N319CM

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 86,935 hrs · 31,883 cycles

CRACK ON THE NR 1 PYLON UPPER SKIRT FAIRING STRUCTURE AT FASTENER HOLE.

Part: RIB — DAMAGED (LT WING) · airframe 86,935 hrs · 31,883 cycles

LEFT WING RIB WEB AT WS 438.2 HAS MULTIPLE ELONGATED HOLES COMMON THE BACKUP FITTING.

Part: WEB — CORRODED (BS 610-632) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON UPPER AND LOWER SIDE OF THE WEB BS 610 - 632, RBL 30 TO 38.

Part: SUPPORT — CORRODED (BS 687) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO FLOOR DRAIN SUPPORT CORRODED BETWEEN SECTION 43-45 FROM LBL 88 & RBL 88.

Part: FLOORBEAM — CORRODED (BS 610) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON THE FLOORBEAM BS 632, RBL 32 TO 39.

Part: RETAINER — CORRODED (BS 287) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

NLG WW AFT DOOR SEAL RETAINER IS CORRODED AND DAMAGED.

Part: RIB — GOUGED (LT WING) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

LEFT WING RIB AT WS 438.2 HAS MULTIPLE GOUGES COMMON TO BACKUP FITTING.

Part: FITTING — CORRODED (BS 955) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO RBL 77 TO RBL 88, PRESSURE DECK FITTING CORROD AT BS 955.

Part: TEE FITTING — DAMAGED (BS 955-977) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

LEFT TEE FITTING DAMAGED.

Part: ANTENNA — CORRODED (BS 400) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON TCAS ANTENNA BS 400.

Part: WEB — DAMAGED (BS 632-654) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

WEB CRACKED IN CENTER AND CORROSION IN VARIOUS AREAS.

Part: PANEL — CORRODED (BS 610) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

BILGE PANEL CORRODED AT BS 610, RBL 6.

Part: STIFFENER — CRACKED (NR 2 PYLON) · airframe 86,935 hrs · 31,883 cycles

NR 2 PYLON, NAC STA. 285.4 HAS A CRACKED VERTICAL STIFFENER ON INBD SIDE OF PYLON.

Part: ANGLE — CHAFED (NR 1 NACELLE) · airframe 86,935 hrs · 31,883 cycles

NR 1 PYLON, NAC STA 303 ON THE INBOARD SIDE HAS AN ANGLE THAT IS CHAFED.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO FLOOR TRACK RBL 33.0 HAS NUMEROUS AREAS OF CORROSION FROM STA 478 TO STA 664.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO FLOOR TRACK RBL 77.0 HAS NUMEROUS AREAS OF CORROSION FROM STA 478-STA 664.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO FLOOR TRACK RBL 54.0 HAS NUMEROUS AREAS OF CORROSION FROM STA 478 TO STA 664.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO FLOOR TRACK RBL 88.0 HAS NUMEROUS AREAS OF CORROSION FROM STA 478 - STA 664.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SHEAR WEB IS CORRODED BETWEEN STA 478 - STA 522 UNDER PANEL 231G.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SHEAR WEB IS CORROSION BETWEEN STA 478 - STA 522 UNDER PANEL 231I.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FLC FLOOR PANEL SUPPORT CORRODED AND OUTBOARD PHENOLIC BLOCK CRACKED AT STA 605 LBL 9 TO LBL 22.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK CORRODED AT STA 654+82 RBL32,

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FLC HAS CORROSION ON BILGE FLOOR PANEL AT STA 619 TO 623 LBL 27.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO TRACK FITTING STATION 654+22 RBL 65 CORRODED.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO FLOOR TRACK LBL 11.0 HAS NUMEROUS AREAS OF CORROSION AT BS 478-664.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FLC BILGE FLOOR PANEL SURFACE UNDER PDU 9R CORRODED.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON UPPER SURFACE OF FLC BILGE PANEL AROUND FLOOR PANEL SUPPORT AT STA 544 AFT OF PDU 6R.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SHEAR WEB IS CORRODED BETWEEN STA 478 - STA 522 UNDER PANEL 232E.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO TRACK FITTING AT STA 654+88 RBL 0 CORRODED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FLC DIAGONAL FLOOR PANEL SUPPORT CORRODED AT STA 544 LBL 19.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO FLOOR TRACK RBL 11.0 HAS NUMEROUS AREAS OF CORROSION FROM STA 478 TO STA 664.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO TRACK AT STA 654+131 RBL 55 RBL 65 CORRODED.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FLC PDU 8L MOUNT PANEL HAS SURFACE CORROSION IN AREAS STA 566 TO 588 LBL 18 TO LBL 28.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER SURFACE OF FLC BILGE PANEL AT STA 588 BL0 CORRODED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FLC FLOOR SUPPORT AT STA 610 RBL 28 CORRODED AROUND NUTPLATES.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO FLOOR TRACK LBL 54.0 HAS NUMEROUS AREAS OF CORROSION AT BS 478-664.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FLC RIGHT SIDE RAIL ATTACH PLATE INTERCOSTAL CORRODED AT STA 629 RBL 40.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO FLOOR TRACK LBL 88.0 HAS NUMEROUS AREAS OF CORROSION AT BS 478-664.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK AT STA 654+121 RBL 12 CORRODED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

INTERCOSTAL SUPPORT ANGLE AT STA 632 RBL 30 IS CORRODED.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO FLOOR TRACK LBL 77.0 HAS NUMEROUS AREAS OF CORROSION AT BS 478-664.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STR 35L JUST AFT OF STA 434.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STR 37L AND SPLICE FROM STA 412 TO STA 456.

Part: SKIN — CRACKED (FUSELAGE) · airframe 86,935 hrs · 31,883 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED, VERIFIED WITH EDDY CURRENT, AT LOWER AFT CORNER OF R-1 DOOR CUTOUT.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORRODED ANGLE JUST INBR OF AREA AT THE FWD LWR SILL LC.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

ANTENNA DOUBLER IS CORRODED ON THE INTERIOR SURFACE LOCATED BTW STA 390 AND STA 412 BTW STR 39L AND STR 39R.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION BELOW UPPER CARGO FLOOR AT INBOARD CORNER OF DRAIN CHANNEL SUPPORT AT STA 1109 AT BUTT LINE 0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON THE AFT SIDE OF WEB ON FLC FLOORBEAM AT FRAME STA 390 BTW STR 39L AND STR 39R.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STR 36L AND SPLICE FROM STA 412 TO STA 456.

Part: WEB — CORRODED (RT WING) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON RIGHT WING LEADING EDGE OUTBOARD OF NUMBER 8 SLAT INBOARD AUX TRACK ON FORWARD SIDE OF CLOSE OUT WEB AS SEE THRU LIGHTNING HOLE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STRINGER 37R AND SPLICE FROM STA 412 TO STA 4566.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STR 38L AND SPLICE FROM STA 412 TO STA 456.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION AROUND NUTPLATES ON SPLICE ANGLE AT STA 503 LBL42.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STR 38R AND SPLICE FROM STA 412 TO STA 456.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STR 39L AND SPLICE FROM STA 412 TO STA 456.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FLC STA, 654+121 LBL23 UNDERSIDE OF FRAME UPPER CHORD, AFT SIDE, HAS CORROSION AROUND NUT PLATE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STRINGER 39R AND SPLICE FROM STA 412 TO STA 456.

Part: STIFFENER — CRACKED (NR 2 PYLON) · airframe 86,935 hrs · 31,883 cycles

NR 2 PYLON CRACKED VERTICAL STIFFENER.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO CORRODED FITTING ON PRESSURE DECK AT REAR SPAR.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FORWARD LOWER CARGO PDU MOUNT PANEL CORRODED.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FORWARD LOWER CARGO BILGE PANEL CORRODED LBL27.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO DRAIN SUPPORT CORRODED.

Part: RIB — DAMAGED (LT WING) · airframe 86,935 hrs · 31,883 cycles

LEFT WING RIB WEB AT WING STATION 438.2 ELONGATED HOLES COMMON TO BACKUP FITTING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FORWARD LOWER CARGO FLOOR SUPPORT CORRODED.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FORWARD LOWER CARGO WEB CORRODED RBL 30.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FORWARD LOWER CARGO INTERCOSTAL CORRODED STATION 629.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FORWARD LOWER CARGO PANEL SUPPORT CORRODED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FORWARD LOWER CARGO FLOOR SUPPORT CORRODED LBL 19.

Part: ANTENNA — CORRODED (TCAS) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

TCAS ANTENNA CORRODED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

INTERCOSTAL CORRODED STATION 632.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FORWARD LOWER CARGO BILGE PANEL CORRODED RBL 6.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CABIN SEAT CORRODED RBL32.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FORWARD LOWER CARGO BILGE PANEL CORRODED 9R.

Part: RETAINER — CORRODED (NLG WW) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

NOSE WHEEL WELL SEAL RETAINER CORRODED.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FORWARD LOWER CARGO PANEL CORRODED.

Part: RIB — GOUGED (LT WING) · airframe 86,935 hrs · 31,883 cycles

LEFT WING RIB AT WS 438.2 GOUGES COMMON TO BACK UP FITTING.

Part: ANGLE — CHAFED (NR 1 PYLON) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

NR 1 PYLON ANGLE CHAFED.

Part: WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

WEB CRACKED STATION 632 RBL35.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FORWARD LOWER CARGO FLOORBEAM CORRODED.

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 86,935 hrs · 31,883 cycles

NR 1 PYLON SKIRT FAIRING CRACKED.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 86,935 hrs · 31,883 cycles

STATION 955 T-FITTING DAMAGED.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

BILGE PANEL CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CABIN SEAT TRACK CORRODED LBL 88.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK CORRODED RBL 12.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO TRACK FITTING CORRODED.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK FITTING CORRODED RBL 65.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK CORRODED RBL 88.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CABIN SEAT TRACK CORRODED RBL 77.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SHEAR WEB CORRODED LBL 11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK CORRODED RBL 55 TO 65.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SHEAR WEB CORRODED RBL 11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK CORRODED RBL 54.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SHEAR WEB CORRODED LBL 55 TO LBL 77.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CABIN SEAT TRACK CORRODED LBL 54.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK LBL 11 CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK CORRODED LBL 77.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION AROUND NUTPLATES ON SPLICE ANGLE AT STA 503, LBL42.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

FORWARD LOWER CARGO STA 654+121, LBL 23 UNDERSIDE OF FRAME UPPER CHORD (AFT SIDE) HAS CORROSION AROUND NUT PLATE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CABIN SEAT TRACK CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO FLOOR TRACK RBL 11.0 HAS NUMEROUS AREAS OF CORROSION.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STR 35L JUST AFT OF STA 434.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON THE AFT SIDE OF WEB ON FLC FLOOR BEAM AT FRAME STA 390 BTW STR 39L AND STR 39R.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STR 39R AND SPLICE FROM STA 412 TO STA 456.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORRODED ANGLE JUST INBD OF AREA AT THE FWD LWR SILL LC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 86,935 hrs · 31,883 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED (VERIFIED WITH EDDY CURRENT)AT LOWER AFT CORNER OF R-1 DOOR CUTOUT.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STR 37R AND SPLICE FROM STA 412 TO 456.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STR 37L AND SPLICE FROM STA 412 TO STA 456.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STR 38R AND SPLICE FROM STA 412 TO STA 456.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION BELOW UPPER CARGO FLOOR AT INBOARD CORNER OF DRAIN CHANNEL SUPPORT AT STA 1109 AT BUTT LINE 0.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STRINGER 36L AND SPLICE FROM STA 412 TO STA 456.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON STR 38L AND SPLICE FROM STA 412 TO STA456.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

ANTENNA DOUBLER IS CORRODED ON THE INTERIOR SURFACE LOCATED BTW STA 390 AND STA 412 BTW STR 39L AND STR 39R.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK(S) ARE CRACKED IN THE RADIUS, ON THE LOWER SURFACES, ON THE FWD AND AFT SIDE OF STA 785.9, LBL88 AND RBL88.

Part: DOOR FRAME — CRACKED (R1) · airframe 86,935 hrs · 31,883 cycles

R1 DOOR LOWER FRAME CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK RBL 11 STA1461-1600 HAS MULTIPLE SPOTS OF CORROSION.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO, RBL 88 SEAT TRACK FS 752-923 CRACKED AT STA 785.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO STA 1600 DRAIN GUTTER SUPPORT ANGLE LBL36-53 IS CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION UNDER SEAT TRACK AT STA 1405 RBL88.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK LBL 11 STA 1461-1600 HAS MULTIPLE SPOTS OF CORROSION.

Part: STRUCTURE — CORRODED (NLG WW) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

NWW STA 247, RBL 25.0 CHORD IS CORRODED AT BULKHEAD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK LBL33 STA 1461-1600 HAS MULTIPLE SPOTS OF CORROSION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

ALC STA 1415 FLOOR SUPPORT BEAM W/CORROSION.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO STA 1480-1540 RBL 82 DOOR SILL CHORD IS CORRODED ON BOTTOM FLANGE.

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

RT OUTBD FLAP UPPER SKIN CORRODED AT AREA ABOVE INDB FAIRING STA 95-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK RBL33 STA 1461-1600 HAS MULTIPLE AREAS OF CORROSION.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

LEFT WING CORRODED AT LOWER CHORD AREA 8 INCHES FROM PYLON.

Part: CAP — CRACKED (RT WING) · airframe 86,935 hrs · 31,883 cycles

RIGHT WING LEADING EDGE UPPER AIRLOAD RIB LOWER CAP CRACKED AT LES 520.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK RBL 54 STA 1461-1600 HAS MULTIPLE OF CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON SEAT TRACK AT STA 1210 RBL11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION AT NUTPLATE ON FLC LOWER FLOORBEAM AT STA 654+121 LBL 24.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

UPPER CARGO SEAT TRACK LBL 54 STA 1461-1600 HAS MULTIPLE SPOTS OF CORROSION.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 86,935 hrs · 31,883 cycles

CRACK INDICATION NOTED IN FAIL-SAFE AT FWD SIDE OF LWR BOLT HOLE COMMON TO "T" FITTING.

Part: BUSHING — CORRODED (RT WING) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

CORROSION ON RT WING LWR SURFACE AT AUX TANK INBD SUMP DRAIN.

Part: BEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,935 hrs · 31,883 cycles

LEFT FWD OVERWING EXIT CUTOUT, FWD LOWER CORNER CORRODED.

Part: SEAL — LEAKING (ENGINE OIL) · airframe 85,761 hrs · 31,246 cycles

PRECAUTIONARY LANDING DUE TO LEFT OIL QUANTITY INDICATING ZERO, ALL OTHER INDICATIONS NORMAL. LEFT ENGINE OIL PRESSURE STEADY 28 PSI.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 83,560 hrs · 30,079 cycles

EICAS MESSAGE: LT STRUT DUCT LEAK. THE PRV CLOSED AUTOMATICALLY BECAUSE THE STRUT TEMPERATURE IS TOO HIGH.

Part: SKIN — CRACKED (BS 456-478) · airframe 83,020 hrs · 29,819 cycles

FUSELAGE EXTERNAL SKIN SHOWS A 1" CRACK, BS 456-478, S-31R-S32R, REF NR 0077.

Part: BEAM — CORRODED (SPOILER) · corrosion level 2 · airframe 79,490 hrs · 28,061 cycles

TRAILING EDGE LOWER PANEL ATTACH CHORD SPOILER SPLIT ON EDGE. OTBD LOWER SPOILER BEAM CHORD R & R IAW REA 47112REA05.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,490 hrs · 28,061 cycles

CORROSION OUT OF LIMITS ON MAIN DECK CARGO DOOR CUT OUT LOWER SILL LOWER SEAL DEPRESSOR. REPAIRED AREA IAW ENGINEERING ASSISTANCE DOCUMENT 47112REA06.

Part: SUPPORT — CRACKED (LT WING) · airframe 79,490 hrs · 28,061 cycles

LEFT WING ROTARY ACTUATOR SUPPORT NR 1 THREE CRACKED HOLES AT 11 O'CLOCK, 12 O'CLOCK & 5 O'CLOCK POSITION. THREE CRACKED HOLES OF THE LT WING ROTARY ACTUATOR SUPPORT REPAIRED IAW REA 47112REA04.

Part: STRUCTURE — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 79,490 hrs · 28,061 cycles

CORROSION NOTED NR 1 PYLON LBL 4 TO LBL 5, WL 123 TO WL 125. R & R CHORD IAW SRM 51-40-02.

Part: STIFFENER — CRACKED (NR 2 PYLON) · airframe 79,490 hrs · 28,061 cycles

NUMBER 2 PYLON AFT SIDE OF STRUT, LT & RT STIFFENERS CRACKED. OLD STIFFENERS REMOVED. NEW STIFFENERS FABRICATED IAW DWG 313T3380 & INSTALLED IAW SRM 51-40-02. PROTECTIVE COATING APPLIED IAW SRM 51-20-01.

Part: ANGLE — CRACKED (WING) · airframe 79,490 hrs · 28,061 cycles

CRACKED ANGLE AT NR 1 LOWER STRUT FAIRING OTBD AFT UPPER CORNER. R & R CRACKED ANGLE IAW SRM 51-40-02.

Part: RIB — CRACKED (LT WING) · airframe 79,490 hrs · 28,061 cycles

LEFT WING INTERNAL LE, AIR LOAD CRACKED AT THE UPPER ATTACHMENT NEAR ILES 685.0 HFEC VERIFIED. R & R LT WING LE AIR LOAD RIB & WEB AT LWS 685 IAW SRM 51-40-02.

Part: RIB — CRACKED (LT WING) · airframe 79,490 hrs · 28,061 cycles

LEFT WING INTERNAL LE, AIR LOAD RIB CRACKED AT THE UPPER ATTACHMENT NEAR ILES 651.1 HFEC VERIFIED. R & R AIR LOAD AT UPPER ATTACHMENT IAW 57-41-09 & 51-40-02 & SRM 51-40-03. PAINTED & C1C PROTECTED IAW SRM 51-20-01 & SRM 53-50-01.

Part: RIB — CRACKED (LT WING) · airframe 79,490 hrs · 28,061 cycles

LEFT WING INTERNAL LE AIR LOAD RIB IS CRACKED AT THE UPPER ATTACHMENT AT ILES 500.0 VERIFIED WITH HFEC. REPLACED LOWER CHORD FOR UPPER ATTACH POINT IAW SRM 57-41-09 & SRM 51-40-02. TREATED & PAINTED WITH CIC PROTECTION IAW SRM 51-20-01 & SRM 53-50-01.

Part: SUPPORT BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 92,360 hrs · 24,103 cycles

LEFT WING TE UPPER PANEL SUPPORT BEAM CORRODED ON UPPER FLANGE ALONG ENTIRE LENGTH AT WS 285. R & R LT WING TE SUPPORT BEAM IAW SRM 51-40-02.

Part: BRACKET — CRACKED (LT MLG DOOR) · airframe 79,037 hrs · 27,898 cycles

LEFT MLG DOOR LOOSE. FWD BRACKET ON MLG DOOR BROKEN. REPLACED FWD TRUNNION DOOR HINGE FITTING & INSTALLED LT TRUNNION DOOR IAW B767 AMM 32-12-11.

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 78,510 hrs · 27,695 cycles

NR 1 ENGINE PYLON INSPECTION, FOUND A CRACK AT ANGLE AT INTERCOSTAL TO FORWARD MIDSPAR FITTING. R & R ANGLE IAW SRM 51-40-2. ACFT GROUNDED.

Part: TRANSFER SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 75,960 hrs · 26,637 cycles

RT MAIN TANK TRANSFERRED FUEL INTO CENTER TANK AT A RATE OF 200 KILOGRAMS PER MINUTE. RETURNED TO STATION. DEFUEL/REFUEL VALVES CHECKED GOOD. R & R RT DEFUELING VALVE IAW AMM 28-26-01/401. R & R CENTER RT DISCHARGE CK VALVE IAW AMM 28-22-05/401. R & R RIGHT VENT CK VALVE IAW AMM 28-22-09/401. R & R RT SHUTOFF VALVE IAW AMM 28-21-02/401. R & R RT SHUTOFF VALVE CONTROL UNIT IAW 28-21-12/401. REMOVED, CLEANED, INSPECTED & INSTALLED MOTIVE FLOW & SCREEN VALVE IAW AMM 28-22-05/404, SCAVENGE JET PUMP IAW AMM 28-22-13/401, FLOAT OPERATED SHUTOFF VALVE IAW 28-22-10/401 & DRAIN CK VALVE IAW AMM 28-21-05/401. OPS TESTED NORMAL IAW AMM 28-21-00/501. FUEL MIGRATION CHECK COMPLIED WITH. NONE NOTED.

Part: WIRE — BURNED (PDU HARNESS) · airframe 75,500 hrs · 26,525 cycles

DURING INSPECTION, FOUND BURNED WIRES AT BS 680 FORWARD CARGO COMPARTMENT POWER DRIVE UNIT WIRE HARNESS IN POSITION 13L. REPAIRED WIRES IAW IAW WDM 25-53-14 SHT 5, 25-53-12 SHT 1 AND SWPM 20-60-11, 20-00-11 AND 20-30-12. OPS TEST NORMAL IAW AMM 25-53-00/501.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR)

DURING FL310, MAIN CARGO DOOR LIGHT ILLUMINATED. THE CREW RETURNED TO DEPARTURE WITHOUT INCIDENT. FOUND SWITCH S9022 OUT OF TOLERANCE. ADJUSTED SWITCH IAW AMM 52-71-09. DOOR LIGHTS AND SWITCHES OP CHECKED GOOD. DEPRESSURIZED ACFT. PREFORMED OPS CHECKED AND TESTED DOOR AND SWITCHES IAW AMM 52-30-00. OPS CHECKED GOOD. ACFT WAS RETURNED TO SERVICE.

Part: SELECTOR SWITCH — DEFECTIVE (ANTI ICE SYSTEM) · airframe 74,854 hrs · 26,353 cycles

RIGHT ENGINE ANTI ICE SWITCH SMOKED AND HAD BURNING ODOR WHEN PLACED TO ON POSITION. MX R & R SWITCH ASSY IAW MM 33-13-00/201 AND WDM 30-21-11. SWITCH OPS CHECK GOOD. VERIFIED, ACFT RELEASED TO ETOPS 180.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR)

DURING CRUISE, THE MAIN CARGO DOOR LIGHT ILLUMINATED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. OPEN

Part: SWITCH — OUT OF ADJUST (CARGO DOOR LATCH) · airframe 74,384 hrs · 26,259 cycles

DURING CRUISE, THE MAIN CARGO DOOR LIGHT ILLUMINATED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX PERFORMED FIM PROCEDURES 52-71-00, FIG 106 BLOCKS 1, 2, 11, AND 22. ADJUSTED AFT DOOR LOCK SWITCH IAW AMM 52-71-09/201. DOOR WARNING SYS CHECKED GOOD IAW AMM 52-32-00/501. ACFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 74,267 hrs · 26,233 cycles

DURING CLIMB OUT, FAULT CODE 52-34-XB-00, MAIN CARGO DOOR LIGHT ILLUMINATED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX PERFORMED CARGO DOOR OPS CHECK IAW IAI 52-32-00. PRESSURIZED ACFT TO 4.5 IAW MM 05-51-22. INDICATIONS WERE NORMAL. INSPECTED ALL DOOR LATCHES FOR SIGNS OF DAMAGE. NONE NOTED. ACFT WAS RETURNED TO SERVICE.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 74,270 hrs · 26,234 cycles

DURING CLIMB OUT, FAULT CODE 52-34-XB-00, MAIN CARGO DOOR LIGHT ILLUMINATED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT MAIN CARGO DOOR SYS AND FOUND LOCK BAR SWITCH OUT OF ADJUSTMENT. THEY ADJUSTED LOCK BAR SWITCH IAW IAI MM SUPPLEMENT 52-71-09 PAGE 205. OPS CHECK GOOD IAW IAI MM SUPPLEMENT 52-32-00. ACFT WAS RETURNED TO SERVICE.

Part: SHUTOFF VALVE — DEFECTIVE (ZONE 100) · airframe 74,141 hrs · 26,207 cycles

DURING DESCENT, SHORTLY AFTER FLAPS 1 SELECTED; EICAS MESSAGES DISPLAYED, C HYD PRIME 1, REV BRAKE VALVE, HYD QTY AND RESERVE BRAKE & STEERING SWITCH VALVE. CREW ACCOMPLISHED CHECKLIST PROCEDURES, AN ADVISORY IN CHECK LIST PROCEDURES WARNED OF POSSIBLE LOSS OF NOSE WHEEL STEERING. PRIOR TO FINAL APPROACH HYD PRESSURE DECREASING AT A RATE OF 10 PSI IAW SECOND AND WHEN LANDING GEAR LOWERED HYD PRESSURE DROPPED TO ZERO & NOSE GEAR FAILED TO EXTEND. ABANDON APPROACH TO EXECUTE ALTERNATE NOSE GEAR EXTENSION PROCEDURES WHICH WAS SUCCESSFUL. AFTER LANDING, NOSE WHEEL STEERING INOPERATIVE. MX REPLACED SHUTOFF CONTROL VALVE, OPS CHECKED GOOD IAW MM 29-11-07 TASK 29-11-07-004-001. ALSO REPLACED HYD QTY MONITOR UNIT, OPS CHECKED GOOD IAW MM 29-33-01. RETURNED TO SERVICE.