N706CK

Part: FRAME — CRACKED (ZONE 100) · airframe 87,161 hrs · 15,090 cycles

STA 2231 AT L5 DOOR STRG 17L FRAME STRAP AND AFT INNER CHORD CRACKED

Part: STRUCTURE — CRACKED (ZONE 300) · airframe 87,161 hrs · 15,090 cycles

WHILE WORKING AD 2016-25-05 G2/SB 747-55A2050, FOUND 2EA HOLE CRACKED AT HORIZONTAL STAB CENTER SECTION I/B OF LBL 43.5

Part: RUB STRIP — DAMAGED (ZONE 200) · airframe 87,161 hrs · 15,090 cycles

FLIGHT DECK CREW ESCAPE HATCH GUIDE/RUB STRIP AFT SIDE IS MISSING A FASTENER, STICKER 20-01. FLIGHT DECK CREW ESCAPE HATCH GUIDE/RUB STRIP FORWARD AND AFT SIDES, THEY HAVE BECOME DISBONDED FROM THE LINER. FLIGHT DECK CREW ESCAPE HATCH EXTERIOR HANDLE DRAIN HOLES SEEM TO BE BLOCKED WITH GREASY DIRT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 79,975 hrs · 13,909 cycles

CONTACT DAMAGE TO LEFT HAND SIDE OF UPPER RUDDER. REPAIRED DAMAGE TO LEFT HAND SIDE OF UPPER RUDDER IAW B747-400 SRM 51-70-07 AND KALITTA AIR EA #9097 REVISION OR.

Part: LIGHT — INOPERATIVE (UNKNOWN) · airframe 79,235 hrs · 13,792 cycles

EMERGENCY LIGHTS WILL NOT EXTINGUISH.

Part: ESCAPE REEL — PARTIAL DEPLOY (UNKNOWN) · airframe 79,235 hrs · 13,792 cycles

FLIGHT COMPARTMENT EMERGENCY DECENT DEVICE #1 POSITION P/N 379103D-23 S/N 19972 EVIDENCE OF DEPLOYMENT

Part: STAND OFF — CRACKED (UNKNOWN) · airframe 79,235 hrs · 13,792 cycles

FOUND CRACK ON SHEAR TIE STAND OFF AT RBL 33.99 AND STA 1000

Part: FLOOR SUPPORT — DAMAGED (UNKNOWN) · airframe 79,235 hrs · 13,792 cycles

FLOOR- SUPPORT HOLES (2) FOR NUTCLIPS DAMAGE, AT STA 1120-1140 RBL 110

Part: STAND OFF — CRACKED (UNKNOWN) · airframe 79,235 hrs · 13,792 cycles

FOUND CRACK ON SHEAR TIE STAND OFF AT LBL 33.99 AND STA 1000

Part: FITTING — CRACKED (UNKNOWN) · airframe 79,235 hrs · 13,792 cycles

FOUND INTERCOSTAL LUG FITTING CRACKED AT LBL 11.33 AND STA 1000

Part: SEAT TRACK — CORRODED (UNKNOWN) · corrosion level 2 · airframe 79,235 hrs · 13,792 cycles

EVIDENCE OF CORROSION ON SEAT TRACK AT STA. 1000 LBL 33

Part: STAND OFF — CRACKED (UNKNOWN) · airframe 79,235 hrs · 13,792 cycles

FOUND CRACK AT SHEAR TIE STAND OFF AT RBL 57.50 AND STA 1000

Part: CHARGER — INOPERATIVE (UNKNOWN) · airframe 79,235 hrs · 13,792 cycles

EMERGENCY BATTERY CHARGER M5169 AT STA 590 R/H INOP

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,755 hrs · 10,089 cycles

L5 MAIN DECK DOOR FWD SURROUND SKIN STRUCTURE BETWEEN STR 22 AND 21 HAS POSSIBLE CRACK.

Part: SEAT TRACK — DAMAGED (BS 1910) · airframe 57,755 hrs · 10,089 cycles

SEAT TRACK DAMAGED BS 1910, RBL 40.

Part: SEAT TRACK — CORRODED (BS 1040-1060) · corrosion level 2 · airframe 57,755 hrs · 10,089 cycles

EVIDENCE OF CORROSION ON MAIN DECK SEAT TRACK BS 1040 TO 1060, LBL 100.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 80,656 hrs · 19,976 cycles

TENSION TIE AT BS 800 STR 11L AT LBL 80 HAS CRACK 1 INCH.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 80,656 hrs · 19,976 cycles

TENSION TIE AT BS 800 STR 11R AT RBL 80, 1.5 INCH.

Part: LIGHT — WEAK (CABIN) · airframe 79,868 hrs · 19,825 cycles

EMERGENCY LIGHT ABOVE UPPER DECK STAIRS IS DIM AND SLOW TO COME ON.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,378 hrs · 19,731 cycles

UPPER DECK EMERGENCY CLOSET LIGHT IS INOP.

Part: SIGN — INOPERATIVE (CABIN) · airframe 78,953 hrs · 19,644 cycles

UPPER DECK RT EMERGENCY EXIT SIGN INOP.

Part: CARGO — FUMES (CARGO BAY) · airframe 78,193 hrs · 19,465 cycles

FUMES COMING FROM NR 1 CARGO PALLET AND OR LOWER FWD CARGO AREA. SUSPECT CARGO FLUID LEAK. AFTER IDENTIFICATION OF ALL AFFECTED CARGO WITH THE USE OF THE PROPER MSDS SHEET, IT WAS DETERMINED THAT A GASEOUS LEAK HAD OCCURRED. ALL AFFECTED CARGO HAS BEEN INSPECTED AND REMOVED FROM THE AIRCRAFT. AIRCRAFT HAS BEEN THOROUGHLY VENTED AND ALL PALLET POSITIONS WERE INSPECTED WITH NO LIQUID SPILLS FOUND, AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (NR 3 PYLON) · airframe 78,065 hrs · 19,416 cycles

NR 3 PYLON INTERIOR HAS A 2 INCH CRACK ON 252 BULKHEAD FRAME LOWER O/B SECTION 2 INCHES ABOVE LOWER HORIZONTAL WEB.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,201 hrs · 19,248 cycles

STA 330 FLOORBEAM WEB CRACKED 3.5 INCHES AT LBL 63.

Part: PLATE — CORRODED (TE FLAP) · corrosion level 2 · airframe 77,201 hrs · 19,248 cycles

LT TRAILING EDGE INBOARD MID-FLAP HAS CORROSION ON TIE PLATE AT WBL 235.20.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,030 hrs · 17,637 cycles

LT SLIDE LIGHT HAS ONE LAMP INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,030 hrs · 17,637 cycles

EMERGENCY LIGHT AT STA 460 ABOVE STAIRS IN UPPER DECK INOP.

Part: SEAT TRACK — CRACKED (BS 320) · airframe 77,201 hrs · 19,248 cycles

F/O`S FWD O/B SEAT TRACK CRACKED.

Part: FRAME — CRACKED (BS 880) · airframe 77,201 hrs · 19,248 cycles

BS 880 FUSELAGE FRAME CRACKED BETWEEN STR 39R AND STR 40R.

Part: SEAT TRACK — CORRODED (BS 1035) · corrosion level 2 · airframe 77,201 hrs · 19,248 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 1035, RBL 98.58.

Part: FRAME — CRACKED (BS 960) · airframe 77,201 hrs · 19,248 cycles

BS 960 FUSELAGE FRAME CRACKED AT STR 39L

Part: SEAT TRACK — CRACKED (BS 998) · airframe 77,201 hrs · 19,248 cycles

SEAT TRACK CRACKED AT STA 998 ON MAIN DECK LBL75.

Part: DOUBLER — CORRODED (ACCESS PANEL) · airframe 77,201 hrs · 19,248 cycles

C2 DOOR ACCESS PANEL HAS CORROSION ON DOUBLER.

Part: STRAP — CRACKED (BS 300) · airframe 77,201 hrs · 19,248 cycles

NLG SIDEWALL SKIN STRAP CRACKED AT BS 300, LBL33

Part: SPAR — CHAFED (NR 1 PYLON) · airframe 21,827 hrs · 77,201 cycles

NR 1 PYLON MID SPAR WEB STIFFENER HAS CHAFF DAMAGE AT NAC. STA-210 R/H TOP.

Part: SUPPORT BEAM — CORRODED (RT WING SPOILER) · corrosion level 2 · airframe 77,201 hrs · 19,248 cycles

RT WING SPOILER SUPPORT BEAM UPPER CHORD CORRODED AT APPROX W.S. 528.

Part: STIFFENER — DAMAGED (NR 3 NACELLE) · airframe 21,827 hrs · 77,201 cycles

NR 3 PYLON NAC STA 248 AFT, LOWER, I/B SIDE VERTICAL STIFFENER DAMAGED.

Part: FITTING — CRACKED (L1 DOOR) · airframe 77,201 hrs · 19,248 cycles

L1 MAIN ENTRY DOOR AFT TOP CORNER FITTING CRACKED.

Part: DOOR FRAME — CRACKED (BS 442-450) · airframe 77,201 hrs · 19,248 cycles

L1 MAIN ENTRY DOOR LOWER FRAME CRACKED AT FWD EDGE BS 442 TO 450.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 77,201 hrs · 19,248 cycles

AFT CARGO DOOR SKIN INNER DOUBLER CORRODED AT AFT LOWER CORNER BS 1915.

Part: SKIN — DENTED (BS 2612 S51R)

DENT IN SKIN AT STA-2612 AT STR-51R. (K)

Part: SKIN — DENTED (BS 2595 S46R)

DENT IN SKIN AT STA-2595 AT STR-46R. (K)

Part: SKIN — DENTED (BS 2610)

DENT IN SKIN AT STA-2610 BETWEEN STR-42R AND STR-46R. (K)

Part: SEAT TRACK — WORN (BS 320)

CAPTAINS INBD SEAT TRACK WORN LBL-36, STA-320. (K)

Part: BEAM — CRACKED (L5 DOOR)

L-5 DOOR FORWARD LOWER CORNER HORIZONTAL BEAM CRACKED .5 INCH. (K)

Part: SKIN — DENTED (BS 2412)

DENT IN SKIN AT STA-2412 INBD OF JACK PAD AT RBL-65R. (K)

Part: DOOR FRAME — CRACKED (FUSELAGE)

L-5 DOOR FORWARD LOWER CORNER VERTICAL FRAME CRACKED .5 INCHES. (K)

Part: SEAT TRACK — WORN (FUSELAGE)

CAPTAINS FORWARD INBD SEAT TRACK, WORN. (K)

Part: SEAT TRACK — CRACKED (FUSELAGE)

CAPTAINS AFT SEAT TRACK IS CRACKED .250 INCH. (K)

Part: SKIN — DENTED (BS 2715)

SKIN, BS 2715 TOP OF FUSELAGE DENTED. (K)

Part: FRAME — CRACKED (BS 210)

RT FRAME CRACKED AT STR CUT OUT STA 210 ABOUT 2 INCHES LONG. (K)

Part: FRAME — CORRODED (BS 1720) · airframe 77,201 hrs · 19,248 cycles

CORROSION ON BS 1720 FUSE FRAME REINFORCEMENT CHORD I/B OF STR-42R.

Part: FRAME — CORRODED (PYLON)

NR PYLON NAC STA 221.9 BULKHEAD RT FWD FRAME WEB CORRODED. (K)

Part: DOUBLER — CORRODED (NR 3 PYLON)

NR 3 PYLON NAC STA 221.9 BULKHEAD FWD FRAME WEB DOUBLERS CORRODED. (K)

Part: FRAME — CORRODED (NR 3 PYLON)

NR 3 PYLON NAC STA 221.9 BULKHEAD LT FWD FRAME WEB CORRODED. (K)

Part: FRAME — CRACKED (NR 3 PYLON)

NR 3 PYLON NAC STA 221.9, BULKHEAD RT AFT FRAME WEB CRACKED AT (2) SPOTS. 750 AND .250. (K)

Part: FRAME — CRACKED (NR 3 PYLON)

NR 3 PYLON NAC STA 221.9 BULKHEAD LT AFT FRAME WEB CRACKED. (K)

Part: SKIN — CORRODED (FUSELAGE)

FUSELAGE SKIN IS CORRODED AT STA 2362, BETWEEN STR 40L AND 46L. (K)

Part: FRAME — CORRODED (FUSELAGE)

AFT BILGE FUSELAGE FRAME UPPER CHORD IS CORRODED AT STA 1880, RBL 18. (K)

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 77,201 hrs · 19,248 cycles

MAIN DECK SEAT TRACK DAMAGED BETWEEN BS 1140 AND 1240, LBL 34.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,201 hrs · 19,248 cycles

MAIN DECK SEAT TRACK CORRODED BETWEEN BS 610 AND 620, RBL 46.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 77,201 hrs · 19,248 cycles

MAIN DECK SEAT TRACK DAMAGED AT BS 1200, LBL 11.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 77,201 hrs · 19,248 cycles

MAIN DECK SEAT TRACK DAMAGED BETWEEN BS 1320 AND 1340, LBL 34.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,201 hrs · 19,248 cycles

MAIN DECK FLOORBEAM UPPER CHORD CORRODED AT BS 640, LBL 103.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,201 hrs · 19,248 cycles

MAIN DECK SEAT TRACK CORRODED AT BS 670, RBL 28.

Part: SKIN — CORRODED (BS 1960-2180)

FUSELAGE SKIN HAS CORROSION AROUND FASTENER HEADS AT STA 1960 TO 2180, STR 46R. (K)

Part: SEAT TRACK — CORRODED (BS 620)

SEAT TRACK AT STA-620 AT LBL-70 CORRODED. (K)

Part: STRINGER — CORRODED (BS 990 S46L)

STRINGER 46-L CORRODED AT STA-990. (K)

Part: DRAG ANGLE — CORRODED (LT MLG TRUNNION) · airframe 77,200 hrs · 19,248 cycles

LT BODY GEAR TRUNNION SUPPORT, DRAG ANGLE CORRODED AT BS 1482, STR-42R. (K)

Part: DRAG ANGLE — CORRODED (LT MLG TRUNNION)

LT BODY GEAR TRUNNION SUPPORT, DRAG ANGLE CORRODED AT BS 1482, STR-42. (K)

Part: WEB — CRACKED (BS 264) · airframe 77,200 hrs · 19,248 cycles

STA-264 UPPER DECK FLOOR WEB CRACKED "1 INCH WL-306. (K)

Part: WEB — CRACKED (BS 264)

STA-264, UPPER DECK FLOOR WEB CRACKED 1 INCH WL-306. (K)

Part: DOOR FRAME — CRACKED (BS 281)

STA 281, RBL-50, W/L-312 CARGO DOOR FRAME CRACKED. (K)

Part: SKIN — CORRODED (CENTER FUEL TANK) · airframe 77,200 hrs · 19,248 cycles

CORROSION ON CENTER TANK UPPER SURFACE STA-1160 RBL-80.

Part: SKIN — CORRODED (CENTER FUEL TANK) · airframe 77,200 hrs · 19,248 cycles

STA-1241 LBL-1 TO LBL-14 CENTER TANK UPPER SKIN HAS CORROSION.

Part: FRAME — GOUGED (FUSELAGE) · airframe 77,200 hrs · 19,248 cycles

FRAME WEB GOUGED AT STA-220 BL-O AT WL-177.

Part: SKIN — CHAFED (FUSELAGE) · airframe 77,201 hrs · 19,248 cycles

EXTERNAL FUSELAGE SKIN IS CHAFFED AT STA 990, STR 39R.

Part: FLOORBEAM — DENTED (BS 720) · airframe 77,201 hrs · 19,248 cycles

FORWARD BILGE HAS A DENT IN FLOORBEAM WEB AT STA 720, LBL 46, WL 108. (S)

Part: SKIN — CORRODED (BS 1000 S40R) · airframe 77,200 hrs · 19,248 cycles

STA 1000 SKIN CORRODED AT STRINGER 40R. (S)

Part: STRINGER — DENTED (BS 660 S44L) · airframe 77,200 hrs · 19,248 cycles

STRINGER CLIP DENTED AT STA 660 STRINGER 44L. (S)

Part: STRINGER — DENTED (BS 695 S39L) · airframe 77,200 hrs · 19,248 cycles

STRINGER 39L DENTED AT STA 695. (S)

Part: STRINGER — DENTED (BS 700 S41L) · airframe 77,200 hrs · 19,248 cycles

STA 700 STRINGER TIE AT STRINGER 41L IS DENTED. (S)

Part: BULKHEAD — DENTED (BS 2360) · airframe 77,200 hrs · 19,248 cycles

AFT PRESSURE BULKHEAD AT STA 2360 DENTED WL340 LBL 35 AFT SIDE. (S)

Part: INTERCOSTAL — DAMAGED (BS 660-680) · airframe 77,200 hrs · 19,248 cycles

INTERCOSTAL UPPER FLANGE BENT BETWEEN BS 660 TO BS 680. (S)

Part: FLOORBEAM — GOUGED (BS 540) · airframe 77,200 hrs · 19,248 cycles

STA 540 FLOORBEAM GOUGED ON UPPER CHORD LBL 41. (S)

Part: SILL — CRACKED (BS 440) · airframe 77,200 hrs · 19,248 cycles

DOOR L-1 DOOR FRAME LOWER SILL FWD CORNER CRACK EXTENDS BEYOND STOP DRILL. (S)

Part: MOUNT — DAMAGED (NR 2 ENGINE) · airframe 77,201 hrs · 19,248 cycles

NR 2 PYLON AFT ENG MOUNT HAS 9 HOLES ELONGATED AT WL 145, LAL 1 TO RBL 9 FOR AFT ENG MOUNT BULKHEAD WEB FRAMES ATTACH AT NAC STA 221.9. (S)

Part: FRAME — CRACKED (BS 442) · airframe 77,201 hrs · 19,248 cycles

MAIN DECK L1 DOOR VERTICAL FRAME IS CRACKED (1.5 INCHES) AT FORWARD LOWER CORNER IN RADIUS AT STA 442, WL 209. (S)

Part: SKIN — DENTED (BS 182) · airframe 77,201 hrs · 19,248 cycles

FUSELAGE SKIN HAS A DENT AT STA 182 BETWEEN STR 45R & 47R. (S)

Part: STRINGER — CORRODED (BS 990 S45R) · corrosion level 2 · airframe 77,201 hrs · 19,248 cycles

FUSELAGE STRINGER IS CORRODED AT STA 990, STR 45R. (S)

Part: STRINGER — DENTED (BS 690 S38L) · airframe 77,201 hrs · 19,248 cycles

FUSELAGE STRINGER IS DENTED AT STA 690, STR 38L. (S)

Part: FRAME — CRACKED (NR 2 NACELLE) · airframe 77,201 hrs · 19,248 cycles

NR 2 PYLON REAR ENG MOUNT BULKHEAD LT FORWARD FRAME WEB IS CRACKED (.250 INCHES) AT 221.9, LBL 5, WL 148.5. (S)

Part: FRAME — CRACKED (NR 3 PYLON) · airframe 77,201 hrs · 19,248 cycles

NR 3 PYLON REAR ENG MOUNT BULKHEAD LT AFT FRAME WEB IS CRACKED (.250 INCHES & .750 INCHES) AT 221.9, LBL 6, WL 148.5. (S)

Part: FRAME — CRACKED (NR 3 NACELLE) · airframe 77,201 hrs · 19,248 cycles

NR 3 PYLON REAR ENG MOUNT BULKHEAD LT AFT FRAME WEB IS CRACKED (.250 & .250 INCHES) AT 221.9, LBL 5, WL 150. (S)

Part: FRAME — CRACKED (NR 2 NACELLE)

NR 2 PYLON REAR ENG MOUNT BULKHEAD LT AFT FRAME WEB IS CRACKED (.750 INCHES) AT 221.9, LBL 5, WL 148.5. (S)

Part: FRAME — CRACKED (BS 460 S12L) · airframe 77,200 hrs · 19,248 cycles

BS 460 3.00 INCH ABOVE S12L FRAME OUTBOARD FLANGE CRACKED IN RADIUS OF DOUBLER .375 INCH LONG AFT SIDE. CRACK MARKED. UPPER DECK. (S)

Part: ATTACH ANGLE — CRACKED (BS 440) · airframe 77,200 hrs · 19,248 cycles

BS 440 S10R LT SIDE FRAME AFT SIDE, STRINGER ATTACH ANGLE CRACKED IN RADIUS .250 INCH CRACK MARKED UPPER DECK. (S)

Part: FRAME — CRACKED (BS 440) · airframe 77,200 hrs · 19,248 cycles

BS 440 S10R FRAME OUTBOARD FLANGE CRACKED IN RADIUS .375 INCH. CRACK MARKED. UPPER DECK. (S)

Part: FRAME — CRACKED (BS 460 S12R) · airframe 77,200 hrs · 19,248 cycles

BS 460 ABOVE S12R APPROX 1 INCH, FRAME OUTBOARD FLANGE CRACKED AT FASTENER HOLE. CRACK .250 INCH LONG. MARKED UPPER DECK. (S)

Part: FRAME — CRACKED (BS 460 S12R) · airframe 77,200 hrs · 19,248 cycles

BS 460 S12R FRAME DOUBLER AFT SIDE CRACKED .500 INCH AT STRINGER CUTOUT, INBOARD UPPER CORNER. CRACK MARKED. UPPER DECK. (S)

Part: STRINGER CLIP — CRACKED (BS 440 S10R) · airframe 77,200 hrs · 19,248 cycles

BS 440 S10R LT SIDE FRAME AFT SIDE, STRINGER ATTACH ANGLE CRACKED IN RADIUS .250 INCH CRACK MARKED. UPPER DECK. (S)

Part: FRAME — DENTED (FUSELAGE) · airframe 77,200 hrs · 19,248 cycles

FWD PIT BS640 FUSELAGE FRAME DENTED AT LBL29, WL101. (S)

Part: FRAME — CRACKED (BS 460 S12L) · airframe 77,200 hrs · 19,248 cycles

BS 460 S12L FRAME DOUBLER AFT SIDE CRACKED .375 INCH AT STRINGER CUTOUT, INBOARD UPPER CORNER. CRACK MARKED. UPPER DECK. (S)

Part: FRAME — CRACKED (BS 460 S12R) · airframe 77,200 hrs · 19,248 cycles

BS 460 S12R FRAME DOUBLER AFT SIDE CRACKED .500 INCH AT STRINGER CUTOUT, INBOARD UPPER CORNER. CRACK MARKED UPPER DECK. (S)

Part: FRAME — CRACKED (BS 440) · airframe 77,200 hrs · 19,248 cycles

BS 440 S10R FRAME OUTBOARD FLANGE CRACKED IN RADIUS .375 INCH CRACK MARKED UPPER DECK. (S)

Part: FRAME — CRACKED (BS 460) · airframe 77,200 hrs · 19,248 cycles

BS 460 ABOVE S12R APPROX 1 INCH FRAME OTBD FLANGE CRACKED AT FASTENER HOLE. CRACK .250 INCH LONG. CRACK MARKED. UPPER DECK. (S)

Part: FRAME — CRACKED (BS 460 S12L) · airframe 77,200 hrs · 19,248 cycles

BS 460 3.00 INCH ABOVE S12L FRAME OUTBOARD FLANGE CRACKED IN RADIUS OF DOUBLER .375 INCH LONG AFT SIDE. CRACK MARKED UPPER DECK. (S)

Part: FRAME — CRACKED (BS 460 S12L) · airframe 77,200 hrs · 19,248 cycles

BS 460 S12L FRAME DOUBLER AFT SIDE, CRACKED .375 INCH AT STRINGER CUTOUT, INBOARD UPPER CORNER. CRACK MARKED UPPER DECK. (S)

Part: FRAME — DENTED (BS 700) · airframe 77,200 hrs · 19,248 cycles

BS 700 FUSELAGE FRAME WEB DENTED ABOVE STR 47R. (S)

Part: FRAME — DENTED (FUSELAGE) · airframe 77,200 hrs · 19,248 cycles

FWD PIT BS640 FUSELAGE FRAME DENTED AT LBL26, WL112. (S)

Part: WEB — DENTED (FUSELAGE) · airframe 77,200 hrs · 19,248 cycles

BILGE TORQUE BOX UPPER WEB DENTED AT BS670, LBL36 AND LBL40, WL118. (S)

Part: FRAME — CRACKED (BS 440) · airframe 77,200 hrs · 19,248 cycles

BS 440 S10R FRAME CRACKED .500 INCH AT STRINGER CUTOUT. CRACK MARKED UPPER DECK. (S)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,453 hrs · 19,101 cycles

RIGHT UPPER DECK DOOR FRAME EMERGENCY LIGHT IS OUT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 76,453 hrs · 19,101 cycles

RIGHT SIDE UPPER DECK EXTERIOR EMERGENCY SLIDE EXIT LIGHT INOP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 76,453 hrs · 19,101 cycles

LEFT SIDE UPPER DECK EXTERIOR EMERGENCY SLIDE EXIT LIGHT INOP.

Part: LIGHT — NOT SEATED (COCKPIT) · airframe 75,228 hrs · 18,855 cycles

DURING CRUISE STRONG ACRID SMELL IN COCKPIT TURNED OFF PILOT FLUORESCENT & SMELL WENT AWAY. FOUND ONE OF THE CAPTAIN`S FLUORESCENT LIGHT BULBS NOT COMPLETELY SEATED IN LIGHT SOCKET. REMOVED AND REPLACED CAPTAIN'S FLUORESCENT LIGHT BULBS IAW B747 MM CHAPT 33-11-11. OPS CHECKED SYSTEM FOR 7 HRS. NO DEFECTS OR ABNORMAL ODORS NOTED. SYSTEM OPS CHECKS GOOD IAW B747 MM CHAPT 33-11-00.

Part: BULKHEAD — CRACKED (NR 4 NACELLE) · airframe 74,821 hrs · 18,772 cycles

NR 4 PYLON NAC STA 179 VERTICAL BULKHEAD HAS SHEARED FASTENER AND CRACKED (1 INCH) IN WEB.

Part: SILL — CORRODED (CARGO DOOR) · airframe 74,430 hrs · 18,689 cycles

C-2 DOOR SILL UPPER CHORD IS CORRODED APPROX AT 1860.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 74,430 hrs · 18,689 cycles

MAIN DECK CARGO DOOR SKIN IS DAMAGED AT FORWARD LOWER AREA AT STA 1790, WL 221.

Part: INTERCOSTAL — DAMAGED (CARGO DOOR) · airframe 74,430 hrs · 18,689 cycles

MAIN DECK CARGO DOOR FRAME INTERCOSTAL IS DAMAGED AT STA 1790, WL 219.

Part: BULKHEAD — CHAFED (NR 3 NACELLE) · airframe 73,344 hrs · 18,471 cycles

NR 3 PYLON NAC STA 221.9 BULKHEAD WEB CHAFED AT HYD FITTINGS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,970 hrs · 19,617 cycles

LEFT UPPER DECK EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (BS 640) · airframe 71,965 hrs · 18,187 cycles

UPPER DECK EMERGENCY LIGHT INOP AT BS 640.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,313 hrs · 18,048 cycles

EMERGENCY EXIT SIGN INOP AT LT UPPER DECK EXIT DOOR STA 400.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,313 hrs · 18,148 cycles

EMERGENCY EXIT LIGHT INOP AT STA 540.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

FLOOR FITTING AT BS460, LBL10 BROKEN

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,313 hrs · 18,048 cycles

MAIN DECK FLOORBEAM UPPER CHORD IS CORRODED AT STA 460, LBL 34 TO LBL 50.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,313 hrs · 18,048 cycles

EMERGENCY EXIT LT IN CEILING AT RT ESCAPE DOOR MOST FWD LIGHT WILL NOT STAY ILLUMINATED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

FLOORBEAM UPPER CHORD STA-460 LBL-72 CORRODED.

Part: FITTING — CORRODED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

STA. 2360 BOLT HOLE NR L85 HAS CORROSION IN STRINGER L16 UPPER HOLE FITTING

Part: STRINGER — MISREPAIRED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

IMPROPER STRINGER REPAIR ON STRINGER 11R BETWEEN STA 1831 TO 1815

Part: WEB — CORRODED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

CORROSION ON BOTTOM OF MAIN DECK FLOOR WEB BS520 RBL64.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

STRINGER CLIP IS DAMAGED AT STA. 1820 ON STRINGER 11R

Part: FRAME — CRACKED (NR 4 PYLON) · airframe 71,313 hrs · 18,048 cycles

PYLON NR 4 AT PYLON STA 221.9 AFT ENG MOUNT BULKHEAD JUST IB OF UPPER SPAR HAS CRACKED HORSESHOE FRAME.

Part: FRAME — CRACKED (NR 4 PYLON) · airframe 71,313 hrs · 18,048 cycles

NR 4 PYLON NAC STA 221.9 AFT ENG MOUNT BULKHEAD JUST OB OF UPPER SPAR HAS STOP DRILLED CRACK IN HORSESHOE FRAME

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

CAPTAINS LT FWD O/B SEAT TRACK CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

FE I/B SEAT TRACK CORRODED AT FWD END

Part: FASTENER — LOOSE (EMPENNAGE) · airframe 71,313 hrs · 18,048 cycles

LOOSE FASTENERS ON L/H SIDE OF EMPENNAGE BETWEEN STA 2680 TO 2701 12 TO 40 INCHES ABOVE APU DOOR HINGE.

Part: SKIN — CORRODED (CENTER WING) · airframe 71,313 hrs · 18,048 cycles

CORROSION ON WING CENTER SECTION UPPER SKIN AT STA 1210 AND 1220 RBL 98 UNDER MAIN DECK FLOOR.

Part: SPAR — BULGED (NR 2 PYLON) · airframe 71,313 hrs · 18,048 cycles

NR 2 PYLON UPPER SPAR WEB AT NAC STA 221 I/B AFT SIDE OF BULKHEAD LOWER UPPER SPAR WEB SURFACE BULGED.

Part: SPAR — BUCKLED (NR 1 PYLON) · airframe 71,313 hrs · 18,048 cycles

NR 1 PYLON MID SPAR WEB AREA BUCKLED NAC STA 221 AFT SIDE OF BULKHEAD LOWER I/B SURFACE.

Part: SUPPORT — CORRODED (HORIZ STAB) · airframe 71,313 hrs · 18,048 cycles

RT HORIZ STAB UPPER I/B POWER PACK ELEVATOR HINGE SUPPORT HAS CORROSION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

SEVERAL AREAS OF CORROSION ON FWD SIDE OF BS 280 FLOORBEAM WEB, LBL30 TO RBL30.

Part: CLIP — MISDRILLED (NLG WW) · airframe 71,313 hrs · 18,048 cycles

ATTACH CLIP MIS-DRILLED ON NOSE WHELL WELL VERTICAL BEAM FWD SIDE RT, BS 280, WL 170.

Part: SKIN — PUNCTURED (NOSE CARGO DOOR) · airframe 71,313 hrs · 18,048 cycles

PUNCTURE IN NOSE CARGO DOOR SKIN FWD OF BS 220, I/B OF STR 43L.

Part: INTERCOSTAL — CRACKED (NLG WW) · airframe 71,313 hrs · 18,048 cycles

NOSE WHEEL WELL INTERCOSTAL CRACKED AT BS 300 I/B OF LBL 20 ABOVE LT BRAKE SNUBBER.

Part: CLIP — CRACKED (NLG WW) · airframe 71,313 hrs · 18,048 cycles

ATTACH CLIP AND STIFFENER CRACKED ON NOSE WHEEL WELL TOP PANEL AT RBL 20 BETWEEN BS 265 AND 280.

Part: CLIP — CRACKED (NLG WW) · airframe 71,313 hrs · 18,048 cycles

ATTACH CLIP CRACKED ON NOSE WHEEL WELL VERTICAL BEAM AFT SIDE AT RT BS 300, WL170.

Part: CLIP — CORRODED (NLG WW) · airframe 71,313 hrs · 18,048 cycles

FIVE CORRODED ATTACH CLIPS IN NOSE WHEEL WELL AT LBL 20 AND LBL 30 BETWEEN BS 265 AND 280.

Part: STIFFENER — CRACKED (NLG WW) · airframe 71,313 hrs · 18,048 cycles

NOSE WHEEL WELL TOP PANEL STIFFENER CRACKED AT LBL 20 BETWEEN BS 265 AND 280.

Part: STIFFENER — CRACKED (NLG WW) · airframe 71,313 hrs · 18,048 cycles

NOSE WHEEL WELL, BS 370 LT SIDE BETWEEN WL 130 AND 140, LBL 10, 1 VERTICAL STIFFENER CRACKED.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

BS 340 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE HAS 3 ELONGATED HOLES WITH NO ED AND CRACK INDICATIONS BETWEEN RBL 10 AND RBL 20.

Part: ATTACH ANGLE — CRACKED (CARGO BAY) · airframe 71,313 hrs · 18,048 cycles

AFT PIT BS 1780 RT PALLET SIDE RAIL ATTACH ANGLE CRACKED.

Part: ANGLE — CRACKED (NLG WW) · airframe 71,313 hrs · 18,048 cycles

NOSE WHEEL WELL ANGLE CRACKED AT LT BS 360, WL 140, LBL 10.

Part: CLIP — CRACKED (NLG WW) · airframe 71,313 hrs · 18,048 cycles

NOSE WHEEL WELL, THREE ATTACH CLIPS CRACKED LT AT BS 340 LBL10 WL140, 150, AND 160.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

BS 360 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE HAS CRACK INDICATION AT LBL 56.

Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

BS 360 UPPER DECK FLOORBEAM UPPER CHORD FWD FLANGE HAS MISS DRILLED FASTENER HOLES AT RBL 19 TO RBL 40.

Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

BS 360 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE HAS DOUBLE DRILLED FASTENER HOLE AT LBL 44.

Part: FIRE SEAL — DAMAGED (NR 1 PYLON) · airframe 71,313 hrs · 18,048 cycles

NR 1 PYLON, INBD FIRE SEAL DAMAGED ALONG THE ENTIRE LENGTH OF THE SEAL.

Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

BS 340 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE HAS MISS DRILLED HOLES BETWEEN RBL 25 AND RBL 35.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,313 hrs · 18,048 cycles

UPPER DECK FLOORBEAM UPPER CHORD CORRODED AT BS 480, RBL3.

Part: SKIN PANEL — CORRODED (HORIZ STAB) · airframe 71,313 hrs · 18,048 cycles

LT HORIZ STAB UPPER SURFACE HAS CORROSION AT STAB STA 165.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 71,313 hrs · 18,048 cycles

SEAT TRACK IS CORRODED AT STA 540 TO 560 RBL 27.99.

Part: SEAT TRACK — DAMAGED (BS 1940-1960) · airframe 71,313 hrs · 18,048 cycles

STA 1940 TO 1960, LBL 11 SEAT TRACK SPLICE DAMAGED.

Part: CHANNEL — CRACKED (BS 900) · airframe 71,313 hrs · 18,048 cycles

STA 900 LEFT TENSION TIE FWD CHANNEL CRACKED AT STEEL U-CHANNEL ATTACH POINT.

Part: SHEAR TIE — CRACKED (BS 440) · airframe 71,313 hrs · 18,048 cycles

FUSELAGE FRAME SHEAR TIE CRACKED AT BS 440 BELOW STR 9L.

Part: SHEAR TIE — CRACKED (BS 440) · airframe 71,313 hrs · 18,048 cycles

FUSELAGE FRAME SHEAR TIE CRACKED AT BS 440 BELOW STR 8R.

Part: SKIN — CORRODED (BS 1000) · corrosion level 2 · airframe 71,313 hrs · 18,048 cycles

CORROSION ON FUSELAGE SKIN AT BS 1000, LBL 55, WL 109, STR 43L.

Part: SKIN — CORRODED (BS 1000) · corrosion level 2 · airframe 71,313 hrs · 18,048 cycles

CORROSION ON FUSELAGE SKIN AT BS 1000, RBL 51, WL 108, STR 43R.

Part: SHEAR TIE — CRACKED (BS 440) · airframe 71,313 hrs · 18,048 cycles

FUSELAGE FRAME SHEAR TIE CRACKED AT BS 440 BELOW STR 9R.

Part: STIFFENER — CRACKED (BS 265-280) · airframe 71,313 hrs · 18,048 cycles

LT NOSE WHEEL WELL SIDEWALL PANEL WEB STIFFENER CRACKED AT BS 265-280 WL 170.

Part: LIGHT — FAILED (CABIN) · airframe 70,811 hrs · 17,944 cycles

RT EMERGENCY SLIDE LIGHT WILL NOT TEST.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 70,414 hrs · 17,863 cycles

CAPTAIN SEAT LEFT SEAT TRACK CRACKED 1.5 INCH AT STOP MOUNT. REPLACED LT AFT CAPT SEAT TRACK IAW AMM 25-11-01.

Part: BULKHEAD — CHAFED (NACELLE) · airframe 70,414 hrs · 17,863 cycles

REAR ENGINE MOUNT BULKHEAD WEB CHAFED AROUND HYDRAULIC UNION, NAC STA 221.90. REMOVED REPAIR AREA FASTENERS AND DAMAGED MATERIAL IAW B747 SRM 54-14-03. FABRICATED 4 X 9 INCH DOUBLER IAW B747 SRM 54-14-13 FIG 16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,970 hrs · 19,617 cycles

LEFT UPPER DECK EMERGENCY LIGHT INOP.