N676NW

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,215 hrs · 6,440 cycles

DURING SERVICE CHECK, FOUND THE MOST AFT LT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPS CHECKED OK IAW AMM 33-51.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,474 hrs · 6,229 cycles

EXIT SIGN AROUND DOOR 3 LT AREA INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY AT DOOR 3L. CHECKED OK IAW AMM 33-51.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,599 hrs · 5,878 cycles

EMERGENCY UPPER DECK LT DOOR BATTERY OK, LIGHT INOPERATIVE. REPLACED BATTERY POWER PACK. OPS CHECKED GOOD.

Part: COMPUTER — MALFUNCTIONED (FIRE DETECTION) · airframe 45,557 hrs · 5,752 cycles

ON SHORT FINAL APPROACH DURING GEAR EXTENSION, CREW RECEIVED WHEEL WELL FIRE INDICATION. AFTER LANDING, VERIFIED NO FIRE PRESENT. MAINTENANCE INSPECTED AREA, NO EVIDENCE OR INDICATION OF FIRE. MAINTENANCE THEN REPLACED LEFT CENTRAL MAINTENANCE COMPUTER PER AMM 45-10 AND INSTALLED SOFTWARE, FIRE INDICATION DISAPPEARED. PERFORMED GROUND TEST OF FIRE DETECTION, OPS CHECKED OK

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 45,249 hrs · 5,713 cycles

DURING INSPECTION FOUND EMERGENCY LIGHT ADJACENT TO SEAT 24H INOPERATIVE. MAINTENANCE REPAIRED THE WIRE AT SEAT 24H PER WDM 33-51. OPERATIONAL CHECKED NORMAL PER AMM33-51.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,115 hrs · 5,696 cycles

DURING INSPECTION FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT DOOR 3L. MAINTENANCE REPLACED LIGHT ASSEMBLY S417N509-1SMI, REF AMM 33-51 AND IPC 33-51. OPS CHECKED OK.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 44,080 hrs · 5,570 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY FLOOR LIGHT AT SEAT 22H WAS FOUND TO BE INOPERATIVE. MAINTENANCE CONNECTED THE ELECTRICAL CONNECTOR OF THE FLOOR PROXIMITY LIGHT. SYSTEM OPERATION WAS NORMAL AFTER THE CONNECTOR WAS SECURED.

Part: WIRE — BROKEN (CABIN) · airframe 43,117 hrs · 5,461 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY FLOOR LIGHT FORWARD OF SEATS 35 D-G WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND BROKEN WIRES AND REPLACED THE LIGHT ASSEMBLY AT SEAT 34 D-G. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT ASSEMBLY WAS REPLACED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,106 hrs · 5,460 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY DOOR EXIT LIGHT AT DOOR 2R WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT ASSEMBLY WAS REPLACED.

Part: SOCKET — INOPERATIVE (CABIN) · airframe 42,740 hrs · 5,418 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY FLOOR LIGHT NEAR LAV 2L WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE SOCKET. SYSTEM OPERATION WAS NORMAL AFTER THE SOCKET WAS REPLACED.

Part: SKIN — WORN (BS 2380-2397) · airframe 39,381 hrs · 5,026 cycles

VERTICAL STABILIZER SEAL INTERFACE INSPECTION LT SIDE FOUND LIGHT WEAR BETWEEN STA 2380-2397. BLENDED AREA, MAX MATERIAL REMOVED IS.006"HFEC NO CRACKS WITHIN LIMITS IAW SRM53- 00-01, FIG 101. TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA5331-01190-02, ERA489979-14AD DOCUMENTS, REWORKED AREA. REQUIRED INSPECTION COMPLETED.

Part: SKIN — DAMAGED (BS 2280-2350) · airframe 39,381 hrs · 5,026 cycles

VERT STAB SEAL INTERFACE INSP JOB CARD 5331-01190-02 RT SIDE FOUND LIGHT WEAR DAMAGE FROM STA 2280-STA 2350. BLENDED AREA. MAX MATERIAL REMOVED IS .008" HFEC NO CRACKS WITHIN LIMITS IAW SRM 53-00-01, FIG 101. TREATED, PRIMED, APPLIED TEFLON COATING IAW AA 5331-01190-02. ERA 489979-14AD DOCUMENTS REWORKED AREA. REQUIRED INSP COMPLETED BY 052015.

Part: SKIN — WORN (BS 2598-2628) · airframe 39,381 hrs · 5,026 cycles

VERTICAL STABILIZER SEAL INTERFACE INSP RT SIDE. FOUND WEAR DAMAGE FROM STA 2598-STA2628. BLENDED AREA, MAX MATERIAL REMOVED IS .006".HFEC NO CRACKS. WITHIN LIMITS IAW SRM 53-00-01, FIG 101. TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA5331-01190-02. REWORKED AREA, REQUIRED INSP COMPLETED.

Part: SKIN — WORN (BS 2538-2557) · airframe 39,381 hrs · 5,026 cycles

VERTICAL STABILIZER SEAL INTERFACE INSP RT SIDE. FOUND LIGHT WEAR DAMAGE STA 2538-STA 2557. BLENDED AREA MAX MATERIAL REMOVED IS .003". HFEC NO CRACKS, WITHIN LIMITS IAW SRM 53-00-01, FIG 101. TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA5331-01190-02. REWORKED AREA REQUIRED INSP COMPLETED.

Part: SKIN — GOUGED (BS 2280-2300) · airframe 39,381 hrs · 5,026 cycles

VERTICAL STABILIZER SEAL INTERFACE INSP LT SIDE FOUND WEAR BETWEEN STA 2280-2300 WITH GOUGE AT STA 2298. BLENDED AREA, MAX MATERIAL REMOVED IS .015". HFEC NO CRACKS WITHIN LIMITS IAW SRM5300-00-01, FIG 101, NOTE K. TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA5331-01190-02. ERA489979-14AD DOCUMENTS REWORKED AREA. REQUIRED INSP COMPLETED.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,381 hrs · 5,026 cycles

DURING A MX VISIT, THE EMERGENCY EXIT LIGHT AT DOOR 4R WAS FOUND INOPERATIVE. MX REPLACED THE FUSE IN POWER SUPPLY M7922 IAW AMM.

Part: SKIN — DAMAGED (BS 2557-2598) · airframe 39,381 hrs · 5,026 cycles

VERT STAB SEAL INTERFACE INSP RT SIDE, FOUND LIGHT WEAR DAMAGE FROM STA 2557-STA 2598. BLENDED AREA, MAX MATERIAL REMOVED IS .006". HFEC NO CRACKS WITHIN LIMITS IAW SRM 53-00-01, FIG 101. TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA 5331-01190-02. ERA 489979-14AD. DOCUMENT REWORKED AREA. REQUIRED INSP COMPLETED.

Part: SKIN — DAMAGED (BS 2360-2397) · airframe 39,381 hrs · 5,026 cycles

VERTICAL STABILIZER SEAL INTERFACE 01190-02, RT SIDE. FOUND LIGHT WEAR DAMAGE FROM STA 2360-STA 2397. BLENDED AREA, MAX MATERIAL REMOVED IS .009" HFEC NO CRACKS, WITHIN LIMITS IAW SRM 53-00-01, FIG 101. TREATED, PRIMED, AND APPLIED TEFLON COATING IAW AA5331-01190-02. ERA 489979-14AD. DOCUMENTS REWORKED AREA. REQUIRED INSP COMPLETED..

Part: SKIN — WORN (BS 2560-2630) · airframe 39,381 hrs · 5,026 cycles

VERTICAL STABILIZER SEAL INTERFACE INSP LT SIDE FOUND WEAR BETWEEN STA 2560-2630. BLENDED AREA, MAX MATERIAL REMOVED IS .004. HFEC NO CRACKS WITHIN LIMITS IAW SRM 53-00-01, FIG101, TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA5331-01190-02. ERA 489979-14AD DOCUMENTS REWORKED AREA. REQUIRED INSP COMPLETED.

Part: SKIN — WORN (BS 2340-2360) · airframe 39,381 hrs · 5,026 cycles

VERTICAL STABILIZER SEAL INTERFACE INSP LT SIDE FOUND WEAR BETWEEN STA 2340-2360. BLENDED AREA, MAX MATERIAL REMOVED IS .010. HFEC NO CRACKS WITHIN LIMITS IAW SRM 53-00-01, FIG 101. TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA5331-01190-02. ERA489979-14AD DOCUMENTS REWORKED AREA. REQUIRED INSP COMPLETE.

Part: SKIN — WORN (BS 2520-2560) · airframe 39,381 hrs · 5,026 cycles

VERTICAL STABILIZER SEAL INTERFACE INSP LT SIDE. FOUND LIGHT WEAR BETWEEN STA 2520-2560 BLENDED AREA MAX MATERIAL REMOVED IS .002" HFEC NO CRACKS. WITHIN LIMITS IAW SRM 53-00-01, FIG 101 TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA 5331-01190-02, ERA 489979-14AD DOCUMENTS. REWORKED AREA. REQUIRED INSP COMPLETED BY 05201 ASSOCIATED AA 5331-01190 ADDED.

Part: SKIN — WORN (BS 2360-2380) · airframe 39,381 hrs · 5,026 cycles

VERTICAL STABILIZER SEAL INTERFACE INSP CARD LT SIDE FOUND WEAR BETWEEN STA 2360-2380. BLENDED AREA, MAX MATERIAL REMOVED IS .010" HFEC NO CRACKS. WITHIN LIMITS IAW SRM 53-00-01, FIG 101, TREATED PRIMED AND APPLIED TEFLON COATING IAW AA 5331-01190-02, ERA 489979-14AD DOCUMENTS REWORKED AREA. REQUIRED INSP COMPLETED ASSOCIATED AA 5331-01190 ADDED.

Part: SKIN — WORN (BS 2320-2340) · airframe 39,356 hrs · 5,023 cycles

VERTICAL STABILIZER SEAL INTERFACE INSP LT SIDE FOUND WEAR BETWEEN STA 2320-2340. BLENDED AREA, MAX MATERIAL REMOVED IS .008" HFEC NO CRACKS WITHIN LIMITS IAW SRM 53-00-01, FIG 101. TREATED, PRIMED AND APPLIED TEFLON COATING IAW AA 5331-01190-02. ERA 489979-14AD DOCUMENTS REWORKED AREA. REQUIRED INSP COMPLETED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,356 hrs · 5,023 cycles

FOUND WEAR BETWEEN STA 2300-2320 WITH GOUGE AT 2313. BLENDED AREA STA 2300-2320 EXCEPT STA 2313. MAX MATERIAL REMOVED IS .007 INCH HFEC NO CRACKS. WITHIN LIMITS PER SRM 53-00-01 FIG 101. TREATED, PRIMED APPLIED TEFLON COATING PER AA 5331-01190-02. ERA 489979-14AD DOCUMENTS REWORKED AREA STA 2313 DRILLED OUT GOUGE TO .190 INCH AND INSTALLED BLIND FASTENER PER SRM 53-00-01 FIG 201. REQUIRES REP INSPECTION AT 1000 FC INTERVALS. REQUIRES PERMANENT REPAIR WITH SOLID FASTENER AT 6000 FC. REQUIRED INSPECTION COMPLETED.

Part: OVEN — SMOKE (NR2 GALLEY) · airframe 38,576 hrs · 4,929 cycles

DURING FLIGHT, SMOKE WAS REPORTED IN THE NR2 GALLEY AREA. UTILITY BUSES WERE SWITCHED OFF, FUEL WAS DUMPED AND THE ACFT RETURNED TO DEPARTURE. MX FOUND OVENS 2-45 & 2-46 WITH MELTED PLASTIC AND REPLACED BOTH OVENS, CONTROLLERS AND SEVERAL RELAYS. OPS CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 38,105 hrs · 4,871 cycles

DURING A LINE CHECK, MAINTENANCE FOUND ONE LT AND ONE RT EMERGENCY OVERWING LIGHT INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD. (2010-00826)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,821 hrs · 4,836 cycles

DURING A LINE CHECK, MAINTENANCE FOUND THE DOOR 3L ROUND EMERGENCY LIGHT INOPERATIVE. AFTER EXTENSIVE TROUBLESHOOTING, MAINTENANCE REPLACED THE L1166 LIGHT ASSEMBLY AND THE M7919 POWER SUPPLY FUSE. OPERATIONAL CHECK WAS GOOD. (2010-00807)

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 37,774 hrs · 4,830 cycles

DURING A LINE CHECK, MX FOUND 4 EMERGENCY PATH LIGHTS AT SEAT 80 INOPERATIVE. MX REPAIRED THE WIRING CONNECTION. OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,477 hrs · 4,788 cycles

DURING LINE CHECK, MX FOUND THE DOOR 3L EMERGENCY EXIT LIGHT, ALONG WITH THE LT 3-4 OVERWING EMERGENCY LIGHTS INOPERATIVE. MX REPLACED THE DOOR 3L POWER SUPPLY AND BATTERY. OPS CHECK OF ALL LIGHTS WAS GOOD.

Part: SLIDE — NO TEST (R3 DOOR) · airframe 65,662 hrs · 4,559 cycles

DURING OVERNIGHT EVAC SLIDE DEPLOYMENT CHECKS, 3R DOOR EVAC SLIDE FAILED TO DEPLOY. MX REPLACED THE SLIDE AND DOOR ASSIST RESERVOIR. SAFETY AND RIG CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 35,048 hrs · 4,488 cycles

DURING LINE CHECK, MX FOUND ALL FWD ZONE RT EMERGENCY LIGHTS INOPERATIVE. MX REPAIRED WIRING. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,650 hrs · 4,441 cycles

DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE LEFT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND THE POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY EXIT) · airframe 34,636 hrs · 4,439 cycles

DURING LINE CHECK RT UPPER DECK DOOR EMERGENCY POWER RESERVOIR FAILED TEST. REPLACED EMERGENCY POWER SYSTEM BATTERY PER AMM 52-23-14. FUNCTION CHECK GOOD AND AIRCRAFT HAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,445 hrs · 4,414 cycles

MAINTENANCE FOUND LEFT MOST FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. SYSTEM TESTED OKAY.

Part: POWER SUPPLY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, FOUND RT SIDE 3 OVERWING EMERGENCY LIGHTS INOP. MX REMOVED AND REPLACED FUSE AND PWR PACK. OPS CHECKED GOOD AND ACFT WAS RETURNED TO SERVICE. (K)

Part: FUSE — FAILED (EMERGENCY LIGHT)

DURING OVERNIGHT CHECK, FOUND LEFT SIDE, 3RD OVERWING EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED FUSE ON POWER SUPPLY. OPS CHECKED GOOD, ACFT WAS RETURNED TO SERVICE. (K)

Part: FUSE — FAILED (POWER SUPPLY)

DURING OVERNIGHT CHECK, FOUND RT SIDE OVERWING EMERGENCY LIGHT INOPERATIVE AT STA 1503. REMOVED AND REPLACED FUSE ON POWER SUPPLY. OPS CHECKED GOOD, AND ACFT WAS RETURNED TO SERVICE. (K)

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 31,028 hrs · 4,008 cycles

DURING OVERNIGHT CHECK FOUND DOOR 3 RT EMERGENCY EXIT SIGN INOP. MX R&R POWER SUPPLY. OPS CHECKED GOOD AND ACFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 26,626 hrs · 3,438 cycles

DURING LINE CHECK, FOUND RT UPPER DECK DOOR RIGHT BATTERY PACK FAILED TEST. REPLACED EMERGENCY POWER SYSTEM BATTERY PACK PER MM 52-23-14. FUNCTION CHECKED GOOD AND AIRCRAFT HAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,296 hrs · 3,395 cycles

DURING OVERNIGHT CHECK, FOUND ZONE E RIGHT SIDE PATH AND EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,173 hrs · 3,378 cycles

DURING OVERNIGHT CHECK FOUND RIGHT SIDE E-ZONE EMERGENCY PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 18,243 hrs · 2,329 cycles

AFTER TAKEOFF, CREW WAS UNABLE TO RETRACT THE T/E FLAPS PAST 5 DEGREES, AND HAD A T/E DRIVE MESSAGE. DECISION WAS MADE TO RETURN TO DTW, 170,000 LBS OF FUEL WAS DUMPED. A YELLOW EMERGENCY WAS DECLARED FOR LANDING, AND A/C LANDED WITHOUT INCIDENT. DTW MAINTENANCE REMOVED AND REPLACED ALL 3 RVDT'S FOR THE OUTBOARD FLAP SYSTEM. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 16,719 hrs · 2,134 cycles

DURING LINE CHECK, FOUND ZONE D RT FLOOR PATH EMERGENCY LIGHTS INOP. RECONNECTED LOOSE LIGHT CONNECTOR AT ROW 43H. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — OUT OF POSITION (CABIN) · airframe 16,719 hrs · 2,134 cycles

DURING LINE CHECK FOUND ZONE E FLOOR PATH EMERGENCY LIGHTS INOP. REINSTALLED BATTERY PACK. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — PINCHED (EMERGENCY LIGHT) · airframe 16,620 hrs · 2,122 cycles

ROW 9-12 LT EMERGENCY PATHWAY LIGHTS OUT. FOUND WIRE PINCHED, REPOSITIONED WIRE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 16,573 hrs · 2,116 cycles

ROW 9-12 LT EMERGENCY PATHWAY LIGHT OUT. RESECURED LT EMERGENCY PATHWAY LIGHT AT ROW 9. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — SPARKS (GALLEY) · airframe 13,954 hrs · 1,777 cycles

WHILE INBOUND TO JFK, FLIGHT ATTENDANT REPORTED U/D OVEN 1-29 RUNS TOO HOT, SPARKS AND SMOKE WERE SEEN COMING FROM CONTROL PANEL. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. JFK MAINTENANCE REPLACED OVEN AND RESEATED RELAY. OPERATIONAL CHECKS NORMAL.

Part: CONNECTOR — LOOSE (EMERGNECY LIGHT) · airframe 8,911 hrs · 1,149 cycles

DURING LINE CHECK, FOUND LT SIDE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51-65. SECURED LOOSE CONNECTION ON LIGHT SOCKET. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (ROW 9F) · airframe 4,487 hrs · 596 cycles

DURING LINE CHECK FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROW 9F - DOOR 2L. REPAIRED WIRE AND OPERTATIONAL CHECK GOOD.

Part: COFFEEMAKER — DIRTY (GALLEY) · airframe 928 hrs · 132 cycles

DURING FLIGHT, A FLIGHT ATTENDANT REPORTED AN ELECTRICAL FUME ODOR IN THE AREA BENEATH THE STAIRS. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. CLEANED COFFEEMAKER, OPERATIONAL CHECK GOOD.