N16183

Part: UNKNOWN — ODOR (CABIN) · airframe 41,463 hrs · 28,375 cycles

SMELL OF SMOKE IN COCKPIT HAPPENED AFTER LIGHT / MOD TURBULENCE IN CRUSE ,  AFTER SHUTTING PAC 1 DOWN SMELL WENT AWAY .SMELL WAS NOT PRESENT THE REST OF THE FLIGHT NO VISIBLE SMOKE OR MSGS PRESENT .SMELL ONLY IN COCKPIT .ELECTRICAL SMELL . NOT IN CABIN OR LAV OR BAG . THE SMELL WAS LIGHT LESS THAN 2 MIN,  MASKS WERE NOT USED AND  FLIGHT LEVEL ABOVE 250 BOTH ENG ON . ALL ANTI ICE WAS ON ., AC NOT IN ICING AND AC  WAS NOT DE ICE PRIOR TO T/O . TLA WAS AT  86% AND  NO EMERGENCY WAS DECLARED " PREFORMED TROUBLE SHOOTING FOR ABNORMAL SMELL IN COCKPIT. RAN BOTH ENG WITH PAC SYSTEM WITH CREW. OPS CHECKED GOOD NO SMELL OR DEFECTS NOTED AC RETUNED TO SERVICE

Part: SKIN — DENTED (FUSELAGE) · airframe 41,383 hrs · 28,295 cycles

ALL DENTS IN AREAS A, B, C,AND D ARE REFERENCED IN ETD EXCEPT DENT IN AREA A1 ON THE LF FWD FUSELAGE I/II SKIN REQUIRE A PERMANENT REPAIR WITHIN 50000FC FROM SEPTEMBER 21, 2022. SKIN REPAIRED WITH A DOUBLER.

Part: GUSSET — CORRODED (LEFT) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

LH GUSSET NO 1 CORRODED. LH GUSSET #1 FOUND OUT OF LIMITS. REPLACED WITH NEW PART

Part: SEAT TRACK — CORRODED (FRMS 18-24) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

LH INBD SEAT TRACK BTW FR 18-24 FOUND CORRODED AT FR22 AND 24. AT CF1, LH INBD SEAT TRACK BTW FR 18-24 CORRODED OUT OF LIMITS. LH SEAT TRACK REMOVED. LH INBD SEAT TRACK BTW FR 18-24 REPLACED WITH NEW PART

Part: FLOOR SUPPORT — CRACKED (FRMS 29-36) · airframe 41,383 hrs · 28,295 cycles

CF2, CRACKS (2X) FOUND ON LH OMEGA BEAM #3 FLOOR STRUCTURE BTW FR 29-36. 2 REPAIR DOUBLERS ON LH CENTER FUSE 2 OMEGA BEAM, ON INBD VERTICAL FLANGE AT FR 31 & 33

Part: FLOOR SUPPORT — CRACKED (FRMS 18-24) · airframe 41,383 hrs · 28,295 cycles

CF1, (X3) CRACKS FOUND ON L/H OMEGA BEAM #1 BTW FR 18-24 L/H OMEGA BEAM #1 BTW FR 18-24 REPLACED.

Part: SUPPORT — CRACKED (RT AILEORN ACT) · airframe 41,383 hrs · 28,295 cycles

RH AILERON SUPPORT ACTUATOR ASSY CRACKED. REMOVAL OF CRACKED SUPPORT ASSY IN PROGRESS. RH AILERON SUPPORT ACTUATOR ASSY REMOVED DUE TO CRACK. RH AILERON SUPPORT ACTUATOR ASSY REPLACED.

Part: DOOR SILL — CORRODED (FRMS 18-20) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

CF1 RH SIDE SERVICE DOOR FWD SILL CORRODED AT FR 18 AND 20 AROUND ANCHOR NUT. CF1 RH SIDE SERVICE DOOR FWD SILL BLENDED AT FR18 AND FR20 AROUND ANCHOR NUT AND FOUND OUT OF LIMITS. RH SIDE SERVICE DOOR FWD SILL AT FR18 REPAIR CARRIED OUT. RH SIDE SERVICE DOOR SILL AT FR20 REPAIR CARRIED OUT.

Part: FLOOR SUPPORT — CRACKED (FRMS 23-30) · airframe 41,383 hrs · 28,295 cycles

CF2, CRACKS (4X) FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BTW FR 23-30. LH OMEGA BEAM #2 REPLACED WITH A NEW ONE

Part: FLOOR SUPPORT — CRACKED (FRMS 46-50) · airframe 41,383 hrs · 28,295 cycles

CF3 LH OMEGA BEAM OUTBD ANGLE FOUND CRACKED BTW FR 46-50. AT LH OMEGA BEAM ANGLE BTW FR 46-50 REMOVED QTY 5 CABLE CLAMPS FOR ACCESS. AT LH OMEGA BEAM OUTBD BTW FR 46-50 REMOVED ANGLE FOR REPLACEMENT. CF3 LH OMEGA BEAM OUTBD ANGLE BTW FR 46-50, REPAIRED AT LH OMEGA BEAM OUTBD ANGLE BTW FR 46-50 5X CABLE CLAMPS INSTALLED

Part: SHEAR TIE — CRACKED (FRM 80 S5-7L) · airframe 41,383 hrs · 28,295 cycles

IN REAR FUSELAGE, BULKHEAD 80 ON LH SIDE, BETWEEN STGR 5L AND STGR 7L SHEAR CLIP CRACKED. REAR FUSELAGE, BULKHEAD 80 LH BTW SR 5L-7L SHEAR CLIP REMOVED, REPLACED WITH NEW PART INSTALLED

Part: FLOOR SUPPORT — CRACKED (FRMS 46-50) · airframe 41,383 hrs · 28,295 cycles

CF3 LH OMEGA BEAM INBD ANGLE FOUND CRACKED BTW FR 46-50. CF3 LH OMEGA BEAM INBD BTW FR 46-50, REMOVED CROSS BEAM AT FR49 FOR ACCESS. CF3, LH OMEGA BEAM INBD BTW FR 46-50 REMOVED ANGLE FOR REPLACEMENT. CF3 LH OMEGA BEAM INBD ANGLE BTW FR 46-50 REPAIRED. CF3 LH OMEGA BEAM INBD BTW FR 46-50 CROSS BEAM AT FR49 INSTALLED

Part: ANGLE — CRACKED (FRM 66) · airframe 41,383 hrs · 28,295 cycles

AT CARGO ENTRY AT FR66 LOWER ANGLE FOUND CRACK UNDER T SUPPORT. AT CARGO ENTRY AT FR66 LOWER ANGLE UNDER T SUPPORT REMOVED AND REPLACED

Part: SKIN — CRACKED (FRM 77-80) · airframe 41,383 hrs · 28,295 cycles

CRACKS SUSPECTED (9X) ON LH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3L-9L. AFTER NDT INSPECTION (9X) CRACKS CONFIRMED ON LH SKIN BTW FR 77-80 AND STR 3L-9L. LH SKIN BTW FR 77-80 AND BTW STR 3L-9L CRACKS REMOVED BY CUT-OUT. LH SKIN, CRACKS (X9) AROUND FASTENERS REPAIRED

Part: FLOOR SUPPORT — CRACKED (FRMS 59-61) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

CF4, LH OMEGA BEAM IN TOILET AREA BTW FR 59-61 FOUND CORRODED AROUND NUT PLATE HOLES. CF4, LH OMEGA BEAM IN TOILET AREA, CUTOUT CARRIED OUT BTW FR 60-61 AT ANCHOR NUT LOCATION. LH OMEGA BEAM REPAIR HAT SECTION FABRICATED. LH OMEGA BEAM AT FR 60 OMEGA BEAM REPAIRED.

Part: BRACKET — CRACKED (FRM 10) · airframe 41,383 hrs · 28,295 cycles

AT FWD FUSE AREA, CRACK FOUND ON LH TOP BRACKET ON FR10 UNDER SIDE COCKPIT WINDOW SURROUND STRUCTURE. BRACKET REMOVED FOR REPLACEMENT. BRACKET LOCALLY FABRICATED. ON COCKPIT LH SIDE BELOW SIDE WINDOW LOWER FRAME, BRACKET REPLACED WITH MADE REPAIR PART AND INSTALLED WITH RIVETS.

Part: SHEAR TIE — CRACKED (FRM 58 S15-16L) · airframe 41,383 hrs · 28,295 cycles

IN CFIV, LH SHEAR CLIP AT FR58 BTW STR 15L-16L FOUND CRACKED. LH SHEAR CLIP AT FR58 FOUND CRACKED. SHEAR CLIP REMOVED. NEW SHEAR CLIP INSTALLED AT FR58 BTW STR 15L-16L.

Part: SKIN — CRACKED (FRM 77-80 S3-9R) · airframe 41,383 hrs · 28,295 cycles

CRACKS SUSPECTED (9X) ON R/H SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3R-9R. AFTER NDT INSPECTION, (9X) CRACKS CONFIRMED ON RH SKIN BTW FT77-80 STR 3R-9R SKIN REPAIRED WITH 7 BUSHINGS AS PER SRM 53-32-01-RE #5 FIG 210 AND A REPAIR DOUBLER AS PER SRM 53-32-01-RE #3 FIG 204

Part: SHEAR TIE — CRACKED (FRM 61 S6-7L) · airframe 41,383 hrs · 28,295 cycles

RF1 LH SHEAR CLIP AT FR61 BTW STR 6-7L FOUND CRACKED. SHEAR CLIP REMOVED AND REPLACED

Part: BEAM — CRACKED (FRMS 35-39) · airframe 41,383 hrs · 28,295 cycles

CF3, CRACKS (2X) FOUND ON LH OMEGA BEAM #4 FLOOR STRUCTURE BTW FR 35-39. LH OMEGA BEAM #4 AT FR 36 CUTOUT PERFORM. LH OMEGA BEAM #4 AT FR 37 CUTOUT. LH OMEGA BEAM #4 AT FR36 AND FR 37 REPAIRED

Part: ANGLE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

RH IB FLAP IB ANGLE CORRODED. OLD ANGLE REMOVED, NEW ANGLE PARTIALLY INSTALLED. INSTALLATION OF NEW BRACKET COMPLETED

Part: GUSSET — CORRODED (FRMS 46-52) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

CF3 RH GUSSET #5 BTW FR 46-52 CORRODED. IN CF3 RH GUSSET #5 BTW FR 46-52 FOUND CORRODED OUT OF LIMIT. CF3 RH GUSSET #5 BTW FR 46-52 REMOVED AND REPLACED

Part: ANGLE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

LH OB FLAP IB ANGLE CORRODED. AT LH OB FLAP, ANGLE BRACKET REMOVED FOR REPLACEMENT. CORROSION FOUND ON BRACKET OUTBOARD FLAP WING BLENDED. NEW LH OB ANGLE INSTALLED

Part: DOOR SILL — CORRODED (L1 DOOR AREA) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

CF1 LH SILL NO 1 CORRODED. #1 LH SILL REMOVED AND REPLACED

Part: GUSSET — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

LH GUSSET TOILET BTW FR 59-61 CORRODED. LH GUSSET IN TOILET AREA BTW FR 59-61 BLENDED AND FOUND OUT OF LIMIT. REMOVED FOR REPLACEMENT. LH GUSSET BTW FR 59-61 INSTALLED WITH A NEW ONE

Part: BRACKET — CRACKED (FRM 46) · airframe 41,383 hrs · 28,295 cycles

CF3 RH CLOSING BRACKET AT FR 46 FOUND CRACKED. ON CF3 RH CLOSING BRACKET AT FR46 REMOVED FOR REPLACEMENT. ON CF3 RH CLOSING BRACKET AT FR46 REPLACED

Part: FRAME — CORRODED (FRM 59 S20-21R) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

CF4 FRAME 59 CORRODED BTW STR 21R-20R UNDER PROFILE. IN CF4 AT FR 59 BTW STR 21R-20R CORROSION BLENDED AND FOUND OUT OF LIMIT. AT FR 59 BTW STR 21R-20R DAMAGE REMOVED. AT FR 59 BTW STR 21R-20R FRAME REPAIRED.

Part: SUPPORT BRACKET — CRACKED (FRM 68) · airframe 41,383 hrs · 28,295 cycles

CARGO DOOR SUPPORT BRACKET FOUND CRACKED AT FR68. ON CARGO DOOR SUPPORT BRACKET AT FR68 REMOVED FOR REPLACEMENT. ON CARGO DOOR SUPPORT BRACKET AT FR68 REPLACED

Part: SHEAR TIE — CRACKED (FRM 61 S6-7R) · airframe 41,383 hrs · 28,295 cycles

RF1 RH SHEAR CLIP AT FR 61 BTW STR 6-7 FOUND CRACKED. IN RF1 SHEAR CLIP AT FR61 BTW STR 6R-7R REPLACED WITH NEW ONE.

Part: SHEAR TIE — CRACKED (FRM 73 S8-10L) · airframe 41,383 hrs · 28,295 cycles

RF1: SHEAR CLIP FOUND CRACKED AT FR 73 BTW RH STR 8L-10L. AT RF1, ON LH FR 73 BTW STR 8L-10L SHEAR CLIP REMOVED FOR REPLACEMENT. AT RF1, ON LH FR73 BTW STR 8L-10L, SHEAR CLIP REPLACED

Part: SHEAR TIE — CRACKED (FRM 73 S8-10R) · airframe 41,383 hrs · 28,295 cycles

RF1: SHEAR CLIP FOUND CRACKED AT FR 73 BTW RH STR 8R-10R. AT RF1, AT RH FR73 BTW STR 8R-10R, SHEAR CLIP REMOVED FOR REPLACEMENT. AT RF1, AT RH FR 73 BTW STR 8R-10R, SHEAR CLIP REPLACED.

Part: SHEAR TIE — CRACKED (FRM 67 S6-7L) · airframe 41,383 hrs · 28,295 cycles

RF1: SHEAR CLIP FOUND CRACKED AT FR67 BTW LH STR 6L-7L. AT RF1, AT LH FR67 BTW STR 6L-7L, SHEAR CLIP REMOVED FOR REPLACEMENT. AT FR67 BTW LH STR 6-7L SHEAR CLIP REPLACED.

Part: SHEAR TIE — CRACKED (FRM 62-S6-8R) · airframe 41,383 hrs · 28,295 cycles

RF1: SHEAR CLIP FOUND CRACKED ON FR 62 BTW RH STR 6R-8R. IN RF1 SHEAR CLIP ON FR62 BTW STR 6R-8R REPLACED WITH NEW ONE.

Part: SHEAR TIE — CRACKED (FRM 25 S15-16R) · airframe 41,383 hrs · 28,295 cycles

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

Part: GUSSET — CORRODED (FRMS 38-46) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

CF3 RH GUSSET #4 BTW FR 38-46 CORRODED. IN CF3 RH GUSSET #4 BTW FR 38-46 FOUND CORRODED OUT OF LIMIT. RH GUSSET #4 REPLACED.

Part: GUSSET — CORRODED (FRM 38-46) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

CF3 LH GUSSET #5 BTW FR 38-46 CORRODED. CF3 LH GUSSET #5 BTW FR 38-46 FOUND CORRODED OUT OF LIMIT. LH GUSSET #5 REPLACED

Part: SHEAR TIE — CRACKED (FRM 66 S6-7L) · airframe 41,383 hrs · 28,295 cycles

RF1: SHEAR CLIP FOUND CRACKED AT FR66 BTW LH STR 6-7L. AT RF1, AT FR66 BTW STR 6L-7L, SHEAR CLIP REMOVED FOR REPLACEMENT. AT FR66, BTW LH STR 6-7L SHEAR CLIP REPLACED.

Part: SHEAR TIE — CRACKED (FRM 24 S16-17L) · airframe 41,383 hrs · 28,295 cycles

CF2 LH SIDE FR24 BTW STR 16-17 SHEAR CLIP CRACKED. AT CF2, LH SIDE FR24 BTW STR 16-17 SHEAR CLIP REMOVED FOR REPLACEMENT. AT CF2, LH SIDE FR24 BTW STR 16-17, SHEAR CLP REPLACED

Part: SHEAR TIE — CRACKED (FRM 25 S15-16L) · airframe 41,383 hrs · 28,295 cycles

CF2, LH SIDE FR25 BTW STR 15-16 SHEAR CLIP CRACKED. AT CF2, LH SIDE FR25 BTW STR 15-16 SHEAR CLIP REMOVED FOR REPLACEMENT. AT CF2 LH SIDE FR25 BTW STR 15-16, SHEAR CLIP REPLACED

Part: SEAT TRACK — CHAFED (FRMS 38-49) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

LH OUTBD SEAT TRACK FOUND CHAFFED AT FR38, 44, AND 49. LH OUTBD SEAT TRACK AT FR38 OUT OF LIMITS, REMOVED AND REPLACED. LH OUTBD SEAT TRACK AT FR44 OUT OF LIMITS REMOVED AND REPLACED. LH OUTBD SEAT TRACK AT FR49 BLENDED WITHIN LIMITS.

Part: SHEAR TIE — CRACKED (FRM 15) · airframe 41,383 hrs · 28,295 cycles

CF1 RH SIDE SHEAR CLIP FR15 BTW STR 15-16 CRACKED. AT CF1, AT FR15 ON RH SIDE BTW STR 15-16, ON EXTERNAL SKIN PAINT STRIPPED AND SHEAR CLIP REMOVED AND REPLACED

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 41,383 hrs · 28,295 cycles

RH MLG BAY AFT BULKHEAD CRACKED. AT RH MLG BAY AFT, BULKHEAD REMOVED, NEW BULKHEAD FULLY DRILLED. AT RH MLG BAY AFT, NEW BULKHEAD INSTALLED

Part: FLOORBEAM — CORRODED (FRM 61) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

AT FR61 RH OUTBD FLOOR T SUPPORT FOUND CORRODED. AT FR61 RH OUTBD FLOOR T SUPPORT BLENDED AND FOUND OUT OF LIMIT. AT FR61 RH OUTBD FLOOR SUPPORT REMOVED FOR REPLACEMENT. AT FR61 RH OUTBD FLOOR T SUPPORT REPLACED WITH NEW ONE

Part: SHEAR TIE — CRACKED (FRM 16 S15-16R) · airframe 41,383 hrs · 28,295 cycles

CF1 RH SIDE SHEAR CLIP FR16 CRACKED BTW STR 15-16. AT CF1, AT FR16 BTW STR 15-16 EXTERNAL SKIN, PAINT STRIPPED FOR ACCESS. SHEAR CLIP REMOVED AND REPLACED

Part: SHEAR TIE — CRACKED (FRM 24 S16-17R) · airframe 41,383 hrs · 28,295 cycles

CF2 RH SIDE FR 24 BTW STR 16R-17R SHEAR CLIP CRACKED. ON CF2 RH SIDE FR24 BTW STR 16R-17R SHEAR CLIP REMOVED AND REPLACED

Part: BEAM — CORRODED (FRMS 65-68) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

CARGO CUTOUT LOWER BEAM FOUND CORRODED BTW FR 65-68. CARGO CUT-OUT LOWER BEA, BTW FR65-68 BLENDED AND FOUND OUT OF LIMIT. CARGO CUT-OUT LOWER BEAM BTW FR 65-68 REMOVED FOR REPLACEMENT. BTW FR 65-68 ITEM 40-45-50-55-60-65 REMOVED FOR ACCESS. CARGO CUTOUT BTW FR 65-68 LOWER BEAM REPLACED WITH NEW ONE. BTW FR 65-68, ITEM 40-45-50-55-60-56 REINSTALLED. CARGO CORNERS REPAIRED.

Part: FLOOR SUPPORT — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

AFTER REMOVAL OF RH GUSSET BTW FR 59-61, OMEGA BEAM FOUND CORRODED. CORROSION ON RH OMEGA BEAM BTW FR 59-61 BLENDED OUT OF LIMITS AND REMOVED BY CUT-OUT. RH OMEGA BEAM BTW FR 59-61 REPAIRED

Part: SHEAR TIE — CRACKED (FRM 26 S15-16R) · airframe 41,383 hrs · 28,295 cycles

CF2 RH SIDE FR26 BTW STR 15-16 SHEAR CLIP CRACKED. CF2 RH SIDE FR26 BTW STR 15-16 SHEAR CLIP REMOVED AND REPLACED

Part: SHEAR TIE — CRACKED (FRM 24 S15-16R) · airframe 41,383 hrs · 28,295 cycles

CF2 RH SIDE FR24 BTW STR 15-16 SHEAR CLIP CRACKED. ON CF2 RH SIDE FR24 BTW STR 15-16 SEAR CLIP REMOVED AND REPLACED.

Part: SHEAR TIE — CRACKED (FRM 27 S15-16R) · airframe 41,383 hrs · 28,295 cycles

CF2 RH SIDE FR27 BTW STR 15R-16R SHEAR CLIP CRACKED. CF2 RH SIDE FR27 BTW STR 15-16 SHEAR CLIP REMOVED AND REPLACED

Part: BRACKET — CRACKED (FRM 15) · airframe 41,383 hrs · 28,295 cycles

CF1 RH SIDE FUEL RELAY BRACKET AT FR15 CRACKED. RH FUEL RELAY BRACKET FOUND CRACKED, NEW BRACKET INSTALLED

Part: SHEAR TIE — CRACKED (FRM 24 S15-16L) · airframe 41,383 hrs · 28,295 cycles

CF2 LH SIDE FR 24 BTW STR 15-16 SHEAR CLIP CRACKED. AT CF2 LH SIDE FR 24 BTW STR 15-16, SHEAR CLIP REMOVED FOR REPLACEMENT. AT CF2 LH SIDE FR24 BTW STR 15-16, SHEAR CLIP REPLACED

Part: FLOORBEAM — CORRODED (FRM 61) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

AT FR61 RH INBD FLOOR T SUPPORT FOUND CORRODED. AT FR61 , RH INBD FLOOR T SUPPORT BLENDED AND FOUND OUT OF LIMIT. AT FR61 RH FLOOR T SUPPORT INBD REMOVED FOR REPLACEMENT. AT FR61 RH FLOOR T SUPPORT INBD REPLACED WITH NEW ONE

Part: FLOORBEAM — CORRODED (FRM 61) · airframe 41,383 hrs · 28,295 cycles

AT FR61 LH OUTBD FLOOR T SUPPORT FOUND CORRODED. AT FR61, LH OUTBD FLOOR T SUPPORT BLENDED AND FOUND OUT OF LIMIT. LH OUTBD FLOOR T SUPPORT REMOVED AND REPLACED.

Part: GUSSET — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 41,383 hrs · 28,295 cycles

RH GUSSET TOILET BTW FR 59-61 CORRODED. RH GUSSET BTW FR 49-61 BLENDED OUT OF LIMIT. RH GUSSET BTW FR 59-61 REPLACED

Part: ACTUATOR — WORN (STICK PUSHER) · airframe 41,384 hrs · 28,295 cycles

STICK PUSHER ACTUATOR CABLE WORN (BROKEN WIRE) FLAT SPOT. STICK PUSHER ACTUATOR REPLACED

Part: CHANNEL — CRACKED (FRMS 18-19) · airframe 41,383 hrs · 28,295 cycles

CF1 ON ON OMEGA BEAM QTY X2 DIAGONAL ANGLES CRACKED BTW FR18-19 CF1 L/H OMEGA BEAM 2 DIAGONAL ANGLES HAVE BEEN REPLACED, ONE WITH A NEW ANGLE AND THE OTHER ONE WITH A REPAIR PART FABRICATED. BOTH INSTALLED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,758 hrs · 27,713 cycles

FA FLASHLIGHT CHARGES INTERMITTENTLY

Part: UNKNOWN — UNKNOWN · airframe 40,059 hrs · 27,103 cycles

UPPER HANDLES ON OVER WING EXIT DOORS ARE LOOSE (WHITE GRAB HANDLES). RESECURED SHROUD.

Part: NONE — NONE · airframe 38,213 hrs · 25,499 cycles

RH OVER WING EXTERNAL EMERGENCY LIGHT IS INSTALLED UPSIDE DOWN. R&R RH OVER WING EMERGENCY LIGHT. OPS CHECK SAT

Part: NONE — NONE · corrosion level 2 · airframe 38,158 hrs · 25,449 cycles

MAIN CABIN CENTER BOX AREA, RH SIDE MOST O/B BUTT STRAP ATTACH ANGLE BELOW FRAME 46 PLUS "5" INCHES THRU PLUS "17" INCHES HAS SEVERAL HI-LOCS THAT HAVE SURFACE CORROSION SHOWING. REMOVED AND REPLACED OB BUTT STRAP ATTACHE ANGLE BELOW FRAME 46 PLUS "5" INCHES THRU PLUS "17" INCHES

Part: NONE — NONE · airframe 38,158 hrs · 25,449 cycles

RIGHT WING CENTER LEADING EDGE #612, HAS LARGE DENT 37 INCHES FROM I/B END. REPAIRED DENT IN RIGHT WING CENTER LEADING EDGE 612 37 INCHES FROM INBD END.

Part: NONE — NONE · corrosion level 2 · airframe 38,158 hrs · 25,449 cycles

THE LH OMEGA BEAM SPLICE PLATE BETWEEN FRMS 20 & 21 HAS CORROSION ON THE SURFACE. REPAIRED LH OMEGA BEAM BETWEEN FRAMES 20 & 21.

Part: BUTTON — CRACKED (EMERGENCY LIGHTS) · airframe 37,672 hrs · 25,021 cycles

FA CABIN EMERGENCY LIGHT BUTTON ON. RE-RERACKED FWD & AFT FA HANDSETS. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED.

Part: ARMREST — CRACKED (SEAT 23A) · airframe 37,460 hrs · 24,827 cycles

SEAT 23A, 21A, 19A, 10A, 7A, 6A, 3A, 2A AISLE ARMREST SUPPORT STRUCTURE CRACKED. REMOVED AND REPLACED 23A, 21A, 19A, 10A, 7A, 6A, 3A, 2A SEAT ASSEMBLIES.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 37,370 hrs · 24,750 cycles

BAGGAGE COMP FIRE EXT WARNING ILLUMINATED WITH NO EICAS MESSAGE. R&R HIGH RATE AND METERING BAGGAGE FIRE BOTTLES. R&R CARGO SMOKE DETECTOR. OPS CHECK COMPLETED. VERIFIED BAGGAGE EXT LIGHT EXTINGUISHED AFTER OPS CHECK. NO FAULTS FOUND.

Part: UNKNOWN — ODOR (APU) · airframe 37,320 hrs · 24,702 cycles

FUEL SMELL IN FLIGHT AND ON GROUND WITH APU RUNNING. PERFORMED RUNS AND CONFIRMED APU CAUSING FUEL SMELL DEFERRED PER MEL (PULLED AND COLLARED C30 C/B`S PLACARD APPLIED) APU HAS BEEN INSPECTED FOR LEAKS WITH NO LEAKS NOTED AT THIS TIME. R/R APU FUEL CONTROL ASSY IAW EMB 145 VCMM 49-32-01. OPS AND LEAK CHECK GOOD. FUEL SMELL NOT PRESENT AT THIS TIME. CIRCUIT BREAKERS RESET. MEL CLEARED. PLACARD REMOVED. APU INSPECTED FOR LEAKS NO LEAKS NOTED AT THIS TIME.

Part: SKIN — CRACKED (RT WING LE) · airframe 36,832 hrs · 24,252 cycles

CRACK IN RH WING LEADING EDGE #3 SKIN AT OUTBD VORTILON MOUNT POINT. REMOVED VORTILON AND FOUND CRACK TO BE APPROX 3/4" LONG EMANATING FROM BLEED HOLE. UPON REMOVAL OF LEADING EDGE, FOUND THE RETAINING ANGLE OF SPLICE BETWEEN LEADING EDGE 2 AND 3 TO BE WORN. R&R RH #3 LEADING EDGE, ALONG WITH THE PICCOLLO TUBE CONNECTOR SEALS. OPS CHECK SAT.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 36,556 hrs · 23,980 cycles

FUMES IN THE COCKPIT ON CLIMB-OUT. FOUND SMOKE ON SHUTDOWN OF #1 ENGINE WHILE TROUBLESHOOTING LPT SHAFT O-RING. NO FURTHER DEFECTS NOTED.

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 34,644 hrs · 22,274 cycles

CORROSION - BAGGAGE DOOR CUTOUT FWD LATERAL L SHAPE. REPAIRED FRAME 65 SHEAR CLIP BETWEEN STRINGER 15L AND 18L. CORROSION FOUND TO BE LEVEL 2.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 34,644 hrs · 22,274 cycles

CORROSION - BAGGAGE DOOR CUTOUT AFT LATERAL L SHAPE. REPAIRED BAGGAGE DOOR CUTOUT AFT LATERAL L SHAPE. CORROSION FOUND TO BE LEVEL 2.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 34,644 hrs · 22,274 cycles

CORROSION - SERVICE DOOR THRESHOLD. REMOVED AND REPLACED SERVICE DOOR THRESHOLD. CORROSION FOUND TO BE LEVEL 2

Part: BRACKET — CORRODED · corrosion level 2 · airframe 34,644 hrs · 22,274 cycles

CORROSION AT CENTER LOWER BRACKET ON FWD END OF VENTRAL FUEL CELL. COMPLIED WITH PERMANENT REPAIR REMOVAL/REPAIR OF CORROSION AT CENTER LOWER BRACKET ON FWD END OF VENTRAL TANK SKIN.

Part: LIGHT — WORN (CABIN) · airframe 34,368 hrs · 22,032 cycles

EMERGENCY EXIT LIGHT STRIP NEAR GALLEY WORN OUT. REMOVED AND REPLACED STRIP LIGHT. NO DEFECTS NOTED AT THIS TIME.

Part: CLAMP — LEAKING (CABIN PRESSURE) · airframe 33,886 hrs · 21,605 cycles

LOST PRESSURIZATION INFLIGHT PACK 1&2 VALVE FAIL MESSAGE DISPLAYED BLEED 1 OVERTEMP EICAS MESSAGE DISPLAYED TEMPORARILY TROUBLESHOT PACK 1 VALVE, FOUND NUMEROUS CLAMPS LEAKING. TIGHTEN CLAMPS AS REQUIRED NO FURTHER LEAKS REF. TROUBLESHOT BLEED 1 OVERTEMP - FOUND FAN AIR VALVE SCREEN FILTER DIRTY. REMOVED AND REPLACED FAN AIR FILTER OPS CHECK AND LEAK CHECK GOOD. PERFORMED ENGINE PNUEMATIC CHECK. OPS CHECK GOOD NO FURTHER DEFECTS NOTED. PACK 2 ON MEL- CLEARED MEL

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 32,477 hrs · 20,173 cycles

LAV SMOKE WARNING IN FLIGHT. PERFORMED LAV SMOKE DETECT OPS. OPS CHECK SAT. INSPECTED LAV SMOKE DETECT SENSOR. NO DEFECTS NOTED AT THIS TIME.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 31,937 hrs · 19,659 cycles

NR 1 HYD SYSTEM FLUID LOW AT BOTTOM OF CAUTION RANGE. ON TOUCH DOWN, THE NR 1 HYDRAULIC SYSTEM PUMP FAILED DURING THE APPLICATION OF THE BRAKES. POST FLIGHT WALKAROUND FOUND A LARGE PUDDLE OF HYDRAULIC FLUID. R & R THE NR 1 EDP. THE NR 1 HYD PRESSURE TRNSMITTER O-RING. OPS AND LEAK CHECKED GOOD.

Part: FLAPPER VALVE — LEAKING (FUEL SYSTEM) · airframe 29,454 hrs · 17,767 cycles

ATC ADVISED THE CREW THAT FUEL WAS LEAKING OUT OF THE WING DURING CLIMBOUT. THE ACFT RETURNED, WHERE OT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE RT WING OTBD FLAPPER, CHECK, VALVE, LEAK CHECKED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COFFEEMAKER — INOPERATIVE (GALLEY) · airframe 27,918 hrs · 16,639 cycles

PILOT REPORTED STRONG ELECTRICAL SMELL IN GALLEY ASSOCIATED WITH USE OF F/O SIDE COFFEE POT. MAINTENANCE CLEANED NR 2 COFFEE TRAY AND DRAINS THEN R & R NR 1 COFFEE BREWER WITH OPS CHECK GOOD. NO SMELL NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 24,135 hrs · 14,154 cycles

THE CREW REPORTED A ACRID FOG IN COCKPIT WHICH OCCURED SIMULTANEOUSLY WITH THE LAVATORY SMOKE ECIAS MESSAGE. FOG NOT SMOKE BUT WAS HIGHLY VISIBLE AND VERY PUNGENT. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. CARBON SEAL DAMAGED. OPS CHECKED LAV SMOKE DETECTOR, GOOD.

Part: WARNING MESSAGE — FALSE INDICATION (LAVATORY SMOKE) · airframe 24,134 hrs · 14,153 cycles

THE CREW REPORTED A LAVATORY SMOKE MESSAGE ON ECIAS FOR ONE MINUTE AFTER TAKEOFF. INSPECTION REVEALED NO SMOKE. MAINTENANCE INSPECTED AND TESTED LAVATORY SMOKE DETECTOR. NO DEFECTS WERE FOUND.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO BAY) · airframe 20,486 hrs · 11,806 cycles

AFTER TAKEOFF, MOMENTARY BAG SMOKE EICAS MESSAGE AND CARGO WARNING LIGHT. EICAS MESSAGE WENT AWAY IMMEDIATELY, WARNING LIGHT REMAINED ILLUMINATED. NO FIRE OR SMOKE OBSERVED THROUGH SIGHT WINDOW IN LAV. MX RESET AND PERFORMED AN OPS CHECK OF THE BAG SMOKE DETECTION SYS SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 19,043 hrs · 10,849 cycles

ACFT IS IN FOR A 4C INSPECTION, WHEN INSPECTION FOUND THE LAV AREA RT OMEGA BEAM TOP CAP HAD AREAS OF CORROSION. MX DRILLED AND COUNTERSUNK A NEW TOPCAP AFTER REMOVAL OF THE OLD TOPCAP IAW SRM 51-20-03 AND 51-40-06; R & R THE TOPCAP IAW SRM 51-40-02.

Part: FRAME — CORRODED · corrosion level 2 · airframe 19,043 hrs · 10,849 cycles

FRAME 80, CORRODED UNDER APU SHUNT CONNECTOR PLATE. BLENDED OUT DAMAGED AREA AND PERFORMED NDT FOR CRACKS. PROTECTED WITH ALODINE, APPLIED HIGH SOLIDS EPOXY TO THE REWORKED AREAS.

Part: ENGINE — LEAKING (NR 2) · airframe 15,733 hrs · 8,820 cycles

THE CREW REPORTED A LAV SMOKE MESSAGE DURING CRUISE. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR 2 ENGINE AND OPS CHECKS WERE GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 15,641 hrs · 8,763 cycles

FLIGHT 2746 - YQB - FLIGHT CREW REPORTED LAV SMOKE WARNING INDICATION ON CLIMBOUT. CREW FOUND NO SMOKE. SYSTEM WAS RESET SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LINE — CHAFED (NR 1 ENGINE) · airframe 15,047 hrs · 8,436 cycles

THE CREW REPORTED ENGINE 1 SHOWING 3 QUARTS OIL REMAINING IN CRUISE. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 1 ENGINE OIL TUBE (PUMP TO FCOC) LEAKING. THE FIRE LOOP WAS CHAFING INTO OIL TUBE CAUSING THE LEAK. THE OIL TUBE AND FIRE LOOP WERE REPLACED.

Part: HYDRAULIC LINE — CHAFED (NR 1 ENGINE) · airframe 14,817 hrs · 8,303 cycles

CLE FLT 2401 THE CREW REPORTED A HYDRAULIC SYSTEM 1 FAIL MESSAGE ALONG WITH LOW QUANTITY MESSAGE ON DESCENT. SYSTEM 1 SHOWING EMPTY ON THE MFD. MAINTENANCE INSPECTED AND REPLACED THE NR 1 HYDRAULIC PUMP PRESSURE HOSE AND ENGINE DRIVEN PUMP. OPERATIONAL CHECKS WERE GOOD.

Part: THRUST REVERSER — DEFECTIVE (NR 1 ENGINE) · airframe 8,140 hrs · 14,537 cycles

TYS - A/C ABORTED TAKEOFF, GOT A E-! DISAGREE MESSAGE ON T/O ROLL EN ROUTE FROM BNA TO EWR. A/C RETURNED TO GATE AND TR MEL. MAINTENANCE REMOVED AND REPLACED THE NR 1 TR IAW TC 6878001, OPS CHECK GOOD, MEL CLEARED AND WAS BACK IN SERVICE.

Part: PCU — DEFECTIVE (RUDDER) · airframe 13,310 hrs · 7,465 cycles

IAH - FLIGHT 2668, THE CREW REPORTED A RUDDER 1 & 2 INOP MESSAGE IN FLIGHT THREE TIMES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RUDDER PCU, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HUB CAP — DAMAGED (RT MLG) · airframe 13,048 hrs · 7,328 cycles

SHV - RIGHT MLG DID NOT RETRACT AFTER TAKEOFF. FOUND RIGHT I/B MLG HUB CAP DAMAGED. REMOVED AND REPLACED HUB CAP IAW EMB 145 XR AMM 32-49-02. PERFORMED OPS CHECK IAW EMB 145 XR AMM 32-30-00. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 9,530 hrs · 5,445 cycles

FLIGHT 3053 - EWR - FLIGHT CREW REPORTED SMOKE IN COCKPIT AND EICAS INDICATION FOR LAV SMOKE. EWR MX RAN ENGINES AND BOTH PACKS, INSPECTED DUCTS AND NO FAULTS OR SMOKE NOTICED. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SHV - DURING C-CHECK LT OMEGA BEAM LOWER FLANGE HAS CORROSION BETWEEN FR 20-24. MAINTENANCE REPAIRED LT OMEGA BEAM LOWER FLANGE BETWEEN FR 20-24 IAW EMB 145 XR SRM 53-00-10 FIGURE 201 SHEET 2. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: THRESHOLD — CORRODED (CARGO DOORWAY)

SHV - DURING C-CHECK CARGO DOOR THRESHOLD HAS CORROSION IN MULTIPLE AREAS AROUND AND BOTTOM CUT OUT ANGLE. MAINTENANCE REMOVED AND REPLACED CARGO DOOR THRESHOLD LOWER BEAM IAW EMB 145 XR SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,177 hrs · 5,224 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM FR 18-23 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM 18-23 IAW EMB 145 XR SRM 51-40-02 AND EC 5320-01140. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS)

FLT 7696 - LAP - FLIGHT CREW REPORTED FLAP OVERSPEED AT 45 DEGREES, 171 KNOTS FOR 3 SECONDS. MAINTENANCE FERRY FLIGHT TO ONT BUT IT HAD TO CLEAR CUSTOMS IN LAX. MAINTENANCE AND INSPECTION DEPARTMENT PERFORMED NDT AND VISUAL INSPECTION ON FLAP TRACKS. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: BLEED VALVE — FAILED (NR 1 ENGINE) · airframe 7,829 hrs · 4,329 cycles

FLT 7771 - RNO TO RNO - DURING TAKEOFF FLIGHT CREW REPORTED BLD 1 VALVE FAIL ON EICAS AT 60 KNOTS. MX PERSONNEL REMOVED AND REPLACED E1 BLD VALVE OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: RELAY — FAILED (SMOKE DETECTION) · airframe 7,786 hrs · 4,300 cycles

FL 7753 - LAX TO LAX - DURING PRE-FLIGHT, FLIGHT CREW REPORTED BAGGAGE SMOKE DETECTION INOP. MX REMOVED AND REPLACED RELAY K0630 OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: CLAMP — MISSING (CUSTOMER AIR) · airframe 7,762 hrs · 4,289 cycles

FLT 7650 - LAX TO LAX - DURING CRUISE FLIGHT CREW REPORTED E1 HIGH ITT. AIRCRAFT RETURNED TO BLOCK WITH NO INCIDENT. MX PERSONNEL FOUND COSTUMER SERVICE DISCHARGE TUBE CLAMP MISSING, CAUSING GASKET ALSO MISSING. MX INSTALLED A NEW CLAMP AND GASKET OPERATIONALLY CHECK HIGH POWER RUNS SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN TO SERVICE.

Part: ACM — MALFUNCTIONED (NR 1) · airframe 5,522 hrs · 2,932 cycles

IAH - FLIGHT 2281, AFTER TAKEOFF WHEN PACKS SELECTED ON, COCKPIT AND CABIN IMMEDIATELY FILLED WITH SMOKE AND PACK 2 VALVE FAIL ADV ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER 1 ACM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 1,097 hrs · 598 cycles

IAH - FLIGHT 3097, THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT WITH NO ASSOCIATED SMOKE IN THE BAGGAGE COMPARTMENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE AFT BAGGAGE COMPARTMENT SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DAU — INOPERATIVE (NR 2) · airframe 1,097 hrs · 598 cycles

IAH - FLIGHT 3097, THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT WITH NO ASSOCIATED SMOKE NOTICED IN THE BAGGAGE COMPARTMENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 2 DAU, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 1,093 hrs · 597 cycles

IAH - FLIGHT 2086, THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT. THE CREW DISCHARGED THE CARGO FIRE BOTTLES AS A PRECAUTION, AND RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REPLACED THE FORWARD BAGGAGE SMOKE DETECTOR, AND BOTH CARGO FIRE BOTTLES. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — STICKING (COCKPIT) · airframe 792 hrs · 436 cycles

CLE - FLIGHT NR 2674, THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT 5 OR 6 TIMES. THE WARNING WENT AWAY AFTER 20-30 SECONDS EACH TIME. MAINTENANCE INSPECTED AND REPLACED RELAYS KO630, KO625, AND KO629. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHT) · airframe 193 hrs · 100 cycles

RIC - DURING ROUTINE INSPECTION, ROW 12 CEILING EMERGENCY LIGHT AND OVERWING EMERGENCY LIGHT DIM/WADE OUT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY. OPERATIONAL TEST WAS PERFORMED SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.