N512JN

Part: COMPRESSOR — VIBRATION (NR 2 ENGINE) · airframe 100,089 hrs · 14,462 cycles

NR 2 ENGINE COMPRESSOR VIBRATION HIGH 5.0 NOT CORRECTABLE, STRONG RUDDER PEDAL VIBRATION AND HAD TO REDUCE POWER.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 99,479 hrs · 14,359 cycles

BLEED AIR TEMP ANNUNCIATED. COMPLETED LEVEL 3 CHECKLIST

Part: OIL SYSTEM — READS HIGH (NR 2 ENGINE) · airframe 98,887 hrs · 14,228 cycles

OIL QUANTITY INDICATING ON MEL. OIL TEMP STARTED RISING, PRESSURE DECREASING. TEMP REACHED 161 DEGREES AND LEVEL 2 ENG OIL TEMP HI ALERT DISPLAYED. OIL PRESS AT 20. RAN CHECKLIST OBSERVED PRESS & TEMP WITH THROTTLE AT IDLE. TEMP DROPPED A FEW DEGREES AND THEN BACK UP TO 160. AT THAT POINT RAN ENGINE SHUTDOWN IN-FLIGHT CHECKLIST.

Part: DETECTOR — MALFUNCTIONED (DUCT BURST) · airframe 98,803 hrs · 14,178 cycles

DURING CLIMB, A LEVEL 3 ENGINE DUCT ALERT WAS DISPLAYED. R3EPLACE ANTI-ICE BURST DETECTION UNIT IAW AMM 30-22-10.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 97,752 hrs · 13,863 cycles

AFT CARGO DOOR HINGE AND PIN HAS EVIDENCE OF CORROSION.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 97,752 hrs · 13,863 cycles

CENTER CARGO DOOR HINGE AND PIN HAS EVIDENCE OF CORROSION.

Part: LANDING GEAR — MALFUNCTIONED (LEFT) · airframe 97,248 hrs · 13,505 cycles

LEFT MAIN LANDING GEAR WOULD NOT RETRACT. RETURNED TO DEPARTURE. PERFORMED AN INSPECTION.

Part: FIRE DETECTOR — FALSE ACTIVATION (NR 2 ENGINE) · airframe 97,047 hrs · 13,383 cycles

AFTER TAKEOFF, LEVEL 3 ENGINE FIRE #2 ALERT FOLLOWED BY LEVEL 1 ENG 2 FIRE FAIL. ALL ALERTS EXTINGUISHED THEN RECYCLED FOUR TIMES. RETURNED TO DEPARTURE AIRPORT.

Part: ENGINE — FLAMED OUT (NR 1) · airframe 96,239 hrs · 13,199 cycles

NR 1 ENGINE FLAMED OUT AT FL330 DURING DESCENT. RESTARTED AT FL170.

Part: PITOT LINE — BLOCKED (PITOT/STATIC SYS) · airframe 94,482 hrs · 12,768 cycles

IAS ALERT DISPLAYED AFTER 250 KNOTS. CAPTAINS AIRSPEED DECREASING WHILE FIRST OFFICERS AIRSPEED WAS INCREASING, THEN LOSS ROLL BARS BOTH SIDES. THEN LOSS OF BOTH CAPTAIN & FIRST OFFICERS PITCH BARS. SELECTED AIRSPEED ALT LEVEL II & ELEVATOR FEEL LEVEL II. PERFORMED PITOT TEST ON BOTH 1 & 2 CADC & FOUND 1 CMDC WITH 10 KNOTS DIFFERENCE BETWEEN COCKPIT INDICATION & PITOT TESTER. FOUND DEBRIS IN CAPTAIN'S PITOT LINE. CLEARED DEBRIS & REPLACED CAPTAINS CADC. PERFORMED PITOT & STATIC TEST ALL NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

POSSIBLE CORROSION UNDER LOWER EDGE OF RT TAIL FILLET, PANEL 347DF ON THE FUSELAGE SKIN.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

MAIN DECK STATION 1229, CTR WING BOX, TOP SURFACE HAS CORROSION IN MULTIPLE AREAS AT APPROX RBL 66 - 100.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

MAIN DECK TOP SKIN OF CTR WING BOX, LT OTBD EDGE HAS EVIDENCE OF CORROSION AROUND FASTENERS AT APPROX STATION 1273.

Part: FRAME — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

AFT ENG NR 2, PYLON SUPPORT FRAME IS CORRODED.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

CORROSION AT STATION 1559 ON LONGERON 31 RT.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

MAIN DECK TOP SKIN OF CTR WING BOX, LT OTBD EDGE HAS EVIDENCE OF CORROSION AROUND FASTENERS AT APPROX STATION 1273.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

CORROSION AT STRINGER 5 LT AT STATION 1851.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

FUSELAGE SKIN AFT OF WASTE SERVICE PANEL HAS CORROSION ON INNER SURFACE OF PANEL CUT OUT.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

MAIN DECK STATION 1229, CTR WING BOX, TOP SURFACE HAS CORROSION IN MULTIPLE AREAS AT APPROX LBL 83 TO 109.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

CORROSION ON LONGERON 37R AT FRAME STATION 5 - 32.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

CORROSION ON FWD END OF LONGERON 34L AT STATION 5 - 7.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,357 hrs · 12,410 cycles

SEAT TRACK HAS CORROSION AT LBL 8 AT STATION 1360.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

SEAT TRACK HAS CORROSION AT RBL 8 AT STATION 1300.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,357 hrs · 12,410 cycles

SEAT TRACK HAS CORROSION AT LBL 8 AT STATION 1401.