N916CK

Part: WEB — CRACKED (BS 832) · airframe 51,324 hrs · 55,601 cycles

MAIN DECK FLOOR WEB UNDER FLOORBOARD FOUND CRACKED

Part: FLOOR SUPPORT — CORRODED (BS 897) · corrosion level 2 · airframe 51,324 hrs · 55,896 cycles

MAIN DECK FLOOR SUPPORT HAS EVIDENCE OF CORROSION.

Part: FLOOR SUPPORT — CORRODED (BS 929) · corrosion level 2 · airframe 51,324 hrs · 55,896 cycles

MAIN DECK FLOOR SUPPORT HAS EVIDENCE OF CORROSION AROUND FASTENER.

Part: BULKHEAD WEB — CORRODED (LT MLG WW) · corrosion level 2 · airframe 50,881 hrs · 55,601 cycles

LEFT WHEEL WELL HAS CORROSION, UPPER PRESSURE BULKHEAD.

Part: SKIN — CORRODED (BS 370-427) · corrosion level 2 · airframe 50,881 hrs · 55,601 cycles

EXTERNAL SKIN FWD LOWER CARGO DOOR CUTOUT CORROSION, LONGERON 25

Part: PAN — CORRODED (LT MLG WW) · corrosion level 2 · airframe 50,881 hrs · 55,601 cycles

LEFT MLG WW UPPER RETAINER PAN CORRODED.

Part: LONGERON — CORRODED (BS 351) · corrosion level 2 · airframe 50,881 hrs · 55,601 cycles

LONGERON CORRODED.

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 50,881 hrs · 55,601 cycles

LEFT WING FLAP LOWER SKIN CORRODED, XFLS 326.

Part: SKIN — CRACKED (BS 266) · airframe 50,881 hrs · 55,601 cycles

FUSELAGE SKIN BS 266 LONGERON 5L HAS EVIDENCE OF A CRACK

Part: FLOOR SUPPORT — CORRODED (MAIN DECK) · corrosion level 2 · airframe 50,881 hrs · 55,601 cycles

MAIN DECK FLOOR SUPPORT BRACKET CORRODED.

Part: SKIN — CRACKED (TAILCON) · airframe 50,881 hrs · 55,601 cycles

TAILCONE EXTERNAL SKIN RT SIDE CRACKED.

Part: SKIN — CRACKED (BS 266) · airframe 50,881 hrs · 55,601 cycles

FUSELAGE SKIN CRACKED.

Part: WARNING LIGHT — ILLUMINATED (OIL PRESSURE) · airframe 50,820 hrs · 55,560 cycles

PERFORMED PRECAUTIONARY SHUTDOWN OF LEFT ENGINE DUE TO OIL PRESSURE LOW LIGHT, LOW OIL PRESSURE & ZERO ON OIL QUANTITY

Part: FUEL TANK — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,787 hrs · 55,539 cycles

CORROSION ON THE FORWARD SIDE OF THE FUEL TANK AT STA 598, RBL 34.

Part: FLOORBOARD — CORRODED (CABIN) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles

AFT OF R1 DOOR FLOORBOARD CORROSION.

Part: BATTERY — DAMAGED (MASTER) · airframe 50,741 hrs · 55,505 cycles

WITH AIRCRAFT ON GROUND, ATTEMPTED TO START APU TO REPOSITION, FOUND SHIP BATTERIES WEAK, INVESTIGATED AND DISCOVERED ONE OF THE SHIP BATTERY CASES DAMAGED. REPLACED BATTERIES AND CHARGER.

Part: STRINGER — CORRODED (BS 225) · corrosion level 2 · airframe 50,660 hrs · 55,453 cycles

CORROSION AT STRINGER 23, RT BS 225 FWD CARGO.

Part: SKIN — CORRODED (BS 330) · corrosion level 2 · airframe 50,426 hrs · 55,299 cycles

CORROSION ON FUSELAGE BELL JUST AFT OF NR 1 DME INTERROGATOR ANTENNA, FS 330.

Part: FUEL CAP — MISSING (RT WING) · airframe 49,324 hrs · 54,559 cycles

FUEL REPORTED AS VENTING FROM RT WING, NOTED FUEL IMBALANCE AND RETURNED TO DEPARTURE. UPON INVESTIGATION, FOUND RT OVERWING FUEL CAP MISSING, REPLACED CAP AND FUELED TO VTO, NO LEAKS NOTED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,966 hrs · 54,322 cycles

INTERCOSTAL CRACKED AT LIGHTNING HOLE, 1 INCH (NR47561).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

PILOTS AFT OUTBOARD SEAT TRACK CORRODED (1 INCH).

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

AFT EMERGENCY DOOR CUTOUT LT LOWER CORNER STRUCTURE CORRODED (1 INCH).

Part: SKIN — CANNING (CARGO DOOR) · airframe 48,966 hrs · 54,322 cycles

FWD LOWER CARGO DOOR SKIN OIL CANNED (NR 46742).

Part: LONGERON — CRACKED (FUSELAGE) · airframe 48,966 hrs · 54,332 cycles

LONGERON CRACK (1 INCH).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

COCKPIT FLOOR SUPPORT UNDER FWD SIDE OF AVIONICS RACK HAS CORROSION (1X1).

Part: FRAME — DAMAGED (FUSELAGE) · airframe 48,966 hrs · 54,332 cycles

STA 69 RIGHT SIDE HAS DAMAGE AREA ON FRAME (1 INCH).

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 48,966 hrs · 54,332 cycles

SEAT TRACK DAMAGED ON END OF VERTICAL LEG INSIDE TRACK SECTION (1 INCH).

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

SPLICE CORRODED 1 IN X 1 IN CORROSION (N/R 21860).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

UPPER FLOORBEAM CAP, TOP SIDE HAS SEVERAL AREAS OF CORROSION 1 IN X 1 IN CORROSION (N/R 21713).

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

PRESSURE PANEL ATTACH ANGLE CORRODED 1 X 2 INCHES.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 48,966 hrs · 54,332 cycles

CUSP WEB CRACKED (1 INCH).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

FRAME TO FLOOR TIE CORRODED 1 X 1 INCH (NR 21870).

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

CORRODED BOLT THROUGH FRAME ATTACHMENT FITTING 1 IN X 1 IN (N/R 21639).

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

FRAME CORRODED MAIN CARGO DECK 1 IN X 1 IN (N/R 21634).

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

LIGHT CORROSION ON FRAME (1 IN X 1 IN) CORROSION (N/R 21783).

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

L-ANGLE ALONG INTERIOR UPPER AREA OF TRAPEZOID PANEL CORROSION 1 IN X 1 IN CORROSION (N/R 22592).

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

AFT HALF OF TIE FITTING CORROSION 1 IN X 1 IN CORROSION (N/R 22828).

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

AFT WALL LOWER TEE CHORD CORRODED 1 IN X 1 IN CORROSION (N/R 22893).

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 47,291 cycles

AFT WALL UPPER TEE CHORD CORRODED 1 IN X 1 IN CORROSION (N/R 22892).

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

INTERCOSTAL WEB HAS AREA OF CORROSION 2 IN X 2 IN CORROSION (N/R 21880).

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,966 hrs · 54,332 cycles

INTERCOSTAL CRACKED 5 INCHES (NR 22889).

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

HORIZONTAL WEB HAS SEVERAL AREAS CORROSION 2 X 2, 1 X 4, 2 X 2 (NR21976).

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

INTERCOSTAL VERTICAL L-ANGLE LOWER FASTENER HOLES CORROSION, 5 X 1 INCHES (REF NR 21740).

Part: WEB — CORRODED (FUSELAGE) · airframe 48,966 hrs · 54,332 cycles

HORIZONTAL FLOOR WEB CRACKED.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

CORROSION ON DOUBLER, DRILLED HOLE ON FRAME, 5 X 5 CORROSION (NR 21758).

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 48,966 hrs · 54,332 cycles

FWD SIDE OF FRAME ATTACH CLIP CRACKED.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

UPPER CANTE BULKHEAD SPLICE PLATE HAS CORROSION 1 X 2 INCHES (NR 21937).

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

FLOOR WEB CORROSION 2 X 2 INCHES (NR 22809).

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,966 hrs · 54,332 cycles

LONGERON TIE FITTING CRACKED, .25 INCH CRACK (NR 21758).

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

WEB CORRODED 4 X 5 INCHES.

Part: BLOWOUT PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

LEFT CANTED BULKHEAD BLOWOUT PANEL CORROSION (1 X 1).

Part: STANCHION — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

SIDEWALL STANCHION CORRODED 1 X 2 INCHES AFT PIT RT SIDE (NR 21769).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

CAPTAINS SEAT TRACK HAS CORROSION (1X1 INCHES) CAPTAINS I/B AFT SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

FIRST OFFICERS SEAT TRACK HAS CORROSION (1X1 INCHES) FIRST OFFICERS FWD O/B SEAT TRACK AFT END.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

FIRST OFFICERS SEAT TRACK HAS CORROSION (1X1 INCHES) FIRST OFFICERS O/B SEAT TRACK STA 147.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

CAPTAINS SEAT TRACK HAS CORROSION (1X1 INCHES) CAPTAINS FWD O/B SEAT TRACK FWD END.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

SEAT TRACK OUT OF LIMITS, 90 INCHES (NR 22794).

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

CANTED BULKHEAD HAS CORROSION, 1X1 INCHES (NR 22833).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

MAIN DECK FLOORBEAM HAS CORROSION ON SKIN AND STIFFENER (SEVERAL SPOTS 1X1 INCHES).

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

MAIN DECK FLOORBOARD HAS CORROSION ON SKIN AND STIFFENER (SEVERAL LOCATIONS 1X1 INCHES).

Part: FLOOR PANEL — CORRODED (COCKPIT) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

FIRST OFFICERS FLOOR PANEL SKIN CORRODED AND PUNCTURED (1X1 INCHES).

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

MAIN DECK FLOORBOARD SKIN & STIFFENERS HAS CORROSION (1 X 1 SEVERAL).

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

MAIN DECK FLOORBOARD SKIN HAS CORROSION (1 X 1 SEVERAL).

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

MAIN DECK FLOORBOARD SKIN & STIFFENER HAS CORROSION (1 X 1 SEVERAL).

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

MAIN DECK FLOORBOARD SKIN AND SPLICE PLATES (1X1 INCHES NUMEROUS LOCATIONS).

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

MAIN DECK FLOORBOARD SKIN & STIFFENER HAS CORROSION (1 X 1 SEVERAL).

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

MAIN DECK FLOORBOARD SKIN AND STIFFENERS ( 1X1 INCHES, NUMEROUS LOCATIONS ).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

PANEL SUPPORT AT FLOOR FOR EPC, BELOW CIRCUIT BREAKERS (1X1 INCHES).

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

MAIN DECK FLOORBOARD SKIN & SPLICE HAS CORROSION (1 X 1 SEVERAL).

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

MAIN DECK FLOORBOARD SKIN AND STIFFENERS (1X1 INCHES).

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

MAIN DECK FLOORBOARD SKIN AND STIFFNERS (1X1 INCHES IN NUMEROUS LOCATIONS).

Part: SILL — CORRODED (FUSELAGE) · airframe 48,966 hrs · 54,322 cycles

MAIN CARGO DOOR SILL PLATE HAS SEVERAL AREAS OF CORROSION (1X1 INCHES).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,966 hrs · 54,322 cycles

SEAT TRACK HAS SEVERAL AREAS OF CORROSION ON LOWER HORIZONTAL LEG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

SEAT TRACK UPPER AND LOWER HORIZONTAL SURFACES HAS SEVERAL AREAS OF CORROSION, 1X1 INCH (NR 21961).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

SEAT TRACK HAS SEVERAL AREAS OF CORROSION ON LOWER HORIZONTAL LEGS, 1X1 INCHES (NR 21942).

Part: SKIN — CRACKED (CARGO DOOR) · airframe 48,966 hrs · 54,322 cycles

FWD CARGO DOOR, INTERNAL SKIN CRACKED BY LOWER AFT DOOR STOP FITTING, (LOCATED AT MAIN CARGO DOOR).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

UPPER FLOORBEAM CAP TOP SIDE HAS SEVERAL AREAS OF CORROSION (1X1 INCHES).

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

FORWARD PIT CORROSION AT STRINGER 29R AND 29L ON FRAME (NR 21784).

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

LOWER CANTED BULKHEAD SPLICE PLATE HAS CORROSION, 1X1 INCH (NR 21904).

Part: ANGLE — CRACKED (RT PYLON) · airframe 48,966 hrs · 54,322 cycles

RIGHT PYLON MID SPAR WEB I/B LOWER ANGLE PREVIOUS REPAIR CRACKED (1 INCH).

Part: FITTING — CRACKED (FUSELAGE) · airframe 48,966 hrs · 54,322 cycles

CRACKED FITTING FWD OF R1 DOOR APPROX BS 160R 1X1 INCHES (NR21854).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

FLOORBEAM LWR HORIZONTAL CHORD UPPER SIDE HAS CORROSION, 1X1 INCHES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

FLOORBEAM LOWER HORIZ FLANGE AFT SIDE CORROSION AROUND FASTENER (NR 21744).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,322 cycles

FLOORBEAM LOWER HORIZ CHORD UPPER SIDE HAS CORROSION, 1X1 INCHES (NR21709).

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,966 hrs · 54,332 cycles

FUSELAGE SKIN AT FWD EDGE OF L1 DOOR STA 160 STR 11 HAS CREASE (KM40-21631).

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,966 hrs · 54,332 cycles

SKIN AT STA 165, STR 30 HAS CORROSION AND CRACKED.