N16151

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 48,220 hrs · 31,975 cycles

LH SHEAR CLIP AT REAR CABIN BULKHEAD BETWEEN STRINGER 6L AND 7L IS CRACKED. REMOVED AND REPLACED LH SHEAR CLIP AT REAR CABIN BULKHEAD BETWEEN STRINGER 6L AND 7L.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,220 hrs · 31,975 cycles

RH FLOORBEAM AT F.S 23 CORRODED. REMOVED AND REPLACED WITH NEW REPAIR DOUBLER ON RH FLOORBEAM AT F.S. 23

Part: FLOOR SUPPORT — DAMAGED (ZONE 100) · airframe 48,220 hrs · 31,975 cycles

LH FWD FLOORSILL IN CARGO DAMAGED. REMOVED AND REPLACED LH SILL AT LH FLOOR SILL IN CARGO.

Part: RIB — CRACKED · airframe 48,220 hrs · 31,975 cycles

RH AFT RIB IN MLG BAY IS CRACKED. REMOVED AND REPLACED RH AFT RIB IN MLG BAY.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,220 hrs · 31,975 cycles

RH FLOORBEAM CAP CORRODED UNDER BULKHEAD AT LAV. REMOVED CORRODED FLOORBEAM CAP, LOCATED AND DRILLED AND INSTALLED

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,220 hrs · 31,975 cycles

RH FLOORBEAM CAP CORRODED AT MOUNT HOLES FOR LAV. REMOVED RH FLOORBEAM CAP FOR REPLACE, LOCATED, AND DRILLED AND INSSTALLED

Part: RIB — CRACKED (ZONE 100) · airframe 48,220 hrs · 31,975 cycles

LH AFT RIB IN MLG BAY HAS MULTIPLE CRACKS. REMOVED AND REPLACED LH AFT RIB IN MLG BAY.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,220 hrs · 31,975 cycles

LH FLOORSILL F.S. 18 - F.S 18A CORRODED. REMOVED CORRODED LH FLOORSILL @ F.S. 18 - F.S. 18A LOCATED AND DRILLED AND INSTALLED NEW SILL.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,220 hrs · 31,975 cycles

CENTER FLOORBEAM CAP CORRODED AROUND MOUNT HOLES AT LAV. REMOVED CORRODED FLOORBEAM CAP, LOCATED AND DRILLED NEW

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,220 hrs · 31,975 cycles

OB FLOORSILL UNDER LAV CORRODED. REMOVED AND REPLACED OB FLOORSILL.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 48,220 hrs · 31,975 cycles

RH SHEAR CLIP AT REAR CABIN BULKHEAD BETWEEN STRINGER 6R AND 7R IS CRACKED. REMOVED AND REPLACED RH SHEAR CLIP AT REAR CABIN BULKHEAD BETWEEN STR 6R-7R.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,220 hrs · 31,975 cycles

FLOOR SILL AT MOUNT BOLT AT F.S. 22 CORRODED. REMOVED AND REPLACED CAP ON FLOORSILL AT FS22

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,220 hrs · 31,975 cycles

CORROSION ON FLOORSILL AT SERVICE DOOR. REMOVED AND REPLACED FLOORSILL AT SERVICE DOOR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,220 hrs · 31,975 cycles

FLOORSILL OB CORRODED FRM 46-49. REMOVED CORRODED SILL AND LOCATED AND DRILLED AND INSTALLED NEW SILL.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 47,993 hrs · 31,749 cycles

LH WTF FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH AFT EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,258 hrs · 31,046 cycles

LH ABOVE THE WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH ABOVE THE WING EMERGENCY LIGHT. OPS CHECK SAT

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,907 hrs · 30,698 cycles

COCKPIT EMERGENCY LIGHT OUT. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT BULB. OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,714 hrs · 30,513 cycles

LH ESCAPE HATCH EXIT IDENTIFIER SIGN INOPERATIVE. REMOVED AND REPLACED LH ESCAPE HATCH EXIT IDENTIFIER SIGN. OPS CHECK FAILED. RESTORED TO ORIGINAL CONFIGURATION. REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER #5. OPS CHECK SAT

Part: ELECTRONIC UNIT — INOPERATIVE · airframe 45,277 hrs · 29,226 cycles

FLAP LOW SPEED AT ACCELERATION ALTITUDE FOLLOWED BY FLAP FAIL SHORTLY AFTER. REMOVED AND REPLACED FECU. OPS CHECK SAT.

Part: HANDLE — OUT OF ADJUST · airframe 44,752 hrs · 28,753 cycles

NOT ABLE TO OPEN THE MAIN CABIN DOOR FROM INSIDE THE PLANE. REPOSITIONED MAIN CABIN DOOR HANDLE. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE · airframe 44,534 hrs · 28,574 cycles

LEFT SIDE ESCAPE HATCH EXIT IDENTIFIER INOPERATIVE. LIGHT FUNCTIONED AFTER RUNNING APU AND PERFORMING FUNCTIONAL TEST. OPS CHECK SAT.

Part: NONE — INOPERATIVE · airframe 44,048 hrs · 28,128 cycles

FOUND LH LOWER HATCH DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LOWER HATCH DOOR EMERGENCY LIGHT. OPS CHECK SAT

Part: NOT REPORTED — NOT REPORTED · airframe 43,680 hrs · 27,791 cycles

MCD EMERGENCY LIGHT INOPERATIVE. REMOVED MCD EMERGENCY LIGHT HOUSING. FOUND BAD GROUND. CLEANED GROUND WIRE RING TERMINAL. REINSTALLED MCD EMERGENCY LIGHT. OPS CHECK SAT

Part: NONE — NONE · airframe 43,285 hrs · 27,433 cycles

COVER FRAME 68 SHEAR CLIP REPAIR INVESTIGATION. AT FRAME 68 SHEAR CLIP REPAIR REMOVED AT FR 68, SHEAR CLIP REPAIRED.

Part: NONE — NONE · airframe 43,285 hrs · 27,433 cycles

AFTER NDT INSPECTION, RH FUSE SKIN FOUND CRACKED AT FR 75 BTW STR 2R-3R. RH FUSE SKIN AT FR 75 BTW STR 2R-3R CRACK REMOVED. RH FUSE SKIN AT FR 75 BTW STR 2R-3R REPAIRED

Part: NONE — NONE · airframe 43,285 hrs · 27,433 cycles

CENTER FUSE I, UNDER FLOOR SKIN CORRODED BTW FRAME 17-19 AND STR 21R-21L. CENTER FUSE I, UNDER FLOOR SKIN BTW FRAME 17-18 AND STR 21R-21L BLENDED FOR INVESTIGATION. AFTER INVESTIGATION, CORROSION ON LOWER SKIN BTW FR 17-19 AND BTW STR 21L-21R FOUND OUT OF LIMITS. DURING THE INSTALLATON OF THE REPAIR DOUBLER, THE SKIN STARTED TO DO AN OIL-CANNING EFFECT AFT OF THE CUTOUT. SKIN REPAIRED IN CF BW FR17-19 AND STR 21L-21R PERFORMED. CORROSION LEVEL 1

Part: NONE — NONE · airframe 43,285 hrs · 27,433 cycles

AFTER NDT INSPECTION, CRACK FOUND IN LH PYLON YOKE BLIND FASTENER HOLE. HOLE REPAIRED WITH BUSHING AND ALTERNATE MATERIAL

Part: NONE — NONE · airframe 43,285 hrs · 27,433 cycles

INSPECT FOR AND TREAT AS NEEDED ANY CORROSION UNDER THE REAR FUSELAGE II NAMEPLATES. ON LOWER REAR FUSE II LH OUTB RIB, BTW FR 79-80 RIB DAMAGED. SPLICE REPAIR ON LOWER REAR FUSE II LH OUTB RIB, BTW FR 79-80 REPAIRED. AT FR 78 NAMEPLATES REMOVED FOR INVESTIGATION AND SKIN FOUND CORRODED OUT OF LIMIT. CORROSION ON SKIN REPAIRED WITH DOUBLER AND NAMEPLATES RE-INSTALLED. CORROSION LEVEL 1

Part: NONE — NONE · airframe 43,285 hrs · 27,433 cycles

CENTER FUSE IV, UNDER FLOOR, SHEAR CLIP FRAME 60 BTW STR 18R-20R CORRODED. CENTER FUSE IV, UNDERFLOOR, SHEAR CLIP FRAME 60 BTW 18R-20R OUT OF LIMITS. CENTER FUSE IV, POST FR60 REMOVED FOR ACCESS AND SHEAR CLIP FR 60 STR 18R-20R REMOVED FOR REPLACEMENT. CENTER FUSE IV, UNDERFLOOR, SHEAR CLIP FR60 BTW STR 18R-20R REPLACED WITH MADE REPAIR PART, LOCALLY FABRICATED AND MASTER PART AND INSTALLED WITH RIVETS. POST AT FR60 REINSTALLED

Part: NONE — NONE · airframe 43,285 hrs · 27,433 cycles

CF2, RH SIDE, FR25 AT FLOOR LEVEL BEHIND SILL, FRAME FOUND CRACKED. FRAME SPLICED.

Part: NONE — NONE · airframe 43,285 hrs · 27,433 cycles

BAGGAGE DOOR SCRATCHED ABOVE FLAPPER DOOR. ON BAGGAGE DOOR ABOVE FLAPPER AREA STRIPPED FOR INVESTIGATION, SCRATCH WITH DENT OUT OF LIMITS. PERFORMED CUT-OUT ON BAGGAGE DOOR. FABRICATED, LOCATED, AND DRILLED REPAIR DOUBLER AND REPAIR FILLER. INSTALLED REPAIR PARTS ON BAGGAGE DOOR ABOVE FLAPPER DOOR. BAGGAGE DOOR SCRATCHES AND DENT REPAIRED.

Part: NONE — NONE · airframe 43,285 hrs · 27,433 cycles

CENTER FUSE IV, UNDER FLOOR, LH GUSSET BTW FRAME 59-61 CORRODED. OMEGA BEAM BLENDED OUT OF LIMITS BTW FR 60-61. CENTER FUSE IV BTW FR 60-61, LH OMEGA BEAM REPAIRED AND GUSSET REPLACED. NO CORROSION FOUND.

Part: NONE — NONE · airframe 43,285 hrs · 27,433 cycles

VENTRAL FUEL TANK, FWD SECTION BRACKET CORRODED. WEB REPAIRED. CORROSION LEVEL 1.

Part: NONE — NONE · airframe 43,285 hrs · 27,433 cycles

CENTER FUSE IV, UNDER FLOOR, CENTER OMEGA BEAM BTW FRAME 59-61 CORRODED. CENTER OMEGA BEAM BTW FR 60-61 IN CENTER FUSE IV UNDERFLOOR, CORROSION UNDER NUT PLATE CUT. CENTER OMEGA BEAM BTW FR60-61 IN CENTER FUSE IV REPAIRED WITH DOUBLER. NO CORROSION FOUND.

Part: NONE — NONE · airframe 43,285 hrs · 27,433 cycles

CENTER FUSE IV, UNDER FLOOR, RH OMEGA BEAM BTW FR 59-61 CORRODED. RH OMEGA BEAM BTW FR 60-61 IN CENTER FUSE IV UNDERFLOOR, CORROSION UNDER NUT PLATE CUT. RH OMEGA BEAM BTW FR60-61 IN CENTER FUSE IV REPAIRED WITH DOUBLER. NO CORROSION FOUND.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,281 hrs · 27,430 cycles

3 EMERGENCY LIGHTS INOPERATIVE AT ROW 18. REMOVED AND REPLACED #3 EMERGENCY BATTERY. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (SEAT18A) · airframe 42,898 hrs · 27,097 cycles

LOWER EMERGENCY LIGHT AT SEAT 18A INOPERATIVE. R&R EXIT ID SIGN. OPS CHECK SAT.

Part: O-RING — DAMAGED (BLEED DUCT) · airframe 42,728 hrs · 26,946 cycles

BLEED 1 LEAK MESSAGE ON EICAS. (CREW REPORTED AT FL220 MESSAGE APPEARED AND HE DECLARED AN EMERGENCY, THE THEN WENT THROUGH THE CHECKLIST AND WHEN BLEED WAS DESELECTED THE MESSAGE WENT OUT SO HE ADVISED TOWER HE RESOLVED THE ISSUE AND DIDN’T NEED PRIORITY LANDING BUT REPORTED AN EMERGENCY WAS STILL DECLARED). R&R AIR BLEED SYSTEM DUCT LINE O-RINGS @ POSITIONS 15, 23 AND 29. PERFORMED AIR BLEED SYSTEM DUCT LEAKAGE TEST. OPS CHECK SAT. LEAK CHECK SAT.

Part: WIRE HARNESS — DISCONNECTED (EXIT SIGN) · airframe 42,549 hrs · 26,786 cycles

LT EMERGENCY EXIT ROW LOWER EXIT ID SIGN INOPERATIVE. INSPECTED LT EMERGENCY EXIT IDENTIFIER SIGN AT THE EMERGENCY EXIT ROW AND RE-CONNECTED HARNESS FOR THE PROPER CONNECTION. OPERATIONS CHECK COMPLETED, NO FAULTS FOUND.

Part: LIGHT — MISSING (CABIN) · airframe 42,448 hrs · 26,697 cycles

EMERGENCY FLOOR LIGHT PATH, FRONT END OF EACH SIDE STRIP RED BLOCKS ARE MISSING OR WORN. ALSO, MISSING 4 END CAPS AT POSITION 9A, 9CD, 22CD AND FWD RIGHT JUST AFT GALLEY. MULTIPLE LOCATION TRACK IS LOOSE FROM FLOOR. INSTALLED EMERGENCY FLOOR LIGHTING PATH FRONT END STRIPS OF MISSING RED BLOCKS. INSTALLED 4 END CAPS AT LOCATIONS 9A, 9CD, 22CD AND FWD RIGHT END AFT GALLEY.

Part: CLAMP — LOOSE (FAN AIR VALVE) · airframe 42,192 hrs · 26,477 cycles

BLEED LEAK IN FLT--- T/S MSG PER FIM TASK 36-20-00. FOUND FAN AIR VALVE CLAMP LOOSE. SAME RETORQUED. PERFORMED OPS CHECK WITH NO FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (BLEED LEAK) · airframe 42,124 hrs · 26,424 cycles

BLEED #1 LEAK IN ICE CONDITIONS. PERFORMED OPS CHECK OF ANTI-ICE SYSTEMS. OPS CHECK GOOD.

Part: BRACKET — BROKEN (LT WING) · airframe 41,012 hrs · 25,509 cycles

BRACKET BROKE INSIDE 1ST LT FUEL UNDERWING ACCESS OPENING ON 1ST RIB. R&R BRACKET INSIDE 1ST LT FUEL UNDERWING ACCESS OPENING ON THE FIRST RIB.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

AFT CARGO FRAME 67 O/B SIDE OF LT OMEGA BEAM FLOOR SUPPORT BRACKET IS CRACKED. REMOVED & REPLACED BRACKET.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

AFT CARGO FRAME 65 RT SIDEWALL LINER SUPPORT HAS CORROSION AT STR 15R. R&R AFT CARGO FRAME 65 RT SIDEWALL LINER SUPPORT.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

LT OMEGA BEAM UPPER DIGITAL AT FRAME 16 CRACKED. REPAIRED LT OMEGA BEAM UPPER DIGITAL.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

CARGO DOOR Z ANGLE FWD AND AFT DOUBLERS ARE CORRODED. REMOVED & REPLACED FWD DOUBLER. AFT DOUBLER SHOES NO CORROSION DAMAGE AND IS SERVICEABLE AS IS.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

SIGNS OF CORROSION ON CARGO FLOOR GUSSET BETWEEN FR 65-68 - REMOVED GUSSET. MATCH DRILLED AND COUNTERSUNK NEW GUSSET. INSTALLED GUSSET BETWEEN FR 65-68.

Part: STAND OFF — CRACKED (TE FLAP) · airframe 41,012 hrs · 25,509 cycles

LT WING T/E O/B FLAP SHROUD I/B SUPPORT STANDOFF IS CRACKED. REMOVED & REPLACED STANDOFF SUPPORT AT LT WING T/E O/B FLAP UPPER SHROUD.

Part: STAND OFF — CRACKED (TE FLAP) · airframe 41,012 hrs · 25,509 cycles

RT WING T/E O/B FLAP SHROUD I/B SUPPORT STANDOFF IS CRACKED. REMOVED & REPLACED STANDOFF SUPPORT AT RT WING T/E O/B FLAP UPPER SHROUD.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

SERVICE DOOR LOWER THRESHOLD HAS CORROSION ON UPPER SURFACE FROM FR 20 THRU 22. BLEND OUT THE DAMAGED AREA AND REMOVED ALL OF THE CORROSION. REQUIRES TO BE NDI. PERFORMED HF EC INSPECTION OF BLENDED AREAS. NO DEFECTS NOTED. GOOD TO CONTINUE WITH REPAIR. REPAIRED THE DAMAGED AREA.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

CARGO DOOR CUT OUT HAS CORROSION AT FR 65 BELOW STR 16. REMOVED UPPER OPENING 'X' ANGLE, FWD (FR 65) SHEAR TIE, AND FWD CARGO DOOT TRACK. DE-RIVETED WEB ASSEMBLY FWD OF FRAME 65 TO ALLOW MOVEMENT FOR CUTTING FRAME 65. REMOVED ACCUPLEX BRACKETS / HDW. PICKED UP AND TRANSFERED HOLES ONTO NEW FR 65 SHEAR CLIP, SPLICED FR 65 AND PICKED UP HOLES ON NEW FR 65 PIECE. FABRICATED DOUBLERS FOR FR 65 SPLICE LOCATION. DRILLED, ALODINED & PRIMED. FABRICATED SHIM FOR USE BEHIND DOUBLER TO ALLOW PROPER RIG OF REPAIR COMPONENTS. BEGAN INSTALLATION OF REPAIR COMPONENTS. INSTALLED UPPER OPENING 'Z' ANGLE & RELATED BRACKETS. INSTALLED REPAIR. FILLET / EDGE SEAL STILL REQUIRES & 5 CHERRY RIVETS AT FRAME 62/UPPER 'Z' ANGLE INTERFACE. REMOVED FWD BAGGAGE DOOR MICROSWITCH TO FOM. APPLIED FILLET EDGE SEALANT & INSTALLED 5 CHERRY RIVET ON 'Z' ANGLE. INSTALLED BAGGAGE DOOR MICROSWITCH, OPS CHECK GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

CENTER OMEGA BEAM CENTER SPLICE IS CRACKED AT FR 20 TO 22. REMOVED ANGLE AT CENTER OMEGA BEAM SPLICE FR 20 TO 22. INSTALLED ANGLE AT CENTER OMEGA BEAM SPLICE FR 20 TO 22.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

SHEAR CLIP CRACKED PAX CABIN LH SIDE AT FRAME 26 STR 15L. R&R CRACKED SHEAR CLIP AT FR 26 STR 15L.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

RT FLOOR SILL AFT OF FRAME 23 CORRODED. BLEND OUT THE DAMAGED AREA AND REMOVED AL OF THE CORROSION STILL REQUIRES TO BE NDI. PERFORMED HF EC INSPECTION OF BLENDED AREA NO DEFECTS NOTED. GOOD TO CONTINUE WITH REPAIR. REPAIRED THE DAMAGED AREA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

LT OMEGA BEAM UPPER DIGITAL HAS CORROSION FWD OF FRAME 19. CUTOUT DAMAGE ON LT OMEGA BEAM UPPER DIGITAL, FWD OF FRAME 19. REQUIRES NDI. PERFORMED HF EC INSPECTION OF CUTOUT EDGES. NO DEFECTS NOTED. GOOD TO CONTINUE WITH REPAIR. FABRICATED DOUBLER AND FILLER AND INSTALLED ON LT OMEGA BEAM UPPER DIGITAL FWD OF FR 19. FINISHED INSTALLATION OF FILLER AND DOUBLER ON LT OMEGA BEAM UPPER DIGITAL AT FWD OF FRAME 19. RESTORED SURFACE PROTECTION.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

RAMP SUPPORT ANGLE CRACKED ON LT OMEGA BEAM AT FRAME 19. REMOVED & REPLACED RAMP SUPPORT ANGLE ON LT OMEGA BEAM AT FR 19.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

LT FLOOR SILL BETWEEN FRAMES 46 & 51 HAVE CORROSION. REMOVED THE 2 LT FLOOR SILLS FROM FRAME 46-FR52 & REPLACED THE AFT ONE & FWD ONE TO FR46 NEEDS DRILLED & INSTALLED YET. INSTALLED THE FWD LT SILL AT FR46.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

CARGO COMPARTMENT SHEAR CLIP CRACKED AT FRAME 65 STR 17L. R&R SHEAR CLIP AT FR 65 STR 17L.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

RT FLOOR SILL AT FRAME 46 & 48 HAVE CORROSION. REMOVED THE RT FLOOR SILL AT FR 46 AND THE ONE AT FR 48. INSTALLED RT FLOOR SILLS AT FR 46 & FR 48.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

RT STEP-UP AT FRAME 23 HAS CORROSION. REMOVED RT STEP-UP AT FRAME 23. INSTALLED RT STEP-UP AT FRAME 23.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

STOP SIGN ON RT OMEGA BEAM AT FRAME 22 HAS CORROSION. REMOVED & REPLACED STOP SIGN ON RT OMEGA BEAM AT FRAME 22.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

RT WALL SEAT TRACKS BETWEEN FRAMES 41 & 50 HAVE CORROSION. R&R CORRODED WALL SEAT TRACKS BETWEEN FRAMES 41 & 50.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

LT FLOOR SEAT TRACKS BETWEEN FRAMES 39 & 42 HAVE LIGHT CORROSION. R&R CORRODED LT FLOOR SEAT TRACKS BETWEEN FRAMES 39 & 42.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

LT OMEGA BEAM UPPER DIGITAL AT FRAME 50 HAS CORROSION. REMOVED SEAT TRACKS AND OMEGA BEAM UPPER DIGITAL. INSTALLED OMEGA BEAM UPPER DIGITAL, SEAT TRACKS STILL NEEDS TO BE INSTALLED. INSTALLED THE SEAT TRACKS.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

CARGO COMPARTMENT RT FLOOR SILL AT FRAME 67 CRACKED. R&R RT FLOOR SILL AT FR 67.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

CRACK AT LT FRAME 46 LOWER FRAME END FITTING BELOW LT FLOOR SILL. R&R THE CRACKED FITTING AT FR 46 BELOW FLOOR SILL.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

LT SILL CORRODED BETWEEN FR 19 & 21. R&R LT SILL BETWEEN FR 19 & 21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

CENTER OMEGA BEAM UPPER DIGITAL HAS CORROSION BETWEEN FRAME 20 & 23. REMOVED CENTER OMEGA BEAM UPPER DIGITAL BETWEEN FRAME 20 AND 23. LOCATED AND DRILLED NEW OMEGA BEAM. STARTED INSTALLATION OF NEW OMEGA BEAM DIGITAL BETWEEN FRAME 23 AND 23. FINISHED INSTALLING OMEGA BEAM UPPER DIGITAL.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

CARGO DOOR LOWER THRESHOLD 'Z' ANGLE HAS CORROSION. REMOVED DAMAGED 'Z' ANGLE. PICKED-UP AND TRANSFEREDHOLE ON TO NEW CARGO DOOR LOWER 'Z' ANGLE. INSTALLED LOWER 'Z' ANGLE. TRIM & EDGE SEAL LEFT REMAINING. APPLIED EDGE SEAL & TRIMMED CARGO DOOR LOWER THRESHOLD.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 41,012 hrs · 25,509 cycles

LT AFT WHEEL WELL WEB IS CRACKED IN 2 PLACES. REMOVED LH AFT WHEEL WELL WEB & LOWER ANGLE. INSTALLED NEW LOWER REAR ANGLE. INSTALLED NEW LH AFT WHEEL WELL WEB.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

AFT CARGO FRAME 73 RT SIDE SHEAR CLIP IS CRACKED BETWEEN STR 9 & 10R. R&R AFT CARGO FR 73 RT SIDE SHEAR CLIP BETWEEN STR 9 & 10R.

Part: SUPPORT — CORRODED (CARGO DOOR) · airframe 41,012 hrs · 25,509 cycles

CARGO DOOR LOWER FRAME ANGLE SUPPORT HAS CORROSION AROUND NUTPLATE HOLES. REMOVED AND INSTALLED CARGO DOOR LOWER FRAME ANGLE SUPPORT. FURTHER WORK INCLUDES INSTALLING NUTPLATES. INSTALLED NUTPLATES ON CARGO DOOR LOWER FRAME ANGLE SUPPORT.

Part: WEB — CRACKED (RT MLG WW) · airframe 41,012 hrs · 25,509 cycles

RT AFT WHEEL WELL WEB IS CRACKED IN 4 PLACES. REMOVED CRACKED LOWER ANGLE ON RT AFT WHEEL WELL WEB. INSTALLED NEW LOWER ANGLE. NUTPLATES STILL NEED INSTALLED. INSTALLED NUTPLATES ON RT AFT WHEEL WELL WEB. OUTBOARD RIB ON WHEEL WELL WEB NEEDS INSTALLED. INSTALLED OUTBOARD RIB ON RT AFT WHEEL WELL WEB.

Part: ANGLE — CORRODED (LT WING) · airframe 41,012 hrs · 25,509 cycles

LT WING L/E UPPER SURFACE AT FRAME 41 BELLY FAIRING 'L' ANGLE ON TOP OF WING IS CRACKED. REMOVED DAMAGED AREA OF SUPPORT ANGLE. REMOVED FUEL PNL 155NZ. REPAIRED LT WING UPPER SURFACE AT FRAME 41 'L' ANGLE. NUTPLATE FOR FWD FAIRING STILL REQUIRES INSTALL. INSTALLED NUTPLATE ON LT 'L' ANGLE. INSTALLED FUEL PANEL 155NZ.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

COCKPIT FR 10 RT SIDE IS CRACKED AT UPPER END BELOW DV SLIDING WINDOW. R&R COCKPIT FR 10 RT SIDE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

AFT CARGO FRAME 68 ABOVE CARGO DOOR SHEAR CLIP IS CRACKED BETWEEN STR 6 & 7 LT. R&R SHEER CLIP AT FR 68 ABOVE CARGO DOOR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

AFT CARGO AT FR 65 SIDEWALL LINER SUPPORT FRAME HAS CORROSION & GOUGES AROUND NUTPLATE HOLES BETWEEN STR 2 THRU 14 LT. REMOVED RIVETS SECURING FRAME TO THE AIRCRAFT, TO ALLOW CUT OUT OF AFFECTED AREA. DEVELOPED RIVET PATTERN AND FABRICATED REPAIR PARTS. COMPLETED REPAIR ON FR 65.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

AFT CARGO DOOR CUT OUT FWD LATERAL 'L' SHAPE ANGLE AT FRAME 65 HAS CORROSION ON LOWER FWD CORNER. REMOVED & REPLACED SHEAR TIE.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 41,012 hrs · 25,509 cycles

AFT CARGO DOOR AFT TORSION BAR LOWER SUPPORT BRACKET IS CRACKED ON BACKSIDE. R&R CARGO DOOR TORSION BAR LOWER SUPPORT BRACKET.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 41,012 hrs · 25,509 cycles

CARGO DOOR CUP HOLDER SUPPORT AT FR 68 IS CRACKED ON LOWER SIDE. R&R CARGO DOOR CUP HOLDER SUPPORT BRACKET AT FR 68.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

AFT CARGO FRAME 62 LT SIDE SHEAR CLIP IS CRACKED BETWEEN STR 7 & 8 L. REMOVED SHEAR CLIP. INSTALLED AFT CARGO FRAME 62 LT SHEAR CLIP.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

AFT CARGO FRAME 67 ABOVE CARGO DOOR SHEAR CLIP IS CRACKED BETWEEN STR 5 & 6L. REMOVED & REPLACED SHEAR CLIP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

COCKPIT FRAME 10 LT SIDE IS CRACKED AT UPPER END BELOW DV SLIDING WINDOW. R&R COCKPIT FR 10 LT SIDE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

RT AFT FUSELAGE EXTERIOR SKIN AT FR 78 AT STR 4R HAS CRACK AROUND 2 EA RIVETS. REMOVED 2 EA RIVETS. UPSIZED HOLE TO .193 AND COUNTERSUNK. PERFORMED HF EC INSPECTION OF REWORKED AREAS. NO DEFECTS NOTED. GOOD TO CONTINUE WITH REPAIR. INSTALLED 2 EA RIVETS.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

AFT CARGO FRAME 73 LT SHEAR CLIP IS CRACKED BETWEEN STR 9 & 10 LT. R&R AFT CARGO FR 73 SHEAR CLIP BETWEEN STR 9&10 LT.

Part: CLOSEOUT PANEL — CORRODED (FUSELAGE) · airframe 41,012 hrs · 25,509 cycles

CARGO DOOR CUT OUT FWD LOWER CORNER AT FRAME 65 CLOSE OUT PANEL HAS CORROSION. REMOVED DAMAGE COMPONENTS / FRAMES. LOCATED & DRILLED NEW CLOSE OUT PANEL. INSTALLED NEW CLOSE OUT PANEL AT FRAME 65.

Part: SUPPORT BRACKET — CRACKED (NLG) · airframe 41,012 hrs · 25,509 cycles

NLG UPLOCK SUPPORT BRACKET IS CRACKED. R & R NLG UPPER SUPPORT BRACKET.

Part: ANTENNA — INOPERATIVE (RADAR ALTIMETER) · airframe 39,982 hrs · 24,695 cycles

RAD/ALT FAIL IN FLIGHT. DEFERRED RAD ALT NR 1. R&R RA ANTENNAS. OPS CHECK GOOD.

Part: DUCT — UNSECURE (AC BAY) · airframe 39,370 hrs · 24,207 cycles

PACK 1 OFF DURING FLIGHT NO OTHER ASOCIATED EICAS MESSAGES, PACK 2 ALREADY ON DEFERRAL. RESEALED EXHAUST DUCT FROM HEAT EXCHANGER. OPS CHECK GOOD.

Part: FUEL TANK — LEAKING (LT WING) · airframe 38,213 hrs · 23,224 cycles

PASSENGER NOTICED FUEL LEAKING FROM THE LEFT WING DURING FLIGHT. FIRST OFFICER VERIFIED FUEL LEAKING FROM THE LEFT WING. CAPTAIN REPORTED LOST 50 LBS FROM THE LEFT WING WITHIN 10 MINUTES. INSPECTED THE LEFT WING FOR LEAKS, FOUND TO BE TYPE 1 RUNNING LEAK, SEALED THE LT FUEL TANK, .LEAK CHECKED GOOD.

Part: CONNECTOR — OUT OF POSITION (WINDWHIELD WIPER) · airframe 38,110 hrs · 23,143 cycles

LEFT WINDSHIELD WIPER FLOPPING AND MOVING LATERALLY DURING CLIMB AND LEVEL FLIGHT. FOUND WIPER OVERHEAD CONTROL PANEL ASSY CONNECTOR OUT OF PLACE AND SECURED IT. OPS CHECKED GOOD.

Part: AHRS — FAILED (NR 1) · airframe 37,585 hrs · 22,742 cycles

AHRS 1 FAIL IN FLIGHT. R&R NR 1 AHRS COMPUTER, OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 37,249 hrs · 22,426 cycles

LEFT OVERWING EMERGENCY SIGN WAS INOPERATIVE. FOUND THE LT OVERWING EMERGENCY SIGN CONNECTOR WAS LOOSE. CONNECTED, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,620 hrs · 21,869 cycles

LT UPPER EMERGENCY DOOR EXIT LIGHT INOP. R&R NR 3 EMERGENCY LIGHT BATTERY, OPS CHECK GOOD.

Part: TRANSDUCER — INTERMITTENT (ENGINE OIL) · airframe 36,011 hrs · 21,323 cycles

NR 1 ENGINE OIL PRESSURE RAPIDLY FLUCTUATED TO ABOUT 163 PSI ABOVE 27000. PRESSURE BECAME NORMAL AGAIN BELOW 27000. R & R THE NR 1 PRESSURE TRANSDUCER, OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,557 hrs · 20,111 cycles

EMERGENCY EXIT LIGHT IN PSU PANEL AT 18CD LIGHT 22 IS INOPERATIVE. R & R EMERGENCY LIGHT BULB AT 18CD. OPS CHECK GOOD.

Part: LINE — FAILED (HYD SYSTEM) · airframe 34,171 hrs · 19,811 cycles

HYD SYSTEM 2 FAIL IN FLIGHT. R & R NR 2 HYD PUMP ENG PRESSURE LINE. OPS AND LEAK CHECK GOOD.

Part: SEAL — WORN (BLEED AIR SYSTEM) · airframe 34,160 hrs · 19,801 cycles

BLEED 2 LEAK. R & R BLEED SEALS. LEAK AND OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 34,023 hrs · 19,686 cycles

LEFT EMERGENCY EXIT DOOR MARKER NR 23 IS INOPERATIVE. UPON INSPECTION, FOUND ELECTRICAL CONNECTORS TO BE DISCONNECTED. CONNECTED THE CONNECTORS. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 33,753 hrs · 19,476 cycles

CEILING EMERGENCY EXIT SIGN AT ROW 18, AFT SIDE, LIGHT 18B IS INOPERATIVE. RE-CONNECTED THE PIN CONTACT FOR CEILING EMERGENCY EXIT SIGN AT ROW 18, AFT SIDE, LIGHT 18B. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (WING) · airframe 31,908 hrs · 18,057 cycles

PASSENGER REPORTED THERE WAS SOMETHING STREAMING FROM WING DURING CRUISE, RETURNED TO BLOCK. MAINTENANCE PERFORMED GVI OF WING FOR LEAKS, NO DEFECTS NOTED.

Part: CONTROL MODULE — SHORTED (CABIN LIGHTS) · airframe 29,842 hrs · 16,695 cycles

PILOT REPORTED A STRONG BURNING ODOR NEAR SEAT 1A WHEN THE ACFT WAS POWERED UP. MX R & R THE CABIN LIGHTING CONTROL MODULE ASSY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,772 hrs · 16,652 cycles

DURING MX INSPECTION THE LT SIDE OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MX R & R LAMP, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SOCKET — BURNED (LIGHT) · airframe 29,755 hrs · 16,640 cycles

THE CREW REPORTED CABIN SMOKE. MAINTENANCE INSPECTED AND REPLACED THE SIDE WALL LIGHT FIXTURE BRACKET AT SEAT 10A. OPS CHECKED WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 29,749 hrs · 16,636 cycles

FLOOR SUPPORT AT Y0.0 AND X 6723.0 IS CORRODED. BLENDED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-21-10.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 29,749 hrs · 16,636 cycles

RIGHT FLOOR SUPPORT JUST AFT OF SERVICE DOOR AT S15R X-6723.0 IS CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 29,749 hrs · 16,636 cycles

FLOOR SUPPORT AT Y0.0 AND X14513.6 IS CORRODED. R & R CENTER FLOORBEAM GUSSET BETWEEN FRAMES 39-46 IAW SRM 51-40-02.

Part: SILL — CORRODED (ZONE 100) · airframe 29,749 hrs · 16,636 cycles

LEFT SILL AT STGR 15L AND X16783.5 IS CORRODED. BLENDED LT SILL AT STGR 15L AND X16783.5 IAW SRM 53-23-10. FOUND TO BE WITH-IN ALLOWABLE LIMITS IAW SRM 53-23-10.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 29,749 hrs · 16,636 cycles

FLOOR SUPPORT AT Y0.0 X 8154.0 IS CORRODED. BLENDED CORROSION ON FLOOR SUPPORT. ALLOWABLE MATERIAL LOSS IS LESS THAN 30 PERCENT. MATERIAL LOSS WAS .008". FOUND TO BE WITHIN LIMITS IAW SRM 53-22-10.

Part: ANTENNA — CORRODED (LOWER TCAS) · airframe 29,749 hrs · 16,636 cycles

LOWER TCAS ANTENNA BASE CORRODED. R & R LOWER TCAS ANTENNA IAW AMM 34-43-03.

Part: STRINGER — CORRODED (ZONE 100) · airframe 29,749 hrs · 16,636 cycles

RIGHT STRINGER 15 BETWEEN BS 11016.4 AND 11388.8 IS CORRODED. BLENDED CORROSION ON RT STRINGER. ALLOWABLE MATERIAL LOSS IS 30 PERCENT MATERIAL LOSS WAS .008". FOUND TO BE WITHIN LIMITS IAW SRM 53-22-10.

Part: FITTING — GOUGED (ZONE 200) · airframe 29,749 hrs · 16,636 cycles

AFT AVIONICS DOOR, FORWARD PIN FUSELAGE BRACKET IS GOUGED. BLENDED GOUGE WITH .010 MATERIAL LOSS IAW EMB ETD2014-145-024302 AND EXPRESSJET EC5330-02878, REV ORIG, DATED 24 MAR 2014. NDT PERFORMED BY KB INSPECTION SERVICES, CRS# K9QR554B ON 24 MAR 2014. AVMAX WORK ORDER 80210; WORK CARD 2269. DMI CREATED TO ACCOMPLISH TASK 53-31-00-220-838-A00 AT INTERVAL OF 4,520 FC. NEXT INSP DUE AT 21,156FC.

Part: STRUCTURE — GOUGED (E/E BAY DOOR) · airframe 29,749 hrs · 16,636 cycles

AFT FUSELAGE AFT AVIONICS DOOR HAS GOUGES AT HANDLE CUTOUT EDGE. BLENDED OUT 3 GOUGES AT HANDLE CUTOUT EDGE WITH DIMENSION OF 1.1" LONG BY .075" WIDE IAW ETD2014-145-022223 AND EC5230-01323, REV, ORIG, DATED 19 MAR 2014. NDT PERFORMED ON 18 MAR 2014. THIS REPAIR HAS RECURRING INSPECTION AND A DMI CREATED FOR ACCOMPLISHMENT OF TASK 52-44-00-220-801-AOO AT AN INTERVAL OF 10,000 FC.

Part: FLAPPER VALVE — LEAKING (ZONE 600) · airframe 28,718 hrs · 15,987 cycles

CREW REPORTED A POSSIBLE FUEL LEAK FROM THE RT WING. ACFT RETURNED TO DEPARTURE WITHOUT INCIDENT. MAINTENANCE R & R FLAPPER VALVE AT RIB 19 ON THE RT WING, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,164 hrs · 14,994 cycles

DURING SCHEDULED MX INSPECTION THE AFT CEILING EMERGENCY LIGHT ABOVE ROW 12 WAS FOUND INOPERATIVE. MX R & R THE CEILING EMERGENCY LIGHT LAMP WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRECOOLER — FAULTY (BLEED AIR SYS) · airframe 23,500 hrs · 12,598 cycles

THE CREW REPORTED A BLEED OVERTEMP IN CLIMB. THE ACFT RETURNED TO DEPLARTURE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR 1 PRECOOLER. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,214 hrs · 12,418 cycles

IAH - FLIGHT 4348 THE CREW REPORTED A SMOKE SMELL IN THE CABIN. MAINTENANCE COMPLIED WITH FIM TASK 72-00-00-810-814 WITH NO DEFECTS OR SMELL NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,537 hrs · 12,040 cycles

IAH - DURING MAINTENANCE INSPECTION THE CEILING PANEL OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAILED (COCKPIT) · airframe 21,771 hrs · 11,625 cycles

EWR FLT 2162 THE CREW REPORTED THE ISIS FAILED IN FLIGHT. SCREEN WENT BLANK. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ISIS CONTROL UNIT AND OPERATIONAL CHECKS WERE GOOD.

Part: ELECTRONIC UNIT — DEFECTIVE (LANDING GEAR) · airframe 21,769 hrs · 11,624 cycles

FLIGHT 2685 - FLIGHT CREW REPORTED LANDING GEAR AIR/GROUND SYSTEM FAIL ON ROTATION DURING T/O. EWR MX REMOVED AND REPLACED LGEU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL MODULE — INOPERATIVE (COCKPIT) · airframe 20,239 hrs · 10,792 cycles

IAH - FLIGHT 2122, THE CREW REPORTED THAT THE THRUST RATING SETTINGS WOULD NOT RESPOND CORRECTLY. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE POWERPLANT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HOUSING — GOUGED (RT MLG) · airframe 19,863 hrs · 10,587 cycles

TYS - RT MLG HOLLOW PIN FWD BEARING HOUSING IS SCRATCHED/GOUGED ACROSS WIDTH AT THE 4 O'CLOCK AND 8 O'CLOCK POSITION. REMOVED AND REPLACED RT FWD SIDE BRACE FITTING IAW EC5750-01418.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,102 hrs · 10,162 cycles

TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RT FLOOR SILL CORRODED FROM FR 48 TO FR 52. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 145XR SRM 51-40-02;09, 51-20-03 AND CPM 51-21-07. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,102 hrs · 10,162 cycles

TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RT FLOOR SILL CORRODED AT FR.60. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 145XR SRM 51-40-02, 06;5120-03. ALODINED IAW EMB 135/145 CPM 51-21-04. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,102 hrs · 10,162 cycles

TYS - AFT SERVICE DOOR SILL CORRODED AT FWD END. REMOVED AND REPLACED AFT SERVICE DOOR SILL.

Part: SENSOR — INOPERATIVE (TAT PROBE) · airframe 17,850 hrs · 9,485 cycles

FLIGHT 2245 - FLIGHT CREW REPORTED TAT NR 1 HEAT INOP INDICATION ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. MX R & R NR 1 TAT PROBE AND PERFORMED OPS CHECK SUCCESSFUL. ACFT APPROVED TO RETURN TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 16,795 hrs · 8,931 cycles

FLIGHT 3070 - EWR - DURING PREFLIGHT, FLIGHT CREW FOUND EMERGENCY LIGHT STRIP BROKEN. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 16,769 hrs · 8,917 cycles

FLIGHT 2355 - EWR - DURING PREFLIGHT CHECK, FLIGHT CREW REPORTED RED MARKING MISSING ON THE EMERGENCY FLOOR STRIP. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT FLOOR STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

FWD EMERGENCY LIGHT INOPERATIVE. AND REPLACED NR 1 & NR 2 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04. OPS CHECK GOOD. NOTE: AC HAS BEEN IN C-CHECK SINCE 8/26. (K)

Part: BONDING STRAP — CORRODED (LT AILERON)

AC IS CURRENTLY IN C-CHECK AND THE LT AILERON SHROUD BONDING STRAPS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE BONDING STRAP PLATE IAW EC 5750-01315. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (K)

Part: BONDING STRAP — CORRODED (RT AILERON)

AC IS CURRENTLY IN C-CHECK AND THE RT AILERON SHROUD BONDING STRAPS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE BONDING STRAP PLATE IAW EC 575001315. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (K)

Part: SEAL — OUT OF POSITION (COCKPIT WINDOW)

ACFT WAS EN ROUTE TO EWR FROM LIT WHEN THE DV WINDOW SEAL STARTED SQUALLING. CREW DIVERTED THE FLIGHT TO TYS WHERE MAINTENANCE REPOSITIONED THE DV WINDOW SEAL ON THE CAPTAIN’S SIDE. LEAK CHECK GOOD AND SIGNED OFF TO SERVICE. (S)

Part: MANIFOLD — INOPERATIVE (APU)

FLIGHT 2358 - EWR - FLIGHT CREW REPORTED STRONG FUEL ODOR IN THE ACFT. EWR MX REMOVED AND REPLACED APU SECONDARY FUEL MANIFOLD ASSEMBLY IAW ENGINE MANUAL 49-31-06 AND PERFORMED OPERATIONAL AND LEAK CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. (A)

Part: SIGN — INOPERATIVE (CABIN) · airframe 12,695 hrs · 6,716 cycles

RIC - DURING ROUTINE INSPECTION, RIC MX FOUND BOTTOM EXIT SIGN AT SEAT 12C INOPERATIVE. MX REMOVED AND REPLACED SIGN AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 9,243 hrs · 4,934 cycles

CLE FLIGHT 2034 - THE CREW REPORTED A HIGH STAGE VALVE 2 FAIL MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE HIGH STAGE BLEED VALVE AND SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: FUEL LINE — LOOSE (APU) · airframe 11,996 hrs · 6,381 cycles

IAH - FLIGHT 2533, THE CREW REPORTED THAT THE APU CAUSES FUEL SMELL IN THE CABIN AND COCKPIT. MAINTENANCE PLACED THE APU ON MEL 49-00-00 CAT-C CTL NR 134748, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. IN BNA, MAINTENANCE TIGHTENED LOOSE FUEL LINE AT APU FUEL CONTROL IAW VCMM HAM SUN 49-32-01 MM. OPS CHECK AND LEAK CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 11,984 hrs · 6,376 cycles

IAH - FLIGHT 2680, THE CREW REPORTED THAT AFTER STARTING THE APU ON THE GROUND, AND OPENING APU BLEED AIR, THERE WAS A STRONG ODOR OF JET FUEL IN THE CABIN. THE AIRCRAFT CONTINUED TO THE GATE WHERE MAINTENANCE OPERATIONALLY CHECKED THE APU WITH NO DEFECTS, OR ODORS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 10,857 hrs · 5,804 cycles

DURING ROUTINE MAINTENANCE THE RIGHT FORWARD EMERGENCY LIGHT WOULD NOT ILLUMINATE. THE NR 2 EMERGENCY BATTERY LIGHT POWER SUPPLY WAS REPLACED. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 9,936 hrs · 5,311 cycles

FLT 2887, DURING SCHEDULED MAINTENANCE THE RT OVERWING EMERGENCY EXIT LIGHT DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 9,934 hrs · 5,310 cycles

MCI - DURING MAINTENANCE INSPECTION, THE FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 8,639 hrs · 4,614 cycles

CLE FLIGHT 2034 - THE CREW REPORTED THE EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING TESTING. MAINTENANCE INSPECTED AND RESECURED THE CONNECTOR ON THE EMERGENCY EXIT SIGN. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 3,588 hrs · 1,904 cycles

IAH - THE CREW REPORTED A LAV SMOKE DETECTOR INDICATION IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LOOSE CONNECTOR ON THE SMOKE DETECTOR PANEL. MAINTENANCE RESECURED THE CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.