — CRACKED (LT FAIRING) · airframe 49,186 hrs · 32,349 cycles

LH WING TO BODY FAIRING, UPPER STRIP SUPPORT CRACKED BTW FRAME 48-49. LH WING TO BODY FAIRING UPPER STRIP SUPPORT BTW FR 48-49 CUT OUT AND REPAIR PARTS FABRICATED AND INSTALLED.

Part: SUPPORT BRACKET — CRACKED (ZONE 400) · airframe 49,186 hrs · 32,349 cycles

LH PYLON, PRECOOLER AFT SUPPORT BRACKET FOUND CRACKED. LH PYLON, PRECOOLER AFT SUPPORT BRACKET REPLACED WITH NEW PART.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 49,186 hrs · 32,349 cycles

SHEAR CLIP FOUND CRACKED AT FR 72 BTW STR 17L-18L. AT FR72 BTW STR 17L-18L, SHEAR CLIP REPLACED

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 49,186 hrs · 32,349 cycles

SHEAR CLIP FOUND CRACKED AT FR73 BTW STR 16L-17L. AT FR73 BTW STR 16L-17L SHEAR CLIP REPLACED

Part: SUPPORT BRACKET — CRACKED (ZONE 400) · airframe 49,186 hrs · 32,349 cycles

RH PYLON, PRECOOLER FWD SUPPORT BRACKET FOUND CRACKED. RH PYLON PRECOOLER FWD SUPPORT BRACKET REPLACED.

Part: ANGLE — CRACKED (ZONE 500) · airframe 49,186 hrs · 32,349 cycles

CF3 ON WING STUB SPAR 2 LH AFT ANGLE FOUND CRACKED BTW FR 46-47. CF3 ON WING STUB SPAR 2 LH AFT ANGLE BTW FR 46-47 REMOVED AND REPLACED

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

2 FLOOR SUPPORT ANGLE FOUND CRACKED ON LH OMEGA BEAM INBD SIDE BTW FR 19-20. FLOOR SUPPORT ANGLES ON LH OMEGA BEAM INBD SIDE BTW FR 19-20 REMOVED AND INSTALLED

Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,186 hrs · 32,349 cycles

SERVICE DOOR CUTOUT LOWER BEAM FOUND CORRODED. ON SERVICE DOOR CUTOUT LOWER BEAM BLENDED AND AREA FOUND OUT OF LIMITS. SERVICE DOOR CUTOUT, LOWER BEAM REMOVED FOR REPLACEMENT. NEW SERVICE DOOR CUTOUT LOWER BEAM REINSTALLED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

SHEAR CLIP FOUND CRACKED AT FR68 BTW STR 6L-9L. SHEAR CLIP AT FR68 BTW STR 6L-9L REMOVED AND INSTALLED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

SHEAR CLIP FOUND CRACKED AT FR 65 BTW STR 7L-9L. SHEAR CLIP AT FR65 BTW STR 7L-9L REMOVED AND INSTALLED

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,186 hrs · 32,349 cycles

RH GUSSET FOUND CORRODED BTW FR 59-61. RH GUSSET BTW FR 59-61 REPLACED

Part: BRACKET — CRACKED (ZONE 800) · airframe 49,186 hrs · 32,349 cycles

AFT CARGO DOOR MECH BRACKET UPPER AND MIDDLE FOUND CRACKED AT FR 67-68 AND STR 4R-5R. CRACKED AFT CARGO DOOR MECH BRACKETS (UPPER AND MID) AT FR 67-68 BTW STR 4-5R. REPLACED AND INSTALLED WITH NEW PARTS AND SOLID RIVETS

Part: SUPPORT — CRACKED (ZONE 100) · airframe 49,186 hrs · 32,349 cycles

FWD CARGO DOOR MECH SUPPORT FOUND CRACKED BTW FR 61-62 AND STR 4R-5R. BAGGAGE DOOR LIFTING AND LOWERING MECHANISM REMOVED FOR ACCESS. PART REMOVED FOR REPLACEMENT. CRACKED FWD CARGO DOOR MECH SUPPORT BTW FR 61-62 AND STR 4-5R REPLACED AND INSTALLED WITH NEW PART AND SOLID RIVETS. BAGGAGE DOOR LIFTING AND LOWERING MECHANISM IS REINSTALLED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

SHEAR CLIP FOUND CRACKED AT FR58 BTW STR 15L-16L. AT FR58 BTW STR 15L-16L SHEAR CLIP REMOVED. AT FR58 BTW STR 15-16L, NEW SHEAR CLIP PARTIALLY INSTALLED. AT FR58, BTW STR 15L-16L SHEAR CLIP REPLACED.

Part: CUP — CORRODED (ZONE 900) · corrosion level 2 · airframe 49,186 hrs · 32,349 cycles

TOILET WASTE CUP CORRODED ON THE EXTERNAL SIDE. TOILET WASTE CUP ON EXT SIDE AREA BLENDED AND FOUND OUT OF LIMITS. ON TOILET WASTE CUP REPLACED WITH NEW PART. ON TOILET WASTE EXTERNAL RE-PROTECTION HEAD FASTENER COVER.

Part: RIB — CRACKED (ZONE 600) · airframe 49,186 hrs · 32,349 cycles

RH AFT WW RIB FOUND CRACKED. CRACKED SECTION OF RH AFT WW RIB REMOVED. CRACKED RH AFT WW RIB REPAIRED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

SHEAR CLIP FOUND CRACKED AT FR26 BTW STR 15R-16R. REMOVED CRACKED SHEAR CLIP AT FR26 BTW STR 15R-16R ON NEW SHEAR CLIP AT FR26 BTW STR 15R-16R DRILLED. NEW SHEAR CLIP AT FR26 BTW STR 15R-16R INSTALLED

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

CF3 ON RH INBOARD OMEGA ANGLE BTW FR 47-50 FOUND CRACKED. RH INBOARD OMEGA BEAM ANGLE BTW FR 47-50 REMOVED AND INSTALLED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

SHEAR CLIP FOUND CRACKED AT FR 71 BTW STR 7R-10R. SHEAR CLIP CRACKED AT FR71 BTW STR 7R-10R REMOVED AND REPLACED

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,186 hrs · 32,349 cycles

RH OMEGA BEAM AT FR20, HEXAGON TOP DOUBLER FOUND CORRODED. AT RH OMEGA BEAM AT FR20, HEXAGON TOP DOUBLER BLENDED OUT OF LIMIT. RH OMEGA BEAM AT FR20, HEXAGON TOP DOUBLER REMOVED AND REPLACED WITH NEW PARTS

Part: FLOORBEAM — DAMAGED (ZONE 100) · airframe 49,186 hrs · 32,349 cycles

LAT CARGO ENTRY FR67 T FLOOR FOUND DAMAGED. LAT CARGO ENTRY FR67 FLOOR REMOVED AND REPAIRED.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 49,186 hrs · 32,349 cycles

SHEAR CLIP FOUND CRACKED AT FR24 BTW STR 16L-17L. REMOVED CRACKED SHEAR CLIP AT FR24 BTW STR 16L-17L. ON NEW SHEAR CLIP AT FR24 BTW STR 16L-17L DRILLED. NEW SHEAR CLIP AT FR 24 BTW STR 16L-17L INSTALLED.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 49,186 hrs · 32,349 cycles

SHEAR CLIP FOUND CRACKED AT FR24 BTW STR 16R-17R. REMOVED CRACKED SHEAR CLIP AT FR24 BTW STR 16R-17R ON NEW SHEAR CLIP AT FR24 BTW STR 16R-17R DRILLED. NEW SHEAR CLIP AT FR24 BTW STR 16R-17R INSTALLED

Part: ANGLE — CRACKED (ZONE 100) · airframe 49,186 hrs · 32,349 cycles

CF3 RH TOP WING TO BODY FAIRING ANGLE FOUND CRACKED AT FR51. AT CF3 RH TOP WING TO BODY FAIRING ANGLE AT FRAME 51 CRACKED PART PLUS REPAIR PARTS FABRICATED. ALL REPAIR PARTS INSTALLED.

Part: TEE ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,186 hrs · 32,349 cycles

LOWER BEAM AT CARGO ENTRY FOUND CORRODED. LOWER BEAM AT CARGO BLENDED OUT OF LIMIT. LOWER BEAM AT CARGO ENTRY REMOVED FOR REPLACEMENT. ON LOWER BEAM AT CARGO ENTRY FR66 AND 67 T ANGLES REMOVED FOR ACCESS. LOWER BEAM REPLACED. FR66 AND FR67 T ANGLES REINSTALLED

Part: SUPPORT — CRACKED (ZONE 100) · airframe 49,186 hrs · 32,349 cycles

RH LOWER WING TO FUSE LATERAL FAIRING SUPPORT FOUND CRACKED AFT ON WW. RH LOWER WING TO FUSE LATERAL FAIRING SUPPORT AFT ON WW REMOVED AND INSTALLED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

SHEAR CLIP FOUND CRACKED AT FR73 BTW STR 8L-9L. SHEAR CLIP AT FR 73 BTW STR 8-9L REMOVED AND INSTALLED

Part: SUPPORT — CRACKED (RT FAIRING) · airframe 49,186 hrs · 32,349 cycles

LH LOWER WING TO FUSE LATERAL FAIRING SUPPORT FOUND CRACKED AFT ON WW. LH LOWER WING TO FUSE LATERAL FAIRING SUPPORT AFT ON WW REMOVED AND REPLACED.

Part: ACTUATOR — INOPERATIVE (ZONE 700) · airframe 49,015 hrs · 32,185 cycles

LANDING GEAR / LEVER DISAGREE EICAS WARNING ON GEAR RETRACTION. RIGHT MAIN GEAR DID NOT RETRACT. REMOVED AND REPLACED RH MANEUVERING ACTUATOR. OPS CHECK SAT. GEAR SWING SAT. LEAK CHECK SAT. ORIGINAL SUBMISSION DATE: 12/6/2024

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 47,909 hrs · 31,148 cycles

EMERGENCY LIGHT BATTERY #4 REQUIRES REPLACEMENT DUE TO MULTIPLE EMERGENCY LIGHTS INOP /R EMERGENCY LIGHT BATTERY #4, OPS CHECK SAT

Part: SKIN — DENTED (ZONE 200) · airframe 49,186 hrs · 32,349 cycles

DENT FOUND ON EXTERNAL SKIN BTW FR 19-20 AND BETWEEN STR 11L-12L. PAINT STRIPPED ON EXTERNAL SKIN BTW FR 19-20 BTW STR 11L-12L FOR INVESTIGATION. ON LH CENTER FUSE I SKIN, BTW FR19-20 AND BTW STR 11L-12L SKIN OUT TO REMOVE THE DAMAGE. SKIN REPAIRED BTW FR19-20 AND BTW STR 11L-12L

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 47,515 hrs · 30,777 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 46,814 hrs · 30,118 cycles

FOUND EMERGENCY LIGHTS FOR BATTERY PACK 4 TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY 4. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 46,814 hrs · 30,118 cycles

EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY #3. OPS CHECK SAT. NO FURTHER DEFECTS NOTED.

Part: PANEL — CRACKED · airframe 45,994 hrs · 29,376 cycles

CAPT OVERHEAD PANEL IS CRACKED AND HAS HDW ATTACH HOLES DAMAGED. REMOVED AND INSTALLED CAPT OVERHEAD PANEL

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 45,994 hrs · 29,376 cycles

CORROSION AT FS60, ON FLOOR STRUCTURE CENTER FLOORBEAM SCREW HOLE. COMPLETED GUSSET INSTALL BY INSTALLING PROTECTIVE TAPE AS REQUIRED

Part: STRINGER CLIP — CRACKED · airframe 45,994 hrs · 29,376 cycles

STRINGER CLIP, JUST AFT OF COCKPIT BULKHEAD ON RH SIDE AT FLOOR LINE HAS A CRACK COMING OUT OF RIVET. REMOVED STRINGER CLIP. STRINGER CLIP WAS REPLACED

Part: ANGLE — CRACKED · airframe 45,994 hrs · 29,376 cycles

LH WING ROOT SKIN ANGLE FOR LATERAL FAIRING IS CRACKED IN ONE LOCATION BETWEEN SPAR 1 AND SPAR 2. REMOVED AND REPLACE ANGLE FOR LATERAL FAIRING

Part: GUSSET — CORRODED · corrosion level 2 · airframe 45,994 hrs · 29,376 cycles

MINOR POWDERING CORROSION, AT FS60, ON FLOOR STRUCTURE CENTER FLOOR BEAM SCREW HOLE. UPON INSPECTION OF CORROSION AT FS60, CORROSION FOUND TO BE LEVEL 2. REMOVED AND REPLACED GUSSET

Part: BRACKET — CRACKED · airframe 45,994 hrs · 29,376 cycles

RH WING ROOT SKIN ANGLE FOR LATERAL FAIRING IS CRACKED IN TWO LOCTIONS BETWEEN SPAR 1 AND SPAR 2. ANGLE BRACKET OF RH WING LATERAL FAIRING BETWEEN SPAR 1 AND SPAR 2 WAS REMOVED AND REPLACED

Part: NONE — OVERHEATED · airframe 45,811 hrs · 29,194 cycles

PACK 1 BURN SMELL IN FLIGHT WITH STRANGE NOISE. PACK 1 OVERHEAT ON GROUND AND NO LONGER COOLS COCKPIT. REMOVED AND REPLACED #1 ACM. OPS CHECK GOOD

Part: NONE — INOPERATIVE · airframe 45,706 hrs · 29,097 cycles

LG/LEVER DISAGREE MSG AFTER T/O LEFT GEAR DID NOT SHOW UP/LOCK. FOLLOWED FIM. COULD NOT DUPLICATE FAULT. FOUND CANNON PLUG ON LH DOWNLOCK PROX SWITCH TO BE LOOSE, RESECURED CANNON PLUG. PERFORMED GEAR SWING. OPS CHECK SAT. REMOVED AND REPLACED LH MLG ACTUATOR. OPS AND LEAK CHECK SAT.

Part: NOT REPORTED — NOT REPORTED · airframe 44,952 hrs · 28,438 cycles

ALL FOUR FLOOR PROXIMITY LIGHT STRIPS AT THE EXIT ROWS ARE INSTALLED 6" TOO FAR AFT - REAR STRIPS ARE BENEATH SEATS AND NOT VISIBLE. EXIT PLACARDS ARE ORIENTED INCORRECTLY. REORIENTED EXIT ROW FLOOR PROXIMITY LIGHT STRIPS 6" FWD AND RE-POSITIONED EXIT PLACARDS TO PROPER ORIENTATION.

Part: LAMP — INOPERATIVE · airframe 44,952 hrs · 28,438 cycles

FOUND COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT. OPS CHECK SAT.

Part: NOT REPORTED — NOT REPORTED · airframe 44,867 hrs · 28,363 cycles

EMERGENCY EXIT SIGN OVER WING 18A INDICATES WRONG DIRECTION. REMOVED AND REPLACED EXIT MARKING SIGN ASSEMBLY. OPS CHECK SAT.

Part: FLOOR SUPPORT — CORRODED (FRMS 57-58) · airframe 44,184 hrs · 27,749 cycles

CROSS FLOOR U-CHANNEL BETWEEN FRAMES 57 AND 58 AND CENTER FLOOR BEAM AND FLOOR BEAM 18 RIGHT HAS CORROSION IN SEVERAL AREAS. BLENDED AREAS ON CROSS FLOOR U-CHANNEL BETWEEN FR 57-58 ND CENTER FLOOR BEAM AND FLOOR BEAM 18" RIGHT.

Part: SEAT TRACK — CORRODED (FRMS 29-35) · airframe 44,184 hrs · 27,749 cycles

LH OUTBOARD SEAT TRACK SUPPORT AT FR29-35 HAS CORROSION AT 16EA AREAS. REMOVED AND REPLACED LH OUTBOARD SEAT TRACK SUPPORT AT FR 29-35

Part: FLOOR SUPPORT — CORRODED (FRMS 48-52) · airframe 44,184 hrs · 27,749 cycles

CORROSION ON CENTER AISLE LH OMEGA BEAM AT FLOOR BOARD MOUNTING SURFACE. REMOVED AND REPLACED CENTER AISLE LH OMEGA BEAM BETWEEN FR 48 AND FR52

Part: DOUBLER — NOT REPORTED (LT WING) · airframe 44,184 hrs · 27,749 cycles

EXTERNAL SKIN EXISTING DOUBLER REPAIR LEFT WING LEADING EDGE BETWEEN RIB 14 AND RIB 15. REPAIRED LEFT WING LEADING EDGE BETWEEN RIB 14 AND RIB 15

Part: WINDOW POST — CRACKED (COCKPIT RIGHT) · airframe 44,184 hrs · 27,749 cycles

CO-PILOTS WINDSHIELD LATERAL POST FRAME HAS CRACK AT UPPER SECTION 4.5 INCHES FROM HORIZONTAL CORNER. REMOVED AND REPLACED CO-PILOTS WINDSHIELD LATERAL POST FRAME

Part: FRAME — DAMAGED (FRM 22 S15L) · airframe 44,184 hrs · 27,749 cycles

FR22 INNER FLANGE HAS DAMAGE AT S15L. REPAIRED FRAME 22 INNER FLANGE AT S15L.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 44,184 hrs · 27,749 cycles

RIGHT WING FUEL TANK ACCESS OPENING FOR 631 BB HAS CORROSION IN SEVERAL AREAS AROUND RIM. REPAIRED RIGHT WING FUEL TANK ACCESS OPENING.

Part: SUPPORT BEAM — CRACKED (PAX DOOR AREA) · airframe 44,184 hrs · 27,749 cycles

PAX DOOR UPPER AFT SUPPORT BEAM CRACKED ON AFT EDGE AS MARKED. REMOVED AND REPLACED PAX DOOR UPPER AFT SUPPORT BEAM.

Part: DOUBLER — NOT REPORTED (FRMS 19-20 S6-8L) · airframe 44,184 hrs · 27,749 cycles

EXTERNAL SKIN EXISTING DOUBLER REPAIR BETWEEN FR19 AND FR20 BETWEEN STR 6L AND STR 8L. REPAIRED EXTERNAL SKIN BETWEEN FR19 AND FR20 BETWEEN STR 6L AND STR 8L.

Part: SHEAR TIE — CRACKED (FRM 66 S6-7L) · airframe 44,184 hrs · 27,749 cycles

SHEAR CLIP CRACKED IN CARGO BAY ON FR66 BETWEEN STGR 6-7L. REMOVED AND REPLACED SHEAR CLIP IN CARGO BAY FR66 BETWEEN STGR 6-7L.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 44,184 hrs · 27,749 cycles

CORROSION ON CARGO DOOR AFT FRAME, AFT FACE, AROUND NUT PLATES HOLE. INSTALLED NEW AFT CARGO DOOR FRAME WEB.

Part: SEAL — TORN (WINDSHIELD) · airframe 43,183 hrs · 26,903 cycles

LOUD BANGING NOISE ON F/O WINDSHIELD. F/O'S HUMP SEAL TORN. REPAIRED THE F/O'S WINDSHIELD HUMP SEAL.

Part: COFFEEMAKER — ARCED (GALLEY) · airframe 42,783 hrs · 26,621 cycles

F/A SMELLS BURNING PLASTIC. NO SMOKE, NO FIRE, PAX REPORTED BURING WIRING SMELL. NO ODOR DETECTED ON ARRIVAL. INSPECTED GALLEY. FOUND NO BURNT OR DAMAGED COMPONENTS. #1 COFFEE BREWER WAS FOUND UNLATCHED AND UNSEATED. THE CONTACTS SMELLED OF ELECTRICAL ARCING. FOUND THAT BREWER #1 COULD NOT LATCH. CLEARED DEBRIS FROM THE DETENT HOLE IN THE BREWER TRACK. LATCHED AND SECURED. OPS CHECK GOOD.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 42,135 hrs · 26,125 cycles

HYD SYS 1 FAIL IN FLT. INDICATION NO FLUID IN SYS #1. FOUND E1 HYD PUMP LEAKING, R&R PUMP LEAK CHECK GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,962 hrs · 25,984 cycles

LT FLOOR SIDEWALL SILL FROM FRAMES 29-35 HAS SIGNS OF CORROSION. REMOVED AND REPLACED LT FLOOR SILL FROM FRAMES 29-35.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,962 hrs · 25,984 cycles

RT FLOOR SILL FROM FRAMES 29-35 HAS SIGNS OF CORROSION. REMOVED AND REPLAXCED RT FLOOR SILL FROM FRAMES 29-35.

Part: FLOOR SUPPORT — ERODED (FRAMES 24-29) · airframe 41,962 hrs · 25,984 cycles

R/H FLOOR SILL IS ERODED BETWEEN FRAMES 24-29. REMOVED AND REPLACED R/H FLOOR SILL BETWEEN FRAMES 24-29

Part: GUSSET — CORRODED (FUSELAGE) · airframe 41,962 hrs · 25,984 cycles

LAV RT GUSSET AT FRAMES 58-60 HAS CORROSION. REMOVED AND REPLACED LAV RT GUSSET AT FRAMES 58-60.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 41,962 hrs · 25,984 cycles

RT STOP SIGN HAS CORROSION AT FRAME 19. REMOVED AND REPLACED RT STOP SIGN AT FRAME 19.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 41,962 hrs · 25,984 cycles

LAV LT GUSSET AT FRAMES 58-60 HAS CORROSION. REMOVED AND REPLACED LAV LT GUSSET AT FRAMES 58-60.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,962 hrs · 25,984 cycles

SERVICE DOOR ENTRANCE SILL HAS CORROSION. REMOVED AND REPLACED SERVICE DOOR ENTRANCE SILL.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,962 hrs · 25,984 cycles

RT SILL AFT OF SERVICE DOOR HAS CORROSION. REMOVED AND REPLACED RT SILL AFT OF SERVICE DOOR.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 41,962 hrs · 25,984 cycles

CARGO BAY DOOR ROD HOLDER BRACKET CRACKED. REMOVED AND REPLACED CARGO BAY DOOR ROD HOLDER BRACKET.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 41,962 hrs · 25,984 cycles

R/H SHEAR CLIP CRACKED AT FRAME 24 BETWEEN STRINGERS 15-16. REMOVED AND REPLACED R/H SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 15-16

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,962 hrs · 25,984 cycles

LT SILL HAS CORROSION BETWEEN FRAMES 18-23. REMOVED AND REPLACED LT SILL BETWEEN FRAMES 18-23.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,962 hrs · 25,984 cycles

RT SILL FROM FRAMES 41-48 HAS SIGNS OF CORROSION. REMOVED AND REPLACED RT SILL FROM FRAMES 41-48.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,077 hrs · 25,259 cycles

INOP EMERGENCY UPPER INNER LIGHT NEAR RH EMERGENCY EXIT. R&R EMER LIGHT ASSEMBLY OPS CHECK GOOD.

Part: O-RING — DAMAGED (RT WING) · airframe 41,077 hrs · 25,259 cycles

POSSIBLE FUEL LEAK COMING FROM RT WING. INSPECTED AND FOUND RT WING FUEL TANK ACCESS PANEL 631CB LEAKING. R&R O'RING ON RT WING FUEL TANK ACCESS PANEL 631CB. LEAK CHECK GOOD.

Part: INSULATION — UNSECURE (E&E BAY) · airframe 41,014 hrs · 25,203 cycles

STRONG CRACKLING NOISE COMING FROMM FWD OF INSTRUMENT PANEL AREA. FOUND INSULATION RUBBING ON FORWARD AVIONICS BAY FANS. RESECURED INSULATION. OTHER MAINTENANCE PERFORMED REFERANCE PAGE 340680 AND 340681 DISC 3 AND 1.

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR)

LANDING GEAR WON`T RETRACT AFTER TAKEOFF. R & R THE LGEU PERFORMED SEVERAL SWINGS, 10 TIMES WITH NO FAULTS NOTED AT THIS TIME.

Part: FIRE DETECTOR — FALSE ACTIVATION (APU BAY) · airframe 39,641 hrs · 24,013 cycles

APU FIRE EICAS MESSAGE. INSPECTED APU, NO INDICTION OF FIRE. INSPECTED APU FIRE LOOP, NO DEFECT NOTED. PERFORMED FIRE SYSTEM TEST. OPS CHECK GOOD, TEST PASSED. RAN APU FOR 1 HOUR CONTNUOUSLY WITH BOTH PACKS ON. NO DEFECT NOTED.

Part: APU — CONTAMINATED · airframe 39,617 hrs · 23,991 cycles

BURNING ODOR & HAZE IN COCKPIT AFTER TAKE OFF. INSPECTION FOUND APU AND COMPARTMENT SOAKED WITH GLYCOL. RAN APU, E1 AND E2 TO 80% N1 WITH PACKS 1 & 2 OPERATING. APU AND ENGINE OIL LOOKS NORMAL. NO DEFECTS NOTED.

Part: LIGHT — WORN (CABIN) · airframe 37,394 hrs · 22,125 cycles

FORWARD AISLE EMERGENCY LIGHT STRIP ACROSS FROM 2A IS WORN. R & R WORN FORWARD AISLE EMERGENCY LIGHT STRIP ACROSS FROM 2A. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,659 hrs · 20,707 cycles

AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY POWER SUPPLY. OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 35,350 hrs · 20,450 cycles

EMERGENCY LIGHT NR 21 WILL NOT ILLUMINATE. REMOVED UPPER PANEL, CONNECTED ELECTRICAL PLUG TO EMERGENCY LIGHT ON SERVICE DOOR CEILING PANEL OPERATIONAL. CHECK GOOD. REINSTALLED SERVICE DOOR CEILING PANEL.

Part: SEAL — LEAKING (RT WING) · airframe 34,078 hrs · 19,602 cycles

THE CREW REPORTED FUEL LEAK FROM THE RT WING, FUEL WAS NOTICED ON TOP OF THE WING BETWEEN THE FLAPS JUST OTBD OF THE OTBD SPOILER. THE ACFT LANDED AT MCI WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT AND R & R THE SEAL AT FUEL PANEL 641AB, LEAK CHECKED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,578 hrs · 19,261 cycles

DURING MAINTENANCE INSPECTION THE AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,488 hrs · 19,214 cycles

DURING AN A-CHECK INSPECTION, THE AFT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT POWER SUPPLY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,002 hrs · 18,902 cycles

DURING MX INSPECTION, THE CEILING EMERGENCY EXIT LIGHT AT THE EXIT ROW WAS DISCOVERED INOPERATIVE. MAINTENANCE R & R THE EMERGENCY LIGHT SYSTEM BATTERY CHARGER ASSY WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 32,140 hrs · 18,361 cycles

DURING PREFLIGHT, THE CREW REPORTED A CEILING EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LGIHTS) · airframe 32,078 hrs · 18,324 cycles

DURING PREFLIGHT INSPECTION THE EMERGENCY EXIT SIGN AT EMERGENCY EXIT ROW IN CABIN ROW 18 WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR F4 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 31,719 hrs · 18,101 cycles

DURING PREFLIGHT INSPECTION, CREW REPORTED AN EMERGENCY LIGHT BURNED OUT. MAINTENANCE INSPECTED AND R & R NR 4 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO DEFECTS NOTED, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 31,613 hrs · 18,033 cycles

DURING MAINTENANCE INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT SYS BATTERY PACK AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,313 hrs · 17,845 cycles

DURING MAINTENANCE INSPECTION BOTH EXTERIOR OVERWING EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,872 hrs · 17,575 cycles

DURING 5A INSPECTION, THE RT OVERWING EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER ASSY, OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (ENGINE FUEL) · airframe 30,772 hrs · 17,513 cycles

THE TOWER REPORTED A VAPOR TRAIL COMING FROM THE NR 2 ENGINE. THE ACFT RETURNED TO DEPARTURE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND FOUND THE LT WING OTBD FLAPPER VALVE TO BE LEAKING. MAINTENANCE R & R THE AFFECTED FLAPPER VALVE, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,690 hrs · 17,466 cycles

DURING 2A CHECK, INSPECTION BOTH AFT EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R NR 4 EMERGENCY LIGHT BATTERY CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 29,403 hrs · 16,595 cycles

DURING C-CHECK THE CARGO DOOR INTERNAL LOWER SKIN WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5230-01208. ACFT APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,481 hrs · 16,017 cycles

DURING MX INSPECTION THE LT AND RT OVERWING EMERGENCY LIGHTS WERE FOUND 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: PROXIMITY SENSOR — DEFECTIVE (NLG) · airframe 19,549 hrs · 10,425 cycles

IAH - FLIGHT 2259, THE CREW REPORTED LANDING GEAR AIR/GRND FAIL AND TR 1&2 DISAGREE MESSAGES ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR AIR/GRND PROXIMITY SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 28,706 hrs · 9,958 cycles

IAH - FLIGHT 2187, THE CREW REPORTED A CARGO SMOKE WARNING DURING CRUISE. THE CREW DISCHARGED BOTH BOTTLES AS A PRECAUTION, AND RETURNED TO IAH, LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE BAGGAGE COMPARTMENT WITH NO DEFECTS NOTED. REMOVED AND REPLACED THE FWD SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 18,706 hrs · 9,958 cycles

IAH - FLIGHT 2187, THE CREW REPORTED A BAGG SMOKE WARNING DURING CRUISE. THE CREW DISCHARGED BOTH BOTTLES AS A PRECAUTION, AND RETURNED TO IAH, LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE BAGGAGE COMPARTMENT WITH NO DEFECTS NOTED. REMOVED AND REPLACED THE AFT SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 17,612 hrs · 9,362 cycles

RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND LT OVERWING EXIT IDENTIFIER EMERGENCY SIGN INOPERATIVE. MX REMOVED AND REPLACED NR 5 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 17,534 hrs · 9,317 cycles

RIC - DURING ROUTINE MAINTENANCE, MX FOUND CEILING EMERGENCY LOCATOR SIGN AT ROW 12 FWD SIDE INOPERATIVE. RIC MX REMOVED AND REPLACED NR 6 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 14,660 hrs · 7,786 cycles

DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN AT COCKPIT DOOR AND THE FORWARD OVERHEAD EMERGENCY EXIT SIGN WERE FOUND INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR OF THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: EXHAUST MIXER — BROKEN (RT ENGINE) · airframe 14,011 hrs · 7,461 cycles

IAH - DURING MAINTENANCE INSPECTION THE EXHAUST MIXER ON THE NUMBER TWO ENGINE WAS FOUND TO BE MISSING HALF, AND HAD DAMAGED THE THRUST REVERSER HOUSING UPON DEPARTURE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, AND THRUST REVERSER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOLENOID VALVE — LEAKING (NLG) · airframe 12,175 hrs · 6,509 cycles

AFTER TAKEOFF, THE CREW THOUGHT THAT THE NOSE LANDING GEAR DOORS MAY NOT HAVE SHUT COMPLETELY. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE. THE NOSE LANDING GEAR DOORS WERE OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,407 hrs · 6,091 cycles

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT AT THE COCKPIT DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT AT THE COCKPIT DOOR. OPERATIONAL CHECKS WERE GOOD.

Part: DISPLAY — SMOKE (COCKPIT) · airframe 7,931 hrs · 4,233 cycles

IAH - DURING INITIAL APPROACH THE CREW REPORTED SMOKE IN THE COCKPIT, THE CREW PERFORMED AN EMERGENCY DESCENT, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE FIRST OFFICERS MFD, OPERATIONALLY CHECKED WITHOUT DEFECT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 5,787 hrs · 3,095 cycles

MKE - FLIGHT 2656, THE CREW REPORTED A FALSE BAGGAGE SMOKE WARNING IN FLIGHT. THE AIRCRAFT LANDED AT MKE WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE BAGGAGE SMOKE DETECTORS ON MEL 26-15-00 CAT C CTL NUMBER 053533, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2743 WHERE MAINTENANCE REMOVED AND REPLACED BOTH BAGGAGE SMOKE DETECTORS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 5,787 hrs · 3,095 cycles

MKE - FLIGHT 2656, THE CREW REPORTED A FALSE BAGGAGE SMOKE WARNING IN FLIGHT. THE AIRCRAFT LANDED AT MKE WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE BAGGAGE SMOKE DETECTORS ON MEL 26-15-00 CAT C CTL NUMBER 053533, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2743 WHERE MAINTENANCE REMOVED AND REPLACED BOTH BAGGAGE SMOKE DETECTORS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — FROZEN (WING FLAP) · airframe 5,300 hrs · 2,681 cycles

CLE FLIGHT NR 3182, THE CREW REPORTED FLAP FAILURE, FLAPS SELECTED TO 9 DEGREES AND FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND WATER PRESENT IN THE NR 2 FLAP ACTUATOR. MAINTENANCE REPLACED THE NR 2 FLAP ACTUATOR, ALL OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE RIGHT HAND FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. THE LIGHT WAS PLACED ON MEL 33-50-04 CONTROL 041499, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO MCI ON 05-30-04 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.