N854FT

Part: LINE — CRACKED (FUEL SYSTEM)

ENGINE EXPERIENCED WHAT APPEARED TO BE A STALL FOLLOWED BY A FIRE WARNING. ENGINE WAS SHUT DOWN AND AN AIR TURN-BACK ACCOMPLISHED. CORE COWL DAMAGE WAS OBSERVED IMMEDIATELY AFTER LANDING. SUBSEQUENT INVESTIATION IDENTIFIED A CRACKED FUEL HYDRAULIC LINE. THE DEFECT CONSIDERED THE LIKELY CAUSE OF EXCESS FUEL SPILLAGE AND IGNITION SOURCE WITHIN NACELLE ENVIRONMENT. MODERATE FIRE DAMAGE WAS OBSERVED IN IMMEDIATE VACINITY OF FAILED TUBE.

Part: COWL — DELAMINATED (NR 2 ENGINE)

NR 2 ENGINE LEFT SIDE FAN COWL FOUND DELAMINATED. REPAIRED PER SRM 51-40-06.

Part: PANEL — DAMAGED (RT TE MIDFLAP)

RIGHT WING INBOARD MID FLAP AFT LOWER PANEL FOUND DAMAGED. REPAIRED PER SRM 51-41-08.

Part: FRAME — CRACKED (BS 360)

MAIN DECK BS 360R STRINGER 24R FOUND CRACK IN FRAME. REPAIRED PER SRM 53-12-00 AND HX RS 531234010.

Part: PANEL — DAMAGE (RT TE MIDFLAP)

RIGHT INBOARD MID FLAP AFT BOTTOM PANEL FOUND DAMAGE. REPAIRED PER SRM 51-40-05.

Part: COWL — DELAMINATED (NR 2 ENGINE)

NR 2 LEFT SIDE FAN COWL FOUND DELAMINATED. REPAIRED PER SRM 51-40-06.

Part: CONTROL CABLE — WORN (NR 2 SPOILER)

LEFT WING NR 2 SPOILER CONTROL CABLE WORN AT NR 3 AND NR 4 CONTROL DRUM AREA. REPLACED PER MM 20-11-03.

Part: SKIN — CORRODED (WS 1315)

LEVEL 1 CORROSION FOUND ON RIGHT WING LOWER SKIN STA 1315. REPAIRED PER SRM 51-10-01.

Part: CHORD — CORRODED (RT TE MIDFLAP)

RIGHT WING INBOARD MID FLAP LOWER CHORD FOUND CORROSION. REPAIRED PER SRM 51-40-04.

Part: SKIN — DAMAGED (NR 1 PYLON)

NR 1 PYLON OUTBOARD LOWER SPAR SKIRT PATCH INNER AND OUTER SKIN DAMAGED. REPAIRED PER SRM 54-30-03.

Part: CONTROL CABLE — WORN (NR 11 SPOILER)

NR 11 SPOILER CONTROL CABLE FOUND WORN AT DRUM ASSEMBLY. REPLACED PER MM 20-11-05.

Part: SKIN — DELAMINATED (RT TE FOREFLAP)

RIGHT INBOARD FOREFLAP ASSY INBOARD LOWER SURFACE FOUND DELAMINATION. REPAIRED PER SRM 51-40-06.

Part: STRAP — CRACKED (BS 1241)

BS 1241 RIGHT SIDE SPLICE STRAP FOUND CRACKED AT FWD AND AFT HOLE OF STRINGER 18R. REPAIRED PER SERVICE BULLETIN 53-2283.

Part: FITTING — CRACKED (RT MLG DOOR ACT)

RT WING LANDING GEAR DOOR ACTUATOR SUPPORT FITTING FWD INTERNAL KEEL BEAM FITTING FOUND CRACKED. REPLACED PER SRM 51-10-01 AND BOEING SB 747 53A2242.

Part: FRAME — CORRODED (L5 DOORWAY)

LEVEL 1 CORROSION ON L5 DOOR FRAME ASSY AFT CUTOUT. REPAIRED PER SRM 51-10-01.

Part: FRAME — CRACKED (BS 380)

MAIN DECK STA 380 SRINGER 25R FOUND FRAME CRACKED. REPAIRED PER SRM 53-12-00 AND HX RS 53-12-34011.

Part: SKIN — CRACKED (NR 2 PYLON)

NR 2 PYLON LEFT EXTERNAL SKIN CRACKED AT LOWER CUTOUT AREA. REPAIRED PER SRM 54-30-03.

Part: SPAR — CRACKED (NR 4 PYLON)

NR 4 PYLON MIDSPAR CRACKED AND DEFORMED UNDER HYD S/O VALVE. REPAIRED PER SRM 54-10-03.

Part: STRINGER — CRACKED (BS 360 & 380)

BS 360 TO BS 380 STRINGER 26R CHORD CRACKED. REPAIRED PER SRM 51-10-01.

Part: FRAME — CORRODED (BS 520)

LEVEL 1 CORROSION AT BS 520-540 UPPER DECK STRINGER 44L. REPAIRED PER SRM 53-10-05.

Part: SKIN — CORRODED (WS 440-1390)

LEVEL 1 SURFACE CORROSION FOUND ON LEFT WING UPPER SURFACE WS 440 - WS 1390. REPAIRED PER SRM 51-10-01 AND HXRS 57-25-34017.

Part: BULKHEAD SPLICE — CRACKED (BS 1480)

BULKHEAD BS 1480 LEFT AND RIGHT SIDE FOUND CRACKS IN SPLICE FITTING. REPAIRED SPLICE FITTING CRACKS PER HX RS 53-43-34021 AND BOEING SB 747-53A-2390.

Part: FITTING — CRACKED (LT MLG ACTUATOR)

LEFT SUPPROT FITTING FOR LEFT WLG ACTUATOR SUPPORT FOUND CRACKED. REPAIRED PER SRM 51-10-01 AND SB 747 53A2245.

Part: FLOOR — DELAMINATED (BS 540-600)

BS 540 TO 600 LBL 28 FLOOR PANEL FOUND DELAMINATED. REPAIRED PER SRM 51-40-06.

Part: FLOOR — DELAMINATED (BS 520-600)

BS 520 TO 600 LBL 47 FLOOR PANEL FOUND DELAMINATED. REPAIRED PER SRM 51-40-06.

Part: DOOR — DELAMINATED (LT MLG)

LEFT OUTBOARD STRUT DOOR FOUND DELAMINATED. REPLACED DOOR PER MM 32-14-05.

Part: SEAT TRACK — CORRODED (BS 520-540)

LEVEL 1 CORROSION ON SEAT TRACK ON UPPER DECK BS 520 TO 540. REPAIRED PER SRM 51-10-05.

Part: BRACKET — CRACKED (BS 880)

FOUND CRACKED SHEAR TIE BRACKET AT BS 880 S10L. REPAIRED PER SRM 53-10-04.

Part: FRAME — CRACKED (BS 1500)

FOUND CRACK ON FRAME AT BS 1500 STR 21L. REPAIRED PER SRM 51-30-01.

Part: SKIN — CORRODED (BS 740-1000)

LEVEL 1 CORROSION FOUND ON STA 740 TO STA 1000 LAP JOINT AT S12L. REPAIRED PER SRM 51-10-01.

Part: FRAME — CRACKED (BS 380)

FOUND CRACK IN FRAME AT BS 380 STR 24L. REPAIRED PER SRM 53-12-00 AND HKRS 5312 340011.

Part: JAMB — CORRODED (L5 DOORWAY)

LEVEL 1 SURFACE CORROSION FOUND ON MAIN DECK L5 DOOR CUTOUT. REPAIRED PER SRM 51-10-01.

Part: BRACKET — CRACKED (BS 1000)

WING CENTER TANK FRONT SPAR SUPPORT STIFFENER T BRACKET FOUND CRACKED AT BS 1000 RBL10. REPLACED PER SRM 51-10-01.

Part: FRAME — CRACKED (BS 1500)

FOUND CRACKED FRAME AT BS 1500 STR 21R. REPAIRED PER SRM 51-10-01.

Part: FAIRING — DELAMINATED (LT WING)

LEFT WING UPPER SURFACE INBOARD OF OUTBOARD AILERON TRAILING EDGE FIXED FAIRING FOUND DELAMINATED. REPAIRED PER SRM 51-40-12.

Part: BRACKET — CRACKED (BS 1520)

BRACKET AT BS 1520 STR 21R FOUND CRACKED. REPAIRED PER SRM 51-30-02.

Part: BRACKET — CRACKED (NR 4 PYLON)

NR 4 PYLON LOWER SPAR STIFFENER INBOARD TIE BRACKET FOUND CRACKED NAC STA 160. REPLACED PER SRM 51-10-01.

Part: STRAP — BROKEN (BS 620-680)

FWD CARGO COMPARTMENT STA 620 STR 680 LT SLOPE PANEL LOWER SUPPORT STRAP FOUND BROKEN. REPLACED PER SRM 51-10-01.

Part: SKIN — CORRODED (BS 741-1000)

LEVEL 1 CORROSION FOUND AT FUSELAGE STATION 741 TO 1000 RIGHT SIDE. REPAIRED PER SRM 51-10-01 AND F1-10-02.

Part: ANGLE — CRACKED (NR 4 PYLON)

NR 4 PYLON NACELLE STATION 221 INBOARD ANGLE CRACKED. REPAIRED PER SB 747-54-2042.

Part: SKIN — CRACKED (BS 360-380)

RT FLAT SIDE SKIN HOLE AND CRACKS FOUND AT STA 360/380 STR 7/STR9. REPAIRED PER HX RS-R53-11-33999 AND SRM 51-40-02.

Part: BRACKET — CRACKED (BS 2220)

BRACKET AT BS 2220L STR 21 L FOUND CRACKED. REPAIRED PER SRM 51-10-01.

Part: PLATE — CORRODED (L1 DOOR)

LEVEL 1 CORROSION FOUND AT L1 DOOR ASSY AFT FRAME CENTER GUIDE FITTING BASE PLATE. REPAIRED PER SRM 51-10-01 AND 51-10-02.

Part: STIFFENER — CRACKED (BS 440)

UPPER DECK VERTICAL STIFFENER AT BS 440L FOUND CRACKED. REPLACED PER SRM 51-10-01.

Part: FAIRING — DAMAGED (FUSELAGE)

RIGHT BODY FAIRING PANEL 194B FOUND DAMAGE. REPAIRED PER SRM 51-48-14.

Part: STOP — BROKEN (RT MLG DOOR)

RT WING LANDING GEAR WW DOOR FOUND BROKEN STOP ASSY. REPLACED PER MM 32-12-00.

Part: SKIN — CORRODED (WS 860-1010)

LEVEL 1 CORROSION FOUND ON RIGHT WING UPPER SURFACE WS 860 TO 1010. REPAIRED PER SRM 51-10-01, 57-30-01, MM 51-24-01.

Part: SKIN — CORRODED (WS 400-640)

LEVEL 1 CORROSION FOUND AT RIGHT WING UPPER SURFACE WING ROOT WS 400 TO 640. REPAIRED PER SRM 51-10-01, 57-30-01 AND MM 51-14-07.

Part: SKIN — CORRODED (WS 400-500)

LEVEL 1 CORROSION FOUND ON RIGHT WING SKIN STA 400 TO 500 UPPER SURFACE. REPAIRED PER SRM 51-10-01, 57-30-01 AND MM 51-04-07.

Part: PANEL — CORRODED (AILERON)

LEFT WING UPPER SURFACE OF OUTBOARD AILERON FIX PANEL SMALL AREA OF CORROSION. REPAIRED PER SRM 51-10-01 AND 51-10-02.

Part: SPAR — CORRODED (WS 410-1390)

LEVEL 1 CORROSION FOUND ON LEFT WING UPPER SURFACE OF REAR SPAR WS 410 TO 1390. REPAIRED PER SRM 51-10-01, 57-30-01 AND MM 51-14-07.

Part: SKIN — CORRODED (WS 830)

LEVEL 1 CORROSION ON LEFT WING LEADING EDGE STATION 830. REPAIRED PER SRM 51-10-01, 57-30-01 AND MM 51-14-07.

Part: SKIN — CORRODED (WS 830-1390)

LEVEL 1 CORROSION FOUND ON UPPER SURFACE OF LEFT WING WS 830 TO 1390. REPAIRED PER SRM 51-10-01, 57-30-01 AND MM 51-14-07.

Part: FAIRING — DAMAGED (FUSELAGE)

FUSELAGE FAIRING PANEL 194B FOUND 1.5 INCH HOLE. REPAIRED PER SRM 51-40-12 FIG 10.

Part: SKIN — CORRODED (WS 670-1080)

LEVEL 1 CORROSION FOUND ON UPPER SURFACE OF RT WING WS 670 TO 1080. REPAIRED PER SMR 51-60-01, 57-30-01 AND MM 51-24-07.

Part: BRACKET — CRACKED (NR 3 ENG COWL)

NR 3 LEFT POWER COWL FWD FRAME CRACKED BRACKET. REPAIRED PER SRM 51-10-01.

Part: PANEL — DAMAGED (FUSELAGE)

LOWER FUSELAGE PANEL 191DD FOUND CORNER DAMAGED. REPAIRED PER SRM 51-40-15.

Part: FRAME — CRACKED (BS 2120)

FRAME AT BS 2120R STR 22 AND 23R FOUND CRACKED. REPAIRED PER SRM 51-10-01.

Part: SKIN — DELAMINATED (LT ELEVATOR)

LEFT INBOARD ELEVATOR UPPER SURFACE FOUND A 1 BY 1 INCH AREA DELAMINATED. REPAIRED PER SRM 51-40-15.

Part: WEB — CORRODED (RT MLG WW)

RIGHT WING GEAR WELL FWD LOWER PANEL FOUND CORROSION ON INBOARD SIDE. REPAIRED PER SRM 51-10-01 AND 51-10-02.

Part: PANEL — DELAMINATED (VERT STAB)

LEFT STABILIZER LOWER PANEL 344GB FOUND DELAMINATED. REPAIRED PER SRM 51-40-06.

Part: FASTENER — CORRODED (BS 140-180)

LEVEL 1 CORROSION FOUND AT STA 140 TO 180 S23R TO S34R ON FASTENERS. REPAIRED PER SRM 51-10-01 AND 51-10-02.

Part: SKIN — DAMAGED (LT ELEVATOR)

LEFT INBOARD ELEVATOR TRAILING EDGE SEVERAL AREAS DAMAGED. REPAIRED PER SRM 51-40-15.

Part: LINK — WORN (RT AILERON)

RIGHT INBOARD AILERON/REACTION LINK FOUND WORN. REPAIRED AND REPLACED BEARINGS PER OHM 20-50-03.

Part: PANEL — CRACKED (TE WING)

TRAILING EDGE PANEL 673BB FOUND CRACKED. REPAIRED PER SRM 51-40-15.

Part: COWL — DAMAGED (NR 3 ENGINE)

NR 3 ENG LT POWER COWL LOWER CHORD FOUND DAMAGED. REPAIRED PER SRM 51-10-01.

Part: PANEL — DELAMINATED (VERT STAB)

LEFT STABILIZER PANEL 334 NBL FOUND DELAMINATED. REPAIRED PER SRM 51-40-01.

Part: SKIN — CORRODED (BS 520)

BS 520/720 S19R FOUND SURFACE CORROSION. REPAIRED PER SRM 51-10-01.

Part: FASTENER — DAMAGED (NR 2 PYLON)

NR 2 PYLON L/E FIXED PANEL FOUND 6 SHEARED FASTENERS. REPAIRED PER SRM 51-30-20.

Part: COWL — CRACKED (NR 3 ENGINE)

NR 3 RIGHT POWER COWL LOWER CHORD FOUND CRACKED. REPAIRED PER SRM 51-10-01.

Part: CHANNEL — DAMAGED (NR 3 ENGINE COWL)

NR 3 ENG LEFT POWER COWL BETWEEN 6/7 FRAMES CHANNEL DAMAGED. REPLACED PER SRM 51-10-01.

Part: STRAP — CORRODED (BS 1240)

LEVEL 1 CORROSION FOUND AT BS 124O R SPLICE STRAP A BOLT HOLES. REPAIRED PER OHM 62440006, SRM 51-10-01, 51-10-02.

Part: BULKHEAD — CORRODED (BS 1480)

LEVEL 1 CORROSION FOUND ON BS 1480 FWD SIDE. REPAIRED PER SRM 51-10-01 AND 51-10-02.

Part: PANEL — CORRODED (FUSELAGE)

LOWER FUSELAGE PANEL 192MR FOUND SURFACE CORROSION. REPAIRED PER SRM 51-10-01.

Part: PANEL — DENTED (VERT STAB)

RIGHT STABILIZER PANEL 341BR-341CR FOUND DENTED. REPAIRED PER SRM 51-10-02 AND SRM 51-00-00.

Part: DOOR — DAMAGED (EXT POWER)

FWD EXTERNAL POWER RECEPTICAL DOOR FOUND DAMAGED. REPAIRED PER SRM 51-40-15.

Part: PANEL — DELAMINATED (VERT STAB)

LEFT STABILIZER PANEL 334MB FOUND DISBONDED. REPAIRED PER SRM 51-40-06.

Part: STRINGER — CORRODED (BS 1319)

LEVEL 1 CORROSION ON BS 1319L STR 16 AND 17. REPAIRED PER SRM 51-10-01 AND 51-10-02.

Part: FAIRING — DELAMINATED (NR 2 PYLON)

NR 2 PYLON V FAIRING FORWARD LOWER AREA FOUND DELAMINATION. REPAIRED PER SRM 51-40-06.

Part: SEAL — LEAKING (NR 4 ENGINE)

NR 4 ENGINE LOST OIL QTY AND PRESSURE. OIL PRESSURE LIGHT CAME ON AND TEMP BEGAN TO RISE. ENGINE SHUT DOWN. FOUND OIL LEAK TO BE FROM CSD PAD. REPLACED CSD SEAL PER BOEING M/M 24-11-01, LEAK CHECK OK.

Part: HYD LINE — FAILED (LT MLG WW)

HYDRAULIC LEAK IN AREA OF LEFT WING ROOT, AFT PORTION OF W/W. REMOVED AND REPLACED HYD LINE PER 20-11-05 NEAR WING GEAR AFT TRUNNION. LEAK CK OK.

Part: PANEL — DELAMINATED (WATER SERVICE)

WATER SERVICE PANEL DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — CRACKED (LT WING)

LT WING FLYING PANEL WBL 197 CRACKED BY FITTING. REMOVED AND REPLACED FLYING PANEL IAW 51-10-01 AND 51-30-02.

Part: FLAP — CRACKED (LT TE MIDFLAP)

LT WING OTBD T/E MIDFLAP HAS 3 FT CRACK ON TRAILING EDGE. PREPARED AREA OF REPAIR, INJECTED CORE ALONG CRACK AND APPLIED FIBERGLASS LAYERS IAW 747 SRM 51-40-09.

Part: SKIN — DELAMINATED (RT TE FOREFLAP)

RT WING T/E INBD FOREFLAP LEADING EDGE SKIN DELAMINATED. SANDED DAMAGED AREA, SMOOTH AND REMOVED DELAMINATED AREA. APPLIED FILLER WITH FIBERGLASS OVERLAYS IAW SRM 51-40-15.

Part: SKIN — CRACKED (LE ELEV)

LEFT INBOARD ELEVATOR LOWER SKIN CRACKED. REPAIRED PER BOEING SRM 51-40-09.

Part: PANEL — DELAMINATED (LT TE FLAP)

LT WING T/E FLAP FIXED PANEL JUST INBOARD OF NR 1 PYLON DELAMINATED. REMOVED DAMAGE, APPLIED FILLERS AND DOUBLERS IAW SRM 51-40-09.

Part: SKIN — DENTED (RT TE FOREFLAP)

RT WING T/E OUTBD FOREFLAP LEADING EDGE DENTED O/B OF O/B LINK. REMOVED DAMAGE PLYS, REMOVED CORD AND REPLACED. FABRICATED FIBERGLASS FILLER AND OVERLAYS AND BONDED IAW SRM 51-40-15.

Part: SEAL — LEAKING (NR 2 GEARBOX)

EXCESSIVE OIL CONSUMPTION ON NR 2 ENG. FOUND GEN GARLOCK SEAL LEAKING. REPLACED SAME, LEAK CHECK GOOD REF MM 72-61-08. RAN ENG AT PART POWER PER MM 71-00-00.

Part: SKIN — DELAMINATED (LT TE FLAP)

LT WING T/E INBD FLAP MIDFLAP DELAMINATED ON LEADING EDGE AREA. REPAIRED FLAP SKIN IAW SRM 51-40-09.

Part: DOOR — DAMAGED (APU COMPT)

APU BATTERY COMPARTMENT DOOR DAMAGED AT AFT CORNER ON AFT FLANGE. REPAIRED DAMAGE AT APU ACCESS DOOR IAW SRM 51-40-02, 51-30-02 AND 51-10-01.

Part: PANEL — CRACKED (FUSELAGE)

PANEL 191H CRACKED AND DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.

Part: FLAP — DELAMINATED (LT TE MIDFLAP)

LT WING I/B T/E MIDFLAP LEADING EDGE DELAMINATED. REPAIRED DELAMINATED AREA BY CUTTING OUT DAMAGE, POTTING CORE AND APPLYING FIBERGLASS OVERLAYS IAW SRM 51-40-09.

Part: PANEL — DAMAGED (BS 1000)

LOWER FUSELAGE BS 1000 PANEL 191AR FORWARD CORNER DAMAGED. REPAIRED PER SRM 51-40-09.

Part: PANEL — DELAMINATED (BS 1000)

LOWER FUSELAGE BS 1000 PANEL 191AL AND SKIN ON INSIDE DELAMINATED. REPAIRED PER SRM 51-40-15.

Part: SKIN — CRACKED (RT MLG WW)

RT BODY GEAR CUT OUT WEB FOR OLEO STRUT CLOSURE SKIN CRACKED ON I/B SIDE. REPAIRED PER SRM 51-40-02.

Part: HINGE — CORRODED (AC BAY DOOR)

A/C PANEL 192HR LOWER FUSELAGE HINGE CORRODED. REMOVED LIGHT SURFACE CORROSION FROM A/C BAY DOOR IAW SRM 51-10-01.

Part: SKIN — DELAMINATED (LT TE FLAP)

LT WING T/E FLAP O/B AFT FLAP DELAMINATED. REPAIRED PER MM 27-51-00.

Part: FRAME — CORRODED (FUSELAGE)

AIR CONDITIONING PANEL 191A CORRODED FRAME UNDERNEATH. REMOVED MINOR SURFACE CORROSION IAW 51-10-02.

Part: SKIN — WORN (BS 640)

FUSELAGE FWD LOWER EXTERNAL SKIN BS 640 HAS LOOSE FASTENERS AT LOWER LAP SEAMS. REMOVED AND REPLACED FASTENERS IAW SRM 51-30-02.

Part: TRIM STRIP — CRACKED (FUSELAGE)

LOWER FUSELAGE PANEL 191ER TRIM STRIP CRACKED. REPAIRED PER SRM 51-40-09.

Part: SKIN — CRACKED (LT WING)

LT WING INBD T/E UPPER SURFACE PANEL JUST FORWARD OF FLYING PANEL IS CRACKED. SANDED PANEL REMOVED DAMAGE SKIN, FABRICATED REPAIR IAW SRM 51-40-15.

Part: PANEL — CRACKED (FUSELAGE)

LOWER FUSELAGE LOWER PANEL 191A 2 CRACKS IN UPPER SURFACE. REPAIRED DAMAGED PANEL IAW SRM 51-40-15.

Part: PANEL — DELAMINATED (FUSELAGE)

PANEL 192MR DELAMINATED AND WITH A HOLE. PANEL REPAIRED IAW SRM 51-40-09.

Part: PANEL — CRACKED (FUSELAGE)

LOWER FUSELAGE AIR COND PANEL 192A CRACKED ON PREVIOUS REPAIR ON UPPER SURFACE. FOUND AND REMOVED OIL AND WATER. CUT OUT DAMAGED AREA AND REPLACED DAMAGED FIBERGLAS IAW 51-40-15.

Part: CLIP — CRACKED (RT MLG WW)

RIGHT BODY GEAR WHEEL WELL CRACKED ANGLE CLIP. REPLACED ANGLE CLIP PER SRM 51-10-01.

Part: SKIN — HOLE (NR 2 PYLON)

NR 2 PYLON HYD DOOR LT INBOARD SKIN HAS HOLE. REPAIRED HOLE IN DOOR PER SRM 51-40-06.

Part: PANEL — CRACKED (FUSELAGE)

LOWER FUSELAGE PANEL 191NL INBD CORNER CRACKED. FOUND PAINT BUILDUP TO BE CRACKED. SANDED AND INSP AREA NO CRACK FOUND IAW SRM 51-40-15.

Part: STANCHIONS — CRACKED (E/E COMPT)

BS 460 RBL 55 LBL 55 E AND E COMPT STANCHIONS CRACKED AND BROKEN BY CANON PLUG ATTACHMENTS. INSTALLED NEW STANCHIONS IAW SRM 51-10-01.

Part: BRACKET — CORRODED (AC COMPT DOOR)

PANEL 191A HOLD OPEN BRACKET CORRODED AND GOUGED. REPAIRED BRACKET PER SRM 51-10-01.

Part: FAIRING — DELAMINATED (FUSELAGE)

LT FUSELAGE LWR FAIRING FWD OF W/GEAR W/W DELAMINATED. REPAIRED PER SRM 51-40-09.

Part: STANCHION — CRACKED (BS 640)

BS 460 RBL 20 STANCHION CRACKED AND BROKEN AT CANON HOLES. REMOVED AND REPAIRED STANCHION 51-10-01.

Part: SKIN — DELAMINATED (WS 1196)

RT WING T/E UPPER SKIN PANEL WS 1196 DELAMINATED ON BOTTOM SURFACE. FABRICATED FIBERGLASS FILLERS AND OVERLAYS AND BONDED NEW REPAIR PER SRM 51-40-15.

Part: HYD DOOR — CHAFED (NR 2 PYLON)

NR 2 PYLON LT HYDRAULIC DOOR CHAFED ON FWD INBOARD SKIN. REMOVED PRIMER FROM CHAFED AREA, FABRICATED DOUBLER THEN BONDED DOUBLER TO REPAIR AREA IAW SRM 51-40-06.

Part: BRACKET — CORRODED (AC DOORWAY)

AIR CONDITIONING DOORS LOWER FUSELAGE LATCH BRACKET CORRODED. REPLACED PER SRM 51-30-02.

Part: PANEL — DAMAGED (RT WING)

RT WING FLYING PANEL PULLED FASTENERS. REMOVED AND REPLACED FASTENERS IAW SRM 51-30-02 AND 51-32-03.

Part: SKIN — DELAMINATED (RT TE AFT FLAP)

R/WING AFT FLAP LOWER SKIN L/E DELAMINATED. REPAIRED DELAMINATION BY REMOVING DELAM, POTTING CORE AND PUTTING ON FIBERGLASS OVERLAYS IAW SRM 51-40-09.

Part: SKIN — DAMAGED (BS 680)

FUSELAGE BS 680 WORKING FASTENERS BETWEEN CORNER LAP SEAMS. REPAIRED WORKING FASTENERS PER SRM 51-30-02.

Part: SKIN — DELAMINATED (RT TE AFT FLAP)

RT WING T/E O/B OR I/B AFT FLAP DELAMINATED I/B OF O/B TRACK. REPAIRED IAW SRM 51-40-09.

Part: SKIN — CRACKED (NR 2 PYLON)

CRACKED SKIN ON NR 2 PYLON ADJACENT TO PANEL 463EL. REPAIRED PER BAC SRM 54-30-03.

Part: PANEL — DELAMINATED (BS 1012)

DELAMINATION ON FUSELAGE PANEL 192HR AT BS 11012, BL 9. REPAIRED PER BAC SRM 51-40-09.

Part: SKIN — DAMAGED (BS 1260)

DAMAGED FUSELAGE SKIN PANEL IN RIGHT WING GEAR WHEEL WELL AT BS 1260. REPAIRED DAMAGE AND REPLACED FASTENERS PER BAC SRM 53-30-02 AND 53-30-03.

Part: DOOR SKIN — PUNCTURED (NR 2 PYLON)

HOLE IN LEFT HYDRAULIC SERVICE DOOR (SAILBOAT) ON NR 2 PYLON. REPAIRED PER BAC SRM 51-40-06.

Part: PANEL — CRACKED (BS 1054)

TWO CRACKS ON UPPER SURFACE OF PANEL 191A AT BS 1054. REPAIRED PER BAC SRM 51-40-15.

Part: ANGLE — CRACKED (NR 2 PYLON)

CRACK ON LEADING EDGE UPPER HORIZONTAL WEB INBOARD ATTACH ANGLE. REPAIRED PER BAC SRM 51-30-03.

Part: PANEL — CORRODED (BS 1240)

LEVEL 1 CORROSION UNDER HINGE PANELS ON FUSELAGE PANEL 192A AT BS 1240. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.

Part: PANEL — DEBONDED (VERT STAB)

DEBONDING AND EROSION ON PREVIOUS REPAIR ON RIGHT EXTERIOR PANEL ON VERTICAL STABLIZER. REPAIRED PER BAC SRM 51-40-09.

Part: FAIRING — DELAMINATED (LT TE FLAP)

DELAMINATION ON LEFT OUTBOARD FLAP OUTBOARD HINGE FAIRING PANEL. REPAIRED PER BAC SRM 51-40-09.

Part: BRACKET — CRACKED (NR 4 PYLON)

CRACKED INBOARD AND OUTBOARD SUPPORT BRACKETS ON NR 4 PYLON LOWER FIREWALL RIB. REPLACED SUPPORT BRACKETS PER BAC SRM 51-30-02.

Part: HYD PUMP — CRACKED (NR 2 ENGINE)

NR 2 HYD SYS FAILURE IN FLIGHT, HYD QTY WENT TO ZERO/LOW QTY LIGHT ON, ADP AND EDP LOW PRESS LIGHTS ON. FOUND CRACKED NR 2 EDP CASE. EDP BLANKING KIT INSTALLED IAW MM 29-11-05, MM 72-61-00. NO CONTAMINATION FOUND IN NR 2 SYS FILTERS. EDP CASE DRAIN FILTER REPLACED DUE TO SLIGHT METAL CONTAMINATION. SYSTEM FLUSHED, NIL FURTHER CONTAMINATION. LEAK CHECK OKAY PER MM 29-11-00.

Part: FOREFLAP — DELAMINATED (RT TE FOREFLAP)

DELAMINATED RT OTBD FOREFLAP O/B END. REPAIRED PER SRM 51-40-15.

Part: SUPPORT — CHAFED (NR 4 ENG COWL)

CHAFE ON INBD CORE COWL UPPER FLANGE INBD SUPPORT NR 4 ENGINE. REPAIRED PER SRM 51-10-01.

Part: COWL HINGE — CRACKED (NR 3 ENGINE)

CRACKED NR 3 ENG INBD CORE COWL AFT TOP HINGE. REPAIRED PER SRM 51-30-02.

Part: FASTENERS — LOOSE (EXHAUST SLEEVE)

LOOSE/WORKING FASTENERS AT 5 O'CLOCK POSITION NR 3 ENG EXHAUST SLEEVE. REPARIED PER SRM 51-30-02.

Part: FASTENERS — LOOSE (NR 3 ENG COWL)

LOOSE FASTENERS NR 3 ENG INBD CORE COWL EXTERIOR SKIN BELOW PRECOOLER DOOR CUTOUT. REPAIRED PER SRM 51-30-02.

Part: FASTENERS — LOOSE (LT WING)

LOOSE FASTENERS, L WING UPPER WING TO BODY PANEL. RETORQUED/REPLACED PER M/M 20-51-01.

Part: JAMB NUT — LOOSE (NR 3 PYLON)

LOOSE RETURN LINE NR 3 PYLON JAM NUT HOLE ELONGATED. REPAIRED PER SRM 51-10-03.

Part: HINGE HOOK — CRACKED (NR 3 ENGINE COWL)

CRACK RIB, 4TH HINGE HOOK FROM FWD END NR 3 CORE COWL. REPARIED PER SRM 51-30-02.

Part: FASTENERS — LOOSE (NR 3 ENG COWL)

LOOSE FASTENERS, NR 3 CORE COWL NR 3 LATCH GUIDE PIN PREVIOUS REPAIR. REPAIRED PER SRM 51-30-02.

Part: PANEL — DELAMINATED (LT WING)

DELAMINATION, L/WING T/EDGE PANEL 573CB. REPAIRED PER SRM 51-40-15, 51-30-02.

Part: FLOOR — TORN (BS 678)

THREE TEARS IN FWD LWR CARGO COMP AT STA 678. REPAIRED PER SRM 51-30-02.

Part: BRACKET — BROKEN (LT WING)

BROKEN WIRE BUNDLE BRACKET, L WING AFT OF NR 7 LED. REMOVED AND REPLACED PER SRM 51-10-01, 51-30-02.

Part: TR SLEEVE — DAMAGED (NR 1 ENGINE)

UPGRADE PREVIOUS REPAIR, NR 1 ENGINE L/THRUST REVERSER SLEEVE 7 O'CLOCK POSITION. REPAIRED PER SRM 51-40-06.

Part: FASTENERS — LOOSE (NR 2 PYLON)

MISSING FASTENERS ON NR 2 PYLON AFT INBD SKIRT. REPAIRED PER SRM 51-30-02.

Part: SKIN — GOUGE (BS 2594)

GOUGE IN SKIN AT STATION 2594 AT S47L. REPAIRED PER SRM 51-10-01.

Part: FASTENERS — LOOSE (NR 3 ENG COWL)

LOOSE FASTENERS, NR 3 ENGINE INBD CORE COWL - NR 3 HINGE HOOK. REMOVED AND REPLACED PER SRM 51-30-02.

Part: FASTENER — MISSING (EXHAUST SLEEVE)

MISSING FASTENERS ON NR 2 ENGINE EXHAUST SLEEVE. REMOVED AND REPLACED PER SRM 51-30-02.

Part: PANEL — DELAMINATED (RT WING)

DELAMINATED, R/WING T/EDGE PANEL NR 681GB. REPAIRED PER SRM 51-40-09.

Part: COWL — GOUGED (NR 3 ENGINE)

GOUGE NR 2 ENGINE INLET COWL AT 3 O'CLOCK POSITION. REPAIRED PER SRM 51-40-06, 51-24-11.

Part: TAIL CONE — DELAMINATED (AFT FUSELAGE)

DELAMINATION, TAIL CONE - UPPER SURFACE, ABOVE APU TAILPIPE. REPAIRED PER SRM 53-30-03.

Part: LIGHT BOX — CRACKED (NLG)

ONE CRACK IN AFT CORNER NLG LIGHT BOX. REPAIRED PER SRM 51-40-09.

Part: PANEL — DELAMINATED (LT WING)

DELAMINATED LT WING T/E PANEL. REPAIRED PER SRM 51-40-15.

Part: RADOME — DELAMINATED (FWD FUSELAGE)

DELAMINATED RADOME FWD TIP. REPAIRED PER SRM 53-58-03.

Part: HINGE — CRACKED (NR 3 ENGINE COWL)

CRACKED HOOK ATTACH RIB TOP MOST AFT HINGE ON NR 3 ENGINE O/B CORE COWL. REPARIED PER SRM 51-30-02.

Part: STOP FITTING — CRACKED (LT MLG DOOR)

CRACK IN L BODY GEAR INBD DOOR AFT STOP FITTING. REMOVED AND REPLACED PER MM 32-14-00.

Part: PANEL — DELAMINATED (LT WING)

DELAMINATION, L/WING T/EDGE PANEL 581KB. REPAIRED PER SRM 51-40-09.

Part: CANOE FAIRING — CRACKED (NR 3 TE FLAP)

CRACKED NR 3 FLAP TRACK CANOE FAIRING LEFT WING. REPAIRED PER SRM 51-40-11.

Part: BRACKET — CRACKED (NR 3 ENG COWL)

CRACK IN NR 3 ENGINE - OTBD CORE COWL AFT RIB - TOP REINFORCING ANGLE. REPAIRED PER SRM 51-30-02, 51-12-02.

Part: BRACKET — DAMAGED (RT WING)

DAMAGED BRACKET, R/WING L/EDGE AFT OF NR 15 LED. REPAIRED PER SRM 51-30-02, 51-10-01.

Part: SKIN — GOUGE (LT TE FOREFLAP)

ONE GOUGE IN LT O/B FOREFLAP, O/B L/E. REPAIRED PER SRM 51-40-15 AND SRM 51-24-11.

Part: DOUBLER — LOOSE (LT DOOR FRAME)

LOOSE DOUBLER - L DOOR FRAME. REPAIRED PER SRM 51-30-02, SRM 51-10-06.

Part: COWL — CHAFED (NR 4 ENGINE)

CHAFED FWD LWR EXHAUST DUCT ON NR 4 OUTBD CORE COWL. BLEND CHAFE PER SRM 51-01-01.

Part: PANEL — DELAMINATED (LT WING)

DELAMINATED LT WING T/E PANEL 5762B. REPAIRED PER SRM 51-40-09.

Part: PRECOOLER FTG — CRACKED (NR 4 ENGINE)

CRACK IN FWD FITTING ASSY PRE-COOLER ASSY BRACKET, NR 4 ENGINE LT SIDE AFT. REMOVED AND REPLACED BRACKET PER MM 36-12-01.

Part: RIVETS — LOOSE (NR 4 ENG COWL)

LOOSE RIVETS - NR 4 CORE COWL AFT LATCH ATTACH ANGLE. REPAIRED PER 51-30-02.

Part: FASTENERS — DAMAGED (NR 4 ENG COWL)

BENT/PULLED FASTENERS ON NR 4 ENGINE OUTBD CORE COWL UPPER FLANGE. REPAIRED PER SRM 51-30-02.

Part: CHANNEL — CRACKED (LWR FUSELAGE)

CRACKED CHANNEL - KEEL BEAM AREA - BETWEEN BODY GEAR DOORS. REPAIRED PER SRM 51-30-02, 51-30-00.

Part: FAIRING — DAMAGED (LT TE FLAP)

HOLE -MARKED- L/WING T/EDGE OUTBD FLAP CANOE (NR 7 TRACK). REPAIRED PER SRM 51-40-09.

Part: SKIN — DELAMINATED (NR 10 LE FLAP)

DELAMINATED, L/WING NR 10 LED AFT END. REPAIRED PER SRM 51-40-09.

Part: STATIC WICK — CORRODED (RT HORIZ STAB)

2 CORRODED STATIC WICKS LOCATED ON RT STABILIZER. REPAIRED PER SRM 51-10-06.

Part: FASTENERS — MISSING (RT WING)

MISSING FASTENERS RT WING TOP L/E NR 20 LEP. REPAIRED PER SRM 51-30-02.

Part: FASTENERS — MISSING (CARGO DOOR)

MISSING 3 FASTENERS, AFT CARGO DOOR - LOWER AFT CORNER PREVIOUS REPAIR. REPARIED PER SRM 51-30-02.

Part: PANEL — DELAMINATED (LT WING)

DELAMINATION - L WING T/EDGE PANEL 573AB. REPAIRED PER SRM 51-40-15.

Part: SKIN — GOUGE (BS 2594)

GOUGE AT BS 2594 AT S45R. REPAIRED PER SRM 53-10-01, 51-40-01, 51-10-06.

Part: BRACE — CHAFED (NR 1 PYLON)

DIAGONAL BRACE CHAFFED FWD END RT SIDE NR 1 ENGINE PYLON. REWORKED AREA PER BOEING SRM 54-40-01.

Part: BRACE — CHAFED (NR 4 PYLON)

DIAGONAL BRACE CHAFFED FWD ENG RIGHT SIDE NR 4 ENGINE PYLON. REWORKED AREA PER BOEING SRM 54-40-01.

Part: BRACE — CHAFED (NR 2 PYLON)

DIAGONAL BRACE CHAFFED FWD END RIGHT SIDE NR 2 ENGINE PYLON. REWORKED AREA PER BOEING SRM 54-40-01.

Part: BRACE — CHAFED (NR 1 PYLON)

DIAGONAL BRACE CHAFED 2 PLACED LEFT SIDE NR 1 ENGINE PYLON. REWORKED PER BOEING SRM 54-40-01.

Part: BRACE — BROKEN (LT WING)

LEFT WING SUPPORT BRACE BROKEN BY NR 6 LEADING EDGE. REMOVED AND REPLACED TUBE ASSY AS PER BOEING MM 57-21-00.

Part: ACTUATOR BEAM — BROKEN (RT MLG DOOR)

RIGHT WING GEAR DOOR REMAINED OPEN AFTER LANDING. FOUND BROKEN RIGHT WING LANDING GEAR DOOR ACTUATOR BEAM. REPLACED ACTUATOR BEAM PER BOEING M/M 32-32-28. CHECKED DOOR RIG PER M/M 32-12-04.

Part: FRAME — CORRODED (NR 1 PYLON)

LEVEL 2 CORROSION, NR 1 PYLON CORROSION ON THE BOTTOM END OF RIGHT FRAME AT NAC STA 162 WL 140.5 SB 54A2159 FINDING. REPAIRED FRAME IAW BOEING SRM 54-10-03 FIG 1.

Part: SKIN — CRACKED (NR 3 PYLON)

NR 3 PYLON SKIN IS CRACKED ON INBD SIDE UNDER SKIN DOUBLER AT NAC ST 180 NAC WL 140.2-142.2, REPAIRED IAW SB 54-2034. NON ROUTINE CARD S/N 6144.

Part: BULKHEAD CHORD — CRACKED (NR 1 PYLON)

CRACK FOUND ON NR 1 PYLON AFT BULKHEAD, INBD VERTICAL CHORD INBD ROW NR 4 FASTENER HOLE, .125 INCH LONG CRACK. REPLACED CHORD IAW SRM 51-10-01 AND SB 747-54A2159 NON ROUTINE CARD S/N 6006.

Part: SPAR CAP — CORRODED (RT WING)

LEVEL 1 CORROSION, WING FRONT SPAR UPPER CAP HAS LIGHT SURFACE CORROSION AT NAC ST 305 RWBL 472-473. REMOVED CORROSION IAW BOEING SRM 51-10-01 NON ROUTINE CARD S/N 7059.

Part: SKIN — CRACKED (NR 1 PYLON)

NR 1 PYLON OUTBD SKIN CRACKED UNDER DOUBLER AT NAC ST 180 NAC WL 140.2. STOP HOLE DRILLED IAW BOEING SRM 51-10-01 SKIN REPAIRED IAW SB 54-2034 FIG 5.

Part: LONGERON — CORRODED (BS 1300-1325)

LEVEL 2 CORROSION, LONGERON BS 1300-1325. REPAIRED PER HAECO RS 53-41-33455. NON ROUTINE CARD S/N 6543.

Part: ACTUATOR BEAM — ELONGATED (BS 580/660)

FASTENER HOLE ELONGATED AT BS 580 AND 660. REPAIRED PER HAECO RS 53-21-33435.

Part: SHEAR TIE — CORRODED (BS 520)

LEVEL 2 CORROSION, SHEAR TIE CORRODED AT BS 520 STR 40R-41R. REPAIRED PER HAECO RS 53-11-33436. NON ROUTINE CARD S/N 5844.

Part: SKIN — CORRODED (BS 2484)

LEVEL 2 CORROSION, SKIN BS 2484 STR 20L-23L. REPAIRED PER HAECO RS 53-21-33454. NON ROUTINE CARD S/N 6404.

Part: SKIN — CORRODED (NR 3 PYLON)

LEVEL 1 CORROSION, NR 3 PYLON AREA LOWER WING SKIN EXTENSION HAS FRETTING TYPE CORROSION AT RWBL 450-456 NAC ST 301.4-306. REMOVED CORROSION IAW SRM 51-10-01 AND REPROTECTED IAW SRM 51-10-02, MM 51-24-11 BLEND OUT IS WITHIN SRM 57-30-01 LIMITS. NON ROUTINE CARD S/N 7083.

Part: SKIN — CORRODED (RT WING)

LEVEL 1 CORROSION ON UNDERWING SKIN AT OUTBD MIDSPAR FITTING RWBL 840. REMOVED CORROSION AND REPROTECTED IAW BOEING SRM 51-10-02. BLEND OUT WITHIN BOEING SRM 57-30-01 LIMITS NON ROUTINE CARD S/N 7004.

Part: BULKHEAD TEE — CORRODED (NR 2 PYLON)

LEVEL 1 CORROSION, NR 2 PYLON TORQUE BULKHEAD 'T' CHORDS HAVE LIGHT SURFACE CORROSION AT NAC ST 301 WL 296-288. REMOVED CORROSION IAW BOEING SRM 51-10-01 AND IS WITHIN SRM LIMITS SRM 54-10-01.

Part: SKIN — CRACKED (NR 1 PYLON)

LEVEL 2 CORROSION, NR 1 PYLON INBD SKIN UNDER DOUBLER HAS CRACK AND CORROSION AT NAC STA 180 WATER LINE 140.2. REPAIRED IAW SB 747-54-2034 FIG 5.

Part: REVEAL PANEL — CRACKED (L 5 DOOR)

MAIN DECK L-5 DOOR FORWARD LOWER CORNER CUT OUT REVEAL PANEL CRACKED. REPLACED PANEL PER BOEING SRM 51-10-01.

Part: FRAME — CRACKED (NR 3 PYLON)

NR 3 PYLON INBD FRAME AT NAC STA 192 WL 153 IS CRACKED AND DEEP CHAFING ADJACENT TO LANYARD CLIP. REPLACED FRAME PER BOEING SRM 51-10-01.

Part: BULKHEAD TEE — CRACKED (NR 1 PYLON)

CRACK FOUND BY NDT METHOD AT THE FASTENER HOLE, NR 1 PYLON AFT BULKHEAD RT SIDE 'T' CHORD. REPLACED 'T' CHORD.

Part: BEAM — CORRODED (L 4 DOOR)

LEVEL 2 CORROSION, MAIN DECK L-4 DOOR BEAM CORROSION/CRACK REVEAL DURING LOWER GATE ASSY. REPLACED L-4 DOOR LOWER BEAM.

Part: FRAME — CRACKED (NR 3 PYLON)

NR 3 PYLON INBD FRAME AT NAC STA 162 WL 146 HAS DEEP CHAFE MARK. REPLACED FRAME PER BOEING SRM 51-10-01.

Part: FRAME — CRACKED (NR 4 PYLON)

NR 4 PYLON INBD AND OUTBD FRAME AT NAC/STA 162 WL 150 HAVE INCORRECT REPAIR, INBD FRAME IS CRACK AND THERE ARE MISSING AND INCORRECT FASTENER AT THE SAME LOCATION. REPLACED FRAME.

Part: SKIN — DELAMINATED (NR 2 SPOILER)

LHW NR 2 SPOILER CENTER SURFACE AREA DELAMINATED. HOT BONDED CUT OUT PER BOEING SRM 51-40-06.

Part: BUKLHEAD CHORD — CRACKED (BS 1000)

CRACK FOUND APPX 1.25 INCH LONG ALONG RADIUS, FORWARD CARGO COMPARTMENT BS 1000 BULKHEAD LOWER CHORD BETWEEN S-46L AND S-47L. STOP DRILLED AS PER SB 747-53-2316.

Part: FITTING — CRACKED (BS 1900)

CRACK FOUND AT BS 1900 AFT CARGO DOOR AFT ROTARY ACTUATOR SUPPORT BEAM. REPLACED FITTING.

Part: FRAME — CRACKED (R2 DOOR)

CRACK FOUND MAIN DECK R-2 DOOR FORWARD LOWER CORNER DOOR FRAME. REPAIRED PER BOEING SRM 52-10-02 FIG 8.

Part: BULKHEAD CHORD — CRACKED (BS 1000)

CRACK FOUND APPX 1.25 INCH LONG ALONG RADIUS FORWARD CARGO COMPARTMENT, BS 1000 BULKHEAD LOWER CHORD BETWEEN S-46R TO S-47R, STOP DRILLED AS PER SB 747-53-2316.

Part: FRAME — CRACKED (R4 DOOR)

CRACK FOUND MAIN DECK R-4 DOOR AFT LOWER CORNER DOOR FRAME. REPAIRED PER BOEING SRM 52-10-02 FIG 8.

Part: FRAME — CRACKED (L3 DOOR)

CRACK FOUND AT FORWARD LOWER CORNER, MAIN DECK L-3 DOOR FORWARD DOOR FRAME. REPAIRED PER BOEING SRM 52-10-02 FIG 8.

Part: BULKHEAD — CRACKED (BS 400)

FORWARD CARGO BS 400 LBL 90 BULKHEAD CRACKED NOSE TUNNEL BS 400 RT SIDEWALL AREA BULKHEAD WEB CRACKED AT RBL 90 APPX. REPAIRED CUTOUT PER SB 747-53-2095.

Part: SKIN — DELAMINATED (NR 3 SPOILER)

LHW NR 3 SPOILER OUTBD AFT CORNER SKIN LIFTED UP, LHW NR 3 SPOILER OUTBD MIDDLE SURFACE FOUND DELAMINATED. HOT BONDED CUT OUT PER BOEING SRM 51-40-06.

Part: SKIN — CRACKED (BS 540)

LEVEL 2, CORROSION FOUND FUSELAGE BS 540 STR 46R - 47R FUSELAGE SKIN BULGED. REPAIRED SKIN PER RS 53-21-33431.

Part: FLOOR BEAM — CRACKED (BS 1860)

AFT CARGO FLOOR SUPPORT CRACK AT BS 1860 LBL 5. REPAIRED FLOOR SUPPORT PER BOEING SRM 51-40-04.

Part: BULKHEAD CHORD — CRACKED (BS 1000)

CRACK FOUND APPX 1.25 INCH LONG ALONG RADIUS, FORWARD CARGO COMPARTMENT, BS 1000 BULKHEAD LOWER CHORD BETWEEN S-46L AND S-47L. STOP DRILLED PER SB 747-53-2316.

Part: FLOOR BEAM — CRACKED (BS 620)

FORWARD CARGO FLOOR SUPPORT FOUND CRACKED AT BS 620 LBL 6. REPAIRED FLOORBEAM PER BOEING SRM 51-40-04 FIG. 2, AFTER TRIM OFF CRACKED AREA.

Part: SKIN — DELAMINATED (NR 8 SPOILER)

RHW NR 8 SPOILER OUTBD SURFACE FORWARD CORNER AREA FOUND DELAMINATION RHW NR 8 SPOILER AFT EDGE LIFTED UP OUTBD TO CENTER INBD TO INBD CORNER AREA. HOT BONDED CUT OUT PER BOEING SRM 51-40-06.

Part: LONGERON — CRACKED (BS 1457-1467)

CRACK FOUND FROM BS 1457-1467 10, LEFT OVERWING LONGERON (FUSELAGE). REPAIRED LONGERON AS PER BOEING SRM 53-10-10 FIG 1.

Part: FRAME — CRACKED (L3 DOOR)

CRACK FOUND AT FORWARD LOWER CORNER, MAIN DECK L-3 DOOR FWD DOOR FRAME. REPAIRED PER BOEING SRM 52-10-02 FIG 8.

Part: SKIN — DELAMINATED (NR 5 SPOILER)

LHW NR 5 SPOILER AFT EDGE OUTBD TO CENTER AREA FOUND DELAMINATION AND LIFTED UP, LHW NR 5 SPOILER INBD FORWARD TOP CORNER AREA FOUND DELAMINATED. HOT BONDED CARRIED OUT PER BOEING SRM 51-40-06.

Part: SKIN — SCRATCHED (BS 430-440)

SCRATCH MARK FOUND FUSELAGE BS 430-440 STR 45R SKIN. REPAIRED SKIN PER BOEING SRM 53-30-03 FIG 1 AT BS 430-440 S45R.

Part: STRINGER — CORRODED (BS 995)

LEVEL 2, CORROSION FOUND FWD CARGO COMPARTMENT, BS 995 STR 44R STR. REPAIRED STRINGERS PER BOEING SRM 53-10-03 FIG 1 AT BS 980-996 STR 44R AREA.

Part: FITTING — CRACKED (L 3 DOOR)

L-3 DOOR FORWARD CUTOUT NR 4 STOP FITTING CRACK FOUND. REPLACED FITTING PER BOEING SRM 51-10-01.

Part: FITTING — CRACKED (R 3 DOOR)

R-3 DOOR FORWARD CUTOUT NR 4 STOP FITTING CRACK FOUND. REPLACED FITTING PER BOEING SRM 51-10-01.

Part: SKIN — DELAMINATED (NR 3 SPOILER)

RHW NR 7 SPOILER INBD AFT CORNER LIFTED UP. HOT BONDED CUT OUT PER BOEING SRM 51-40-06.

Part: CONNECTOR — MISWIRED (FUEL SOV)

APPARENT MALFUNCTION DETECTED DURING OPERATIONAL CHECKS OF THE ENGINE FUEL SHUT OFF VALVES. IT WAS NOTICED THE INDICATOR LIGHTS DID NOT RESPOND TO MOVEMENT OF THE ENGINE START LEVERS ON THE PEDESTAL; WHEREAS, NORMAL RESPONSE WAS OBSERVED DURING OPERATION OF THE FIRE SWITCHES ON THE OVERHEAD PANEL. INVESTIGATION SHOWED THAT WIRES W629-1Q1221-20 AND 1Q1223-20 WERE SPLICED TOGETHER NEAR CONNECTOR D2316P. THE WIRING DIAGRAM SHOWED THESE WIRES AS TERMINATING IN PINS 12 AND 11 OF CONNECTOR D2316P. SIMILAR DISCREPANCIES WERE FOUND FOR EACH OF THE OTHER ENGINE SHUT OFF VALVES. THE EFFECT OF THIS MODIFICATION WAS TO BYPASS THE FUNCTION OF THE ENGINE FUEL SHUT OFF SWITCHES ASSOCIATED WITH THE ENGINE START LEVERS.

Part: CONNECTOR — MISWIRED (FUEL SOV)

APPARENT MALFUNCTION DETECTED DURING OPERATIONAL CHECKS OF THE ENGINE FUEL SHUT OFF VALVES. IT WAS NOTICED THE INDICATOR LIGHTS DID NOT RESPOND TO MOVEMENT OF THE ENGINE START LEVERS ON THE PEDESTAL; WHEREAS, NORMAL RESPONSE WAS OBSERVED DURING OPERATION OF THE FIRE SWITCHES ON THE OVERHEAD PANEL. INVESTIGATION SHOWED THAT WIRES W629-1Q1221-20 AND 1Q1223-20 WERE SPLICED TOGETHER NEAR CONNECTOR D2316P. THE WIRING DIAGRAM SHOWED THESE WIRES AS TERMINATING IN PINS 12 AND 11 OF CONNECTOR D2316P. SIMILAR DISCREPANCIES WERE FOUND FOR EACH OF THE OTHER ENGINE SHUT OFF VALVES. THE EFFECT OF THIS MODIFICATION WAS TO BYPASS THE FUNCTION OF THE ENGINE FUEL SHUT OFF SWITCHES ASSOCIATED WITH THE ENGINE START LEVERS.

Part: STRINGER — CORRODED (BS 1660-1670)

LEVEL 1 CORROSION AFT CARGO STR FOUND AT STA 1660 TO 1670 STR 49R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: KEEL BEAM WEB — CORRODED (BS 1260)

LEVEL 1 CORROSION FX KEEL BEAM BOX PNL SUPPORT WEB RT REVEALED AT BS 1260. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SHEAR TIE — CORRODED (BS 1820)

LEVEL 1 CORROSION AFT CARGO SHEAR TIE FOUND AT STA 1820 STR 51L TO 51R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 1302)

LEVEL 1 CORROSION RT WLG W/W OVERWING LONGERON RADIUS AT BS 1302. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED 51-10-02.

Part: STRINGER — CORRODED (BS 1390)

LEVEL 1 CORROSION RT BG W/W OVERWING LONGERON WEB AT BS 1390. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 1438-1460)

LEVEL 1 CORROSION RT BG W/W OVERWING LONGERON WEB BTN BS 1438 TO 1460. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 1680-1700)

LEVEL 1 CORROSION AFT CARGO STR FOUND AT STA 1680 TO 1700 STR 50L. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 1140-1455)

LEVEL 1 CORROSION LT BG W/W OVERWING LONGERON BTN BS 1440 TO 1455. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 1416-1438)

LEVEL 1 CORROSION LT BG W/W OVERWING LONGERON BTN BS 1416 TO 1438. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED 51-10-02.

Part: STRINGER — CORRODED (BS 1680-1720)

LEVEL 1 CORROSION AFT CARGO STR FOUND AT STA 1680 TO 1720 STR 51L. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 1371)

LEVEL 1 CORROSION LT BG OVERWING LONGERON AT BS 1371. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: FRAME — CORRODED (FUSELAGE)

LEVEL 1 CORROSION FX BODY FAIRING SUPPORT BTN 191EL AND 191HL A FLOAT NUT AREA. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 1660-1670)

LEVEL 1 CORROSION AFT CARGO STR FOUND AT STA 1660 TO 1670 STR 51L. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 1760-1800)

LEVEL 1 CORROSION AFT CARGO STR FOUND AT STA 1760 TO 1800 STR 48R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: FRAME — CORRODED (FUSELAGE)

LEVEL 1 CORROSION FX PNL 192ER FAIRING SUPPORT ANCHOR NUTS AREA. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 995)

LEVEL 1 CORROSION FWD CARGO COMPT BS 995 STR 44R STRINGER. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 1300-1325)

LEVEL 1 CORROSION RT WLG W/W OVERWING LONGER RADIUS BTN BS 1300 TO 1325. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: BULKHEAD TEE — CORRODED (NR 2 PYLON)

LEVEL 1 CORROSION NR 2 PYLON TORQUE B/HEAD T-CHORDS HAVE LIGHT SURFACE AT NAC STN 301 NAC WL 296 TO 288 APPROX. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. AD: NR 94-15-18.

Part: STRINGER — CORRODED (BS 1640-1660)

LEVEL 1 CORROSION AFT CARGO STR FOUND AT STA 1640 TO 1660 STR 51L. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 1660-1680)

LEVEL 1 CORROSION AFT CARGO STR FOUND AT STA 1660 TO 1680 STR 49L. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 1394-1416)

LEVEL 1 CORROSION RT BG W/W OVERWING LONGERON WEB BTN BS 1394 TO 1416. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: KEEL BEAM WEB — CORRODED (BS 1350)

LEVEL 1 CORROSION FX KEEL BEAM PNL SUPPORT WEB REVEALED AT BS 1350. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: KEEL BEAM WEB — CORRODED (BS 1270)

LEVEL 1 CORROSION FX KEEL BEAM BOX LHS PNL SUPPORT WEB REVEALED AT BS 1270. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SKIN — CORRODED (BS 1840-1900)

LEVEL 1 CORROSION AFT CARGO SKIN FOUND AT STA 1840-190 TO STR 45R TO 46R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: STRINGER — CORRODED (BS 1462-1480)

LEVEL 1 CORROSION LT BG W/W OVERWING LONGERON BTN BS 1462 TO 1480. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SKIN — CORRODED (BS 2160-2180)

LEVEL 1 CORROSION AFT OF BULK CARGO COMPT BS 2160 TO 2180 STR 44R TO 46R SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SPAR CHORD — CORRODED (NR 2 PYLON)

LEVEL 1 CORROSION NR 2 PYLON I/B AND O/B MID SPAR CHORDS HAVE LIGHT SURFACE AT UPPER AND LOWER SURFACE AT NAC ST 296-286 NAC WL 181. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. AD: NR 94-15-18.

Part: SKIN — CORRODED (BS 2220-2240)

LEVEL 1 CORROSION AFT OF BULK CARGO COMPT BS 2220 TO 2240 STR 36L TO 37L SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SKIN — CRACKED (NR 2 PYLON)

NR 2 PYLON SKIN CRACKED UNDER SKIN DOUBLER. REPAIRED CARRIED OUT IAW SB 54-2034. NON ROUTINE CARD S/N 6270.

Part: SKIN — CORRODED (NR 2 PYLON)

LEVEL 1 CORROSION NR 2 PYLON CAP SKIN AT NAC ST 221-222 LWBL 463. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. AD: NR 94-15-18.

Part: SKIN — CORRODED (NR 1 PYLON)

LEVEL 1 CORROSION NR 1 PYLON CAP SKIN UNDER SADDLE FAIRING HAS LIGHT SURFACE AT FAIRING ATTACHMENT FASTENER HOLES AND REQUIRES PAINT TOUCH UP. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. AD: NR 94-15-18.

Part: SKIN — CORRODED (NR 2 PYLON)

LEVEL 1 CORROSION, NR 2 PYLON CAP SKIN IS CORRODED AT NAC ST 221-222 LWBL 463. REMOVED CORROSION IAW BOEING SRM 51-10-01 AND IS WITHIN LIMITS PER BOEING SRM 54-10-01 NON ROUTINE CARD S/N 6274.

Part: SKIN — CORRODED (BS 2180-2200)

LEVEL 1 CORROSION AFT OF BULK CARGO COMPT BS 2180 TO 2200 STR 42R TO 44R SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SPAR CHORD — CORRODED (NR 2 PYLON)

LEVEL 1 CORROSION, NR 2 PYLON INBD AND OUTBD MID SPAR CHORDS HAVE LIGHT SURFACE CORROSION AT NAC ST 296-286 NAC WL 181. REMOVED CORROSION IAW BOEING SRM 51-10-01 WITHIN SRM LIMITS 54-10-01 NON ROUTINE CARD S/N 6275.

Part: SKIN — CORRODED (NR 3 PYLON)

LEVEL 1 CORROSION NR 3 PYLON SKIN JUST FWD OF UPPER LINK FWD FITTING (PYLON CAP SKIN) NAC ST 221-217. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. SB/EO: NR 747-54-2159.

Part: SKIN — CORRODED (NR 3 PYLON)

LEVEL 1 CORROSION, NR 3 PYLON CAP SKIN IS CORRODED JUST FORWARD OF UPPER LINK FORWARD FITTING NAC ST 221-217 RWBL 473-467. REMOVED CORROSION IAW BOEING SRM 51-10-01 AND REPROTECTED CUT OUT SRM 51-24-11. NON ROUTINE CARD S/N 6143.

Part: BULKHEAD CHORD — CORRODED (BS 1000)

LEVEL 1 CORROSION FWD CARGO STA 1000 BULKHEAD LOWER CHORD S46L TO S47L. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SKIN — CORRODED (BS 625-635)

LEVEL 1 CORROSION FWD CARGO BS 625 TO 635 STR 40R TO 41R SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: BULKHEAD CHORD — CORRODED (BS 1000)

LEVEL 1 CORROSION FWD CARGO STA 1000 BULKHEAD LOWER CHORD S43L TO S44L. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: BULKHEAD TEE — CORRODED (NR 4 PYLON)

LEVEL 1 CORROSION, NR 4 PYLON AFT BULKHEAD 'T' CHORDS HAVE LIGHT SURFACE CORROSION. REMOVED CORROSION IAW BOEING SRM 51-10-01 AND SB 747-54-2159 R2, REPROTECTED IAW SRM 51-10-02, MM 57-26-11 NON ROUTINE CARD S/N 6004 WITHIN SRM 54-10-01 LIMITS.

Part: BULKHEAD CHORD — CORRODED (BS 1000)

LEVEL 1 CORROSION FWD CARGO STA 1000 BULKHEAD LOWER CHORD S46R TO S47R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: BULKHEAD — CORRODED (NR 1 PYLON)

LEVEL 1 CORROSION NR 1 PYLON AFT BULKHEAD I/B AND O/B CHORDS HAVE LIGHT SURFACE ON FWD FACE FROM MID SPAR TO 12 DOWN. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. SB/EO: NR 747-54-2159.

Part: BULKHEAD CHORD — CORRODED (BS 1000)

LEVEL 1 CORROSION FWD CARGO STA 1000 BULKHEAD LOWER CHORD S45L TO S46L. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: FITTING — CORRODED (NR 4 PYLON)

LEVEL 1 CORROSION, UPPER LINK FORWARD FITTING (ON PYLON) BORE CORRODED NR 4 PYLON. REMOVED CORROSION IAW SB 54-2164. NON ROUTINE CARD S/N 6002.

Part: SKIN — CORRODED (BS 592-600)

LEVEL 1 CORROSION FWD CARGO BS 592 TO 600 STR 40R TO STR 41R SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SKIN — CORRODED (BS 609-612)

LEVEL 1 CORROSION FWD CARGO BS 609 TO 612 STR 40R TO 41R SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: BULKHEAD TEE — CORRODED (NR 4 PYLON)

LEVEL 1 CORROSION NR 4 PYLON AFT BULKHEAD T-CHORDS HAVE LIGHT SURFACE AT NAC ST 267 WL 176 TO 161 APPROX. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. SB/EO: NR 747-54-2159.

Part: BULKHEAD CHORD — CORRODED (BS 1000)

LEVEL 1 CORROSION FWD CARGO STA 1000 BULKHEAD LOWER CHORD S47L TO S47R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: BULKHEAD CHORD — CORRODED (BS 1000)

LEVEL 1 CORROSION FWD CARGO STA 1000 LOWER LOBE BULKHEAD LOWER CHORD S43R TO S44R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SKIN — CORRODED (BS 658-660)

LEVEL 1 CORROSION FWD CARGO BS 658 TO 660 STR 40R TO 41R SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SPAR CHORD — CORRODED (NR 4 PYLON)

LEVEL 1 CORROSION NR 4 PYLON I/B AND O/B MID SPAR CHORDS HAVE LIGHT SURFACE AT NAC ST 267 TO 257 ON UPPER AND LOWER SURFACE WL 180. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER SRM 51-10-02. SB/EO: NR 747-54-2159.

Part: SKIN — CORRODED (BS 605-607)

LEVEL 1 CORROSION FWD CARGO BS 605 TO 607 STR 40R TO 41R SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SPAR CHORD — CORRODED (NR 1 PYLON)

LEVEL 1 CORROSION, NR 1 PYLON INBD AND OUTBD MID SPAR CHORDS HAVE LIGHT SURFACE CORROSION AT NAC ST 253.9-261 AT WL 181 ON UPPER AND LOWER SURFACE OF CHORDS. REMOVED CORROSION PER BOEING SRM 51-10-01 REWORKED AREA REPROTECTED IAW SRM 51-10-02, NON ROUTINE WORK CARD S/N 5913.

Part: SPAR CHORD — CORRODED (NR 4 PYLON)

LEVEL 1 CORROSION, NR 4 PYLON INBD AND OUTBD MID SPAR CHORDS HAVE LIGHT SURFACE CORROSION AT NAC ST 267-257 NAC WL 180. REMOVED CORROSION AND CHORDS REPROTECTED PER BOEING SRM 51-10-01, 54-10-01 AND SB 747-54-2159 R2, NON ROUTINE CARD S/N 6003.

Part: BULKHEAD TEE — CORRODED (NR 1 PYLON)

LEVEL 1 CORROSION, NR 1 PYLON AFT BULKHEAD 'T' CHORDS HAVE LIGHT SURFACE CORROSION OF FWD FACE. REMOVED CORROSION PER BOEING SRM 51-10-02, 51-10-01 AND REPROTECTED PER SRM 51-24-11, NON-ROUTINE WORK CARD S/N 5912.

Part: SKIN — CRACKED (NR 1 PYLON)

LEVEL 2 CORROSION, NR 1 PYLON INBD SIDE SKIN IS CRACKED AND CORRODED UNDER SKIN DOUBLER AT NAC ST 186-174, NAC WL 140.2. REPAIRED CARRIED OUT IAW SB 747-54-2034. NON ROUTINE CARD S/N 5999.

Part: BULKHEAD CHORD — CORRODED (BS 1000)

LEVEL 1 CORROSION FWD CARGO STA 1000 BULKHEAD LOWER CHORD S45R TO S46R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: BULKHEAD TEE — CORRODED (NR 4 PYLON)

LEVEL 1 CORROSION, NR 4 PYLON AFT BULKHEAD 'T' CHORDS HAVE LIGHT SURFACE CORROSION. REMOVED CORROSION IAW BOEING SRM 51-10-01 AND SB 747-54-2159 R2 REPROTECTED IAW BOEING SRM 51-10-02, MM 51-24-11 NON ROUTINE CARD S/N 6004 WITHIN SRM 54-10-01 LIMITS.

Part: SKIN — CRACKED (NR 4 PYLON)

LEVEL 2 CORROSION, NR 4 PYLON OUTBD SIDE SKIN IS CRACKED AND CORRODED AT NAC ST 186-174, NAC WL 142.2 - 140.2. REPAIRED CARRIED OUT PER SB 747-54-2034. NON ROUTINE CARD S/N 6000.

Part: FRAME — CRACKED (NR 4 PYLON)

NR 4 PYLON INBD AND OUTBD FRAMES AT NAC ST 162-WL 150 HAVE INCORRECT REPAIRS, AND MISSING FASTENERS. INBD FRAME IS CRACKED AT THE SAME LOCATION. REPLACED FRAME PER BOEING SRM 51-10-01.

Part: BULKHEAD CHORD — CORRODED (BS 1000)

LEVEL 1 CORROSION FWD CARGO BS 1000 BULKHEAD LOWER CHORD S44R TO S45R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SPAR CHORD — CORRODED (NR 1 PYLON)

LEVEL 1 CORROSION NR 1 PYLON MID SPAR CHORDS I/B AND O/B HAVE LIGHT SURFACE ON UPPER AND LOWER SURFACE FROM NAC ST 253.9-261. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER SRM 51-10-02. SB/EO: NR 747-54A-2159.

Part: SHEAR TIE — CORRODED (BS 520)

LEVEL 1 CORROSION FWD CARGO SHEAR TIE AT STN 520 STR 40R TO 41R FWD FACE AND AFT FACE. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.

Part: SKIN — CORRODED (BS 980-1000)

LEVEL 1 CORROSION FWD CARGO SKIN AT STN 980 TO 1000 S43R TO 44R. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER SRM 51-10-02.

Part: ANTENNA — LIGHTNING STRIKE (FUSELAGE)

IN CRUISE, BOTH VOR SYSTEMS INOPERATIVE. MAINTENANCE ON GROUND FOUND EVIDENCE OF LIGHTNING STRIKE HOLE IN VOR ANTENNA. REMOVED AND REPLACED ANTENNA PER BOEING MAINTENANCE MANUAL 34-31-03, OPERATIONAL CHECK PER 34-31-00. LIGHTNING STRIKE INSPECTION PERFORMED PER 05-51-13.

Part: DOUBLER — CRACKED (LT PYLON)

NR 2 ENGINE PYLON OLD DOUBLER REPAIR BY G/B SLOT SEAL CORNER CRACKED. REMOVED AND REPLACED DOUBLER PER BOEING 51-30-02 AND 51-10-01 EDDY CURRENT IAW NTD 54-40-13 PART 6.

Part: ACTUATOR — FAILED (RT AILERON)

RIGHT OUTBOARD AILERON INDICATES NOT MOVING WITH FLAPS DOWN, VERIFIED NO MOVING BY GROUND CREW. REMOVED AND REPLACED RIGHT OUTBOARD AILERON LOCKOUT ACTUATOR PER BOEING M/M 27-11-16, OPERATIONAL CHECK PER 27-11-16.

Part: END CAP — FAILED (BRAKE SYST)

NR 4 HYDRAULIC SYSTEM LOST 7 GALLONS. ISOLATION PROCEDURE SHOWED EDP LOSING FLUID. NR 1 HYDRAULIC SYSTEM LOST ALL FLUID WHEN SECONDARY BRAKE SOURCE SELECTED DUE TO NR 4 SYSTEM FLUID LOSS. FOUND END CAP ON BRAKE SYSTEM RETURN SURGE ACCUMULATOR BROKEN OFF. REPLACED END CAP, CHECKED PRESSURE, AND RETURN FILTERS. OPERATIONAL AND LEAK CHECKS PERFORMED PER 29-24-10, 32-41-22 AND 32-41-00. ACCUMULATOR TO BE REPLACED AT JFK.

Part: ANGLE — CRACKED (NR 2 ENGINE)

CRACK ON FORWARD SUPPORT ANGLE FOR NR 2 ENGINE INBOARD COWL HINGE. REPAIRED PER BAC SRM 54-10-03.

Part: CASE RAIL — CRACKED (NR 2 ENGINE)

CRACK ON NR 2 ENGINE TURBINE CASE S-RAIL. WELDED CRACK PER PRATT AND WHITNEY OHM 72-53-01.

Part: STRAP — BROKEN (BS 1700)

BROKEN FRAME STRAP IN LEFT AFT CARGO COMPARTMENT SIDEWALL AT APPROX BS 1700. REPAIRED PER BAC SRM 51-40-04 AND SRM 51-30-02.

Part: FLOORBEAM — DAMAGED (BS 1820)

DAMAGED UPPER CHORD ON FLOORBEAM IN AFT CARGO COMPARTMENT AT BS 1820. BLENDED DAMAGED AREA PER BAC SRM 51-10-01 AND RETREATED PER BAC SRM 51-10-02.

Part: SKIN — DELAMINATED (RT TE FOREFLAP)

DELAMINATION ON INBOARD RIGHT FOREFLAP LEADING EDGE. REPAIRED AND PAINTED PER BAC SRM 51-40-09 AND 51-24-11.

Part: PANEL — CRACKED (RT WING)

CRACK ON RIGHT WING FLYING PANEL OUTBOARD EDGE. STOP DRILLED CRACK AND APPLIED FIBERGLASS OVERLAY AND PAINTED PER BAC SRM 51-40-09 AND SRM 51-24-11.

Part: THRESHOLD — BROKEN (NR 3 PAX DOOR)

BROKEN LEFT CORNER ON NR 3 MAIN ENTRY DOOR THRESHOLD. WELDED PER BOEING PROCESS 5975 AND INSPECTED PER BAC NDTM 20-50-02, NO CRACKS FOUND.

Part: COWLING — DELAMINATION (NR 3 ENGINE)

DELAMINATION TO INSIDE EDGE OF NR 3 ENGINE FAN COWL. REBONDED DELAMINATED AREA PER BAC SRM 51-40-06.

Part: SKIN — PUNCTURED (LT WING)

SMALL PUNCTURE IN LEFT WING UPPER LEADING EDGE APPROX 4 FEET OUTBD OF FUSELAGE. APPLIED FIBERLAYS AND PAINTED PER BAC SRM 51-40-09 AND SRM 51-24-11.

Part: SKIN — CRACKED (FUSELAGE)

BULGING AND CRACKED SKIN ON LOWER CENTER FUSELAGE ADJACENT TO PNEUMATIC SERVICE DOOR. REMOVED PANEL AND REPAIRED WITH A DOUBLER, TREATED AND PAINTED PER BAC SRM 51-30-02, 51-40-02 AND 51-24-11, REINSTALLED.

Part: FOREFLAP — DELAMINATED (LT TE FLAP)

DELAMINATIONS AT TWO SPOTS ON THE LEFT INBOARD FOREFLAP LEADING EDGE. REPAIRED DELAMINATIONS WITH FIBERGLASS OVERLAYS AND PAINTED PER BAC SRM 51-40-09 AND SRM 51-24-11.

Part: PANEL — PUNCTURED (NR 3 PYLON)

PUNCTURE ON INNER SKIN OF NR 3 PYLON OUTBOARD SAILBOAT PANEL. REPAIRED PER BAC SRM 51-40-06.

Part: PITOT PROBE — MALFUNCTIONED (FUSELAGE)

RIGHT MAIN PITOT PROBE HEATER LIGHT ILLUMINATED IN CRUISE. DUE TO WEATHER EN ROUTE THE DECISION WAS MADE TO RETURN TO MELBORNE. REPLACED THE RIGHT MAIN PITOT PROBE, FUNCTIONAL AND LEAK CHECKED PER MAINTENANCE MANUAL 34-11-01.

Part: RADAR SCOPE — INOPERATIVE (NR 1)

CAPTAIN'S WEATHER RADAR INDICATOR WENT BLANK WITH SMELL OF SMOKE IN COCKPIT - PULLED CIRCUIT BREAKER. REPLACED RADAR INDICATOR PER BAC MM 34-43-05 AND TESTED PER MM 34-43-00.

Part: SKIN — MISSING (RT TE FLAP)

RIGHT OUTBOARD TRAILING EDGE FLAP LOWER SURFACE OF MID-FLAP LEADING EDGE HAS APPROXIMATELY 2.5 INCH BY 3 FOOT SECTION OF SKIN MISSING WITH EXPOSED HONEY COMB DAMAGED AND PROTRUDING, AREA SURROUNDING THE MISSING MATERIAL SOFT. REPAIRED PER BOEING SRM 51-40-07.

Part: SLEEVE — CRACKED (NR 4 ENGINE)

SMALL CRACK NR 4 ENGINE EXHAUST SLEEVE AT 9 O'CLOCK POSITION. STOP DRILLED CRACK AND FABRICATED DOUBLER AND INSTALLED AS PER BOEING SRM 51-40-02 AND REPLACED LOOSE FASTENERS PER BOEING SRM 51-30-02.

Part: BRACKET — BROKEN (LT MLG DOOR)

BROKEN AFT SUPPORT BRACKET FOR THE LEFT WING LANDING GEAR GULL DOOR. REMOVED AND REPLACED BROKEN SUPPORT BRACKET PER BOEING SRM 51-10-01.

Part: ANTENNA — CORRODED (RADIO ALT)

LEVEL 1 CORROSION ON CONNECTOR TO RADIO ALTIMETER ANTENNA. PILOT REPORT FIRST OFFICERS RADIO ALTIMITER CYCLES DURING FLIGHT. CLEANNED CORROSION AND OPERATIONAL CHECKED PER BOEING MAINTENANCE MANUAL 34-33-03.

Part: SKIN — SEPARATED (NR 1 PAX DOOR)

SKIN SEPARATION ON NR 1 MAIN ENTRY DOOR AT FORWARD UPPER CORNER. REPAIRED PER BOEING SRM 51-30-00.

Part: INTERCOSTAL — CRACKED (BS 2742)

CRACKED INTERCOSTAL BS 2742 LBL 12. FABRICATED AND REPLACED INTERCOSTAL PER BOEING SRM 51-30-02.

Part: HINGE COVER — DENTED (L1 DOOR)

DENT ON NR 1 LEFT ENTRY DOOR FORWARD CENTER HINGE COVER. MANUFACTURED AND REPLACED HINGE COVER PER BOEING SRM 51-10-06.

Part: HINGE COVER — CRACKED (L1 DOOR)

CRACKED HINGE COVER LEFT NR 1 ENTRY DOOR LOWER OUTER. REPAIRED PER BOEING SRM 51-10-01 FIG II PAGE 19 TO 21.

Part: RIB — CORRODED (NR 1 PYLON)

LEVEL 1 CORROSION NR 1 PYLON FIRE BOTTLE SUPPORT RIB. REMOVED CORROSION PER BOEING SRM 51-10-01 TREATED PER BOEING SRM 51-10-02.

Part: EXHAUST PLUG — DENTED (NR 1 ENGINE)

DENTED END CAP ON NR 1 ENGINE EXHAUST PLUG. REMOVED AND REPLACED PER BOEING MAINTENANCE MANUAL 78-32-08.

Part: SLEEVE — DENTED (ENG TR SLEEVE)

DENT NR 1 ENGINE FAN REVERSER SLEEVE AT 3 O'CLOCK POSITION. REPAIRED PER BOEING SRM 54-34-03 PAGE 85.

Part: COWL PIN/SUPPORT — DAMAGED (ENGINE)

DAMAGED ALIGNMENT PIN AND SUPPORT ON NR 2 ENGINE CORE COWL. REPAIRED PER BAC SRM 51-10-01.

Part: LOCK ARM — BENT (MAIN DECK CARGO)

BENT FORWARD LOCK ARM ON MAIN DECK SIDE RAIL AT STA 1780. REPLACED SIDE RAIL LOCK ARM PER BAC MM 25-58-00.

Part: COWL — CRACKED (NR 3 ENGINE)

CRACK AT 5TH LATCH ON NR 3 ENGINE POWER COWL. REPAIRED PER BAC SRM 51-10-01.

Part: SKIN — DAMAGED (ENG TR SLEEVE)

DAMAGED TRAILING EDGE SKIN ON NR 3 ENGINE T-FAN THRUST REVERSER SLEEVE. REPAIRED WITH HOT BONDED DOUBLER PER BAC SRM 51-40-06.

Part: HOUSING — TORN (NOSE TAXI LIGHT)

TORN LEFT CORNER OF NOSE TAXI LIGHT HOUSING. REPAIRED PER BAC SRM 51-40-09.

Part: SKIN — CRACKED (AFT FUSELAGE)

CRACK ON SMALL FAIRING AND FAIRING IS LOOSE AFT FUSELAGE ON LEFT UNDER APU EXHAUST DUCT. REPAIRED PER BAC SRM 51-10-01 AND 51-40-02.

Part: PANEL — DELAMINATED (RT WING LE)

DELAMINATED UNDERWING PANEL AT RIGHT INBOARD LEADING EDGE. REPAIRED DAMAGED AREA PER BAC SRM 51-40-09.

Part: SEQ CARRIAGE — CRACKED (LT TE FLAP)

LEFT INBOARD FLAP SEQUENCE CARRIAGE FAILED DAMAGING THE LEFT INBOARD FORE FLAP. REMOVED AND REPLACED LEFT INBOARD FORE FLAP, CARRIAGES AND TRACK OPERATIONAL CHECK GOOD PER BOEING MAINTENANCE MANUAL 27-51-02.

Part: ROLLER TRAY — DAMAGED (CARGO DECK)

DAMAGED ROLLER TRAY BS 1820 LBL 33. REPLACED ROLLER TRAY PER BOEING SRM 51-10-01.

Part: ROLLER TRAY — DAMAGED (BS 1800)

DAMAGED ROLLER TRAY BS 1800 RBL 6. REPLACED ROLLER TRAY PER BOEING SRM 51-10-01.

Part: STANTION — CRACKED (BS 460)

STANTION CRACKED AFT END OF THE E AND E COMPARTMENT BS 460 WL 135 RBL 24. REPAIRED PER BOEING SRM 51-40-03.

Part: ENGINE — OIL LEAK (NR 2)

AT CRUISE NR 2 ENGINE OIL QUANTITY STEADILY DECREASED FROM APPROX 5.6 GALLONS TO ZERO WITHIN 45 MINUTES FROM TAKEOFF. SHUT DOWN ENGINE AND RETURNED TO AMS. WINDMILL TIME 1 HOUR 16 PSI OIL PRESSURE. FOUND OIL LEAK TO BE INTERNAL REMOVED AND REPLACED ENGINE PER BOEING MAINTENANCE MANUAL 71-00-02.

Part: CSD — OVERHEATED (NR 1 ENGINE)

DURING CLIMB AT FL 310, NR 1 ENGINE HAD DUAL FIRE WARNING LIGHTS ILLUM WITH PEGGED NACELLE INDICATORS. PULLED THROTTLE BACK TO IDLE AND LIGHTS WENT OUT, INDICATIONS NORMAL AND CONTINUED FLIGHT. ON GROUND FOUND CSD OVERHEATED AND BODY CRACKED WIRING BURNT ON CSD. REPLACED CSD PER BOEING MAINTENANCE MANUAL 24-11-01.

Part: HILOCK FASTENER — HEAD SHEARED (RT WING)

HEAD SHEARED ON HILOCK RIGHT WING AFT SPAR, LOWER CHORD, JUST OUTBOARD OF WING GEAR AFT TRUNNION. REPLACED HILOCK PER BOEING SRM 51-10-01.

Part: ATTACH FITTING — BROKEN (LT MLG DOOR)

ON ARRIVAL, FOUND LEFT HAND BODY GEAR DOOR FOLLOW-UP ROD ATTACH FITTING BROKEN. REMOVED AND REPLACED FITTING IAW MM 32-14-01. INSPECTION REVEALED NO SIGN OF CORROSION. SUSPECT FATIGUE CRACK/WEAR OF BUSHINGS FOR ROD END BOLT.

Part: ACTUATOR — MALFUNCTIONED (LT AILERON)

AFTER PUSHBACK, DURING FLIGHT CONTROL CHECK, FLIGHT CREW OBSERVED THAT LEFTHAND OUTBOARD AILERON DID NOT MOVE WITH FLAPS DOWN, RETURNED TO BLOCKS. CLEANED ELECTRICAL PLUG ON AILERON LOCKOUT ACTUATOR, OPERATIONAL CHECK SATISFACTORY PER MM 27-00-00.

Part: FOREFLAP — DAMAGED (LT/RT TE FLAP)

FOUND DAMAGE TO LT O/B FOREFLAP AND RT I/B FOREFLAP DUE TO LOOSE BOLT IN MIDFLAP. INTERIM AIRWORTHY REPAIR PERFORMED IAW MA 5750-04-01, PERMANENT REPAIR PERFORMED JFK IAW SRM 51-00-04.

Part: PANEL — DELAMINATED (WS 294.62)

ON WALKAROUND FOUND RT PANEL LOWER WING MOST FORWARD BETWEEN WBL1500 WS 294.620 DELAMINATED. APPEARS TO HAVE BEEN CAUSED BY POWER UNIT PLACED UNDER WING. REPLACED PANEL IAW SRM 51-30-02.

Part: SKIN — CRACKED (CARGO DOOR)

ON PREDEPARTURE CHECK, FOUND SKIN DAMAGE AT FORWARD EDGE OF OPENING FOR REAR LOWER CARGO DOOR. DOOR FRAME TEAR STRIP AND OUTER SKIN DISTORTED AND CRACKED. REPAIRED PER DOCUMENT R747-5310-28-1/1.

Part: TIRE — BLOWN (NR 10)

BLEW NR 10 TIRE ON TAKEOFF FROM HONG KONG. RETURNED TO HONG KONG, MADE UNEVENTFUL LANDING. REMOVED AND REPLACED TIRE IAW MM 32-45-01.

Part: DUCT — CRACKED (NR 2 PYLON)

AFTER ENGINE START, WING LEADING EDGE OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO BLOCKS. FOUND LEADING EDGE PNEUMATIC DUCT INBOARD OF NR 2 ENGINE CRACKED. REPLACED DUCT ASSEMBLY, INSPECTED AND LEAK CHECKED IAW MM 36-10-00.

Part: CONTROL RODS — DISCONNECT (ELEVATOR)

DURING GROUND CHECK, FOUND BOTH OUTBOARD ELEVATOR RODS DISCONNECTED. RECONNECTED AND PERFORMED OPERATIONAL CHECK IAW MM 27-31-02. INVESTIGATING TO DETERMINE WHY DISCONNECTED.

Part: BEARING — CORRODED (LT SPOILER)

FOUND LEVEL 1 CORROSION ON LEFT WING SPOILER POSITION TRANSMITTER FINE ADJUSTMENT ROD BEARING. END ASSEMBLY REPLACED, FUNCTION CHECK SATISFACTORY IAW SRM 27-68-00.

Part: SKIN — CORRODED (LT WING)

FOUND LEVEL 1 CORROSION ON LEFT WING UPPER SURFACE AT WBL 579, WBL 565, WLB 370, CENTER SPAR AREA. CORROSION REMOVED, FOUND WITHIN SRM 57-30-01.

Part: PANEL — DELAMINATED (LT WING)

ON LEFT WING OUTBOARD MIDFLAP LEADING EDGE, FOUND TWO DELAMINATED AREAS BETWEEN NR 1 AND NR 2 FLAP TRACKS. FIBERGLASS REPAIR CARRIED OUT IAW SRM 51-40-09.

Part: BRACKET — CRACKED (RT WING)

FOUND RT WING ANGLE BRACKET CRACKED AT ILGS 949.5. REMOVED AND REPLACED IAW MM 57-31-17.

Part: PANEL — DELAMINATED (RT WING)

FOUND TWO DELAMINATED AREAS NEAR AFT EDGE OF FIXED T/E PANEL FORWARD OF INBOARD AILERON, RIGHT WING. FIBERGLASS REPAIR CARRIED OUT IAW MM 51-40-09.

Part: STIFFENER — CRACKED (LT WING)

FOUND LEFT WING STIFFENER CRACKED AFT OF NR 11 L/E FLAP. STIFFENER REPAIRED AND REINSTALLED IAW SRM 51-40-03.

Part: BRACKET — CRACKED (NR 4 PYLON)

NR 4 PYLON AFT FAIRING DOOR FOURTH BRACKET ANGLES CRACKED. ANGLES REPLACED AND BRACKET ASSY REINSTALLED IAW MM 54-32-01.

Part: BRACKET — DAMAGED (RT WING)

FOUND SUPPORT BRACKET FOR LEADING EDGE MIDSECTION DUCT DAMAGED. NEW BRACKET INSTALLED IAW SRM 36-11-12.

Part: SUPPORT — CRACKED (RT WING)

FOUND SUPPORT TUBE ASSY AT ILES 949.5 FOR WING L/E LOWER SURFACE PANEL CRACKED. REPLACED IAW MM 57-31-17.

Part: SKIN — DELAMINATED (LT WING)

FOUND DELAMINATED AREA ON INBOARD FOREFLAP LOWER SKIN BETWEEN NR 4 AND NR 5 FLAP TRACKS ON LEFT WING. FIBERGLASS REPAIR CARRIED OUT IAW SRM 51-51-00.

Part: S FLANGE — CRACKED (3 ENGINE)

FOUND NR 3 ENGINE S-FLANGE CRACKED AT 1:30 O'CLOCK POSITION. WELDING CARRIED OUT IAW AMS 58-17.

Part: BRACKET — BROKEN (NR 2 ENGINE)

FOUND NR 2 ENGINE UPPER RIGHT FIRE DETECTOR MOUNTING BRACKET BROKEN OFF. REPAIRED AND REINSTALLED IAW MM 26-11-02.

Part: BRACKET — CRACKED (BS 1000)

FOUND BS 1000 SUPPORT BRACKET FOR POTABLE WATER TANK LOWER SUPPORT BRACE CRACKED. NEW SUPPORT BRACKET INSTALLED IAW SRM 53-11-22.

Part: SKIN — CORRODED (FUSELAGE)

FOUND LOWER SKIN CORRODED NEAR VHF ANTENNA NR 2 MOUNTING POINT. LEVEL ONE CORROSION REMOVED, WITHIN SRM 53-30-01 LIMITS.

Part: SKIN — DELAMINATED (LT AILERON)

FOUND LEFT WING INBOARD AILERON UPPER SKIN DELAMINATED. FIBERGLASS REPAIRED IAW SRM 51-40-09.

Part: BRACES — BROKEN (WATER TANK)

POTABLE WATER TANK LOWER SUPPORT BRACES LEFT AND RIGHT BROKEN. NEW SUPPORT BRACES INSTALLED PER IPC 38-11-02.

Part: BRACKET — CRACKED (NR 3 ENGINE)

FOUND CRACKED BRACKET AT FLANGE 'P' AT APPROX 1 O'CLOCK OF NR 3 ENGINE. CRACKED BRACKET REPLACED IAW MM 72-50-00.

Part: PNEU DUCT — CRACKED (NR 3 ENGINE)

FOUND NR 3 ENGINE PNEUMATIC DUCT CRACKED. REPAIRED PER MM 36-10-02.

Part: PANEL — DELAMINATED (RT WING)

FOUND RIGHT WING FIXED T/E PANEL ASSY BL 128.47 TO 263.94 DELAMINATED. REPAIRED IAW SRM 57-30-04.

Part: RIB — BROKEN (NR 4 ENGINE)

RIGHT LOWER SLOT SEAL FAIRING SUPPORT RIB ON NR 4 ENGINE FOUND BROKEN OFF. REPLACED IAW SRM 54-30-01.

Part: BRACKET — CRACKED (NR 3 ENGINE)

NR 3 ENGINE TT2 SENSOR SUPPORT BRACKET AND MOUNTING PLATE FOUND CRACKED. REPAIRED AND REINSTALLED IAW MM 73-21-04.

Part: SKIN — DELAMINATED (RT WING)

FOUND SKIN DELAMINATION ON INBOARD T/E AFT FLAP LOWER SURFACE BETWEEN FLAP CANOE NR 5 AND NR 6. FIBERGLASS REPAIR CARRIED OUT IAW SRM 51-50-09.

Part: R-FLANGE — CRACKED (NR 4 ENGINE)

FOUND NR 4 ENGINE RIGHT HAND R-FLANGE CRACKED AT 3:30 POSITION. WELDED IAW AMS 58-17 IAW P/W 72-53-01.

Part: TUBE ASSY — CRACKED (RIGHT WING)

FOUND CRACK IN RIGHT WING SUPPORT TUBE ASSY FOR WING LEADING EDGE LOWER SURFACE. REMOVED AND REPLACED TUBE ASSY IAW IPC 57-31-17.

Part: SKIN — CRACKED (RT TE FOREFLAP)

FOUND CRACK AT RIGHT WING OUTBOARD T/E FOREFLAP BETWEEN FLAP TRACKS NR 7 AND NR 8. FIBERGLASS REPAIRED IAW SRM 51-40-09.

Part: TIE DUCT — BROKEN (NR 4 ENGINE)

FOUND NR 4 ENGINE RIGHT HAND PNEUMATIC DUCT TIE LINK BROKEN. REMOVED AND REPLACED TIE LINK IAW 36-11-01.

Part: STRUCTURE — CRACKED (BS 736)

FOUND PDU SUPPORT STRUCTURE AT BS 736 CRACKED. REPAIRED IAW SRM 53-10-07.

Part: BRACKET — CRACKED (NR 3 PYLON)

NR 3 PYLON LT AFT FAIRING DOOR, AFT MOST BRACKET ANGLES FOUND CRACKED. ANGLE REPLACED IAW MM 54-32-01.

Part: EGT HARNESS — BROKEN (APU)

FOUND APU EGT HARNESS BROKEN AT 8 O'CLOCK AND 9 O'CLOCK POSITIONS. LEFT AND RIGHT EGT HARNESS ASSY'S REPLACED IAW MM 49-61-04.

Part: SKIN — DELAMINATED (RT TE FLAP)

FOUND RIGHT WING OUTBOARD T/E AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AS PER SRM 51-40-09.

Part: PANEL — DELAMINATED (LT WING)

LEFT WING FIXED TRAILING EDGE FOUND DELAMINATED OUTBOARD OF OUTBOARD FLAPS. FIBERGLASS REPAIR CARRIED OUT IAW SRM 51-40-09.

Part: BRACKET — CRACKED (NR 2 PYLON)

NR 2 PYLON TT2 SENSOR BRACKET FOUND CRACKED. BRACKET REPLACED PER MM 73-22-02.

Part: FAIRING — CRACKED (NR 3 ENGINE)

FOUND NR 3 ENGINE FORWARD FAIRING CRACKED AT FRAME. REPAIRED IAW MM 51-40-03 AND REINSTALLED PER MM 71-40-08.

Part: PRECOOLER MOUNT — CRACKED (NR 3 ENGINE)

NR 3 ENGINE PRE-COOLER FORWARD LOWER MOUNT FOUND CRACKED. REPAIRED AND REINSTALLED IAW MM 36-12-01.

Part: DUCT LINK — BROKEN (NR 1 ENGINE)

NR 1 ENGINE PNEUMATIC DUCT LINK AT PYLON HORIZONTAL FIREWALL FOUND BROKEN ON LEFT SIDE. LINK ASSY REPLACED AND SECURED IAW MM 36-11-01.

Part: VANE — CRACKED (NR 2 ENGINE)

FOUND NR 2 ENGINE CASCADE VANE CRACKED AT 8 O'CLOCK POSITION BELOW JACKSCREW. REPAIRED IAW OHM 78-31-51.

Part: BRACKET — CRACKED (BS 1480)

FOUND 4 BRACKETS ATTACHED TO BS 1480 BULKHEAD CRACKED AND BENT. REPAIRED AND REPLACED AS REQUIRED IAW SRM 53-10-22.

Part: VANE — CRACKED (NR 3 ENGINE)

NR 3 ENGINE CASCADE VANE ASSY 2ND FROM TOP, LT SIDE FOUND CRACKED. REPAIRED AND REINSTALLED AS PER MM 78-31-07.

Part: S FLANGE — CRACKED (NR 2 ENGINE)

NR 2 ENGINE S-FLANGE FOUND CRACKED AT 5:30 O'CLOCK POSITION. REPAIRED IAW MM 72-53-02.

Part: TIRE — FAILED (MLG)

DURING LANDING ROLLOUT, TIRES 10 AND 12 FAILED, DUE TO SUSPECTED LOCKED WHEEL CONDITION. CAUSED MATERIAL LOSS WHICH PENETRATED THE INBOARD RIGHT MIDFLAP, CAUSING A HOLE APPROXIMATELY 2.5 INCHES BY 2.5 INCHES. REPLACED FAILED AND ADJACENT TIRES AND WHEEL ASSEMBLIES. LOCKED OUT NUMBERS 10 AND 12 BRAKES PER MEL 32-05. REPAIR MIDFLAP PER SRM 51-40-09.

Part: LINE — CRACKED (LT WING FAIRING)

DURING CRUISE, FLIGHT DECK HAD HYDRAULIC FUMES. AIRCRAFT RETURNED TO NADI. FOUND 2 HYD LINES CRACKED IN LT WING FAIRING AREA. LINES REPAIRED AND OTHER INSP CARRIED OUT AS REQUIRED. FULL REPORT WILL BE IN MAIL.

Part: HYD LINE — CRACKED (NR 2 PACK)

SMOKE/VAPOR IN COCKPIT, SMELLS OF BURNT SKYDROL, DISSIPATED AFTER 10 TO 12 MINUTES. CREW DONNED OXYGEN MASKS AND RETURNED LANDING OVERWEIGHT WITH LOW SINK RATE. FOUND HYDRAULIC LEAK AND CRACKED HYDRAULIC RETURN LINE NR 2 PACK AREA. SUSPECT INGESTION INTO AIR CONDITIONING SYSTEM. REPAIRED WITH TEMPORARY LINE IAW MM 20-11-05, OVERWEIGHT INSPECTION COMPLIED WITH.

Part: HINGE — BROKEN (RT MLG DOOR)

DURING WALK-AROUND, FOUND RIGHT HAND FORWARD MAIN GEAR DOOR FORWARD UPPER HINGE BROKEN. REPLACED UPPER HINGE HALF IAW MM 32-12-00.

Part: DOOR — DELAMINATED (NR 1 PACK)

NR 1 PACK HEAT EXCANGER ACCESS DOOR HAS AN AREA OF DELAMINATION. REMOVED AND HOT BOND REPAIRED PANEL PER BOEING SRM 51-40-12, REINSTALLED PANEL.

Part: SWITCH — DIRTY (NLG)

TOP OF CLIMB, RED GEAR WARNING LIGHT ON FORWARD PANEL ON WITH GEAR HANDLE UP AND NORMAL HYDRAULICS. FEO'S ANNUNCIATOR LIGHT SHOWS NOSE GEAR DOWN AND LOCKED IN PRIMARY AND ALTERNATE. CLEANED SWITCHES, PERFORMED OPERATIONAL CHECK OF NOSE GEAR, SYSTEM CHECKED NORMAL. DEFFERED PRIMARY SWITCH PER MEL.

Part: TE SKIN — DELAMINATED (RT TE MID FLAP)

DURING POST FLIGHT INSPECTION, FOUND RIGHT OUTBOARD TRAILING EDGE MIDFLAP DAMAGED AND DELAMINATED. REPAIRED IN ACCORDANCE WITH BOEING SRM.

Part: COMP BLADES — FAILED (ENG)

THREE HOURS INTO FLIGHT CLIMBING FROM FL 330 TO FL 370, EXPERIENCED SHUDDER, MUFFLED BOOM, EGT RISE TO 920 DEGREES, EGT WARNING LIGHT, ERP AND N1 LOSS FOLLOWED BY EGT DROP AND ENGINE FAILURE. SHUT DOWN ENGINE, VISUAL INSPECTION NO APPARENT PHYSICAL DAMAGE. FLIGHT CONDITIONS, SMOOTH, VMC. PERFORMED INSPECTION OF ENGINE PER MM 71-00-2 AND 71-00-46. WHICH REVEALED DAMAGE TO 8TH STAGE. ENGINE TO BE REPLACED.

Part: TEMP BULB — FAILED (NR 1 CSD)

FLT 281 - JFK - AIR TURN BACK, AFTER TAKEOFF NR 1 CSD TEMPERATURE HIGH RISE OUT ALSO HIGH. NR 4 CSD ALREADY PLACARDED. REPLACED NR 1 CSD OUT TEMPERATURE BULB OPERATIONAL CHECK OK. RECONNECTED NR 4 CSD, CLEANED AND SECURED MAIN DISCONNECT CANNON PLUG. OPERATIONAL CHECK OK. (M)

Part: PS4 LINE — LEAKING (NR 1 ENGINE)

VCP/JFK - EN ROUTE AT FL 350 IN CRUISE, NR 1 ENGINE LOST POWER, N1, N2, EPR, AND FUEL FLOW DECREASED AND EGT INCREASED. RE-START ATTEMPTED, BUT WAS UNSUCCESSFUL. DESCENDED TO FL 310 AND WAS ABLE TO RE-START ENGINE USING GROUND START PROCEDURE. REST OF FLIGHT UNEVENTFUL. POST-FLIGHT BORESCOPE INSPECTION FOUND NO DISCREPANCIES. ADDITIONAL INSPECTION FOUND A LEAK AT A B-NUT ON THE PS4 LINE. TIGHTENED B-NUT. ENGINE RUN-UP PERFORMED IAW MM. ALL PARAMETERS NORMAL.