N748CK

Part: FIRESHIELD — DAMAGED (NR 1 PYLON) · airframe 114,184 hrs · 25,720 cycles

NR 1 PYLON I/B SKIN FIRESHIELD DAMAGED BETWEEN NAC STA 180 AND 219.5

Part: SEAT TRACK — CORRODED (BS 2240-2260) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

CORROSION ON SEAT TRACK FRAME AT BS 2240-2260 RBL 34.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 113,005 hrs · 25,456 cycles

STA 460 LEFT EMERGENCY LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 113,005 hrs · 25,456 cycles

BS 420 RIGHT EMERGENCY LIGHT INOPERATIVE.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

LEFT WING T/E WBL 158 UPPER SURFACE WHERE T/E PANEL MEETS SPAR HAS POPPED RIVETS AND EVIDENCE OF CORROSION.

Part: STRINGER — CORRODED (BS 996 S44L) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

S-44L CORRODED AT APPROX BS 996.

Part: FRAME — CRACKED (BS 400) · airframe 113,005 hrs · 25,456 cycles

BS 400 4" I/B OF S44L ONE HOLE HAS CRACK INDICATION.

Part: FRAME — CRACKED (BS 400) · airframe 113,005 hrs · 25,456 cycles

STA 400 4" I/B OF STR 44L ONE HOLE HAS CRACK INDICATION.

Part: FRAME — CRACKED (BS 2280) · airframe 113,005 hrs · 25,456 cycles

BS 2280 FUSELAGE FRAME WEB CRACKED 1" AT BOTTOM LT CORNER OF CUTOUT LBL-8.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

RT WING GEAR WHEEL WELL AT BS 1335 FOUND CORROSION ON FRAME 6" UP FROM OVERWING LONGERON.

Part: WEB — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

STA 320 - 340, FLOOR WEB IS CRACKED AT STR 25L AT SKIN HOLES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

MAIN DECK STA 1000 TO STA 1100, RBL 10 CORROSION ON SEAT TRACK AROUND NUT PLATES.

Part: WEB — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

FLOOR WEB BETWEEN STA 320 & 360 AT STR 25L IS CRACKED.

Part: WEB — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

FLOOR TO SKIN WEB CRACKED BS 340 - 360 RIGHT SIDE MAIN CARGO DECK.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

CRACK INDICATION AT BS 440 UPPER DECK FLOORBEAM UPPER CHORD WEB AT APPROX RBL 44.

Part: WEB — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

STA 320 - 340, FLOOR WEB AT STR 25R IS CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

MAIN DECK SEAT TRACK FLAKING AT STA 1260 LBL 99.

Part: WEB — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

FLOOR TO SKIN WEB CRACKED BS 380 RIGHT SIDE MAIN CARGO DECK.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

WING GEAR BEAM STA 1350 BL 0 CORROSION ON ATTACH BRACKET.

Part: WEB — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

STA 360 - 380, FLOOR WEB IS CRACKED AT STR 25L AT SKIN HOLES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

SEAT TRACK AT LBL 11.99 IS CORRODED AT STA 2280.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 113,005 hrs · 25,456 cycles

TWO INCH CRACK AT FWD END OF STIFFENER ANGLE INSIDE AFT CARGO DOOR BS 1820, S-38R.

Part: FRAME — CRACKED (FUSELAGE) · airframe 113,000 hrs · 25,455 cycles

FUSELAGE FRAME CRACKED AT BS 2231, STR 24L IN THE AFT LOWER HOLE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

CRACK INDICATION IN THE UPPER BOLT HOLE OF THE LT SUPPORT FRAME OUTER FITTING AT STA 2598 AND S-11L.

Part: FITTING — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

CRACK INDICATIONS IN THE LOWER BOLT HOLE OF THE LT SUPPORT FRAME OUTER FITTING AT STA 2598 AND S-11L.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

BS 380 UPPER DECK FLOORBEAM WEB CRACKED AT 2 FASTENER HOLES AT APPROX LBL 77.

Part: STIFFENER — CRACKED (BS 400) · airframe 113,005 hrs · 25,456 cycles

BS 400 UPPER DECK FLOORBEAM AT LBL 8 WEB STIFFENER IS CRACKED.

Part: STIFFENER — CRACKED (BS 400) · airframe 113,005 hrs · 25,456 cycles

BS 400 UPPER DECK FLOORBEAM AT LBL 16 WEB STIFFENER IS CRACKED.

Part: FRAME — DAMAGED (NR 2 PYLON) · airframe 113,005 hrs · 25,456 cycles

NR 2 PYLON NAC STA 221, RT AFT FRAME DAMAGED NEAR TOP RBL 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

MAIN DECK STA 780 AND 800 RBL 99 SEAT TRACK IS CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

MAIN DECK SEAT TRACK CORRODED BS 480 LBL 85.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

POSSIBLE CORROSION ON SEAT TRACK BS 520, LBL 93.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

POSSIBLE CORROSION ON FLOORBEAM BS 480, LBL 86.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

MAIN DECK STA 1000, LBL 11 TO RBL 11, CORROSION AROUND NUT PLATES.

Part: STRINGER FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

STRINGER 44L END FITTING CORRODED AT BS 1000.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

MAIN DECK STA 960, RBL 99 SEAT TRACK CORRODED.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 113,005 hrs · 25,456 cycles

SKIN CRACKED IN AREA OF CAP SKIN DOUBLER NR 2 PYLON.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

MAIN DECK STA 1900, RBL 99, SEAT TRACK CRACKED BOTTOM SIDE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 113,005 hrs · 25,456 cycles

MAIN DECK STA 660, 680, 700, RBL 99 SEAT TRACK IS CORRODED.

Part: WEB — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

CRACKED HOLE ON UPPER WEB CHORD AT BL 0 STA 340-360 ON FLIGHT DECK.

Part: FRAME — CRACKED (FUSELAGE) · airframe 113,005 hrs · 25,456 cycles

BS 2701.5 WL 315 LBL 36 FRAME IS CRACKED AT STIFFENER HOLES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 113,000 hrs · 25,455 cycles

UPPER DECK STA 580 CEILING EMERGENCY LIGHT IS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 113,000 hrs · 25,455 cycles

L1 SILL FORWARD LIGHT IS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 113,000 hrs · 25,455 cycles

MAIN DECK EMERGENCY LIGHT (M417) IS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 113,000 hrs · 25,455 cycles

UPPER DECK SLIDE LIGHT IS INOP.

Part: DRAIN LINE — LOOSE (NR 2 PYLON) · airframe 112,544 hrs · 25,306 cycles

NR 2 PYLON CASE DRAIN LINE LOOSE AND CHAFING BULKHEAD AT NAC STA 222.

Part: FIRESHIELD — CHAFED (PYLON) · airframe 112,544 hrs · 25,306 cycles

NR 32 PYLON I/B FIRESHIELD CHAFED AT STA 220 / RT SIDE OF PYLON AFT SECTION OF FIRESHIELD.

Part: SKIN — DAMAGED (NR 2 PYLON) · airframe 112,544 hrs · 25,306 cycles

NR 2 PYLON I/B LOWER SKIN DAMAGED AT NAC STA 229.

Part: FIRESHIELD — DAMAGED (NR 2 PYLON) · airframe 112,544 hrs · 25,306 cycles

NR 2 PYLON I/B LOWER FIRESHIELD DAMAGED AT NAC STA 229.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 111,369 hrs · 24,846 cycles

UPPER DECK SLIDE LIGHT INOPERATIVE, BS 590.

Part: DOUBLER — CRACKED (ZONE 400) · airframe 111,369 hrs · 24,846 cycles

NR 2 PYLON I/B SKIN EXISTING DOUBLER CRACKED AT NAC STA 222.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 110,476 hrs · 24,625 cycles

CRACK FOUND ON STRUCTURE NEAR LT WING FIXED TRAILING EDGE RIB ATTACH FITTING AT WBL 432.

Part: BULKHEAD — CHAFED (NR 3 PYLON) · airframe 110,476 hrs · 24,625 cycles

NR 3 PYLON HYDRAULIC PRESSURE LINE AT NAC STA 221.9 BULKHEAD IS CHAFED INTO BULKHEAD.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 108,183 hrs · 24,204 cycles

DURING CRUISE MAIN DECK CARGO SMOKE DET ZONE 3 LIGHT ILLUM. RELAMP NR 3 SMOKE DETECTOR "B" SYS AS PER B747 MM 26-14-02. ACCOMPLISHED WITH MAIN CARGO COMPARTMENT SMOKE DETECTOR SYS TEST IAW B747 MM 26-14-00. TEST OK, NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 107,956 hrs · 24,162 cycles

RT EXTERIOR UPPER DECK ESCAPE SLIDE LIGHT INOP.

Part: WEB — CORRODED (L5 DOOR) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

L-5 DOOR UPPER HINGE BOX LOWER WEB CORRODED UNDER LEVELING COMPOUND AT BS 2244.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

STR 51R END FITTING CORRODED AT BS 2598.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

BS 2618 FROM STR 49L TO STR 50R FRAME CORRODED ON INNER CHORD.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

CORROSION ON STR 11L AT BS 2657.

Part: SKIN — WORN (NR 2 PYLON) · airframe 107,956 hrs · 21,744 cycles

NR 2 PYLON O/B SKIN LOWER EDGE WORN BETWEEN NAC STA 210 AND 217.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

STRINGER 51L AT BS 2598 TO 2610 IS CORRODED.

Part: FRAME — BENT (ZONE 200) · airframe 107,956 hrs · 24,162 cycles

STA 1120 FUSELAGE FRAME OUTER FLANGE IS BENT BETWEEN STR 3R AND 4R.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

RT WING LOWER SKIN SPLICE FWD OF FRONT SPAR CORRODED A WS 1500.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 107,956 hrs · 24,162 cycles

STR 9L UPPER FLANGE CRACKED BETWEEN BS 2020 AND 2040.

Part: FRAME — BENT (FUSELAGE) · airframe 107,956 hrs · 24,162 cycles

BS 1700 FUSELAGE FRAME OUTER FLANGE BENT BETWEEN STR 7R AND STR 8R.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

LT WING LANDING GEAR WHEEL WELL FWD CANTED PRESSURE DECK UPPER CHORD CORRODED AT BS 1265 BETWEEN LBL 70 AND LT O/B END.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 107 hrs · 24,162 cycles

FLOORBEAM SUPPORT UPPER ATTACH ANGLE CORRODED AT BS 2200 RBL 33.

Part: STOP FITTING — CRACKED (L1 DOOR) · airframe 107,956 hrs · 24,162 cycles

L-1 DOOR AFT UPPER CORNER STOP FITTING CRACKED 3 INCHES AT BS 480.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

AFT SIDE OF FLOORBEAM WEB CORRODED AT STA 2200 AT RBL 15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

AFT SIDE OF FLOORBEAM WEB CORRODED AT STA 2200 RBL 25 TO RBL 32.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

CORROSION ON SKIN AT STA 2460 BETWEEN STR 23L AND STR 24L.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

AFT SIDE OF FLOORBEAM WEB CORRODED, STA 2200, RBL 15.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

FLOOR WEB SUPPORT ATTACH FITTING HAS CORROSION AT FLOORBEAM STA 400 RBL 66.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 107,956 hrs · 24,162 cycles

FLOOR WEB SUPPORT ATTACH FITTING HAS CORROSION AT FLOORBEAM AT STA 420 RBL 66.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 107,956 hrs · 24,162 cycles

MAIN DECK SEAT TRACK AT STA 846 LBL-11 HAS CRACKED FLANGE .250 INCH.

Part: WIRE — BROKEN (CABIN) · airframe 107,700 hrs · 24,111 cycles

DURING T/S EMERGENCY LIGHT TEST WHEN EMERGENCY LIGHTS ARMED AFT 2 EMERGENCY LIGHTS UPPER DECK STAY ON. REPAIRED BROKEN WIRE 1938-L4726 IAW SWPM 20-10-13. LIGHTS OP CHECK NORMAL IAW AMM 33-51-00.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 107,633 hrs · 24,101 cycles

EPRL COMPUTER BUTTONS OVERHEATED AND SMELLED LIKE BURNT PLASTIC. R&R TAT / EPRL CONTROL PANEL. OPS CKS NORMAL REF MM 34-15-00.

Part: BULKHEAD — CHAFED (NR 4 PYLON) · airframe 107,579 hrs · 24,090 cycles

NR 4 PYLON NAC STA 221.9 BULKHEAD WEB CHAFED AT HYD RETURN LINE.

Part: STIFFENER — CRACKED (NR 3 PYLON) · airframe 107,579 hrs · 24,090 cycles

NR 3 PYLON HAS CRACKED OTBD STIFFENER AT APPROX NAC STA 132.00, JUST AFT OF THE FWD ENGINE MOUNT BULKHEAD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 107,132 hrs · 24,010 cycles

UPPER DECK EMERGENCY EXIT SIGN IS INOPERATIVE.

Part: SEAT TRACK — CRACKED (BS 1910)

AFT PIT SEAT TRACK CRACKED AT BS 1910, RBL 46. (K)

Part: FRAME — CRACKED (BS 2231 S21-22L)

MAIN DECK L5 DOOR REVEAL IS CRACKED (2") AT STA 2231 BETWEEN STR 21L AND 22L. (K)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 107,132 hrs · 24,010 cycles

UPPER DECK EMERGENCY LIGHT INOPERATIVE ABOVE STAIRS. WILL NOT GO OUT. (K)

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 107,118 hrs · 24,006 cycles

EMERGENCY EXIT LIGHT ABOVE F/O'S SEAT INOP.