N21197

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 41,072 hrs · 27,901 cycles

MULTIPLE INTERIOR EMERGENCY LIGHTS INOPERATIVE (ROW 18). REMOVED AND REPLACED #3 BATTERY PACK. OPS CHECK SAT

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 41,018 hrs · 27,852 cycles

EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY #4. OPS CHECK SAT, EMERGENCY LIGHTS BACK TO NORMAL OPERATION

Part: INVERTER — INOPERATIVE (ZONE 200) · airframe 40,589 hrs · 27,456 cycles

FWD CEILING EMERGENCY SIGN AT ROW 18 INOPERATIVE. REMOVED AND REPLACED FWD CEILING EMERGENCY EXIT SIGN INVERTER #6. OPS CHECK SAT.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 40,531 hrs · 27,402 cycles

FWD OVERHEAD EXIT SIGN AT EMERGENCY EXIT ROW INOPERATIVE. REMOVED AND REPLACED EXIT LOCATING SIGN. OPS CHECK SAT.

Part: FLOOR SUPPORT — CRACKED (FRMS 21-23) · airframe 40,039 hrs · 26,939 cycles

CF1, UNDERFLOOR, LH OMEGA BEAM NO 1 INBD SIDE, CRACK SUSPECTED AT FR21, 22, AND 23. CF1, LH OMEGA BEAM NO 1 INBD SIDE, CUTOUT PERFORED AT FR 21, 22, 23. LH OMEGA NO 2 INBD SIDE, FR21, 22, 23 REPAIRED

Part: SKIN — CRACKED (FRM 77-80 S3-9R) · airframe 40,039 hrs · 26,939 cycles

RH EXTERNAL FUSELAGE, BTW FRAME 77-80 AND BTW STR 3R-9R, CRACKS (6X) FOUND AROUND FASTENERS. 4 BUSHINGS REPAIRS AND A REPAIR DOUBLER ON RH REAR FUSELAGE II SKIN, BTW FR 77 & 79 AND BTW STR 3R-7R

Part: FLOOR SUPPORT — CRACKED (FRMS 24-25) · airframe 40,039 hrs · 26,939 cycles

CF2, UNDERFLOOR, LH OMEGA BEAM NO 2, 2 CRACKS SUSPECTED AT FR24,25. 2 REPAIR DOUBLERS ON LH CENTER FUSELAGE 1 OMEGA BEAM, ON INBD VERTICAL FLANGE AT FR24 & 25

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 40,039 hrs · 26,939 cycles

LH EXTERNAL FWD FUSELAGE, SCRATCH FOUND LOWER GPU POWER CONNECTOR AT REPAIR DOUBLER. ON LH EXTERNAL FWD FUSELAGE, LOWER GPU POWER CONNECT AT REPAIR DOUBLER SCRATCH BLEND OUT OF LIMITS. EXISTING DOUBLER REMOVED FOR REPLACEMENT. REPAIR DOUBLER FABRICATED. REPAIR DOUBLER INSTALLED ON LH EXTERNAL FWD FUSE LOWER GPU POWER CONNECTOR.

Part: SUPPORT ANGLE — CRACKED (FRMS 67-68 S4R) · airframe 40,039 hrs · 26,939 cycles

RF1, CARGO DOOR LIFTING AND LOWERING MECHANISM AT RH SIDE, UPPER HORIZONTAL SUPPORT ANGLE BTW FR 67-68 AND AT STR 4R FOUND CRACKED. RF1, CARGO DOOR LIFTING AND LOWERING MECHANISM AT RH SIDE UPPER HORIZONTAL SUPPORT ANGLE BTW FR 67-68 AT STR 4R REPLACED.

Part: GUSSET — CORRODED (FRMS 24-30) · corrosion level 2 · airframe 40,039 hrs · 26,939 cycles

CF2, UNDERFLOOR, LH GUSSET NO 2 BTW FR 24-30 FOUND CORRODED. CF2, UNDER FLOOR, LH GUSSET #2 BTW FR 24-30 CORROSION BLENDED AND FOUND OUT OF LIMIT. CF2, UNDER FLOOR, LH GUSSET NO 2 BTW FR 14-30 IS REMOVED. CF2, UNDER FLOOR LH GUSSET NO 2 BTW FR 24-FR 30 INSTALLED

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 40,039 hrs · 26,939 cycles

COCKPIT ABOVE RH WINDSHIELD, HORIZONTAL RIB-OVERHEAD PANEL FOUND CRACKED. IN COCKPIT ABOVE RH WINDSHIELF HORIZONTAL RIB-OVERHEAD PANEL REPAIRED AND INSTALLED

Part: FLOOR SUPPORT — CRACKED (FRM 41) · airframe 40,039 hrs · 26,939 cycles

CENTER FUSE 3, UNDER FLOOR STRUCTURE, BRACKET RH OMEGA BEAM AT FRAME 41 FOUND CRACKED. IN CF3, UNDER FLOOR STRUCTURE, ON RH OMEGA BEAM AT FR41, SUPPORT BRACKET REPLACED

Part: SHEAR TIE — CRACKED (FRM 68 S7-8L) · airframe 40,039 hrs · 26,939 cycles

RF1, LH SHEAR CLIP AT FR68 BTW STR 8L-7L FOUND CRACKED. RF1, LH SHEAR CLIP AT FR68 BTW STR 8L-7L REMOVED AND REPLACED

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 40,039 hrs · 26,939 cycles

COCKPIT WINDSHIELD OVERHEAD PANEL FR PN 123-07751-005 FOUND CRACKED. LH COCKPIT OVERHEAD PANEL FR PN 123-07751-005 REPAIR PERFORMED.

Part: LATCH — BROKEN (RADOME) · airframe 40,039 hrs · 26,939 cycles

FWD FUSELAGE 1, FR 1A LH & RH UPPER RADOME LATCHE FAIRING BROKEN. LH AND RH UPPER RADOME LATCHE REMOVED AND REPLACED

Part: FLOOR SUPPORT — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 40,039 hrs · 26,939 cycles

CENTER FUSELAGE IV, UNDERFLOOR, RH GUSSET BTW FRAME 59-61 FOUND CORRODED. CF4 RH GUSSET BTW FR 59-61 REMOVED AND REPLACED

Part: SKIN — CRACKED (FRMS 77-80 S3-9L) · airframe 40,039 hrs · 26,939 cycles

LH EXTERNAL FUSELAGE, BTW FRAME 77-80 AND STR 3L-9L, CRACKS (X5) FOUND AROUND FASTENERS. LH EXTERNAL FUSE, PAINT REMOVED BTW FR 77-80 AND BTW STR 3L-9L. LH EXTERNAL FUSELAGE, BTW FRAME 77-80 AND STR 3L-9L. LH EXTERNAL FUSELAGE BTW FR 77-80 STR 3L-9L FOUR REPAIR BUSHINGS INSTALLED.

Part: FLOOR SUPPORT — CORRODED (FRM 59) · airframe 40,039 hrs · 26,939 cycles

CENTER FUSELAGE IV, UNDERFLOOR, CENTER OMEGA BEAM AT FRAME 59, CORROSION FOUND UNDER NUT PLATE. CENTER OMEGA BEAM REPAIRED AT FR59 AND FR60

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,039 hrs · 26,939 cycles

CENTER FUSE 3, UNDER FLOOR STRUCTURE, LH SILL 5 FOUND CORRODED. CENTER FUSE 3, UNDER FLOOR STRUCTURE LH SILL 4 BLEND OUT OF LIMITS. AT CENTER FUSE 3, LH SILL 5 REPLACED

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,039 hrs · 26,939 cycles

CENTER FUSELAGE 4, RH SILL 6 CORRODED. ON CENTER FUSELAGE 4, RH SILL BLEND OUT CORROSION OUT OF LIMITS. CENTER FUSELAGE 4, RH SILL 6 REMOVED. ON CENTER FUSELAGE 4, RH SILL, 6 INSTALLED

Part: SHEAR TIE — CRACKED (FRM 73 S7-10R) · airframe 40,039 hrs · 26,939 cycles

RF1, RH SHEAR CLIP AT FR 73 BTW STR 7R-10R FOUND CRACKED. RF1, RH SHEAR CLIP AT FR73 BTW STR 7R-10R REMOVED, REPLACED WITH NEW PART

Part: GUSSET — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 40,039 hrs · 26,939 cycles

CF4, UNDER FLOOR, CENTER GUSSET BTW FRAME 59-61 FOUND CORRODED. CTR GUSSET BTW FR59-61 REPLACED.

Part: SHEAR TIE — CRACKED (FR 61 S6-7R) · airframe 40,039 hrs · 26,939 cycles

CENTER FUSELAGE IV, SHEAR CLIP CRACKED AT FRAME 61 BTW 7R-6R CENTER FUSELAGE IV SHEAR CLIP AT FR 61 BTW STR 7R-6R REPLACED (MADE REPAIR PART), INSTALLED WITH SOLID RIVETS.

Part: ANGLE — CRACKED (LT WG-BDY FAIRIG) · airframe 40,039 hrs · 26,939 cycles

L/H WING TO BODY FAIRING UPPER ANGLE #1 AND #3 FOUND CRACKED. ON L/H WING TO BODY FAIRING UPPER ANGLE #1 AND #3 REPAIRED.

Part: SHEAR TIE — CRACKED (FRM 56 S15-16L) · airframe 40,039 hrs · 26,939 cycles

SHEAR CLIP CRACKED BTW STR 15L-16L AT FR 56 SHARE CLIP AT FR56 BTW STR 15L-16L REPLACED

Part: ANGLE — CRACKED (FRMS 67-68 S3-4R) · airframe 40,039 hrs · 26,939 cycles

VERTICAL U-SHAPE ANGLE BTW FR 67-68 AND BTW STR 3-4R CRACKED. VERTICAL U-SHAPE ANGLE BTW FR 67-68 AND BTW 3R-4R REPLACED.

Part: SHEAR TIE — CRACKED (FRM 73 S15-16L) · airframe 40,039 hrs · 26,939 cycles

RF1, L/H SHEAR CLIP AT FR73 BTW STR 15L-16L FOUND CRACKED. L/H SHEAR CLIP AT FR73 BTW STR 15L-16L REPLACED.

Part: SHEAR TIE — CRACKED (FRM 65 S18-19L) · airframe 40,039 hrs · 26,939 cycles

REAR FUSELAGE 1, UNDR FLOOR, SHEAR CLIP CRACKED AT FRAME 65 BTWN STR 19L-18L SHEAR CLIP AT FR 65 STR 19L-18L REPLACED

Part: SHEAR TIE — CRACKED (FR 71 S17-18L) · airframe 40,039 hrs · 26,939 cycles

REAR FUSELAGE 1, UNDER FLOOR, SHEAR CLIP CRACKED AT FRAME 71 BTWN STR 18L-17L SHEAR CLIP AT FR71 BTW STR17L-18L REPLACED.

Part: SHEAR TIE — CRACKED (FR 72 S17-18L) · airframe 40,039 hrs · 26,939 cycles

REAR FUSELAGE, UNDER FLOOR, SHEAR CLIP CRACKED AT FRAME 72 BTW STR 18L-17L. REAR FUEDLAGE, UNDER FLOOR, SHEAR CLIP AT FRAME 72 BTW STR 18L-17L REPLACED WITH NEW PART.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 40,039 hrs · 26,939 cycles

CARGO DOOR LIFTING AND LOWERING MECHANISI, FWD BOX SUPPORT CRACKED BTW FR 61-62 AND BTW STR 3R-4R CORGO DOOR LIFTING AND LOWERING MECHANISM FWD BOX SUPPORT REPLACED

Part: SHEAR TIE — CRACKED (FRM 66 S6-7L) · airframe 40,039 hrs · 26,939 cycles

RF1, L/H SHEAR CLIP AT FR66 BTW STR 6L-7L FOUND CRACKED RF1, L/H SHEAR CLIP AT FR66 BTW STR 6L-7L REMOVED AND REPLACED.

Part: SHEAR TIE — CRACKED (FRM 26 S15-16R) · airframe 40,039 hrs · 26,939 cycles

CF2, UNDERFLOOR, R/H SHEAR CLIP AT FR 26 BTW STR 15R-16R FOUND CRACKED. R/H CHEAR CLIP AT FR26 BTW STR 15R-16R REMOVED AND REPLACED.

Part: SHEAR TIE — CRACKED (FRM 24 S15-16L) · airframe 40,039 hrs · 26,939 cycles

CF2 UNDERFLOOR , L/H SHEAR CLIP AT FR24 BTW STR 15L-16L FOUND CRACKED.CF2, UNDERFLOOR, L/H SHEAR CLIP AT FR 24 BTW STR 15L-16L REMOVE AND REPLACE WITH NEW PART.

Part: SHEAR TIE — CRACKED (FRM 26 S15-16L) · airframe 40,039 hrs · 26,939 cycles

CF2, UNDERFLOOR, L/H SHEAR CLIP AT FR26 BTW STR 15L-16L FOUND CRACKED REMOVED AND REPLACED L/H SHEAR CLIP AT FR26 BTW STR 15L-16L

Part: SHEAR TIE — CRACKED (FR 27 S15-16R) · airframe 40,039 hrs · 26,939 cycles

CF2, UNDERFLOOR, R/H SHEAR CLIP AT FR27 BTW STR 15R-16R FOUND CRACKED AT FR27 BTW STR 15R-16R, NEW SHEAR CLIP INSTALLED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,039 hrs · 26,939 cycles

CF1, UNDERFLOOR, PASSENGER DOOR, BOTH LOWER U SHAPE ANGLE FOUND CORRODED. CF1, UNDERFLOOR, PASSENGER DOOR, BOTH LOWER U SHAPE ANGLE BLENDED OUT OF LIMITS. ON CF1, UNDER FLOOR PASSENGER DOOR BOTH LOWER U SHAPE ANGLE REMOVED. CF1 UNDER FLOOR, PASSENGER DOOR, BOTH LOWER U SHAPE ANGLE INSTALLED

Part: SHEAR TIE — CRACKED (FR 27 S15-16L) · airframe 40,039 hrs · 26,939 cycles

L/H SHEAR CLIP CRACKED AT FR27 BTW STR 15L-16L L/H SHEAR CLOP MADE REPAIRED PART AT FR27 BTW STR 15L16L REPLACES.

Part: SHEAR TIE — CRACKED (FRM 25- S15-16R) · airframe 40,039 hrs · 26,939 cycles

CF2, UNDERFLOOR, R/H SHEAR CLIP AT FR25 BTW STR 15R-16R FOUND CRACKED NEW SHEAR CLIP AT FR 25 BTW STR 15R-16R INSTALLED

Part: FLOOR SUPPORT — CORRODED (FRS 19-23) · corrosion level 2 · airframe 40,039 hrs · 26,939 cycles

CF1, UNDERFLOOR, L/H SILL NO.1 BTW FR 19-23 FOUND CORRODED ON CF1. UNDERFLOOR, L/H SILL NO1 BTW FR 19-23 CORROSION REMOVED. AT FR19, L/H CROSS BEAM AND T ABGLE REMOVED FOR ACCESS. L/H SILL BTWEEM 18-23 REMOVED FOR REPLACEMENT.CF1. UNDERFLOOR, L/H SILL NO1 BTW FR 19-23 REPLACED WITH NEW PART. CF1 L/H CROSS BEAM AND T ANGLE AT FR 19 REINSTALLED.

Part: DOOR SILL — CORRODED (CABIN) · corrosion level 2 · airframe 40,039 hrs · 26,939 cycles

CF1, UNDERFLOOR, SERVICE DOOR AFT SILL FOUND CORRODED. CF1 UNDERFLOOR SERCIVE DOOR AFT SILL CORROSION AREA CUT OUT, CF1 UNDERFLOOR SRVICE DOOR AFT SILL REPAIRED.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 40,039 hrs · 26,939 cycles

CF3, UNDER FLOOR STRUCTURE, LH SILL 4 FOUND CORRODED. CF3, UNDER FLOOR L/H SILL, #4 BLENDED OUT OUT LIMIT. CF3 L/H SILL #4 REMOVED FOR REPLACEMENT. AT CF3, UNDER FLOOR STRUCTURE, LH SILL 4 REPLACED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,039 hrs · 26,939 cycles

CENTER FUSE 3, UNDER FLOOR STRUCTURE, RH SILL 3 FOUND CORRODED R/H SILL #3 REMOVED FOR REPLACEMENT. ON CENTER FUDE 3, RH SILL 3 REPLACED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,265 hrs · 26,183 cycles

BURNING SMELL IN CABIN ON APPROACH BETWEEN ROWS 5-18. INSPECTED ACM, NO DEFECTS NOTED. PERFORMED GROUND HIGH POWER ENGINE RUNS AND PERFORMED FIM. NO DEFECTS NOTED

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 38,500 hrs · 25,488 cycles

SUPPLEMENTAL (NEW) INFORMATION: REMOVED AND REPLACED MAIN DOOR SEAL FOUND ORIGINAL SEAL TO BE UNEVENLY PLACED AT SEAL TRACK UPTO PRESS LEAK CHECK. OPS/LEAK CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,102 hrs · 25,138 cycles

FWD AISLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FWD AISLE EMERGENCY LIGHT BULB. OPS CHECK SAT.

Part: NONE — NONE · airframe 37,552 hrs · 24,642 cycles

EMERG EXIT OVERHEAD SIGN NOT PROPERLY CONNECTED (AISLE AFT FACING). RESECURED MERG EXIT SIGN OVERHEAD AT EXIT ROW

Part: NONE — NONE · airframe 37,368 hrs · 24,478 cycles

EMERGENCY EXIT SIGN IN CABIN FALLING OFF (CENTER CEILING). RESECURED CENTER CABIN CEILING EMERGENCY EXIT SIGN. OPS CHECK SAT. NO FURTHER DEFECTS NOTED AT THIS TIME

Part: NONE — NONE · airframe 36,766 hrs · 23,963 cycles

OVERHEAD EMERGENCY EXIT SIGN FALLING OFF. RESECURED EMERGENCY EXIT SIGN. .

Part: LIGHT — UNSECURE (GALLEY) · airframe 36,207 hrs · 23,436 cycles

FLOOR PATH LIGHTING LOOSE AROUND GALLEY. RE-SECURED TO FLOOR WITH DOUDLE SIDE CARPET TAPE AS REQUIRED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,714 hrs · 22,989 cycles

LH AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE AND RH WING LIGHT INSPECTION INOPERATIVE. R AND R LH AFT EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT. R AND R RH WING INSPECTION LIGHT LAMP ASSEMBLY. OPS CHECK SAT.

Part: FRAME — CORRODED (FRM 65) · airframe 35,711 hrs · 22,986 cycles

FRAME 65 BTW LH STR 11-15 FOUND CORRODED. FRAME Z REPLACED

Part: SUPPORT — CORRODED (FRAME46) · corrosion level 2 · airframe 35,711 hrs · 22,986 cycles

CF3, L/H OMEGA BEAM INBD FLANGE CORRODED FROM FR46 TO SKIN JUNCTION (FR52-53) - CORROSION LEVEL 2. OMEGA BEAM REPLACED

Part: VORTILON — CRACKED (LT WING LE) · airframe 35,711 hrs · 22,986 cycles

L/H L/E NO 3 UNDER VORTILLONS NO 3 ET NO 4 CRACK FOUND. LH WING LEADING EDGE III CRACK UNDER #3 AND #4 VORTILLONS REPAIRED

Part: WING — CRACKED · airframe 35,711 hrs · 22,986 cycles

LH WING LEADING EDGE III CRACK UNDER #2 VORTILLON REQUIRES PERMANENT REPAIR WITHIN 750 FC. LH WING LEADING EDGE III CRACK UNDER #2 VORTILLON REPAIRED

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,443 hrs · 27,454 cycles

CF3, CTR OMEGA BEAM INBD FLANGE CORRODED FROM FR46 TO SKIN JUNCTION (FR52-53) - CORROSION LEVEL 2. OMEGA BEAM REPLACED

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 35,711 hrs · 22,986 cycles

RH OVERWING EMERGENCY DOOR FWD L-SHAPE ANGLE FOUND CRACKED AT 2 LOCATIONS. RH OVERWING EMERGENCY DOOR, FWD L-SHAPE ANGLE REPLACED AND SKIN MISALIGNED HOLES REPAIRED

Part: DIODE — SHORTED (GPU) · airframe 35,711 hrs · 22,986 cycles

WHEN DISCONNECTING THE GROUND POWER UNIT, THE GPU AVAILABLE LIGHT AND ALL CABIN LIGHTS STAY ON. SHORTLY BURNT SMELL APPEARS MAIN BATTERIES DISCONNECT FOR SAFETY. TROUBLESHOOTING CARRIED OUT, FOUND DIODE CR046 AND SOME WIRES BURNT, CR0465 SHORT CIRCUIT AND THE BACK UP BATTERY VOLTAGE TOO LOW. DIODE REPLACED AND WIRING REPAIRED. FUNCTIONAL CHECK OF ALL AFFECTED SYSTEM IN PROGRESS.

Part: WING — CRACKED · airframe 35,711 hrs · 22,986 cycles

RH WING L/E NO 3. UNDER VORTILLON NO 3 CRACK FOUND. RH WING LEADING EDGE - 3 CRACK UNDER #3 VORTILLON REPAIRED

Part: DOOR — RUSTED · airframe 35,711 hrs · 22,986 cycles

BAGGAGE DOOR LATERAL AFT L-SHAPE CORRODED. CORROSION AT BAGGAGE DOOR LATERAL AFT SHAPED SHEAR CLIP REPAIRED.

Part: YOKE — CRACKED · airframe 35,711 hrs · 22,986 cycles

FOLLOWING NDT INSPECTION ON TASK. 2X CRACK FOUND ON PYLON YOKES UPPER FLANGE 2X HOLE LOCATION. 2 HOLES REWORKED.

Part: SKIN — CHAFED · airframe 35,711 hrs · 22,986 cycles

CHAFFING FOUND ON EXTERNAL RH SKIN BETWEEN FR 67-68 AND BTW STR 7-8 INSIDE ENGINE PYLON. EXTERNAL SKIN BTW FR 67-68 AND BTW STR 7-8 RH SIDE INSIDE ENG. PYLON REPAIRED.

Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 35,711 hrs · 22,986 cycles

BAGGAGE DOOR FWD LATERAL L-SHAPE CORRODED. BAGGAGE DOOR FWD LATERAL L-SHAPE BLENDED OUT OF LIMITS REMOVED. BAGGAGE DOOR FWD LATERAL L-SHAPE REWORKED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,711 hrs · 22,986 cycles

EXTERNAL BAGGAGE DOOR CUTOUT, NICK AND SCRATCHED ON FWD EDGE. EXTERNAL BAGGAGE DOOR CUTOUT, NICK AND SCRATCHES ON FWD EDGE REPAIRED.

Part: SKIN — CRACKED · airframe 35,711 hrs · 22,986 cycles

CRACK SUSPECTED ON EXTERNAL SKIN AT FR 78 BTW LT STR 6-7. ON EXTERNAL SKIN AT FR 78 BTW LH STR 6-7 DOUBLER LOCALLY FABRICATED FOR REPAIR. ON EXTERNAL SKIN AT FR 78 BTW LH STR 6-7 CRACK REPAIRED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,711 hrs · 22,986 cycles

TWO CRACK SUSPECTED ON EXTERNAL SKIN FR 78 BTW RT STR 4-7. RT REAR FUSELAGE SKIN AT FR 78 BTW STR 4R-7R REPAIRED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,182 hrs · 22,526 cycles

LH EXTERIOR OVER WING EMERGENCY LIGHT INOPERATIVE. R&R LH EXTERIOR OVER WING EMERGENCY LIGHT. OPS CHECK SAT.

Part: FCU — MALFUNCTIONED (FUEL SYSTEM) · airframe 34,888 hrs · 22,265 cycles

FUEL LOW LEVEL IN FLIGHT BOTH WINGS. RR WING 1 AND 2 FCU. OPS CHECK SAT. NO FURTHER DEFECTS NOTED. TRANSFERRED FUEL FROM BOTH WINGS. OPS CHECK SAT.

Part: CONTROL UNIT — INOPERATIVE (TE FLAPS) · airframe 34,756 hrs · 22,156 cycles

DURING DESCENT TO 230 SPS ADVANCED AND FLAP LOW SPEED PRESENTED WHEN FLAP 9 SELECTED FLAP FAIL. R&R FECU. OPS CHECK NO DEFECTS NOTED.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 33,565 hrs · 21,075 cycles

MAIN CABIN DOOR AND SERVICE DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. RELAMPED MCD LIGHT. REPAIRED WIRES W716-0007-20 AND W716-0008-20. OPS CHECK GOOD.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 33,446 hrs · 20,987 cycles

LT AND RT OVER WING EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT LT AND RT OVER WING EMERGENCY LIGHTS. FOUND WIRES W170-8278-22 AND W170-8279-22N BROKEN, REPLACED WIRED. OPS CHECK FAILED. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHASSIS ASSEMBLY. OPS CHECK SAT.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 33,406 hrs · 20,952 cycles

LT AND RT OVER WING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. EMERGENCY LIGHT BATTERY CRADLE NR 4 FOUND AT FAULT. R&R EMERGENCY LIGHT POWER SUPPLY CHARGER. OPS CHECK FAILED. T/S BLOWN FUSE IN NR 4 BATTERY POWER SUPPLY. REMOVED LIGHT BULBS AND CHECK FOR SHORTS AND OPENS AT P803 AND P8532. NO DEFECTS NOTED. RESTORED BULBS AND PLUGS, ALL WIRING FOR AIRCRAFT BATTERY SUPPLY NR 4 CHECKS GOOD. SLAVED A NEW EMERGENCY LIGHT INVERTER IN NR 6. OPS CHECK FAILED. T/S OVER WING EXTERNAL EMERGENCY LIGHT CONNECTOR AND FOUND 0 VOLTAGE. R&R BATTER POWER SUPPLY NR 4. OPS CHECK SAT. POWER SUPPLY REMOVED PN BA5-0933-901 SN C03022. PN INSTALLED 11-049 SN 23852 (PART FAILED - REMOVED) PN 100865 SN ID11151 INSTALLED.

Part: SIGN — DETACHED (ROW 18) · airframe 33,242 hrs · 20,814 cycles

OVERHEAD EMERGENCY EXIT SIGN AT ROW 18 FELL DOWN. SECURED EMERGENCY EXIT SIGN AT ROW 18. NO DEFECTS NOTED.

Part: SKIN — DAMAGED (PAX DOOR)

DURING MAINTENANCE INSPECTION THE PASSENGER DOOR SKIN WAS FOUND TO BE DAMAGED AT THE LOWER AFT CORNER. REMOVED THE DAMAGE AND INSTALLED A DOUBLER REPAIR. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE ON 04/27/2018.

Part: DISPLAY — FAULTY (COCKPIT) · airframe 28,514 hrs · 17,088 cycles

THE CREW REPORTED MFD HAD BURNING ODOR AND C/B POPPED. MAINTENANCE REPLACED THE NR 1 MFD. OPS CHECKS WERE GOOD.

Part: UNKNOWN — LEAKING (FUEL SYSTEM) · airframe 28,404 hrs · 17,016 cycles

PAX REPORTED A FOOT WIDE STREAM OF FUEL COMING FROM RT WING FROM THE TAKEOFF TO 3-5 MINUTES AFTER DEPARTURE. MX PERFORMED GVI OF RT WING NO SIGNS OF FUEL LEAK. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,307 hrs · 15,483 cycles

DURING MX INSPECTION THE UPPER ESCAPE HATCH EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE R & R THE NR 4 INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — ODOR (CABIN LIGHTS) · airframe 25,894 hrs · 15,195 cycles

CREW REPORTED A BURNING ODOR NEAR SEAT 24A LIGHT. MAINTENANCE R & R THE WALL LIGHT HARNESS ASSEMBLY AT SEAT 24A WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,205 hrs · 10,770 cycles

RT TOP CAP IN LAVATORY IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED TOP CAP. AIRCRAFT STILL IN C-CHECK.

Part: SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 19,205 hrs · 10,770 cycles

CARGO DOOR CUTOUT LOWER THRESHOLD CORRODED BEYOND LIMITS. REMOVED AND REPLACED CARGO DOOR SILL. AIRCRAFT STILL IN C-CHECK.

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER) · airframe 16,355 hrs · 8,930 cycles

DURING CLIMB THE CREW REPORTED A RUDDER OVERBOOST INDICATION ON THE EICAS DISPLAY. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT WHERE MX REPLACED THE RUDDER NR 1 PRESSURE SWITCH, PERFORMED OPS CHECKS AND CLEARED THE DISCREPANCY.

Part: ENGINE — FAULTY (NR 1) · airframe 15,687 hrs · 8,567 cycles

IAD FLT 5861 THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.

Part: SENSOR — FAULTY (LAVATORY) · airframe 15,555 hrs · 8,460 cycles

ORD FLT 6090 THE CREW REPORTED A LAV SMOKE WARNING MESSAGE IN FLIGHT WITH NO VISIBLE SMOKE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE SENSOR. OPERATIONAL CHECKS WERE GOOD.

Part: FLAPPER VALVE — LEAKING (LT WING) · airframe 14,840 hrs · 8,049 cycles

OMA - THE CREW REPORTED A FUEL LEAK FROM THE LEFT WING DURING CLIMB. THE AIRCRAFT RETURNED TO OMA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAPPER CHECK VALVE AT RIB 19 ON THE LEFT WING, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE WARNING — MALFUNCTIONED (COCKPIT) · airframe 12,904 hrs · 6,978 cycles

FLIGHT 2470 - EWR - FLIGHT CREW REPORTED APU FIRE INDICATION IN FLIGHT AT 29500 AND ATTEMPTED TO START THE APU. FOR APPROX 2-3 SECS, CREW GOT HIGH ITT AND MASTER WARNING, EICAS APU FIRE MESSAGE. CREW RAN QRH AND MESSAGE/INDICATIONS CLEARED WHILE DOING QRH. ACFT LANDED UNEVENTFULLY. EWR MX PERFORM SEVERAL OPERATIONAL CHECKS (FIRE WARNING CHECK, CMC DOWNLOADING, OIL AND FUEL LEAK CHECK, BLEED CHECK) SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: OUTFLOW VALVE — DEFECTIVE (CABIN PRESSURE) · airframe 11,262 hrs · 6,077 cycles

FLIGHT 2223 - EWR - FLIGHT CREW REPORTED EXCESSIVE FLUCTUATION IN CABIN PRESSURE DURING DESCENT AND CABIN RATE ALSO EXCESSIVE. EWR MX REMOVED AND REPLACED THE ELECTRO-PNEUMATIC OUTFLOW VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONNECTOR — DEFECTIVE (SMOKE WARNING)

IAH - FLIGHT 3095, THE CREW REPORTED GETTING A LAV SMOKE MESSAGE ON EICAS FOUR TIMES DURING THE FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED CONNECTORS J8100 AND P8100, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DEFECTIVE (SMOKE WARNING) · airframe 10,693 hrs · 5,761 cycles

IAH - FLIGHT 3095, THE CREW REPORTED GETTING A LAV SMOKE MESSAGE ON EICAS FOUR TIMES DURING THE FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED CONNECTOR J8100 AND P8100, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — DEFECTIVE (SMOKE DETECTION) · airframe 10,689 hrs · 5,759 cycles

IAH - FLIGHT 2865, ON DESCENT, THE CREW REPORTED A LAV SMOKE INDICATION. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, VERIFIED ALL WIRING, AND REMOVED AND REPLACED THE LAV SMOKE DETECTOR PANEL. OPERATIONAL TESTS WERE PERFORMED WITHOUT DEFECT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — ACTIVATED (LAVATORY) · airframe 10,682 hrs · 5,756 cycles

SJD - DURING CRUISE THE CREW REPORTED A LAV SMOKE INDICATION WITH EVIDENCE OF A PASSENGER SMOKING IN THE LAV. THE AIRCRAFT LANDED AT SJD WITH NO INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED OPERATIONAL TESTS OF THE LAV SMOKE DETECTION SYSTEM WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRESSURE SWITCH — CRACKED (ZONE 400) · airframe 10,180 hrs · 5,483 cycles

CLE FLT NR 3143 - THE CREW REPORTED A BLEED VALVE NR 1 FAIL DURING TAKEOFF. ABORTED TAKEOFF AND TAXIED BACK TO GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 HIGH STAGE PRESSURE SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — FAULTY (CABIN) · airframe 10,171 hrs · 5,475 cycles

CLE FLT 2948 THE CREW REPORTED THE EXIT LIGHT AT SEAT 12 BC WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 10,068 hrs · 5,412 cycles

FLIGHT 2900 - EWR - FLIGHT CREW REPORTED THAT AFTER LANDING AND ENGINE NR 2 SHUT DOWN, ELECTRIC SYSTEM SHUT DOWN, NO NOSE STEERING, ACFT HAD TO BE TOWED TO THE GATE. EWR MX RESET ELECTRICAL POWER AND PERFORMED ALL OPERATIONAL TESTS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,538 hrs · 5,113 cycles

SHV - DURING C-CHECK SERVICE DOOR CUTOUT LOWER FRAME CORRODED (CORRODED LEVEL 2) AROUND FASTENER HOLES. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR LOWER CENTER SILL IAW EMB-135/145 SRM 51-40-02 AND CPM 51-21-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,538 hrs · 5,113 cycles

SHV - DURING C-CHECK LT FWD CARGO FLOOR SILL HAS TWO AREAS OF CORROSION (LEVEL 2 LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED LT FWD CARGO FLOOR SILL IAW EMB-145XR SRM 51-40-02 AND EC5320-07137 AND EC5320-01140. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,538 hrs · 5,113 cycles

SHV - DURING C-CHECK RT FORWARD CARGO FLOOR SILL HAS CORROSION (LEVEL 2 LOCAL) IN TWO AREAS. MAINTENANCE REMOVED AND REPLACED FORWARD CARGO SILL IAW EMB-145 SRM 51-40-02 AND 51-20-03 AND EC5320-01140 REV ORIG AND EC5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — GOUGED (AILERON) · airframe 9,538 hrs · 5,113 cycles

SHV - DURING C-CHECK LT AILERON DAMPNER FITTING GOUGED. MAINTENANCE REMOVED AND REPLACED LT AILERON DAMPNER FITTING IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — WORN (SPOILER) · airframe 9,538 hrs · 5,113 cycles

SHV - DURING C-CHECK RT CENTER SPEED BRAKE TO WING BRACKET HAS MIGRATED BUSHING I/B SIDE OF BRACKET. MAINTENANCE REMOVED AND REPLACED RT CENTER SPEED BRAKE TO WING BRACKET IAW EMB-145XR AMM 20-10-01 AND SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — WORN (SPOILER) · airframe 9,538 hrs · 5,113 cycles

SHV - DURING C-CHECK RIGHT O/B GROUND SPOILER TO WING BRACKET HAS MIGRATED BUSHING I/B SIDE OF BRACKET. MAINTENANCE REMOVED AND REPLACED RIGHT O/B GROUND SPOILER TO WING BRACKET IAW EMB-145XR AMM 57-51-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — WORN (SPOILER) · airframe 9,538 hrs · 5,113 cycles

SHV - DURING C-CHECK RIGHT I/B GROUND SPOILER TO WING BRACKET HAS MIGRATED BUSHING ON O/B SIDE OF BRACKET. MAINTENANCE REMOVED AND REPLACED RIGHT I/B GROUND SPOILER TO WING BRACKET IAW EMB-145XR AMM 57-51-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (SPOILER) · airframe 9,538 hrs · 5,113 cycles

SHV - DURING C-CHECK LT GROUND SPOILER O/B HINGE I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED LT GROUND SPOILER O/B HINGE I/B HAT BUSHING IAW EMB-145XR EC5740-01152 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (PAX DOOR) · airframe 9,538 hrs · 5,113 cycles

SHV - DURING C-CHECK PAX DOOR MAIN SWING ARM UPPER ATTACH POINT UPPER AND LOWER HAT BUSHING MIGRATED. MAINTENANCE REWORKED PAX DOOR MAIN SWING ARM UPPER ATTACH POINT UPPER AND LOWER HOUSINGS AND INSTALLED NEW OVERSIZED HAT BUSHINGS IAW EC5210-01085 REV C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (THROTTLE) · airframe 8,901 hrs · 4,767 cycles

FLIGHT 2236 - EWR - DURING APPROACH INTO EWR THE CREW REPORTED THAT THE "FADEC GOES INTO ETO WHEN THE LANDING GEAR IS LOWERED". THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT WHERE MAINTENANCE FOUND THE CONDITION TO BE A NORMAL OPERATION OF THE SYSTEM PER THE ROLLS ROYCE OPERATIONS MANUAL, SECTION 10, PARAGRAPH 1(J).

Part: CONTROL UNIT — FAULTY (HORIZ STAB) · airframe 8,511 hrs · 4,557 cycles

IAH - DURING CLIMB THE FLIGHT CREW REPORTED THAT THE MAIN PITCH TRIM WAS INOPERATIVE. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT TO CORRECT THE DISCREPANCY.

Part: ENGINE — SMOKE (ZONE 400) · airframe 8,144 hrs · 4,355 cycles

IAH - FLIGHT 2371, THE CREW REPORTED A LAV SMOKE INDICATION ON EICAS AFTER TAKEOFF. THE ACFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MX R&R THE NR 2 ENGINE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LOOSE (FUEL SYSTEM) · airframe 6,183 hrs · 3,335 cycles

FLT 0422 - GEG - FLIGHT CREW REPORTED FUEL LEAKING FROM LEFT WING AT FL 340. ONT MX RESECURED LOOSE FLAPPER VALVE IN LEFT WING, OPERATIONALLY AND LEAK CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 4,545 hrs · 2,436 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM CORRODED FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 20 DUE TO OUT OF LIMIT CORROSION. COMPLIED WITH EC 5320-0437 AND 5320-01140. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 144 hrs · 86 cycles

CLE FLIGHT 3033 THE CREW REPORTED THE CABIN REAR CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND RECONNECTED THE CONNECTOR P8644 AT THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: PRESSURE VALVE — FAULTY (ENG OIL TANK) · airframe 121 hrs · 70 cycles

THE CREW REPORTED THE NR 2 ENGINE OIL PRESSURE IN AMBER AND INTERMITTENT RED IN FLIGHT. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE OIL TANK PRESSURE VALVE. OPERATIONAL CHECKS WERE GOOD.