N765CK

Part: STRINGER — CORRODED (ZONE 300) · corrosion level 3 · airframe 90,877 hrs · 27,713 cycles

CORROSION FOUN DURING SURFACE HFEC AT HORZ STAB UPPER STRINGER S-5L AND LBL 39 ON LOWER AFT FLANGE UPPER SURFACE. REPAIRED PER KALITTA DWG 55102302-1 OR.

Part: STIFFENER — CRACKED (ZONE 700) · airframe 90,877 hrs · 27,713 cycles

DURING ACCOMPLISHMENT OF AD 2005-02-02. CRACK INDICATION WAS FOUND EXTENDING BELOW WL 160. REPAIR WAS ACCOMPLISHED PER BOEING.

Part: FRAME — CORRODED (ZONE 200) · airframe 90,877 hrs · 27,713 cycles

CORROSION FOUND ON AFT LOWER SIDE OF PRESSURE DECK FRAME AT STA 977, RBL 97. REPAIRED PER KALITTA DWG 53502301.1-OR

Part: STRINGER — CORRODED (ZONE 300) · airframe 90,877 hrs · 27,713 cycles

CORROSION FOUND ON SURFACE HFEC AT HORZ STAB UPPER STRINGER S-9L AND LBL 39 ON LOWER AFT FLANGE UPPER SURFACE.

Part: STRINGER — CORRODED (ZONE 300) · corrosion level 3 · airframe 90,877 hrs · 27,713 cycles

FOUND SURFACE CORROSION ON HORIZONTAL STABILIZER UPPER STRINGER S-10R AND RBL 39 ON LOWER FLANGE. REPAIRED PER KALITTA DWG 55102304-1.

Part: LAMP — BLOWN (ZONE 200) · airframe 90,877 hrs · 27,713 cycles

FLIGHT DECK EMERGENCY LIGHT INOPERATIVE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,664 hrs · 27,634 cycles

AFTER TAKEOFF, TCAS FAILED AND CB POPPED. RESET CB. ONE HOUR INTO FLIGHT GOT MESSAGE FWD EQUIP COOLING AND SMELLED SMOKE. PULLED TCAS CB AND SMELL SLOWLY DISSIPATED.

Part: SKIN — CORRODED (BS 1210 S39R) · corrosion level 3 · airframe 89,898 hrs · 27,363 cycles

CORROSION AND CRACK FOUND ON LOWER FUSELAGE SECTION 46 SKIN, BS 1210, S39R.

Part: LIGHT — INOPERATIVE · airframe 89,059 hrs · 26,941 cycles

RIGHT OVERHEAD EMERGENCY LAMP ON FLIGHT DCK FAILS TO ILLUMINATE

Part: LIGHT — INOPERATIVE · airframe 89,059 hrs · 26,941 cycles

L1 DOOR EXIT SIGN FAILS TO ILLUMINATE

Part: LIGHT — INOPERATIVE · airframe 89,059 hrs · 26,941 cycles

L1 DOOR WINDOW SILL EMERGENCY LAMP (L313) FAILS TO ILLUMINATE

Part: SEAT TRACK — CRACKED · airframe 89,059 hrs · 26,941 cycles

CAPTAIN`S FWD INBOARD SEAT TRACK IS CRACKED ON FWD END

Part: WEB — DAMAGED · airframe 89,059 hrs · 26,941 cycles

WEB FLOOR DAMAGED AT APPROX STA. 548-566 RBL 31-38

Part: INTERCOSTAL — DAMAGED · airframe 89,059 hrs · 26,941 cycles

INTERCOSTAL DAMAGED AT APPROX STA. 510 RB2 46-54

Part: DOOR SILL — CORRODED · corrosion level 2 · airframe 89,059 hrs · 26,941 cycles

FORWARD CARGO COMPARTMENT DOOR CUTOUT SURROUND - LWR SILL AREA @ APPROX. STA 585 HAS EVIDENCE OF CORROSION

Part: TARGET — INCORRECT (LE SLAT SYSTEM) · airframe 87,479 hrs · 26,156 cycles

LEADING EDGE ASYMMETRIC. FOUND INBOARD AND OUTBOARD LEADING EDGE SLAT SENSOR TARGETS SWAPPED. REPOSITIONED TO CORRECT POSITIONS, IAW B767 AMM 20-11-00. OPERATIONS CHECKS GOOD, IAW B767 AM 27-88-01.

Part: FUEL TANK — CORRODED (FUEL SYSTEM) · corrosion level 2 · airframe 87,011 hrs · 25,928 cycles

EVIDENCE OF CORROSION AROUND FASTENER HEADS OF TOP SURFACE OF CENTER FUEL TANK AT APPROX STA 958 LBL 18.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,011 hrs · 25,928 cycles

EVIDENCE OF CORROSION INSIDE THE BORE OF MDCD LATCH PIN FITTING NR 7 P/N 95345-203.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,011 hrs · 25,928 cycles

EVIDENCE OF CORROSION INSIDE THE BORE OF MDCD LATCH PIN FITTING NR 4 P/N 95345-204.

Part: FITTING — CHAFED (RT AILERON) · airframe 87,011 hrs · 25,928 cycles

RIGHT INBOARD AILERON, OUTBOARD FAIL-SAFE FITTING HAS CHAFING DAMAGE.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,011 hrs · 25,928 cycles

EVIDENCE OF CORROSION TOP SIDE OF LT LOWER KEEL BEAM CHORD APPROX STA 795.

Part: KEELBEAM — CORRODED (BS 914) · corrosion level 2 · airframe 87,011 hrs · 25,928 cycles

EVIDENCE OF CORROSION TOP SIDE OF R/H LOWER KEEL BEAM CHORD APPROX STA 914

Part: KEELBEAM — CORRODED (BS 921) · corrosion level 2 · airframe 87,011 hrs · 25,928 cycles

EVIDENCE OF CORROSION TOP SIDE OF L/H LOWER KEEL BEAM CHORD APPROX STA 921

Part: KEELBEAM — CORRODED (BS 954) · corrosion level 2 · airframe 87,011 hrs · 25,928 cycles

EVIDENCE OF CORROSION TOP SIDE OF R/H LOWER KEEL BEAM CHORD APPROX STA 954

Part: KEELBEAM — CORRODED (BS 911) · corrosion level 2 · airframe 87,011 hrs · 25,928 cycles

EVIDENCE OF CORROSION TOP SIDE OF R/H LOWER KEEL BEAM CHORD APPROX STA 911

Part: KEELBEAM — CORRODED (BS 898) · corrosion level 2 · airframe 87,011 hrs · 25,928 cycles

EVIDENCE OF CORROSION TOP SIDE OF L/H LOWER KEEL BEAM CHORD APPROX STA 898

Part: STOP FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

AFT CARGO DOOR AFT HOOK STOP FITTING CORRODED.

Part: MOUNT FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

LT O/B FLAP SUPPORT MECHANISM FLAP SUPPORT TO WING REAR SPAR FITTING ON O/B MOUNT INSIDE BORE HAS CORROSION.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON TORQUE BOX WEB IN AFT CARGO COMPARTMENT AT STA 1272 - 1280, RBL 11 - 16.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

TORQUE BOX WEB BS 1263 - 1285 RBL 38 SHOWS EVIDENCE OF CORROSION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FRAME UPPER CHORD HAS CORROSION AT STA 1285 RBL 35.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO COMPARTMENT DOOR LOWER SILL WEB AT STA 1367 RBL 45.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT TORQUE BOX INTERCOSTAL HAS EVIDENCE OF CORROSION AT STA 610 RBL 24.

Part: ACCESS PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

WEB ACCESS PANEL HAS CORROSION AT STA 1263 - 1285 LBL 32 - 39.

Part: ACCESS PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

WEB ACCESS PANEL HAS CORROSION AT STA 1263 TO 1285 RBL 17 - 33.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOOR INTERCOSTAL STA 1329 LBL 25.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT LWR FRAME UPPER CHORD HAS EVIDENCE OF CORROSION STA 654 +44 LBL 20.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON UPPER CHORD IN AFT PIT FLOOR, STA 1285 APPROX RBL 25.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

CORROSION ON SUPPORT AT STA 1263-1285 LBL 33.

Part: FRAME — CORRODED (BS 1197) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FRAME UPPER CHORD HAS CORROSION @ STA 1197 +22

Part: WEB — CORRODED (TORQUE BOX) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON TORQUE BOX WEB @ STA 630 RBL 30 IN FWD PIT

Part: FRAME — CORRODED (BS 1263) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CORGO COMPARTMENT FLOOR FRAME UPPER CHORD AT STA 1263 RBL 22

Part: STIFFENER — CORRODED (BS 1809 BULKHEAD) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON STIFFENER AT STA 1809.5 BULKHEAD RBL 5

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

CORROSION ON INTERCOSTAL FWD PIT STA 510 RBL 4.

Part: INTERCOSTAL — CORRODED (BS 610) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT TORQUE BOX INTERCOSTAL HAS EVIDENCE OF CORROSION @ STA 610 RBL 27

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON STIFFENER AT STA 1809.5 RBL 10.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

STA 1809.5 BULKHEAD LWR AFT CHORD REPAIR ANGLE HAS CORROSION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT LWR FRAME UPPER CHORD HAS EVIDENCE OF CORROSION AT STA 654+110 RBL 5.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

TORQUE BOX WEB AT STA 1332 LBL 31 HAS EVIDENCE OF CORROSION.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO TORQUE BOX UPPER WEB SCREW HOLES STA 1153 BL 0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOOR BEAM STA 1241 LBL 40.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON TORQUE BOX WEB AND PREVIOUS WEB REPAIR AT STA 1336 - 1342, RBL 17 - RBL 24.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOOR INTERCOSTAL STA 1351 LBL 30.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

INTERCOSTAL AT STA 1153 - 1175 RBL 10 HAS EVIDENCE OF CORROSION.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

TORQUE BOX WEB AT STA 1350 LBL 18 HAS EVIDENCE OF CORROSION.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

INTERCOSTAL AT STA 1153 - 1175 LBL 10 HAS EVIDENCE OF CORROSION.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

TORQUE BOX WEB AT STA 1336 LBL 11 - LBL 18 HAS EVIDENCE OF CORROSION.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

AFT CARGO DOOR SILL AFT LOWER HOOK STOP ASSEMBLY HAS CORROSION AT MOUNTING AREA AT APPROX STA 1335.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT CHORD HAS EVIDENCE OF CORROSION AT STA 654 +66 TO 654 +88 RBL 42.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

TORQUE BOX WEB AT STA 1336 RBL 15 HAS EVIDENCE OF CORROSION.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

TORQUE BOX UPPER WEB IN AFT PIT BETWEEN STA 1263 AND 1285 LBL 38 HAS POSSIBLE CORROSION.

Part: FRAME — CORRODED (BS 654) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT LOWER FRAME UPPER CHORD HAS EVIDENCE OF CORROSION AT STA 654+22

Part: FITTING — CORRODED (STRINGER 36R) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

STRINGER END FITTING HAS EVIDENCE OF CORROSION AT STA 1809.5 S-36R

Part: FRAME — CORRODED (BS 654) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT LOWER FRAME UPPER CHORD HAS EVIDENCE OF CORROSION AT STA 654+121 LBL 25

Part: FRAME — CORRODED (BS 654) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT LWR FRAME UPPER CHORD HAS EVIDENCE OF CORROSION AT STA 654+88 LBL 22

Part: WEB — CORRODED (BS 1461-1480) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

WEB IN BULK CARGO PIT AT STA 1461-1480 STR 33R IS CORRODED

Part: TORQUE BOX — CORRODED (BS 500) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT TORQUE BOX TOP SURFACE WEB JUST OUTBOARD OF PDU STATION 500 RBL APPRX 36 HAS CORROSION

Part: DOOR FRAME — CORRODED (ACCESS DOOR) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

ACCESS DOOR 313AL, R/H SIDE FRAME HAS EVIDENCE OF CORROSION

Part: WEB — CORRODED (BS 1417-1439) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

BULK CARGO COMPARTMENT WEB ASSY BETWEEN STA 1417 AND 1439 RBL 43 HAS EVIDENCE OF CORROSION

Part: ANGLE — CORRODED (BS 1450) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON BULK CARGO DOOR CUTOUT UPPER INTERIOR ANGLE STA 1450, LBL 80, WL 180

Part: TORQUE BOX — CORRODED (BS 610-632) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT TORQUE BOX HAS SUSPECTED CORROSION BENEATH TORQUE BOX FIXED PANEL STATION APPRX 632 TO 610 RBL APPRX 18

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT LWR FRAME UPPER CHORD HAS EVIDENCE OF CORROSION AT STA 676 RBL 22.

Part: STRINGER — CRACKED (LT HORIZ STAB) · airframe 85,070 hrs · 24,889 cycles

CRACK ON STRINGER AT LT HORIZ STAB BL 333.5 INSIDE ACCESS PNL 335 ACZ.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

STRINGER S-32R HAS EVIDENCE OF CORROSION FROM STA 1809.5-1832.

Part: FLOOR PANEL — CORRODED (COCKPIT) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

POSSIBLE CORROSION FLIGHT DECK FLOOR STA 164.5 TO 212.5.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

MAIN EQUIP CENTER ELECTRONICS ACCESS DOOR CUTOUT HAS CORROSION ON LT SIDE AT DOOR CLIP ATTACHMENT.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT AT STA 486 RBL 19 POSSIBLE CORROSION UNDER INTERCOSTAL AT NUTPLATE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

MAIN DECK LT FUSELAGE STA 1087 STR 12L WALL FRAME HAS EVIDENCE OF CORROSION.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

AFT CARGO DOOR SILL FWD LOWER HOOK STOP ASSEMBLY HAS CORROSION ON MOUNTING AREA AT APPROX STA 1285.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1087 LBL 20.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

AREAS OF POSSIBLE CORROSION ON FUSELAGE SKIN AT THE FWD END OF TAIL SKID FAIRING AREA.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT TORQUE BOX WEB HAS EVIDENCE OF CORROSION AT STA 485 RBL 2.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

AREAS OF POSSIBLE CORROSION ON AFT END OF TAIL SKID FAIRING AREA ON FUSELAGE SKIN.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT TORQUE BOX WEB HAS EVIDENCE OF CORROSION STA 612 LBL 9.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOOR BEAM STA 1197 +88 LBL 40.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1109 RBL 20.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1197 +132 RBL 40.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1241 LBL 8.

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1131 RBL 5.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

FWD PIT PALLET LOCK STRUCTURE, STATION APPRX 615 RBL APPRX 5 HAS CORROSION WHERE MEETS TORQUE BOX SKIN.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1197 +110 RBL 18 TO RBL 40.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1131 RBL 22.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1219 LBL 18 TO LBL 40.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1219 RBL 18 TO RBL 40.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1197 +66 RBL 18 TO RBL 40.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1197 +44 RBL 18 TO RBL 40.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1197 +44 RBL 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1153 LBL 18 TO LBL 40.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1197 RBL 18 TO RBL 40.

Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

HORIZONTAL STAB BOX UPPER STRINGER 2 AT LBL 40 HAS EVIDENCE OF CORROSION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1153 RBL 18 TO RBL 40.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1197 LBL 18 TO LBL 40.

Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

HORIZONTAL STAB BOX UPPER STRINGER 4 AT LBL 41 HAS EVIDENCE OF CORROSION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

EVIDENCE OF CORROSION ON AFT CARGO FLOORBEAM STA 1175 LBL 40.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

TORQUE BOX WEB HAS EVIDENCE OF CORROSION AT STA 1347 - 1351 RBL 33 - RBL 36.

Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

HORIZONTAL STAB BOX UPPER STRINGER NR 5 AT LBL 41.5 HAS EVIDENCE CORROSION.

Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

HORIZONTAL STAB BOX UPPER STRINGER 9 AT LBL 38 HAS EVIDENCE OF CORROSION.

Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

HORIZONTAL STAB BOX UPPER STRINGER 10 AT RBL 40 HAS EVIDENCE OF CORROSION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,070 hrs · 24,889 cycles

CRACK DETECTED ON INNER CHORD OF FRAME AT STA 903.5 ON RT SIDE OF AIRCRAFT BELOW WL 200.

Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

HORIZONTAL STAB BOX UPPER STRINGER 6 AT LBL 41.5 HAS EVIDENCE CORROSION.

Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

HORIZONTAL STAB BOX UPPER STRINGER 11 AT LBL 41 HAS EVIDENCE OF CORROSION.

Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

HORIZONTAL STAB BOX UPPER STRINGER 8 AT LBL 41 HAS EVIDENCE OF CORROSION.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

AFT CARGO FLOOR FRAME INTERCOSTAL AT STA 1405 LBL 19 HAS EVIDENCE OF CORROSION.

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

TORQUE BOX WEB AT STA 1334 LBL 40 HAS EVIDENCE OF CORROSION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

AFT CARGO FLOOR FRAME CAP AT STA 1395 HAS AREAS WITH EVIDENCE OF CORROSION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

AFT CARGO FLOOR FRAME CAP AT STA 1373 HAS AREAS WITH EVIDENCE OF CORROSION.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,070 hrs · 24,889 cycles

AFT CARGO FLOOR INTERCOSTALS HAVE EVIDENCE OF CORROSION AT STA 1395 RBL 6 - RBL 9.

Part: SHEAR TIE — CORRODED (BS 1395) · corrosion level 2 · airframe 85,058 hrs · 24,883 cycles

SHEAR TIE HAD EVIDENCE OF CORROSION AT BS 1395, STRINGERS 35R - 36R