N11193

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 42,449 hrs · 29,721 cycles

MAIN CABIN DOOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED MAIN CABIN DOOR EMERGENCY LIGHT. OPS CHECK SAT.

Part: PRECOOLER — LEAKING (BLEED SYS) · airframe 41,355 hrs · 28,662 cycles

BLEED 2 OVERTEMP IN FLIGHT. RAN QRH DESELECTED BLEED 2 SYSTEM MESSAGE EXTINGUISHED, DURING CLIMB OUT FROM FL200 - FL2100, ROUGHLY AT 270-280 KIAS, OCCURRED IN ICING. REMOVED AND REPLACED BOTH RH FAN AIR CONTROL THERMOSTATS. WHILE PERFORMING ENGINE RUNS. FOUND PRE COOLER TO BE LEAKING. REMOVED RH PRE COOLER. INSTALLED RH PRECOOLER. PERFORMED OC OF AIR BLEED SYSTEM. OPS CHECK SAT. NO LEAKS. RETURNED AIRCRAFT TO ORIGINAL CONFIGURATION. WHEN BLEED 2 OVERTEMP PRESENTED, BLEED 1 WAS CLOSED AND CROSS-BLEED OPENED. BLEED 1 TEMPERATURE ROSE TO THE RED AND BLEED 1 OVERTEMP DISPLAYED ON EICAS. PERFORMED AIR BLEED SYSTEM OPERATIONAL TEST. AFTER RH THRUST LEVER SET TO 90%, N2 BLEED 2 TEMP ROSE INTO THE UPPER GREEN SCALE AND OVERTEMP OCCURS WITHIN TWO MINUTES. WHEN PRECOOLER VALVE 2 CB PULLED, BLEED 2 OVERTEMP OCCURS AT A FASTER RATE. PACK 2 OVERHEAT ALSO PRESENTED ON EICAS AND IS SUSPECTED TO HAVE BEEN CAUSED BY LEAKS AND HIGH BLEED AIR TEMP COMING OUT OF THE PRE-COOLER, RECOMMEND FURTHER EVALUATION OF E2 BLEED TUBES, PRE-COOLER REGION AND FAN AIR VALVE.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 41,211 hrs · 28,531 cycles

LEFT FWD EXTERIOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED LAMP. OPS CHECK SAT.

Part: GUSSET — CRACKED (FRMS 52-59) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CFIV, CORROSION FOUND ON LH GUSSET #7 BTW FR 52-59 IN FLOOR STRUCTURE AREA. AT CFIV, ON LH GUSSET #7 BTW FR 52-59 IN FLOOR STRUCTURE AREA CORROSION BLENDED OUT OF LIMIT. AT CFIV, ON LH GUSSET #7 BTW FR 52-59 IN FLOOR STRUCTURE AREA REMOVED AND REPLACED

Part: SKIN — CRACKED (FRMS 77-80 S3-9L) · airframe 39,914 hrs · 27,297 cycles

CRACKS SUSPECTED (20X) ON LH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3L-9L. AFTER NDT INSPECTION, 30 CRACKS FOUND. SKIN REPAIRED WITH 2 DOUBLERS ON LH REAR FUSE 2 SKIN, AT FR 79 BTW STR 5L-7L AND BTW STR 8L - SKIN EDGE. ALSO, 2 BUSHINGS ON LH REAR FUSE 2 SKIN, AT FR 78 BTW STR 2L-4L AND WITH 21 BUSHINGS REPAIR ON LH REAR FUSE 2 SKIN BTW FR 77-80 AND BTW STR 2L-9L

Part: SKIN — CRACKED (FRMS 77-80 S3-9R) · airframe 39,914 hrs · 27,297 cycles

CRACKS SUSPECTED (22X) ON RH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3R-9R. AFTER NDT INSPECTION (47X) CRACKS CONFIRMED ON RH SKIN BTW FR77-80 STR 3R-9R. (8X) CRACKS ON RH SKIN BTW FR 77-80 STR 3R-9R REPAIRED WITH BUSHING. (39X) CRACKS ON RH SKIN BTW FR 77-80 STR 3R-9R REPAIR WITH A DOUBLER.

Part: FLOOR SUPPORT — CRACKED (FRM 25) · airframe 39,914 hrs · 27,297 cycles

CF2, CRACK FOUND ON CENTER OMEGA BEAM #1 FLOOR STRUCTURE FLANGE AT FR25. REPAIR DOUBLER ON CENTER FUSE 2 CENTER OMEGA BEAM, ON LH VERTICAL FLANGE AT FR25

Part: CONTROL CABLE — FRAYED (STICK PUSHER) · airframe 39,914 hrs · 27,297 cycles

STICK PUSHER ACTUATOR CABLE STAND BROKEN WIRE OUT OF LIMIT. STICK PUSHER ACTUATOR REPLACED

Part: STRAP — CORRODED (FRMS 60-61) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

RF1, CORROSION FOUND ON U/FLOOR SKIN STRAP BTW FR 60-61 AND BTW STR 20R-21R. RF1, UNDER FLOOR, SKIN SPLICE STRAP BTW FR 60-61 AND BTW STR 20R-21R CORROSION BLENDED AND FOUND OUT OF LIMIT. RF1, UNDER FLOOR SKIN SPLICE STRAP BTW FR 60-61 CUTOUT. RF1, UNDER FLOOR BTW FR 60-61 AND BTW STR 20L-21R SKIN SPLICE STRAP REPAIRED

Part: STRUCTURE — CORRODED (FRM 65) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

RF1, CARGO DOOR SURROUND STRUCTURE FWD L-SHAPE AT FR65 FOUND CORRODED. RF1, CARGO DOOR SURROUND STRUCTURE FWD L-SHAPE AT FR65 FOUND CORROSION OUT OF LIMITS. REMOVED SPLICE AND LOWER SEGMENT OF FR65 FOR REPAIR. REPAIR COMPLETED

Part: CROSSBEAM — CORRODED (FRM 29) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF2, MIDDLE ALLEY CROSSBEAM ON FLOOR STRUCTURE AT FR29 FOUND CORRODED. AT CF2, MIDDLE ALLEY CROSSBEAM AT FR29, REMOVED FOR INVESTIGATION. AT CF2 MIDDLE ALLEY CROSSBEAM AT FR29 BLENDED OUT OF LIMITS. CF2, MIDDLE ALLEY CROSSBEAM ON FLOOR STRUCTURE AT FR29 INSTALLED

Part: FLOOR SUPPORT — CRACKED (FRMS 18-24) · airframe 39,914 hrs · 27,297 cycles

CF1, CRACKS (3X) FOUND ON LH OMEGA BEAM #1 FLOOR STRUCTURE BTW FR18-24. LH OMEGA BEAM #1 BTW FR16-24 REMOVED FOR REPLACEMENT. NEW OMEGA BEAM #1 BTW FR16-24 INSTALLED

Part: GUSSET — CORRODED (FRMS 18-24) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF1, LH GUSSET #1 BTW FR 18-24 FOUND CORRODED. REMOVED AND REPLACED LH GUSSET #1 BTW FR 18-24 AND INSTALLED

Part: SKIN — CORRODED (FRM 61-62 S21L/R) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

RF1, CORROSION FOUND BELLY SKIN BTW FR 61-62 AND BTW STR 21L-21R AROUND DRAIN FITTINGS. BELLY SKIN FR61-62 STR 21L-21R REPAIRED

Part: SHEAR TIE — CRACKED (FRM 61 S6-7L) · airframe 39,914 hrs · 27,297 cycles

CF4, FRAME 61, LH SHEAR CLIP FOUND CRACKED BTW STR 6L-7L. LH SHEAR CLIP FR61 BTW STR 6L-7L REPLACED WITH NEW SHEAR CLIP.

Part: ANGLE — CORRODED (FRM 68) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

RF1, CARGO DOOR SURROUND STRUCTURE AFT L-SHAPE AT FR 68 FOUND CORRODED. RF1, CARGO DOOR SURROUND STRUCTURE AFT L-SHAPE AT FR68 FOUND OUT OF LIMITS. RF1, AFT L-SHAPE AT FR68 REPAIR COMPLETED AND INSTALLED.

Part: ANGLE — BENT (FRM 66) · airframe 39,914 hrs · 27,297 cycles

RF1, LH ANGLE POST CARGO DOOR ENTRANCE FLOOR STRUCTURE AT FR66 FOUND BENT. RF1, LH ANGLE POST CARGO DOOR ENTRANCE FLOOR STRUCTURE AT FR66 REMOVED FOR REPLACEMENT. LH ANGLE POST CARGO DOOR ENTRANCE NEW PART HOLES TRANSFERRED. LH ANGLE POST CARGO DOOR ENTRANCE NEW PART INSTALLED

Part: SHEAR TIE — CRACKED (FRM 16 S16-17R) · airframe 39,914 hrs · 27,297 cycles

CF1, FRAME 16 RH SHEAR CLIP FOUND CRACKED BTW STR 16R-17R. IN CF1 AT FR16 BTW STR 16R-17R. SHEAR CLIP REPLACED WITH MADE REPAIR PART LOCALLY FABRICATED.

Part: ANGLE — CRACKED (FRM 66) · airframe 39,914 hrs · 27,297 cycles

RF1, LH ANGLE CARGO DOOR ENTRANCE FLOOR STRUCTURE AT FR 66 FOUND CRACKED. RF1, LH ANGLE CARGO DOOR ENTRANCE DOOR STRUCTURE AT FR66 REMOVED FOR REPLACEMENT. LH ANGLE CARGO DOOR ENTRANCE AT FR66, NEW CARGO DOOR ENTRANCE AT FR66, NEW PART HOLES TRANSFERRED. LH CARGO DOOR ENTRANCE FLOOR STRUCTURE ANGLE AT FR 66, NEW PORT INSTALLED

Part: FLOOR SUPPORT — CRACKED (FRMS 29-36) · airframe 39,914 hrs · 27,297 cycles

CF2, CRACKS (3) FOUND ON LH OMEGA BEAM #3 FLOOR STRUCTURE BTW FR 29-36. AFTER NDT INSPECTION, CRACKS (3) CONFIRMED ON LH OMEGA BEAM #3 AT FR33, 34, AND 35. AT CF2, ON LH OMEGA BEAM #3 BTW FR 29-36 3X ANGLES REPAIR FABRICATED. AT CF2, ON LH OMEGA BEAM #3 AT FR33,34, AND 35 CRACK REMOVED. AT CF2, ON LH OMEGA BEAM #3 AT FR33, 34, 35 3X FILLERS FABRICATED AND 3X ANGLES REPAIR DRILLED. AT CF2, ON LH OMEGA BEAM #3, AT FR 33, 34, AND 35 3X ANGLES REPAIR AND 3X FILLER INSTALLED

Part: GUSSET — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AFTER REMOVAL OF LH GUSSET BTW FR 59-61, OMEGA BEAM FOUND CORRODED BTW FR60-61. LH OMEGA BEAM BTW FR 60-61, CUTOUT MADE FOR BEAM REPAIR. LH OMEGA BEAM REPAIRED BTW FR 60-61

Part: SHEAR TIE — CRACKED (FRM 61 S6-7R) · airframe 39,914 hrs · 27,297 cycles

CF4, FRAME 61, RH SHEAR CLIP FOUND CRACKED BTW STR 6R-7R. AT CF4, FR61, ON RH BTW STR 6R-7R SHEAR CLIP REMOVED FOR REPLACEMENT. AT CF4, FR 61 ON RH BTW STR 6R-7R SHEAR CLIP REPLACED

Part: GUSSET — CORRODED (FRMS 23-30) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CF II, CORROSION FOUND ON RH GUSSET #1 BTW FR 23 AND FR30 IN FLOOR STRUCTURE AREA. AT CFII, ON RH GUSSET #1 BTW FR 23-30 IN FLOOR STRUCTURE BLENDED OUT OF LIMIT. AT CFII RH GUSSET #1 BTW FR 23-30 IN FLOOR STRUCTURE AREA REMOVED FOR REPLACEMENT. AT CFII, ON RH GUSSET #1 BTW FR 23-30 IN FLOOR STRUCTURE AREA REPLACED.

Part: SHEAR TIE — CRACKED (FRM 72 S17-18L) · airframe 39,914 hrs · 27,297 cycles

AT RF1, FRAME 72, LH SHEAR CLIP U/FLOOR BTW STR 17L-18L FOUND CRACKED. AT RF1, ON FR 72, LH SHEAR CLIP U/FLOOR BTW STR 17L-18L REMOVED. AT RF1, ON FR72, LH SHEAR CLIP U-FLOOR BTW STR 17L-18L REPLACED.

Part: ANGLE — BENT (FRM 67) · airframe 39,914 hrs · 27,297 cycles

RF1, LH ANGLE POST CARGO DOOR ENTRANCE FLOOR STRUCTURE AT FR67 FOUND BENT. RF1, ANGLE POST CARGO DOOR ENTRANCE FLOOR STRUCTURE AT FR67 REMOVED FOR REPLACEMENT. RF1, LH ANGLE POST CARGO DOOR ENTRANCE AT FR67 NEW PART HOLES TRANSFERRED. RF1, LH ANGLE POST CARGO DOOR ENTRANCE AT FR 67 NEW PART INSTALLED

Part: FLOORBEAM — CRACKED (FRM 75 S14R) · airframe 39,914 hrs · 27,297 cycles

RF1, CRACK FOUND ON RH LOWER CROSSBEAM OF ELECTRIC RACK ASSY AT FR 75 STR 14R. RF1, RH LOWER CROSSBEAM OF ELECTRIC RACK REMOVED AND REPLACED

Part: BEAM — CORRODED (FRMS 65-68) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

RF1, LOWER BEAM OF CARGO DOOR SURROUND STRUCTURE BTW FR 65-68 FOUND CORRODED. RF1, LOWER BEAM OF CARGO DOOR SURROUND STRUCTURE BTW FR 65-68 LH REMOVED FOR ACCESS. BEAM SURROUND STRUCTURE BTW FR65-68 LH FOUND OUT OF LIMITS. RF1, LOWER BEAM DOOR SURRPUNT BTW FR 65-68 NEW PORT HOLES TRANSFERS. RF1, NEW LOWER BEAM DOOR SURROUND BTW FR 65-68 INSTALLED

Part: TEE ANGLE — CORRODED (FRM 68) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

RF1, CORROSION FOUND ON AFT T ANGLE LOWER CARGO DOOR SURROUND STRUCTURE AT FR68. RF1, AFT T ANGLE LOWER CARGO DOOR SURROUND STRUCTURE AT FR68 REMOVED FOR ACCESS. R-ANGLE AT FR68 FOUND OUT OF LIMITS. T-ANGLE A FR68 REPLACED

Part: DOUBLER — DAMAGED (LT ENG INTAKE) · airframe 39,914 hrs · 27,297 cycles

LH ENGINE AIR INTAKE REAR BULKHEAD TOP DOUBLER FROM COWL ALIGNMENT PIN DAMAGED. LH ENGINE AIR INTAKE REAR BULKHEAD TOP DOUBLER FOR COWL ALIGNMENT PAN REPAIR CARRIED OUT

Part: SHEAR TIE — CRACKED (FRM 60 S15-16L) · airframe 39,914 hrs · 27,297 cycles

CF4, FRAME 60, LH SHEAR CLIP FOUND CRACKED BTW STR 15L-16L. AT FRAME 60, LH BTW STR 15L-16L SHEAR CLIP REPLACED WITH MADE REPAIR PART LOCALLY FABRICATED

Part: FRAME — CRACKED (FRM 59 S15-16L) · airframe 39,914 hrs · 27,297 cycles

CF4, CRACK FOUND ON LH FRAME 59 AT FLOOR STRUCTURE BTW STR 15L-16L. FRAME REPAIRED

Part: FLOOR SUPPORT — CRACKED (FRMS 46-50) · airframe 39,914 hrs · 27,297 cycles

CF3, LH OMEGA BEAM WING STUB INBD ANGLE BTW FRAME 46-50 FOUND CRACKED. CF3, LH OMEGA BEAM WING INBD ANGLE BTW FR 46-50 REMOVED FOR REPLACEMENT. LH NEW ANGLES REPAIR BTW FR46-50 INSTALLED

Part: FLOOR SUPPORT — CRACKED (FRMS 46-50) · airframe 39,914 hrs · 27,297 cycles

CF3, LH OMEGA BEAM WING STUB OUTB ANGLE BTW FRAME 46-50 FOUND CRACKED. CF3, LH OMEGA BEAM WING STUB O/B ANGLE BTW FR46-50 REMOVED AND DISCARDED FOR REPLACEMENT. LH NEW ANGLE REPAIR BTW FR 46-50 INSTALLED

Part: FLOOR SUPPORT — CORRODED (FRMS 46-50) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF3, CENTER OMEGA BEAM WING STUB RH ANGLE BTW FR 46-50 FOUND CORRODED. ANGLE REPAIRED

Part: SHEAR TIE — CORRODED (FRM 61 S18-19L) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

RF1, FRAME 61, LH U/FLOOR SHEAR CLIP BTW STR 18L-19L FOUND CORRODED. REMOVED AND REPLACED

Part: FLOOR SUPPORT — CORRODED (FRMS 46-50) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF3, CENTER OMEGA BEAM WING STUB LH ANGLE BTW FRAME 46-50 FOUND CORRODED. ANGLE REPAIRED

Part: SHEAR TIE — CRACKED (FRM 15 S15-16R) · airframe 39,914 hrs · 27,297 cycles

CF1, FRAME 15, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. IN CF1 AT FR15, SHEAR CLIP BTW STR 15R-16R REPLACED WITH NEW ONE.

Part: SHEAR TIE — CRACKED (FRM 73 S16-17L) · airframe 39,914 hrs · 27,297 cycles

AT RF1, FRAME 73, LH SHEAR CLIP U/FLOOR BTW STR 16L-17L FOUND CRACKED. AT RF1, FRAME 73, LH U/FLOOR BTW STR 16L AND 17L REMOVED AND INSTALLED SHEAR CLIP.

Part: SHEAR TIE — CRACKED (FRM 80 S5-7L) · airframe 39,914 hrs · 27,297 cycles

AT RF2, FRAME 80, LH SIDE SHEAR CLIP BTW STR 5L-7L FOUND CRACKED. AT FR80, BTW STR 5L-7L LH SIDE SHEAR CLIP REMOVED FOR REPLACEMENT. AT FR80 BTW STR 5L-7L SHEAR CLIP REPLACED.

Part: SHEAR TIE — CORRODED (FRMS 80 S5-7R) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT RF2, FRAME 80, RH SIDE SHEAR CLIP BTW STR 5R-7R FOUND CORRODED. AT FR80 BTW STR 5R-7R RH SHEAR CLIP REMOVED FOR REPLACEMENT AT FR80 BTW STR 5R-7R RH SHEAR CLIP REPLACED

Part: FLOOR SUPPORT — CORRODED (FRMS 15-18) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF1, CORROSION FOUND ON BOTH MAIN DOOR LOWER FLOOR LH ANGLES U-SHAPE BTW FR 15-18. CORROSION ON BOTH MAIN DOOR FLOOR ANGLES U-SHAPE BLENDED OUT OF LIMITS. BOTH FLOOR ANGLES U-SHAPE BTW FR 15-18 REPLACED BY NEW ANGLES

Part: GUSSET — CORRODED (FRMS 29-36) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CF2, CORROSION FOUND ON LH GUSSET #3 BTW FR 29 AND FR 36 IN FLOOR STRUCTURE AREA. AT CF2, ON LH GUSSET #3 BTW FR 29 AND FR36 IN FLOOR STRUCTURE AREA CORROSION BLENDED OUT OF LIMITS. AT CF2, ON LH GUSSET #3 BTW FR 29 AND FR36 IN FLOOR STRUCTURE AREA REMOVED FOR REPLACEMENT. AT CF2, ON LH GUSSET #3 BTW FR29 AND FR36 IN FLOOR STRUCTURE AREA REPLACED

Part: FLOORBEAM — CORRODED (FRM 20) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF1, CORROSION FOUND ON MIDDLE ALLEY CROSSBEAM AT FR 20 ON FLOOR STRUCTURE AREA. MIDDLE ALLEY CROSSBEAM AT FR20 REMOVED FOR ACCESS, CF1, MIDDLE ALLEY CROSSBEAM AT FR20 BLENDED OUT OF LIMITS. CF1, MIDDLE ALLEY CROSSBEAM AT FR20 INSTALLED

Part: FLOOR SUPPORT — CORRODED (FRMS 20-22) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF1, CORROSION FOUND ON RH DOUBLERS FLOOR STRUCTURE AT FR 20 AND FR 22. IN CF1, ON RH SIDE, DOUBLERS AT FR 20+22 BLENDED AND FOUND OUT OF LIMIT. IN CF1, RH SIDE DOUBLERS AT FR 20+22 REPLACED WITH NEW ONE.

Part: SUPPORT — CORRODED (FRMS 18-24) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF1, LH SILL #1 BTW FR 18-24 FOUND CORRODED. IN CF1 LH SILL #1 BTW FR18-24 BLENDED AND FOUND OUT OF LIMIT. IN CF1, LH SILL #1 BTW FR 18-24 REPLACED

Part: GUSSET — CORRODED (FRMS 23-30) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CF2, CORROSION FOUND ON LH GUSSET #2 BTW FR 23 AND FR 30 IN FLOOR STRUCTURE AREA. CF2, LH GUSSET #2 BTW FR 23-30 CORROSION BLENDED AND FOUND OUT OF LIMITS. CF2, LH GUSSET #2 REPLACED

Part: FLOOR SUPPORT — CRACKED (FRMS 46-50) · airframe 39,914 hrs · 27,297 cycles

CF3, RH OMEGA BEAM WING STUB INBD ANGLE BTW FRAME 46-50 FOUND CRACKED. CF3, RH OMEGA BEAM WING STUB INBD ANGLE BTW FR 46-50 REMOVED FOR REPLACEMENT. CF3, RH OMEGA BEAM WING STUB INBD ANGLE BTW FR 46-50, PARTS DRILLED. CF3 RH OMEGA BEAM WING STUB INBD ANGLE BTW FR 46-50, REPLACED

Part: DOOR FRAME — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF1, CORROSION FOUND ON RH SERVICE DOOR FWD SILL FRAME BTW FR 18-20. IN CF1, RH SERVICE DOOR FWD SILL BTW FR 18-20 BLENDED AND FOUND OUT OF LIMITS. IN CF1 RH SERVICE DOOR SILL BTW FR 18-20 REMOVED AND REPLACED

Part: FLOOR SUPPORT — CRACKED (FRMS 35-39) · airframe 39,914 hrs · 27,297 cycles

CF3, CRACKS (2X) FOUND ON LH OMEGA BEAM #4 FLOOR STRUCTURE BTW FR 35-39. CF3, LH OMEGA BEAM #4 BTW FR 35-39 REMOVED FOR REPLACEMENT. CF3, LH OMEGA BEAM #4 BTW FR 35-39 REPLACED WITH NEW PART

Part: FLOOR SUPPORT — CRACKED (FRMS 23-30) · airframe 39,914 hrs · 27,297 cycles

CF2, CRACKS (5) FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BTW FR 23-30. CF2, L OMEGA BEAM #2 REMOVED FOR REPLACEMENT. CF2, LH OMEGA BEAM #2 REPLACED

Part: GUSSET — CORRODED (FRMS 29-36) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CFII, CORROSION FOUND ON RH GUSSET #2 BTW FR 29 AND FR 36 IN FLOOR STRUCTURE AREA. AT CFII, ON RH GUSSET #2 BTW FR29 AND FR30 IN FLOOR STRUCTURE AREA CORROSION BLENDED OUT OF LIMIT AND REMOVED FOR REPLACEMENT. AT CFII, ON RH GUSSET #2 BTW FR29 AND FR36 IN FLOOR STRUCTURE AREA REPLACED

Part: CHANNEL — CORRODED (FRMS 20-22) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF1, CORROSION FOUND ON RH SERVICE DOOR LOWER CHANNEL FRAME BTW FR20-22. RH SERVICE DOOR LOWER CHANNEL BTW FR 20-22 BLENDED AND FOUND OUT OF LIMIT. RH SERVICE DOOR LOWER CHANNEL BTW FR 20-22 REPLACED WITH NEW ONE.

Part: FLOOR SUPPORT — CORRODED (FRMS 18-22) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF1, CORROSION FOUND ON MIDDLE GUSSET FLOOR STRUCTURE BTW FR18-22. IN CFI CTR GUSSET BTW FR 18-22 BLENDED OUT OF LIMITS. IN CF1, CTR GUSSET BTW FR 18-22 REPLACED WITH NEW ONE

Part: BRACKET — CRACKED (FRM 10) · airframe 39,914 hrs · 27,297 cycles

AT FWD FUSE AREA, CRACK FOUND ON LH TOP BRACKET ON FR 10 UNDER SIDE COCKPIT WINDOW SURROUND STRUCTURE. LH TOP BRACKET ON FR10 REPLACED BY NW BRACKET

Part: BRACKET — CRACKED (LT PYLON) · airframe 39,914 hrs · 27,297 cycles

IN LH ENG PYLON, LH ENG PYLON STRUCTURE FWD PRECOOLER BRACKET IS CRACKED AND BENT. LH ENG PYLON STRUCTURE FWD PRECOOLER BRACKET REMOVED AND REPLACED

Part: SHEAR TIE — CRACKED (FRM 68 S6-9L) · airframe 39,914 hrs · 27,297 cycles

AT RF1, FRAME 68, LH SIDE SHEAR CLIP BTW STR 6L-9L FOUND CRACKED. AT RF1, FRAME 68, LH SIDE SHEAR CLIP BTW STR 6L-9L REMOVED AND REPLACED WITH NEW PART

Part: SHEAR TIE — CRACKED (FRM 73 S8-10R) · airframe 39,914 hrs · 27,297 cycles

AT RF1, FRAME 73, RH SHEAR CLIP U/FLOOR BTW STR 8R-10R FOUND CRACKED. AT RF1, FR73 RH SHEAR CLIP U/FLOOR BTW STR 8R-10R REMOVED AND REPLACED WITH NEW PART.

Part: FLOOR SUPPORT — CORRODED (FRMS 23-30) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CFII, CORROSION FOUND ON LH SILL #2 BTW FR 23 AND FR 30 IN FLOOR STRUCTURE AREA. LH SILL #2 BTW FR 23-FR30 BLENDED OUT OF LIMITS. LH SILL #2 REPLACEMENT. LH SILL #2 BTW FR 23-FR36 REPLACED

Part: SHEAR TIE — CRACKED (FRM 24 S15-16L) · airframe 39,914 hrs · 27,297 cycles

CF2, FRAME 24, LH SHEAR CLIP FOUND CRACKED BTW STR 15L-16L. LH SHEAR CLIP AT FR24 BTW STR 15L-16L REPLACED

Part: SHEAR TIE — CRACKED (FRM 26 S15-16L) · airframe 39,914 hrs · 27,297 cycles

CF2, FRAME 26, LH SHEAR CLIP FOUND CRACKED BTW STR 15L-16L. LH SHEAR CLIP AT FR 26 BTW STR 15L-16L REPLACED

Part: DOUBLER — CORRODED (FRM 49) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF3, RH DOUBLER ON FLOOR STRUCTURE AT FR 49 OVER OMEGA BEAM FOUND CORRODED. RH DOUBLER AT FR49 FLOOR STRUCTURE BLENDED OUT OF LIMITS. RH DOUBLER AT FR 49 REMOVED AND INSTALLED

Part: SHEAR TIE — CRACKED (FRM 26 S15-16R) · airframe 39,914 hrs · 27,297 cycles

CF2 FRAME 26, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. AT FR26, RH SHEAR CLIP BTW STR 15-16 REPLACED.

Part: FLOOR SUPPORT — CORRODED (FRMS 23-30) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CFII, CORROSION FOUND ON RH SILL #1 BTW FR 23 AND FR 30 IN FLOOR STRUCTURE AREA. CORROSION ON RH SILL #1 BTW FR 23-30 BLENDED OUT OF LIMITS. RH SILL #1 BTW FR 23-30 REMOVED FOR REPLACEMENT. NEW RH SILL #1 BTW FR 23-30 INSTALLED WITH RIVETS

Part: SHEAR TIE — CRACKED (FRM 24 S15-16R) · airframe 39,914 hrs · 27,297 cycles

CF2, FRAME 24, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. AR FR24 RH SHEAR CLIP BTW STR 15-16 REPLACED.

Part: SHEAR TIE — CRACKED (FRM 27 S15-16R) · airframe 39,914 hrs · 27,297 cycles

CF2, FRAME 27, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. AT FR27 BTW STR 15R-16R RH SHEAR CLIP REPLACED

Part: SHEAR TIE — CRACKED (FRM 25 S15-16R) · airframe 39,914 hrs · 27,297 cycles

CF2, FRAME 25, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. AT FR25 BTW STR 15-16 RH SHEAR CLIP REPLACED.

Part: UPLOCK — CRACKED (NLG WW) · airframe 39,914 hrs · 27,297 cycles

NLG W/WELL, CRACK FOUND ON NLG UP-LOCK AFT CROSSBEAM. REMOVED AND REPLACED

Part: FLOOR SUPPORT — CORRODED (FRM 35) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF2, RH DOUBLER ON FLOOR STRUCTURE AT FR35 OVER OMEGA BEAM FOUND CORRODED. RH DOUBLER ON FLOOR STRUCTURE AT FR35 BLENDED OUT OF LIMITS. RH DOUBLER AT FR35 REPLACED

Part: SUPPORT — CORRODED (FRMS 47-43) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CFIII, CORROSION FOUND ON RH SILL #5 BTW FR 47 AND FR53 IN FLOOR STRUCTURE AREA. RH SILL #5 BTW FR 47 AND FR 53 IN FLOOR STRUCTURE, CORROSION BLENDED AND FOUND OUT OF LIMIT. NEW RH SILL #5 INSTALLED

Part: FLOOR SUPPORT — CORRODED (FRMS 29-36) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CFII, CORROSION FOUND ON RH SILL #2 BTW FR 29 AND FR 36 IN FLOOR STRUCTURE AREA. RH SILL #2 BTW FR 29 AND FR 36 IN FLOOR STRUCTURE AREA, CORROSION BLENED AND FOUND OUT OF LIMITS. RH SILL #2 BTW FR 29 AND FR 36 REMOVED AND REPLACED.

Part: FLOOR SUPPORT — CORRODED (FRMS 35-42) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CFIII, CORROSION FOUND ON RH SILL #3 BTW FR35 AND FR42 IN FLOOR STRUCTURE AREA. RH SILL #2 BTW FR35 AND FR42 IN FLOOR STRUCTURE AREA BLENDED CORROSION AND FOUND OUT OF LIMIT. RH SILL #3 BTW 35 AND FR42 REMOVED AND INSTALLED WITH RIVETS.

Part: SUPPORT — CORRODED (FRMS 35-42) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CFIII, CORROSION FOUND ON LH SILL #4 BTW FR35 AND FR42 IN FLOOR STRUCTURE AREA. LH SILL #4 BTW FR35-FR42 BLENDED OUT OF LIMIT. LH SILL #4 BTW FR35-FR42 REPLACED

Part: FLOOR SUPPORT — CORRODED (FRMS 29-36) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CFII, CORROSION FOUND ON LH SILL #3 BTW FR 29 AND FR 36 IN FLOOR STRUCTURE AREA. LH SILL #3 BTW FR 29-FR36 BLENDED OUT OF LIMITS. LH SILL #3 BTW FR 29-FR36 REPLACED

Part: FLOOR SUPPORT — CORRODED (FRMS 41-48) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CFIII, CORROSION FOUND ON LH SILL #5 BTW FR 41 AND FR 48 IN FLOOR STRUCTURE AREA. LH SILL #5 BTW FR 41-FR48 BLENDED OUT OF LIMITS. LH SILL #5 BTW FR 41-FR48 REPLACED

Part: FLOOR SUPPORT — CORRODED (FRMS 47-53) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CFIII, CORROSION FOUND ON LH SILL #6 BTW FR 47 AND FR 53 IN FLOOR STRUCTURE AREA. LH SILL #6 BTW FR 47-FR53 BLENDED OUT OF LIMITS. LH SILL #6 BTW FR 47-FR53 REPLACED

Part: GUSSET — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF4, LH GUSSET IN TOILET AREA BTW FR59-61 FOUND CORRODED. CF4, LH GUSSET IN TOILET AREA BTW FR59-61 BLENDED AND FOUND OUT OF LIMIT. CF4, LH GUSSET IN TOILET AREA BTW FR59-61 REMOVED FOR REPLACEMENT. CF4, LH GUSSET IN TOILET AREA BTW FR59-61 INSTALLED.

Part: GUSSET — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF4, RH GUSSET IN TOILET AREA BTW FR 59-61 FOUND CORRODED. RH GUSSET IN TOILET AREA BTW FR 59-61 BLENDED OUT OF LIMITS. RH GUSSET BTW FR 59-61 REPLACED BY NEW GUSSET

Part: GUSSET — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

CF4, MIDDLE GUSSET IN TOILET AREA BTW FR59-61 FOUND CORRODED. IN CF4, CTR GUSSET BTW FR 59-61 BLENDED OUT OF LIMITS AND REMOVED FOR REPLACEMENT. IN CF4, CTR GUSSET BTW FR59-61 REPLACED WITH NEW ONE.

Part: GUSSET — CORRODED (FRMS 46) · corrosion level 2 · airframe 39,914 hrs · 27,297 cycles

AT CFIII, CORROSION FOUND ON LH GUSSET #5 BTW FR38 AND FR 46 IN FLOOR STRUCTURE AREA. IN CFIII, LH GUSSET #5 BTW FR 38-46 BLENDED AND FOUND OUT OF LIMIT. AT CFIII, LH GUSSET #5 BTW FR38 AND FR46 IN FLOOR STRUCTURE AREA REMOVED FOR REPLACEMENT. AT CFIII, LH GUSSET #5 BTW FR38-46 IN FLOOR STRUCTURE AREA INSTALLED

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 39,700 hrs · 27,098 cycles

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

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,051 hrs · 26,505 cycles

ICU CABIN AND CABIN EMERGENCY LIGHTS FAIL TO RESET. FOUND A BROKEN WIRE AT PLUG P8300 PIN 29. REPAIR THE WIRE. PERFORMED OPS CHECK. OPS CHECK SAT AT THIS TIME.

Part: NONE — NONE · airframe 38,658 hrs · 26,155 cycles

SMOKE COMING FROM SINK IN THE LAV ELECTRICAL BURNING SMELL. FOUND BOTH POT WATER DRAIN HEATERS WORKING NORMALLY. SUSPECT SINK DRAIN HEATER OR ASSOCIATED WIRING. PULLED AND COLLARED CB E-11. INSPECTED WIRING BEHIND AND UNDER LAV SINK COMPARTMENT AND FOUND SMELL FROM CALL SWITCH CIRCUIT BOARD. REMOVED AND REPLACED LAV ATTEND CALL SWITCH CIRCUIT BOARD. OPS CHECK SAT.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,471 hrs · 25,994 cycles

LH EXTERIOR FORWARD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT LAMP. OPS CHECK FAILED. TROUBLESHOT TO #1 EMERGENCY LIGHT BATTERY AND CHARGER ASSEMBLY INOPERATIVE. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY. REMOVED AND REPLACED #1 BPS CHARGER. OPS CHECK GOOD.

Part: NONE — NONE · airframe 37,524 hrs · 25,137 cycles

REMOVED BOTH PILOTS AND COPILOTS O2 MASKS BOX FOR FOM AND FOUND FITTINGS DISCONNECTED. RECONNECTED FITTINGS AND INSTALLED BOTH O2 MASK BOXES. OPS CHECK SAT

Part: NONE — NONE · airframe 37,524 hrs · 25,137 cycles

FWD LH EXTERNAL EMERGENCY LIGHT AS CONDENSATION IN THE LENS. REMOVED LENS AND DRIED CONDENSATION. RE-INSTALLED LENS.

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

RAD ALT 2, ANTENNA HAS SIGNS OF CORROSION. REMOVED AND REPLACED ANTENNA SUPPORT.

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

RAR #2 ANTENNA BASE HAS SIGNS OF CORROSION. REMOVED CORROSION AT RAR #2 ANTENNA BASE, FOUND CRACKS, CUTOUT DAMAGE AREA AND PERFORMED REPAIR. THIS REPAIR IS CONSIDERED TEMPORARY

Part: NONE — NONE · airframe 37,120 hrs · 24,791 cycles

BAG BAY CUTOUT TRAILING EDGE GOUGED. BLENDED OUT DAMAGED AREA AND EVALUTATED. FOUND TO BE OUT OF LIMITS. PERFORMED ET AND UT INSPECTION BY BARON NDT, LLC

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

RH VERTICAL PARTITION LOWER SILL ATTACH POINT HAS SIGNS OF CORROSION AT FASTENER HOLES. ACCOMPLISHED PERMANENT REPAIR. SPLICE DOUBLER FABRICATED. CORROSION LEVEL II.

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

LH OB FLOOR SILL SHOWS SIGNS OF CORROSION BETWEEN FRAMES 42-49. REMOVED AND REPLACED DAMAGE SILL BETWEEN FRAMES 42-49 LH SIDE

Part: NONE — NONE · airframe 37,120 hrs · 24,791 cycles

PAX DOOR LOWER FWD CORNER BENT. CUTOUT DAMAGE AREA, FABRICATED DOUBLER AND FILLER FROM 2024T3 .080". INSTALLED REPAIR PARTS AT PAX DOOR LOWER FWD CORNER.

Part: MOUNT — CORRODED (PARTITION) · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

RH VERTICAL PARTITION LOWER SILL ATTACH POINT HAS SIGNS OF CORROSION AT FASTENER HOLES. ACCOMPLISHED BEAM FUSELAGE !, FRAME 61 DOUBLER REPAIR AT RH VERTICAL PARTITION LOWER.

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

LH FLOOR SILL FROM FRM 53-59 HAS SIGNS OF CORROSION. REMOVED AND REPLACED FLOOR SILL FROM FR 53 TO 59. RESTORED FINISH AND APPLIED CIC

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

SIGNS OF CORROSION ON RH UPPER FLOOR BEAM TRACK SUPPORTS AFT OF FRM 52. REMOVED AND REPLACED BEAM, HAT ASSY FROM FR 49 - FR 55 RH

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

SIGNS OF CORROSION UNDER GUSSET CENTER AT HAT BEAM FR59-61, BLO. ACCOMPLISHED CENTER FUSELAGE IV-CF IV FLOOR STRUCTURE-OMEGA BEAM CORROSION PERMANENT REPAIR. HAT BEAM, CENTER FR59-FR61, BLO

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

LH AFT FUSELAGE, INTERIOR AT FR59-FR61 @ Y=479.0 HAS SIGNS OF CORROSION UNDER FLOOR BY LAV. REMOVED AND REPLACED LH FR 59 - FR 61 @ Y=479 GUSSET

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

SIGNS OF CORROSION UNDER GUSSET LH AT HAT BEAM FR59-61 BL-479. ACCOMPLISHED CENTER FUSELAGE IV-CF IV FLOOR STRUCTURE OMEGA BEAM, CORROSION PERMANENT REPAIR AT FR 59 AT FR61 BL479 L

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

AFT FUSELAGE INTERIOR, FR 59-61 C Y=0.0 HAS SIGNS OF CORROSION UNDER FLOOR BY LAV. REMOVED AND REPLACED GUSSET AT FR 59 - 61 CY=0.0

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

RH FLOOR SILL FROM FR 65-68 HAS SIGNS OF CORROSION. REMOVED AND REPLACED DAMAGE SILL AT FR 65-68 RH SIDE,

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

FLOOR BEAM DOUBLERS LOCATED AT STGR 15R BETWEEN FRM 20 & 22 SHOW SIGNS OF CORROSION ON HARDWARE HOLES. BLEND OUT CORROSION DOUBLER AT FR 22 FOUND TO BE IN LIMITS AND RESTORED FINISH. REMOVED AND REPLACED DOUBLER AT FR 20 RH.

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

LH OB FLOOR SILL SHOWS SIGNS OF CORROSION BETWEEN FRAMES 36-42. REMOVED AND REPLACED FLOOR SILL FRAME 36-42 LH OB SIDE

Part: NONE — NONE · corrosion level 2 · airframe 37,120 hrs · 24,791 cycles

REINFORCEMENT SILL SHOWS SIGNS OF CORROSION AFT OF SERVICE DOOR STARTING AT FRM 22. REPAIRED AREA AT AFT OF SERVICE DOOR STARTING AT FR 22. CORROSION LEVEL 2

Part: MUFFLER — FAILED (RECIRC FAN) · airframe 36,977 hrs · 24,652 cycles

COULD NOT COOL DOWN CABIN IN FLIGHT. ECS SHOWS 18C BUT FA COMPLAINS IT WAS TOO HOT. R/R #1 RECIRC FAN MUFFLER IAW EMB 145XR MM 21-24-02, OPS CK GOOD IAW EMB 145XR MM 21-51-00

Part: LIGHT — INOPERATIVE (MAIN DECK CARGO) · airframe 36,609 hrs · 24,320 cycles

MCD EMERGENCY LIGHT INOPERATIVE. R&R MCD EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.

Part: ARM — INCORRECT (MLG) · airframe 36,530 hrs · 24,254 cycles

LH AND RH MLG BOTH GREASE FITTINGS ON LOWER SIDE ARM FACING AFT. REMOVED AND INSTALLED LOWER SIDE ARM IN CORRECT ORIENTATION. PERFORMED GEAR SWINGS. OPS CHECK SAT.

Part: ARMREST — CRACKED (SEAT 19A) · airframe 36,309 hrs · 24,061 cycles

19A, 22A, 18A, 10A, 4A, & 2A PASSENGER SEATS ARMREST STRUCTURE IS CRACKED. R&R PASSENGER SEATS.

Part: LEVER — INOPERATIVE (MLG) · airframe 36,221 hrs · 23,987 cycles

LG LEVER DISAGREE DURING LG RETRACTION (3 GREEN REMAINED THE ENTIRE TIME). REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE, EXT/RET OPERATIONS CHECK GOOD WITH NO DEFECTS NOTED.

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 34,861 hrs · 22,742 cycles

ABORTED TAKE OFF IN LOW SPEED REGIME DUE TO ELECTRICAL SMOKE SMELL. NO OTHER SMOKE/FIRE INDICATION. SMELL PRESENT IN COCKPIT AND CABIN. FOLLOWED FIM 21-20-00-810-801-A. DID NOT NOTICE ANY ELECTRICAL OR OIL SMELL. SUSPECT SUSPICIOUS SMELL WAS DEICE FLUID INGESTION. PERFORMED ENGINE RUNS AT HIGH POWER SETTING WITH PACKS ON FOR SEVERAL MINUTES. NO SMELL NOTED.

Part: LIGHT — MISSING (CABIN) · airframe 34,294 hrs · 22,204 cycles

EMERGENCY FLOOR PATH STRIP WITH RED DOT AT MAIN CABIN DOOR IS MISSING. REPLACED MISSING FLOOR LUMINESCENT STRIP AT FWD MAIN CABIN DOOR. OPS CHECK SAT. NO OTHER DEFECTS NOTED.

Part: RECEPTACLE — CORRODED (WASTE SERVICE) · corrosion level 2 · airframe 33,756 hrs · 21,682 cycles

WASTE SERVICE PANEL RECEPTACLE HAS AREAS OF CORROSION AROUND DISCHARGE NOZZLE. REMOVED AND REPLACED WASTE SERVICE PANEL RECEPTACLE.

Part: PANEL — CORRODED (FRAME 65) · corrosion level 2 · airframe 33,756 hrs · 21,682 cycles

FR 65 PANEL Z HAS 7 EA AREAS OF CORROSION. REPAIRED FR 65 PANEL Z CORROSION BY BLEND OUT, FABRICATION INSTALLATION NEW DOUBLER ON PANEL Z FR 65.

Part: CONNECTOR — DISCONNECTED (LANDING GEAR) · airframe 33,248 hrs · 21,239 cycles

LG A/G FAIL MESSAGE ON LIFT OFF, COULDN’T RETRACT LANDING GEAR. FOUND CONNECTOR J0775 DISCONNECTED. PERFORMED OPS CHECK OF GEAR RETRACTION AND EXTENSION, AND OPS CHECK OF GEAR HANDLE. OPS CHECK SAT. NO DEFECTS NOTED.

Part: LIGHT — UNKNOWN (CABIN) · airframe 31,483 hrs · 19,509 cycles

EMERGENCY EXIT LIGHTS WILL NOT ARM. PERFORMED OPS CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,396 hrs · 19,428 cycles

EMERGENCY LIGHT ABOVE THE SERVICE DOOR WILL NOT TEST. R & R THE NR 2 EMERGENCY LIGHT BATTERY IAW 33-50-04, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,160 hrs · 19,187 cycles

EMERGENCY LIGHTS WILL NOT TURN ON. RECHARGED BATTERIES FOR EMERGENCY LIGHTS IAW AMM 33-50-08.

Part: SEAL — PEELING (COCKPIT WINDOW) · airframe 31,065 hrs · 19,090 cycles

LOUD WHISTLING NOISE COMING FROM FLT DECK AT CRUISE AT 20,000 FT, REDUCED TO A HISS WHEN DECENDING BELOW 10,000 FT. UPON INSPECTING THE SEALS FOUND 2 SPOTS PEELED OFF SEALS ON BOTH THE WINDOW SIDE AND AIRFRAME SIDE. SEALED THE SEALS. LEAK CHECK OF PILOTS DV WINDOW SAT. NO DEFECTS NOTED AT THIS TIME.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 31,063 hrs · 19,088 cycles

LAVATORY SMOKE ON EICAS RECEIVED DURING CLIMBOUT. PERFORMED HIGH POWER RUNS. NO SMOKE OR ODORS. NO SMOKE IN LAVATORY WITH BLEED ON BR OFF. ALL CHECKED GOOD. R & R THE LAVATORY SMOKE DETECTOR. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: SEAL — FAILED (COCKPIT WINDOW) · airframe 30,889 hrs · 18,926 cycles

FIRST OFFICER`S SIDE DV WINDOW SEAL BLEW OUT. REPAIRED THE SEAL. OP & LEAK CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,844 hrs · 18,880 cycles

SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE NR 2 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,907 hrs · 18,174 cycles

DURING C-CHECK STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 13 AND 14. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW SRM 53-00-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,907 hrs · 18,174 cycles

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

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,907 hrs · 18,174 cycles

DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 78) · airframe 23,255 hrs · 13,644 cycles

DURING A-CHECK INSPECTION, ACFT AFT SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 78 BELOW STRINGER 5R. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A FILLER-DOUBLER REPAIR IAW ETD2014-145-007155A, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — FAULTY (HORIZ STAB) · airframe 16,980 hrs · 9,436 cycles

FLT 4490 EWR-CREW REPORTED MAIN PITCH TRIM INOP ON EICAS DURING CLIMB AND PERFORMED AIR RETURN BACK TO EWR WITHOUT INCIDENT. EWR MX REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT BUT DID NOT FIX. EWR MX ALSO REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR IAW EMB145 AMM 27-40-02 WITH OPERATIONAL CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 15,926 hrs · 8,826 cycles

TYS - A/C WAS ABE TO ORD WHEN THE CREW GOT A WARNING INDICATION OF LAV SMOKE WITH SOME HAZE IN CABIN. A/C WAS FERRIED TO TYS WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW 145AMM 71-00-00. A/C WAS RELEASED AFTER OPS CHECKS AND LEAK CHECKS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,190 hrs · 7,154 cycles

SHV - DURING C-CHECK RT OMEGA BEAM CORRODED AT FR 23. REPAIRED RT OMEGA BEAM IAW EC 5320-01443. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,226 hrs · 4,413 cycles

SHV - DURING C CHECK LT OMEGA BEAM LOWER FLANGE HAS CORROSION BETWEEN FR 20-24. MX REPAIRED LT OMEGA BEAM BETWEEN FR 20-24 IAW EMB 145XR SRM 53-00-10. THE ACFT WAS APPROVED TO RETURN FOR SERVICE.

Part: BRACE — CORRODED (WING) · airframe 8,226 hrs · 4,413 cycles

SHV DURING C CHECK LT FWD SIDE BRACE WING FITTING BEARING HOUSING HAS SCRATCHES ON INTERNAL SURFACE AND PITTING CORROSION. MX R&R LT FWD SIDE BRACE WING FITTING. IAW EC5750-01369. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 7,575 hrs · 4,049 cycles

FLT MX - ONT - WHILE PERFORMING PRELIMINARY INSPECTION ON AIRCRAFT, QC PERSONNEL FOUND A FLOOR PROXIMITY LIGHTING SEGMENT MISSING AT 18BC. MX PERSONNEL INSTALLED A NEW PROXIMITY LIGHTING SEGMENT OPERATIONALLY CHECKED SATISFACTORY AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: BUTTON — DEFECTIVE (COCKPIT) · airframe 7,015 hrs · 3,752 cycles

FLT 0030 - MCI - FLIGHT CREW REPORTED NR 1 WING ANTI-ICE FAIL ON EICAS. FLIGHT DIVERTED FROM OMA TO MCI. MX PERSONNEL REMOVED AND REPLACED NR 1 WING ANTI-ICE PUSH BUTTON, OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN TO SERVICE.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 7,015 hrs · 3,752 cycles

FLT 0030 - MCI - FLIGHT CREW REPORTED NR 1 WING ANTI-ICE FAIL ON EICAS. FLIGHT DIVERTED FROM OMA TO MCI. MX PERSONNEL REMOVED AND REPLACED NR 1 WING ANTI-ICE PUSH BUTTON, OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN TO SERVICE.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 4,736 hrs · 2,530 cycles

CABIN CALL/ CABIN EMERGENCY AND PA SYSTEM NOT WORKING. VERIFIED NORMAL OPERATION CABIN EMERGENCY PA SYSTEM. NO SYTEMS FAULT FOUND.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 4,108 hrs · 2,191 cycles

FLT 54 - ONT - CREW REPORTED LAV SMOKE INDICATION ON EICAS. ONT MX REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB 145 AMM 26-14-01. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 4,108 hrs · 2,191 cycles

FLT 54 - ONT - CREW REPORTED LAV SMOKE INDICATION ON EICAS. ONT MX REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB 145 AMM 26-14-01. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.