N16147

Part: SKIN — DAMAGED · airframe 46,360 hrs · 31,011 cycles

SCREWS HOLES ELONGATED ON BOTH STARKE SPLICE SKIN. STARKE SPLICE SKIN (2X) FABRICATED.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

CF4, EXTERNAL POTABLE WATER DRAIN DOUBLER BTW FR 57-58 AND STR 19R-20R FOUND CORRODED. CF4 EXTERNAL POTABLE WATER DRAIN DOUBLER BTW FR 57-58 AND STR 19R-20R REMOVED FOR ACCESS, CORROSION BLENDED WITHIN LIMIT. AFTER INVESTIGATION, INTERNAL SKIN BTW FR 57-59 AND BTW STR 19R-29 FOUND CORROSION OUT OF LIMIT. INTERNAL SKIN BTW FR 57-59 AND BTW STR 19R-20R REPAIRED.

Part: RACK — CRACKED (ZONE 100) · airframe 46,360 hrs · 31,011 cycles

REAR FUSELAGE I AVIONIC COMPARTMENT, AT FR 75 AND STR 14R SUPPORT ON ELECTRIC RACK CRACKED. REAR FUSE I AVIONIC COMPARTMENT AT FR 75 AND STR 14R SUPPORT ON ELECTRIC RACK REMOVED AND REPLACED

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

CF3, SHEAR CLIP AT FR 52 BTW STR 21L-21R FOUND CORRODED. CF3, SHEAR CLIP ON FR52 BTW STR 21L-21R BOTH SHEAR CLIPS BLENDED AND FOUND OUT OF LIMIT. CF3, SHEAR CLIPS ON FR52 BTW STR 21-21R REMOVED AND INSTALLED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

LH FR 72 BTW STR 16L-17L SHEAR CLIP FOUND CRACKED. AT FR72 BTW STR 16L-17L SHEAR CLIP REMOVED FOR REPLACEMENT. AT FR72 BTW STR 16L-17L INSTALLED.

Part: ANGLE — CRACKED (WG-BDY FAIRING) · airframe 46,360 hrs · 31,011 cycles

RH WING TO BODY FAIRING, ANGLE #3 FOUND CRACKED. RH WING TO BODY FAIRING, ANGLE #3 REPLACED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

CF1, RH OMEGA BEAM FOUND CORRODED AT FR20 AND AT FR23. AFTER INVESTIGATION, NO CORROSION FOUND AT FR20, ONLY CORROSION FOUND AT FR23. AT CF1 FR23 RH OMEGA BEAM BLENDED OUT OF LIMITS. AT CF1 FR23 CUTOUT MADE ON RH OMEGA BEAM. REPAIR PART FABRICATED. AT CF1 FR23 REPAIR PART INSTALLED ON RH OMEGA BEAM

Part: SPAR — CRACKED (ZONE 600) · airframe 46,360 hrs · 31,011 cycles

RIGHT WING FRONT SPAR LOWER FLANGE CRACKED AT ONE HOLE. RT WING FRONT SPAR LOWER FLANGE REPAIRED WITH A DOUBLER.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

STRINGER 21R BTW FR 53-54 FOUND CORRODED. S21R BTW FR 53-54 CORROSION BLENDED AND STRINGER FOUND TO BE OUT OF LIMIT. S21R CUTOUT PERFORMED. S21L REPAIR PERFORMED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

LH FR 71 BTW STR 5L-6L SHEAR CLIP FOUND CRACKED. SHEAR CLIP FABRICATED AND INSTALLED

Part: HINGE FITTING — DAMAGED (ZONE 500 AILERON) · airframe 46,360 hrs · 31,011 cycles

INBD HINGE FITTING #1 NICKED ON LH AILERON. BUSHING REPAIRS AND ALTERNATE FASTENERS ON LH AILERON INBD FITTING.

Part: SKIN — DENTED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

DENT ON LH FWD FUSE I SKIN, BTW FR 6-7 AND ABOVE STR 15L, UNDER GPU ACCESS DOOR. ON LH FWD FUSE I SKIN, BTW FR 6-7 AND ABOVE STR 15L UNDER GPU ACCESS DOOR REPAIR PERFORMED.

Part: FRAME — CRACKED (ZONE 100) · airframe 46,360 hrs · 31,011 cycles

FR 59 LH FOUND CRACKED BTW STR 15L-16L. FR59 LH SPLICE REMOVED BTW STR15L-16L FOR REPAIR ACCESS. FR 59 LH BTW STR 15-16 REPAIRED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

SHEAR CLIP AT FR 59 AND BTW STR 15L-16L FOUND CRACKED. SHEAR CLIP AT FR 59 BTW STR 15L-16L REMOVED AND REPLACED

Part: ANGLE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

AT FR 59 LH ANGLE BTW FR 59 AND OMEGA BEAM FOUND CRACKED. AT FR59 LH ANGLE BTW FR 59 AND OMEGA BEAM REMOVED. AT FR59 LH ANGLE BTW FR 59 AND OMEGA BEAM REPLACED

Part: CUP — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

CF4, TOILET WASTE CUP EXTERNAL SIDE FOUND CORRODED. CF4 TOILET WASTE CUP BLENDED OUT OF LIMITS. TOILET WASTE CUP REMOVED AND REPLACED

Part: PARTITION — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

RIGHT FR 61 FRAME PARTITION FOUND CORRODED AT FLOOR LEVEL. RT FR 61 FRAME PARTITION BLENDED, FOUND OUT OF LIMIT. RT FR 61 FRAME PARTITION REMOVED AND REPLACED.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

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

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

SHEAR CLIP AT FR 58 AND BTW STR 20R-21R FOUND CORRODED. SHEAR CLIP AT FR 58 AND BTW STR 20R-21R REMOVED AND REPLACED

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

CARGO DOOR CUT-OUT BTW FR 65-68 LOWER BEAM FOUND CORRODED. ON CARGO DOOR CUT-OUT BTW FR 65-68 LOWER BEAM REMOVED AND REPLACED

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

LH OMEGA BEAM AT FR 59-61 FOUND CRACKED AT 2 ANCHOR NUT LOCATION. LH OMEGA BEAM AT FR 59-61 CUTOUT AT 2 ANCHOR NUT LOCATION. LH OMEGA BEAM BTW FR 59-61 REPAIRED

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

STR 20 RH AT FR 58 FOUND CORRODED. STR 20R CORROSION FOUND ON STRINGER AT FR 59 ALSO. STR 20R, BLENDED AND FOUND OUT OF LIMIT. STR 20R BTW FR 57-60 REMOVED AND REPLACED

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

SHEAR CLIP AT FR 59 AND BTW STR 19R-20R FOUND CORRODED. SHEAR CLIP AT FR59 AND BTW STR 19R-20R REMOVED AND INSTALLED

Part: PARTITION — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

LEFT FR 61 FRAME PARTITION FOUND CORRODED AT FLOOR LEVEL. LT FR 61 FRAME, PARTITION REMOVED AND REPLACED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

RH FR 73 BTW STR 8R-10R SHEAR CLIP FOUND CRACKED. CRACKED SHEAR CLIP AT RH FR 73 BTW STR 8R-10R REMOVED AND REPLACED

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

SHEAR CLIP AT FR 59 AND BTW STR 20R-21R FOUND CORRODED. SHEAR CLIP AT FR 59 AND BTW STR 20R-21R BLEND OUT OF LIMITS. SHEAR CLIP REMOVED AND REPLACED.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

LOWER SIDE WINDOW CUT-OUT AREA, RH FR10 ANGLE FOUND CRACKED. AT LOWER SIDE WINDOW CUT-OUT AREA, RH FR10 ANGLE REMOVED AND REPLACED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

IN REAR COMPARTMENT, BULKHEAD 80, LH SHEAR CLIP CRACKED BETWEEN STRINGER 9 AND STRINGER 11. IN REAR COMPARTMENT BULKHEAD 80 LH SHEAR CLIP BTW STRINGER 9 AND STRINGER 11 REPLACED.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

CF1 BTW FR 15-16 AND BTW 7R-9R SUPPORT ASSY CRACKED. CF1 BTW FR 15-16 INBD BTW STR 7R-9R SUPPORT ASSY REMOVED AND REPLACED

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

CARGO DOOR CUT-OUT STRUCTURE, LH FR 65 AT FLOOR LEVEL BRACKET FOUND CORRODED. ON CARGO DOOR CUT-OUT STRUCTURE, LH FR 65 AT FLOOR LEVEL BRACKET REMOVED AND INSTALLED

Part: FRAME — CRACKED (ZONE 100) · airframe 46,360 hrs · 31,011 cycles

CF2, FR25 BTW STR 15R-16R FOUND CRACKED. CF2 FR 25 BTW STR 15R-16R CUT OUT PERFORMED. FR25 BTW STR 15R-16R PART FABRICATED. CF2 FR25 BTW STR 15R-16R REPAIRED.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

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

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

CF4, SHEAR CLIP AT FR54 BTW STR 21L-21R FOUND CORRODED. SHEAR CLIP FABRICATED AND INSTALLED.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 46,360 hrs · 31,011 cycles

SHEAR CLIP FR 65 BTW STR 17L-16L CRACKED. SHEAR CLIP AT FR65 BTW STR 17L-16L REMOVED AND INSTALLED

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

INT SKIN BTW FR 61-62A AND STR 21L-19R FOUND CORRODED. REPAIR DOUBLER PERFORMED ON REAR FUSELAGE I RH LOWER SKIN AT FR62 AND BTW STR 19R-20R.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

CF2 LH SHEAR CLIP FR 28 BTW STR 15L-16L CRACKED. CF2 LH SHEAR CLIP FR28 BTW STR 15L-16L REMOVED AND REPLACED

Part: INLET — DAMAGED (ZONE 400) · airframe 46,360 hrs · 31,011 cycles

RH ENGINE AIR INTAKE, BLENDED SPOT TO BE INVESTIGATED. REPAIR DOUBLER ON RH NACELLE AIR INLET MODULE INNER SKIN.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

LH FR 67 BTW STR 6L-7L SHEAR CLIP FOUND CRACKED. LH SHEAR CLIP AT FR67 BTW STR 6L-7L REMOVED AND REPLACED.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

CF4, SHEAR CLIP AT FR 53 BTW STR 21L-21R FOUND CORRODED. CF4, SHEAR CLIPS ON FR53 BTW STR 21L-21R, BOTH SHEAR CLIPS BLENDED AND FOUND OUT OF LIMIT. AT CF4, BOTH SHEAR CLIPS ON FR53 BTW STR 21L-21R REMOVED AND INSTALLED.

Part: SKIN — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

RF1 FUSE SKIN AT FR75 AND AT STR 2L CRACKED. SKIN AT FR75 AND AT STR 2L PAINT STRIPPED. CUT-OUT AT FR75 CRACKED LOCATION PERFORMED. SKIN AT FR75 AND AT STR 2L REPAIRED.

Part: ANGLE — CRACKED (ZONE 800) · airframe 46,360 hrs · 31,011 cycles

RH INTERNAL STRUCTURE BTW FR 67-68 AND STR 4R-5R. CARGO DOOR MECHANISM MIDDLE ANGLE FOUND CRACKED. RH INTERNAL STRUCTURE BTW FR 67-68 AND STR 4R-5R CARGO DOOR MECH MIDDLE ANGLE REPLACED ,

Part: ANGLE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

RH INTERNAL STRUCTURE BTW FR 61-62 AND STR 4R-5R, ANGLE FOUND CRACKED. RH INTERNAL STRUCTURE BTW FR 61-62 AND STR 4R-5R ANGLE REMOVED AND REPLACED.

Part: DOUBLER — MISINSTALLED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

CTR FUSELAGE I, UNRECORDED REPAIR DOUBLER FOUND ON UPPER SKIN PANEL BTW FR16-17 AND STR 3R-4R. CTR FUSELAGE, UNRECORDED REPAIR DOUBLER REMOVED. CTR FUSELAGE 1 PATCH REPAIR MADE BTW FR 16-17 AND STR 3R-4R CTR FUSELAGE 1 PATCH REPAIR INSTALLED BTW FR 16-17 AND STR 3R-4R

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

CF2 RH SHEAR CLIP FR24 BTW STR 15R-16R CRACKED. CF2 RH SHEAR CLIP FR24 BTW STR 15R-16R REMOVED AND INSTALLED

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 46,360 hrs · 31,011 cycles

FR72 BTW STR 17L-18L SHEAR CLIP FOUND CRACKED. FR72 BTW STR 17L-18L SHEAR CLIP REPLACED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

CF2 RH SHEAR CLIP FR25 BTW STR 16R-17R CRACKED. CF2 RH SHEAR CLIP FR 25 BTW STR 16R-17R REMOVED AND REPLACED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

CF2 RH SHEAR CLIP FR25 BTW STR 15R-16R CRACKED. CF2 RH SHEAR CLIP FR25 BTW STR 15R-16R REMOVED AND INSTALLED.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 46,360 hrs · 31,011 cycles

SHEAR CLIP AT FR58 AND BTW STR 15L-16L FOUND CRACKED. SHEAR CLIP AT FR58 AND BTW STR 15L-16L REMOVED AND INSTALLED

Part: PROFILE — CRACKED (ZONE 300) · airframe 46,360 hrs · 31,011 cycles

BOTTOM OF VERT STAB, AFT OF REAR SPAR 3, RH PROFILE CRACKED AT LOWER SECTION. BOTTOM OF VERT STAB AFT OF REAR SPAR 3 RH PROFILE CRACK BLENDED. BOTTOM OF VERT STAB AFT OF REAR SPAR 3 RH AT LOWER SECTION WAS REPAIRED AND INSTALLED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

LH FR 66 BTW STR 6L-7L SHEAR CLIP FOUND CRACKED. LH FR 66 BTW STR 6L-7L SHEAR CLIP REMOVED AND INSTALLED

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

FWD AND AFT DIGITAL PLATE JOINT ANGLES FOUND CRACKED AT CENTER OMEGA BEAM INBD AND OUTBD SIDE ON LH OMEGA BEAM INBD SIDE. FWD AND AFT DIGITAL PLATE JOINT ANGLES AT CENTER OMEGA BEAM AND LH OMEGA BEAM JOINT ANGLE REPLACED.

Part: CABLE — OUT OF LIMITS (STICK PUSHER) · airframe 46,360 hrs · 31,011 cycles

STICK PUSHER CABLE CHAFED OUT OF LIMIT. STICK PUSHER ACTUATOR REMOVED. STICK PUSHER ACTUATOR INSTALLED.

Part: SUPPORT — CRACKED (ZONE 200) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

LH SILL BTW FR 61-65 FOUND CORRODED. LH SILL BTW FR 61-65 BLENDED FOUND OUT OF LIMIT. LH SILL BTW FR 61-65 REMOVED AND REPLACED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

CF2 RH SHEAR CLIP FR26 BTW STR 15R-16R CRACKED. CF2 RH SHEAR CLIP FR 26 BTW STR 15R-16R REMOVED AND INSTALLED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

CF2 LH SHEAR CLIP FR24 BTW STR 15L-16L CRACKED. CF2 LH SHEAR CLIP AT FR 24 BTW STR 15L-16L REMOVED AND REPLACED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

LH FR 68 BTW STR 6L-9L, SHEAR CLIP FOUND CRACKED. LH FR 68 BTW 6L-9L STR SHEAR CLIP REMOVED AND INSTALLED

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

CF2 LH SHEAR CLIP FR26 BTW STR 15L-16L CRACKED. CF2 LH SHEAR CLIP FR 26 BTW STR 15L-16L REMOVED AND REPLACED

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

INBD ANGLE BTW WING STUB AND CENTER OMEGA BEAM FOUND CORRODED BTW FR 46 TO FR 50. BTW FR 46-50, INBD ANGLE BTW WING STUB AND CENTER OMEGA BEAM FOUND OUT OF LIMITS. INBD ANGLE BTW WING STUB AND CENTER OMEGA BEAM, BTW WING STUB AND CENTER OMEGA BEAM, BTW FR46 TO FR50 REPLACED.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

RH FR 71 BTW STR 6R-10R, SHEAR CLIP FOUND CRACKED. RH FR 71 BTW STR 6R-10R, SHEAR CLIP REMOVED AND INSTALLED

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

LH GUSSET 4 BTW FR 35-39 FOUND CORRODED. LH GUSSET 4 BTW FR 35-39 BLENDED AND FOUND WITHOUT LIMIT. LH GUSSET 4 BTW FR 35-39 REMOVED AND REPLACED. LH PASSENGER SEAT TRACK BTW FR 35-39 OVER GUSSET WERE REMOVED AND INSTALLED

Part: TOILET — CORRODED (ZONE 900) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

TOILET CUP PROFILE Z FOUND CORRODED. TOILET CUP PROFILE Z BLENDED OUT OF LIMITS. TOILET CUP PROFILE Z REMOVED AND REPLACED

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

RH SILL 3 BTW FR 35-42 FOUND CORRODED. BTW FR 35-42 RH SILL 3 BLENDED OUT OF LIMITS. BTW FR 35-42 RH SILL #3 REMOVED AND REPLACED

Part: PROFILE — CORRODED (ZONE 900) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

TOILET CUP PROFILE Z FOUND CORRODED. TOILET CUP PROFILE Z BLENDED OUT OF LIMITS, TOILET CUP PROFILE Z REMOVED AND REPLACED

Part: SUPPORT — CORRODED (ZONE 10) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

RH SILL BTW FR53-59 CORRODED. BTW FR 53-59 RH SILL BLENDED OUT OF LIMITS. RH SILL BTW FR 53-59 REMOVED AND REPLACED.

Part: ANGLE — CRACKED (ZONE 200) · airframe 46,360 hrs · 31,011 cycles

CF1, ANGLE ON INBD SIDE OF LH OMEGA BEAM BTW FR 19-20 FOUND CRACKED. CF1 ANGLE ON INBD SIDE ON LH OMEGA BEAM BTW FR 19-20 REMOVED AND REPLACED

Part: SHEAR TIE — CRACKED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

SHEAR CLIP AT FR60 BTW STR 19R-20R FOUND CORRODED. SHEAR CLIP AT FR60 BTW STR 19R-20R BLENDED OUT OF LIMITS. SHEAR CLIP AT FR 50 BTW STR 19R-20R REMOVED AND INSTALLED

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

SHEAR CLIP AT FR61 BTW STR 19R-20R FOUND CORRODED. SHEAR CLIP AT FR61 BTW STR 19R-20R BLENDED OUT OF LIMITS. SHEAR CLIP AT FR61 BTW STR 19R-20R DRILLED NEW HOLES IN NEW SHEAR CLIP. INSTALLED NEW SHEAR CLIP AT FR61.

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

CF1, CHANNEL BTW FR20-22 AT SERVICE DOOR LOCATION FOUND CORRODED. CF1, CHANNEL BTW FR 20-22 AT SERVICE DOOR BLENDED OUT OF LIMIT. REPAIR PART FABRICATED. AT CF1, CHANNEL BTW FR 20-22 AT SERVICE DOOR, REPAIR PART INSTALLED.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 46,360 hrs · 31,011 cycles

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

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

CF1, CENTER OMEGA BEAM GUSSET BTW FR 18-23 FOUND CORRODED. AT CF1 CENTER OMEGA BEAM GUSSET BTW FR 18-23 BLENDED OUT OF LIMIT. AT CF1 CENTER OMEGA BEAM GUSSET BTW FR 18-23 REMOVED AND REPLACED

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

CF1, ANGLE ON INBD SIDE OF CENTER OMEGA BEAM BTW FR18-20 FOUND CORRODED. AT CF1 ANGLE ON INBD SIDE OF CENTER OMEGA BEAM BTW FR18-20, ANGLE REMOVED. AT CF1 ANGLE ON INBD SIDE OF CENTER OMEGA BEAM BTW FR 18-20 FOUND CORRODED OUT OF LIMIT. DRILLED NEW HOLES FOR NEW SUPPORT ANGLE. AT CF1 CENTER OMEGA BEAM BTW FR18-20 REPLACED SUPPORT ANGLE ON INBD SIDE.

Part: FAIRING — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

CORROSION FOUND AROUND LH, RH EXTERNAL EMERGENCY LIGHTS ON FWD BODY FAIRING. FWD BODY FAIRING LIGHTS FROM FAIRING PLATE REMOVED, CORROSION REMOVED OUT OF LIMITS. FWD BODY FAIRING PLATE NEW DRILLED. FWD BODY FAIRING PLATE AND LIGHT EMERGENCY INSTALLED.

Part: DOOR FRAME — FOD (ZONE 200) · airframe 45,515 hrs · 30,198 cycles

MCD TAKES EXCESSIVE EFFORT TO OPENING AND CLOSING. REMOVED DEBRIS FROM DOORWAY AND CLEANED AND LUBED MCD STOPS. OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (MAIN DOOR) · airframe 45,328 hrs · 30,011 cycles

MAIN CABIN DOOR HARD TO OPEN/CLOSE. LUBED MAIN CABIN DOOR ROLLERS. OPS CHECK GOOD.

Part: CONTROL UNIT — INOPERATIVE (TE FLAPS) · airframe 45,159 hrs · 29,841 cycles

FLAP FAIL MESSAGE WHEN PERFORMING CLIMB CHECK AT 1300 AFTER MOVING FLAP LEVER FROM 9 TO 0 DEGREES. ON POST WALK AROUND FLAPS ARE STILL AT 9 DEGREES, SPEED WHEN THE FLAP FAIL OCCURRED WAS AROUND 160 TO 170 KNOTS. FOUND RH TRANSMISSION FAIL ON CMC. PERFORMED FIM. NO FAULTS FOUND. WHEN POWERING AIRCRAFT FLAP FAIL ON EICAS, USED FLAP BREAKOUT BOX AND FOUND FECU TO BE FAULTY. REMOVED AND REPLACED FECU. OPS CHECK SAT. NO DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,576 hrs · 29,306 cycles

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

Part: PDU — FAILED (TE FLAPS) · airframe 44,480 hrs · 29,212 cycles

FLAP FAIL ON APPROACH TO LANDING WHEN SELECTING FLAP 45. PERFORMED TROUBLESHOOTING WITH BREAKOUT BOX GSE 398, CODES SENT TO ENGINEERING, ADVISED TO PERFORMED 0 DEG FLAP RIGGING, WHEN ACTUATING FLAPS NOTICE FFS (FLAP FLEXIBLE SHAFT) NR 5 ON RT SIDE HAVING SOME VIBRATION. R & R RT FFS NR 5, PERFORMED FLAP ZERO DEGREE RIGGING, NO DEFECTS NOTED, ACTUATED FLAP 10 TIMES FROM 0 TO 45, NO DEFECTS NOTED OR MESSAGES. PERFORMED REMOVAL AND INSTALL FPDU ON WING STUB STRUCTURE. INISHED FPDU INSTALLATION, INSTALLED FFS#1 ON RH AND LH SIDE OF FPDU. PERFOMED OPS CHECK 5 CYCLES , OPS CHECK SAT, NO DEFECTS NOTED

Part: CHARGER — INOPERATIVE (UNKNOWN) · airframe 44,080 hrs · 28,858 cycles

MCD EMERGENCY LIGHT AND LH WING LOWER EMERGENCY LIGHTS OUT. REMOVED AND REPLACED BPS #1. OPS CHECK FAIL. LIGHTS TURN ON BUT DIM RAPIDLY AND TURN OFF. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 44,061 hrs · 28,838 cycles

MCD EMERGENCY LIGHT AND LH WING LOWER EMERGENCY LIGHTS OUT. REMOVED AND REPLACED BULB ON MCD. OPS CHECK FAIL. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY. OPS CHECK SAT

Part: BATTERY PACK — BURNED OUT (UNKNOWN) · airframe 44,005 hrs · 28,783 cycles

FOUND LH OVERWING EMERGENCY LIGHT BURNT. REMOVED AND REPLACED BATTERY POWER SUPPLY #1 FOR THE LH FWD LWR FAIRING EXTERNAL EMERGENCY LIGHT. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 43,918 hrs · 28,686 cycles

FOUND EMERGENCY MARKER EXIT MAIN DOOR AND COCKPIT STEP INOPERATIVE. REMOVED AND REPLACED NUMBER 1 EMERGENCY LIGHT BATTERY. LIGHT OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 43,840 hrs · 28,617 cycles

FOUND LH FORWARD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND OPS CHECK. OPS CHECK FAIL. FOUND EMERGENCY LIGHT BPS ONE CHARGER AND BATTERY BURNT. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY. OPS CHECK SAT.

Part: ENGINE — FAILED (NR 2) · airframe 42,523 hrs · 27,443 cycles

#2 ENGINE FAILURE AT CRUISE. REMOVED AND REPLACED RH ENGINE. OPS AND LEAK CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE · airframe 41,996 hrs · 26,988 cycles

FOUND BOTH RH AND LH ESCAPE HATCH EXIT IDENTIFIER SIGN LIGHTS NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY #3. OPS CHECK SAT

Part: NONE — NONE · airframe 41,870 hrs · 26,870 cycles

BLEED 2 LEAK ON EICAS AND OVERHEAD PANEL. INSPECTED PACK 2. FOUND LARGE SLEEVE CONNECTED TO DUAL TEMP CONTROL VALVE NOT FULLY ON TUBE BUT NOT LEAKING. RE-SECURED LARGE SLEEVE CONNECTED TO DUAL TEMP CONTROL VALVE. PERFORMED COOLING PACK SYSTEM OPS TEST. OPS TEST SAT. NO LEAKS PRESENT. OUTFLOW VALV TOOLING REQUIRES REMOVAL. OUTFLOW VALVE REMOVED. COMPLIED WITH BLEED LEAK CHECK OF #2 PRE COOLER WITH ENGINE RUN "NO LEAKS FOUND".

Part: LAMP — INOPERATIVE · airframe 41,632 hrs · 26,661 cycles

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

Part: NOT REPORTED — NOT REPORTED · airframe 41,366 hrs · 26,432 cycles

CORROSION - "Y" - 18 AT FR 23 THRU FR 29 +5 OMEGA BEAM I/B LWR FLANGE - MULTIPLE LOCATIONS. REMOVED AND REPLACED OMEGA BEAM AT FR 23 - FR 29 +5"

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 41,366 hrs · 26,432 cycles

REAR FUSELAGE SKIN HAS CORROSION UNDER RAT #2 ANTENNA BASE. CUT OUT DAMAGE ON EXTERNAL SURFACE OF FUSELAGE SKIN AT RAT #2 ANTENNA LOCATION AND INSTALLED REPAIR DOUBLER, FILLER AND SHIM

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 41,366 hrs · 26,432 cycles

REAR FUSELAGE SKIN HAS CORROSION UNDER RAR #2 ANTENNA BASE. CUT OUT DAMAGE AT RAR #2 FR68-69 STR 21L-21R AND INSTALLED REPAIR DOUBLER AND FILLER

Part: NOT REPORTED — NOT REPORTED · airframe 41,366 hrs · 26,432 cycles

CARGO DOOR INNER LOWER SKIN HAS SEVERAL AREAS OF DAMAGE (CHAFING AND GOUGES). REMOVED AND REPLACED CARGO DOOR INNER LOWER SKIN

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 41,366 hrs · 26,432 cycles

LH OVERWING EXIT HATCH HAS CORROSION ON LOWER FRAME UNDER RUBBER STOP. REMOVED AND REPLACED BEAM 4 ON LH OVER WING EXIT HATCH

Part: NOT REPORTED — NOT REPORTED · airframe 41,366 hrs · 26,432 cycles

CARGO DOOR LOWER OUTER FRAME HAS SEVERAL AREAS OF DAMAGE (CHAFING AND GOUGES). REMOVED AND REPLACED CARGO DOOR LOWER OUTER FRAME PROFILE

Part: NONE — NONE · airframe 41,363 hrs · 26,431 cycles

BIRD STRIKE. PERFORMED SECTION 1: TEMPORARY REPAIR TO FWD FUSELAGE SKIN.

Part: NONE — NONE · airframe 41,154 hrs · 26,252 cycles

PHOTO LUMINESCENT FLOOR EMERGENCY LIGHT STRIP NEAR GALLEY IS FADED. REMOVED AND REPLACED PHOTO LUMINESCENT EMERGENCY LIGHT STRIP NEAR GALLEY. OPS CHECK SAT

Part: BALLAST — MELTED (CABIN LIGHTS) · airframe 41,115 hrs · 26,216 cycles

SMELL OF INSULATION BURNT IN CABIN APPROX HALF WAY UP FOUND PLASTIC BULB SOCKET ON CEILING LIGHT BALLAST AT SEAT 18A MELTED. REMOVED AND REPLACED HARNESS ASSEMBLY ELECTRICAL. OPS CHECK SAT.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,360 hrs · 31,011 cycles

RH GUSSET BTW FR 59-61 FOUND CORRODED. RH GUSSET BTW FR 59-61 FOUND CORRODED OUT OF LIMIT. RH GUSSET BTW FR59-61 REMOVED AND REPLACED

Part: CONTROL UNIT — INOPERATIVE (PITCH TRIM) · airframe 40,431 hrs · 25,618 cycles

PITCH TRIM MAIN INOPERATIVE. R&R HSCU. OPS CHECK SAT. PERFORMED HOR STAB ELECTRICAL/ELECTONIC OPS. NO DEFECTS NOTED. PERFORMED TROUBLESHOOTING, APPEARS TO BE TRANSITORY CONDITION.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,359 hrs · 25,559 cycles

EMERGENCY LIGHT AT MAIN DOOR ENTRY WILL NOT ILLUMINATE. R&R #1 EMERGENCY LIGHT INVERTER. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: SENSOR — FALSE ACTIVATION (BRAKE TEMP) · airframe 40,096 hrs · 25,318 cycles

BRAKE OVERHEAR INDICATION ON EICAS DURING CLIMB OUT. LT INBOARD BRAKE TEMP IN MAX RANGE. REMOVED AND REPLACED LT INBOARD BRAKE TEMP SENSOR. OPERATIONS CHECK SATISFACTORY. RECONNECTED CANNON PLUG P1077.

Part: LIGHT — DIM (EXTERIOR EMER) · airframe 40,085 hrs · 25,308 cycles

MCD EXTERNAL EMERGENCY LIGHT VERY DIM. R & R MCD EXTERNAL EMERGENCY LIGHT. OPERATIONS CHECKS SATISFACTORY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,776 hrs · 25,042 cycles

EMERGENCY LIGHTS FOR REAR WINDOWS EXIT ARE INOPERATIVE. TWO ON THE RIGHT SIDE, ONE ON THE BOTTOM LIGHT. REMOVED AND REPLACED EMERGENCY LIGHT NR 3 BATTERY POWER SUPPLY. OPS CHECK COMPLETED, BUT LEFT SIDE EXIT IDENTIFIER SIGN ON REAR WINDOW EXIT WOULD NOT TURN ON. REMOVED AND REPLACED LEFT SIDE EXIT IDENTIFIER SIGN ON THE REAR WINDOW EXIT. OPS CHECK COMPLETED. ALL LIGHTS ARE WORKING.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 39,651 hrs · 24,919 cycles

MULTIPLE INTERIOR EMERGENCY LIGHTS INOPERATIVE. CHARGED THE EMERGENCY LIGHT BATTERIES WITH THE AIRCRAFTS DC POWER SUPPLY. OPERATIONS CHECK SATISFACTORY.

Part: DUCT — BLOWN (NR 2 A/C PACK) · airframe 39,634 hrs · 24,899 cycles

BLEED 1 LEAK MESSAGE ON EICAS. PERFORMED OPS CHECK OF THE DISTRIBUTION SYSTEM. OPS CHECK FAILED. PERFORMED GVI OF #1 AND #2 PACKS, FOUND BLOWN DUCT ON THE #2 PACK. NEW DUCT AND CLAMP REQUIRED. R&R FWD UPPER COUPLING ON #2 DUEL TEMP CONTROL VALVE. OPS CHECK SAT.

Part: PROXIMITY SWITCH — FAILED (MLG) · airframe 38,509 hrs · 23,889 cycles

LG AIR/GROUND FAIL ON EICAS ON SHORT FINAL. PERFORMED CMC DOWNLOAD. FOUND LEFT WOW PROX SWITCH FAIL MESSAGE. R&R AFT & FWD MLG WOW PROX SWITCH. R&R LGEU. OPS CHECK SAT. NO LG AIR/GROUND FAIL MESSAGE ON EICAS.

Part: WIRE — BROKEN (EXTERIOR LIGHT) · airframe 37,769 hrs · 23,184 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE W716-007-20 WITH A SPLICE. OPS CHECK SAT.

Part: SLEEVE — TORN (NR 2 A/C PACK) · airframe 36,934 hrs · 22,471 cycles

PACK 1 AND 2 VALVE CLOSED MESSAGE IN FLIGHT ALONG WITH PACK 1 OVERHEAT MESSAGE AT 17000' CABIN ATTITUDE AT 10100'. CREW REPORTED THAT THERE WAS NO OVERWEIGHT LANDING. FOUND #2 PACK DUAL TEMP CONTROL VALVE OUTPUT TOP SLEEVE TORN/BLOWN AND FOUND #1 PACK DUAL TEMP CONTROL VALVE TOP SLEEVE LEAKING. R&R SLEEVE. FOUND #1 PACK VALVE SENSE LINE LEAKING. RE SECURE SENSE LINE. PERFORMED OPS CHECK. OPS CHECK AND LEAK CHECK SAT AT THIS TIME. NO OTHER DEFECTS NOTED.

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 36,908 hrs · 22,444 cycles

ACRID BURNING SMELL DURING DESCENT THROUGH 10,000 FEET IN FORWARD CABIN AND FLIGHT DECK. DEBRIEF: DURING DESCENT THROUGH 10,000' AFTER MANEUVERING AROUND A THUNDERSTORM THE CAPT/FO NOTICED A BURNING SMELL. SMELL BEGAN AFTER CLEARING THE STORM IN CLEAR AIR. CAPT STATED IN INITIALLY SMELLED SWEET TO HIM BUT THE FO FELT IT SMELLED ACRID/ELECTRICAL. THE SMELL IS STILL WEAKLY PRESENT IN THE CABIN. CREW OPENED THEIR GASPERS AND THERE WAS FRESH AIR COMING OUT, NO ABNORMAL ODORS. STRONG SMELL PERSISTED FOR ABOUT 5 MINUTES AND BEGAN TO DISSIPATE AROUND 5,000'. THE ODOR WAS STRONGER IN THE FORWARD CABIN/FLT DECK THAN IN THE REAR CABIN. THERE WAS NO VISIBLE SMOKE IN THE CABIN OR FLIGHT DECK. PERFORMED FIM TASK 21-20-00-810. NO DEFECTS WERE NOTED AT THIS TIME. OCF SATISFACTORY.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,780 hrs · 22,321 cycles

CORROSION ON THE LOWER THRESHOLD OF THE FWD SERVICE DOOR LOCATED BETWEEN FR 20-22. INSTALLED NEW LOWER THRESHOLD FWD SERVICE DOOR.

Part: BEARING — CORRODED (LT MLG) · airframe 36,780 hrs · 22,321 cycles

LEFT MLG FWD BEARING CAP CORRODED. REMOVED AND REPLACED THE BEARING CAP.

Part: BEARING — CORRODED (LT MLG) · airframe 36,780 hrs · 22,321 cycles

LEFT MLG AFT BEARING CAP CORRODED. REMOVED AND REPLACED THE BEARING CAP.

Part: TRUNNION — CORRODED (NLG) · airframe 36,780 hrs · 22,321 cycles

RT NLG UPPER DRAG BRACE BEARING HAD CORROSION. REPLACED THE NLG TRUNNION ASSY.

Part: FLOOR SUPPORT — CORRODED (FRAMES 35-38) · airframe 26,780 hrs · 22,321 cycles

CENTER OMEGA BEAM CORRODED BETWEEN FRAMES 35 - 38. REMOVED AND REPLACED THE OMEGA BEAM.

Part: SKIN — DENTED (FRAMES 19-20) · airframe 36,780 hrs · 22,321 cycles

FUSELAGE SKIN BETWEEN FRAMES 19 - 20, STRINGERS 11L - 12L WAS FOUND DENTED. REPAIRED IAW ETD.

Part: SKIN — MECHANIC ERROR (FRAME 20) · airframe 36,780 hrs · 22,321 cycles

RIVET INSTALLED IN EDGE OF CHEM MIL OF SKIN AT REPAIR LOCATED AFT OF FR 20 AND BELOW STGR 14L REMOVED PREVIOUS REPAIR DOUBLE INTALLED NEW REPAIR DOUBLER FOR AREA AFT OF FR 20 AND BELOW STGR 14L

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 36,780 hrs · 22,321 cycles

PAX DOOR INTERNAL HANDLE SUPPORT BOX WAS CRACKED. REMOVED AND REPLACED THE HANDLE SUPPORT BOX.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 36,780 hrs · 22,321 cycles

BRACKET FOR THE CARGO DOOR AFT SPRING REEL WAS CRACKED. REMOVED AND REPLACED THE BRACKET.

Part: FLOOR SUPPORT — CRACKED (FRAMES 47-48) · airframe 36,780 hrs · 22,321 cycles

RIGHT CENTER OMEGA BEAM WAS CRACKED BETWEEN FRAMES 47-48. REMOVED AND REPLACED THE OMEGA BEAM.

Part: SKIN — DENTED (FRAMES 19-20) · airframe 36,780 hrs · 22,321 cycles

SKIN DENTED, FRAMES 19 - 20, STRINGERS 12L - 13L. OUT OF LIMITS. REPAIRED THE DENT.

Part: LIGHT — UNSECURE (CABIN) · airframe 36,212 hrs · 21,733 cycles

FLOOR EMERGENCY LIGHT PATH STRIP NOT SECURE AT ROW 2. RE SECURED FLOOR LIGHT STRIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,096 hrs · 21,613 cycles

AISLE EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE LAMP AND OPS CHECKED OK.

Part: LIGHT — MISSING (CABIN) · airframe 35,798 hrs · 21,313 cycles

EMERGENCY LIGHT STRIP MISSING. REPLACED THE LIGHT AND OPS CHECK GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 35,608 hrs · 21,119 cycles

OVERHEAD EMERGENCY EXIT LIGHTS AT ROW 18 INOPERATIVE, ON BOTH SIDES. SECURED PIN G ON CONNECTOR 8031.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 35,608 hrs · 21,119 cycles

OVERHEAD EMERGENCY EXIT LIGHTS AT ROW 18, INOPERATIVE ON BOTH SIDES. SECURED PIN G ON CONNECTOR 8031.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,577 hrs · 21,091 cycles

EMERGENCY EXIT LIGHTS AT ROW 18 ARE INOPERATIVE. R & R THE NR 5 INVERTER.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 35,571 hrs · 21,085 cycles

ROW 18 PASSAGE WAY LIGHTS INOPERATIVE. CLEANED AND SECURED THE CONNECTOR ON POWER SUPPLY NR 3.

Part: POWER SUPPLY — ABNORMAL (EMERGENCY LIGHTS) · airframe 35,560 hrs · 21,077 cycles

BOTH OVER WING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. R & R THE POWER SUPPLY. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,415 hrs · 20,939 cycles

OVERHEAD EMERGENCY LIGHT OUT AT ROW 22. R & R THE BULB. OPS CHECKED SATISFACTORY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,388 hrs · 20,915 cycles

FA EMERGENCY EXIT LIGHT ON RT SIDE OF THE CABIN IS INOPERATIVE. R & R ASSOCIATED INVERTER POWER SUPPLY OPS CHECK SAT.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 35,261 hrs · 20,792 cycles

EMERGENCY LIGHTS AT ROW 18 INOPERATIVE. SECURED AND CHARGED AFT BATTERY POWER SOURCE, OPS CHECKED SAT.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 35,252 hrs · 20,783 cycles

TWO CABIN EMERGENCY LIGHTS AT ROW 18 INOPERATIVE. RESEATED THE CONNECTOR FOR THE BATTERY. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 35,137 hrs · 20,671 cycles

EMERGENCY LIGHTS AT EXIT ROW, LT AND RT SIDES INOPERATIVE. PERFORMED POWER RESET. OPS CHECKED SAT.

Part: BUTTON — STUCK · airframe 35,062 hrs · 20,611 cycles

CABIN AND CABIN EMERGENCY PUSH BUTTON LIGHT STUCK. RESET CABIN PUSH BUTTON, OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 34,744 hrs · 20,357 cycles

EMERGENCY LIGHTS WILL NOT STAY ON. CHARGED EMERGENCY BATTERIES WITH APU OPS CHECK SAT.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,624 hrs · 20,244 cycles

SECOND EMERGENCY CEILING LIGHT INOPERATIVE. R & R THE NR 1 BATTERY ASSY, OPS TESTED GOOD.

Part: FIRE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 34,531 hrs · 20,148 cycles

BAGGAGE FIRE DETECTION INOPERATIVE. COMPLIED WITH FIM TASKS AND OPS CHECK WAS GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,452 hrs · 20,068 cycles

CEILING EMERGENCY LIGHT AT ROW 18 INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,444 hrs · 20,061 cycles

CEILING EMERGENCY LIGHT ABOVE ROW 3 INOPERATIVE. R & R THE BATTERY PACK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,444 hrs · 20,061 cycles

EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 3. R & R NR 1 POWER SUPPLY.

Part: ENGINE — POWER LOSS (NR 2) · airframe 34,048 hrs · 19,670 cycles

NR 2 ENGINE FAILED TO ACCELERATE PAST 26 PERCENT N2. FUEL FLOW WAS NOTED TO BE 320. NO INCREASE IN ITT WAS NOTED. FUEL VAPORS PRESENT IN THE CABIN. PERFORMED ENGINE RUNS MULTIPLE TIMES ON BOTH FADEC AND STARTER CHANNELS. NO DEFECTS NOTED.

Part: DOOR SILL — CORRODED (FRAMES 20-22) · corrosion level 2 · airframe 33,663 hrs · 19,383 cycles

DURING C-CHECK THE SERVICE DOOR 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: CONTROL UNIT — FAULTY (BRAKE) · airframe 33,321 hrs · 19,145 cycles

PILOT REPORTED THE BRAKES SLOW TO RESPOND AND REDUCED BRAKING EFFECTIVENESS ON LANDING. NOTED: BRAKES FEEL SPONGY AND OPERATING OUTSIDE OF WHAT FEELS NORMAL. MAINTENANCE R & R THE BRAKE CONTROL UNIT AND BLED BRAKES WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR SERVICE.

Part: ACM — FAILED · airframe 33,137 hrs · 19,013 cycles

AT CRUISE, DURING FLIGHT, AIRCREW NOTICED SMOKE IN COCKPIT AND CABIN. ACFT DIVERTED AND AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND RT ACM MAKING LOUD SQUEALING NOISE AND SMOKING. MAINTENANCE R & R THE RT ACM IAW AMM 21-51-03. THE UNIT OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — SHORTED (EMERGENCY LIGHTS) · airframe 32,785 hrs · 18,792 cycles

ACFT WAS IN FOR A 3A CHECK WHEN THE NR 2 EMERGENCY LIGHT INVERTER WAS FOUND INOPERATIVE. MAINTENANCE R & R THE NR 2 INVERTER IAW AMM 33-50-11. OPS CHECK GOOD AND WAS RELEASED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,115 hrs · 18,324 cycles

DURING MAINTENANCE INSPECTION, THE LT OVERWING FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT BATTERY CHARGER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,762 hrs · 17,450 cycles

DURING A-CHECK, THE EMERGENCY EXIT LIGHT AT EXIT ROW SEAT 18C WOULD NOT ILLUMINATE. MAINTENANCE R & R THE LIGHT ASSY IAW AMM 33-50-14. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — BURNED (SEAT 1-2A) · airframe 30,324 hrs · 17,163 cycles

THE CREW REPORTED BURNING ODOR COMING FROM LIGHTS ABOVE SEAT 1A, 2A. MAINTENANCE INSPECTED AND REPLACED 1ST 2 LIGHTING ASSEMBLIES FOR OVERHEAD LIGHTS IAW 33-21-06. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 26,810 hrs · 14,914 cycles

DURING ROUTINE MX THE SERVICE DOOR FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT BATTERY AND OPS CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,969 hrs · 13,088 cycles

THE CREW REPORTED THE EXIT MARKER NEAR THE MAIN CABIN DOOR WAS INOPERATIVE. MX R & R THE AFFECTED LIGHTP, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 23,688 hrs · 12,912 cycles

DURING C-CK LT FUSELAGE SKIN HAS CRACKS FR 79-81, STR 8L-10L. REPAIRED SKIN IAW EC5330-02501. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 23,688 hrs · 12,912 cycles

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

Part: SUPPORT — CORRODED (ZONE 100) · airframe 23,688 hrs · 12,912 cycles

DURING C-CK. BAGGAGE DOOR LOWER CUTOUT CORRODED. R & R LOWER CARGO DOOR CUT OUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE LOOP — FAILED (NR 2 NACELLE) · airframe 23,643 hrs · 12,889 cycles

CREW REPORTED ENGINE NR 2 FIRE DETECTOR FAIL IN FLT. MX R & R ENGINE NR 2 FIRE DETECTOR LOOP IAW AMM 26-11-0I WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SELECTOR SWITCH — INOPERATIVE (COCKPIT) · airframe 21,641 hrs · 11,646 cycles

VSA - FLIGHT 2964 THE CREW REPORTED THAT THE NUMBER ONE ELECTRIC HYDRAULIC PUMP CIRCUIT BREAKER POPPED WITH A STRONG ELECTRICAL SMELL. MAINTENANCE REMOVED AND REPLACED THE SELECTOR SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 21,590 hrs · 11,617 cycles

FLIGHT 2665 - EWR - FLIGHT CREW REPORTED SMOKE IN CABIN AFTER T/O FOLLOWED BY LAV SMOKE INDICATION ON EICAS. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX PERFORMED ENGINE NR 1 AND NR 2 RUN UP AT HIGH POWER WITH BLEED SYSTEM ON FOR 3 MIN (TWICE). NO SMOKE NOTICED. MX ALSO PERFORMED LAV SMOKE DETECTOR OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CARGO BAY) · airframe 19,440 hrs · 10,428 cycles

FLIGHT 3070 - EWR - FLIGHT CREW REPORTED HEAVY AROMA OF LAV FLUID IN CARGO BIN. EWR MX OPENED CARGO FLOORBOARD AND INSPECTED FOR LAV FLUID LEAK. NO LEAKAGE FOUND. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LINE — LOOSE (ANTI-ICE SYS) · airframe 18,755 hrs · 10,053 cycles

IAH FLT 2738 THE CREW REPORTED A WING ANTI-ICE FAIL MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RE-SECURED LOOSE LINE ON WING ASSY SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,748 hrs · 10,048 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 24-25. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 18,748 hrs · 10,048 cycles

SHV - DURING C-CHECK LT FUSELAGE SKIN HAS CRACK AROUND RIVET FR 77. REPAIRED SKIN IAW EC5330-02099. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 18,748 hrs · 10,048 cycles

SHV - DURING C-CHECK RT FUSELAGE SKIN HAS CRACK AROUND RIVET FR 79. REPAIRED SKIN IAW EC5330-02099. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 18,748 hrs · 10,048 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 33-34. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,748 hrs · 10,048 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 33-34. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,748 hrs · 10,048 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TAT PROBE — FAULTY (NR 1) · airframe 18,250 hrs · 9,794 cycles

CLE FLIGHT 2659 THE CREW REPORTED A "TAT 1 HEAT INOP" MESSAGE ON THE EICAS IN FLIGHT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 TAT PROBE AND OPERATIONAL CHECKS WERE GOOD.

Part: CLAMP — MISSING (BLEED AIR SYS) · airframe 18,136 hrs · 9,724 cycles

FLIGHT 2968 - EWR - FLIGHT CREW REPORTED THAT ON CLIMBOUT NR 2 ENGINE ITT ROSE INTO THE AMBER RANGE AT E-CLIMB POWER. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. E2 RUNS ABOUT 150 DEGREES HIGHER THAN E1. UPON LANDING, E2 EXCEEDANCE ON EICAS. E2 RAN AT 570 DEG ON IDLE, FUEL FLOW ABOUT 250 LB/HR HIGHER THAN E1. EWR MX FOUND MISSING CLAMP AT COMPRESSOR AIR DISCHARGER VALVE. MX INSTALL MISSING CLAMP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 14,406 hrs · 7,701 cycles

FLIGHT 2074 EWR FLIGHT CREW REPORTED EMERGENCY EXIT IDENTIFIER ABOVE FORWARD FLIGHT ATTENDANT SEAT INOPERATIVE. EWR MX R&R NR 1 EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SLEEVE — BLOWN (A/C PACK)

EWR FLIGHT 2879, THE CREW REPORTED A BLEED VALVE 2 FAIL IN FLIGHT. THE ACFT DIVERTED INTO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED A BLOWN SLEEVE ON THE NR 2 ENVIRONMENTAL CONTROL UNIT. ALSO REPLACED THE NR 2 BLEED PUSH BUTTON P/N 4800-112. OPERATIONAL CHECKS WERE GOOD. (S)

Part: FITTING — GOUGED (HORIZONTAL STAB)

SHV - DURING C-CHECK IT WAS FOUND THAT THE LT HORIZONTAL STAB HINGE PIN FITTING WAS GOUGED. MAINTENANCE PERFORMED A REAMING PROCEDURE TO THE FIRST OVERSIZE IAW EMB 145XR SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: FITTING — WORN (HORIZONTAL STAB)

SHV - DURING C-CHECK IT WAS FOUND THAT THE RT HORIZONTAL STAB HINGE PIN FITTING HAD MIGRATED PLAIN BUSHINGS. MAINTENANCE PERFORMED A REAMING PROCEDURE TO THE SECOND OVERSIZE IAW EMB 145XR SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: SKIN — GOUGED (FUSELAGE)

SHV - DURING C-CHECK IT WAS FOUND THAT THE CENTER FUSELAGE SKIN HAD AN INTERNAL GOUGE BETWEEN FRAMES 16 AND 17, AND STRINGERS 3R AND 4R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145XR SRM 53-21-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,279 hrs · 5,547 cycles

IAH - FLIGHT 2071, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE F/A HEADREST TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — FAULTY (EMERGENCY LIGHT) · airframe 7,254 hrs · 3,930 cycles

CLE FLIGHT NR 2330, THE CREW REPORTED THE FORWARD EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 7,006 hrs · 3,796 cycles

IAH - FLIGHT 2008, DURING POSTFLIGHT INSPECTION, THE CREW REPORTED THAT THE GALLEY EMERGENCY LIGHTS WOULD NOT EXTINGUISH. MAINTENANCE REPAIRED A LOOSE WIRE ON GROUND BLOCK GS8506DC, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HOLDER — SHORTED (COCKPIT) · airframe 2,682 hrs · 1,414 cycles

THE CREW REPORTED THAT A SPRING BEHIND THE F/O'S MAP HOLDER MADE CONTACT WITH AN EXPOSED WIRE CAUSING SMOKE. MAINTENANCE REMOVED AND REPLACED THE F/O'S MAP HOLDER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.