N16149

Part: PUMP — FAILED (HYD SYS) · airframe 49,696 hrs · 32,649 cycles

HYD SYS 1 FAIL, E1 HYD PUMP FAIL EICAS MESSAGES AND HYD 1 QTY 0 IN CRUISE. REMOVED AND REPLACED #1 ENGINE DRIVE HYDRAULIC PUMP. FOUND AFT DPI TO NOT BE SEATED ON MANIFOLD DUE TO BACKUP RING INSTALLED INCORRECTLY REMOVED AND REPLACED AFT DPI WITH NEW ORINGS AND BACKUP RING VERIFIED OTHER TWO DPIS WERE INSTALLED CORRECTLY. SERVICED #1 HYD SYSTEM TO FULL. COMPLETED DPI INSTALL. LEAK/OPS CHECK SAT. COMPLETED #1 EDHP INSTALL. OPS/LEAK CHECK SAT. REMOVED AND REPLACED #1 HYD PUMP FILTERS. NO CONTAMINATION NOTED. OPS AND LEAK CHECK SAT.

Part: CHANNEL — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

CFII, LH OMEGA BEAM INBD VERTICAL FLANGE FOUND CRACKED AT FR33. REPAIR DOUBLER ON CFII, LH OMEGA BEAM, ON INBD VERTICAL FLANGE AT FR33

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 49,667 hrs · 32,625 cycles

LH THRUST REVERSER EXTERNAL SKIN OUTBD SIDE IS CRACKED NEAR THE UPPER DOOR. LH THRUST REVERSER EXTERNAL SKIN OUTBD SIDE UPPER DOOR PAINT REMOVED FOR INSPECTION. LH THRUST REVERSER EXTERNAL SKIN OUTBD SIDE NEAR THE UPPER DOOR SKIN REPAIRED.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

RFI EXT, SKIN UNDER ANTENNA BTW FR 70-68 AND STR 21R-21L FOUND CORRODED. REPAIR DOUBLER ON RFI LOWER SKIN, BTW FR 68-69 AND BTW 21L-21R

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

RFI, FWD RADIO ALTEMETER ANTENNA DOUBLER BTW FR 65-66 AND STR 21R-21L FOUND CORRODED. RF1, ANTENNA DOUBLER BTW FR 65-66 AND STR 21L-21R BLENDED AND FOUND OUT OF LIMIT. RF1, FWD RADIO ALTIMETER ANTENNA DOUBLER BTW FR 65-66 AND STR 21R-21L REPLACED.

Part: SKIN — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

AT REAR FUSE, CRACK FOUND ON LH TOP SKIN AT FR 75 BTW STR 2L-3L. REPAIR DOUBLER ON LH REAR FUSE I UPPER SKIN, AT FR 75 AND AT STR 2L

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

SERVICE DOOR FWD SILL BTW FR 18-20 FOUND CORRODED. AT CFI, SERVICE DOOR FWD SILL BTW FR 18-20 SILL CORRODED OUT OF LIMIT. CFI, SERVICE DOOR FWD SILL BTW FR 18-20 REPLACED.

Part: FLOOR SUPPORT — CRACKED (CRACKED) · airframe 49,667 hrs · 32,625 cycles

LH OMEGA BEAM INBD VERTICAL FLANGE FOUND CRACKED AT FR25. REPAIR DOUBLER ON CFII, LT OMEGA BEAM, ON INBD VERTICAL FLANGE AT FR 25

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

CFI, LH OMEGA BEAM INBD VERTICAL FLANGE FOUND CRACKED AT FR22. REPAIR DOUBLER ON CFI, LH OMEGA BEAM, ON INBD VERICAL FLANGE AT FR 22

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

CFII, LH OMEGA BEAM INBD VERTICAL FLANGE FOUND CRACKED AT FR 26. REPAIR DOUBLER ON CFII, LH OMEGA BEAM, ON INBD VERTICAL FLANGE AT FR26

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

CFII, LH OMEGA BEAM INBD VERTICAL FLANGE FOUND CRACKED AT FR34. REPAIR DOUBLER ON CFII, LH OMEGA BEAM, ON INBD VERTICAL FLANGE AT FR34

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

RH OMEGA BEAM #1 FOUND CORRODED BTW FR 18-19. AT RH OMEGA BEAM #1 BTW FR 18-20 OMEGA BEAM CORRODED OUT OF LIMIT. RH OMEGA BEAM #1 BTW FR 18-20 REPAIRED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

CFI, LH OMEGA BEAM INBD VERTICAL FLANGE FOUND CRACKED AT FR21. REPAIR DOUBLER ON CFI, LH OMEGA BEAM, ON INBD VERICAL FLANGE AT FR 21.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

CFII, LH OMEGA BEAM INBD VERTICAL FLANGE FOUND CRACKED AT FR31. REPAIR DOUBLER ON CFII, LH OMEGA BEAM, ON INBD VERTICAL FLANGE AT FR31

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

RF1, CARGO ENTRANCE L-FRAME 68 BTW STR 17L-18L FOUND CORRODED. RF1, CARGO ENTRANCE L-FRAME 68 BTW STR 17L-18L BLENDED. RF1 CARGO ENTRANCE L-FRAME 68 BTW STR 15L-16L CUTOUT WAS DONE. RF1 CARGO ENTRANCE L-FRAME 68 BTW STR 17L-18L REPAIRED.

Part: FRAME — CRACKED (ZONE 100) · airframe 49,667 hrs · 32,625 cycles

CF2, BTW STR 15R-16R, RH FRAME 25 FOUND CRACKED. FRAME REPAIRED. U CHANNEL AND REPAIR SPLICE FABRICATED WITH AN ALTERNATE MATERIAL.

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CTR CROSSBEAM AT FR20 FOUND CORRODED. MADE REPAIR PART FABRICATED

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

FR 59 FOUND CORRODED BTW STR 21L-20L. CFIV, FR 59 BTW STR 21L-20L BLENDED FOUND OUT OF LIMIT. CF4, FR59 BTW STR 21L-20L CUTOUT PERFORMED AND REPAIR PARTS PREDRILLED. CF4, FR59 LOWER SECTION BTW STR 20R-20L REPAIR PART PARTIALLY INSTALLED. CF4, FR59 BTW STR 21R-20L CORROSION REPAIRED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFII, LH SILL #3 BTW FR 29-36 FOUND CORRODED. CFII, LH SILL #2 BTW FR 29-36 BLENDED AND FOUND OUT OF LIMIT. CFII, LH SILL #3 BTW FR 29-36 REMVOED AND REPLACED WITH NEW.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

CFIV, SHEAR CLIP AT FR58 BTW STR 15L-16L FOUND CRACKED. CFIV, SHEAR CLIP AT FR58 BTW STR 15L-16L REMOVED AND REPLACED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

CFIII, RH GUSSET BTW FR 35-39 FOUND CRACKED. CFIII, RH GUSSET BTW FR 35-39 REMOVED AND REPLACED.

Part: HINGE — CRACKED (ZONE 100) · airframe 49,667 hrs · 32,625 cycles

HINGE ON TOILET WASTE ACCESS DOOR BTW FR 60-61 AND BTW STR 18R-20R FOUND CRACKED. CF4, ON TOILET WASTE ACCESS DOOR BTW FR 60-61 AND BTW STR 18R-20R HINGE REPLACED.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFI, LH SILL BTW FR 18-24 FOUND CORRODED. AT CF1, LH SILL BTW FR 18-24 SILL FOUND CORRODED OUT OF LIMITS. SILL REMOVED AND NEW SILL INSTALLED

Part: RIB — CRACKED (ZONE 500) · airframe 49,667 hrs · 32,625 cycles

AT RT WING TO FUSELAGE WHEEL WELL, AFT RIB CRACKED. AT RH WING TO FUSELAGE WHEEL WELL AFT RIB REMOVED AND INSTALLED.

Part: SUPPORT — CORRODED (WASTE VALVE) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CF4, CORROSION FOUND ON TOILET WASTE VALVE SUPPORT BTW FR 60-61 AND BTW STR 18R-20R. CF4, ON TOILET WASTE CUP BTW FR 60-61 AND BTW STR 18R-20R IS OUT OF LIMIT. TOILET CUP REMOVED AND INSTALLED.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 49,667 hrs · 32,625 cycles

CF2, AT FR 25 BTW STR 16R-17R SHEAR CLIP FOUND CRACKED. CF2, AT FR 25 BTW STR 16R-17R SHEAR CLIP REMOVED AND REPLACED

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 49,667 hrs · 32,625 cycles

RFI, CARGO ENTRANCE AREA, SUPPORT ANGLE UNDER T-POST AT FR67 FOUND CRACKED. RFI, CARGO ENTRANCE AREA, SUPPORT ANGLE UNDER T-POST AT FR67 REMOVED AND REPLACED.

Part: ANGLE — CRACKED (ZONE 100) · airframe 49,667 hrs · 32,625 cycles

RF1, CARGO ENTRANCE ON AFT FR 68 BTW 17L-18L LOWER ANGLE FOUND CRACKED. RF1, CARGO ENTRANCE ON AFT FR68 BTW STR 17L-18L LOWER ANGLE REMOVED AND REPLACED.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 49,667 hrs · 32,625 cycles

RFI, CARGO ENTRANCE AREA, SUPPORT ANGLE UNDER T-POST AT FR66 FOUND CRACKED. RFI, CARGO ENTRANCE AREA, SUPPORT ANGLE UNDER T-POST AT FR66 REMOVED AND REPLACED.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

RFI, CARGO ENTRANCE CHANNEL BTW FR 65-68 FOUND CORRODED. RFI, CARGO ENTRANCE CHANNEL BTW FR 65-68 IS OUT OF LIMIT. RFI, CARGO ENTRANCE CHANNEL BTW FR 65-68 REPLACED

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

ENTRANCE CARGO L-FRAME 65 BTW STR 17L-19L FOUND CORRODED. RF1, ENTRANCE CARGO L-FRAME 65 BTW STR 17L-19L OUT OF LIMIT. RF1, ENTRANCE CARGO L-FRAME 65 BTW STR 15L-16L CUTOUT WAS DONE. RF1 ENTRANCE CARGO L-FRAME 65 CORROSION BTW STR 17L-19L REPAIRED.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFI, RH GUSSET BTW FR18-24 FOUND CORRODED. AT CF RH GUSSET BTW FR18-24 GUSSET BLENDED OUT OF LIMIT. CF1, RH GUSSET BTW FR 18-24 REMOVED AND INSTALLED.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFI, SERVICE DOOR AFT SILL BTW FR 22-24 FOUND CORRODED. AT CF1, SERVICE DOOR AFT SILL BTW FR 22-24 SILL BLENDED OUT OF LIMIT. CFI, SERVICE DOOR AFT SILL BTW FR 22-24 REPLACED

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFII, RH SILL #2 BTW FR 29-36 FOUND CORRODED. CFII, RH SILL #2 BTW FR 29-36 FOUND OUT OF LIMIT. CFII, RH SILL #2 BTW FR 29-36 REPLACED.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 49,667 hrs · 32,625 cycles

CFI, SHEAR CLIP AT FR16 BTW STR 15R-16R FOUND CRACKED. AT CF1 FR16 BTW STR 15R-16R SHEAR CLIP REMOVED AND NEW SHEAR CLIP INSTALLED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

CF1, SHEAR CLIP AT FR15 BTW STR 15R-16R FOUND CRACKED. AT CF1 AT FR15 BTW STR 15R-16R SHEAR CLIP REMOVED AND NEW SHEAR CLIP INSTALLED.

Part: PRECOOLER — NO TEST (LT ENGINE) · airframe 49,667 hrs · 32,625 cycles

LH ENG BLEED AIR PRECOOLER FAILED PRESSURE TEST. LH PRECOOLER REMOVED AND REPLACED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

CFI, ON CENTER OMEGA BEAM, SUPPORT ANGLE BTW FR 18-20 FOUND CRACKED. AT CF1, ON CENTER OMEGA BEAM SUPPORT ANGLE BTW FR 18-20 REMOVED AND INSTALLED.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFII, RT SILL NR 1 BTW FR 23-30 FOUND CORRODED. CFII, RT SILL NR 1 BTW FR 23-30 BLENDED, FOUND OUT OF LIMIT AND REMOVED FOR REPLACEMENT. CFII, RT SILL NR 1 BTW FR 23-30 IS REPLACED.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 49,667 hrs · 32,625 cycles

CFII, SHEAR CLIP AT FR27 BTW STR 15R-16R FOUND CRACKED. CFII AT FR27 BTW STR 15R-16R SHEAR CLIP REMOVED FOR REPLACEMENT. CFII AT FR27 BTW STR 15R-16R SHEAR CLIP REPLACED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

CFII, SHEAR CLIP AT FR26 BTW STR 15R-16R FOUND CRACKED. CFII AT FR26 BTW STR 15R-16R SHEAR CLIP REMOVED FOR REPLACEMENT. CFII AT FR26 BTW STR 15R-16R SHEAR CLIP REPLACED

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 49,667 hrs · 32,625 cycles

CFII, SHEAR CLIP AT FR25 BTW FR 15R-16R FOUND CRACKED. CFII AT FR 25 BTW STR 15R-16R SHEAR CLIP REMOVED AND REPLACED.

Part: FUEL TANK — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

SURFACE CORROSION ON VENTRAL FUEL TANK EXTERNAL FWD FACE AROUND FUEL VENT TUBE BRACKET. AFTER INVESTIGATION, NO CORROSION FOUND ON BRACKET, ONLY ON RIB I OF VENTRAL TANK. SURFACE BLENDED AND FOUND OUT OF LIMIT. VENTRAL TANK ON RIB I CUT OUT PERFORMED. VENTRAL FUEL TANK RIB I, REPAIR DOUBLER, FILLER AND SHIM FABIRCATED. VENTRAL FUEL TANK RIB I, REPAIRED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,667 hrs · 32,625 cycles

CFII, SHEAR CLIP AT FR24 BTW STR 15R-16R FOUND CRACKED. CFII AT FR24 BTW STR 15R-16R SHEAR CLIP REMOVED FOR REPLACEMENT. CFII AT FR24 BTW STR 15R-16R SHEAR CLIP REPLACED

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFI, SERVICE DOOR CUT OUT, LOWER CHANNEL BTW FR 20-22 FOUND CORRODED. AT CF1 SERVICE DOOR CUT OUT, LOWER CHANNEL BTW FR 20-22, CHANNEL CORRODED OUT OF LIMIT. CF1 SERVICE DOOR CUT OUT LOWER CHANNEL BTW FR 20-22 REMOVED AND REPLACED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFIII, LH SILL BTW FR 41-48 FOUND CORRODED. CF3, LH SILL BTW FR 41-48 FOUND OUT OF LIMITS. CF3, LH SILL BTW FR 41-48 REMOVED AND REPLACED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFIII, LH SILL BTW FR 35-42 FOUND CORRODED. CF3, LH SILL BTW FR 35-42 FOUND OUT OF LIMITS. CF3, LH SILL BTW FR 35-42 REMOVED AND REPLACED.

Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

RIGHT DIGITAL AT FR22 FOUND CORRODED. AT CF1, RT DIGITAL AT FR22 DOUBLER BLENDED OUT OF LIMIT. AT CF1, RT DIGITAL AT FR22 DIGITAL REMOVED AND INSTALLED.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

RF1, AFT RADIO ALTEMETER ANTENNA INTERNAL RETAINER BTW FR 68-70 FOUND CORRODED. RFI, AFT RADIO ALTIMETER ANTENNA, INTERNAL RETIANER BTW FR 68-70 BLENDED AND FOUND OF LIMIT. REMOVED AND INSTALLED

Part: GUSSET — CORRODED · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFIII, LH GUSSET BTW FR 45-53 FOUND CORRODED. CF3, LH GUSSET BTW FR 45-53 FOUND OUT OF LIMITS. CF3, LH GUSSET BTW FR 45-53 REMOVED AND REPLACED WITH NEW

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFIV, RH STEP ANGLE AT FR59 FOUND CORRODED. CFIV, RH STEP ANGLE AT FR59 BLENDED AND FOUND OUT OF LIMITS. CFIV, RH STEP ANGLE AT FR59 REPLACED

Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CF1, RH DIGITAL AT FR20 FOUND CORRODED. AT CF1 RH DIGITAL AT FR 20 DIGITAL CORRODED OUT OF LIMIT. AT CF1 RH DIGITAL AT FR DIGITAL REMOVED AND INSTALLED.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFIV, RH SILL BTW FR 59-60A FOUND CORRODED. CFIV, RH SILL BTW FR 59-60A BLENDED AND FOUND OUT OF LIMIT. AT CFIV RH BTW FR 59-60A STILL REMOVED AND REPLACED

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

RIGHT GUSSET IN TOILET AREA BTW FR 59-61 FOUND CORRODED. CFIV, RH GUSSET IN TOILET AREA BTW FR 59-61 BLENDED AND FOUND OUT OF LIMIT. CFIV, RH GUSSET IN TOILET AREA BTW FR 61-59 REMOVED AND REPLACED.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFIII, LT GUSSET BTW FR 35-39 FOUND CORRODED. CF3, LT GUSSET BTW FR 35-39 FOUND OUT OF LIMITS. CFIII, LT GUSSET BTW FR 35-39 REPLACED.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

RFI EXT RADIO ALTEMETER ANTENNA DOUBLER BTW FR 68-70 AND STR 21L-21R FOUND CORRODED. RF1 EXT BTW FR 68-70 AND STR 21L-21R DOUBLER BLENDED AND FOUND OUT OF LIMIT AND REMOVED AND REPLACED

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

LEFT SILL NR 2 BTW FR 23-30 FOUND CORRODED. LT SILL NR 2 BTW FR 23-30 BLENDED AND FOUND OUT OF LIMITS. LT SILL NR 2 BTW FR 23-30 REPLACED.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFIII, RH SILL BTW FR 41-48 FOUND CORRODED. CF3, RH SILL BTW FR41-48 FOUND OUT OF LIMITS. CFIII, RH SILL BTW FR 41-48 REPLACED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,667 hrs · 32,625 cycles

CFIII, RH SILL BTW FR 36-42 FOUND CORRODED. CF3, RH SILL BTW FR 36-42 FOUND OUT OF LIMITS. CF3, RH SILL BTW FR 36-42 REMOVED AND REPLACED.

Part: DOOR — LACK OF LUBE (ZONE 800) · airframe 49,488 hrs · 32,455 cycles

MCD HARD TO OPEN. LUBRICATED MCD. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 49,164 hrs · 32,152 cycles

EMERGENCY LIGHT UNDER FLIGHT DECK DOOR INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 49,125 hrs · 32,119 cycles

LH AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH AFT EXTERIOR EMERGENCY LIGHT. OPS CHECK SAT.

Part: STOP FITTING — FAULTED (ZONE 800) · airframe 48,471 hrs · 31,488 cycles

MCD WILL NOT CLOSE. REMOVED AND REPLACED AFT UPPER STOP SEAT. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 48,109 hrs · 31,112 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT BULB. OPS CHECK SAT.

Part: DOOR — UNKNOWN (ZONE 800) · airframe 48,072 hrs · 31,075 cycles

MAIN CABIN DOOR JAMMED. OPS CHECK PAX DOOR. OPS CHECK GOOD. NO DEFECTS NOTED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,233 hrs · 30,293 cycles

LH OVERWING EMERGENCY LIGHT OUT. REMOVED AND REPLACED BULB. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,167 hrs · 30,235 cycles

MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EMERGENCY LIGHT BULB. OPS CHECK GOOD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,515 hrs · 29,623 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. LUBRICATED MAIN CABIN DOOR. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,344 hrs · 29,464 cycles

TOP OF MAIN CABIN DOOR IS NOT CLOSED FLUSH AT EXTERIOR. PERFORMED MCD TO FUSELAGE SKIN STEP MEASUREMENTS AND FOUND POINT 12 OUT OF LIMITS BY APPROX. NO OTHER DEFECTS FOUND. COMPLETED GVI OF TOP OF MCD AND MEASURED POINT 12. NO DEFECTS NOTED ALSO, COMPLETED PRESSURIZATION FOR MCD LEAK CHECK. NO DEFECTS NTOED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,315 hrs · 29,438 cycles

MAIN CABIN DOOR WON'T OPEN. ADJUSTED MAIN CABIN DOOR TRIM ON UPPER FWD SIDE.

Part: BATTERY PACK — INOPERATIVE · airframe 46,144 hrs · 29,282 cycles

EMERGENCY LIGHTS NOT STAYING LIT FOR PROPER AMOUNT OF TIME. REMOVED AND REPLACED BP3. ALL OPS CHECK COMPLETED. NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE · airframe 46,144 hrs · 29,282 cycles

EMERGENCY LIGHT BATTERY POS 4 TESTED INOPERATIVE. REPLACE EMERGENCY LIGHT BATTERY POS 4. OPS CHECK SAT. NO FURTHER DEFECTS NOTED.

Part: SWITCH — PILOT ERROR (FUEL SYSTEM) · airframe 45,256 hrs · 28,494 cycles

WING 1 FUEL QTY INDICATED 0 IN FLIGHT. FOUND REFUEL SWITCH IN OPEN POSITION. MOVED TO CLOSED POSITION. ALL MESSAGES CLEARED AND FUEL TY RETURNED TO NORMAL. VERIFIED QTY INDICATION CORRECT BY STICK MEASUREMENT. OPS CHECK GOOD

Part: NONE — NONE · airframe 45,009 hrs · 28,270 cycles

EMERGENCY LIGHTS WERE LEFT ON. ALL EMG LT BATTERIES DRAINED". R&R ALL 4 EMERGENCY BATTERIES. OPS CK GOOD #1 - PN ABS-2013-1A SN 41687 TSN 3856.43 CSN 3496 #2 - PN 2013-1ASMI SN 9609 TSN 6705.44 CSN 5255 #3 - PN 2013-1ASMI SN 13318 TSN 1271.30 CSN 1155 #4 - PN ABS-2013-1A SN 50054 TSN 4125.34 CSN 3683

Part: NONE — NONE · corrosion level 2 · airframe 44,048 hrs · 28,128 cycles

LAV/CARGO LATERAL FLOOR SUPPORT FR61-66 STR 15R CORROSION. REMOVED AND REPLACED LATERAL FLOOR SUPPORT AT STR15R FROM FR61-66

Part: NONE — NONE · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

LAV/CARGO PARTITION DOUBLER POSSIBLE CORROSION FR61 STR15L. REMOVED AND REPLACED LAV/CARGO PARTITION DOUBLER FR61 STR 15L

Part: NONE — NONE · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

CABIN LATERAL FLOOR SUPPORT BETWEEN FRAMES 48-52 AT STRINGER 15L HAS SIGNS OF CORROSION. CUT-OUT FLOOR SILL DAMAGE SECTION AT STR 15L BETWEEN FRAME 49+10 -52. FABRICATED NEW SECTION AND INSTALL AT LH FLOOR SILL STR 15L BETWEEN FRAME 49+10-52

Part: NONE — NONE · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

RH WING FLEX SHAFTS 1-4 HAVE CORROSION ON FITTINGS UNDER HEAT SHRINK. REMOVED AND REPLACED FLAP FLEX SHAFTS ON RIGHT WING

Part: NONE — NONE · airframe 44,676 hrs · 27,959 cycles

COCKPIT CEILING RH A/O FRAME CRACKED. REMOVED AND REPLACED FRAME AT COCKPIT CEILING RH A/O FRAME

Part: NONE — NONE · airframe 44,676 hrs · 27,959 cycles

DENT LOCATED ON PASS DOOR AT 7" FROM LOWER EDGE AND ON AFT EDGE. FABRICATED AND IND INSTALLED REPAIR DOUBLER AND REPAIR FILLER AT PASS DOOR AT 7" FROM LOWER AFT SIDE.

Part: NONE — NONE · airframe 44,676 hrs · 27,959 cycles

LT WING FLAP FLEX SHAFTS #1, #2, #4 DAMAGED FERRULES. REMOVED AND REPLACED LEFT WING FLAP FLEX SHAFTS SECTIONS 1, 2, AND 4.

Part: NONE — NONE · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

SIGNS OF CORROSION AT RH SERVICE DOOR AT STRINGER 16 FRM ST20 AND 22 LWR FWD AND AFT CORNERS. REMOVED AND REPLACED SILL AT SERVICE DOOR AT STR 16 FR 20 AND 22

Part: NONE — NONE · airframe 44,676 hrs · 27,959 cycles

RT WING AILERON ON AILERON DAMPER HINGE GOUGED. REMOVED AND REPLACED RT WING AILERON DAMPER HINGE.

Part: NONE — NONE · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

CABIN LATERAL FLOOR SUPPORT BETWEEN FRAMES 48-52 AT STRINGER 15R HAS SIGNS OF CORROSION. REMOVED AND REPLACED CABIN LATERAL FLOOR SUPPORT BETWEEN FRAMES 48-52 STRINGER 15R

Part: NONE — NONE · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

PASSENGER DOOR FRAME HAS SIGNS OF CORROSION UNDER THRESHOLD FR15-FR18. REMOVED AND REPLACED SHAPE Y

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

MIDDLE LATERAL FLOOR SUPPORT BETWEEN FRAMES 16-18 IN FWD WET AREA HAS SIGNS OF CORROSION. REMOVED AND REPLACED MIDDLE LATERAL FLOOR SUPPORT BETWEEN FRAMES 16-18 FWD WET AREA.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

LAV/CARGO LATERAL FLOOR SUPPORT FR 59-61+4 BUT LINE 0 CORROSION. REMOVED AND REPLACED LAV/CARGO LATERAL FLOOR SUPPORT FR 59-61+4 BUT LINE 0

Part: NONE — NONE · airframe 44,676 hrs · 27,959 cycles

DENT LOCATED ON BAGGAGE DOOR AT 2.25 FROM UPPER EDGE AND 11.5 FROM AFT EDGE. DRESS BACK DENT LOCATED ON BAGGAGE DOOR AT 2.25 FROM UPPER EDGE AND 11.5 FROM AFT EDGE AND PERFORMED NDT

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

LAV/CARGO LATERAL FLOOR SUPPORT FR 59-61+4 STR 17L CORROSION. REMOVED AND REPLACED LAV/CARGO LATERAL FLOOR SUPPORT FR 59 - 61+4 STR 17L. NO DEFECTS NOTED AT THIS TIME

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

SIGNS OF CORROSION ON LH IB FLAP IB SHROUD RING SUPPORT NUT PLATE. REMOVED AND REPLACED SUPPORT AT LH IB FLAP IB SHROUD

Part: NOT REPORTED — NOT REPORTED · airframe 44,676 hrs · 27,959 cycles

PERFORM REPAIR AT REAR FUS II AT NAME PLATE MOUNT LOCATION. PERFORMED REPAIR AT REAR FUS II AT NAMEPLATE MOUNT LOCATION. RESTORED FINISH.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

RH AFT LAV FLOOR SUPPORT HAS SIGNS OF CORROSION FR 59-61+5 STR 17R. REMOVED AND REPLACED GUSSET

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

SKIN RIVETS ON STRINGERS 21L + 21R FROM FRAME 38 TO FRAME 39 SHOW SIGNS OF CORROSION. REMOVED AND REPLACED FASTENERS AT STR 21L TO 21R FROM FRAME 38 TO 39

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 44,676 hrs · 27,959 cycles

LH UPPER AILERON PANEL LANDING T/E CORROSION. BLENDED OUT AREA AND EVALUATED NOMINAL THICKNESS .080 REMAINING THICKNESS .079 AREA WITHIN LIMITS AT LH UPPER AILERON PANEL LANDING T/E, APPLY ALODINE, PRIMER AND TOP COAT.

Part: NOT REPORTED — NOT REPORTED · airframe 44,676 hrs · 27,959 cycles

RT WING TRAILING EDGE UPPER SURFACE FWD OF OBD FLAP POSSIBLE CORROSION. CLEANED AREA AT RH WING TRAILING EDGE UPPER SURFACE FWD OF OUTBD FLAP, FOUND TO BE DAMAGED PAINT. NO CORROSION FOUND.

Part: NOT REPORTED — NOT REPORTED · airframe 44,676 hrs · 27,959 cycles

RH UPPER T/E SKIN ON AILERON SHROUD LANDING HAS SIGNS OF CORROSION. CLEANED AREA AT RH UPPER T/E SKIN OF AILERON SHROUD LANDING, FOUND TO BE DAMAGED PAINT, NO CORROSION FOUND.

Part: TARGET — OUT OF ADJUST (NLG WOW) · airframe 43,738 hrs · 27,116 cycles

LG AIR/GND FAIL ON TAKE OFF. NLG WOW PROX SWITCH TARGET FOUND OUT OF ADJUSTMENT. ADJUSTED NLG WOW SWITCH TARGET. BREAKOUT BOX CONNECTED, CHECKED ALL WOW, DOWN LOCKS AND UP LOCKS. OPS CHECK SAT. GEAR SWINGS PERFORMED. ALL CHECKS SATISFACTORY.

Part: STRUT — INOPERATIVE (LT MLG) · airframe 43,602 hrs · 26,994 cycles

LH MLG SIDE STRUT LOWER BEARING FLANGE HAS MISSING ARROWS. REMOVED AND REPLACED LH MLG LOWER SIDE BRACE. OPS CHECK GOOD.

Part: ARMREST — CRACKED (SEAT 7A) · airframe 43,451 hrs · 26,858 cycles

FOUND CRACK UNDER ARMREST 7A MIDWAY UP. REMOVED AND REPLACED SEAT 7A.

Part: SEAT FRAME — CRACKED (SEAT 18A) · airframe 43,264 hrs · 26,700 cycles

PASSENGER SEATS 2A AND 18A HAVE CRACKED SUPPORTS BELOW AISLE ARMREST. SEATS 3A, 6A, AND 7A HAVE CRACKED SUPPORTS. R&R PASSENGER SEATS. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: ENGINE — FAILED (NR 2) · airframe 43,213 hrs · 26,653 cycles

ENGINE 2 FAILED AND SHUT DOWN ON CLIMB OUT. INSTALLED REPLACEMENT NR 2 ENGINE. OPERATIONS AND LEAK CHECK SATISFACTORY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,106 hrs · 26,562 cycles

SERVICE DOOR LOWER EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR LOWER EMERGENCY LIGHT LAMP. OPERATIONS CHECK SATISFACTORY, NO FURTHER DEFECTS NOTED.

Part: BOLT — DAMAGED (INT DOOR HANDLE) · airframe 42,993 hrs · 26,447 cycles

MAIN CABIN DOOR DOES NOT OPEN FROM INSIDE. OPENS WITH OUTSIDE HANDLE. FOUND SECURING BOLT FOR HANDLE SPLINE TO BE LOOSE AND STRIPPED. REMOVED AND REPLACED BOLT AND NUT. OPERATIONS CHECK SATISFACTORY.

Part: GEARBOX — OVERPRESSURED (ACCESSORY) · airframe 42,933 hrs · 26,391 cycles

E2 BLEED CAUSES OIL SMELL IN AIR COND. PERFORMED OIL-RELATED SMOKE/ABNORMAL SMELL IN CABIN/COCKPIT FIM TASK. FOUND ENGINE NR 1 EMITTING OIL SMELL THROUGH PACK SYSTEM WITH BLEED NR 1 ON, APU SHUT OFF AND ENGINE NR 2 OFF. NO INDICATION OF LEAKAGE OR PUDDLING FOUND. REMOVED AFT LOWER OUTBOARD OUTER BYPASS ACCESS PANEL TO FOM. FOUND AGB PRESSURE TO BE 22 PSI. THIS EXCEEDS THE MAX CASE PRESSURE OF 18PSI. INSTALLED REPLACEMENT NR 1 ENGINE.

Part: STRIP — LOOSE (CABIN) · airframe 42,933 hrs · 26,391 cycles

EMERGENCY REFLECTIVE STRIP LOOSE BY 1A. SECURED LOOSE PROX STRIP BY SEAT 1A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,881 hrs · 26,346 cycles

MULTIPLE INTERNAL AND ONE EXTERNAL EMERGENCY LIGHTS INOPERATIVE. R&R NR 2 EMERGENCY LIGHT BATTERY, OPS CHECK SAT.

Part: SKIN — CRACKED (VORTILON) · airframe 42,818 hrs · 26,280 cycles

CRACK FOUND EXTENDED OUT FROM VORTILON NUMBER 1 ON LEADING EDGE. REMOVED AND REPLACED LEADING EDGE 111. OPERATIONS CHECK SATISFACTORY.

Part: O-RING — DAMAGED (APU) · airframe 42,678 hrs · 26,127 cycles

SMELL OF HYD OR FUEL DURING TAKE OFF. SMELL WENT AWAY AFTER APU SHUTDOWN AND BLEEDS TRANSFERRED TO ENGINES. PERFORMED T/O POWER RUNS IN THESE SCENARIOS - APU OFF, BOTH ENGINES AT T/O POWER, BLEED 2 OPEN, BLEED 1 CLOSED AND PACK 1 ON. ONLY SMELL FROM THIS SET UP. NEXT, BLEED 1 OPEN, BLEED 2 CLOSED AND PACK 1 ON. NO NOTICEABLE SMELL. PERFORMED 2 MORE TIMES TO VERIFY SMELL WAS FROM THE #2 SIDE. RAN APU WITH BOTH PACKS, NO OIL OR FUEL SMELL. INSPECTED THE APU AND COWLING INSIDE AND OUT. NO OIL OR FUEL LEAKS OR SMELLS OF EITHER. RUN PACK 1 AND 2 WITH APU BLEED, THEN WITH #2 ENGINE BLEED. FOUND OIL LEAK AT LOW OIL PRESSURE SWITCH. R&R OIL PRESSURE SWITCH O-RING. PERFORMED ENGINE RUN AT IDLE POWER. NO LEAK EVIDENCE. R&R APU BLEED AIR VALVE. R&R APU ANTI SURGE VALVE. R&R APU MAIN FUEL SOLENOID. OPS CHECK SAT. NO LEAKS OR SMELL OF FUEL/HYD NOTED IN THE COCK-PIT AND CABIN AT THIS TIME. PN 4952829 SN 0175C TSN 1097.52 CSN 936 PN 4950899 SN 2072 TSN 3062.59 CSN 2827 PN 4952316-2 SN 1999 TSN 3062.59 CSN 2827

Part: PUMP — CONTAMINATED (FUEL SYSTEM) · airframe 42,677 hrs · 26,126 cycles

INVESTIGATE SOURCE OF FIBROUS DEBRIS IN RH ENGINE FUEL FILTER. FOUND PIECE OF CLOTH STUCK IN EJECTOR PUMP, NO OTHER DEBRIS. REMOVED, CLEANED AND REINSTALLED PUMP.

Part: UNKNOWN — ODOR · airframe 42,677 hrs · 26,126 cycles

STRONG FUEL SMELL ON TAKE-OFF WITH APU RUNNING. INSPECTED ALL FUEL NOZZLES, FUEL NOZZLE GASKETS, NOZZLE MANIFOLD, FUEL CONTROL, FUEL LINES, FUEL HOSES, AND COMBUSTOR DRAIN LINE WITH APU RUNNING. OBSERVED NO LEAKAGE OR EVIDENCE OF LEAKAGE BEFORE, DURING, OR AFTER APU RUN.

Part: FUEL CONTROL — MALFUNCTIONED (APU) · airframe 42,673 hrs · 26,123 cycles

SMELL OF FUEL ON TAKE OFF WITH APU RUNNING. R&R APU FUEL CONTROL. HIGH POWER ENGINE RUNS OPS CHECK SAT. NO FUEL SMELL NOTED AT THIS TIME.

Part: SNAP RING — OUT OF POSITION (CABIN DOOR) · airframe 41,737 hrs · 25,350 cycles

MAIN CABIN DOOR WILL NOT OPEN. MAIN CABIN DOOR INTERNAL HANDLE INTERMEDIATE TORQUE TUBE ON RT SIDE END HAS A SNAP RING OUT OF PLACE, CAUSING TORQUE TUBE TO SHIFT AND INTERFERE WITH OPENING. REMOVED AND REINSTALLED TORQUE TUBE WITH NEW SLIP RING. PERFORMED INTERNAL HANDLE OPS CHECK. OPS CHECK SAT.

Part: LIGHT — UNSECURE (CABIN) · airframe 41,497 hrs · 25,106 cycles

EMERGENCY LIGHT STRIP BY SEAT 1A NOT SECURED. RE SECURED EMERGENCY FLOOR LIGHTING NEAR SEAT 1A.

Part: SKIN — CORRODED (FRAMES 80-81) · airframe 41,120 hrs · 24,761 cycles

DURING MX INSPECTION, CORROSION WAS DISCOVERED ON THE AFT EXTERNAL FUSELAGE SKIN COMING FROM UNDER THE AIRCRAFT DATA PLATE. MX CUT OUT THE DAMAGED AREA AND PERFORMED A FILLER/DOUBLER REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: BRACKET — CRACKED (PAX DOOR ROLLER) · airframe 40,078 hrs · 23,999 cycles

DURING C CHECK INSPECTION MAIN CABIN DOOR FORWARD UPPER ROLLER BRACKET HAD A DAMAGED NUTPLATE. MAINTENANCE REMOVED ROLLER BRACKET ASSEMBLY AND FOUND BRACKET TO BE CRACKED. THE CRACKED HOLE WAS DRILLED OVERSIZED TO .375" TO REMOVE CRACK. THE HOLE WAS REAMED AND HFEC WAS PERFORMED. NO CRACK WAS FOUND. A REPAIR BUSHING WAS INSTALLED AND BRACKET WAS REINSTALLED TO MAIN DOOR FUSELAGE FRAME. ALL WORK DONE I/A/W EO145-53-20-00004 AND ETD 2018-145-113775.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,078 hrs · 23,999 cycles

DURING C CHECK FOUND CRACK ON FRAME 10 RHS INNER FLANGE AT TOP FORWARD RIVET AT ATTACHMENT TO WINDOW SILL STRUCTURE. MAINTENANCE REPLACED FRAME 10 RHS INNER FLANGE IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,078 hrs · 23,999 cycles

SHEAR CLIP CRACKED AT FRAME 80 BETWEEN STRINGER 5L AND 7L. MAINTENANCE REPLACED SHEAR CLIP AT FRAME 80 STRINGER 5L AND 7L.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,078 hrs · 23,999 cycles

DURING C CHECK CORROSION WAS FOUND ON OMEGA BEAM BETWEEN FRAME 22 AND FRAME 23 JUST AFT OF THE SERVICE DOOR. MAINTENANCE REPAIRED OMEGA BEAM IAW SRM 53-21-10.

Part: RIB — CRACKED (LT WING) · airframe 40,078 hrs · 23,999 cycles

DURING C CHECK INSPECTION FOUND LEFT WING WEB CRACKED BETWEEN RIB 20-21. VERIFIED BY EDDY CURRENT. MAINTENANCE REPAIRED LEFT WING RIB 21 WEB IAW SRM 57-20-07.

Part: RIB — CRACKED (RT WING) · airframe 40,078 hrs · 23,999 cycles

DURING C CHECK INSPECTION FOUND RIGHT WING RIB WEB CRACKED BETWEEN RIB 20-21. MAINTENANCE REPAIRED WING RIB WEB BETWEEN RIB 20-21 IAW ETD2018-145-105347 AND SRM 57-20-07

Part: FITTING — CRACKED (RT PYLON) · airframe 40,078 hrs · 23,999 cycles

DURING C CHECK FOUND RIGHT ENGINE FORWARD LOWER PYLON YOKE FITTING CRACKED. MAINTENANCE REPLACED FORWARD YOKE FITTING.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,078 hrs · 23,999 cycles

DURING C CHECK FOUND DENT BELOW PANEL 113EZ. GPU SERVICE PANEL. BETWEEN FR 07 AND FRAME 08. MAINTENANCE REPAIRED IAW SRM 53-12-01

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,067 hrs · 21,864 cycles

THE CREW REPORTED THAT THE EMERGENCY LIGHT STRIP AT THE GALLEY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPS TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FADEC — INOPERATIVE · airframe 35,790 hrs · 20,970 cycles

NR 1 ENGINE LOSS 20 PERCENT N1, FADEC INOPERATIVE. MX REMOVED AND REPLACED THE FADEC 1A AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,100 hrs · 20,477 cycles

THE CREW REPORTED EMERGENCY LIGHT ABOVE THE F/A SEAT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: FRAME — CRACKED (FRM 10) · airframe 34,880 hrs · 20,313 cycles

DURING C-CHECK THE FRAME 10 SEGMENT JUST BELOW THE PILOT'S DV WINDOW WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FRAMES 20-22) · corrosion level 2 · airframe 34,880 hrs · 20,313 cycles

DURING C-CHECK, THE SERVICE DOOR CUTOUT CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FRAMES 65-66) · airframe 34,673 hrs · 20,152 cycles

GROUND DAMAGE WAS DISCOVERED ON THE AFT FUSELAGE BETWEEN FRAMES 65-66, STRINGERS 20L-21L. MAINTENANCE REMOVED THE DAMAGE AND INSTALLED A FILLER AND DOUBLER REPAIR. LEAK CHECKS WERE PERFORMED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,641 hrs · 18,753 cycles

CREW REPORTED THE EMERGENCY LIGHT OVER EXIT ROW NOT WORKING. MAINTENANCE R & R NR 4 EMERGENCY BATTERY PACK WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,278 hrs · 18,511 cycles

DURING PRE-FLIGHT, THE CREW REPORTED THAT THE EXIT LIGHT AT THE FRONT OF THE CABIN WAS INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 29,272 hrs · 16,595 cycles

DURING C-CHECK, DUMP VALVE EXTERNAL HOUSING CORRODED, LOCAL LEVEL 2, AT SEVERAL AREAS. MAINTENANCE R & R WASTE DRAIN DUMP SUPPORT ASSY IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAMES 77-80) · airframe 29,272 hrs · 16,595 cycles

DURING C-CHECK, VISUAL INDICATION OF CRACKS ON FUSELAGE BETWEEN FRAMES 77-80, S3-6L. MAINTENANCE REPAIRED SKIN IAW EC5330-01849. MAJOR REPAIR IAW EC5330-02849. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 29,272 hrs · 16,595 cycles

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

Part: FAIRING — DAMAGED (LT WING TE FLAP) · airframe 29,272 hrs · 16,595 cycles

DURING C-CHECK, LEFT OTBD FLAP INBD FAIRING FLANGE HAS MULTIPLE DRILL HOLES. MAINTENANCE REPAIRED IAW EC5750-01566. ACFT APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — FAULTY (COCKPIT) · airframe 21,576 hrs · 11,593 cycles

FLIGHT 2370 - MSP - FLIGHT CREW REPORTED BURNING SMELL AND LIGHT SMOKE IN COCKPIT COMING FROM FO MFD. CREW DECLARED EMERGENCY AND PERFORMED EMERGENCY DESCENT AND LANDED UNEVENTFULLY. CLE MX REMOVED AND REPLACED FO MFD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: DISPLAY — FAULTY (COCKPIT) · airframe 21,576 hrs · 11,593 cycles

THE CREW REPORTED THE F/O MFD WENT BLANK WITH A BURNING SMELL AND LIGHT SMOKE. MX INSPECTED AND REPLACED THE F/O DISPLAY UNIT. OPS CHECKS WERE GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 21,568 hrs · 11,589 cycles

DURING FLIGHT, THE AIRCREW RECEIVED AN EICAS MESSAGE THAT THE E1 HYD PUMP FAILED. THE FLIGHT WAS DIVERTED AND THE ACFT LANDED WITHOUT INCIDENT. AN EMERGENCY WAS NOT DECLARED. MX R & R THE DEFECTIVE PUMP IAW AMM 29-10-03. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 21,335 hrs · 11,462 cycles

TYS - A/C WAS ON SENT TO TYS FOR A LIGHTNING STRIKE DAMAGE BETWEEN STR 20/21R NEAR FR 72. MAINTENANCE INSTALLED A SMALL DAMAGE REPAIR TO FUSELAGE SKIN AT FR72 AND STR 20/21R IAW ETD 2011-145/00377. A/C WAS RELEASE AFTER PRESSURE CHECKS TO SERVICE. DMI WAS THEN CLEARED.

Part: WARNING SYSTEM — FALSE ACTIVATION (ANIT-ICE SYSTEM) · airframe 20,415 hrs · 10,945 cycles

FLIGHT 2224 - EWR - FLIGHT CREW REPORTED ENGINE 1 ANTI ICE FAIL - UNABLE TO CONTINUE DUE TO WEATHER. EWR MX PERFORMED OPERATIONAL CHECK OF ANTI ICE SYSTEM AND COULD NOT DUPLICATE INDICATION. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (ANTI-ICE SYSTEM) · airframe 20,415 hrs · 10,945 cycles

FLIGHT 2224 - EWR - FLIGHT CREW REPORTED ENG 1 ANTI ICE VALVE FAIL MESSAGE ON EICAS. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX PERFORMED OPERATIONAL AND FUNCTIONAL CHECK OF THE BLEED SYSTEM AND COULD NOT DUPLICATE MESSAGE. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SWITCH — FAILED (ANTI ICE SYSTEM) · airframe 20,321 hrs · 10,892 cycles

FLIGHT 2769 DURING CLIMB THE CREW REPORTED AN ENGINE ONE ANTI-ICE FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE ANTI-ICE ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED THE ENGINE ONE ANTI-ICE PUSH BUTTON SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 20,145 hrs · 10,796 cycles

LT EMERGENCY LIGHT EXIT SIGN AT ROW 12A INOP. REMOVED AND REPLACED EXIT IDENTIFIER IAW EMB 145 AMM 330-50-15, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,094 hrs · 10,675 cycles

FLIGHT 3009 - EWR - FLIGHT CREW REPORTED EMERGENCY LIGHT STRIP INOP. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (LANDING GEAR) · airframe 19,694 hrs · 10,539 cycles

IAH - FLIGHT 2604, THE CREW REPORTED THAT AFTER DEPARTURE THE LANDING GEAR LEVER WOULD NOT RETRACT WITHOUT SEVERAL ATTEMPTS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RELAY K0024, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — INOPERATIVE (MLG) · airframe 19,681 hrs · 10,531 cycles

FLIGHT CREW REPORTED THAT AFTER T/O, LANDING GEAR WOULD NOT RETRACT WITHOUT PRESSING THE DOWNLOCK RELEASE BUTTON. MX R & R LANDING GEAR CONTROL LEVER MODULE AND PREFORMED EXT/RET OF LANDING GEAR CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 17,753 hrs · 9,499 cycles

IAH - FLIGHT 2081, THE CREW REPORTED INTERMITTENT LAV SMOKE WARNINGS ON EICAS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 16,257 hrs · 8,693 cycles

IAH - FLIGHT 2240, DURING CLIMB THE CREW REPORTED ELEC EMERGENCY ABNORMAL, BUT NO SYSTEM PROBLEMS NOTED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BATTERY CONTROL PANEL, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 15,248 hrs · 8,153 cycles

MAIN DOOR HARD TO OPEN AND CLOSE. ADJUSTED MAIN DOOR IAW EMB 145 AMM 52-18-06. OPS CK GOOD. ACFT RELEASED AND RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 15,108 hrs · 8,076 cycles

BTR - FLIGHT 2050 - DURING CLIMB THE CREW REPORTED A SMOKE SMELL IN THE COCKPIT AND CABIN. THE AIRCRAFT DIVERTED TO BTR WHERE IT LANDED WITHOUT INCIDENT. LCH MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE ENGINES, PACKS, AND APU ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

TYS - DURING C-CHECK THE LT WING EMERGENCY LIGHT WAS FOUND DIM DURING AN OPS CHECK. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY FOR THE LT WING EMERGENCY LIGHT IAW EMB 145XR 33-50-04 AND OPS CHECKED GOOD. ACFT WILL BE RELEASED WHEN C-CHECK IS COMPLETE. (S)

Part: BRACKET — GOUGED (RT AILERON)

A/C WAS IN A C CHECK STATUS AND THE O/B BUSHION HOLE ON THE PCA BRACKET ATTACH POINT WAS FOUND OVERSIZE ON THE RT AILERON. MX REPLACED THE PCA BRACKET IAW EC 5750-01177. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED BACK TO SERVICE.

Part: BEARING — CORRODED (VERTICAL STAB)

A/C WAS IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE LT SPHERICAL BEARING. MX REMOVED THE CORROSION REMOVED SPHERICAL HOUSING AND REAM TO THE 1ST OVERSIZE TO INSTALL A NEW BUSHION. REPLACED THE BEARING. INSTALL THE SPHERICAL BEARING AND PERFORMED ALL CHECKS. A/C WAS RELEASED AT THE CLOSE OF THE C-CHECK. ALL WORK WAS ACCOMPLISHED IAW EMB 145XR SRM 55-37-00, 55-30-02.

Part: SWITCH — INOPERATIVE (FIRE DETECTION) · airframe 13,176 hrs · 7,018 cycles

FLIGHT 2053 - EWR - FLIGHT CREW REPORTED BAG FIRE DETECTION LIGHT INOPERATIVE. EWR MX REMOVED AND REPLACED TEST SWITCH AND RELAY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 11,439 hrs · 6,150 cycles

TYS - DURING ROUTINE MAINTENANCE VARIOUS EMERGENCY LIGHTS WERE FOUND NOT WORKING. THE NR 1 BATTERY PACK WAS REMOVED AND REPLACED IAW EMB 145XR AMM 33-50-04. OPS CHECKS WERE GOOD AND THE A/C WAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUELAGE) · airframe 4,339 hrs · 2,331 cycles

DURING A SCHEDULED 1C INSPECTION CORROSION WAS FOUND ON FRAME TO SKIN SHEAR TIE LOCATED AT FRAME 65, STRINGER 15L. MAINTENANCE FABRICATED AND INSTALLED A NEW SHEAR CLIP AS PER EMBRAER IC. AIRCRAFT TO BE RELEASED TO SERVICE FOLLOWING COMPLETION OF SCHEDULED 1C INSPECTION.