N761CK

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

CORROSION ON TE PANEL SUPPORT LEFT HAND WING ACCESS PANEL 552BB AFT TOP O/B SIDE APPROX WBL 261

Part: FRAME — CORRODED (BS 1280 LBL10-20) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX UPPER FRAME AT STA 1280 LBL 10-20 HAS EVIDENCE OF CORROSION

Part: PANEL — CORRODED (BS 1275 RBL2) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX UPPER PANEL HAS EVIDENCE OF CORROSION AT STA 1275 RBL 2

Part: INTERCOSTAL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1329-1351 RB 16 HAS EVIDENCE OF CORROSION

Part: INTERCOSTAL — CORRODED (1329-1351) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1329-1351 RBL 22 HAS EVIDENCE OF CORROSION

Part: SHEAR TIE — CORRODED (BS 1439 S33-34L) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

FAA FINDING, FRAME SHEAR TIE IS CORRODED AT STA 1439 BETWEEN 33L & 34L MARKED FA-1

Part: WEB — CORRODED (BS 1328 RBL 26) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION IN AFT PIT STA 1328 RBL 26 FLOOR WEB

Part: WEB — CORRODED (BS 1153-1175 BL0) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX WEB AT STA 1153-1175 BL 0 HAS EVIDENCE OF CORROSION.

Part: INTERCOSTAL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1329-1351 RBL 33 HAS EVIDENCE OF CORROSION

Part: FITTING — CORRODED (BS 1579 S38-39L) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION IN AREA AFT OF BULK PIT STA 1579 STR38-39L

Part: INTERCOSTAL — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1263-1285 RBL 33 HAS EVIDENCE OF CORROSION

Part: INTERCOSTAL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1329-1351 RBL 14 HAS EVIDENCE OF CORROSION

Part: INTERCOSTAL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1329-1351 RBL 18 HAS EVIDENCE OF CORROSION

Part: WEB — CORRODED (BS 1328 RBL 3) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION IN AFT PIT STA 1328 RBL 3 FLOOR WEB

Part: INTERCOSTAL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1329-1351 RBL 25 HAS EVIDENCE OF CORROSION

Part: PANEL — CORRODED (BS 1265-1285) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX UPPER PANEL HAS EVIDENCE OF CORROSION AT STA 1265-1285 RBL 17-33

Part: PANEL — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

UPPER TORQUE BOX PANEL AT STA 1263-1285 RBL 45 HAS EVIDENCE OF CORROSION

Part: FLOORBEAM — CORRODED (BS 1153) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

CORROSION FOUND IN AFT PIT STA 1153 LBL 46-RBL 46 FLOOR FRAME TOP FLANGE LOWER SURFACE

Part: PANEL — CORRODED (1263-1285) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

UPPER TORQUE BOX PANEL AT STA 1263-1285 LBL 45 HAS EVIDENCE OF CORROSION

Part: PANEL — CORRODED (BS 1275 LBL 33) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

REF W/O 100081853 ADDITIONAL CORROSION FOUND ON PANEL IN AFT CARGO COMPARTMENT AT STA 1275 LBL 33.15. TRANSFERRED FROM LOG BOOK 100081875

Part: INTERCOSTAL — CORRODED (BS 1265-1285) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1265-1285 RBL 17 HAS EVIDENCE OF CORROSION

Part: FLOOR SUPPORT — CORRODED (BS 1345-1351) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION IN AFT PIT STA 1345-1351 LBL 11 FLOOR STRUCTURE C-CHANNEL TOP FLANGE LOWER SURFACE

Part: INTERCOSTAL — CORRODED (BS 1265-1285) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1265-1285 RBL 25 HAS EVIDENCE OF CORROSION

Part: CHANNEL — CORRODED (BS 1445 LBL 16) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION IN AFT PIT STA 1445 LBL 16 CEILING U-CHANNEL BOTTOM FLANGE TOP SURFACE UNDER NUTPLATE

Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL HAS EVIDENCE OF CORROSION AT STA 1268 LBL 8

Part: ATTACH ANGLE — CORRODED · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX UPPER PANEL ATTACH ANGLE AT STA 1265-1285 RBL 41 HAS EVIDENCE OF CORROSION

Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1265-1285 LBL 23 HAS EVIDENCE OF CORROSION

Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL HAS EVIDENCE OF CORROSION AT STA 1268 LBL 12

Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1265-1285 RBL 15 HAS EVIDENCE OF CORROSION

Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1265-1285 LBL 25 HAD EVIDENCE OF CORROSION

Part: WEB — CORRODED · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE ON AFT CARGO DOOR WEB APPROX 33 INCHES FROM FRONT EDGE OF DOOR AT TOP EDGE

Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1265-1285 RBL 24 HAS EVIDENCE OF CORROSION

Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT TORQUE BOX INTERCOSTAL AT STA 1265-1285 LBL 17 HAS EVIDENCE OF CORROSION

Part: STRINGER — CORRODED (BS 1280 S39R) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

STR 39R AT STA 1280 HAS EVIDENCE OF CORROSION

Part: FRAME — CORRODED (BS 1131) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

CORROSION FOUND IN AFT PIT STA 1131 LBL40-46 FLOOR FRAME TOP FLANGE LOWER SURFACE

Part: FRAME — CORRODED (BS 1395) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION IN AFT PIT STA 1395 RBL45 UNDER ROLLER TRAY ON FLOOR FRAME LOWER SURFACE

Part: FRAME — CORRODED (BS 1197) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

CORROSION FOUND IN AFT PIT AT STA 1197 +88 LBL47-RBL45 ON FLOOR FRAM "J FITTING" TOP FLANGE UPPER AND LOWER SURFACES

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 94,067 hrs · 25,912 cycles

CAPTAIN`S FWD INBD SEAT TRACK HAS DAMAGE AT AFT EDGE OF TRACK

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 94,067 hrs · 25,912 cycles

FIRST OFFICER`S FWD OUTBD SEAT TRACK HAS CRACK ALONG FWD EDGE OF TRACK

Part: STIFFENER — CRACKED (BS 1480 LBL 8) · airframe 94,067 hrs · 25,912 cycles

BULK CARGO STIFFENER SATION 1480 LBL 8 IS CRACKED

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLES ON AFT CARGO DOOR FRAME  APPROX 4 INCHES FROM AFT EDGE OF DOOR AND 26 INCHES FROM TOP EDGE OF DOOR

Part: STIFFENER — CRACKED (BS 1461 LBL 8) · airframe 94,067 hrs · 25,912 cycles

STIFFENER BULK CARGO STATION 1461 LBL 8 IS CRACKED

Part: FRAME — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE ON AFT CARGO DOOR FRAME 10 INCHES FROM AFT EDGE OF DOOR AND 25 INCHES FROM BOTTOM EDGE OF DOOR

Part: FRAME — CORRODED (BS 1197) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT FRAME INNER  CHORD AT STA 1197+44 HAS EVIDENCE OF CORROSION

Part: STIFFENER — CRACKED (BS 1480 RBL 10) · airframe 94,067 hrs · 25,912 cycles

FLOOR WEB STIFFNER CRACKED AT STA 1480 RBL 10 IN AFT PIT

Part: STIFFENER — CRACKED (BS 1461 RBL 10) · airframe 94,067 hrs · 25,912 cycles

FLOOR WEB STIFFENER  CRACKED AT STA 1461 RBL10 IN AFT PIT

Part: STRINGER SPLICE — CORRODED (BS 1300-1314) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

FACTORY STRINGER SPLICE AT STA 1300-1314 STR 39R HAS EVIDENCE OF CORROSION

Part: SHEAR TIE — CORRODED (BS 1285 S38-39L) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

SHEAR TIE AT STA 1285 BETWEEN STR 38L-39L HAS EVIDENCE OF CORROSION

Part: SHEAR TIE — CORRODED (BS 1285 S39L/R) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

SHEAR TIE AT STA 1285 BETWEEN STR 39L-39R HAS EVIDENCE OF CORROSION.

Part: WEB — CORRODED (AFT CARGO) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE ON AFT CARGO DOOR WEB 3 INCHES FROM FRONT EDGE OF DOOR AT TOP EDGE OF DOOR

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE ON AFT CARGO DOOR FRAME APPROX 16 INCHES FROM AFT EDGE OF DOOR AND 26 INCHES FROM TOP EDGE OF DOOR

Part: WEB — CORRODED (AFT CARGO) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLES ON AFT CARGO DOOR WEB 29 INCHES FROM FRONT EDGE OF DOOR AND 7 INCHES FROM TOP EDGE

Part: FRAME — CORRODED (BS 1109) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

CORROSION FOUND IN AFT PIT STA 1109 LBL 42-46 UNDER ROLLER TRAY  ON FLOOR FRAME LOWER SURFACE

Part: ANGLE — CORRODED (BS 1579 S38-39R) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION IN AREA AFT OF BULK PIT STA 1579 BETWEEN STR 38-39R ON L-ANGLE

Part: LAP JOINT — CORRODED (BS 1279 LBL27) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

REF WO 100081853 CORROSION FOUND ON LAPSEAM AT STA 1279 LBL 27. TRANSFERRED FROM LOG BOOK 100081874.

Part: STRUCTURE — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE ON AFT CARGO DOOR  APPROX 16 INCHES FROM AFT EDGE AND 16 INCHES FROM TOP EDGE OF DOOR.

Part: SHEAR TIE — CORRODED (BS 1562) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION ON SHEAR TIE @ STA. 1562 BL 0

Part: TEAR STRAP — CORRODED (BS 1285 S35-38R) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

INNER TEAR STRAP AT STA 1285 BETWEEN STR 35L-38R HAS EVIDENCE OF CORROSION

Part: WEB — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE ON AFT CARGO DOOR WEB 21 INCHES FROM AFT EDGE OF DOOR AND BOTTOM EDGE.

Part: SHEAR TIE — CORRODED (BS 1285 S38-39R) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

SHEAR TIE AT STA 1285 BETWEEN STR 39R-38R HAS EVIDENCE OF CORROSION

Part: FLOORBEAM — CORRODED (BS 1197) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION FOUND IN AFT PIT STA 1197 +22 RBL 40-45 FLOOR FRAME TOP FLANGE LOWER SURFACES

Part: SHEAR TIE — CORRODED (BS 1280 S35-36L) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

SHEAR TIE AT STA 1280 BETWEEN STR 35L-36L HAS EVIDENCE OF CORROSION

Part: FLOORBEAM — CORRODED (BS 1219) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

CORROSION FOUND IN AFT PIT AT STA 1219 LBL44-RBL39 IN MULTIPLE AREAS OF FLOOR FRAME "J FITTING" TOP FLANGE UPPER AND LOWER SURFACES

Part: FAILSAFE — CORRODED (BS 1562 S39L/R) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

CORROSION ON FAIL SAFE CHORD AT DRAIN HOLE @ BS 1562 BETWEEN STRINGERS S-39L AND S-39R

Part: FLOORBEAM — CORRODED (BS 654) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION ON BOTTOM SURFACE OF CORD AT STA 654.44 JUST AFT OF PDU 11L IN FWD PIT

Part: STIFFENER — CORRODED (BS 1219) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

AFT PIT FRAME STIFFNER AT STA 1219 RBL 20 CORRODED

Part: SHEAR TIE — CORRODED (BS 1285 S36-37L) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

SHEAR TIE AT STA 1285 BETWEEN STR 36L-37L HAS EVIDENCE OF CORROSION

Part: SHEAR TIE — CORRODED (BS 1285 S37-38L) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

SHEAR TIE AT STA 1285 BETWEEN STR 37L-38L HAS EVIDENCE OF CORROSION

Part: WEB — CORRODED (BS 1334) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION IN AFT STA 1334 RBL 3 FLOOR WEB

Part: SHEAR TIE — CORRODED (BS 1241 S38-39R) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

SHEAR TIE AT STA 1241 BETWEEN STR 39R & 38R HAS EVIDENCE OF CORROSION

Part: FLOORBEAM — CORRODED (BS 654) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION ON UPPER SURFACE OF CORD IN FWD PIT AT STA 654.44 AND LBL 18

Part: SHEAR TIE — CORRODED (BS 1219 S38-39R) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

SHEAR TIE AT STA 1219 BETWEEN STR 39R & 38R HAS EVIDENCE OF CORROSION

Part: DOOR FRAME — CORRODED · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE ON AFT CARGO DOOR FRAME 4 INCHES FROM AFT EDGE OF DOOR AND 33 INCHES FROM BOTTOM EDGE OF DOOR

Part: DOOR FRAME — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE ON AFT CARGO DOOR FRAME 8 INCHES FROM AFT EDGE OF DOOR 37 FROM TOP EDGE OF DOOR

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE ON AFT CARGO DOOR  FRAME 4 INCHES FROM AFT EDGE OF DOOR AND 33 INCHES FROM BOTTOM EDGE OF DOOR

Part: WEB — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE ON AFT CARGO DOOR WEB 28 INCHES FROM AFT EDGE OF DOOR AND BOTTOM EDGE

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE  ON AFT CARGO DOOR FRAME 11 INCHES FROM BOTTOM OF DOOR AT AFT EDGE

Part: DOOR FRAME — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE ON AFT CARGO DOOR 18 INCHES FROM AFT EDGE OF DOOR AND 33 FROM BOTTOM EDGE OF DOOR

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 94,067 hrs · 25,912 cycles

EVIDENCE OF CORROSION AROUND FASTENER HOLE ON AFT CARGO DOOR WEB 3 INCHES FROM AFT EDGE OF DOOR AND BOTTOM EDGE OF DOOR

Part: STIFFENER — CRACKED (LT NACELLE) · airframe 94,067 hrs · 25,912 cycles

LEFT NACELLE STRUT AFT TORQUE BOX AREA I/B INTERIOR VERTICAL STIFFENER AFT OF ACCESS PANEL 436 AR @ APPROX NAC 254 HAS MARKED CRACK.

Part: LIGHT — INOPERATIVE (L1 DOOR AREA) · airframe 94,066 hrs · 25,912 cycles

L1 DOOR EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,066 hrs · 25,912 cycles

2EA EMERGENCY DOME LIGHTS ARE INOP.

Part: LIGHT — INOPERATIVE · airframe 93,670 hrs · 25,623 cycles

L1 DOOR SILL EMERGENCY LIGHT , L313 INOP

Part: LIGHT — INOPERATIVE · airframe 93,111 hrs · 25,427 cycles

EMERGENCY LIGHT TEST FAILED. COMES ON FOR LESS THAN A SECOND AND GOES OFF

Part: FAILSAFE — CRACKED (BS 995) · airframe 92,596 hrs · 25,187 cycles

CRACK INDICATION NOTED ON R/H BS 955 FAIL SAFE STRAP DURING UT INSPECTION PER AD 2012-09-04 I & J AND SB 767-53A0100 R3

Part: FITTING — CORRODED (BS 955) · corrosion level 2 · airframe 92,596 hrs · 25,187 cycles

R/H UPPER KICK LOAD FITTING AT STA 955 HAS EVIDENCE OF CORROSION

Part: FAILSAFE — CORRODED (BS 955) · corrosion level 2 · airframe 92,596 hrs · 25,187 cycles

FAIL SAFE STRAP HAS EVIDENCE OF CORROSION AT STA 955 UNDER UPPER KICK LOAD FITTING R/H SIDE

Part: SEAT TRACK — CRACKED (COCKPIT LT) · airframe 92,596 hrs · 25,187 cycles

FIRST OFFICER'S FWD INBOARD SEAT TRACK IS CRACKED

Part: SEAT TRACK — BROKEN (COCKPIT RT) · airframe 92,596 hrs · 25,187 cycles

CAPTAINS AFT INBOARD SEAT TRACK MISSING LARGE PIECE AT FWD EDGE

Part: SEAT TRACK — CRACKED (COCKPIT LT) · airframe 92,596 hrs · 25,187 cycles

FIRST OFFICER'S AFT OUTBOARD SEAT TRACK IS CRACKED

Part: HINGE FITTING — DAMAGED (RUDDER) · airframe 92,596 hrs · 25,187 cycles

RUDDER HINGE FITTING AT RUDDER STA 156.074 IS DAMAGED

Part: SKIN — CORRODED (EXTERIOR) · corrosion level 2 · airframe 92,124 hrs · 24,943 cycles

EXT SKIN CORRODED AT STA 1300 STR 38 L.

Part: SKIN — CORRODED (EXTERIOR) · corrosion level 2 · airframe 92,124 hrs · 24,943 cycles

EXT SKIN CORRODED AT STA 1412 STR 35 L.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,124 hrs · 24,943 cycles

STRINGER 35 L AT STA 1417 CORRODED.

Part: UNKNOWN — ODOR (CABIN) · airframe 90,472 hrs · 24,136 cycles

DURING CLIMB OUT AND PART OF CRUISE FLIGHT PACK OUTPUT AIR HAS JET FUEL FUMES. BURNS EYES AND NOSE. TERMINATING SERVICE B767 FIM 21-00 TASK 803, PERFORMED IDLE ENGINE RUN OF #1 AND #2 ENGINE IAW B767-300 AMM 71-00-00 TEST 4, PERFORMED OPS CHECK OF CODING PACK SYSTEM IAW B767-300 AMM 21-00-00, PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW B767-300 AMM 05-51-56, PERFORMED REMOVAL OF 0.1 CONTAMINATION FROM THE AIR CONDITIONING AND PNEUMATIC SYSTEMS IAW B767-300 AMM 21-00-21. NO DEFECTS NOTED AT THIS TIME. ALL CHECKS GOOD NO FUMES NOTICED IN FLIGHT DECK AIRCRAFT OK FOR CONTINUED SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 90,474 hrs · 24,137 cycles

ON CLIMB OUT AND PART OF CRUISE STRONG ODOR OF FUEL. REMOVED RIGHT HAND WATER EXTRACTOR; INSPECTED. NO DEFECT FOUND, REINSTALLED RIGHT HAND WATER EXTRACTOR. OPERATION AND LEAK CHECK GOOD IAW B767 AMM 21-51-04 AND 21-51-00 601 E.(1). FOUND NO ODOR IN COCKPIT.

Part: UNKNOWN — ODOR (CABIN) · airframe 90,470 hrs · 24,135 cycles

IN CRUISE FLIGHT STRONG SMELL OF JET FUEL FROM PACK AIR. INSPECTED AND PERFORMED SYSTEM TEST ON BOTH PACK SYSTEM IAW B767 AMM'S 21-00-21, 21-51-00, AND NO OIL CONTAMINATION FOUND NO DEFECT AND SYSTEM TEST GOOD AND IAW SMOKE OR FUMES IN THE CABIN AMM 05-51-56.

Part: CAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 90,314 hrs · 24,029 cycles

MCD FWD MID SPAN LATCH CAM PITTED SIGNS OF WEAR.

Part: CAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 90,314 hrs · 24,029 cycles

#11 LOWER MAIN CARGO DOOR LOWER LATCH CAM PITTED / SIGNS OF WEAR. SUPPLEMENTAL INFORMATION: UNIQUE CONTROL NUMBER NEEDS TO BE CHANGED FROM KCSA201907101162 TO KCSA201907151162.

Part: PIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 90,314 hrs · 24,029 cycles

MCD FWD MID SPAN LATCH PIN PITTED / SIGNS OF WEAR.

Part: STIFFENER — CRACKED (NR 1 NACELLE) · airframe 88,238 hrs · 22,793 cycles

CRACKED STIFFENER INSIDE THE NR 1 PYLON ON INBD SIDE, NAC STA 290.

Part: FITTING — CRACKED (NR 1 NACELLE) · airframe 88,238 hrs · 22,793 cycles

CRACKED FITTING ON THE TOP OF THE NR 1 PYLON, NAC STA 205.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 88,238 hrs · 22,793 cycles

NR 1 ENGINE. OTBD SIDE AT NAC STA 225, HAS A CRACK PAST A STOP DRILL.

Part: FITTING — CRACKED (NR 2 PYLON) · airframe 88,238 hrs · 22,793 cycles

CRACKED FITTING ON TOP OF NR 2 PYLON NAC STA 205.