N852FT

Part: WEB — CRACKED (NOSE WHEEL WELL) · airframe 86,527 hrs · 21,435 cycles

NOSE WHEEL WELL VERTICAL BEAM INSPECTION IAW MA A5310-33:01 REVEALED A CRACK AT STANDOFF HOLE 2-3/8" LONG AT VERTICAL BEAM STN 320 R/H SIDE, WEB 2. CRACK REPAIRED IAW SRM 51-40-02, PAGE5, DETAIL 111.

Part: WEB — CRACKED (NOSE WHEEL WELL) · airframe 86,527 hrs · 21,435 cycles

NOSE WHEEL WELL VERTICAL BEAM INSPECTION IAW MA A5310-33:01 REVEALED A CRACK 1-3/8" LONG AT WEB TO CHORD FASTENER LOCATION AT VERTICAL BEAM STN 320 R/H SIDE, WEB 2. REPAIRED IAW SRM 51-40-02, PAGE 5, DETAIL 111.

Part: PANEL — DELAMINATED (LT WING) · airframe 85,817 hrs · 21,275 cycles

LT WING PANEL AT L/E 4TH PANEL FROM FUSELAGE DELAMINATED. REMOVED AND REPLACED LT WING PANEL L/E 4TH FORM FUSELAGE AS PER SRM 51-30-02.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 65,460 hrs · 21,189 cycles

DELAMINATION FOUND ON RT WING INBOARD LOWER FLAP WBL 163. REPAIRED PER SRM 51-40-08.

Part: PANEL — DELAMINATED (LT WING) · airframe 85,460 hrs · 21,189 cycles

LT WING PANEL WBL 461 OF INBOARD AILERON HAS LOOSE FIBERGLASS. REPAIR CARRIED OUT IAW SRM 51-40-08.

Part: PANEL — DELAMINATED (RT WING) · airframe 85,460 hrs · 21,189 cycles

RT WING PANEL BEHIND NR 2 INBOARD SPOILER FIBERGLASS COMING LOOSE. FIBERGLASS PANEL REPAIRED PER SRM 51-40-08.

Part: FAIRING — DAMAGED (WING) · airframe 85,460 hrs · 21,189 cycles

DAMAGE FOUND ON NR 6 CANOE FIXED FAIRING WBL 353. FAIRING REPAIRED PER SRM 51-40-08.

Part: PANEL — DELAMINATED (RT WING) · airframe 85,460 hrs · 21,189 cycles

RT WING PANEL BEHIND NR 1 INBOARD SPOILER WBL 264 FIBERGLASS COWLING LOOSE. FIBERGLASS PANEL REPAIRED AS PER SRM 51-40-08.

Part: FAIRING — DAMAGED (WING) · airframe 85,460 hrs · 21,189 cycles

DAMAGE FOUND ON FIX FAIRING IN FRONT OF NR 6 CANOE. FAIRING REPAIRED PER SRM 51-40-08.

Part: PANEL — DELAMINATED (LT WING) · airframe 85,460 hrs · 21,189 cycles

LT WING PANEL ON L/EDGE OF FUSELAGE WBL 150 HAS LOOSE FIBERGLASS. REPAIRED CARRIED OUT PER SRM 51-40-08.

Part: PANEL — DELAMINATED (LT WING) · airframe 85,460 hrs · 21,189 cycles

LT WING PANEL THAT IS BEHIND FLYING PANEL HAS FIBERGLASS COMING LOOSE STA 197. REPAIRED CARREID OUT IAW SRM 51-40-08.

Part: PANEL — DELAMINATED (LT WING) · airframe 85,460 hrs · 21,189 cycles

LT PANEL DIRECTLY BEHIND FLYING PANEL LT WING WBL 197 HAS LOOSE FIBERGLASS. REPARIED CARRIED OUT IAW SRM 51-40-08.

Part: SKIN — DELAMINATED (MID FLAP) · airframe 85,353 hrs · 21,166 cycles

DELAMINATION FOUND ON LEFT O/B MID FLAP. REPAIRED PER PAO-LGB01-00045F.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 86,863 hrs · 21,510 cycles

EMERGENCY LIGHT IN CEILING AFT OF P6 PANEL ILLUMINATES ONLY MOMENTARILY. REPLACED EMERGENCY LIGHT AFT OF P6. OPS CHECK OK.

Part: BOLT — SHEARED (PYLON MOUNT) · airframe 84,021 hrs · 20,887 cycles

ON PYLONS NR 1, 3 AND 4, SHEARED .375 BOLTS ON HORIZONTAL FIRE WALL ADJACENT TO THE AFT MOUNT LUGS. BOLTS ARE VERTICAL THROUGH AFT MOUNT FITTING AND LOWER PYLON SKIRT CHORDS. REMOVED AND REPLACED ALL 8 BOLTS PER PYLON. REPLACED WITH OVERSIZED TO .4375 PER BOEING LETTER PAO-LGB-00-00006H. ACCOMPLISHED PHASE II HARD LANDING INSPECTON.

Part: TORQUE TUBE — DAMAGED (PAX DOOR) · airframe 83,917 hrs · 20,864 cycles

LEFT ENTRY DOOR LIGHT DR1 CAME ON DURING DESCENT AND REMAINED ON. DR1 LIGHT CAME ON AT APPROX 2.4 PSI DIF PRESS. REMOVED AND REPLACED LOWER TORQUE TUBE ASSY, PER MM 52-11-00, ADJUSTED DOOR WARNING LIGHT PER MM 52-17-00. OPS CHECK OK ON GROUND.

Part: PUSH ROD — FAILED (TE FLAP)

DURING WALK-AROUND INSPECTION, NR 3 FAIRING CANOE WAS FOUND PIERCED WITH FLAP PUSH ROD. ON INVESTIGATION AFTER DROPPING THE FLAPS (T/E), FOUND THE FLAP PUSH ROD HAD SHEARED ON THE FORWARD END. THE BROKEN PUSH ROD PIERCED THE FAIRING DURING FLAP RETRACTION. PRELIMINARY INSPECTION FOUND PUSH ROD ON NR 4 FAIRING ALSO DAMAGED. PUSH RODS REMOVED AND REPLACED PER PAC MM AND AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — FAILED (NR 1)

NR 1 ENGINE SHUT DOWN DUE TO STEADY STATE STALL AFTER DESCENDING FROM 370 TO 350. ATTEMPTED TO RESTART AT 350 AND 280, UNSUCCESSFUL. LAST START WAS AT 0050Z, WINDMILL TIME 1 HOUR AND 33 MIN. N1-30 PERCENT, N2-21 PERCENT, OIL PRESSURE 15 PSI, FL 280, IAS 295. INSPECTED FUEL FILTER, NO DEFECTS. CHECKED EVC AND CONDITION MOTOR, NO DEFECTS. GROUND START OPS CHECK GOOD. ALSO, COMPARED TO NR 4 ENG, ALL MATCH. OPS CHECK GOOD PER MM 73-23-00.

Part: SKIN — PUNCTURED (BS 2500)

CENTER AFT LOWER FUSELAGE APPROX STA 2500 FOUND HOLE. REPAIRED IAW SRM 53-30-03.

Part: SKIN — PUNCTURED (APU DOOR)

RT APU DOOR PUNCTURED BY WORK STAND DURING LIGHT WIND STORM. REPAIRED IAW SRM 52-40-02.

Part: PANEL — CRACKED (RT WING)

RIGHT WING FLYING PANEL CRACKED ON LOWER SIDE IN BOX AREA. REMOVED AND REPLACED FLYING PANEL PER MM 57-22-01.

Part: SKIN — DELAMINATED (NR 2 ENG COWL)

NR 2 ENGINE I/B FAN COWL UPPER AFT CORNER BENT AND DELAMINATED. REPAIRED IAW SRM 51-40-06.

Part: ENGINE — FAILED (NR 4 ENGINE)

AT FL 330 NR 4 ENGINE STALLED WITH AN AUDIBLE SOUND AND WENT TO A OVER TEMP OF 950Ý FOR 3-4 SECONDS. ENGINE WAS THEN SHUT DOWN, PER CHECK LIST. RELIGHT WAS ATTEMPED AT FL 240 BUT THE EGT WAS MUCH HIGHER AS ENGINE STARTED TO ACCELERATE. THE ENGINE WAS SHUT DOWN. FOUND METAL IN TAIL PIPE. ENGINE WAS CHANGED PER POLAR WORK CARD M7100-002 AND RUN PER M7100-O11.

Part: LOGIC MODULE — MALFUNCTION (LANDING GEAR)

FOLLOWING TAKEOFF HAD GEAR UP WARNING LIGHT AND AUDIBLE WARNING HORN. ALL LANDING GEAR WARNING LTS AT F/E STATION REMAINED ILL. RETURNED TO HKG. REPLACED LANDING GEAR LOGIC MODULE IAW MM 31-26-03. OPS CHECK OK.

Part: LOGIC BOX — MALFUNCTION (LANDING GEAR)

FOLLOWING T/O, RED GEAR LIGHT ON P2 WITH HORN. AIR TURN BACK. REPLACED LANDING GEAR LOGIC MODULE IAW MM 31-26-03, OPS CHECK OK.

Part: DECK — CORRODED (BS 1354)

LEVEL 1 CORROSION FOUND ON PRESSURE DECK SKIN BS 1354 BL 113 LEFT. REPAIRED PER REPAIR SCHEME R53-48-33819 AND 8110-03.

Part: LONGERON — CRACKED (BS 1480)

OVERWING LONGERON BULKHEAD FORGING AT BS 1480 STR 32-33R FOUND CRACK 6 INCHES LONG PLUS NUMEROUS MINOR BOLT HOLE CRACKS IN FITTINGS OF ASSOCIATED AREA. REPAIRED PER HAECO REPAIR SCHEME R53-43-33825 AND NUMEROUS 8110-3 FORMS AND BOEING SB 53A2390.

Part: FRAME — CRACKED (BS 960)

FRAME AT BS 960L STR 5 LEFT FOUND CRACKED. REPAIRED PER SRM 53-10-04 FIG 54.

Part: WEB — CORROSION (BS 1242)

LEVEL 1 CORROSION FOUND ON WING GEAR WHEEL WELL BS 1242 TO 1246 WL 155 RIGHT WEB. REPAIRED PER SRM 53-10-01 FIG 1.

Part: FRAME — CRACKED (BS 960)

FRAME CHORD AT BS 970 STR 8 AND 9 RIGHT FOUND CRACKS. REPAIRED FRAME PER SRM 53-10-04 FIG 54.

Part: SKIN — CRACKED (BS 360-520)

FOUND 65 LONGITUDINAL FASTENER HOLES IN SKIN CRACKED. REAMED OUT HOLES, HFEC, FREEZE PLUGS AND REPAIRED SKIN PER SRM 53-22-72.

Part: FRAME — CRACKED (BS 960)

FRAME AT BS 960 STR 5-6 RIGHT FOUND CRACKED. REPAIRED PER SRM 53-10-04 FIG 54.

Part: BULKHEAD SPLICE — CRACKED (BS 1480)

NUMEROUS BOLT HOLE CRACKS IN COMMON FITTINGS OF THE BODY STATION 1480 BULKHEAD LONGERON SPLICE. REPAIRED PER HAECO REPAIR SCHEME R53-61-33817 AND NUMEROUS 8110 REPORTS AND SB 53A2390.

Part: FRAME — CRACKED (BS 380)

FRAME STRUCTURES AT BS 380 LEFT STR 23-25R FOUND EXTENSIVE CRACKING LEFT AND RIGHT SIDES. REPLACED FRAME ASSY PER PAO-HKG 98-0140 AND HAECO RS 5312-23812 AND 8110-03.

Part: LONGERON — CORRODED (BS 1840-1860)

LEVEL 1 CORROSION FOUND ON LONGERON AT BS 1840 TO 1860 STR 45 LEFT. CORROSION REMOVED PER SRM 53-10-01.

Part: SEAT TRACK — CORRODED (BS 600)

LEVEL ONE CORROSION FOUND AT UPPER DECK RT SEAT TRACK, BS 600-710, WL 300, BL R46. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02 AND MM 51-24-11.

Part: SEAT TRACK — CORRODED (BS 600)

LEVEL ONE CORROSION FOUND AT UPPER DECK RT SEAT TRACK, BS 600-700, WL 300, BL R27. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02 AND 53-10-05.

Part: INTERCOSTAL — CRACKED (BS 380)

UPPER DECK BS 380-390 STR 7R INTERCOSTAL FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-10-01.

Part: SEAT TRACK — CORRODED (BS 600)

LEVEL ONE CORROSION FOUND AT CROWN AREA OF UPPER DECK LT SEAT TRACK, BS 600-700, WL 300. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02 AND 53-10-01.

Part: SKIN — CORRODED (BS 1725)

LEVEL ONE CORROSION FOUND AT MAIN DECK BS 1725 STR 12L LAP JOINT AREA. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 51-10-02, 53-30-01 AND MM 51-24-11.

Part: SEAT TRACK — CORRODED (BS 600)

LEVEL ONE CORROSION FOUND AT UPPER DECK LT SEAT TRACK CROWN AREA, BS 600-710, WL 300, LBL 46. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02 AND 53-10-05.

Part: SEAT TRACK — CORRODED (BS 600)

LEVEL ONE CORROSION FOUND AT UPPER DECK LT SEAT TRACK, BS 600-700, WL 300. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02, 53-10-01, AND MM 51-24-11.

Part: SEAT TRACK — CORRODED (BS 545-560)

LEVEL ONE CORROSION AND CRACK FOUND AT UPPER DECK RBL 23 SEAT TRACK OUTBOARD FLANGE, BS 545-560. CORROSION REMOVED, AREA REPAIRED AND REPROTECTED AS PER SRM 51-10-01, 51-10-02, AND 53-10-01.

Part: SKIN — CORRODED (BS 2200-2280)

LEVEL ONE CORROSION FOUND AT MAIN DECK CROWN BS 2200-2280 STR 4R LAP JOINT AREA. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 51-10-02 AND 53-30-01.

Part: SKIN — CORRODED (BS 1520)

LEVEL ONE CORROSION FOUND AT MAIN DECK BS 1520 SKIN, STRINGER 19L. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 51-10-02 AND 53-40-01.

Part: LONGERON — CRACKED (BS 1580)

MAIN DECK BS 1580 STR 5L FOUND CRACKED. REPAIRED AS PER SRM 53-10-03 AND MM 51-24-11.

Part: SEAT TRACK — CORRODED (BS 600)

LEVEL ONE CORROSION FOUND AT UPPER DECK LT SEAT TRACK CROWN SURFACE, BS 600-710, WL 300. CORROSION REMOVED AND SEAT TRACK REPLACED AS PER SRM 51-10-01, 53-10-01, 53-10-05 AND MM 51-24-11.

Part: INTERCOSTAL — CRACKED (BS 380)

UPPER DECK BS 380-390 S5R-6R INTERCOSTAL FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-10-01.

Part: LONGERON — CRACKED (BS 1495)

MAIN DECK BS 1495 STR 2L FOUND CRACKED. REPAIRED AS PER SRM 53-10-03 FIGURE 5.

Part: SEAT TRACK — CORRODED (BS 600)

LEVEL ONE CORROSIN FOUND AT UPPER DECK RT SEAT TRACK, BS 600-710, WL 300, RBL 64. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02 AND 53-10-01.

Part: STRINGER — CORRODED (BS 1625)

LEVEL ONE CORROSION FOUND BS 1625 STRINGER 2L. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 51-10-02, AND 53-10-01.

Part: SKIN — CORRODED (BS 1800-1960)

LEVEL 1 CORROSION FOUND BS 1800-1960 STR 12R LAP JOINT. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND MM 51-24-11.

Part: SKIN — CORRODED (BS 1960)

LEVEL 1 CORROSION FOUND AT BS 1960 STR 12R LAP JOINT. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND MM 51-24-11.

Part: STRINGER — CORRODED (BS 1565)

LEVEL 1 CORROSION FOUND AT BS 1565 STR 12L. REPAIRED CORROSION AND REPROTECTED PER SRM 51-10-01, 53-10-01 AND 51-10-02.

Part: SKIN — CORRODED (BS 1740)

LEVEL 1 CORROSION FOUND AT BS 1740 STR 19R LAP JOINT. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND 53-30-01.

Part: STRINGER — CORRODED (BS 1620)

LEVEL ONE CORROSION FOUND AT BS 1620 STR 1R. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 51-10-02 AND MM 51-24-11.

Part: SHEAR TIE — CORRODED (BS 1580)

LEVEL ONE CORROSION FOUND MAIN DECK BS 1580 SHEAR TIE AFT FACE, BETWEEN S4R AND S7R. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 53-10-01, 51-10-02.

Part: SKIN — CORRODED (BS 1620)

LEVEL ONE CORROSION FOUND AT LAP JOINT AREA OF STR 12R, BS 1620-1640. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 53-30-01 AND 51-10-02.

Part: SKIN — CORRODED (BS 1740)

LEVEL ONE CORROSION FOUND AT MAIN DECK BS 1740-1820 STR 4R LAP JOINT. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 51-10-02 AND 53-30-01.

Part: SKIN — CORRODED (BS 1740-1820)

LEVEL 1 CORROSION FOUND AT BS1740-18820 STR 12R LAP JOINT. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND MM 51-24-11.

Part: SKIN — CORRODED (BS 1520)

LEVEL 1 CORROSION FOUND AT BS 1520R STR 12R LAP JOINT. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01, 53-30-01 AND 51-10-02.

Part: CLIP — CORRODED (BS 1580)

LEVEL ONE CORROSION FOUND ON TIE CLIP BS 1580, STR 3L. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 53-10-02.

Part: TRUNNION — CRACKED (NLG)

NOSE GEAR TRUNNION FITTING FWD CUTOUT WEB CRACKED LEFT AND RIGHT SIDES. REPAIRED PER SB 53-2293 REPAIR.

Part: SKIN — CORRODED (BS 2258)

LEVEL 1 CORROSION ON MAIN DECK CROWN SKIN BS 2258 S2R. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND MM 51-24-11.

Part: STRINGER — CRACKED (BS 1580)

MAIN DECK BS 1580 STRINGER 5R CRACK FOUND. REPAIRED PER SRM 53-10-03.

Part: STRINGER — CORRODED (BS 1960-2180)

LEVEL 1 CORROSION FOUND AT STRINGER 12R FROM STA 1960 TO 1280 RIGHT LAP JOINT. CORROSION REMOVED AND REPROTECTED AREA PER SRM 51-10-01, 51-10-02 AND MM 51-24-11.

Part: STRINGER — CORRODED (BS 2120)

LEVEL 1 CORROSION FOUND AT BS 2120 STR 2L. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND 51-24-11.

Part: SKIN — CORRODED (BS 2180-2200)

LEVEL 1 CORROSION FOUND ON MAIN DECK CROWN BS 2180-2200 STR 12R LAP JOINT. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND 53-30-01.

Part: STRINGER — CORRODED (BS 2080-2160)

LEVEL 1 CORROSION FOUND ON MAIN DECK BS 2080-2160 STR 4L LAP JOINT AREA. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01, 51-10-02, 53-30-01.

Part: SKIN — CORRODED (BS 1940-1960)

LEVEL 1 CORROSION FOUND AT MAIN DECK CROWN BS 1940-1960 STR 4R LAP JOINT SEALANT AREA. REMOVED CORROSION AND REPROTECTED.

Part: SKIN — CORRODED (BS 1960-2180)

LEVEL 1 CORROSION FOUND FROM BS 1960-2180 STRINGER 19L LAP JOINT. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND 53-30-01.

Part: SKIN — CORRODED (BS 1650)

LEVEL 1 CORROSION FOUND ON MAIN DECK BS 1650 12L LAP JOINT. CORROSION REMOVED AND REPROTECTED PER SRM 53-30-01, 52-10-01, 53-10-02.

Part: FRAME — CRACKED (BS 600)

BS 600 RT BODY FRAME RADIUS FOUND CRACKED. REPAIRED FRAME PER RS5322-33811, SRM 51-10-01, 51-30-02.

Part: SKIN — CORRSODED (BS 2020-2180)

LEVEL 1 CORROSION FOUND AT SKIN LAP JOINT AREA BS 2020-2180 STR 4R. REMOVED CORROSION, BLENDED AND REPROTECTED PER SRM 51-10-01, 53-30-01, 51-10-02 AND MM 51-24-11.

Part: KEEL BEAM — CORROSION (BS 1220)

LEVEL 1 CORROSION FOUND ON KEEL BEAM LOWER WEB BS 1220-40 BL R9-L9. REMOVED AND BLENDED CORROSION SURFACE PER SRM 51-10-01, 51-10-02 AND 51-24-11.

Part: SKIN — CORRODED (BS 1960-2220)

LEVEL 1 CORROSION FOUND AT SKIN LAP JOINT BS 1960-2220 STR 12L. CLEANED CORROSION, BLENDED AREA AND REPROTECTED PER SRM 51-10-01, 53-30-01, 51-10-02 AND MM 51-24-11.

Part: STRINGER — CORRODED (BS 1960-2180)

LEVEL 1 CORROSION FOUND ON STRINGER 19R FROM BS 1960-2180 AT LAP JOINT AREA. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01, 51-10-02, 51-24-11.

Part: KEEL BEAM — CORROSION (BS 1240-1260)

LEVEL 1 CORROSION ON RIVET HEADS ON KEEL BEAM AT BS 1240 TO 1260. REMOVED CORROSION, BLENDED AREA AND TREATED SURFACE PER SRM 51-10-01, 51-10-02 AND 51-24-11.

Part: STRINGER — CORRODED (BS 2100)

LEVEL 1 CORROSION FOUND AT BS 2100 STR 3L. REMOVED CORROSION, BLENDED AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND MM 51-24-11.

Part: STRINGER — CORRODED (BS 2080)

LEVEL 1 CORROSION FOUND AT BS 2080 STR 2L. REMOVED CORROSION AND RETREATED AREA PER SRM 51-10-01, 51-10-02 AND MM 51-24-11.

Part: STRINGER — CORRODED (BS 2060)

LEVEL 1 CORROSION STRINGER L1. REMOVED CORROSION AND BLENDED AREA AND RETREATED PER SRM 51-10-01, 51-10-02 AND MM 51-24-04.

Part: STRINGER — CORRODED (BS 1960)

LEVEL 1 CORROSION FOUND AT MAIN DECK BS1960 STRINGER R12. BLENDED OUT AND REMOVED CORROSION PER SRM 51-10-02 AND 51-24-11.

Part: STRINGER — CORRODED (BS 2100)

LEVEL 1 CORROSION AT BS 2100 STR 3L. REMOVED CORROSION AND BLENDED AREA AND REPROTECTED PER SRM 51-10-01, 53-10-01 AND 51-10-02.

Part: FAIRING — DELAMINATED (NR 3 PYLON)

NR 3 PYLON NAC STA 320 SAIL BOAT RT FAIRING 474D HAS OUTER SKIN DELAMINATION. HOT BOND REPAIR PER SRM 51-40-06 FIG 13.

Part: FRAME — CRACKED (BS 820)

BS 820 STR 3L BODY FRAME RADIUS CRACKED. REPAIRED PER SRM 53-10-04.

Part: SKIN — CORRODED (RT MLG WW)

LEVEL 1 CORROSION RT BODY GEAR WHEEL WELL SKIN WEB. REMOVED CORROSION AND REPROTECTED PER SRM 51-40-02 FIG 1.

Part: PANEL — CORRODED (BS 1040)

AIR CONDITIONING PANEL BS 1040 BL 10-30 HAS CORRSOION. CORROSION REMOVED AND SURFACE REPROTECTED PER SRM 51-10-00 AND 51-10-02.

Part: BRACKET — CRACKED (BS 1500)

SUPPORT BRACKET AT BS 1500 STR 21-22 RIGHT FOUND CRACKED. REPLACED SUPPORT BRACKET PER SRM 51-10-01.

Part: FRAME — CRACKED (BS 780)

MAIN DECK BODY FRAME RADIUS FOUND CRACKED AT STR 6L BS 780. REPAIRED BODY FRAME PER SRM 53-10-04 FIG 54.

Part: PANEL — CORRODED (KEEL BEAM)

KEEL BEAM ACCESS PANEL 191KK REAR ATTACH SUPPORT LOWER CHORD HAS SURFACE CORROSION. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — CORRODED (RT WING)

LEVEL 1 CORROSION ON RT WING UPPER WING SKIN SURFACE FORWARD AND OUTBOARD OF NR 7 SPOILER. REMOVED, PEENED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — CORROSION (BS 800-840)

LEVEL 1 CORROSION ON FUSLEAGE SKIN STA 800-840 BELLY STR 44L-44R. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AND SRM 51-10-02.

Part: SKIN — CORRODED (BS 530&570)

LEVEL 1 CORROSION ON FUSELAGE SKIN STA 530 AND 570 BELOW VHF ANTENNA. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — CORRODED (BS 740)

LEVEL 1 CORROSION ON FUSELAGE SKIN STA 740 STR 42-44R. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND SRM 51-10-02.

Part: FLOOR — CRACKED (BS 2020)

BULK CARGO BS2020 LBL 48 AND 52 FLOOR PANEL SUPT HAT SECTION CRACKED. REPAIRED PER SRM 51-40-03.

Part: CONTROL CARD — OVERHEATED (COCKPIT)

APPROXIMATELY 6 HOURS INTO FLIGHT HAD STRONG ODOR OF ELECTRICAL COMPONENTS OVER HEATING/BURNING. ALSO, HAD VISIBLE SMOKE HAZE. RAN SMOKE SOURCE AND ELECTRICAL FIRE CHECKLIST. CREW USED OXYGEN ODOR DISSIPATED AFTER 20 TO 30 MINUTES. FOUND WING ANTI-ICE CONTROL CARD AND RELAY WITH EVIDENCE OF OVERHEAT/BURNING. REPLACED RELAY AND CONTROL CARD OPERATIONAL CHECK NORMAL PER M/M 36-11-00 AND 24-00-00. ALSO, REPLACED A1, A8, A10, A13, AND A17 MASTER DIMMER CONTROL CARDS DUE TO SIGNS OF OVERHEATING PER M/M 33-12-00.

Part: ENGINE — MALFUNCTIONED (NR 2)

ON LANDING, NR 2 ENGINE OIL PRESSURE LIGHT CAME ON, EGT ROSE IMMEDIATELY. SHUT DOWN ENGINE. EGT WAS 938 DEGREES PER M/M 71-00-00 PAGE 216 AREA B OVER TEMPERATURE. ACCOMPLISHED VISUAL INSPECTION PER M/M 72-00-00, M/M 72-00-43 PAGE 115, 71-00-42, 71-00-46 AND 78-34-08. NO DISCREPANCIES NOTED. SUSPECT STALL IN REVERSE PLACARDED THRUST REVERSER PRECAUTIONARY. AIRCRAFT SCHEDULED FOR BORESCOPE WITHIN 80 HOURS.

Part: O-RING — CUT (NR 3 OIL FILTER)

LOW OIL QUANTITY INFLIGHT DOWN TO 1.06 GALS. PRECAUTIONARY SHUT-DOWN. FOUND O-RING FOR MAIN OIL FILTER DAMAGED. REPLACED O-RING RAN ENG AFTER OIL SERVICING, NO LEAKS FOUND. RESERVICED ENGINE AFTER RUN TO TOTAL OF 28 QTS PER MM REF 72-61-05.

Part: FAIRING — CORROSION (LOWER BODY)

FUSELAGE LOWER BODY FAIRING PANEL HAS CORROSION. REMOVED CORROSION, APPLIED FILLER, APPLIED CONDUCTIVE COATING, PRIMED AND PAINTED PER SRM 51-10-01, 51-40-08, 51-24-17.

Part: SKIN — DAMAGED (RT AILERON)

RT OUTBD AILERON UPPER SURFACE OUTBD HAS SPEED TAPE REPAIR. REMOVED DAMAGED FIBERGLASS SKIN, REPAIRED SAME USING OVERLAYS AND FILLERS. PRIMED AND PAINTED PER SRM 51-40-07 AND 51-24-11.

Part: PANEL — DELAMINATION (VERT STAB)

COMP PANEL NR 324L ON LT SIDE OF VERTICAL STAB HAS 3 AREAS OF DELAMINATION. FABRICATED NEW PANEL MATERIAL, CUT NEW CORE, HOT BONDED CORE TO MATERIAL, CURED, TRIMMED TO FIT, PRIMED PER SRM 51-40-06.

Part: SKIN — DISBONDED (NR 10 SPOILER)

SPOILER RT WING HAS LARGE DISBONDED REPAIR TO UPPER SURFACE. REMOVED AND REPLACED NR 10 SPOILER PANEL PER MM 27-61-02.

Part: PANEL — DISBONDED (RT WING)

RT WING UPPER SURFACE PANEL DISBONDED. REMOVED DAMAGED CHECKED FOR MOISTURE. DID FIBERGLASS OVERLAYS AND FILLERS PRIMED AND PAINTED PER SRM 51-40-07 AND 51-24-11.

Part: PANEL — CRACKED (LT TE MIDFLAP)

LT INBD MIDFLAP COVE LIP PANEL AT OUTBOARD END CRACKED. STOP DRILLED CRACK/INSTALLED FIBERGLASS OVERLAYS PRIMED AND PAINTED PER SRM 51-40-15 AND 51-24-11.

Part: SPOILER — DELAMINATION (NR 4 SPOILER)

NR 4 SPOILER LT WING LOWER SURFACE HAS DELAMINATION. REMOVED AND REPLACED NR 4 SPOILER PANEL PER MM 27-61-02.

Part: PANEL — CORROSION (NR 8 SPOILER)

NR 8 SPOILER RT HAS CORROSION A BOTH INBD AND OUTBD SEALS. REMOVED AND REPLACED NR 8 SPOILER PANEL PER MM 27-61-01.

Part: PANEL — DISBONDED (NR 6 SPOILER)

NR 6 SPOILER LT WING LOWER SURFACE HAS DISBONDED AREA. CUTOUT DAMAGED AREA, REPLACED CORE, FABRICATED FILLER AND DOUBLER BONDED, CURED, SEALED, PRIMED AND PAINTED PER SRM 51-40-06 AND 51-24-11.

Part: SKIN — DELAMINATED (LT LE FLAP)

LT INBOARD FOREFLAP L/E OUTBD SIDE DELAMINATED. REPAIRED DELAMINATION PER SRM 51-40-11 AND 51-24-11.

Part: MOUNT BOLT — LOOSE (NR 4 ENGINE)

NR 4 PYLON FWD MOUNT INBD BOLT WASHER ON HEAD SIDE LOOSE. REMOVED WEIGHT OF ENGINE FROM FWD MOUNT. RETORQUED LOOSE BOLD PER MM 71-21-01.

Part: PANEL — DAMAGE (RT WING)

RT WING GEAR FLYING PANEL AFT CORNER HAS DAMAGE. REMOVED DAMAGED AREA, APPLIED FIBERGLASS FILLERS AND OVERLAYS, APPLIED CONDUCTIVE COATING PER SRM 51-40-11 AND 51-24-11.

Part: SPOILER — DELAMINATION (NR 1 SPOILER)

NR 1 SPOILER LT WING LWR SURFACE HAS DELAMINATION. CUTOUT DAMAGED AREA AND REPAIRED PER SRM 57-50-00 AND 51-24-11 AND MM 27-61-02.

Part: PANEL — CRACKED (LT TE MIDFLAP)

LT INBD MIDFLAP COVE LIP PANEL AT OUTBD END CRACKED. STOP DRILLED CRACK/INSTALLED FIBERGLASS OVERLAYS PRIMED AND PAINTED PER SRM 51-40-15 AND 51-24-11.

Part: CHECK VALVE — CRACKED (NR 2 PYLON)

ON LANDING GROUND SAW SMOKE AND POSSIBLE FLAMES COMING FROM NR 2 ENGINE AT SAME TIME LOST QUANTITY FROM NR 2 HYDRAULIC SYSTEM. NO WARNING FROM FIRE DETECTION EQUIPMENT OR OTHER ABNORMAL ENGINE READINGS. FOUND CHECK VALVE ON NR 2 HYDRAULIC MODULE CRACKED. REPLACED PER BOEING M/M 29-11-23.

Part: WINDSHIELD — CRACKED (COCKPIT)

CAPTIANS FORWARD WINDSHIELD CRACKED IN FLIGHT. REPLACED WINDOW PER M/M 56-11-01, LEAK CHECK GOOD.

Part: CANOE — DAMAGED (NR 6 TE FLAP)

ON POST FLIGHT, FOUND EXTENSIVE DAMAGE TO NR 6 CANOE. CANOE REMOVED AND TRANSFERED TO DMI LOG FOR FERRY FLIGHT. CANOE REPLACED PER M/M 27-51-02.

Part: FLAP — OUT OF ADJUST (RT TE FLAP)

ON POST FLIGHT, FOUND RIGHT INBOARD AFT TRAILING EDGE FLAP MISALIGNED (NOT STOWED PROPERLY). REPAIRED RIGHT INBOARD TRAILING EDGE FLAP PER MA5750-02:01. RIG AND OPERATIONAL CHECK PER M/M 27-51-39.

Part: TORQUE LINK — BROKEN (LT WING)

ON POST FLIGHT INSPECTION, FOUND BROKEN TORQUE LINK HAD PUNTURED THROUGH THE RIGHT SIDE OF NR 3 CANOE. REMOVED AND REPLACED TORQUE LINK ASSY PER M/M 27-51-26. REPAIRED CANOE PER POLAR MA5750-08:01 AND SRM 51-40-09.

Part: SKIN — DAMAGED (TE FLAP)

ON POST FLIGHT, FOUND AFT TRAILING EDGE FLAP UNDER INBOARD AILERON DAMAGED. REPAIRED PER MA5750-08:01 AND BOEING SRM 51-40-09.

Part: SKIN — PUNCTURED (NR 5 TE FLAP)

ON POST FLIGHT INSPECTION FOUND HOLE IN NR 5 FLAP. REPAIRED PER MA5750-08:01 AND SRM 51-40-09.

Part: FITTING — CORRODED (LT MLG)

LEVEL 2 CORROSION ON LEFT WING LANDING GEAR H FITTING. REPLACED H FITTING AND GLAND NUT PER BAC MM 57-43-01.

Part: LINK — BROKEN (RT LE FLAP)

BROKEN NR 17 LEADING EDGE FLAP (RIGHT SIDE) BULLNOSE DRIVE LINK. REPLACED LINK PER BAC MM 27-81-07.

Part: PRECOOLER — CRACKED (NR 4 ENGINE)

CRACK ON NR 4 ENGINE PRECOOLER. WELDED PRECOOLER PER BAC PROCESS 5975.

Part: PRECOOLER — CRACKED (NR 3 ENGINE)

CRACK ON NR 3 ENGINE PRECOOLER. WELDED PRECOOLER PER BAC PROCESS 5975.

Part: STRINGER — CRACKED (FUSELAGE)

CRACKED STRINGER CAUSED BY SKIN DENT ON FORWARD FUSELAGE 18 INCHES AFT OF RADOME AT 6 O'CLOCK. REPAIRED WITH FABRICATED STRINGER SPLICE AND SKIN PATCH PER BAC SRM 53-30-03 AND 53-30-01.

Part: FLANGE — CRACKED (NR 2 ENGINE)

CRACKED R FLANGE (RAIL) ON NR 2 ENGINE TURBINE EXHAUST CASE. WELDED AND STRESS RELIEVED CRACK PER PWA ENGINE MANUAL 72-53-01.

Part: PNEUMATIC DUCT — CRACKED (BS 1540)

CRACKED APU PNEUMATIC SUPPLY DUCT IN LOWER AFT CARGO COMPARTMENT AT STA 1540. REPLACED PNEUMATIC DUCT PAR BAC MM 36-11-01.

Part: SKIN — DENTED (FUSELAGE)

SKIN DENTED WITH CREASES IN SEVERAL PLACES ON THE LEFT AFT FUSELAGE AFT OF L5 DOOR. FABRICATED AND INSTALLED SKIN DOUBLERS PER BAC SRM 53-30-03.

Part: PNEUMATIC DUCT — CRACKED (NR 4 PYLON)

CRACKED PNEUMATIC DUCT IN NR 4 PYLON FOR NR 4 AIR DRIVEN HYDRAULIC PUMP TURBINE DRIVE. WELD REPAIRED AND PRESSURE TESTED DUCT PER BAC PROCESS 5975.

Part: DUCT — CRACKED (RT WING)

CRACKED NR 4 RIGHT LEADING EDGE DRIVE UNIT PNEUMATIC SUPPLY DUCT. REPLACED DUCT PER BAC MM 36-11-00.

Part: T-CHORD — CRACKED (NLG WW)

CRACKED NOSE WHEEL WELL FORWARD BULKHEAD LEFT T CHORD. FABRICATED AND INSTALLED T CHORD PER BAC SRM 51-30-02.

Part: ACTUATOR — FAILED (RUDDER)

FAILURE OF LOWER RUDDER ACTUATOR FILTER HOUSING DURING ENGINE START CAUSED COMPLETE NR 2 HYDRAULIC SYSTEM FLUID LOSS. REPLACED LOWER RUDDER ACTUATOR PER BAC MM 27-21-16.

Part: OVERHEAT WIRE — SHORTED (LT WING)

INTERMITTENT LEFT WING OVERHEAT LIGHT ON. ISOLATION VALVE AND ENGINES 1 AND 2 BLEED VALVES CLOSED. FOUND WIRE W640-1W728-18R SHORTED, REPAIRED WIRING PER BAC WDM AND OPS CHECK PERFORMED IN CONJUNCTION WITH HIGH POWER ENGINE RUN OPS NOW NORMAL. CLEARED DEFERAL NOTED IN REPORT P5CA9701389.

Part: PRBC — FAILED (NR 1 ENGINE)

ABORTED TAKEOFF AT LOW SPEED 100 KIAS, UNABLE TO MAINTAIN TAKEOFF POWER AT 1.43 ON NR 1 ENGINE WITHOUT EXCEEDING MAX EGT, EGT AT 932 DEGREES FOR 14 SECONDS. VISUALLY INSPECTED ENGINE AND PERFORMED BORESCOPE PER BAC MM 72-50-0, NO ABNORMAL CONDITIONS. DURING RUN CHECK FOUND NO ENGINE BLEED CLOSURE. REPLACED PRESSURE RATIO BLEED CONTROLLER PER BAC MM 75-32-01, FUEL/AIR CONVERTER VALVE PER BAC MM 75-32-02.

Part: OVERHEAT WIRE — SHORTED (LT WING LE)

OVERHEAT WARNING LIGHT FOR LEFT WING ON IN FLIGHT, LEFT WING ISOLATION VALVE AND ENGINES 1 AND 2 BLEED VALVES CLOSED AND LIGHT OFF. FOUND WING OVERHEAT SENSOR S1052 DAMAGED. DEACTIVATED AND DEFERED S 1052 PER MEL 26-22-1A.

Part: DUCT — LEAKING (LT WING)

IN CRUISE FL 290 LEFT WING OVERHEAT LIGHT ILLUMINATED, COMPLIED WITH WING OVERHEAT PROCEDURE ISOLATED LEFT WING AND NR 1 AND NR 2 ENGINES WITH PYLON VALVES LIGHT WENT OUT. RETURNED THRUST TO NORMAL, LIGHT STAYED OUT. FOUND PNEUMATIC LEAK 1 FOOT INBOARD OF NR 4 LEFT LEADING EDGE DEVICE LEAK WAS BLOWING AIR ON OVERHEAT SWITCH. RESEALED DUCT AND LEAK CHECKED PER M/M 36-11-01 AND 36-11-00.

Part: OVERHEAT SWITCH — OUT OF POSITION (LT WING)

LEFT WING LEADING EDGE OVERHEAT LIGHT FLICKERED INTERMITTENTLY, WING BLEED ISOLATED, LIGHT CONTINUED TO FLICKER. FOUND S-898 LEADING EDGE OVERHEAT SWITCH TOUCHING STRUCTURE CORRECTED SWITCH POSITION TO NORMAL TESTED PER M/M 26-18-00. ALSO, CHECKED FOR PNEUMATIC LEAKS AND NO LEAKS NOTED.

Part: COWL — CRACKED (NR 1 ENGINE)

CRACK FOUND BELOW CSD DOOR NR 1 OUTBD CORE COWL. REPAIRED PER BOEING SRM 51-10-02.

Part: COWL — CRACKED (NR 2 ENGINE)

NR 2 RT CORE COWL LWR AFT FLANGE CRACKED. REPAIRED PER BOEING SRM 54-30-01.

Part: COWL — CRACKED (NR 3 ENGINE)

FOUND CRACK AT NR 3 ENGINE INBD CORE COWL COVER. REPAIRED PER BOEING SRM 53-30-01.

Part: COWL RIB — CRACKED (NR 4 ENGINE)

NR 4 ENGINE INBD CORE COWL NR 3 RIB CRACKED. REPAIRED PER BOEING SRM 54-10-03 AND 54-14-03.

Part: OUTER CASE — DAMAGED (NR 3 ENGINE)

NR 3 ENGINE OUTER CASE AT 11 O'CLOCK POSITION DAMAGED. REPAIRED PER BOEING SRM 51-40-02, 852F.

Part: SKIN — DELAMINATED (LT TE FOREFLAP)

A HOLE WAS FOUND L/OUTBD FOREFLAP OUTBD END. REPAIRED PER BOEING SRM 51-01-14 AND PAINTED PER BOEING 51-24-11.

Part: LATCH — CORRODED (CARGO DOOR)

LEVEL 2 - CORROSION AFT CARGO DOOR NR 7 LATCH IS PITTING. REMOVED AND REPLACED LATCH ASSY PER MM 52-34-01.

Part: FLYING DOOR — CRACKED (LT MLG)

CRACK FOUND L/WING GEAR, FLYING DOOR. REPAIRED PER BOEING SRM 51-40-09.

Part: COWL ANGLE — CRACKED (NR 2 ENGINE)

CRACK FOUND AT NR 2 CORE COWL, HOOK ANGLE. REPAIRED PER BOEING SRM 51-10-02.

Part: SEAL — TORN (RT HORIZ STAB)

RT HORIZONTAL STABILIZER PANEL SEAL TORN ALONG EDGE. REPAIRED PER BOEING SRM 51-24-11.

Part: SKIN — DELAMINATED (RT AILERON)

RT WING, INBD AILERON DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — DELAMINATED (RT TE FOREFLAP)

HOLE FOUND R/OUTBD FOREFLAP. REPAIRED PER BOEING SRM 57-51-05.

Part: COWL — CHAFED (NR 1 ENGINE)

NR 1 ENGINE OTB CORE COWL 3 RIBS CHAFED. REPAIRED PER BOEING SRM 53-30-01, PAINTED PER BOEING SRM 51-10-02.

Part: ANGLE — CRACKED (NR 4 PYLON)

CRACK FOUND #4 DOGHOUSE - AFT R/H INNER ATTACH ANGLE. REPAIRED PER BOEING SRM 54-12-03.

Part: INNER COVER — TORN (CARGO DOOR)

AFT CARGO DOOR, AFT PRESSURE RELIEF DOOR, INNER COVER TORN. REPAIRED PER BOEING SRM 51-40-09.

Part: COWL RIB — CRACKED (NR 2 ENGINE)

CRACK FOUND NR 2 ENGINE O/BD CORE COWL RIB. REPAIRED PER BOEING SRM 53-10-01.

Part: SKIN — CRACKED (NR 4 PYLON)

CRACKS FOUND AT NR 4 DOGHOUSE, AFT R/S SKIN. REPAIRED PER BOEING SRM 54-32-03.

Part: PULLEY COVER — CRACKED (NLG STEERING)

CRACK FOUND NOSE GEAR PULLEY COVER. REPAIRED PER BOEING SRM 51-40-09.

Part: 'R' RAIL — CRACKED (NR 2 ENGINE)

NR 2 ENGINE 'R' RAIL CRACKED. REPAIRED, WELD IAW 72-53-01 AND 70-42-04.

Part: EXHAUST CASE — DAMAGED (NR 2 ENGINE)

NR 2 EXHAUST CASE DAMAGED AT 3 O'CLOCK POSITION. REPAIRED PER BOEING SRM 51-10-01.

Part: COWL — CRACKED (NR 2 ENGINE)

CRACK FOUND AT NR 2 INBD CORE COWL LWR END. REPAIRED PER BOEING SRM 54-10-03.

Part: SKIN — DELAMINATED (RT HORIZ STAB)

A HOLE WAS FOUND R/HORIZONTAL STABILIZER. REPAIRED PER BOEING SRM 51-40-06.

Part: FITTING — CRACKED (NR 2 SPOILER ACT)

CRACK FOUND AT NR 2 SPOILER ACTUATOR SUPPORT FITTING. REMOVED AND REPLACED PER MM 27-61-02, OPS CK 27-61-00.

Part: COWL — DELAMINATED (NR 3 ENGINE)

NR 3 NOSE COWL ASSY DELAMINATED 7 O'CLOCK POSITION. REPAIRED PER BOEING SRM 51-40-05.

Part: CAM ROLLER — TWISTED (PAX DOOR)

L-1 DOOR LIGHT ON IN FLIGHT, COMPLIED WITH ALTERNATE PROCEDURE. FOUND UPPER AND LOWER CAM ROLLERS SHEARED. ALSO, FOUND THE AFT NR 3 DOOR STOP CRACKED. REMOVED AND REPLACED CAM ROLLERS AND DOOR STOP PER MAINTENANCE MANUAL 52-11-01.

Part: S RAIL — CRACKED (NR 2 ENGINE)

NR 2 ENGINE S-RAIL CRACKED 3 PLACES. REMOVED ENGINE FOR EXHAUST CASE REPLACEMENT PER POLAR AIR CARGO WORK CARD M7100-002.

Part: ENGINE — FAILED (NR 4)

AT 08:57 Z FLIGHT LEVEL 29,700, NR 4 ENGINE COMPRESSOR STALLED EGT WENT TO 908 DEGREES CELSIUS AND ALL OTHER PARAMATERS REMAINED NORMAL. SHUT DOWN NR 4 ENGINE I/A/W POLAR PROCEDURE. FOUND METAL IN TAIL PIPE. ENGINE REPLACED PER POLAR AIR CARGO FORM M7100-002.

Part: SENSOR ACTUATOR — WRONG PART (RT MLG)

AFTER TAKEOFF AND GEAR RETRACTION WITH GEAR LEVER OFF, LANDING GEAR LEVER LATCH REMAINED IN VIEW. RIGHT WING LANDING GEAR TILT ANNUNCIATOR INDICATED PRI. AND ALT TILT AMBER LIGHTS ILLUMINATED. FOUND THE RIGHT WING LANDING GEAR TRUCK POSITION SENSOR ACTUATOR TO BE THE WRONG PART. REPLACED SENSOR ACTUATOR AND ADJUSTED PER BOEING MAINTENANCE MANUAL 32-61-04 PAGE 207 RETRACTED PER 32-32-00, OPS CHECK NORMAL.

Part: DOOR — CORRODED (RT MLG)

LEVEL 1 CORROSION ON RIGHT BODY LANDING GEAR INBOARD AND OUTBOARD DOORS. REMOVED CORROSION PER BOEING SRM 51-10-01.

Part: SUPPORT — CORRODED (BS 1260-1460)

LEVEL 1 CORROSION FOUND ON KEEL BEAM SUPPORT STRUCTURE BETWEEN BS 1260 AND BS 1460. BLENDED OUT CORROSION PER BOEING SRM 51-10-01.

Part: KEEL BEAM — CORRODED (BS 1260-1480)

MINOR CORROSION FOUND ON KEEL BEAM SUPPORT STRUCTURE BETWEEN STA 1260 TO 1480. BLENDED OUT CORROSION, FOUND TO BE WITHIN LIMITS IAW SRM 51-10-01, REPROTECTED AREA.

Part: ANGLE — CORRODED (BS 1760)

LEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1760 BETWEEN S51L AND S50L. CORROSION REMOVED PER BAC SRM 53-10-04, FIGURE 3.

Part: TRUNNION — CORRODED (LT MLG)

REMOVED LEFT WING LANDING GEAR OUTER CYLINDER AFT TRUNNION SLEEVE TO CONFIRM SERVICE BULLETIN 32-2190 MODIFICATION STATUS. FOUND AFT TRUNNION WITH DEEP PITTING CORROSION. REWORKED PER DOWTY WORK ORDER NR 101000-1-1 AND OVERHAUL MANUAL 32-11-41.

Part: ANGLE — CORRODED (BS 1800)

LEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1800 BETWEEN S51L AND S50L. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.

Part: ANGLE — CORRODED (BS 1800)

LEVEL 2 CORROSION SHEAR ANGLE BS 1800 BETWEEN S51L AND S51R AT BL ZERO. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.

Part: SHEAR ANGLE — CORRODED (BS 1760)

LEVEL 1 CORROSION ON SHEAR ANGLE AT BS 1760 AT BL 0 BETWEEN S51R AND S51L. CORROSION REMOVED PER BAC SRM 53-10-04, FIGURE 3.

Part: ANGLE — CORRODED (BS 1760)

LEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1760 BETWEEN S49L AND S48L. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.

Part: ANGLE — CORRODED (BS 1920)

LEVEL 2 CORROSION SHEAR ANGLE BS 1920 BETWEEN S51L AND S51R AT BL ZERO. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.

Part: ANGLE — CORRODED (BS 1660)

LEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1660 BETWEEN S47R AND S48R. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.

Part: ANGLE — CORRODED (BS 1880)

LEVEL 2 CORROSION SHEAR ANGLE BS 1880 BETWEEN S51L AND S51R AT BL ZERO. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.

Part: ANGLE — CORRODED (BS 1820)

LEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1820, BETWEEN S51R AND S50R. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.

Part: ANGLE — CORRODED (BS 1820)

LEVEL 2 CORROSION SHEAR ANGLE BS 1820 BETWEEN S51R AND S50R. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.

Part: ANGLE — CORRODED (BS 1820)

LEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1820, BETWEEN S50L AND S49L. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.

Part: ANGLE — CORRODED (BS 1800)

LEVEL 2 CORROSION SHEAR ANGLE BS 1800 BETWEEN S51L AND S50L. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.

Part: ANGLE — CORRODED (BS 1920)

LEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1920, BL 0, BETWEEN S51L AND S51R. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.

Part: ANGLE — CORRODED (BS 1820)

LEVEL 2 CORROSION SHEAR ANGLE BS 1820 BETWEEN S50L AND S49L. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.

Part: ANGLE — CORRODED (BS 1760)

LEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1760 BETWEEN S49L AND S48L. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.

Part: ANGLE — CORRODED (BS 1800)

LEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1800, BL 0, BETWEEN S51L AND S51R. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.

Part: ANGLE — CORRODED (BS 1880)

LEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1880, BL 0, BETWEEN S51L AND S51R. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.

Part: ANGLE — CORRODED (BS 1760)

LEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1760 BETWEEN S49L AND S50L. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.

Part: ANGLE — CORRODED (BS 1660)

LEVEL 2 CORROSION SHEAR ANGLE BS 1660 BETWEEN S47R AND S48R. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.

Part: ANGLE — CORRODED (BS 1760)

LEVEL 2 CORROSION SHEAR ANGLE BS 1760 BETWEEN S49L AND S50L. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.

Part: SHEAR ANGLE — CORRODED (BS 1760)

LEVEL 2 CORROSION SHEAR ANGLE BS 1760 BETWEEN S49L AND S48L. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.

Part: ACCESS PANEL — CRACKED (FUSELAGE)

ACCESS PANEL 191ML FORWARD HINGE AREA UNDER HINGE CRACKED FIBERGLASS. REPAIRED PER BOEING SRM 51-40-09.

Part: SKIN — GOUGED (DOOR CUTOUT)

TWO GOUGES IN FUSELAGE SKIN AT AFT CARGO DOOR CUT AFT SIDE. BLENDED GOUGES PER BOEING SRM 51-10-01.

Part: RIVETS — POPPED (BS 1980/2030)

EIGHT POPPED RIVETS AT BULK CARGO DOOR FRAME 5 AT BS 1980 AND 3 AT BS 2030. REPLACED RIVETS PER BOEING SRM 51-30-02.

Part: ROD ENDS — LACK OF LUBE (TE FLAPS)

FLAPS ARE EXTREMELY SLOW AND HARD TO MOVE, HANDLE IS SPRINGY AT FLAPS 25, 30 AND FULL UP. RIG CHECKED FLAP CONTROL CABLES, COMPLETED TENSION CHECK, FOUND ROD ENDS BINDING ON FLAP POWER PACKAGE, CLEANED AND LUBRICATED ROD ENDS AND ALL VISABLE CABLE RUNS AND PULLEYS OPERATIONAL CHECK GOOD PER MAINTENANCE MANUAL 27-51-00.

Part: TORQUE TUBE — SHEARED (RT LT FLAPS)

SHEARED TORQUE TUBE OUTBOARD OF THE RIGHT WING SET 4 LEADING EDGE POWER DRIVE UNIT. REPAIRED PER BOEING SRM 51-30-02, INSTALLED PER MAINTENANCE MANUAL 27-81-05, RIG AND FUNCTIONAL CHECKED PER 27-81-00.

Part: CONTROLLER — FAILED (COCKPIT)

AT 13 FT THE AUTO FAIL LIGHT CAME ON, WENT MANUAL BACK TO AUTO FAIL LIGHT OFF AND BACK ON. CABIN WENT TO 8.6 FEET DIFFERENTIAL PRESSURE 9.4 BOTH OUT FLOW VALVES CLOSED, CABIN STILL CLIMBING AT FL 20.0. REPLACED AUTO PRESSURE CONTROLLER, OPERATIONAL CHECK OF PER BOEING MAINTENANCE MANUAL 21-31-02.

Part: ANGLE — CHAFED (NR 2 ENGINE)

NR 2 ENGINE FWD NOSE FAIRING AFT LT/RT ANGLES AND BRACKETS WITH DEEP CHAFE MARKS. BURNISHED ANGLES AND BRACKET IAW SRM 53-10-01. REPLACED ANGLE ON FWD NOSE FAIRING IAW SRM 51-30-02.

Part: SKIN — DAMAGED (NR 3 SAILBOAT)

NR 3 ENGINE I/B O/B SAILBOAT FAIRING INNER SKIN HAS A HOLE. REPAIRED WITH METAL TO METAL BOND IAW SRM 51-40-06.

Part: COWL SKIN — CRACKED (NR 3 ENGINE)

NR 3 ENGINE RT FAN COWL HANGER FAIRING FWD HINGE CUTOUT SKIN CRACKED AT 1 O'CLOCK POSITION. BLENDED OUT MINOR CRACK AND SMOOTHED OUT AREA IAW SRM 51-10-01.

Part: TR SKIN — SEPARATING (NR 1 ENGINE)

NR 1 ENGINE INBOARD SIDE OF T/R COWL AT 4 O'CLOCK POSITION SKIN SEPARATING. REBONDED SKINS IAW SRM'S 51-21-04 AND 51-70-00.

Part: COWL SKIN — GOUGED (NR 3 ENGINE)

NR 3 ENGINE O/B CORE COWL INNER SKIN AND ANGLES CAVE-IN, GOUGED, AND WORN OUT 7 EA LOCATIONS. BLENDED OUT GOUGE IAW SRM 51-10-01.

Part: SKIN — DAMAGED (RT INBD SAILBOAT)

RIGHT HAND INBOARD SAILBOAT INNER SKIN HAS A HOLE. CLEANED, APPLIED FILLER, HOT BONDED DOUBLER IN PLACE IAW SRM 51-40-06.

Part: COWL SKIN — CRACKED (NR 2 ENGINE)

NR 2 ENGINE O/B CORE COWL BREATHER EXHAUST OUTER SKIN CRACKED ALONG WELD JOINT AREA. SKIN REWELDED AT JOINT IAW SRM 51-10-40.

Part: SKIN — CHAFED (LT LE FLAP)

HOLE CHAFED IN OUTBOARD END LEADING EDGE OF LEFT OUTBOARD LEADING EDGE FLAP. CLEANED, POTTED AND APPLIED A FIBERGLASS OVERLAY REPAIR PER BAC SRM 51-40-09.

Part: SKIN — DAMAGED (NR 2 ENGINE COWL)

DAMAGED AND WORN SKIN ON BLOW OUT DOOR AND CUTOUT OF NR 2 ENGINE INBOARD CORE COWL. BLENDED DAMAGED AREAS PER BAC SRM 51-10-01.

Part: ANGLE — GOUGED (NR 2 ENG COWL)

DEEP GOUGE ON NR 2 ENGINE OUTBOARD CORE COWL HAT SECTION STRUCTURAL ANGLE. FABRICATED NEW ANGLE AND INSTALLED PER BAC SRM 51-10-01.

Part: RIVETS — LOOSE (NR 2 ENGINE COWL)

SKIN LIFTING AT PRECOOLER EXHAUST CUTOUT ON NR 2 INBOARD CORE COWL DUE TO LOOSE RIVETS. REPAIRED BY RECOUNTOURING SKIN AND REPLACING LOOSE RIVETS PER BAC SRM 51-30-02.

Part: SKIN — CRACKED (NR 2 PYLON)

NR 2 PYLON LOWER FWD PYLON ACCESS PANEL 463CL CUTOUT HAS .5 INCH CRACK AT THE AFT UPPER END. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW SRM 54-30-05.

Part: PANEL — DELAMINATED (NR 7 SPOILER)

DELAMINATED NR 7 SPOILER PANEL ON RIGHT WING. REPLACED NR 7 SPOILER PANEL PER BAC MM 27-62-01.

Part: RIVETS — MISSING (NR 3 ENG FAIRING)

MISSING AND PULLED THROUGH RIVETS AT ABOUT 30 PLACES ON LEFT AND RIGHT SKIRT FAIRING ON NR 3 ENGINE. REPLACED RIVETS ON LEFT AND RIGHT SKIRT FAIRINGS PER BAC SRM 51-30-02.

Part: SKIN — DAMAGED (NR 3 ENGINE COWL)

DAMAGED AND WORN OUTER SKIN AT NR 3 ENGINE INBOARD CORE COWL BLOW OUT PANEL AND CUTOUT RADIUS. REPAIRED DAMAGED AREA PER BAC SRM 51-40-02.

Part: ANGLE — GOUGED (NR 2 ENG COWL)

GOUGED INNER FORWARD STRUCTURAL ANGLE ON NR 2 ENGINE OUTBOARD CORE COWL. REPLACED ANGLE PER BAC SRM 51-10-01.

Part: RIVET — PULLED THROUGH (ENGINE FAIRING)

SUNK RIVETS ON NR 2 SLOT SEAL FAIRING. REPLACED RIVETS PER BAC SRM 51-30-02.

Part: ANGLE — CRACKED (NR 3 ENG COWL)

CRACKS, HOLES AND CAVED IN SECTIONS AT 3 PLACES ON LOWER STRUCTURAL HAT ANGLE OF NR 3 ENGINE INBOARD CORE COWL. FABRICATED AND INSTALLED NEW HAT ANGLE ON NR 3 ENGINE CORE COWL PER BAC SRM 51-10-01.

Part: SKIN — CORRODED (3R DOOR)

LEVEL 1 CORROSION TO RIVET HEADS ON NR 3R DOOR OUTER SKIN. REMOVED AND REPLACED CORRODED RIVETS PER BAC SRM 51-30-02.

Part: SKIN — DAMAGED (NR 3 PYLON)

DAMAGED SKIN ON PYLON LEADING EDGE FROM 11 O'CLOCK TO 7 O'CLOCK. TRIMMED DAMAGED AREA PER BAC SRM 54-30-01.

Part: COWL SKIN — LIFTED (NR 3 ENGINE)

LIFTED OUTER SKIN ON NR 3 ENGINE OUTBOARD CORE COWL MID SECTION. REPLACED SKIN PER BAC SRM 51-10-01.

Part: RIVETS — MISSING (NR 2 ENGINE)

MANY MISSING AND PULLING THROUGH RIVETS ON NR 2 ENGINE EXHAUST SLEEVE. REPLACED RIVETS PER BAC SRM 51-30-02.

Part: RIVETS — MISSING (ENGINE FAIRING)

SEVERAL LOOSE OR MISSING RIVETS ON NR 2 SLOT SEAL FAIRING. REPLACED RIVETS PER BAC SRM 51-30-02.

Part: ANGLE — CRACKED (NR 2 ENGINE COWL)

CRACKED, WORN AND CAVED IN STRUCTURAL ANGLE ON NR 2 ENGINE INBOARD CORE COWL. FABRICATED AND REPLACED STRUCTURAL ANGLE PER BAC SRM 51-10-01.

Part: DOUBLER — DAMAGED (NR 2 PYLON)

DAMAGED AND WORN SKIN DOUBLER ON NR 2 PYLON AFT OF ENGINE MOUNT AREA. FABRICATED AND INSTALLED NEW FILLER AND DOUBLER PER BAC SRM 51-10-01.

Part: COWL — DENTED (NR 2 ENGINE FAN)

SEVERAL DENTS ON NR 2 ENGINE OUTBOARD FAN COWL. REPAIRED WITH HOT BOND FILLER AND DOUBLER PER BAC SRM 51-40-06 AND PAINTED PER BAC SRM 51-24-11.

Part: GULL FAIRING — DAMAGED (LT MLG DOOR)

DAMAGED GULL FAIRING LEFT WING LANDING GEAR LOWER STRUT DOOR AT AFT END. REPAIRED PER BOEING SRM 51-40-09.

Part: TRACK — WORN (RT TE MID FLAP)

WORN FORE FLAP TRACK TO RIGHT OUTBOARD TRAILING EDGE MID FLAP. REPLACED TRACK PER BOEING MAINTENANCE MANUAL 27-51-04 AND 27-51-06.

Part: TRACK — WORN (LT TE MID FLAP)

WORN FORE FLAP TRACK TO LEFT OUTBOARD TRAILING EDGE MID FLAP. REPLACED TRACK PER BOEING MAINTENANCE MANUAL 27-51-04 AND 27-51-06.

Part: SKIN — DELAMINATED (LT TE FORE FLAP)

DELAMINATE LEADING EDGE OF THE LEFT OUTBOARD TRAILING EDGE FORE FLAP BY THE OUTBOARD EDGE. REPAIRED PER BOEING SRM 51-40-07.

Part: HYD LINE — CRACKED (LT WING)

NR 1 HYDRAULIC QUANTITY LOW. FOUND CRACKED LINE NR 1 HYDRAULIC SYSTEM FROM T-FITTING INBOARD OF NR 1 PYLON TO T-FITTING OUTBOARD OF NR 1 PYLON. INSTALLED TEMPORARY FLEX LINE PER BOEING MAINTENANCE MANUAL 29-00-00 PAGE 5.

Part: BRACKETS — BROKEN (APU LT DOOR)

APU LEFT DOOR FORWARD AND AFT FIRE DETECTOR ELEMENT BRACKETS BROKE OFF DOOR. REPAIRED PER BOEING SRM 51-40-03.

Part: PANEL — DELAMINATED (WS 420)

DELAMINATED PANEL LEFT WING UPPER ABOVE FALSE SPAR AREA WS 420. REPLACED PANEL PER BOEING SRM 51-10-01.

Part: FAIRING — PUNCTURE (NR 4 FLAP TRACK)

NR 4 FLAP TRACK CANOE FAIRING HAS PUNCTURE IN LOWER AFT END. REMOVED DAMAGED SKIN, POTTED CORE, FABRICATED FILLER AND DOUBLERS AND INSTALLED REPAIR IAW SRM 51-40-15.

Part: ANGLE — WORN (LT MLG STRUT DR)

LEFT BODY GEAR STRUT DOOR OUTER AFT ANGLE WORN WITH A HOLE. REPLACED ANGLE PER BOEING SRM 51-30-02.

Part: COWL — CRACKED (NR 3 ENGINE)

NR 3 LEFT FAN COWL LOWER EDGE IS CRACKED BETWEEN THE AFT AND MIDDLE U-BOLTS. REPAIRED CRACK PER BOEING SRM 51-40-06.

Part: PULLEY — BROKEN (MAIN DECK)

MAIN DECK TO UPPER DECK LADDER PULLEY BROKEN. REPLACED PULLEY I/A/W MAINTENANCE MANUAL 25-50-01.

Part: CHANNEL — BENT (NR 1 CORE COWL)

NR 1 ENGINE OUTBOARD CORE COWL LOWER EDGE CHANNEL VERY BENT, WITH PULLED RIVETS AND LOST DOUBLERS. REMOVED FABRICATED AND INSTALLED CHANNEL PER BOEING SRM 51-40-03.

Part: SKIN — DELAMINATED (LT TE FOREFLAP)

LEFT WING OUTBOARD FOREFLAP HAS PREVIOUS GOUGE AND DELAMINATION AT OUTBOARD LEADING EDGE. REMOVED DAMAGED SKIN, POTTED CORE, FABRICATED FILLER AND DOUBLERS AND INSTALLED IAW SRM 51-40-15.

Part: PANEL — CRACKED (NR 4 PYLON)

NR 4 ENGINE PYLON LOWER EDGE PANEL CRACKED. REMOVED FABRICATED AND INSTALLED PANEL PER BOEING SRM 51-10-01.

Part: SKIN — PUNCTURED (LT TE AFT FLAP)

LEFT WING OUTBOARD AFT FLAP UPPER SURFACE HAS SMALL PUNCTURE. REMOVED DAMAGED SKIN, POTTED CORE, FABRICATED FILLER AND DOUBLERS AND INSTALLED REPAIR IAW SRM 51-40-11 AND 51-40-15.

Part: DOOR — CRACKED (RT MLG STRUT)

RIGHT WING LANDING GEAR STRUT LOWER DOOR LEADING EDGE AREA CRACKED ALONG FAIRING ASSEMBLY. REPAIRED PER BOEING SRM 51-40-05.

Part: COVE PANEL — CRACKED (LT TE MIDFLAP)

LEFT WING OUTBOARD MIDFLAP TRAILING EDGE COVE PANEL CRACKED AT MIDPOINT. REMOVED DAMAGED PANEL AND CORE, FABRICATED CORE, FILLER AND DOUBLERS AND INSTALLED IAW SRM 51-40-09 AND 51-40-12.

Part: FAIRING — DELAMINATED (FUSELAGE)

DELAMINATED BODY FAIRING PANEL LOCATED BETWEEN LEADING EDGE OF MAIN LANDING GEAR CENTER DOORS. REPLACED PANEL PER BOEING SRM 51-30-02 AND 51-24-11.

Part: ANGLE BRACKET — CRACKED (NR 4 PYLON)

NR 4 ENGINE PYLON, ANGLE BRACKET BENT AND CRACKED INBD AFT. REMOVED, FABRICATED AND INSTALLED BRACKET PER BOEING SRM 51-32-01 AND 51-10-02.

Part: SKIN — CRACKED (NR 4 PYLON)

NR 4 PYLON INBOARD SIDE LOWER SKIN FLANGE CRACKED. REMOVED, FABRICATED AND INSTALLED SKIN FLANGE IAW BOEING SRM 51-30-02 AND 54-12-01.

Part: SKIN — CRACKED (LT MLG DOOR)

LEFT BODY GEAR INBOARD DOOR LOWER INNER SKIN LEADING EDGE MID SECTION CRACKED AND DEFORMED. REPAIRED PER BOEING SRM 52-80-02.

Part: SKIN — CRACKED (NR 1 NACELLE)

NR 1 ENGINE INBOARD FAN COWL, TOP FORWARD HINGE HAS CRACK IN SKIN TOP SURFACE. WORKED AND BLENDED OUT CRACK IAW BOEING SRM 51-10-06, TREATED AND PRIMED IAW SRM 51-40-02.

Part: BRACKET — CRACKED (NLG WW)

HORIZONTAL ANGLE CRACKED ON VERTICAL BEAM RIGHT SIDE OF NOSE LANDING GEAR WHEEL WELL BS 320. REMOVED, FABRICATED AND INSTALLED ANGLE PER BOEING SRM 51-10-01, 51-10-02 AND 51-40-03.

Part: ANGLE — CRACKED (NR 4 PYLON)

NR 4 ENGINE PYLON UPPER END OF SUPPORT ANGLE CRACKED IN RADIUS INBOARD AND OUTBOARD STATION 221.9 ABOVE AFT ENGINE MOUNT INSIDE PANEL. INSTALLED DOUBLERS IAW BOEING SRM 54-10-03 FIG 19.

Part: BRACKET — CRACKED (NR 4 PYLON)

CRACKED SUPPORT BRACKET NR 4 PYLON, GENERATOR LEAD SUPPORT. REMOVED, FABRICATED AND REPLACED BRACKET PER BOEING SRM 51-30-02 AND 51-10-01.

Part: ANGLE — CRACKED (NR 1 NACELLE)

NR 1 OUTBOARD CORE COWL HAS CRACKED REPAIR ANGLE INSIDE TO EDGE AT BEND. REMOVED, FABRICATED AND INSTALLED ANGLE IAW BOEING SRM 51-30-02 AND 51-10-01.

Part: SEAL RETAINER — BENT (CARGO DR CUTOUT)

FWD LOWER CARGO COMPARTMENT CUTOUT SEAL RETAINER AFT EDG BENT AND DEFORMED. FABRICATED NEW SEAL RETAINER PER BOEING SRM 51-32-01, INSTALLED PER BOEING SRM 51-10-01.

Part: DOOR SILL — CRACKED (CARGO COMPT)

BULK CARGO DOOR SILL CRACKED 2 PLACES. WELD REPAIRED PER BAC59755905 USING TITANIUM TIG ROD, INSTALLED PER BOEING SRM 51-10-01.

Part: COWL — TORN (NR 4 ENGINE)

NR 4 ENGINE CORE COWL FRONT LATCH AREA TORN AND DEFORMED. REMOVED, FABRICATED AND INSTALLED U-CHANNEL PER BOEING SRM 51-30-02 AND 51-10-01.

Part: PANEL — PUNCTURED (LT TE MIDFLAP)

LEFT WING INBOARD MIDFLAP INBOARD UPPER STRESS PANEL PUNCTURED. INSTALLED FILLER AND DOUBLER IAW SRM 51-40-06.

Part: SKIN — WORN (RT TE MIDFLAP)

RIGHT HAND INBOARD MIDFLAP TRAILING EDGE HAS EXPOSED HONEYCOMB. POTTED SMALL PUNCTURE, APPLIED FILLER AND OVERLAY IAW SRM 51-40-09.

Part: FITTING — CRACKED (NR 4 PYLON)

FOUND NR 4 PYLON FORWARD FAIRING OUTBOARD LATCH 'U' FITTING CRACKED. REMOVED AND REPLACED FORWARD FAIRING RETAINER FITTING IAW SRM 54-10-03 AND MM 54-32-01.

Part: BOGIE PIN — PITTED (NR 7 FLAP TRACK)

FOUND NR 7 FLAP TRACK BOGIE PINS PITTED. REMOVED AND REPLACED PINS IAW MM 27-51-04.

Part: PANEL — DELAMINATED (RT TE MIDFLAP)

RIGHT HAND INBOARD MIDFLAP TOP SURFACE CENTER PANEL HAS LARGE AREAS OF DELAMINATION. REMOVED PANEL AND INSTALLED NEW PANEL IAW SRM 51-10-01.

Part: SUPPORT — CRACKED (NR 1 TE FLAP)

NR 1 FLAP TRACK SEQUENCE TOGGLE ROLLER SUPPORT LINK CRACKED. REMOVED AND REPLACED SUPPORT LINK IAW MM 27-51-00.

Part: BRACE — CRACKED (NR 4 TE FLAP)

FOUND NR 4 MOVEABLE CANOE FORWARD SUPPORT FITTING CRACKED. REMOVED AND REPLACED BRACE IAW MM 27-51-00 AND MM 27-51-45.

Part: CHANNEL — CRACKED (NR 3 COWL)

NR 3 INBOARD CORE COWL LOWER EDGE CHANNEL CRACKED AND BENT. REMOVED CHANNEL, FABRICATED CHANNEL AND SPLICE AND INSTALLED IAW SRM 51-40-03.

Part: COVER — CRACKED (NLG STEERING)

NOSE GEAR STEERING CABLE HOUSING COVER CRACKED. SANDED OUT CRACK, COLD BOND PLY LAYUP BONDED AND SEALED IAW SRM 51-40-09.

Part: PRESS MODULE — CRACKED (NR 3 SYSTEM)

ON ARRIVAL, FOUND HYDRAULIC LEAK FROM NR 3 HYDRAULIC SYSTEM IN SAILBOAT AREA. FOUND NR 3 HYDRAULIC SYSTEM PRESSURE MODULE HOUSING CRACKED. REMOVED AND REPLACED SAME, OPS AND LEAK CHECK NORMAL IAW MM 29-11-23.

Part: ENGINE — BIRD STRIKE (NR 3 ENGINE)

UPON INSPECTION OF NR 3 ENGINE FOUND EVIDENCE OF BIRD STRIKE. COMPLIED WITH CONDITIONAL INSPECTION PER 5-51-14 AND BORESCOPE INSPECTION PER MM 72-00-00, NO DAMAGE FOUND.

Part: SOLENOID — FAILED (COCKPIT)

DURING CRUISE, EXPERIENCED SMOKE IN COCKPIT FOR 4 TO 5 MINUTES. SMOKE DISPERSED ON ITS OWN. UPON LANDING FOUND LANDING GEAR LEVER LOCK CIRCUIT BREAKER POPPED, SOLENOID FAILED. DEFERRED PER MEL 32-16 CATEGORY A, TO BE REPAIRED WITHIN 7 FLIGHT DAYS.

Part: TIRE — BLOWN (NR 9 MAIN)

ON TAKEOFF, TOWER ADVISED AIRCRAFT OF RUBBER FOUND ON RUNWAY, NO COCKPIT INDICATIONS. WHEN GEAR EXENDED ON LANDING ANC BOTH PRIM AND ALT GEAR TILT LIGHTS OF RIGHT BODY GEAR CAME ON. FOUND NR 9 MAIN TIRE BLOWN. REMOVED AND REPLACED SAME IAW MM 32-45-01, COMPLIED WITH BLOWN TIRE INSPECTION IAW MM 5-51-25, C/W ANTI-SKID BITE CHECK IAW 32-42-00. REMOVED TIRE DEBRIS FROM TRUCK POSITION SWITCH AREA, PERFORMED FUNCTIONAL TEST OF BOTH PRI AND ALT TILT SWITCH SYSTEM IAW 32-13-00, NO DEFECTS NOTED.

Part: RETENTION SCREWS — LOOSE (NR 10 WHEEL)

FOUND NR 10 WHEEL ASSEMBLY ALIGNMENT KEYS MIGRATED DUE TO LOOSE/MISSING RETENTION SCREWS, CAUSED DAMAGE TO BRAKE ASSEMBLY. REMOVED AND REPLACED NR 10 WHEEL ASSEMBLY PER MM 32-45-01. REMOVED AND REPLACED BRAKE ASSEMBLY PER MM 32-41-15. BRAKE ASSEMBLY (P/N 2601902-60) (S/N B0903).

Part: FUEL CONTROL — MALFUNCTIONED (NR 4 ENGINE)

NR 4 ENGINE FLAME-OUT AT 29,000 FT, ATTEMPTED ENGINE RESTART, UNSUCCESSFUL. FLIGHT RETURNED TO MIAMI. REPLACED FCU, FUEL PUMP, TT2 SENSOR IAW MM 73-11 01 AND 73-21 01. LEAK CHECK AND RUNUP OK.

Part: OVERHEAT WARNING — ACTIVATED (RT WING)

RT WING LEADING EDGE OVERHEAT FAULT, ON TAXI OUT FOR TAKEOFF. RETURNED TO GATE, UNABLE TO DUPLICATE OVERHEAT CONDITION WITH EITHER APU OR ENGINE PNEUMATICS. DETERMINED TO BE FALSE WARNING.

Part: CIRCUIT BREAKER — FAILED (NR 1 BOOST PUMP)

ON TAXI OUT, NR 1 MAIN FORWARD BOOST PUMP LOW PRESSURE LIGHT AND NR 4 MAIN AFT BOOST PUMP LOW PRESSURE LIGHT CAME ON. FOUND CIRCUIT BREAKERS AT FAULT, REPLACED SAME IAW MM 28-22-01. BOOST PUMPS OPS CHECKS NORMAL.

Part: SEAT TRACK — CRACKED (RT COCKPIT)

FOUND FIRST OFFICER'S AFT INBOARD SEAT TRACK CRACKED. REMOVED AND REPLACED SAME IAW MM 25-11-01.

Part: SEAT TRACK — CRACKED (LT COCKPIT)

FOUND CAPTAIN'S FORWARD OUTBOARD SEAT TRACK CRACKED. REMOVED AND REPLACED SAME IAW MM 25-11-01.

Part: EVC — FAILED (NR 4 ENGINE)

NR 4 ENGINE SHUT DOWN IN-FLIGHT WITH LOW OIL QTY AND OIL PRESSURE LIGHT ON. OIL PRESSURE DROPPED TO 37 PSI WITH ALL OTHER INDICATIONS NORMAL. ENGINE WINDMILLED FOR 2 HOURS. REPLACED NR 4 EVC IAW MM 75-31-01. ALSO, REPLACED EVC ACTUATOR, P/N 719999-6, S/N 6050074, IAW 75-31-02. OPS AND LEAK CHECK GOOD.

Part: WHEEL — FAILED (NR 11 WHEEL)

THE NR 11 WHEEL AND TIRE DAMAGED ON LANDING DUE TO FAILURE OF WHEEL RIM. REPLACED TRUCK BEAM ASSY DUE TO OVERHEAT OF AXLE. WHEEL AND TRUCK BEAM REPLACED IAW MM 32-13-11. TOTAL LANDINGS SINCE SHOP VISIT 211.

Part: DOOR HINGE — CORRODED (NR 3 ACM)

NR 3 ACM FAIRING DOOR FORWARD HINGE HAS EXFOLIATED CORROSION. REMOVED AND REPLACED HINGE IAW SRM 51-10-01.

Part: FITTING — CRACKED (DOOR SILL)

FORWARD CARGO DOOR SILL NR 8 TRUSS FITTING CRACKED IN LOWER RADIUS. REMOVED AND REPLACED TRUSS FITTING IAW SRM 51-10-01.

Part: EXHAUST SHROUD — CRACKED (NR 4 ENGINE)

NR 4 EXHAUST SHROUD WORN AND CRACKED AT FORWARD FLANGE, 7 O'CLOCK POSITION. BLENDED DAMAGED AREA, FABRICATED AND INSTALLED INTERNAL DOUBLER AND EXTERNAL WEAR PLATE IAW SRM 54-30-03.

Part: COWLING — CRACKED (NR 3 ENGINE)

NR 3 ENGINE INBOARD COWLING, 4TH FRAME FROM FRONT CRACKED INBOARD SIDE. REMOVED DAMAGE, ROUTED ANGLES TO SHOP FOR FABRICATION, INSTALLED NEW ANGLES PER SRM 54-10-03.

Part: TE PANEL — CRACKED (RT ELEV)

RIGHT INBOARD ELEVATOR PANEL, INBOARD TRAILING EDGE CRACKED AND DELAMINATED. SANDED AND CLEANED DAMAGED AREA, APPLIED FIBERGLASS OVERLAYS AS REQUIRED PER SRM 51-40-15.

Part: TR RAIL — CRACKED (NR 2 ENGINE)

NR 2 ENGINE R-RAIL CRACKED AT THE FOUR-THIRTY POSITION. WELDED CRACK IAW P AND W MM 72-53-01.

Part: PANEL — CRACKED (PACK ACCESS DOOR)

PACK ACCESS DOOR FAIRING PANEL 191ML CRACKED AT FORWARD OUTBOARD CORNER. SANDED AND CLEANED AREA, HOT BONDED FIBERGLASS OVERLAYS IAW SRM 51-40-12.

Part: PANEL — DELAMINATED (PACK ACCESS DOOR)

FAIRING PANEL 191ML HAS DELAMINATED SPOT AT FORWARD END. SANDED AND CLEANED AREA, HOT BONDED FIBERGLASS OVERLAYS IAW SRM 51-40-12.

Part: S-RAIL — CRACKED (NR2 ENGINE)

NR 2 ENGINE S-RAIL CRACKED AT 6 O'CLOCK POSITION. WELDED CRACK IAW P AND W MM 72-53-01.

Part: TR RAIL — CRACKED (NR 3 ENGINE)

NR 3 ENGINE R-RAIL CRACKED IN TWO PLACES, APPROXIMATELY 5 O'CLOCK POSITION. WELDED CRACK IAW P AND W MANUAL 72-53-01.

Part: PCU — CRACKED (RUDDER)

DURING SYDNEY GROUND TIME, OBSERVED HYDRAULIC FLUID COMING FROM UPPER RUDDER POWER CONTROL UNIT. FOUND TWO INCH CRACK IN FILTER HOUSING. REPLACED POWER CONTROL UNIT IAW MM 27-21-17.

Part: ENGINE — OIL LEAKING (NR 1)

DURING CLIMB-OUT, LOSS OF OIL IN NR 1 ENGINE SHUT DOWN ENGINE. FOUND OIL TO BE COMING OUT TAIL PIPE, ENGINE CHANGED.

Part: PANEL — DELAMINATED (LT WING LE)

DELAMINATED FIBERGLASS PANEL LEFT WING LEADING EDGE UPPER PANEL INBOARD OF NR 2 PYLON. REPAIRED PER BOEING SRM 51-40-09.

Part: TE PANEL — DELAMINATED (LT WING)

DELAMINATED FIBERGLASS PANEL LEFT WING TRAILING EDGE OUTBOARD OF OUTBOARD AILERON, PCU UPPER ACCESS PANEL. REPAIRED PER BOEING SRM 51-40-09.

Part: PDU — BROKEN (NR 1 LE FLAP)

CRACKED MOUNT LUG NR 1 RIGHT LEADING EDGE PDU. REPLACED PDU PER BOEING MAINTENANCE MANUAL 27-81-03.

Part: T-CHORD — SHEARED (BS 880)

SHEARED T-CHORD AT BS 880, BETWEEN MIDDLE 2 ROLLER TRACKS FORWARD CARGO COMPARTMENT. REPLACED T-CHORD AND STIFFENERS PER BOEING SRM 51-40-00.

Part: COVER PANEL — CRACKED (LT WING)

CRACKED COVER PANEL AT OUTBOARD END OF INBOARD TRAILING EDGE FLAP COVER AREA. REPAIRED PER BOEING SRM 51-40-09.

Part: SUPPORT — BROKEN (WS 970)

BROKEN SUPPORT LINK FOR RIGHT WING LOWER LEADING EDGE PANEL, AT LES 970. REPLACED LINK.

Part: FAIRING — CRACKED (NR 4 PYLON)

CRACKED FAIRING NR 4 STRUT FORWARD. REPAIRED PER BOEING SRM.

Part: PRESS DECK — CORRODED (GEAR WHEEL WELL)

CORROSION ON PRESSURE DECK FLOOR ABOVE LANDING GEAR SELECTOR VALVE. REMOVED CORROSION, FOUND WITHIN LIMITS PER BOEING SRM 3-10-01, DOUBLER INSTALLED PER SRM 51-40-06.

Part: TE SKIN — DELAMINATED (NR 7 SPOILER)

DELAMINATION AT LOWER TRAILING EDGE AREA OF NR 7 SPOILER. REPAIRED PER BOEING SRM 51-40-09.

Part: TE WEDGE — DELAMINATED (LT WING)

DELAMINATED FIBERGLASS TRAILING EDGE WEDGE SECTION OUTBOARD OF OUTBOARD TRAILING EDGE FLAP AND INBOARD OF NR 1 PYLON TRAILING EDGE FAIRING. REPAIRED PER BOEING SRM 51-40-09.

Part: STIFFENER — CRACKED (RT WING)

CRACKED INBOARD AILERON INBOARD SUPPORT RIB STIFFENER AT UPPER END. REPLACED FITTING PER BOEING SRM 51-40-00.

Part: FAIRING — DELAMINATED (NR 8 CANOE)

DELAMINATION OF NR 8 CANOE FAIRING AT BOTTOM. REPAIRED PER BOEING SRM 51-40-09.

Part: FAIRING — PUNCTURED (NR 1 FLAP)

PUNCTURE IN NR 1 TRAILING EDGE FLAP MOVABLE FAIRING. FIBERGLASS REPAIR COMPLETED PER BOEING SRM 51-40-09

Part: PDU — BROKEN (RT WING)

CRACKED MOUNT LUG NR 1 RIGHT LEADING EDGE PDU. REPLACED PDU PER BOEING MAINTENANCE MANUAL 27-81-03.

Part: SKIN — CRACKED (NR 16 LE FLAP)

CRACK ON NR 16 KRUEGER FLAP AFT SIDE OUTBOARD LOWER EDGE. REPAIRED PER BOEING SRM.

Part: PRECOOLER — CRACKED (NR 3 ENGINE)

PRECOOLER COVER ON NR 3 ENGINE HAS CRACK 1 INCH, ALONG ITS LOWER CORNER. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (NR 3 PYLON)

NR 3 PYLON BULKHEAD AT NACELLE STA 221 CRACKED AT OUTBOARD FORWARD AND AFT FACES. REPLACED BULKHEAD ANGLES AND STRAPS.

Part: EXHAUST — CRACKED (NR 2 ENGINE)

CRACKS ON NR 2 ENGINE R-FLANGE AT FIVE O'CLOCK POSITION, S-FLANGE AT 3 LOCATIONS BETWEEN SIX-THIRTY AND SEVEN-THIRTY POSITION. WELD REPAIRED PER PRATT AND WHITNEY MAINTENANCE MANUAL 72-53-01.

Part: LADDER — CRACKED (MAIN DECK)

CRACKED UPPER DECK ACCESS LADDER AT PULLEY LOCATION. REPAIRED LADDER.

Part: STIFFENER — CORRODED (BS 1350)

CORRODED STIFFENER IN LEFT BODY GEAR WHEEL WELL, BS 1350 AT LBL 87. REMOVED CORROSION WITHIN LIMITS OF BOEING SRM 51-10-01 FIG 1.

Part: SKIN — PUNCTURED (RT TE MIDFLAP)

SMALL PUNCTURE HOLE IN RIGHT WING INBOARD MIDFLAP FORWARD OF NR 5 CANOE FAIRING. REPAIRED PER BOEING SRM 51-40-09.

Part: TE PANEL — CRACKED (LT WING)

CRACKED AND DELAMINATED FIBERGLASS PANEL, LEFT WING TRAILING EDGE OUTBOARD OF INBOARD AILERON. REPAIRED PER BOEING SRM.

Part: L-CHORD — CORROSION (BS 1283-1333)

CORROSION ON LT OUTBOARD LONGERON L-CHORD, BS 1283 TO BS 1333. REPAIRED PER BOEING TELEX PAO-SIN-95-0002RE.

Part: EXHAUST — CRACKED (NR 1 ENGINE)

CRACKS ON NR 1 ENGINE ON R-FLANGE, TWO-THIRTY AND S-FLANGE AT 2 O'CLOCK POSITION. WELD REPAIRED PER PRATT AND WHITNEY MAINTENANCE MANUAL 72-53-01.

Part: ANGLE — CORRODED (CARGO DOOR)

CORROSION ON ANGLE ON AFT CARGO DOOR, FORWARD OF NEGATIVE PRESSURE RELIEF VALVE CUTOUT. REPLACED ANGLE.

Part: PRESS DECK — CORRODED (BS 1325)

CORROSION AT BS 1325 RIGHT OUTBOARD PRESSURE DECK FLOOR, OUTBOARD LOWER CHORD JOINT. CORROSION REMOVED WITHIN LIMITS PER BOEING SRM 53-10-01, INSTALLED DOUBLER WHERE MATERIAL WAS REMOVED AS PER BOEING SRM 51-40-02.

Part: SPAR — CORRODED (WS 1520)

CORROSION BULGE AT RIGHT WING FRONT SPAR LOWER CHORD AT WS 1520. REPAIRED PER BOEING SRM 57-30-03 FIG 9.

Part: BRACKETS — CRACKED (NR 3 PYLON)

CRACKED LATCH SUPPORT BRACKETS, 2ND AND 4TH FROM FRONT ON NR 3 PYLON INBOARD TRAILING EDGE DOOR. REPLACED BRACKETS.

Part: CANOE FAIRING — DELAMINATION (NR 7)

DELAMINATION AND PUNCTURE NR 7 CANOE FAIRING. REPAIRED PER BOEING SRM.

Part: PANEL — CORRODED (WS 758 LE)

CORROSION RIGHT WING LOWER LEADING EDGE SURFACE APPROXIMATLEY WS 758. REMOVED CORROSION WITHIN LIMITS PER BOEING SRM 57-30-01, REPROTECTED SURFACE.

Part: SPAR — CORRODED (RT TE MIDFLAP)

CORROSION ON RIGHT WING INBOARD MIDFLAP REAR SPAR UPPER T-CHORD, APPROXIMATELY WBL 230. CORROSION REMOVED AND SURFACE REPROTECTED PER BOEING SRM 51-10-01.

Part: SKIN — DELAMINATED (RT TE MIDFLAP)

DELAMINATION ON RIGHT WING INBOARD MIDFLAP, OUTBOARD UPPER PANEL. REPAIRED PER BOEING SRM 51-40-09.

Part: LE SKIN — PUNCTURED (RT TE FOREFLAP)

PUNCTURE RIGHT WING OUTBOARD FOREFLAP AT OUTBOARD LEADING EDGE. REPAIRED PER BOEING SRM 51-40-09.

Part: EXHAUST CASE — CRACKED (NR 3 ENGINE)

CRACKS ON NR 3 ENGINE RT FLANGE AT FOUR THIRTY, S-FLANGE AT FIVE O'CLOCK AND SIX THIRTY. WELD REPAIRED PER PRATT AND WHITNEY MANINTENCE MANUAL 72-53-01.

Part: TE PANEL — CRACKED (RT WING)

CRACKED PANEL RIGHT WING UPPER TRAILING EDGE, FORWARD OF NR 8 SPOILER PANEL. REPAIRED PER SRM 51-40-09.

Part: EXHAUST LINER — CRACKED (APU)

SEVERAL CRACKS APU EXHAUST LINER. REPLACED LINER.

Part: SKIN — CORRODED (LT WING)

CORROSION FOUND AROUND RIVET HEAD, TOP OF LEFT WING BETWEEN FRONT AND REAR SPARS. CLEANED CORROSION WITHIN LIMITS PER BOEING SRM 51-30-03.

Part: TE PANEL — CORRODED (NR 7/8 SPOILERS)

LIGHT CORROSION ON TRAILING EDGES OF NR 7 AND NR 8 SPOILER PANELS. REMOVED CORROSION AND REPROTECTED SURFACES PER BOEING SRM 51-10-01.

Part: PANEL — CRACKED (RT WING LE)

CRACK RIGHT WING LOWER LEADING EDGE PANEL JUST OUTBOARD OF NR 3 PYLON, LES 740. REPAIRED PER BOEING SRM 51-40-09.

Part: TE PANEL — DELAMINATED (RT WING)

DELAMINATED WING TRAILING EDGE PANEL FORWARD OF THE INBOARD AILERON RIGHT WING. REPAIRED PER BOEING SRM 51-40-09.

Part: SUPPORT PLATE — CRACKED (BS 1350)

CRACKED SUPPORT PLATE BS 1350 RBL 72, RIGHT BODY GEAR BAY. REPLACED SUPPORT PLATE.

Part: SKIN — CRACKED (FUSELAGE)

DURING INSPECTION PER AD 94-12-09, 6 HOLES CRACKED S19R BS 526 TO BS 534, 5 HOLES CRACKED BS 546 TO BS 551, 5 HOLES CRACKED BS 625 TO BS 630. REPAIRED PER BOEING SB 747-53-2307.

Part: SKIN — CRACKED (FUSELAGE)

DURING INSPECTION PER AD 94-12-09, 7 HOLES CRACKED S19L BS 527.5 TO BS 535, 6 HOLES CRACKED BS 547 TO BS 553.5, 3 RIVET HOLES CRACKED BS 571 TO BS 573.5, 1 RIVET HOLE CRACKED BS 592, 3 RIVET HOLES CRACKED BS 668 TO 671. REPAIRED PER BOEING SB 747-53-2307.

Part: TURBINE SLEEVE — BUCKLED (NR 3 ENGINE)

NR 3 ENGINE TURBINE SLEEVE BUCKELED ALONG LEADING EDGE 6 AND 9 O'CLOCK POSITION. REPAIRED IAW SRM 51-40-2 AND 51-10-01. (M)

Part: OIL LINE — DAMAGED (NR 2 ENGINE)

ANC-ORD - EN ROUTE THE NR 2 ENGINE EXPERIENCED A GRADUAL LOSS OF OIL. WHEN OIL TEMPERATURE STARTED TO RISE AND LOW PRESSURE LIGHT STARTED TO FLICKER, THE ENGINE WAS SHUTDOWN USING ALTERNATE PROCEDURES. LANDED ORD WITHOUT INCIDENT. MAINTENANCE REPLACED OIL LINE TO DIFFERENTIAL PRESSURE TRANSMITTER DUE TO A PIN HOLE LEAK. SERVICED OIL RESERVOIR. LEAK CHECK NORMAL. REPLACED OIL FILTER AS REQUIRED PER MM. ACFT RELEASED FOR FLIGHT.