N725CK

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,927 hrs · 37,535 cycles

STA 850 L/H LBL 65 CORROSION FOUND ON BOTTOM OF FLOOR BEAM.

Part: STRAP — CORRODED (BS 740 LBL55) · corrosion level 2 · airframe 68,927 hrs · 37,535 cycles

STA 740 L/H LBL 55 EVIDENCE OF CORROSION ON STRAP ON THE UNDERSIDE OF FRAME.

Part: NONE — NONE (NONE) · corrosion level 2 · airframe 68,927 hrs · 37,535 cycles

EVIDENCE OF CORROSION AROUND NUTPLATE HOLES ON MAIN DECK FLOOR STRUCTURE UPPER SURFACE AT APPROX STA 1138-1156 LBL 60.

Part: FLOOR SUPPORT — CORRODED (BS 380-440 RBL65) · airframe 68,927 hrs · 37,535 cycles

EVIDENCE OF CORROSION IN MULTIPLE LOCATIONS FROM STA 380 TO STA 440 APPX RBL 65 FLOOR SUPPORT Z CHANNEL.

Part: PUMP — INOPERATIVE · airframe 68,546 hrs · 37,323 cycles

#3 SHUT DOWN IN FLIGHT CORRECTIVE ACTION: R&R #3 ENG FUEL PUMP IAW P&W MM 73-11-01 R&R #3 FUEL CONTROL IAW P&W MM 75-21-01. PERFORMED LEAK CHECK, ENGINE TESTS B,D,H AND NOTE 2 IAW P&W MM 72-00-00 ADJ/TEST -01. ALL CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME. PARTS CHANGED, FUEL PUMP / FCU P/N OFF 378200 / 743602-5 S/N OFF 4292F / 64481

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,114 hrs · 37,150 cycles

CORROSION ON CENTER TANK AT STA 780 LBL 48

Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,114 hrs · 37,150 cycles

EVIDENCE OF CORROSION UNDER MAIN DECK FLOOR APPROX STA 880 LBL 68

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,114 hrs · 37,150 cycles

AFT PIT FRAME AT STATION 1030 STRING 27 R HAS EVIDENCE OF CORROSION ON UPPER SURFACE

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,114 hrs · 37,150 cycles

FRAME AT STATION 1166 OUTBOARD OF STRINGER 29 RIGHT HAS EVIDENCE OF CORROSION AT INTERFACE BETWEEN LOWER CHORD AND WEB

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,114 hrs · 37,150 cycles

AFT PIT FRAME AT STATION 1010 BETWEEN STRINGER 26R AND 27R HAS EVIDENCE OF CORROSION ON UPPER SURFACE

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,114 hrs · 37,150 cycles

AFT PIT STRINGER 28 RIGHT, STATION 980 TO 1010 IS CORRODED

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,114 hrs · 37,150 cycles

EVIDENCE OF CORROSION ON STRINGER 27 RIGHT SPLICE AT STATION 1050

Part: STRINGER — DAMAGED (ZONE 100) · corrosion level 2 · airframe 68,114 hrs · 37,150 cycles

FRAME DAMAGED AT STA 1070 RBL 21 STR 27

Part: RETAINER — DAMAGED (EMERGENCY EXIT) · airframe 67,046 hrs · 36,558 cycles

LEFT HAND FWD EMERGENCY EXIT HATCH #7 UPPER SEAL RETAINER HAS DAMAGEED HOLES, ELONGATED HOLES. R&R SEAL RETAINER IAW B727 SRM 51-30-2

Part: FRAME — CRACKED (FUSELAGE)

AFT CARGO CONPARTMENT FRAME CRACKED STA 1130 LBL 48

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,046 hrs · 36,558 cycles

FLOORBEAM UPPER SURFACE HAS POSSIBLE CORROSION @ CLIP NUT HOLES STA 1030 RBL 24-48

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

FLOORBEAM CORROSION STA 950C RBL 50-59

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,046 hrs · 36,558 cycles

FLOORBEAM LOWER SURFACE HAS POSSIBLE CORROSION @ CLIP NUT HOLES STA 1130 RBL 24 - 48

Part: FLOORBEAM — CORRODED (BS 1070) · corrosion level 2 · airframe 67,046 hrs · 36,558 cycles

FLOORBEAM LOWER CHORD CORRODED @ STA 1070 RBL 55

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,046 hrs · 36,558 cycles

SEAT TARCK CORRODED STA 950 + 10 RBL 48

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,046 hrs · 36,558 cycles

SEAT TRACK CORROSION STA 1110 - 1130 RBL 48

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,046 hrs · 36,558 cycles

SEAT TRACK CORRODED STA 870-960 LBL 46

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

FLOORBEAM CORROSION STA 950C LBL 46 TO 64

Part: GATE — CORRODED (R1 DOOR) · corrosion level 2

R1 DOOR LOWER GATE CORRODED

Part: SERVICE DOOR — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,046 hrs · 36,558 cycles

L/H AFT SERVICE DOOR CORRODED

Part: RETAINER — CRACKED (CARGO DOOR) · airframe 67,046 hrs · 36,558 cycles

MAIN CARGO DOOR FWD UPPER CORNER UNDER BULB SEAL HAS A CRACK

Part: SEAL — CRACKED (CARGO DOOR) · airframe 67,046 hrs · 36,558 cycles

MAIN CARGO DOOR AFT UPPER CORNER UNDER BULB SEAL HAS A CRACK

Part: RETAINER — DAMAGED (EMERGENCY EXIT) · airframe 67,046 hrs · 36,558 cycles

L/H FWD EMERGENCY EXIT HATCH HAS DAMAGED HOLES #4 UPPER SEAL RETAINER

Part: RETAINER — DAMAGED (EMERGENCY EXIT) · airframe 67,046 hrs · 36,558 cycles

EMERGENCY EXIT HATCH L/H FWD HATCH #3 UPPER SEAL RETAINER HAS DAMAGED HOLES

Part: RETAINER — ELONGATED (EMERGENCY EXIT) · airframe 67,046 hrs · 36,558 cycles

L/H FWD EMERGENCY EXIT HATCH #3 LOWER SEAL RETAINER HAS DAMAGED HOLES

Part: RETAINER — DAMAGED (ESCAPE HATCH) · airframe 67,046 hrs · 36,558 cycles

L/H FWD EMERGENCY EXIT HATCH HAS DAMAGED HOLE ON SEAL RETAINER #2 LOWER

Part: RETAINER — DAMAGED (ZONE 200) · airframe 67,046 hrs · 36,558 cycles

R/H AFT EMERGENCY EXIT HATC SEAL RETAINER HAS DAMAGED HOLES

Part: RETAINER — DAMAGED (EMERGENCY EXIT) · airframe 67,046 hrs · 36,558 cycles

L/H FWD EMERGENCY EXIT HATCH #6 LOWER SEAL RETAINER HAS ELONGATED HOLES

Part: LIGHT — DETACHED (CABIN) · airframe 67,046 hrs · 36,558 cycles

L1 DOOR EMERGENCY EXIT LIGHT HAS FALLEN OFF

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 66,392 hrs · 36,283 cycles

DURING LEVEL FLIGHT AT 10000 FEET WITH CARGO HEAT OUTFLOW VALVE CLOSED PRESSURIZATION WILL NOT MAINTAIN WITH ONE PACK OPERATION.

Part: FRAME — CORRODED (BS 950C) · corrosion level 2 · airframe 66,392 hrs · 36,283 cycles

FRAME HAS CORROSION

Part: FITTING — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 66,392 hrs · 36,283 cycles

AFT PIT DOOR FITTING CORRODED

Part: FITTING — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 66,392 hrs · 36,283 cycles

AFT PIT DOOR FITTING CORROSION

Part: STRUCTURE — CORRODED (BS 294.5) · corrosion level 2 · airframe 66,392 hrs · 36,283 cycles

CORROSION BETWEEN ANGLE & WEB ABOVE HORIZONTAL WALKWAY BEAM

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,392 hrs · 36,283 cycles

CORROSION ON WEB FLOOR SUPPORT CHANEL ABOVE HORIZONTAL WALKWAY BEAM

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 66,392 hrs · 36,283 cycles

#1 PYLON FASTENER HOLE "A" CRACK INDICATION

Part: FRAME — CORRODED (BS 1130) · corrosion level 2 · airframe 66,392 hrs · 36,283 cycles

FRAME IN AFT PIT CORRODED.

Part: FRAME — CORRODED (BS 1148) · corrosion level 2 · airframe 66,392 hrs · 36,283 cycles

FRAME IN AFT PIT CORRODED.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,392 hrs · 36,283 cycles

CHORD HAS CORROSION

Part: STRUCTURE — CORRODED (BS 1176) · corrosion level 2 · airframe 66,392 hrs · 36,283 cycles

CHORD HAS CORROSION

Part: SEAT TRACK — CORRODED (BS 1141) · corrosion level 2 · airframe 66,392 hrs · 36,283 cycles

I/B SEAT TRACK LEG HAS CORROSION

Part: DUCT — CRACKED (ZONE 400) · airframe 65,985 hrs · 36,120 cycles

AFTER TAKEOFF WHEN CLIMBING THRU 1300 FEET NR 1 PYLON STRUT OVERHEAT LIGHT ILLUMINATED, PER AOM VOL 1 CHAP 4 REDUCED THRUST TO IDLE TO GET LIGHT TO EXTINGUISH. UNSCHEDULED LANDING.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 65,815 hrs · 36,045 cycles

APPROXIMATELY 15 MINUTES INTO THE FLIGHT, HEARD A RUMBLING NOISE WHILE CLIMBING TO FL320. PRIOR TO REACHING THE FLT ENGINEER COULD NOT CONTROL THE CABIN, INITIALLY THE CABIN WAS AT 5500 FEET APPROACHING FL260. IT SHOULD HAVE BEEN AROUND 4400 FEET AT FL 260. STOPPED THE CLIMB AT FL260 BUT THE CABIN CONTINUED TO CLIMB, AND WORKED THROUGH THE CHECKLIST. DECENDED AND IT TOOK 10000 FEET TO STABILIZE THE CABIN. RETURNED TO DEPARTURE.

Part: LINE — LEAKING (B HYD SYS) · airframe 65,739 hrs · 36,012 cycles

RETURNED TO DEPARTURE DUE TO A HYDRAULIC B SYSTEM LOSS. REMOVED AND INSTALLED TEMPORARY FLEX LINE ON THE NR 1 HYD B PUMP IAW AMM 20-10-12, AND 20-80-01, LEAK AND OPS CHECKED GOOD.

Part: STRINGER — CORRODED (BS 1010-1030) · airframe 65,479 hrs · 35,885 cycles

STRINGER 29R CORRODED AT BS 1010 - 1030.

Part: SKIN — CORRODED (BS 1010-1030) · airframe 65,479 hrs · 35,885 cycles

FUSELAGE SKIN CORRODED AT BS 1010 - 1030, STRINGER 29R.

Part: PITOT TUBE — OBSTRUCTED (PITOT/STATIC SYS) · airframe 65,214 hrs · 35,777 cycles

NO AIR SPEED ON CAPTAINS INDICATOR, ABORTED TAKE OFF AND RETURNED TO BLOCKS. INSPECTED PITOT TUBE AND REMOVED DEBRIS, OP'S AND LEAK CHECK GOOD IAW AMM 34-11-00.

Part: ENGINE — FLUCTUATES (NR 1) · airframe 65,194 hrs · 35,769 cycles

NR 1 ENGINE AT TAKEOFF AND CLIMB OUT, EPR, N1, N2, FUEL FLOW, AND EGT SURGED WITH BLEED PRESSURE FLUXING 20-40 PSI.

Part: FITTING — CORRODED (LT UPPER) · airframe 64,678 hrs · 35,551 cycles

LEFT UPPER AFT LINK ATTACH POINT FOR JACKSCREW HAS EVIDENCE OF CORROSION UNDER WASHER UNDER ACCESS PANEL 9705

Part: PLUG — CORRODED (WINDOW) · corrosion level 2 · airframe 64,678 hrs · 35,551 cycles

BS 730B LT SIDE OF ACFT HAS POSSIBLE CORROSION AROUND WINDOW PLUG

Part: BUSHING — CORRODED (RT WING) · airframe 64,678 hrs · 35,551 cycles

RIGHT WING REAR SPAR TO BODY FITTING AFT BUSHING HAS CORROSION ON FLANGE

Part: PIN — CORRODED (RT WING) · airframe 64,678 hrs · 35,551 cycles

RIGHT WING REAR SPAR TO BODY FITTING BOTTLE PIN HAS CORROSION ON FLANGE

Part: FLAP SYSTEM — FAILED · airframe 64,415 hrs · 35,444 cycles

AFTER TAKEOFF, THE LEADING EDGE FLAPS DID NOT RETRACT, RETURNED TO DEPARTURE.

Part: SUPPORT BEAM — CORRODED (BS 942) · corrosion level 2 · airframe 64,022 hrs · 35,267 cycles

RIGHT MLG SUPPORT BEAM LOWER SURFACE CORROSION, BS 942.65 BETWEEN WBL 81.65 AND WBL 125.18.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 63,999 hrs · 35,258 cycles

PRESSURIZATION CONTROLLER WOULD NOT MAINTAIN PRESSURIZATION IN AUTO, STANDBY, AC/DC, MANUAL MODES. TEARDOWN REPORT AUTO MODE BOARD ASSY, AF RELAYS, STANDBY BOARD ASSY, OUT OF CALIBRATION.

Part: ANGLE — CORRODED (BS 888) · corrosion level 2 · airframe 63,934 hrs · 35,229 cycles

UPPER PRESSURE PANEL LT ANGLE CORROSION, LT WHEEL WELL 60" OTBD FROM KEELBEAM AT BS 888.

Part: FRAME — CORRODED (MLG WW) · corrosion level 2 · airframe 63,934 hrs · 35,229 cycles

HORIZONTAL FRAME HAS SMALL AREA OF CORROSION LT WHEEL WELL OTBD AT BS 888.

Part: PLUG — CORRODED (BS 740) · corrosion level 2 · airframe 63,934 hrs · 35,229 cycles

WINDOW PLUG CORROSION.

Part: STRUCTURE — CORRODED (BS 670) · corrosion level 2 · airframe 63,934 hrs · 35,229 cycles

FUSELAGE CORROSION AT FWD EDGE OF WINDOW.

Part: SKIN — CORRODED (BS 1012) · corrosion level 2 · airframe 63,934 hrs · 35,229 cycles

AFT PIT UNDER INTERCOSTAL HAS CORROSION ON SKIN AT RBL 18, STA 1012.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 63,803 hrs · 35,171 cycles

CABIN PRESSURIZATION COULD NOT BE CONTROLLED IN ANY MODE AT FL200 CABIN WARNING HORN COME ON.

Part: FIRE WARNING — ILLUMINATED (MLG WW) · airframe 63,685 hrs · 35,121 cycles

WHEEL WELL FIRE DETECTION LIGHT ILLUMINATED INTERMITTENTLY AFTER TAKEOFF AT 9,000 FEET. COMPLIED WITH EMERGENCY PROCEDURES AND RETURNED TO DEPARTURE.

Part: SEAT TRACK — CORRODED (BS 863) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORROSION FS 863, RBL 46.

Part: SEAT TRACK — DAMAGED (BS 950E) · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK DAMAGED FS 950E AND 3 LBL 25.

Part: FLOORBEAM — CORRODED (BS 1068) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORRODED FS 1068, RBL 44.

Part: FLOORBEAM — CORRODED (BS 930) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORRODED LOWER TEE FS 930, RBL 13.

Part: FLOORBEAM — CORRODED (BS 930) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORRODED LOWER CHORD FS 930, RBL 12 AND 57.

Part: FLOORBEAM — CORRODED (BS 910) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORRODED FS 910, LBL 66.

Part: FRAME — CRACKED (BS 930) · airframe 63,355 hrs · 34,978 cycles

FRAME CRACKED AT FS 930, STR 14L.

Part: FLOORBEAM — CORRODED (BS 900) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORRODED LOWER CHORD, FS 900, LBL 2.

Part: DOUBLER — CORRODED (BS 1164) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

INNER DOUBLER ON SKIN CORRODED, FS 1164, STR 20 - 22 LT.

Part: FLOORBEAM — CORRODED (BS 890) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORRODED LOWER CHORD, FS 890, LBL 35.

Part: FLOORBEAM — CORRODED (BS 870) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORRODED FS 870, LBL 49.

Part: FLOORBEAM — CORRODED (BS 870) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORRODED UPPER TEE FS 870, RBL 48.

Part: FLOORBEAM — CORRODED (BS 928) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORRODED FORWARD LOWER FLANGE FS 928, LBL 66.

Part: FLOORBEAM — CORRODED (BS 870) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORRODED LOWER CHORD, FS 870, RBL 23.

Part: PRESSURE DECK — CORRODED (BS 930) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

LEFT WHEEL WELL PRESSURE DECK CORROSION AT STA 930.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORROSION STA 312, LBL 30.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

MAIN DECK FLOOR STRUCTURE CORROSION BS 328, LBL 29.

Part: FLOOR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOOR PANEL CORROSION STA 340 AND 370, LBL 50.

Part: FRAME SPLICE — CRACKED (BS 930) · airframe 63,355 hrs · 34,978 cycles

FRAME STRAP CRACKED, FS 930, STR 14L.

Part: SEAT TRACK — CORRODED (BS 872) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORRODED FS 872, LBL 46.

Part: BEAM — CRACKED (ZONE 300) · airframe 63,355 hrs · 34,978 cycles

VERTICAL STAB KICKLOAD BEAM LT WEB POST CRACKED WERE IT ATTACHES TO STRINGER 11 IAW SB 727-55-0093, FIG 3, SHEET 4 FOR LOCATION.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORRODED FS 720A, LBL 63.

Part: SEAT TRACK — CORRODED (BS 1035) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORROSION STA 1035, RBL 45.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORROSION STA 380, RBL 46.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORRODED, BS 950C-950F, RBL 40.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORROSION STA 1010 - 1030, LBL 46.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORRODED BS 870 & 890, RBL 46.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORROSION STA 900, LBL 35 AND 49.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORROSION STA 900, LBL 35 AND 49.

Part: SEAT TRACK — CORRODED (BS 725) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORROSION, STA 725, LBL 46.

Part: FLOORBEAM — CORRODED (BS 890) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORROSION STA 890, LBL 35.

Part: SEAT TRACK — CORRODED (BS 1050-1070) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORROSION STA 1050 AND STA 1070, LBL 46.

Part: FLOORBEAM — CORRODED (BS 344) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

MAIN DECK FLOORBEAM CORROSION STA 344, LBL 47.

Part: FLOORBEAM — CORRODED (BS 305) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

MAIN DECK FLOORBEAM CORRODED, STA 305, RBL 12.

Part: FLOORBEAM — CORRODED (BS 344) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

MAIN DECK FLOORBEAM CORROSION, STA 344, LBL 62.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK FLANGE CRACKED STA 380, RBL 46.

Part: SEAT TRACK — CORRODED (BS 950B) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORRODED STA 950B + 16", LBL 46.

Part: FLOORBEAM — CORRODED (BS 910) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

FLOORBEAM CORROSION, STA 910, LBL 35 & LBL 47.

Part: SEAT TRACK — CORRODED (BS 1130) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORRODED STA 1130, LBL 46.

Part: SEAT TRACK — CORRODED (BS 560-620) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORROSION STA 560-620, RBL 24.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,355 hrs · 34,978 cycles

EMERGENCY EXIT LIGHTS DO NOT WORK IN THE ON POSITION.

Part: SEAT TRACK — CORRODED (BS 690) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORRODED STA 690, LBL 24.

Part: SEAT TRACK — CORRODED (BS 600-690) · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORRODED STA 600-690, RBL 46.

Part: SEAT TRACK — CORRODED (BS 500-600) · corrosion level 2 · airframe 63,355 hrs · 34,978 cycles

SEAT TRACK CORRODED STA 500-600, RBL 46.

Part: SPAR — CRACKED (RT ELEVATOR) · airframe 63,355 hrs · 34,978 cycles

RIGHT ELEVATOR REAR SPAR CRACKED.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 63,355 hrs · 34,978 cycles

NR 1 PYLON FASTENER HOLE "P" HAS CRACK INDICATION, REF SB 727-54A0010.

Part: CLAMP — BROKEN (APU EXHAUST) · airframe 62,924 hrs · 34,808 cycles

ON GROUND, APU SHOWED FIRE WARNING, VISUAL FIRE CONFIRMED, BOTTLE DISCHARGED. ON INVESTIGATION, THE INNER EXHAUST DUCT V BAND CLAMP BROKE SENDING HOT AIR INTO THE SPACE BETWEEN THE INNER AND OUTER EXHAUST PIPE IGNITING RESIDUAL OIL AND FUEL. APU WILL BE REPLACED.

Part: HANDLE — LACK OF LUBE (MLG) · airframe 62,017 hrs · 34,418 cycles

GEAR DOOR LIGHT ILLUMINATED, NO EMERGENCY PROCEDURES DECLARED, RETURNED TO DEPARTURE. LUBED GEAR HANDLE IAW AMM 20-60-02, OP'S CHECKED IAW 32-61-12, NO DEFECTS NOTED.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

FORWARD BILGE BULKHEAD SUPPORT ANGLE CORRODED BS 740, STR 27R.

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

MAIN DECK WINDOW FRAME CORRODED, BS 710.

Part: TRUNNION — CORRODED (ZONE 700) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

LEFT FWD TRUNION INNER SURFACE CORRODED.

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

REPAIR WINDOW FORGING FROM STA 720B - 720D DUE TO PREVIOUSLY INSTALLED DOUBLER AT BS 720C - 720D RT SIDE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

STRINGER 29L, CORROED BS 950A + 10 TO BS 1000.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

STRINGER 28R CORRODED, BS 990.

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

AFT CARGO DOOR THRESHOLD WEB CORRODED BS 950F +10, RBL 20.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

BS 950E PLUS 6 INCHES STUB FRAME CORROSION AFT SIDE BETWEEN 27-29R.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

BS 950E, PLUS 6, SHEAR TIE OTBD OF STRINGER 28R IS CORRODED.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

FUSELAGE FRAME SHEAR TIE CORRODED.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

FUSELAGE FRAME SHEAR TIE CORRODED BS 970, S29R.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

STUB FRAME CORRODED, BS 990 -6.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

STRINGER CORRODED IN FWD BILGE BS 720F - 740, S27R.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

CORROSION ON AFT SIDE OF BS 990 FUSELAGE FRAME SHEAR TIE OTBD OF S29L.

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

MAIN DECK WINDOW FRAME CORRODED, BS 1080.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

FUSELAGE FRAME SHEAR TIE CORROSION BS 990, STR 28L.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

CORROSION ON BS 990 FUSELAGE FRAME SHEAR TIE OTBD OF S28L.

Part: STRINGER CLIP — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

STRINGER TO FRAME ATTACH CLIP CORRODED STA 900, STR 27L.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

SHEAR TIE CORRODED BS 990, STR 29R.

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

MAIN DECK WINDOW FRAME CORRODED, BS 980.

Part: SKIN — CRACKED (ZONE 100) · airframe 62,014 hrs · 34,413 cycles

SKIN HAS CRACK INDICATIONS AT FOUR LOWER ROW FASTENERS BS 580 - 600, S4R.

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,014 hrs · 34,413 cycles

AFT CARGO THRESHOLD LOWER CORRODED, (2 X 2)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,700 hrs · 34,281 cycles

FLOORBEAM STA 360 FLANGE CORRODED AT FASTENER HOLE, 1X1 INCHES (NR 0169,0231).

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 60,696 hrs · 33,846 cycles

AT FL280 FIRE BELL SOUNDED, LOWER CARGO LIGHT ILLUMINATED, AFT CARGO MESSAGE ON MX DISPLAY LIGHT EXTINGUISHED DURING DESCENT. RAN LOWER CARGO FIRE CHECKLIST, CONTINUED TO DAL ASKED FOR FIRE TRUCKS TO MEET AIRCRAFT. DAL FIRE AND RESCUE FOUND NO FIRE AND DAMAGE TO AIRCRAFT. TRANSFERRED TO DMI 7250016 IAW KII MEL 26-19 CAT C DUE 4/18/11 PLACARDS INSTALLED. PART REPAIRED, FINDINGS NO PHYSICAL DAMAGE, UNIT FAILED PRELIM TEST DUE TO LOW QUIESCENT, UNIT WAS CLEANED, LOGIC BOARD REPLACED AND FUNCTIONAL TESTED.

Part: SMOKE DETECTOR — DIRTY (CARGO BAY) · airframe 60,692 hrs · 33,843 cycles

AT FL340 FIRE BELL SOUNDED LOWER CARGO LIGHT ILLUMINATED AND AFT CARGO ON MX DISPLAY LIGHT EXTINGUISHED DESENDING THROUGH APPROX 16,000 FT. INSPECTED AND CLEANED LOWER AFT CARGO SMOKE DETECTORS OF DEBRIS, SYSTEM OP'S CHECKS NORMAL IAW HOLLINGSHEAD / SECURAPLANE AMM SUPPLEMENT 25-15-00-7. NO HARD FAILURE OF DETECTOR TO IDENTIFY WHICH CAUSED THE DEFECT.

Part: FRAME — DENTED (FUSELAGE) · airframe 59,804 hrs · 33,444 cycles

FRAME DENTED 2 EA. 1 INCH DIA. DENTS 6 INCHES APART.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,767 hrs · 33,410 cycles

M/D FLOOR SUPPORT CORROSION STA 335 RBL 55 1 X 1 INCHES.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,771 hrs · 33,411 cycles

M/D FLOOR SUPPORT CORROSION AT STA 335 RBL 45 1 X 1 INCHES.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,771 hrs · 33,411 cycles

RAM AIR DOOR ACTUATOR ACCESS DOOR EXT SKIN CORRODED 1 X 1 INCHES.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,771 hrs · 33,411 cycles

WEB CORROSION 1 X 1 INCHES.

Part: ATTACH ANGLE — CORRODED (LT WING) · corrosion level 3 · airframe 59,771 hrs · 33,411 cycles

LOWER SPAR CAP FWD ATTACH ANGLE FLANGE HAS CORROSION AT LEFT WING FSS 415.

Part: ANGLE — CRACKED (FUSELAGE) · corrosion level 3 · airframe 59,771 hrs · 33,411 cycles

AFT PRESSURE BULKHEAD UPPER ANGLE CRACKED 4 INCH CRACK.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,771 hrs · 33,411 cycles

STRINGER HAS CORROSION 8 INCHES.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,768 hrs · 33,411 cycles

AFT PRESSURE BULKHEAD HORIZONTAL STIFFENER CRACKED.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,771 hrs · 33,411 cycles

EXTERNAL FUSELAGE STA 610 RT WINDOW FRAME CORRODED 1 X 1 INCHES.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,771 hrs · 33,411 cycles

RT WINDOW FRAME CORROSION 1 X 1 INCHES.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,771 hrs · 33,411 cycles

SKIN HAS CREASE 1 X 1 INCHES.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,771 hrs · 33,411 cycles

SKIN HAS CREASE 1 X 1 INCHES.