N746CK

Part: FIRESHIELD — DAMAGED (NR 3 NACELLE) · airframe 118,076 hrs · 23,545 cycles

NR 3 PYLON LT FIRE SHIELD DAMAGED AT NAC STA 234.

Part: FIRESHIELD — DAMAGED (NR 1 NACELLE) · airframe 118,076 hrs · 23,545 cycles

NR 1 PYLON LT FIRE SHIELD DAMAGED AT NAC STA 182.

Part: SEAT TRACK — CORRODED (BS 480-560) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

BS 480 - 560, RBL 24 SEAT TRACK CROWN CORRODED.

Part: SEAT TRACK — CORRODED (BS 480-520) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

BS 480-520 RBL 47, SEAT TRACK CORRODED ON INBD FLANGE.

Part: SEAT TRACK — CORRODED (BS 520-540) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

BS 520 - 540, RBL 47, SEAT TRACK CORRODED.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 2050, RBL 11.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK WORN BS 780 - 800, LBL 12.

Part: SEAT TRACK — CRACKED (BS 1870) · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK CRACKED AT APPROXIMATELY BS 1870, RBL 12.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK CRACKED AT BS 980 - 1000, LBL 12.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 2150, RBL 12.

Part: STIFFENER — CRACKED (NR 2 NACELLE) · airframe 118,076 hrs · 23,545 cycles

NR 2 PYLON LT ANGLE STIFFENER CRACKED AT NAC STA 221.9 ABOVE UPPER SPAR.

Part: SEAT TRACK — CORRODED (BS 480) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK HAS EVIDENCE OF CORROSION AT APPROXIMATELY BS 480, RBL 35.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 2110, RBL 12.

Part: SEAT TRACK — CORRODED (BS 2175) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK HAS CORROSION AT APPROXIMATELY BS 2175, LBL 11.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 1670, LBL 12.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

WEB ON MAIN DECK FLOOR SUPPORT CORRODED BS 840 - 860, LBL 12.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 1810, RBL 12.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK SUPPORT CORRODED AT BS 960 - 980, LBL 12.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

SEAT TRACK ON MAIN DECK HAS CORROSION AT BS 1780 - 1800, RBL 13.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK CORRODED BS 2175, RBL 11.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

SEAT TRACK ON MAIN DECK CORRODED AT BS 800 - 820, RBL 13.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 1660 TO 1620, RBL 12.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 900 - 920, LBL 12.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 1630, LBL 12.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 118,076 hrs · 23,545 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 1465, RBL 99.

Part: STRINGER SPLICE — CRACKED (BS 2598) · airframe 1,177,706 hrs · 23,386 cycles

BS 2598 BULKHEAD AFT SIDE S11R SPLICE FITTING HAS CRACK INDICATION.

Part: FIRESHIELD — DAMAGED (NR 2 NACELLE) · airframe 117,706 hrs · 23,386 cycles

NR 2 PYLON OTBD LOWER SKIRT FIRESHIELD DAMAGED AT NAC STA 226.5.

Part: STRUCTURE — CRACKED (BS 2598) · airframe 117,706 hrs · 23,386 cycles

BS 2598, OTBD CHORD HAS A CRACK IN FASTENER HOLE AT S12R, COMMON TO LOWER FWD SPLICE FITTING.

Part: STRINGER SPLICE — CRACKED (BS 2598) · airframe 117,706 hrs · 23,386 cycles

BS 2598, BULKHEAD FWD SIDE STRINGER SPLICE 11R FITTING HAS A CRACK.

Part: SKIN — DAMAGED (NR 2 NACELLE) · airframe 117,706 hrs · 23,386 cycles

NR 2 PYLON OTBD LOWER SKIN DAMAGED AT NAC STA 226.5.

Part: LIGHT — INOPERATIVE (UPPER CABIN) · airframe 117,706 hrs · 23,386 cycles

UPPER DECK DOME LIGHT, EMERGENCY LIGHT INOPERATIVE.

Part: SKIN — DAMAGED (NR 2 NACELLE) · airframe 117,706 hrs · 23,386 cycles

NR 2 PYLON INBD SKIN LOWER SKIRT DAMAGED FROM NAC STA 214-227.

Part: LIGHT — INOPERATIVE (UPPER CABIN) · airframe 117,706 hrs · 23,386 cycles

UPPER DECK RT AFT EMERGENCY LIGHT INOPERATIVE.

Part: FIRESHIELD — DAMAGED (NR 2 NACELLE) · airframe 117,706 hrs · 23,386 cycles

NR 2 PYLON INBD INNER SURFACE, FIRE SHIELD, APPROXIMATELY NAC. STA 223 HAS DAMAGE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 116,174 hrs · 22,963 cycles

MAIN DECK RIGHT OVERWING INTERCOSTAL LOWER CHORD CRACKED AT BS 1220, RBL 116.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 166,174 hrs · 22,963 cycles

MAIN DECK LEFT OVERWING INTERCOSTAL LOWER CHORD CRACKED AT BS 1180, LBL 108.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 116,174 hrs · 22,963 cycles

MAIN DECK LEFT OVERWING INTERCOSTAL WEB CRACKED AT BS 1180, LBL 108.

Part: FIRESHIELD — DAMAGED (NR 1 PYLON) · airframe 115,633 hrs · 22,818 cycles

NR 1 PYLON RIGHT LOWER FIRESHIELD DAMAGED AT NAC STA 227.9.

Part: FIRESHIELD — DAMAGED (NR 3 PYLON) · airframe 114,481 hrs · 22,495 cycles

NR 3 PYLON FIREWALL SHIELD DAMAGED BETWEEN NAC STA 205 TO 215 LT SIDE.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 113,469 hrs · 22,201 cycles

OVERWING LONGERON SPLICE FITTING (LEFT SIDE OF A/C) AT STA 1372, HAS CORROSION IN THE AFT, LWR HOLE OF THE VERTICLE FLANGE OF THE SPLICE FITTING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 113,469 hrs · 22,201 cycles

UPPER DECK EMERGENCY LIGHT IN CEILING BY ESCAPE DOOR INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 113,469 hrs · 22,201 cycles

UPPER DECK EMERGENCY LIGHT IN CEILING BY ESCAPE DOOR.

Part: LIGHT — INOPERATIVE (UPPER DECK) · airframe 113,469 hrs · 22,201 cycles

UPPER DECK ESCAPE DOOR EMERGENCY SLIDE LIGHT INOP.

Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 2 PYLON STRUT CHORD HAS CRACK INDICATION IN AFT I/B LEFT HOLE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 113,469 hrs · 22,201 cycles

FUSELAGE FITTING AT BS 2485, STR 23L CRACKED IN O/B FLANGE.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 113,469 hrs · 22,201 cycles

CORROSION BLEND OUT AT STA 2484 STR 24L OUT OF LIMITS.

Part: STRAP — CORRODED (FUSELAGE) · airframe 113,469 hrs · 22,201 cycles

CORROSION BLENDOUT AT STATION 2485 STR 23L OUT OF LIMITS.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 113,469 hrs · 22,201 cycles

CORROSION BLEND OUT AT STA 2460 STR 24L TO 25L OUT OF LIMITS.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,469 hrs · 22,201 cycles

CORROSION BLEND OUT AT STA 2412 STR 23L OUT OF LIMITS.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,469 hrs · 22,201 cycles

CORROSION ON FUSELAGE SKIN AT BS 982 TO 988 BETWEEN STR 3L AND 4L.

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 113,469 hrs · 22,201 cycles

LEFT WING LEADING EDGE UPPER SUPPORT ON BULLNOSE CORRODED FROM FSSI 562 TO 620.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 113,469 hrs · 22,201 cycles

UPPER DECK FLOORBEAM WEB AT STA 400 LBL 58 IS CRACKED.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,469 hrs · 22,201 cycles

OVERWING LONGERON ATTACH AT FUSELAGE SKIN CORRODED AT STA 1362, STRINGER 32L, WL 152.

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 2 PYLON LT FRAME CRACKED (DAMAGED) AT TOP UPPER END NAC STA 190.

Part: STRAP — CRACKED (NR 4 PYLON) · airframe 73,616 hrs · 9,463 cycles

NR 4 PYLON AT NAC STA 221, BULKHEAD STRAP HAS A .8 INCH CRACK.

Part: STRUCTURE — CHAFED (NR 4 NACELLE) · airframe 113,469 hrs · 22,201 cycles

NR 4 PYLON, PNEUMATIC DUCT - TO ENGINE CONNECTION - ANTI ROTATION STRAP CHAFING STRUCTURE INBOARD NACELLE STA 200 APPROX.

Part: STRUCTURE — CHAFED (NR 1 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 1 PYLON, PNEUMATIC DUCT - TO ENGINE CONNECTION - ANTI ROTATION STRAPS CHAFING STRUCTURE - BOTH SIDES- NAC STA 200 APPROX.

Part: STRUCTURE — CHAFED (NR 2 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 2 PYLON, PNEUMATIC DUCT- TO ENGINE CONNECTION - ANTI ROTATION CHAFING STRUCTURE - BOTH SIDES - NAC STA 200 APPROX.

Part: STRUCTURE — CHAFED (NR 3 NACELLE) · airframe 113,469 hrs · 22,201 cycles

NR 3 PYLON, PNEUMATIC DUCT - TO ENGINE CONNECTION - ANTI ROTATION STRAPS CHAFING STRUCTURE - BOTH SIDES, NAC STA 200 APPROX.

Part: SKIN — CRACKED (NR 3 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 3 PYLON UPPER SKIN HAS A CRACK AT NAC STA 221 - .5 INCH.

Part: STRAP — CRACKED (NR 2 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 2 PYLON NAC STA 221 BULKHEAD STRAP CRACKED AT TOP CENTER AFT LT HOLE .125 INCH LONG.

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 2 PYLON NAC STA 221 LT UPPER FRAME HAS A .75 INCH CRACK.

Part: STRAP — CRACKED (NR 3 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 3 PYLON NAC STA 221 RBL ONE, BULKHEAD STRAP HAS A 1.0 INCH CRACK.

Part: FRAME — CRACKED (NR 3 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 3 PYLON NAC STA 221 RT UPPER AFT FRAME HAS A 1.0 INCH CRACK.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 1 PYLON UPPER SKIN HAS A .5 INCH CRACK AT NAC STA 222.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 2 PYLON UPPER SKIN HAS A .5 INCH CRACK AT NAC STA 221.

Part: SKIN — CRACKED (NR 4 PLYON) · airframe 113,469 hrs · 22,201 cycles

NR 4 PYLON UPPER SKIN HAS 3 EA CRACK INDICATIONS BETWEEN NAC STA 213 AND NAC STA 216.

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 2 PYLON NAC STA 221 BULKHEAD LT UPPER FWD FRAME CRACKED .5 INCH.

Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 2 PYLON STRUT CHORD CRACKED, NAC STA 221.9. HFEC INDICATED CRACK IN AFT LT I/B HOLE.

Part: FRAME — CRACKED (NR 4 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 4 PYLON LT FWD FRAME CHORD AT NAC STA 221 HAS 3 EA CRACK INDICATIONS AT UPPER END.

Part: FRAME — CRACKED (NR 3 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 3 PYLON NAC STA 221 BULKHEAD LT UPPER FWD FRAME CRACKED .5 INCH.

Part: FRAME — CRACKED (NR 3 PLYON) · airframe 113,469 hrs · 22,201 cycles

NR 3 PYLON NAC STA 221 BULKHEAD RT UPPER FWD FRAME CRACKED .5 INCH.

Part: FRAME — CRACKED (NR 4 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 4 PYLON RT FWD FRAME CHORD AT NAC STA 221 HAS 2 EA CRACK INDICATIONS AT UPPER END.

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 2 PYLON NAC STA 221 BULKHEAD RT UPPER FWD FRAME CRACKED .5 INCH.

Part: FRAME — CRACKED (NR 1 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 1 PYLON NAC STA 221 BULKHEAD RT UPPER FWD FRAME CRACKED .5 INCH

Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 2 PYLON STRUT CHORD CRACKED, NAC STA 221.9, AFT LT I/B HOLE - CRACK INDICATED HFEC.

Part: FRAME — CRACKED (NR 1 PYLON) · airframe 113,469 hrs · 22,201 cycles

NR 1 PYLON NAC STA 221 BULKHEAD LT UPPER FWD FRAME CRACKED .5 INCH.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 111,283 hrs · 21,747 cycles

FUSELAGE FRAME DAMAGED AT BS 1860, STR 13R.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 111,283 hrs · 21,747 cycles

FUSELAGE FRAME DAMAGED AT BS 1760, STR 12R.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 109,430 hrs · 21,389 cycles

UPPER DECK EXTERNAL MOUNTED SLIDE LIGHT IS INOP.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 108,516 hrs · 21,150 cycles

BS 880 MAIN DECK TENSION TIE FWD CHANNEL CRACKED LBL 75 APPROX STR 9L.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 108,516 hrs · 21,150 cycles

EXTERNAL FUSELAGE SKIN CORRODED AT BS 1238 BETWEEN STR 1R AND STR 3R.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 108,516 hrs · 21,150 cycles

STR 16L SPLICE ANGLE IS CRACKED AT BS 1358.

Part: SKIN — CORRODED (CENTER WING) · corrosion level 2 · airframe 108,516 hrs · 22,989 cycles

CENTER WING UPPER SKIN CORRODED AT BS 1140 RBL 37.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 108,516 hrs · 21,150 cycles

STR 22L CRACKED AT BS 1133.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 108,516 hrs · 21,150 cycles

STABILIZATION STRAP DAMAGED AT BS 1733 LBL 75.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 108,516 hrs · 21,150 cycles

STABILIZATION STRAP DAMAGED AT BS 1650 LBL 75.

Part: FRAME — CRACKED (NR 4 PYLON) · airframe 108,516 hrs · 21,150 cycles

NR 4 PYLON REAR ENG MOUNT BULKHEAD I/B FWD FRAME LOWER FASTENER HOLE CRACKED.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 108,516 hrs · 21,150 cycles

MAIN DECK SLOPING SHEAR WEB CRACKED AT BS 820 BETWEEN STR-10R AND STR-10AR.

Part: STRINGER — CRACKED (NR 2 PYLON) · airframe 108,516 hrs · 21,150 cycles

NR 2 PYLON O/B STRINGER CRACKED AT FWD ENG MOUNT BULKHEAD CHORD INTERNAL ANGLE ATTACH POINT, LOWER SIDE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 108,516 hrs · 21,150 cycles

FUSELAGE SKIN CORRODED ON INTERIOR SURFACE AT BS 1243 BETWEEN STR-8R AND STR-9R.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 108,516 hrs · 21,150 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 1027, LBL-11.

Part: STRUCTURE — CRACKED (L5 DOOR) · airframe 108,516 hrs · 21,150 cycles

L-5 DOOR INTERNAL FWD LOWER CORNER HORIZONTAL CHORD CRACKED.