N11106

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 45,020 hrs · 27,963 cycles

BOTH LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED (1) FUSE ON NR 4 EMERGENCY BATTERY TRAY. OPERATIONS CHECK GOOD.

Part: SKIN — CRACKED (FRAME 75A) · airframe 44,968 hrs · 27,908 cycles

REAR FUSE 1, LOWER SKIN CRACKED AT FR 75A BETWEEN STR 21P-21S. REPAIRED DOUBLER AND TRIPLER INSTALLED AND FRAME BOTTOM SECTION REPLACED.

Part: SKIN — DAMAGED (FRAMES 19-20) · airframe 44,968 hrs · 27,908 cycles

DURING REMOVAL OF REPAIR DOUBLER LOCATED ON RT CENTER FUSE 1 BETWEEN FRAME 19-20 AND STR 18-19R. RT CENTER FUSELAGE I BETWEEN FR 19-20 AND BETWEEN STR 18R-20R DAMAGE TO SKIN REPAIRED.

Part: SKIN — DAMAGED (FRAMES 11-12) · airframe 44,968 hrs · 27,908 cycles

SKIN DAMAGE ON RT FWD FUSE 2, BETWEEN FR 11-12 AND BETWEEN STR 17R-18R. SKIN REPAIRED ON RT FWD FUSELAGE 2, BETWEEN FR 11-12, BETWEEN STR 17R-18R.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

LAV CENTER OMEGA BEAM AT FR 59 HAS CORROSION AROUND NUT PLATE HOLE - CUT-OUT DAMAGE AROUND NUT PLATE HOLE AT FR 59 CENTER OMEGA BEAM. PERFORMED HF EC INSPECTION OF CUT OUT AREA, NO DEFECTS NOTED, GOOD TO CONTINUE WITH REPAIR. REPAIRED CENTER OMEGA BEAM AT FR 59.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

FRAME 18 AFT DIGITAL SUPPORT IS CORRODED - REMOVED AFT DIGITAL SUPPORT AT FR 18. INSTALLED AFT DIGITAL SUPPORT AT FR 18.

Part: CHANNEL — CRACKED (COCKPIT) · airframe 44,668 hrs · 27,609 cycles

CHANNEL IS CRACKED AT FR 10 UNDER RH DV WINDOW - R&R LH FR 10 UNDER DV WINDOW. INSTALLED NEW RH FR 10 UNDER DV WINDOW.

Part: CHANNEL — CRACKED (COCKPIT) · airframe 44,668 hrs · 27,609 cycles

CHANNEL IS CRACKED AT FR 10 UNDER LH DV WINDOW - R&R LH FR 10 CHANNEL.

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 44,668 hrs · 27,609 cycles

CARGO DOOR UPPER & LOWER EDGE HAS LIGHT CORROSION AROUND FASTENER HOLES - REMOVED LOWER DOOR ANGLE, UPPER ANGLE FOUND TO BE PAINT DAMAGE PREPPED AND PAINTED AFFECTED AREA. STARTED INSTALLATION OF LOWER ANGLE. FINISHED INSTALLING ANGLE.

Part: WEB — CRACKED (LT MLG WW) · airframe 44,668 hrs · 27,609 cycles

L/H W/W REAR WEB IS CRACKED AT TOP O/B CORNER....R&R L/H W/W REAR WEB.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 44,668 hrs · 27,609 cycles

#1 ENGINE PYLON FWD YOKE LOWER FWD LINKAGE FITTING IS CRACKED - REMOVED AND REPLACED #1 ENGINE PYLON FWD YOKE LOWER FWD LINKAGE FITTING.

Part: WEB — CRACKED (ZONE 100) · airframe 44,668 hrs · 27,609 cycles

LH W/W REAR WEB IS CRACKED AT TOP O/B CORNER - R/R LH W/W REAR WEB, NEEDS BELLY FAIRING TEMP INSTALLED TO PICK UP NUTPLATE HOLES. INSTALLED NUTPLATES ON LH W/W REAR WEB.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

LH OVER WING LATERAL FAIRING NUTPLATE ATTACH ANGLE SUPPORT ON SIDE OF FUSELAGE BELOW OVER WING EXIT IS CRACKED - REMOVED LH OVERWING LATERAL FAIRING ATTACH ANGLE SUPPORT AT FR 43, STARTED LOCATING FASTENER HOLES. COMPLETED INSTALL OF NEW LH OVERWING LATERAL FAIRING ATTACH ANGLE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN RH OMEGA BEAM O/B LOWER SUPPORT ANGLE IS CRACKED BETWEEN FR 47 & 48 - REMOVED O/B LOWER SUPPORT AND LOCATED HOLES IN NEW PART. INSTALLED RH OMEGA BEAM LOWER SUPPORT.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 44,668 hrs · 27,609 cycles

LH OVER WING LATERAL FAIRING NUTPLATE SUPPORT ANGLE ON L/E OF WING UPPER SURFACE IS CRACKED AT FR 41 - REPAIRED LH OVER WING NUTPLATE SUPPORT ANGLE AT FR 41, STILL NEEDS NUTPLATE HOLES PICKED UP AND COLLARS INSTALLED ON HILOCS. INSTALLED COLLARS ON HI LOCS AND PICKED UP NUTPLATE HOLES ON LH OVERWING NUTPLATE ANGLE AT FR 41.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN STOP SIGN ON RH OMEGA BEAM HAS CORROSION AT FR 20 ON UPPER SURFACE - R&R MAIN CABIN STOP SIGN ON RH OMEGA BEAM AT FR 20.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN RH SIDE FLOOR SILL HAS CORROSION AT FR 40 ON UPPER SURFACE. REMOVED FLOOR SILL AT FR 40, LOCATED FASTENER AND STARTED INSTALL. COMPLETED INSTALL OF NEW FLOOR SILL AT FR 40.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN CENTER OMEGA BEAM RAMP ANGLE SUPPORT AFT END HAS CORROSION ON LOWER SIDE AT FR 20 - REMOVED RAMP ANGLE AT FR 20. INSTALLED GALLEY RAMP ANGLE AT FR 20 ON CENTER OMEGA BEAM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN RH SIDE FLOOR SILL HAS CORROSION BETWEEN FR 40 THRU 47 - REMOVED & REPLACED MAIN CABIN RH FLOOR SILL BETWEEN FR 40 THRU 47.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN LH OMEGA BEAM O/B LOWER SUPPORT IS CRACKED BETWEEN FR 47 & 48 - BEGAN REMOVING HI-LOK COLLARS FROM THE LH OMEGA BEAM O/B LOWER SUPPORT AT FR 47 & 48. REMOVED AND BEGAN REPAIR ON THE LH OMEGA BEAM O/B LOWER SUPPORT AT FR 48 & 48. INSTALLED REPAIR SECTION ON THE LH OMEGA BEAM O/B LOWER SUPPORT AT FR 47 & 48.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

LH SIDEWALL SEAT TRACK HAS CORROSION BETWEEN FR 20 THRU 23 - REMOVED THE LH SIDEWALL SEAT TRACK. INSTALLED SEAT TRACK LH.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

CENTER OMEGA BEAM UPPER DIGITAL HAS CORROSION AROUND FASTENER HOLE AT FR 16 - BEGAN REPAIR ON THE FWD DIGITAL PLATE, CENTER OMEGA BEAM AT FR 16. COMPLETED REPAIR ON THE FWD DIGITAL PLATE ON CENTER OMEGA BEAM AT FR 16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

RH SIDEWALL SEAT TRACKS HAVE LIGHT CORROSION BETWEEN FR 28 THRU 32 - REMOVED SEAT TRACK ON WALL AT FRAME 29. INSTALLED SEAT TRACK AT FRAME 29.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN RH FLOOR SILL HAS CORROSION FROM FR 30 THRU 35 RH - REMOVED AND LOCATED HOLES TO NEW SILL. INSTALLED FLOOR SILL AT FR 30.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN LH FLOOR SILL HAS CORROSION FROM FR 30 THRU 25 - R&R LH FLOOR SILL FROM FRAME 30 THRU 35.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN RH OMEGA BEAM I/B LOWER SUPPORT ANGLE IS CRACKED BETWEEN FR 47 & 48 - REPAIRED RH OMEGA BEAM I/B LOWER SUPPORT AT FR 47.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN FR 26 SHEER CLIP IS CRACKED AT STR 16 RH - R/R MAIN CABIN FR 26 SHEER CLIP AT STR 16 RH.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN FR 25 SHEER CLIP IS CRACKED AT STR 15 RH - R&R MAIN CABIN FR 25 SHEER CLIP AT STR 15 RH.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

SERVICE DOOR THRESHOLD HAS CORROSION AROUND NUTPLATE HOLES BETWEEN FR 20 THRU 22 - R&R SERVICE DOOR THRESHOLD BETWEEN FR 20-22.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN CENTER OMEGA BEAM O/B LOWER SUPPORT ANGLE IS CORRODED AND CRACKED BETWEEN FR 46 & 47 - REMOVED OMEGA BEAM LWR SUPPORT, PICKED UP HOLES IN NEW SUPPORT AND STARTED INSTALLING. FINISHED INSTALLING MAIN CABIN CENTER OMEGA BEAM O/B LOWER SUPPORT ANGLE.

Part: RIVET — DEFECTIVE (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN CENTER OMEGA BEAM UPPER DIGITAL HAS CORROSION BETWEEN FR 20 THRU 23 - UPON FURTHER INSPECTION FOUND TO BE DAMAGED PAINT AND HIGH RIVETS. REMOVED AND REPLACED RIVETS. PREPPED AND PAINTED AFFECTED AREA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN FLOOR SUPPORT BETWEEN LH OMEGA BEAM AND CENTER OMEGA BEAM AT FR 20 HAS CORROSION - REMOVED FLOOR SUPPORT BETWEEN LH & CTR OMEGA BEAM AT FR 20. INSTALLED CARBON FIBER FLOOR SUPPORT BETWEEN LH & CENTER OMEGA BEAM AT FR 20. STILL NEED NUTPLATES INSTALLED. INSTALLED NUTPLATES ON THE FR20 CARBON FIBER SUPPORT BETWEEN LH & CENTER BEAM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN LH FLOOR SILL HAS CORROSION FROM FR 26 THRU 29 - REMOVED MAIN CABIN LH FLOOR SILL FR 26-29, STARTED LOCATING FASTENER HOLES. COMPLETED INSTALL OF NEW FLOOR SILL IN MAIN CABIN FROM FR 26-29.

Part: FLOOR SUPPORT — BENT (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

LH FLOOR STEP UP BETWEEN CENTER OMEGA BEAM AND RH OMEGA BEAM IS BENT AT FR 18 - R&R FLOOR STEP UP AT FR 18

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

LH FLOOR SILL HAS CORROSION AT FR 20 - REMOVED THE LH FLOOR SILL AT FR 20. INSTALLED LH FLOOR SILL AT FR 20.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN RH FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FR 50 - REMOVED RH FLOOR SILL AT FR 50. STARTED LOCATING FASTENER HOLES IN NEW RH FLOOR SILL AT FR 50. STARTED INSTALLING MAIN CABIN RH FLOOR SILL AT FR 50. COMPLETED INSTALL OF MAIN CABIN RH FLOOR SILL AT FR 50.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

RH FLOOR SILL FWD OF SERVICE DOOR AT FR 20 HAS CORROSION AROUND NUTPLATE HOLE - FABRICATED FWD SILL REPAIR. INSTALLED FWD SILL REPAIR ON RH FLOOR SILL FWD OF SERVICE DOOR AT FR 20.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN FR 16 SHEER CLIP IS CRACKED AT STR 15 RH - REMOVED AND REPLACED SHEER CLIP AT FR 16 RH SIDE.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

MAIN CABIN LH SIDE FLOOR SILL HAS CORROSION ON UPPER SURFACE BETWEEN FR 26 THRU 39 - R&R LH FLOOR SILL AT FR 36 THRU 39.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

SHEER CLIP IS CRACKED AT FR 68 BETWEEN STR 6L-7L - REMOVED SHEER CLIP AT FR 68. INSTALLED SHEER CLIP AT FRAME 68

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

LH LAV FLOOR SILL HAS CORROSION AROUND NUT PLATE HOLES - R&R LH LAV FLOOR SILL.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

CTR GUSSET IN LAV HAS CORROSION AROUND NUT PLATE HOLES - REMOVED CTR GUSSET AT LAV. LOCATED HOLES ON NEW CTR LAV GUSSET AND INSTALLED.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

SHEER CLIP CRACKED AT FR 62 BETWEEN STR 6L-7L - PERFORMED HF EC INSPECTION OF SHEER CLIP CRACK CONFIRMED, GOOD TO CONTINUE WITH REPAIR. REMOVED CRACKED SHEER CLIP AT FR 62 BETWEEN STR 6L-7L. INSTALLED NEW CLIP.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

RH LAV GUSSET HAS CORROSION AROUND NUT PLATE HOLES - REMOVED RH LAV GUSSET. LOCATED HOLES IN NEW GUSSET AND INSTALLED RH LAV GUSSET.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

SHEER CLIP IS CRACKED AT FR73 STR 8R- PERFORMED HF EC INSPECTION OF INDICATED AREA CRACK CONFIRMED. REMOVED CRACKED SHEER CLIP AT FR 72 STR 8R. INSTALLED NEW CLIP.

Part: SUPPORT BEAM — BENT (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

CARGO FLOOR SUPPORT BEAM IS BENT AT FR-68 BETWEEN CTR AND LH GUSSETS - REMOVED AND REPLACED SUPPORT BEAM AT FR 68.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

CARGO RAMP FWD SUPPORT LOWER ATTACH BRACKET IS CRACKED - REMOVED AND REPLACED BRACKET.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

SHEER CLIP IS CRACKED AT FR 72 STR 17L- REMOVED & REPLACED SHEER CLIP AT FRAME 72 STR 17L

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

RH LAV FLOOR SILL HAS CORROSION AROUND NUT PLATE HOLES - REMOVED CORROSION ON RH LAV FLOOR SILL AROUND NUT PLATE HOLE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

SHEER CLIP IS CRACKED FR67 BETWEEN STR 6L-7L - REMOVED SHEEAR CLIP AT FR67. INSTALLED SHEER CLIP AT FR 67.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

SHEER CLIP IS CRACKED AT FR 73 STR8L - R&R SHEER CLIP AT FR 73 STR8L

Part: GUSSET — CORRODED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

LH LAV GUSSET HAS CORROSION AROUND NUT PLATE HOLES - REMOVED LH LAV GUSSET. LOCATED HOLES ON NEW LH LAV GUSSET AND INSTALLED.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

INSIDE ACCESS 312AR FRAME 80 SHEER CLIP IS CRACKED BETWEEN STR 4 & 5RH - DRILLED OUT RIVETS AND REWORKED SHEER CLIP OFF OF AIRPLANE, HOLES NEED TO BE PICKED UP ON NEW CLIP. STARTED DRILLING UP NEW PLATE AND FINDING HOLES. HOLES CONNECTING TO AIRCARFT SKIN STILL NEED TO BE PICKED-UP THEN PLATE CAN BE PRIMED, SEALED AND SHOT ON. NEW PLATE IS DRILLED UP PRIMED AND SEALED IN PLACE ON STRINGER #5 ON RH SIDE AND IS RIVETED BACK ON. COMPLETED INSTALLING FRAME 80 SHEER CLIP.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 44,668 hrs · 27,609 cycles

PAX DOOR INTERNAL HANDLE SUPPORT BRACKET HAS POSSIBLE CRACK - PERFORMED HF EC INSPECTION OF INDICATED LOCATION, CRACK CONFIRMED. R&R PAX DOOR INTERNAL HANDLE SUPPORT BRACKET.

Part: CHANNEL — CRACKED (RT PYLON) · airframe 44,668 hrs · 27,609 cycles

R/H PYLON INSIDE ACCESS PANEL 424DB UPPER "U" CHANNEL SUPPORT STIFFNER, P06 X22901.50 IS CRACKED AT O/B END....R&R UPPER "U" CHANNEL IN R/H PYLON ACCESS PANEL 424DB.

Part: ANGLE — CRACKED (FAIRING) · airframe 44,668 hrs · 27,609 cycles

LH W/W FWD O/B CORNER CENTER BELLY FAIRING 'L' ANGLE NUTPLATE SUPPORT IS CRACKED - FABRICATED AND PARTIALLY INSTALLED REPAIR FOR LH W/W FWD O/B CORNER CENTER BELLY FAIRING L ANGLE. BELLY FAIRING NEEDS TO BE TEMP INSTAALED TO PICK UP NUTPLATE POSITION. INSTALLED NUTPLATES ON CENTER BELLY FAIRING L ANGLE REPAIR.

Part: ANGLE — CRACKED (FAIRING) · airframe 44,668 hrs · 27,609 cycles

L/H W/W FWD O/B CORNER CENTER BELLY FAIRING "L" ANGLE NUTPLATE SUPPORT IS CRACKED....R&R L/H W/W FWD O/B CORNER CENTER BELLY FAIRING "L" ANGLE.

Part: CHANNEL — CRACKED (RT PYLON) · airframe 44,668 hrs · 27,609 cycles

R/H PYLON INSIDE ACCESS PANEL 424DB UPPER "U" CHANNEL SUPPORT STIFFNER, P07 X23061.50 IS CRACKED AT O/B END....R&R UPPER "U" CHANNEL IN R/H PYLON ACCESS PANEL 424DB.

Part: SUPPORT BRACKET — CRACKED (VERTICAL STAB) · airframe 44,668 hrs · 27,609 cycles

VERTICAL STAB RH SIDE VERT TOP, RH MOVABLE FAIRING 'L' ANGLE SUPPORT BRACKET IS CRACKED - R&R VERTICAL STAB RH SIDE VERY TOP "L" ANGLE BRACKET.

Part: ANGLE — CRACKED (FAIRING) · airframe 44,668 hrs · 27,609 cycles

L/H W/W FWD O/B CORNER CENTER BELLY FAIRING "L" ANGLE NUTPLATE SUPPORT IS CRACKED....R&R L/H W/W FWD O/B CORNER CENTER BELLY FAIRING "L" ANGLE.

Part: HINGE — CRACKED (TE FLAP) · airframe 44,668 hrs · 27,609 cycles

RH WING O/B FLAP SHROUD I/B AFT HINGE HALF IS CRACKED X2 PLACES - REMOVED HINGE, DRILLED UP NEW HINGE, INSTALLED PIN, SAFTIED, SCREWS NEED COUNTERSUNK AND SCREWS INSTALLED. COUNTERSUNK AND INSTALLED SCREWS AND NUTS.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 44,668 hrs · 27,609 cycles

FWD FUSELAGE BELLY HAS DENT AT FR 11 RH SIDE BETWEEN STR 13 & 14 RH - PERFORMED REPAIR ON THE RH FWD FUSELAGE AT FR 11 BETWEEN STR 13R & 14R.

Part: DOOR — CRACKED (EXTERNAL POWER) · airframe 44,668 hrs · 27,609 cycles

EXTERNAL POWER RECEPTACLE DOOR IS CRACKED AT LATCH CUTOUT - REMOVED AND REPLACED EXTERNAL POWER RECEPTACLE DOOR.

Part: SUPPORT — CRACKED (COCKPIT) · airframe 43,023 hrs · 26,333 cycles

COCKPIT CENTER POST GRAB HANDLE SUPPORT STRUCTURE HAS CRACK. MADE A CUT OUT OF THE DAMAGED AREA. REPAIRED GRAB HANDLE SUPPORT, STILL REQUIRES 2 NUT PLATES TO BE INSTALLED. INSTALLED 2 NUT PLATES ON GRAB HANDLE SUPPORT.

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 43,023 hrs · 26,333 cycles

CARGO DOOR Z ANGLE IS CORRODED. R&R CARGO DOOR Z ANGLE, REQUIRES SEALANT, PAINT & FILLER IN BOTTOM CORNERS. PAINTED, SEALED, APPLIED FILLER IN BOTTOM CORNERS & INSTALLED CARGO BAY DOOR PROTECTIVE PLATE.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 43,023 hrs · 26,333 cycles

AFT CARGO DOOR CUTOUT AT FR 65 & 68 LATERAL-L SHAPE HAVE CORROSION @ LOWER FWD & AFT CORNERS. R&R AFT FR 65 & 68 LATERAL-L SHAPE AT LOWER FWD & AFT CORNERS.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 42,885 hrs · 26,237 cycles

BURING SMELL IN COCKPIT (MX REPORTS SMELL OF CHLORINE). RAN HYD, PACKS, ELECTRICAL, PANELS WHILE IN FTL DECK. NO SMOKE OR BURING SMELL FOUND. CLEANER IS NOTED BY MULTIPLE MX. A/C OK FOR SERVICE.

Part: TRACK — DIRTY (WINDOW) · airframe 42,643 hrs · 26,044 cycles

CA DV WINDOW WILL NOT CLOSE. CLEANED DV WINDOW TRACK AND LUBRICATED OPS CHECK GOOD.

Part: SMOKE DETECTOR — FAULTY (AFT CARGO) · airframe 42,034 hrs · 25,591 cycles

BAGGAGE SMOKE DETECTION LIGHT ILLUMINATED WITHOUT AURAL WARNING INDICATION. R&R BAG SMOKE DETECTOR #2. OPS CHECK PERFORMED. OPS CHECK GOOD AT THIS TIME.

Part: ACM — FAULTY (AC BAY) · airframe 41,547 hrs · 25,202 cycles

SMOKE IN THE CABIN REPORTED BY FLIGHT ATTENDANT. PERFORMED FIM TASK, DETERMINED SMOKE WAS DUE TO FAULTY PACK II ACM. DEFERRED ON DISC BLOCK 1 LOG PG 352056.

Part: BALLAST — BURNED OUT (CABIN) · airframe 41,536 hrs · 14,192 cycles

SMOKE BURING SMELL IN CABIN. PERFORMED INSPECTION OF CABIN LIGHTS OK. RAN AIR CYCLE MACHINES OK. REMOVED AND REPLACE BALLAST FOR SEATS 9. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: FIRE DETECTOR — FAILED (NR 1 ENGINE) · airframe 41,379 hrs · 25,057 cycles

NR 1 ENGINE FIRE DETECTION SYS FAILED. R & R THE NR 1 ENGINE FIRE DETECTOR ASSY, OPS CHECKED GOOD. NO FURTHER DEFECTS FOUND.

Part: DOOR SEAL — OUT OF POSITION (CABIN DOOR)

TRIM/FOD HANGING OUT OF MAIN CABIN DOOR AREA AFTER DOOR WAS CLOSED. RESECURED LOOSE RUBBER TRIM SEAL FROM THE CABIN DOOR.

Part: SWITCH — LEAKING (APU) · airframe 40,124 hrs · 23,992 cycles

FUEL ODOR IN THE FLIGHT DECK DURING CLIMB OUT. DISSIPATED AFTER 10 MINUTES. INSPECTED AND FOUND FUEL LEAKING FROM APU PRESSURE SWITCH.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 BLEED) · airframe 40,099 hrs · 23,971 cycles

BLEED 2 LEAK EICAS IN ICING CONDITIONS. PERFORMED TROUBLESHOOTING CHECKS. NO FAULT FOUND.

Part: SENSE LINE — FAILED (BLEED SYS) · airframe 39,108 hrs · 23,097 cycles

BLEED 1 OVERTEMP IN FLIGHT DURING ICING CONDITIONS IN CLIMB. FOUND MULTIPLE HOLES IN SENSE LINE. REMOVED AND REPLACED THE NR 1 SENSE LINE. OPS CHECKED GOOD.

Part: THERMOSTAT — INTERMITTENT (NR 2) · airframe 39,107 hrs · 23,096 cycles

BLEED 1 OVERTEMP, IN AND OUT OF ICING CONDITIONS. R & R THE BLEED 1, NR 2 THERMOSTAT AND SWAPPED WITH THE NR 1 THERMOSTAT IAW AMM 36-11-06. OPS CHECKED GOOD.

Part: VALVE — INOPERATIVE (BLEEDS 1 & 2) · airframe 39,106 hrs · 23,095 cycles

BLEED 1 AND 2 OVERTEMP. R & R THE NR 1 FAN AIR VALVE IAW IAW AMM 36-11-03, REMOVED AND CLEANED THE NR 2 FAN AIR VALVE FILTER AND REINSTALLED IAW AMM 36-11-03. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 ANTI ICE) · airframe 38,836 hrs · 22,888 cycles

WING 2 ANTI-ICE FAULT ON EICAS. PERFORMED ENG RUN OPS CHECK OPS CHECK GOOD.

Part: CLAMP — LOOSE (NR 2 PACK) · airframe 38,761 hrs · 22,827 cycles

NR 2 BLEED LEAK ON EICAS. PERFORMED A CHECK OF THE BLEED AIR LINES, TIGHTENED TWO CLAMPS AT THE NR 2 PACK IAW AMM 36-11-10. NO FURTHER LEAKS NOTED. ACFT OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 2 BLEED) · airframe 38,671 hrs · 22,749 cycles

NR 2 BLEED LEAK IN ICING CONDITONS. PERFORMED AN OPS TEST OF ENGINE BLEED VALVES IAW AMM 36-11-05. NO FAULTS OR LEAKS FOUND. INSPECTED BLEED DUCTS IAW AMM 36-11-09, NO LEAKS FOUND AT THIS TIME.

Part: DUCT — LEAKING (NR 1 BLEED) · airframe 38,050 hrs · 22,226 cycles

NR 1 BLEED LEAK AFTER TAKE OFF. REMOVED AND REPLACED NR 1 BLEED DUCT IN AFT CARGO BAY UNDER FLOOR. OPS CHECKED GOOD

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 36,842 hrs · 21,215 cycles

MAIN PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE ADJUSTED UPPER AND LOWER MAIN DOOR ROLLERS, OPS CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (BLEED LEAK) · airframe 36,747 hrs · 21,135 cycles

BLEED 1 LEAK IN FLT. RAN AND LOOKED FOR BLEED LEAK NO LEAK DETECTED. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,637 hrs · 19,467 cycles

COCKPIT STEP EXIT IDENTIFIER NR 9 IS INOPERATIVE. MAINTENANCE REPLACED STEP LIGHT PLATE ASSY, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,637 hrs · 19,467 cycles

INTERIOR EMERGENCY LIGHT SIGN AT EXIT ROW IS INOPERATIVE. MAINTENANCE REPLACED BULB. OPS CHECKED GOOD. MAINTENANCE REPLACED NR 4 POWER SUPPLY, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,637 hrs · 19,467 cycles

LEFT FWD WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT NR 3 INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD. REPLACED NR 1 POWER SUPPLY, OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,510 hrs · 19,386 cycles

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

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,969 hrs · 19,031 cycles

DURING MX INSPECTION, THE LOWER SERVICE DOOR EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MX R & R THE SERVICE DOOR LOWER EMERGENCY EXIT IDENTIFIER SIGN WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,969 hrs · 19,031 cycles

DURING MX INSPECTION THE EMERGENCY EXIT LIGHT ABOVE THE SERVICE DOOR WOULD NOT ILLUMINATE. MAINTENANCE R & R THE NR 2 EMERGENCY LIGHT SYS INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DIRTY (SMOKE DETECTOR) · airframe 31,693 hrs · 17,567 cycles

THE CREW REPORTED A CARGO SMOKE INDICATION IN FLIGHT. LANDED WITHOUT INCIDENT, MAINTENANCE INSPECTED AND CLEANED FWD CARGO BAY SMOKE DETECTOR CONNECTOR, OPS TESTED WITH NO DEFECTS, AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (ZONE 600) · airframe 31,295 hrs · 17,334 cycles

ACFT AND TOWER REPORTED THICK WHITE SMOKE FROM NR 2 ENGINE DURING TAKEOFF ROLL. SYSTEMS MONITORED INFLIGHT, NO E2 ABNORMAL PARAMETERS NOTED. MX PERFORMED NR 2 ENGINE HIGH POWER RUNS FOR 20 MINUTES WITHOUT LEAKS OR SMOKE NOTED. FOUND SIGN OF FUEL LEAKING FROM NR 2 WING T/E. R & R NR 2 WING FLAPPER VALVE WITH LEAK CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 28,286 hrs · 15,397 cycles

THE CREW REPORTED SMOKE IN COCKPIT AND CABIN DURING CLIMBOUT. RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND REPLACED THE NR 1 ENGINE. OPS CHECKED GOOD.

Part: SKIN — CORRODED (ZONE 100) · airframe 27,869 hrs · 15,112 cycles

FWD LOWER COCKPIT SKIN HAS AREAS OF CORROSION FR 12-13, STR 21R-21L. REPAIRED SKIN IAW EC5310-01625. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (ZONE 700) · airframe 25,945 hrs · 13,921 cycles

AFTER TAKEOFF THE CREW NOTED THAT THE NLG DOORS DID NOT CLOSE AFTER THE GEAR WAS RETRACTED. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. WHERE MX REPLACED THE NLG UPLOCK BOX PROXIMITY SWITCH, PERFORMED OPS TESTS AND CLEARED THE DISCREPANCY.

Part: GROUND STUD — LOOSE (CABIN) · airframe 23,408 hrs · 12,431 cycles

RIC - DURING ROUTINE MAINTENANCE, MX FOUND GALLEY CEILING EMERGENCY LIGHT, GALLEY DOOR LOWER EXIT SIGN, 12C LOWER EXIT SIGN AND COCKPIT STOP SIGN INOPERATIVE. RIC MX TIGHTENED LOOSE GROUND STUD G58506 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,137 hrs · 12,282 cycles

SHV - DURING C-CHECK CORROSION AT NUT PLATED AREA FRAME 65 STRIKER PLATE. MAINTENANCE REPAIRED FRAME 65 AT STRIKER PLATE IAW EC5310-01505. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (RT MLG) · airframe 21,744 hrs · 11,524 cycles

IAH - FLIGHT 2508, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER RETRACTION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR PROXIMITY SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — DEFECTIVE (NLG) · airframe 21,351 hrs · 11,302 cycles

IAH - FLIGHT 2278, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOWN LOCK PROXIMITY SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — FAULTY (EMERGENCY LIGHTS) · airframe 18,898 hrs · 9,976 cycles

DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN OVER THE FLIGHT ATTENDANTS SEAT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 18,385 hrs · 9,699 cycles

IAH - FLIGHT 2736, DURING PREFLIGHT INSPECTION THE CREW REPORTED A STRONG ELECTRICAL SMELL FROM THE LAVATORY. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LAVATORY LIGHT BALLAST. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — WORN (AILERON) · airframe 18,288 hrs · 19,643 cycles

SHV - DURING C-CHECK RT PCA TO AILERON I/B ROD O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT AILERON TO PCA ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — WORN (AILERON) · airframe 18,288 hrs · 19,643 cycles

SHV - DURING C-CHECK RT PCA TO AILERON I/B ROD I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — WORN (AILERON) · airframe 18,288 hrs · 19,643 cycles

SHV - DURING C-CHECK LT PCA TO AILERON ATTACHMENT HAS MIGRATED BUSHING. MAINTENANCE REMOVED AND REPLACED LT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 19,643 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAD CORROSION AT CROSSBEAM BETWEEN FRAME 48-49. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT CROSSBEAM FRAME 48-49 IAW IC2009-145/02742. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — WORN (RT AILERON) · airframe 18,288 hrs · 19,643 cycles

SHV - DURING C-CHECK RT AILERON TO PCA BRACKET MOST I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT AILERON TO PCA ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — MIGRATED (AILERON) · airframe 18,288 hrs · 19,643 cycles

SHC - DURING C-CHECK RT PCA TO AILERON O/B ROD O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,288 hrs · 19,643 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CROSSBEAM BETWEEN FRAMES 48-49. MAINTENANCE REPAIRED LT OMEGA BEAM AT CROSSBEAM BETWEEN FRAME 48-49 IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — GOUGED (LT AILERON) · airframe 18,288 hrs · 19,643 cycles

SHV - DURING C-CHECK LT AILERON PCA ATTACH POINT BRACKET O/B ROD ATTACHMENT I/B AND O/B HAT BUSHING HOUSINGS ARE GOUGED. MAINTENANCE REMOVED AND REPLACED LT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — GOUGED (RT AILERON) · airframe 18,288 hrs · 19,643 cycles

SHV - DURING C-CHECK BRACKET ON THE RT AILERON THAT GOES TO THE PCA IS GOUGED. MAINTENANCE REMOVED AND REPLACED RT PCA TO AILERON ATTACHMENT BRACKET IAW EMB-145 SRM 51-40-02 AND EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · airframe 18,288 hrs · 19,643 cycles

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

Part: BRACKET — WORN (LT AILERON) · airframe 18,288 hrs · 19,643 cycles

SHV - DURING C-CHECK LT AILERON DAMPNER BRACKET I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED LT AILERON DAMPNER BRACKET IAW SRM 51-40-02. MAINTENANCE PREPPED, PRIMED AND PAINTED LT AILERON DAMPNER BRACKET IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COWLING — CRACKED (APU) · airframe 18,217 hrs · 9,606 cycles

DENT JUST BELOW APU AIR INLET ON TAIL CONE. THE APU WAS DEACTIVATED AND CONSIDERED INOPERATIVE FOR TRIP TO SHV. UPON ARRIVING IN SHV MAINTENANCE REMOVED AND INSTALLED A NEW APU TAIL CONE IAW AMM 49-15-00. THE APU WAS REACTIVATED IAW AMM 49-13-00. OPS CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 18,015 hrs · 9,502 cycles

IAH - FLIGHT 2050, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE INTERIOR LEFT EMERGENCY EXIT SIGN AT THE WING WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 15,649 hrs · 8,250 cycles

CLE FLIGHT 2879 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL WHEN GEAR WAS SELECTED DOWN. MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE GEAR DOOR ACTUATOR. OPERATIONAL CHECKS WERE GOOD.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 12,069 hrs · 6,401 cycles

IAH - FLIGHT 2271 - THE CREW REPORTED, RECEIVED A LANDING GEAR AIR GROUND FAILED EICAS MESSAGE WHEN THE GEAR WAS SELECTED DOWN, AND CLEARED WHEN GEAR EXTENDS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — CORRODED (FUSELAGE) · airframe 13,730 hrs · 7,278 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 193 AAB WITH BAD BONDING PLATES. MAINTENANCE REPAIRED PANEL 193 AAB IAW EMB 145 EC 5750-01315. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — CORRODED (FUSELAGE) · airframe 13,730 hrs · 7,278 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197 DR HAS CORRODED BONDING PLATES. MAINTENANCE REPAIRED PANEL 197 DR IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — CORRODED (FUSELAGE) · airframe 13,730 hrs · 7,278 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197CL HAS CORRODED BONDING PLATES. MAINTENANCE REPAIRED PANEL 197CL IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (CARGO BAY) · airframe 13,730 hrs · 7,278 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND SHEAR CLIP AT FRAME 65 & CARGO DOOR CUTOUT LOWER BEAM WITH CORROSION. MAINTENANCE REPAIRED SHEAR CLIP AT FRAME 65 IAW EC 5330-01458 & REMOVED AND REPLACED CARGO DOOR CUTOUT SILL IAW EMB 145XR SRM 51-40-00. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — CORRODED (AILERONS) · airframe 13,730 hrs · 7,278 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND RIGHT TOP AILERON SHROUD WITH CORROSION AT BONDING PLATES. MAINTENANCE REPAIRED RIGHT TOP AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — CORRODED (AILERON) · airframe 13,730 hrs · 7,278 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND RIGHT LOWER AILERON SHROUD WITH CORROSION AT BONDING PLATES. MAINTENANCE REPAIRED RIGHT LOWER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — CORRODED (LT AILERON) · airframe 13,730 hrs · 7,278 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND LT AILERON UPPER SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED LEFT AILERON UPPER SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — CORRODED (FUSELAGE) · airframe 13,730 hrs · 7,278 cycles

SHV - DURING C-CHECK MAINTENANCE FOUND PANEL 197 AB HAS CORRODED BONDING PLATES. MAINTENANCE REPAIRED PANEL 197 AB IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 12,804 hrs · 6,802 cycles

FLT 2761 - EWR - CREW REPORTED FLUORESCENT STRIP IN GALLEY AREA MISSING. EWR MX INSTALLED EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 9,034 hrs · 4,781 cycles

LEFT OMEGA BEAM CORRORED AT RAMP ANGLE CARBON BEAM. REMOVED CORRODED AREA, FABRICATED DOUBLER, DRILLED, COUNTERSUNK, INSTALLED, ALODINED, PRIMED AND PAINTED IAW EMB 145XR SRM 53-00-10. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 8,630 hrs · 4,564 cycles

TYS - A DENT JUST FWD OF SKIN SPLICE BETWEEN FR 23 AND 24 AND STR 18R AND 19R WAS FOUND. MAINTENANCE PERFORMED A REPAIR TO THE DAMAGE SKIN IAW IC2005-145/7374, ALODINED, PRIMED AND PAINTED IAW CPM 51-21-07. LEAK CHECK WAS GOOD. AIRCRAFT WAS RELEASED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 7,212 hrs · 3,797 cycles

DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ON OVERHEAD PANEL IS INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER FOR THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,745 hrs · 2,497 cycles

DURING A SCHEDULED 1C INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE CORRODED AREA WAS SUBSEQUENTLY REMOVED AND A FILLER AND DOUBLER WAS INSTALLED IAW THE EMB SRM. ACFT WAS RELEASED FOLLOWING COMPLETION OF THE 1C INSPECTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,745 hrs · 2,497 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON SEAT TRACK LF1 AT THE MOST FORWARD END. MAINTENANCE REMOVED AND REPLACED SEAT TRACK LF1 IAW MM 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,745 hrs · 2,497 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CABIN TO GALLEY STEP-UP PLATE. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (GALLEY FLOOR) · corrosion level 2 · airframe 4,745 hrs · 2,497 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD DIGITAL JUST AFT OF THE COCKPIT DOOR STEP. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,745 hrs · 2,497 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT GUSSET AT FRAME 15. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,745 hrs · 2,497 cycles

DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM TOPCAP AT FRAME 22. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: LIGHT — BROKEN (CABIN)

EWR---CO2205, CREW REPORTED, (EMERGENCY LIGHTING STRIP BY MAIN CABIN DOOR MISSING AND GALLEY STRIP IS BROKEN). MAINTENANCE REPLACED MISSING EMERGENCY LIGHT FLOOR STRIP AND BROKEN EMERGENCY LIGHT FLOOR STRIP. IAW EMB145 MM NR 33-50-12, OPS. CHECKED EMERGENCY LIGHTING GOOD.