N382WA

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,116 hrs · 13,679 cycles

CORROSION WAS FOUND ON SKIN AJC7060, FROM STA Y:2140 TO 2163, L-33R TO L-35R. REPAIR CORROSION AREA IAW EI W2013A53B-1996, REV 1. COND CHECKED NORMAL.

Part: FRAME — CORRODED (BS 410) · airframe 70,116 hrs · 13,679 cycles

CORROSION WAS FOUND ON FUSELAGE FRAME, AT STA Y 410, BETWEEN X 15 AND X -10. REPLACE DAMAGE FRAME WITH NEW FRAME IAW SRM 51-35-01 AND 51-33-01, REV 53 AND EI NR W2013A53B-2032, REV 1.

Part: SKIN — CRACKED (LT WING) · airframe 70,116 hrs · 13,679 cycles

CRACK ON LT WING FIXED L/E NOSE SKIN AT STA XOS 944. REPAIR THE DAMAGE AREA, IAW EI W2013A57B-1989, REV1. CONDITION CHECKED NORMAL.

Part: SKIN — CRACKED (RT WING) · airframe 70,116 hrs · 13,679 cycles

CRACK ON RT WING FIXED L/E NOSE SKIN AT STA XOS 776. REPAIR RT WING FIXED L/E NOSE SKIN IAW EI W2013A57B-1995, REV 1. CONDITION CHECKED NORMAL.

Part: WEDGE — DEBONDED (LT WING TE FLAP) · airframe 70,116 hrs · 13,679 cycles

DISBOND WAS FOUND ON LT WING OTBD FLAP, NRC6753-503L, WEDGE UPPER SKIN AT STA X OF 614.25 TO 676.5. PERFORM THE LT WING OTBD FLAP WEDGE UPPER SKIN REPAIR IAW EI W2013A57B-2048, REV: 0. CHECK CONDITION SATISFACTORY.

Part: LINE — LOOSE (OIL SYSTEM) · airframe 66,503 hrs · 12,811 cycles

CREW REPORTED THAT APPROX 2 HOURS INTO FLIGHT THEY NOTICED THAT THE NR 2 ENG OIL QUANTITY WAS DROPPING. THE OIL QUANTITY CONTINUED TO DROP AT AN APPROX RATE OF 1 QT PER HOUR. OIL PRESS AND TEMP REMAINED NORMAL. APPROX 1 HOUR PRIOR TO LANDING THE OIL QTY WAS AT ZERO HOWEVER PRESS AND TEMP WERE STILL NORMAL. APPROX 18 MIN PRIOR TO LANDING THE OIL TEMP STARTED TO INCREASE AND THE PRESS STARTED TO DECREASE. THE CREW SHUTDOWN THE ENGINE AND DECLARED AND EMERGENCY. THEY LANDED WITH NO FURTHER ISSUES. UPON INSPECTION MAINTENANCE FOUND A LINE FROM THE OIL FILTER TO THE PRESS SWITCH LOOSE. MAINTENANCE SECURED THE LINE AND LEAKED CHECK WAS GOOD.

Part: DOOR FRAME — CORRODED (R3 DOORWAY) · airframe 66,493 hrs · 12,810 cycles

FOUND MAIN DECK DOOR FRAME HAS CORROSION AT L18-19R. REPAIRED IAW EI W2012A53B-095 REV 00,01, & 02.

Part: SKIN — CORRODED (RT WING) · airframe 66,493 hrs · 12,810 cycles

DURING 2C CHECK, FOUND CORROSION ON EXTERNAL UPPER SURFACE OF RT WING UPPER SKIN BETWEEN WING STATION XCW 118- XORS 949. REPAIRED IAW EI W2012A57B-089 REV:00, REV:01 & REV:02.

Part: FUEL CELL — CORRODED (CENTER WING AREA) · airframe 66,493 hrs · 12,810 cycles

FOUND CORROSION ON CENTER WING TANK UPPER SURFACE AT XCW = 96.5 S-15-S-18. REPAIRED IAW EI W2012A57B-051. REV:00, REV:01 & REV:02

Part: FUEL CELL — CORRODED (CENTER) · airframe 66,493 hrs · 12,810 cycles

DURING 2C CHECK, MECHANICS FOUND CORROSION ON CENTER WING TANK UPPER SKIN SURFACE AT XCW = 99.0 S-15. REPAIR ACCOMPLISHED AS PER EGAT EI NO: W2012A57B-027 REV:00, REV:01 & REV:01.

Part: FRAME — CRACKED (TAILCONE) · airframe 64,348 hrs · 12,289 cycles

TAIL CONE FRAME CANTED STA 2165.062 CRACKED. TEMPORARY REPAIR PER SRT ENGINEERING INSTRUCTIONS 53-EI-268842.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 62,924 hrs · 11,931 cycles

CORROSION - DURING C01 CHECK, FOUND LONGERON CORROSION AT STA 6-90 L-47L, NRC U05051 ISSUED. REPAIRED THE CORROSION AREA AT STA 6-90 L47L IAW MD-11 SRM 53-00-05 REPAIR 1 FIGURE 202 REV 43, COND SATISFACTORY.

Part: SKIN — DENTED (FUSELAGE) · airframe 62,724 hrs · 11,886 cycles

MAIN CARGO DOOR CUTOUT DENTED BEYOND LIMITS AT LOWER FORWARD CORNER. CORRECTIVE ACTION SRM 53-00-15 REPAIR 8 FIG 203.