N323NG

Part: ENGINE — FAILED (NR 1) · airframe 7,469 hrs · 7,073 cycles

ON SHORT FINAL, CREW RECEIVED SMOKE INDICATION IN THE AFT CARGO AND F/A REPORTED SMOKE IN THE CABIN. F/A REPORTED THAT THE LAVATORY SMOKE ALARM WAS GOING OFF AND AS PRECAUTION SPRAYED THE TRASH BIN AND TOILET. CAPTAIN DECLARED AN EMERGENCY AND LANDED. MAINTENANCE INSPECTED AND FOUND NO SIGNS OF OIL IN ANY SIGHT GLASS AND THE THE P2.7 EXHAUST DUCT COVERED IN OIL. MAINTENANCE SERVICED THE NR 1 ENGINE WITH 8 QUARTS OF OIL, STARTED AND SELECTED THE BLEEDS ON AND THE CABIN STARTED TO FILL WITH SMOKE. MAINTENANCE R & R THE 1 ENGINE IAW AMM. ACFT IS OUT OF SERVICE.

Part: BATTERY — UNSECURE (MEGAPHONE) · airframe 6,606 hrs · 6,246 cycles

CREW REPORTED THAT THE MEGAPHONE BATTERY WAS DEAD. MAINTENANCE SECURED BATTERY IAW AMM AND OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 6,428 hrs · 6,071 cycles

COCKPIT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-00-00. OPS CHECKED GOOD.

Part: DOOR — INOPERATIVE (MLG) · airframe 5,980 hrs · 5,633 cycles

CREW REPORTED THAT THE MLG DOOR INDICATION WAS FLASHING AFTER THEY SELECTED GEAR UP. CREW FOLLWED THE QRH AND RETURNED TO DEPARTURE. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MAINTENANCE RERIGGED THE ALTERNATE EXTENSION SYS OF THE DOORS IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 5,979 hrs · 5,632 cycles

DURING HEAVY CHECK FOUND RT INBD SEAT TRACK AT BS 670 TO 782 CORRODED OUT OF LIMITS. MX R & R SEAT TRACK IAW SRM 51-40-07, 51-41-00, 51-40-15,51-42-05.

Part: PANEL — CORRODED (FUEL SYS) · corrosion level 2 · airframe 5,979 hrs · 5,632 cycles

DURING HEAVY CHECK, FOUND FUEL PANEL 521BT HAS CORROSION AT SCREW HOLES. MX R & R FUEL PANEL IAW AMM 57-11-06-40-802.

Part: ACCESS PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 5,979 hrs · 5,632 cycles

DURING HEAVY CHECK, FOUND FUEL PANEL 621BT HAS CORROSION IN COUNTER SINK HOLES. MX R & R FUEL PANEL IAW AMM 57-11-06-400-802.

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 5,979 hrs · 5,632 cycles

DURING HEAVY CHECK, FOUND FUEL ACCESS PANEL 522CT CORRODED IN COUNTER SINK HOLES. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS. R & R FUEL ACCESS PANEL IAW AMM 57-11-01-400-801.

Part: ACCESS PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 5,979 hrs · 5,632 cycles

DURING HEAVY CHECK FOUND FUEL PANEL 622BT HAS CORROSION AT SCREW HOLES. MX R & R FUEL PANEL IAW AMM 57-21-01-400-801.

Part: PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 5,979 hrs · 5,632 cycles

DURING HEAVY CHECK FOUND FUEL PANEL 522AT HAS CORROSION AT SCREW HOLES. MX R & R FUEL PANEL IAW AMM 57-11-01-400-801.

Part: SKIN — DENTED (ZONE 200) · airframe 5,979 hrs · 5,632 cycles

WHILE ACFT WAS IN FOR HEAVY CHECK, FOUND MULTIPLE DENTS ON LT SIDE FUSELAGE BETWEEN FS 281.0 AND 321.0, STR 6P-13P. REQUIRES PERMANENT REPAIR ACCOMPLISHED ON RD 8/4-53-5756. MX INSTALLED DOUBLER IAW RD 8/4-53-5756, ISSUE NR 1 DATED 10/11/2013. DOUBLER ATTACHED TO LT SKIN PANELS 85360131 AND 85360111. ACFT REMAINS FOR COMPLETION.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 5,979 hrs · 5,632 cycles

DURING HEAVY CHECK, FOUND SEAT TRACK AT FS 697 TO 725 AT Y29.50 HAS CORRODED. R & R SEAT TRACK IAW SRM 51-42-05, 51-42-45.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 5,979 hrs · 5,632 cycles

DURING HEAVY CHECK, FOUND CORROSION ON RT INBD SEAT TRACK AT BS 564 TO 664.5. MX R & R SEAT TRACK IAW SRM 51-25-25. ACFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 5,979 hrs · 5,632 cycles

DURING HEAVY CHECK, FOUND RT INBD SEAT TRACK AT BS 660 HAS CORROSION. MX FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK BETWEEN BS 564.5 TO 664.5, IAW SRM 51-42-05, 51-41-05, 51-40-15.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 5,979 hrs · 5,632 cycles

DURING HEAVY CHECK, FOUND SEAT TRACK CORRODED AT X68.0. MAINTENANCE R & R SEAT TRACK IAW SRM 51-42-05.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 5,939 hrs · 5,594 cycles

CREW REPORTED THAT THE FWD F/A FLASHLIGHT WAS NOT WORKING. MX REPLACED BATTERIES IN FWD F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 5,681 hrs · 5,352 cycles

CREW REPORTED THAT THE FWD F/A FLASHLIGHT WAS INOPERATIVE. MX R & R THE BATTERIES IN FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 5,580 hrs · 5,249 cycles

CREW REPORTED THAT ONE COCKPIT FLASHLIGHT WAS MISSING. MX REPLACED MISSING COCKPIT FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 2) · airframe 4,340 hrs · 4,041 cycles

CREW REPORTED LOSING ALL FLUID IN NR 2 SYSTEM WHILE ON DEICE PAD. MAINTENANCE REPORTED NR 1 BRAKE FALLING APART AND WHEEL ASSY SHIFTED ON AXLE. MAINTENANCE BLEED AND LEAK CHECKED THE HYDRAULICS AND CHANGED THE LEFT O/B TIRE AND WHEELS ASSY PER BOMBA AMM.

Part: SKIN — DENTED (FUSELAGE) · airframe 4,317 hrs · 4,021 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED DAMAGE TO MID LWR FUSE AT STA 216. MAINTENANCE PERFORMED MAJOR REPAIR TO MID LWR FUSE AT STA 216 IAW BOMBARDIER RD 8/4-53-731. REPAIR MATERIAL MADE FROM 2024-T3 .050 CLAD MATERIAL (QQ-A-250/5). AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: HYDRAULIC SYSTEM — LEAKING (NR 2) · airframe 3,568 hrs · 3,310 cycles

GATE RETURN DUE TO MX (NR 2 HYD LEAK). MAINTENANCE SERVICE NR 1 HYD SYSTEM OPS CHECK GOOD.

Part: DOOR — LEAKING (CABIN) · airframe 3,027 hrs · 2,801 cycles

AT 13000FT 10NM NORTH OF COATE INTERSECTION CREW HEARD A LOUD NOISE FROM L1 ESCAPE HATCH DOOR. NO LOSS OF CABIN PRESSURE OCCURRED AND THE A/C DESCENDED TO 10000FT AND RETURNED BACK TO EWR FOR FURTHER MX INSPECTION. CREW DID NOT DECLARE AN EMERGENCY AND A/C LANDED IN EWR WITHOUT FURTHER INCIDENT.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 1,956 hrs · 1,795 cycles

FUSELAGE EXTERNAL JOINT STRAP HAD LIGHTNING DAMAGE LOCATED ON AND ADJACENT TO A FASTENER HEAD AND AROUND THE COUNTERSINK. APPROX 1.3 TO 1.5 INCHES AFT OF X547.0 BETWEEN STRINGER 31P AND 32P. DAMAGED MEASURED APPROX .100 DIA BY .029 INCHES DEEP. REPAIR WAS COMPLETED BY REMOVING STRAP THE DAMAGED SECTION OF THE EXTERNAL JOINT STRAP (APPROX 18 INCHES), FABRICATING A REPAIR STRAP FROM THE SAME GAUGE AND CONTOURS AS THE ORIGINAL, AND COMPLETING THE REPAIR IAW CALGAN AIR TD 400-53-10-75.