N14158

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

RIGHT OMEGA BEAM BTW FR 59-61 CORRODED. 2 REPAIR DOUBLERS ON CENTER FUSE IV RT OMEGA BEAM, ON UPPER SURFACE BTW FR 59-60 AND BTW FR 60-61 CUTOUT

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,605 hrs · 32,092 cycles

CENTER FUSE II, LEFT OMEGA BEAM CRACKED AT FRAME 33. CF II, REPAIR DOUBLER ON LT OMEGA BEAM INBD VERT FLANGE AT FR 33.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,605 hrs · 32,092 cycles

CENTER FUSELAGE II, LT OMEGA BEAM CRACKED AT FRAME 34. REPAIR DOUBLER ON LT OMEGA BEAM INBD VERT FLANGE AT FR 34.

Part: DOOR — CRACKED (THRUST REVERSERS) · airframe 49,605 hrs · 32,092 cycles

ON LH TR UPPER DOOR, FWD INBD EDGE FOUND CRACKED. ON LH TR UPPER DOOR, FWD INBD EDGE OF KICKER PLATE, FASTENERS REMOVED. ON LH TR UPPER DOOR, FWD IB KIKER PLATE REMOVED AND REPLACED.

Part: SPAR CAP — CORRODED · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

LT AND RT WING SPAR II CAP SURFACE TO BE CLEAN AND REPROTECTED AT LOCATION OF AILERON LOWER SHROUD. AT LT & RT WING SPAR II CAP SURFACE FOUND CORRODED, LH WING SPAR II CAP SURFACE CORRODED OUT OF LIMIT AND RH WING SPAR II CAP SURFACE BLENDED WITHIN LIMIT. AT TH WING SPAR II CAP SURFACE REPROTECTED. AT LH WING SPAR II CAP SURFACE REMOVED AND INSTALLED.

Part: RIB — CRACKED (ZONE 400) · airframe 49,605 hrs · 32,092 cycles

RH ENGINE UPPER COWLING, FWD RIB AT XN810 FOUND CRACKED. ON RH ENGINE UPPER COWLING, FWD RIB AT XN810 REMOVED AND REPLACED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,605 hrs · 32,092 cycles

CENTER FUSE II, LH OMEGA BEAM CRACKED AT FRAME 35. CENTER FUSE II, LH OMEGA BEAM AT FRAME 35 CUT-OUT PERFORMED AND REPAIRED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 49,605 hrs · 32,092 cycles

CENTER OMEGA BEAM CRACKED AT FRAME 28. REPAIR DOUBLER INSTALLED ON CTR FUSELAGE II CTR OMEGA BEAM, AT FR 28 INBD VERTICAL FLANGE.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

LEFT INBD SEAT TRACK NR 2, 4, 5, 6, 7, 15, 20, 21, 29, 33 FOUND CORRODED. AT LT INBD SEAT TRACK NR 2, 4, 5, 6, 7, 15, 20, 21, 29, AND 33 REMOVED FOR INSPECTION. SEAT TRACKS BLENDED OUT OF LIMITS. AT LT INBD SEAT TRACK NR 15 NEW SEAT TRACK INSTALLED.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

RIGHT INBD SEAT TRACK NR 2, 4, 6, 10, 18, 20, 26, 28 FOUND CORRODED. RT INBD SEAT TRACK NR 2, 4, 6, 10, 18, 20, 26, 28 BLENDED. RT INBD SEAT TRACK NR 2, 4, 10, 18, 20, 26, 28 REPROTECTED. AT RT INBD SEAT TRACK NR 6 REMOVED AND INSTALLED.

Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · airframe 49,605 hrs · 32,092 cycles

CENTER OMEGA BEAM BETWEEN 58-63 DAMAGED DURING REPAIR. CTR OMEGA BEAM BTW 58-63 FR REPAIRED.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

CENTER FUSE I, CENTER CROSSBEAM AT FRAME 20, LOWER AND UPPER SURFACE CORRODED. CENTER FUSE I CENTER CROSSBEAM AT FR20 BLENDED OUT OF LIMITS. CENTER FUSE I, CENTER CROSSBEAM AT FRAME 20 MADE REPAIR PART FABRICATED. CENTER FUSE I, CENTER CROSSBEAM AT FRAME 20 MADE REPAIR PART INSTALLED.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

CENTER GUSSET BTW FR 59-61 FOUND CORRODED. CENTER GUSSET BTW FR 59-61 BLENDED AND FOUND OUT OF LIMIT. CENTER GUSSET BTW FR 59-61 REMOVED AND REPLACED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

CENTER OMEGA BEAM AT FR59 FOUND CORRODED. CF4, CENTER OMEGA BEAM AT FR59 BLENDED AND FOUND OUT OF LIMIT. CF4, CENTER OMEGA BEAM AT FR59 CUTOUT PERFORMED. CF4 CENTER OMEGA BEAM AT FR59, OMEGA BEAM DAMAGED DURING REPAIR. CENTER OMEGA BEAM AT FR59 REPAIRED.

Part: TEE ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

AT FRAME 61 BETWEEN LT SILL & LT OMEGA BEAM, TEE PROFILE. TEE PROFILE WAS REPLACED.

Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

RIGHT FR61 AT FLOOR LEVEL FRAME DOUBLER FOUND CORRODED. RT FR61 AT FLOOR LEVEL, FRAME DOUBLER BLENDED OUT OF LIMIT. RH FR61 AT FLOOR LEVEL, FRAME DOUBLER REPLACED WITH NEW PART

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

LEFT GUSSET BTW FRAME 19-23 FOUND CORRODED. LT GUSSET BTW FR 19-23, GUSSET REMOVED AND REPLACED.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

CENTER FUSE I, LT SILL BTW FRAME 19-23 FOUND CORRODED. LT SILL BTW FRAME 19-23 REPLACED WITH NEW.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

RH SILL #6 CORRODED BTW FR 53-59. BTW FR 53-54 RH SILL #6 BLENDED OUT OF LIMITS. RH SILL #6 BTW FR 53-39 REMOVED AND REPLACED

Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

LH FR 61 AT FLOOR LEVEL, FRAME DOUBLER CORRODED. LT FR 61 AT FLOOR LEVEL, FRAME DOUBLER IS OUT OF LIMIT. LT FR 61 AT FLOOR LEVEL, FRAME DOUBLER REPLACED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 49,605 hrs · 32,092 cycles

LEFT FR 73 BTW STR 8L-10L, SHEAR TIE FOUND CRACKED. CRACKED LT FR 73 SHEAR TIE BTW STR 8L-10L REMOVED AND INSTALLED.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 49,605 hrs · 32,092 cycles

LH FR 71 BTW STR 17L-18L SHEAR CLIP FOUND CRACKED. CRACKED SHEAR CLIP AT LH FR 71 BTW STR 17L-18L REMOVED AND REPLACED.

Part: ANGLE — CRACKED (ZONE 600) · airframe 49,605 hrs · 32,092 cycles

RH OVERWING PANEL #194ER, #2 LOWER ANGLE CRACKED AT YA-1085 (RIB 1A). RH OVERWING PANEL #194ER, #2 LOWER ANGLE REMOVED AND REPLACED.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

RIGHT GUSSET BTW FR 59-51 CORRODED. RT GUSSET BTW FR 59-61 REMOVED AND REPLACED.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

LH GUSSET BTW FR 59-61 FOUND CORRODED. LH GUSSET BTW FR 59-61 BLENDED OUT OF LIMIT. REMOVED AND REPLACED LH GUSSET BTW FR 59-61.

Part: DOUBLER — BENT (ZONE 200) · airframe 49,605 hrs · 32,092 cycles

CENTER FUSELAGE III, DOUBLER ON TOP RH OMEGA BEAM AT FRAME 35 BENT. CFII DOUBLER ON TOP RH OMEGA BEAM AT FRAME 35 REMOVED AND REPLACED.

Part: PROFILE — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

RH FR 61 BTW RH SILL AND RH OMEGA BEAM, T-PROFILE FOUND CORRODED. RH FR 61 BTW RH SILL AND RH OMEGA BEAM, T-PROFILE BLENDED AND FOUND OUT OF LIMITS. RH FR 61 BTW RH SILL AND RH OMEGA BEAM, T-PROFILE WAS REPLACED.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

LH SILL BTW FR 60-65 FOUND CORRODED. LH SILL BTW FR 60-65 BLENDED AND FOUND OUT OF LIMIT. LH SILL BTW FR 60-65 REPLACED WITH NEW PART.

Part: ANGLE — CRACKED (ZONE 200) · airframe 49,605 hrs · 32,092 cycles

R/H OVERWING PANEL #194ER, #3 LOWER ANGLE CRACKED AT YA-1085 (RIB 1A). RT OVERWING PANEL 104ER, #3 LOWER ANGLE REMOVED AND REPLACED.

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

CENTER FUSELAGE III, RT CROSSBEAM AT FRAME 35 CORRODED. CFIII, RH CROSSBEAM AT FRAME 35 BLENDED AND FOUND OUT OF LIMIT. CENTER FUSELAGE III, RH CROSSBEAM AT FRAME 35 REMOVED AND REPLACED

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

CENTER FUSE II. LH GUSSET BTW FRAME 29-35 CORRODED. CENTER FUSE II, LH GUSSET BTW FRAME 29-35 BLENDED AND FOUND OUT OF LIMIT. CENTER FUSELAGE II LH GUSSET BTW FR 29-35 REMOVED AND REPLACED

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

CENTER FUSE I, FWD DIGITAL FOUND CORRODED. CENTER FUSE I, FWD DIGITAL CORROSION BLENDED AND FOUND OUT OF LIMITS. CENTER FUSE I, FWD DIGITAL CUTOUT DOUBLER AND DRILLED WERE DONE. CENTER FUSE I, FWD DIGITAL DOUBLER AND FILLER WERE PROTECTED. CENTER FUSE I, FWD DIGITAL DOUBLER AND FILLER WERE INSTALLED.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 49,605 hrs · 32,092 cycles

CENTER FUSELAGE, RT SILL FOUND CORRODED AT FRAME 19, BLENDED AND FOUND OUT OF LIMITS, CENTER FUSELAGE RH SILL CORROSION REMOVED, CUTOUT PERFORMED. CENTER FUSELAGE & RT SILL DOUBLE WAS MADE, DRILLED, PROTECTED AND INSTALLED. CENTER FUSELAGE RT SILL, ANGLE WAS REPLACED.

Part: PUMP — INOPERATIVE (ZONE 100) · airframe 49,333 hrs · 31,833 cycles

HYD 2 LOW QTY ON EICAS IN FLIGHT. REMOVED AND REPLACED EDP. PERFORMED OPS CHECK. RAN ENG 2. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME. SERVICED #2 HYD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 48,978 hrs · 31,504 cycles

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

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 47,889 hrs · 30,515 cycles

MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB ON MCD EMERGENCY LIGHT. OPS CHECK FAILED. REMOVED AND REPLACED MCD EMERGENCY LIGHT HOUSING. OPS CHECK SAT

Part: LIGHT — MISINSTALLED (RT OVERWING) · airframe 47,522 hrs · 30,203 cycles

RH OVERWING EXTERNAL EMERGENCY LIGHT INSTALLED UPSIDE DOWN. REMOVED AND CORRECTLY INSTALLED RH OVERWING EXTERNAL EMERGENCY LIGHT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,404 hrs · 30,109 cycles

RH EMERGENCY EXIT HATCH UPPER LIGHT INOPERATIVE. REMOVED AND REPLACED RH EMERGENCY EXIT HATCH UPPER LIGHT. OPS CHECK FAILED. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER NUMBER 6. OPS CHECK SAT

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,404 hrs · 30,109 cycles

EMERGENCY EXIT ROW OVERHEAD FWD EMERGENCY EXIT LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER #5. OPS CHECK SAT

Part: EXTINGUISHER — EMPTY (LAVATORY) · airframe 47,027 hrs · 29,803 cycles

LAV AUTO DISCHARGE FIRE EXTINGUISHER FOUND EMPTY. REMOVED AND REPLACED LAV FIRE EXTINGUISHER.

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 46,442 hrs · 29,240 cycles

PAX CABIN SEATS 18CD HAVE INOP OVERHEAD PSU EMERGENCY LIGHT. REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT BULB. OPS CHECK GOOD.

Part: PANEL — DAMAGED (UNKNOWN) · airframe 46,183 hrs · 28,999 cycles

DURING WALKAROUND FOUND DAMAGE FROM GROUND EQUIPTMENT TO AFT RIGHT SIDE OF WTF FAIRING AND FUSELAGE FURTHER AFT. MAPPED WTF PANEL #198CB FOR RTS REPAIR OR ALLOWABLE DAMAGE REQUEST. NO FURTHER DAMAGE BEHIND PANEL AND NO BLEED LEAKS. NO DAMAGE NOTED AFT OF PANEL 198CB BETWEEN FRAMES 62 AND 64. REMOVED AND REPLACED REAR-SECTION AFT PANEL OF WING-TO-FUSELAGE FAIRING 198CB. SEALED REAR SECTION AFT PANEL OF WING TO FUSELAGE FAIRING 198CB.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,845 hrs · 28,703 cycles

DURING TO/CLIMB OR DECENT FUEL SMELL IN PACKS. PERFORMED A VISUAL INSPECTION OF APU THROUGH APU OIL SERVICING DOOR, NO OIL FUEL SPILL, NO DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,787 hrs · 28,655 cycles

SMELL OF HYD FROM BLEED SYSTEM 1. RAN PACKS ON ALL SOURCES, COULD NOT DUPLICATE SMELL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,676 hrs · 28,558 cycles

FUEL SMELL THROUGH PACKS ON TAKE OFF AND APPROACH. PERFORMED RR FIM. NO ABNORMAL ODOR PRESENT AT THIS TIME

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,217 hrs · 28,152 cycles

MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EXT MCD EMERGENCY LIGHT BULB. FAILED OPS CHECK. MCD EMERGENCY LIGHT OPS CHECK SAT. FOUND EXT MCD EMERGENCY LIGHT TO FAIL OPS CHECK. REMOVED AND REPLACED EXT MCD EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 45,205 hrs · 28,137 cycles

REAR FLASHLIGHT INOPERATIVE. PERFORMED OPS CHECK. OPS CHECK SAT.

Part: FLASHLIGHT ASSY — ODOR (RT CABIN) · airframe 45,167 hrs · 28,105 cycles

FUMES ON DECENT COMING FROM COCKPIT VENTS. SMELLS LIKE BURNT SILICON. FOUND ABNORMAL SMELL ON CAPT SIDE EMERGENCY FLASH LIGHT. REMOVED AND REPLACED. OPS CHECK SAT.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 45,165 hrs · 28,104 cycles

VERY STRONG SMELL IN COCKPIT ON DECENT. COMPLIED WITH FIM TASK FOR ABNORMAL SMELL. RAN PACKS AND ENGINES WITH CREW. NO DEFECTS FOUND. COULD NOT DUPLICATE

Part: FRAME — CRACKED (FRM 59 S15-16L) · airframe 44,894 hrs · 27,855 cycles

CRACK FOUND ON LH FRAME 59 BTW STR 15L-16L IN CF4 FLOOR STRUCTURE AREA. EXTENDED SPLICE REPAIRED ON CENTER FUSE 4 FR BTW STR 15L-16L

Part: FLOOR SUPPORT — CRACKED (FRMS 24-29) · airframe 44,894 hrs · 27,855 cycles

CF2 UNDERFLOOR LH OMEGA BEAM CRACK SUSPECTED AT FRAME 24-25-26-27-28-29. AFTER NDT INSPECTION, 6 CRACKS CONFIRMED ON LH OMEGA BEAM #2 AT FR 24-25-26-27-28-29, CF2 UNDERFLOOR LH OMEGA BEAM CRACK AT FR 24-25-26-27-28-29 REPAIRED

Part: FLOOR SUPPORT — CRACKED (FRMS 30-31) · airframe 44,894 hrs · 27,855 cycles

CF2, UNDERFLOOR, LH OMEGA BEAM CRACK SUSPECTED AT FRAME 30 ANND 31. AFTER NDT INSPECTION, 2 CRACKS CONFIRMED ON LH OMEGA BEAM #3 AT FR30 AND FR31. FABRICATED REPAIR PARTS (2). AT CF2, UNDERFLOOR LH OMEGA BEAM AT FR30 AND 31, INSTALLED REPAIR PARTS

Part: FLOOR SUPPORT — CRACKED (FRMS 21-23) · airframe 44,894 hrs · 27,855 cycles

LH OMEGA BEAM CRACK SUSPECTED AT FR 21, 22, AND 23. AFTER NDT INSPECTION, ONLY 2 CRACKS FOUND AT FR21 AND FR23 LH OMEGA BEAM CRACK AT FR21 AND FR 23 REPAIRED

Part: FLOOR SUPPORT — CRACKED (FRMS 45-53) · corrosion level 2 · airframe 44,894 hrs · 27,855 cycles

CF3 LH OMEGA BEAM BTW FR 45-53 FOUND CORRODED AND CRACK SUSPECTED AT FR51. AFTER NDT INSPECTION, 1 CRACK CONFIRMED ON LH BEAM AT FR51. CORROSION ON LH OMEGA BEAM BTW FR 48-49 BLENDED OUT OF LIMITS. CF3 LH OMEA BEAM BTW FR 48-49 REPAIRED AND INSTALLED. CF3 LH OMEGA BEAM AT FR51 REPAIRED

Part: SHEAR TIE — CRACKED (FRM 66 S6-7L) · airframe 44,894 hrs · 27,855 cycles

CRACK FOUND ON LH SHEAR CLIP AT FR 66 BTW STR 6L-7L IN RF1 AREA. CRACK FOUND ON LH SHEAR CLIP AT FR 66 BTW STR 6L-7L IN RF1 AREA. SHEAR CLIP FABRICATED WITH AN ALTERNATE MATERIAL. LH SIDE AT FR 66 BTW STR 6L-7L FABRICATED SHEAR CLIP INSTALLED.

Part: SHEAR TIE — CRACKED (FRM 72 S7-10L) · airframe 44,894 hrs · 27,855 cycles

SUSPECTED CRACK FOUND ON LH SHEAR CLIP AT FR 72 BTW STR 7L-10L IN RF1 AREA. SUSPECTED CRACK FOUND ON LH SHEAR CLIP AT FR 72 BTW STR 7L-10L IN RF1 AREA

Part: SHEAR TIE — CRACKED (FRM 58 S15-16L) · airframe 44,894 hrs · 27,855 cycles

CRACK FOUND ON LH SHEAR CLIP FR 58 BTW STR 15L-16L. CRACK FOUND ON LH SHEAR CLIP AT FR 58 BTW STR 15L-16L. SHEAR CLIP REPLACED AT FR 58 BTW STR 15L-16L

Part: NONE — NONE · corrosion level 2 · airframe 44,894 hrs · 27,855 cycles

CORROSION ON REAR FUSE 2 LOWER SKIN, BTW FR 80-81 AND BTW STR 19L-21L. REPAIR DOUBLER ON LOWER REAR FUSE 2 SKIN, BTW FR 80-81 AND BTW STR 18L-21L. EXTERNAL AND INTERNAL DET, THRESHOLF OF 5000 FC, INTERNAL OF 5000 FC

Part: FLOORBEAM — CORRODED (FRM 59) · corrosion level 2 · airframe 44,894 hrs · 27,855 cycles

CORROSION FOUND ON CENTER U FLOOR SECTION FRAME 59 IN CF4 FLOOR STRUCTURE AREA. FRAME REPAIRED ON CENTER FUSE 4 FR59, ON UPPER FLANGE BTW STR 21L-21R

Part: NONE — NONE · corrosion level 2 · airframe 44,894 hrs · 27,855 cycles

CORROSION FOUND ON LH GUSSET BTW FR 59 - FR 61 IN CF4 TOILET FLOOR STRUCTURE AREA. REPAIR DOUBLER ON LH CENTER FUSE 4 OMEGA BEAM BTW FR 59-60

Part: NONE — NONE · airframe 44,762 hrs · 27,733 cycles

DURING DECENT, AT APPROX 13000 FT, STRONG FUEL BURNING SMELL PRESENT IN COCKPIT AND FORWARD SECTION OF CABIN. C/W EMB 145 FIM TASK FOR ABNORMAL SMELL AND RR FIM TASK FOR OIL OR FUEL BURNING SMELL C/W RR FIM`S 72-00-00-990-801 & 72-00-00-810-814. NO FAULTS FOUND / INSPECTED #1 PACK ACM. NO FAULTS FOUND.

Part: ENGINE — UNKNOWN · airframe 44,729 hrs · 27,707 cycles

PACK #1 PRODUCED STRONG SMELL OF FUMES IN FLIGHT. TOTAL TIME (HOURS) HAS BEEN CORRECTED TO 44729.3

Part: NONE — NONE · airframe 44,569 hrs · 27,560 cycles

LARGE EMERGENCY EXIT SIGN IN GALLEY INOPERATIVE. REMOVED AND REPLACED EXIT MARKING SIGN AT GALLEY. OPS CHECK SAT

Part: LAMP — INOPERATIVE · airframe 44,300 hrs · 27,314 cycles

EMERGENCY LIGHTS MAIN CABIN DOOR AND SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS AT MAIN CABIN DOOR AND SERVICE DOOR. MAIN CABIN DOOR EMERGENCY LIGHT OPS CHECK SAT. OPS CHECK SAT

Part: CONTROL UNIT — INOPERATIVE (TE FLAP SYSTEM) · airframe 43,604 hrs · 26,703 cycles

FLAP FAIL AFTER TAKE OFF CALL OUT. FLAPS INDICATING AMBER DASH. R&R FECU. OPS CECK SAT. R&R FLAP POWER DRIVE UNIT. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,334 hrs · 26,459 cycles

EMERGENCY LIGHTS WILL NOT LIGHT. R&R EMERGENCY BATTERY PACK NO 3 AND NO 4. OPS CHECK SAT. #4 PN 2013-1A SN 91402 TSN 29997.06 CSN 22944 #3 PN ABS-2013-1A SN 51099 TSN 2674.38 CSN 2428

Part: ARMREST — CRACKED (SEAT 8A) · airframe 42,933 hrs · 26,121 cycles

CONFIRMED WITH EDDY CURRENT MACHINE A CRACK INDICATION AT SEAT 8A ARMREST STRUCTURE. R&R PASSENGER SEAT 8A. NO FURTHER DEFECTS NOTED AT THIS TIME

Part: SKIN — NOT REPORTED (EXTERIOR) · airframe 42,821 hrs · 26,017 cycles

LH EXTERNAL SKIN CF4 BTW STR 3L-4L DOUBLER FOUND. REPAIR DOUBLER ON LH CENTER FUSE 4 BTW FR 57-58 AND BTW STR 3L-4L REPAIRED

Part: SKIN — DENTED (CARGO DOOR) · airframe 42,821 hrs · 26,017 cycles

MULTIPLE DENTS FOUND ON CARGO DOOR. REPAIR DOUBLER ON BAGGAGE DOOR AT STA X22716.2 AND BEAM #3 REPAIRED.

Part: HINGE — LOOSE (EXT PWR DOOR) · airframe 42,821 hrs · 26,017 cycles

EXTERNAL POWER ACCESS DOOR HINGE LOOSE. REPAIR DOUBLER ON LH FWD FUSE 2, BTW FR 6-7, STR 13L-15L REPAIRED

Part: DOUBLER — NOT REPORTED (FUSELAGE SKIN) · airframe 42,821 hrs · 26,017 cycles

LH EXT FUSE RF1 BTW FR 75-75A BTW STR 2L-3L DOUBLER FOUND. LH EXT FUSE RF1 BTW FR 75-75A STR 2L-3L DOUBLER REMOVED. LH EXT FUSE RF1 BTW FR 75-75A STR 2L-3L DOUBLER REPLACED

Part: DOUBLER — NOT REPORTED (FUSELAGE SKIN) · airframe 42,821 hrs · 26,017 cycles

RH RF 2 BTW FR79-80 AND STR 8R-10R DOUBLER FOUND ON SKIN. RH RF 2 BTW FR 79-80 AND STR 8R-10R DOUBLER REMOVED FROM SKIN. RH RF 2 BETWEEN FR 79-80 AND STR 8R-10R DOUBLER REWORKED.

Part: SKIN — DENTED (SERVICE DOOR) · airframe 42,821 hrs · 26,017 cycles

RH SERVICE DOOR LOWER SKIN AFT CORNER DENT FOUND. DAMAGE CUT OUT ON RH SERVICE DOOR LOWER SKIN AFT CORNER. RH SERVICE DOOR LOWER AFT CORNER REPAIRED.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,821 hrs · 26,017 cycles

DENT FOUND ON LH CTR FUSE 1, ON FR 20 AND ON STR 14L. DENT ON LH CENTER FUSELAGE-1 ON FRAME 20 BETWEEN STR 13L-15L REPAIRED

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,284 hrs · 25,519 cycles

PILOT REPORTED EMERGENCY LIGHTS AROUND BOTH DOORS AT SEAT 18 ARE NOT WORKING. MX REMOVED AND REPLACED #3 BATTERY PACK ASSY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BEARING — FAILED (GENERATOR) · airframe 34,678 hrs · 22,215 cycles

MOB - FLIGHT 4053 THCREW REPORTED A STRONG SMOKE SMELL IN THE CABIN POSSIBLY FROM ENGINE 1. THE AIRCRAFT LANDED AT MOB WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE #1 GENERATOR HAD SUFFERED A CATASTROPHIC BEARING FAILURE CAUSING THE GENERATOR TO SEVERELY OVERHEAT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GENERATOR AND SEVERAL OTHER PARTS ON THE #1 ENGINE INCLUDING THE GEAR BOX, #3 GENERATOR, AND PMA AS A PRECAUTION. OPERATIONAL AND LEAK CHECKS WERE PERFORMED SATISFACTORILY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — SMOKE (CABIN) · airframe 39,606 hrs · 23,563 cycles

IAH - FLIGHT 4369, THE CREW REPORTED THAT THE OVERHEAD CEILING LIGHT AT ROW 4 ADJACENT TO SEAT 4D STARTED SMOKING. THE AIRCRAFT LANDED AT OIAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THA AIRCTRAFT AND PLACED THE OVERHEAD LIGHT ON MEL 33-20-00-2, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. *** SDR FILED OPEN PENDING FINAL CORRECTIVE ACTION*** **SUPPLEMENTAL*** ON 09/29/18 TYS MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY ABOVE ROW 4D, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR CLOSED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,636 hrs · 22,875 cycles

DURING MX INSPECTION, THE AFT FACING OVERWING EMERGENCY EXIT SIGN, LEFT OVERWING EMERG EXIT, LEFT SIDE EXIT SIGNS, AND RIGHT OVERWING UPPER EXIT SIGN WAS FOUND INOPERATIVE. MX R & R THE NR 3 BATTERY PACK, OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — UNKNOWN (CABIN) · airframe 38,394 hrs · 22,713 cycles

DURING A PREFLIGHT INSPECTION, THE CREW REPORTED THA THE AISLE EMERGENCY LIGHT STRIPS AT SEATS 3C & 4C WERE FOUND TO BE NOT GLOWING. MAINTENANCE INSPECTED THE AIRCRAFT , OPERATIONALLY TESTED THE LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — UNKNOWN (4C) · airframe 38,394 hrs · 22,713 cycles

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THA THE AISLE EMERGENCY LIGHT STRIPS AT SEATS 3C & 4C WERE FOUND TO BE NOT GLOWING. MAINTENANCE INSPECTED THE AIRCRAFT , OPERATIONALLY TESTED THE LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)

LOSS OF PRESSURIZATION, ACFT DID NOT PRESSURIZATION ON TAKE OFF. AIRCRAFT PERFORMED AN AIR RETURN. MAINTENANCE PERFORMED RESET OF PRESSURIZATION SYSTEM IAW AMM 21-31-00. CLEANED FILTER ON MANUAL PRESSURIZATION CONTROLLER IAW AMM 21-31-02. SYSTEM OPS CHECKED GOOD IN BOTH AUTO AND MANUAL MODE. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 37,301 hrs · 21,925 cycles

THE CREW REPORTED THAT NOT ALL EMERGENCY LIGHTS ILLUMINATE WHEN THE SYSTEM TURNS ON, WITH THE FOLLOWING BEING INOP.; REAR PART OF EXIT ROW O/HEAD SIGN, BOTH SIDEWALL EXIT SIGNS ON LEFT SIDE, ONLY WALL SIGN ON RIGHT SIDE EXIT ROW. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVE AND REPLACED THE AFT BATTERY PACK FOR THE EMERGENCY LIGHTS, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,914 hrs · 20,961 cycles

PILOT REPORTED THE EMERGENCY LIGHT WON'T TURN ON. RAN APU FOR 20 MINS, COMPLIED WITH AN OPERATION CHECK, CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. NO FURTER DEFECT NOTED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,695 hrs · 20,803 cycles

THE CREW REPORTED THE EMERGENCY EXIT LIGHTS BY ROW 18 WERE NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE NR 3 POWER SUPPLY. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,241 hrs · 20,473 cycles

EMERGENCY LIGHTS STAY ON IN THE ARMED POSITION. MX REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN FOR SERVICE.

Part: FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 34,477 hrs · 19,928 cycles

DURING C-CHECK THE CARGO DOOR FORWARD FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5230-01393. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 34,477 hrs · 19,928 cycles

DURING C-CHECK THE AFT CARGO DOOR FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5230-01393. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,554 hrs · 14,658 cycles

DURING ROUTINE MX THE AISLE PATH EMERGENCY LIGHT STRIP AT ROW 1 WAS FOUND INOPERATIVE. MX REPLACED THE LIGHT STRIP AND OPS CHECKS WERE GOOD.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 23,406 hrs · 12,624 cycles

ACFT IN FOR A C-CHECK, LT SIDE SHEAR CLIP NEAR THE WASTE VALVE WAS FOUND CORRODED. MX REMOVED, FABRICATED A NEW CLIP, NDT TREATED, PRIMED AND INSTALLED AT STRINGER 17. ALL WORK ACCOMPLISHED IAW AMM 53-31-00. ACFT WILL BE RELEASED A THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 23,406 hrs · 12,624 cycles

ACFT FOR A C-CHECK, CORROSION WAS FOUND AT THE DIGITAL OMEGA BEAM AT Y=0. MX REPLACED THE DIGITIAL BEAM. ACFT WILL BE RELEASED AT THE END OF THE CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 23,406 hrs · 12,624 cycles

ACFT IN FOR A C-CHECK, BAGGAGE DOOR CUT OUT AT AFT POSITION "L" (FR-68 TO FR 69) SHEARFOOT SHAPE WAS FOUND CORRODED. MX C/W EC3520-01494, REV A.

Part: HOUSING — CORRODED (ZONE 900) · airframe 23,406 hrs · 12,624 cycles

ACFT FOR A C-CHECK, LAVATORY DUMP HOUSING WAS FOUND CORRODED AT THE MOUNTING FLANGE. MX R & R THE DUMP VALVE HOUSING IAW AMM 53-30-29. ACFT WILL BE RELEASED AT THE END OF THE CHECK.

Part: HANDLE — FAULTY (NLG STEERING) · airframe 21,727 hrs · 11,585 cycles

CLE FLT 2370 THE CREW REPORTED A STEERING SYSTEM MALFUNCTION DURING TAKEOFF ROLL ABOVE 80 KNTS. ALSO REPORTED DISCONNECTS ON TAXI INTERMITTENTLY. MAINTENANCE INSPECTED AND REPLACED THE STEERING HANDLE. OPERATIONAL CHECKS WERE GOOD.

Part: VALVE — DAMAGED (LT WING) · airframe 21,541 hrs · 11,482 cycles

FLIGHT 5836 - RIC - FLIGHT CREW REPORTED FUEL LEAKING OUT OF LEFT WING. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. RIC MX REMOVED AND REPLACED LEFT WING FLAP VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UPLOCK — INOPERATIVE (ZONE 700) · airframe 19,641 hrs · 10,402 cycles

ACA - FLIGHT 3100, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE ON TAKEOFF AND THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO ACA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED THE CONNECTOR ON THE RIGHT PROXIMITY SWITCH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT TOOK OFF ONCE AGAIN AND RECEIVED THE SAME INDICATION AND RETURNED TO ACA WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT FERRIED TO IAH ON 11/01/10 WHERE IT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK BOX, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 18,661 hrs · 9,868 cycles

IAH - FLIGHT 2081 THE CREW REPORTED A LAV SMOKE INDICATION ON EICAS. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 18,633 hrs · 9,853 cycles

IAH - IT WAS REPORTED THAT THERE WAS A LAV SMOKE INDICATION ON EICAS. MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY TESTED THE LAV SMOKE DETECTOR WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 18,583 hrs · 9,829 cycles

IAH - IT WAS REPORTED THAT THE LAV SMOKE DETECTOR WENT OFF. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED OPERATIONAL TEST OF SMOKE DETECTOR WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (RT MLG) · airframe 18,555 hrs · 9,813 cycles

EWR FLT 2657 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE DURING CLIMBOUT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR AFT AIR/GROUND PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 18,460 hrs · 9,760 cycles

SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65-68 AND STRINGERS 15-16L. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 18,460 hrs · 9,760 cycles

SHV - DURING C CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 5-7L. MAINTENANCE PERFORMED BUSHING REPAIRS IAW EC5330-02156. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,820 hrs · 10,007 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM BETWEEN FRAMES 23.5-25 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED CORROSION AND FOUND TO BE IN LIMITS IAW EMB-145 SRM 53-22-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — FAULTY (NR 1 PACK) · airframe 17,355 hrs · 9,184 cycles

IAH FLT 2124 THE CREW REPORTED A PACK 1 OVERLOAD MESSAGE IN FLT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED NR 1 PACK OVER TEMP SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: THERMOSTAT — INOPERATIVE (BLEED SYSTEM) · airframe 15,527 hrs · 8,196 cycles

FLIGHT CREW REPORTED BLEED 1 LOW TEMP INDICATION ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED THERMOSTAT AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,136 hrs · 7,989 cycles

TYS - DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT AT ROW 12BC WAS FOUND INOP. THE NR 5 EMERGENCY LIGHT INVERTER WAS REMOVED AND REPLACED AND OPS CHECKED GOOD IAW EMB 145XR AMM 33-50-12. A/C WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 14,980 hrs · 7,913 cycles

FLIGHT 3072 - EWR - FLIGHT CREW REPORTED SEVERAL EMERGENCY LIGHT NOT ILLUMINATING. EWR MX REMOVED AND REPLACED NR 3 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 14,604 hrs · 7,706 cycles

NR 2 MFD & PFD BLANKED OUT IN FLIGHT. REMOVED AND REPLACED PILOTS AND COPILOTS MFD & PFD BEZELS IAW EMB 145XR AMM 34-22-02. REMOVED AND REPLACED PILOTS REVISIONARY PANEL IAW EMB 145XR AMM 34-22-03, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: BUSHING — WORN (AILERON)

ACFT CURRENTLY IN C-CHECK STATUS. MAINTENANCE FOUND THE LT AILERON IB PCA HAD BUSHING MIGRATED. MAINT REMOVED AND REPLACED THE HAT BUSIONS IAW EC5740-01152 AND WILL BE RELEASED AT THE END OF THE CHECK. (K)

Part: SILL — CORRODED · airframe 4,114 hrs · 2,136 cycles

DURING A SCHEDULED 1C INSPECTION THE CARGO DOOR CUTOUT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL ASSEMBLY AS PER THE EMB 145XR SRM AND EC5330-01458. ACFT WILL BE RELEASED TO SERVICE FOLLOWING COMPLETION OF THE 1C INSPECTION.