N659BR

Part: STRAP — DAMAGED (BS 559) · airframe 32,314 hrs · 29,583 cycles

FOUND CORROSION ON THE RT STRAP AT BS 559 BETWEEN RBL 36 - 40. REMOVED AND REPLACED THE STRAP IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 574-619) · airframe 32,314 hrs · 29,583 cycles

CORROSION ON LBL 27 FLOOR SUPPORT FROM BS 574 TO 619. REPLACED THE FLOOR SUPPORT IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · airframe 32,314 hrs · 29,583 cycles

TWO SPOTS OF CORROSION ON THE RT FLOOR SUPPORT BETWEEN BS 559+112 TO 574. REMOVED THE CORROSION IAW REO.

Part: DOOR SILL — CORRODED (BS 348-364) · airframe 32,314 hrs · 29,583 cycles

PAX DOOR LOWER SILL BETWEEN FS 348-364 CORRODED. BLENDED THE CORROSION IAW SRM AND REO.

Part: DOOR FRAME — GOUGED (PAX) · airframe 32,314 hrs · 29,583 cycles

GOUGE ON PAX DOOR SURROUND, MATING SURFACE FOR DOOR SEAL BY FWD LATCH PIN SOCKET. PERFORMED REPAIR BY TRIMMING AWAY DAMAGE AND INSTALLING REPAIR STRAP IAW REO.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 32,314 hrs · 29,583 cycles

HORIZONTAL STABILIZER LT LEADING EDGE HAS A DENT ON THE UPPER SIDE AT HSS 67.79. REWORKED THE DENTED AREA IAW REO.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 32,314 hrs · 29,583 cycles

DENT ON RIGHT INBOARD FLAP ON UPPER SURFACE. REPLACED THE SKIN IAW REO.

Part: NOT REPORTED — DENTED · airframe 32,314 hrs · 29,583 cycles

DENT AT BS 271, STRINGER 22R. REPAIRED .

Part: NOT REPORTED — DENTED (BS 258) · airframe 32,314 hrs · 29,583 cycles

DENT FOUND AT BS 258, STRINGER 20R. DRESSED BACK THE DENT TO ORIGINAL CONTOUR IAW REO.

Part: NOT REPORTED — DENTED (BS 690) · airframe 32,314 hrs · 29,583 cycles

DENT FOUND AT BS 690, STRINGER 23L. REPAIRED IAW SRM AND REO.

Part: ADC — FAILED (NR 1) · airframe 30,286 hrs · 27,332 cycles

DURING APPROACH, LOST NR 2 ADC. SWITCHED TO NR 1 AND SHORTLY AFTER LOST THE NR 1 ADC LOSING ALL INDICATIONS. AFTER DESCENDING TO LOWER ALTITUDE THE NR 1 ADC CAME BACK ONLINE. DECLARED AN EMERGENCY. REMOVED AND REPLACED THE NR 1 AND 2 ADC IAW AMM. PERFORMED OPS TEST OF AIR DATA COMPUTER AND LEAK CHECK OF MAIN PITOT AND STATIC SYSTEM IAW AMM. OPS AND LEAK CHECK GOOD.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 28,865 hrs · 25,780 cycles

DENT AT WS113.00 ON THE LT INBD FLAP LOWER SKIN FOUND TO BE OUT OF LIMITS. COMPLETED ALL STEPS OF REPAIR IAW SRM.

Part: DOOR SILL — CORRODED (BS 310-349) · airframe 28,865 hrs · 25,780 cycles

PAX DOOR SILL ANGLE CORRODED FROM FS 310.0 TO FS 349.0. R & R PASSENGER DOOR FLOOR SUPPORT ANGLE IAW SRM.

Part: SKIN — CHAFED (RT WING AILERON) · airframe 28,865 hrs · 25,780 cycles

RIGHT WING OTBD AILERON L/E PANEL 699BB HAS CHAFING ON MULTIPLE AREAS. REPLACED RT AILERON LOWER LEADING PANEL 699BB, PN 601R13031-164 IAW SRM AND REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 28,865 hrs · 25,780 cycles

LEFT INBD FLAP VANE L/E IS CHAFED, OTBD OF THE OTBD VANE ACTUATOR. REMOVED CHAFED OUT OF LIMITS OTBD L/E SECTION OF THE LT INBD FLAP VANE AND INSTALLED NEW L/E SECTION, PN 601R14303-43 IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 28,865 hrs · 25,780 cycles

LEFT INBD FLAP VANE L/E IS CHAFED, OTBD OF THE MIDDLE VANE ACTUATOR. REMOVED CHAFED OUT OF LIMITS MIDDLE L/E SECTION OF THE LT INBD FLAP VANE AND INSTALLED NEW L/E SECTION IAW SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,481 hrs · 22,392 cycles

FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: SENSOR — FAILED (ANTI ICE SYSTEM) · airframe 25,415 hrs · 22,316 cycles

WING ANTI-ICE SENSOR CAUTION MESSAGE. R & R RT WING CONTROL SENSOR IAW AMM. PERFORMED TEST OF NEW RT WING CONTROL SENSOR IAW AMM. R & R RT WING SUFFICIENT HEAT SENSOR IAW AMM. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT WING ANTI ICE) · airframe 25,408 hrs · 22,310 cycles

RT WING ANTI-ICE CAUTION MESSAGE WITH WINGS ON STANDBY. PERFORMED OPS CHECK OF WING ANTI-ICE CONTROL AND INDICATION IAW AMM. DID NOT RECEIVE RT WING ANTI-ICE CAUTION WHILE IN STBY MODE. OPS CHECKED GOOD AT THIS TIME.

Part: BUSHING — GALLED (ENGINE MOUNT) · airframe 25,292 hrs · 22,189 cycles

LEFT ENGINE, YOKE MOUNT LINK BUSHINGS ARE GALLED. R & R LT ENGINE MOUNT YOKE LINK ASSY WITH SERVICEABLE UNIT IAW AMM.

Part: RISER — CORRODED (LT PYLON) · airframe 25,292 hrs · 22,189 cycles

LEFT ENGINE PYLON, FRETTING WEAR ON THE PRODUCTION RISER ON THE OTBD RIB. TREATED FRETTED SURFACE IAW REO.

Part: BUSHING — GALLED (ENGINE MOUNT) · airframe 25,292 hrs · 22,189 cycles

LEFT ENGINE, YOKE MOUNT LINK END BUSHING IS GALLED. R & R LT ENGINE MOUNT YOKE ASSY WITH A SERVICEABLE UNIT IAW AMM.

Part: PIN — GALLED (ENGINE MOUNT) · airframe 25,292 hrs · 22,189 cycles

LEFT ENGINE, YOKE MOUNT UPPER PIN, SN 1145, HAS GALLING MARKS. R & R LEFT ENGINE FORWARD YOKE MOUNT UPPER PIN IAW AMM.

Part: BUSHING — GALLED (ENGINE MOUNT) · airframe 25,275 hrs · 22,175 cycles

THE RIGHT ENGINE YOKE LINK HAS GALLING ON THE BUSHING. R & R RT ENGINE UPPER YOKE LINK AND CLAMP UP BUSHING IAW AMM.

Part: VERTICAL SUPPORT — CRACKED (BS 409) · airframe 24,879 hrs · 21,814 cycles

VERTICAL POST AT FS 409+128, LBL 18. OTBD IS CRACKED IN LOWER RADIUS. REPAIRED VERTICAL POST IAW REO.

Part: VERTICAL SUPPORT — CRACKED (BS 409) · airframe 24,879 hrs · 21,814 cycles

CRACK IN BS 409+128 VERTICAL POST AT BL 0 IN THE RT C-CHANNEL, AFT RADIUS. REPLACED VERTICAL POST IAW REO.

Part: VERTICAL SUPPORT — CRACKED (BS 409) · airframe 24,879 hrs · 21,814 cycles

VERTICAL POST AT FS 409+128, RBL 18, OTBD SIDE IS CRACKED AT LOWER RADIUS. REPAIRED VERTICAL POST IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 521) · airframe 24,879 hrs · 21,814 cycles

LIGHT SURFACE CORROSION AROUND DOME NUT AT FLOOR SUPPORT RBL 40 BS 521. REPAIRED FLOOR SUPPORT IAW REO.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 24,879 hrs · 21,814 cycles

LT FUEL PANEL 540BB OUTER RING HAS CORROSION. REPAIRED PANEL 540BB OUTER RING IAW REO.

Part: FLOOR PANEL — CORRODED (BS 548) · airframe 24,879 hrs · 21,814 cycles

LIGHT SURFACE CORROSION AROUND DOME NUT AT FLOOR PANEL 262DRF, RBL 40, BS 548. C-CHECK, REPAIRED FLOOR ANGLE IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 530) · airframe 24,879 hrs · 21,814 cycles

LIGHT SURFACE CORROSION AROUND DOME NUT AT FLOOR SUPPORT RBL 40, BS 530. REPAIRED FLOOR SUPPORT IAW REO.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 24,879 hrs · 21,814 cycles

RT FUEL PANEL 640BB OUTER RING HAS CORROSION. REPAIRED PANEL OUTER RING IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 536) · airframe 24,879 hrs · 21,814 cycles

LIGHT SURFACE CORROSION AROUND DOME NUT AT FLOOR SUPPORT RBL 40, BS 536. REPAIRED FLOOR SUPPORT IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 518) · airframe 24,879 hrs · 21,814 cycles

LIGHT SURFACE CORROSION AROUND DOME NUT AT FLOOR SUPPORT RBL 40, BS 518. REPAIRED FLOOR SUPPORT IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 505) · airframe 24,879 hrs · 21,814 cycles

LIGHT SURFACE CORROSION AROUND DOME NUT AT FLOOR SUPPORT RBL 40, BS 505. REPAIRED FLOOR SUPPORT IAW REO.

Part: ANGLE — CRACKED (BS 280) · airframe 24,879 hrs · 21,814 cycles

BS 280, RBL 9, INBD ANGLE CRACKED. INSTALLED NEW INBD ANGLE IAW SRM.

Part: ANGLE — CRACKED (BS 280) · airframe 24,879 hrs · 21,814 cycles

BS 280, LBL 9, LT OTBD ANGLE CRACKED. INSTALLED NEW OTBD ANGLE IAW SRM.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 24,879 hrs · 21,814 cycles

RT MLG DOOR L/E LOWER INNER SKIN CHAFED AT SECOND BEND. REPAIRED DOOR IAW REO.

Part: SKIN — CHAFED (LT MLG WW) · airframe 24,879 hrs · 21,814 cycles

LT MLG L/E LOWER INNER SKIN CHAFED AT SECOND BEND. REPAIRED L/E MLG L/E LOWER INNER SKIN CHAFE IAW SRM.

Part: STRUCTURE — DENTED (LT WING) · airframe 23,921 hrs · 20,901 cycles

DENT IN THE LT WING. DENT OUT OF LIMITS IAW FLT#4694 REPAIRED DENT IAW SRM.

Part: UNKNOWN — MALFUNCTIONED (FLIGHT CONTROL) · airframe 22,966 hrs · 19,969 cycles

UNCOMMANDED ROLL TO THE RIGHT WHEN SELECTING FLAPS 45 DEGREES. (FLT 4716) VISUALLY INSPECTED BOTH LEFT AND RIGHT WINGS, FLAPS AND SPOILERS. CLEANED GREASE, SAND AND LOOSE PAINT FROM SPOILERS AND FLAPS IAW AMM. NO DEFECTS NOTED ON WING BODY AT THIS TIME. OPERATED FLAPS, NO VISUAL DIFFERENCE IN EXTENSION NOR RETRACTION LEFT TO RIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,967 hrs · 18,987 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4715) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,907 hrs · 18,931 cycles

AFT CEILING EMERGENCY LIGHT BURNED OUT. (FLT 4773) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,774 hrs · 18,803 cycles

NR 4 LEFT OUTER EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,677 hrs · 18,710 cycles

FURTHEST AFT OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 4705) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,566 hrs · 18,609 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4541) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,511 hrs · 18,558 cycles

NR 7 EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,431 hrs · 18,485 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,306 hrs · 18,367 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4456) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,238 hrs · 18,303 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) REPLACED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,144 hrs · 18,212 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4679) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,064 hrs · 18,135 cycles

FLT 4825, NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,738 hrs · 17,801 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,680 hrs · 17,740 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4607) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 20,680 hrs · 17,740 cycles

FLOOR EMERGENCY LIGHT AT SEAT 1C DOES NOT LIGHT UP. (FLT 4820) REPAIRED EMERGENCY FLOOR STRIP WIRING PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,625 hrs · 17,684 cycles

RIGHT AFT OVER WING EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,204 hrs · 17,286 cycles

AFT LEFT EXTERNAL EMERGENCY LIGHT AND NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 19,943 hrs · 17,034 cycles

FLOOR LEVEL EMERGENCY LIGHTS AT ROW 1 ARE OUT. (FLT 4760) RECONNECTED FLOOR LEVEL EMERGENCY STRIP PLUG.

Part: FLAP — MALFUNCTIONED (WING) · airframe 12,863 hrs · 11,045 cycles

FLIGHT 5217 - FLAPS FAIL CAUTION MESSAGE INTO BNA. AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: VALVE — OUT OF POSITION (CABIN PRESSURE) · airframe 12,511 hrs · 10,759 cycles

FLIGHT 5148 - AIRCRAFT WOULD NOT PRESSURIZE. FOLLOWED QRH, RETURNED TO CVG, LANDED WITHOUT INCIDENT. FOUND OVERBOARD AND INBOARD VALVES IN WRONG POSITION. REPOSITIONED VALVES. NO FURTHER DEFECTS.

Part: BPSU — FAULTY (RIGHT) · airframe 12,412 hrs · 10,678 cycles

FLIGHT 5673 - RECEIVED FLAP FAIL MESSAGE. LANDED WITHOUT INCIDENT. REPLACED RIGHT BPSU AND PERFORMED EO 27-046AD. NO FURTHER DEFECTS.

Part: FLAP — MALFUNCTIONED (WING) · airframe 12,412 hrs · 10,678 cycles

FLIGHT 5120 - RECEIVED FLAP CAUTION MESSAGE. LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.

Part: FLAP — MALFUNCTIONED (WING) · airframe 12,390 hrs · 10,061 cycles

FLIGHT 5383 - FLIGHT LEVEL 32,000 FT, OAT -39C, FLAPS FAIL CAUTION MESSAGE. FLAPS FAILED AT 0 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: FLAP — MALFUNCTIONED (WING) · airframe 12,248 hrs · 10,556 cycles

FLIGHT 5688 - FLAPS FAIL CAUTION MESSAGE AT 30 DEGREES. ABORTED FIRST APPROACH AND LANDED SAFELY ON SECOND APPROACH IN CAK. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: PRIORITY VALVE — FAULTY (MLG) · airframe 11,451 hrs · 9,928 cycles

FLIGHT 4984 - ON APPROACH RECEIVED GEAR DISAGREE WARNING MESSAGE. RAN QRH. LANDED CVG WITHOUT INCIDENT. REPLACED NLG PRIORITY VALVE. PROBLEM PERSISTED. REPLACED MLG PRIORITY VALVE. NO FURTHER DEFECTS.

Part: TIRE — FAILED (LT MLG)

NR 2 MAIN TIRE TREAD SEPARATED ON TAKEOFF CAUSING DAMAGE TO LEFT INBOARD FLAP.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,915 hrs · 8,486 cycles

INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RT SIDE AT FS 484 BL 36.00.

Part: PLATE — CRACKED (FUSELAGE) · airframe 9,915 hrs · 8,486 cycles

CARGO LANDING PLATE IS CRACKED AT RIVETS ATTACHING IT TO THE INTERCOSTALS .250 INCH.

Part: RIB — CRACKED (LT WING) · airframe 9,915 hrs · 8,486 cycles

LT BATT RIB IS CRACKED 1.5 INCH.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,915 hrs · 8,486 cycles

INTERCOSTAL CRACKED AT .25 INCH IN LENGTH ON LT INBOARD SIDE AT FS 484 LEFT BETWEEN BL 27.00.

Part: RIB — CRACKED (RT WING) · airframe 9,915 hrs · 8,486 cycles

RT BATT RIB IS CRACKED .750 INCH BETWEEN ATTACHING FASTENERS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,915 hrs · 8,486 cycles

INTERCOSTAL CRACKED AT .250 IN LENGTH ON RT OUTBD SIDE AT FS 484 LEFT BETWEEN BL 36.00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,915 hrs · 8,486 cycles

INTERCOSTAL CRACKED AT .250 IN LENGTH ON LT OUTBOARD SIDE AT FS 484 BETWEEN BL 36.00.

Part: ENGINE — VIBRATES (NR 2)

CREW REPORT STATED, SETTING THRUST FOR TAKEOFF CREW NOTICED A LEFT HAND N2 VIBE GAUGE AND ABORTED THE TAKEOFF. TAXIED TO THE GATE. WO HAS BEEN OPENED. NOW IS IN APPR STATUS.

Part: APU — SHUTDOWN (APU BAY)

APU AUTO SHUTDOWN WITH OIL TEMP MSG. OPENED DM2514110-1 IAW MEL 49-10-01 CAT C.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE RIGHT HAND AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,931 hrs · 4,905 cycles

DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING IN ROW 1C WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY TRACK LIGHT AT ROW 1C. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — FAULTY (AC BAY)

AFTER LANDING, THE CREW RECEIVED A "TOILET SMOKE" EICAS MESSAGE FOLLOWED BY CONFIRMED SMOKE IN THE CABIN. THE AIRCRAFT WAS STOPPED AND PASSENGERS WERE EVACUATED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE RT AIR CONDITIONING PACK AIR CYCLE MACHINE (ACM). THE PACK COALESCER SOCKS WERE REPLACED DUE TO THE SMOKE AND THE OVERWING EMERGENCY EXIT DOORS WERE INSPECTED AND REINSTALLED. OPERATIONAL AND PRESSURIZATION CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.