N673UP

Part: WARNING LIGHT — ILLUMINATED (NR 4 ENGINE) · airframe 71,087 hrs · 20,719 cycles

NR 4 ENGINE FIRE, AFTER SETTING CLIMB THRUST, NR 4 ENGINE FIRE LIGHT LIT AND BELL SOUNDED. CONFIRMED BOTH NR 4 NACELLE TEMP. INDICATORS PEGGED OUT HIGH. ACCOMPLISHED ENGINE FIRE SEVERE DAMAGE CHECKLIST WITH FIRE INDICATION OUT AFTER ONE BOTTLE. APPROXIMATELY 5 MIN. LATER FIRE LIGHT AND BELL SOUNDED AGAIN; DISCHARGED SECOND BOTTLE AND RETURNED TO OBBI.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE: PFLT, MAIN ENTRY DOOR JAMB EMERGENCY EXIT LIGHT INOPERATIVE. CHECKS NORMAL, UNABLE TO DUPLICATE.

Part: LIGHT — INOPERATIVE (MAIN DECK)

INSPECTION TYPE: PFLT, INOPERATIVE MAIN DECK EMERGENCY LIGHT AFT RIGHT OF CREW LADDER. OPERATIONAL CHECK NORMAL, COULD NOT DUPLICATE.

Part: LIGHT — INOPERATIVE (MAIN DECK)

INSPECTION TYPE: PFLT, INOPERATIVE MAIN DECK EMERGENCY LIGHT AFT LEFT OF CREW LADDER. OPS CHECK NORMAL. COULD NOT DUPLICATE.

Part: SKIN — GOUGED (FUSELAGE)

INSPECTION TYPE: PFLT, (FUSELAGE SKIN REPAIR REF "D" 246890) FUSELAGE SKIN REPAIR DOUBLER AT TAIL STAND DENTED & GOUGED. DRILLED OFF DAMAGED REPAIR DOUBLER. REMOVED TAILSTAND ATTACH FITTING FROM STRINGER 46 RT STA 2598. FABRICATED NEW DOUBLER & DRILLED. BEGAN FASTNER INSTALLATION IN REPAIR DOUBLER. COMPLETED INSTALLATION OF REMOVED PARTS & DOUBLER PER 747 SRM 51-30-02.

Part: FIRE WARNING — FALSE INDICATION (COCKPIT)

INSPECTION TYPE:N/A AFTER APPROX 1 HOUR IN CRUISE FLIGHT. A RED WARNING LIGHT ON THE OVERHEAD ILLUMINATED FOR A SPLIT SECOND. RESEATED ALL THE FIRE DET CARDS. TESTED SYSTEMS IAW MM 26-10-00, ALL TEST CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT OVERHEAD EMERGENCY LIGHT ADJACENT TO SMOKE EVACUATION HOLE WILL NOT STAY ILLUMINATED WHEN POWER IS LOST AND EMERGENCY LIGHTS ARMED. REMOVED AND REPLACED BATTERY PACK ASSY IAW M/M 33-51-00. OPS CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT AFT OF DOOR L-5 IS INOP (CEILING LOCATION). REMOVED AND REPLACED BATTERY PACK ASSY IAW MM 33-51-00, OPS CHECK OK.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT CEILING EMERGENCY LIGHT ABOVE UPPER DECK EMERGENCY EXIT DOOR INOP. RECHARGED BATTERY, OPS CHECK GOOD.

Part: SKIN — CRACKED (L3 DOOR) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - DURING FINAL DOOR CLOSE UP L3 DOOR EXTERNAL SKIN CRACKED AT BS 1295 & 1305 WL 210 AREA 2 LOCATIONS AS MARKED. DOOR SKIN REPAIRED AS PER SRM 52-10-02 FIG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 500 RBL 97 SEAT TRACK FLANGE FOUND CORROSION DAMAGED. SEAT TRACK REPLACED AS PER SRM 51-10-01.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C DURING LT SIDE STA 1241 EXTERNAL LONGERON REMOVE, NR 13 BOLT (FROM FWD) FOUND BROKEN AND BOLT HOLE FOUND CORROSION. BOLT HOLE CORROSION REMOVED, LONGERON SPLICE STRAP, B/H GORGING AND SKIN REAMED TO 0.875 INCH, HFEC INSPECTION PERFORMED AS PER NTM PT 6 51-00-00 FIG 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C BULK CARGO COMPT - BS 1980 RBL 45 - 50 LONG FLOOR SUPPORT FOUND CORROSION DAMAGE. FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C CRACK FOUND AT BS 980 S-38R INTERNAL BATHTUB FITTING VERTICAL FLANGE 1 EA BOLT CRACK LENGTH .125 INCH APPROX RUNNING DOWNWARD. BS 980 RH S-38R BATHTUB FITTING REPLACED AS PER SRM 51-10-01 PG 8.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - AFTER R1 DOOR INTERIOR HANDLE MECHANISM HOUSING REMOVED, THE DOOR CTR FRAME ACCESS HOLE CUTOUT FOUND CRACKED NEAR WINDOW AREA. FRAME WEB REPAIRED PER SRM 51-40-02 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - LBL 57 BS 2240 FLOORBEAM AFT SIDE WEB CORRODED (NEAR UPPER CHORD). FLOORBEAM WEB REPLACED AS PER SRM 51-10-01, REFER NRC 7698.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - LBL 11 BS 2240 FLOORBEAM WEB CORRODED (NEAR LWR CHORD). FLOORBEAM WEB REPLACED AS PER SRM 51-10-01 PG 8.

Part: FITTING — CRACKED (WING) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C LT BS 1241 WING REAR SPAR UPPER SPLICE FITTING NR 3 HOLE FOUND CRACKED, PLS REFER ATTACH SKETCH. LT BS 1241 WING REAR SPAR UPPER SPLICE FITTING REPLACED AS PER UPS EO B747-5740-4366-E APPENDIX F, H AND I.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - SEAT TRACK FOUND CORROSION AT BS 2225 RBL 75 AFTER FLOOR PANEL REMOVED. SEAT TRACK REPLACED AS PER SRM 51-10-01.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C NLG W/W LT VERTICAL BEAM WEB MIDDLE AREA 1EA HORIZ SUPPORT ANGLE CRACKED AT STA 390 AREA (ACCESS FROM LT SIDE TUNNEL JUST AFT OF NLG CABLE AREA). SUPPORT ANGLE REPLACED AS PER SRM 51-10-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 218 RBL 45 SEAT TRACK FLANGE CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - LBL 75 - 90 BS 2240 - 2280 FLOOR SUPPORT CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - FLOOR SUPPORT FOUND CORROSION AT BS 2240 RBL 75-85 AFTER FLOOR PANEL REMOVED. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - LBL 75 BS 2240-2280 FLOOR SUPPORT CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 2240 RBL 75 - RBL 33 FLOORBEAM WEB FOUND CORRODED. FLOORBEAM REPLACED AS PER SRM 51-10-01 PG 8.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C LT WLG W/W STA 1241 B/H FOUND CORROSION AT WL 143 LBL 0-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 2196 RBL 11 SEAT TRACK CROWN FOUND CORRODED. BS 2190 - 2250 RBL 11 SEAT TRACK REPLACED PER SRM 51-10-01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C AFT OF BULK CARGO - S49R BS 2218 STRINGER CORRODED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C RT WLG W/W OVERWING LOWER LONGERON FOUND EXFOLIATION CORROSION AT STA 1246-1249 RBL 125-127. CORROSION REMOVED AND SHOT-PEEN C/O AS PER SRM 51-10-01 & SOPM 20-10-03.

Part: HINGE — DAMAGED (R1 DOOR) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - R1 DOOR HINGE UPPER DOUBLER FOUND NONSTANDARD REPAIR. DOOR UPPER HINGE CUTOUT REPAIRED AS PER SB 52-2144.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C, AFT BULK CARGO S-51R BS 2218 STRINGER CRACKED. STRINGER REPAIR SRM 53-10-03 FIG 1.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C FX - KEEL BEAM ACCESS PANEL ANCHOR NUT SUPPORT FOUND CORROSION AT STA 1400 FROM LBL 8 TO RBL 8. FX BS 1400 BEAM REPLACED PER SRM 51-10-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C AFT BULK CARGO, S-50R BS 2210 STRINGER CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C AFT CARGO COMPT - BS 1560 S51R STRINGER CORRODED.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C AFT CARGO COMPT - RBL 46 BS 1860 - 1900 TIE DOWN TRACK CORRODED. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 5.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C, LT SIDE NOSE W/W ON BS 380 VERT BEAM WEB FOUND 2 EA INSULATION STANDOFF HOLES CRACKED, 1 EA JUST BETWEEN 1 & 2 STIFFENER AND 1 EA JUST BETWEEN NR 5 STIFFENER AND 1 EA JUST BETWEEN NR 5 STIFFENER. VERT BEAM WEB REPLACED AS SRM 51-10-01.

Part: CLIP — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C RT SIDE NOSE W/W ON BS 320 VERTICAL BEAM CLIP FOUND CRACK AT NR 5 CLIP (COUNT FROM TOP) AS MARKED. CLIP REPLACED AS PER SRM 51-10-01.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C LT SIDE NOSE W/W ON BS 320 VERTICAL BEAM WEB FOUND 1 EA INSULATION BLANKET STAND-OFF HOLE CRACKED, JUST BETWEEN NR 4 & 5. VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C LEFT WLG W/W PRESSURE DECK WEB FOUND CORROSION CRACK AT STA 1319-1323 LBL 128-130. PATCH REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C AFT CARGO COMPT - RBL 31-42 BS 1660 FLOORBEAM UPPER CHORD CORRODED. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-41-04 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C CRACK REVEALED ON LEFT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING AT HOLE NR 5 BY APPROX 0.030 IN LONG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C CRACK AND CORROSION REVEALED ON RIGHT BS 1480 BULKHEAD EXTENSION FITTING AT HOLE NR 9.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C AFT CARGO COMPT - RBL 25 BS 1870 TIE DOWN TRACK CORRODED DAMAGED. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 5.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C CRACK REVEALED ON LT BS 1480 BULKHEAD HOLE NR 3 AT EXTENSION FITTING, SKIN, BULKHEAD CHORD AND OUTER CHORD SPLICE FITTING. LT BS 1480 BULKHEAD HOLE NR 3 EXTENSION FITTINGG REAMED TO 0.650 INCH, SKIN REAMED TO 0.687 INCH, BULKHEAD CHORD REAMED TO 0.625 INCH & OUTER CHORD SPLICE FITTING REAMED TO 0.687 INCH AS PER EO B747-5310-10732 & NDT CONFIRMED NR 3 HOLE NO CRACK REVEAL. REPAIR BUSHING INSTALLED ON NR 3 HOLE AS PER SB 747-53A2390 R1 FIG 11.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C RIGHT BLG W/W PRESSURE DECK O/B LWR SURFACE BETWEEN BS 1367 & 1372 AREA CORRODED AS MARKED. PRESSURE DECK BOND SKIN REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C RT SIDE NOSE W/W ON BS 320 VERTICAL BEAM WEB FOUND 1 EA INSULATION BLANKET STAND OFF HOLE CRACKED AT JUST BETWEEN NR 1 AND 2 STIFFENER. VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C RT SIDE W/W ON BS 300 VERTICAL BEAM WEB FOUND 1 EA INSULATION BLANKET STAND-OFF HOLE CRACKED AND JUST BETWEEN NR 1 & 2 STIFFENER. VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 360 S-22R FRAME FOUND CRACKED. M/D BS 360 FRAME REPAIRED AS PER SRM 53-10-04 FIG 85.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C FWD CARGO COMPT, S-43L TO S-44L BS 760 FLOORBEAM SHEAR TIE CORROSION CRACKED. SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 1820 RBL 97 SEAT TRACK CROWN FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 1740 RBL 97 SEAT TRACK CROWN FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 2350 S-51R STRINGER FOUND CRACKED. M/D BS 2350 S-51R CRACKED STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 1780 RBL 95 SEAT TRACK CROWN FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 260 LBL 10 & 22 NOSE WHEEL UPPER SURFACE STIFFENER ATTACH ANGLE CRACK. ATTACH ANGLES (2 EA) REPLACED AS PER SRM 51-10-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D BS 1900 RBL 97 SEAT TRACK CROWN CORROSION FOUND. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 1860 RBL 97 SEAT TRACK CROWN FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 380 S-22L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 85.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 2350 S-51R STRINGER FOUND CRACKED. M/D BS 2350 S-51R CRACKED STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - L1 DOOR LOWER HINGE CUTOUT DOUBLER FOUND CRACKED. DOOR HINGE CUTOUT REPAIRED AS PER SB 747-52-2144.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 360 S-18R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 85.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 260 LBL 8 AND NOSE WHEEL UPPER SURFACE STIFFENER ATTACH ANGLE CRACK. ATTACH ANGLES (2 EA) REPLACED AS PER SRM 51-10-01.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C FWD CARGO COMPT - E/E COMPT BS 400 S-31R BULKHEAD WEB FOUND CRACKED. BULKHEAD WEB REPAIRED AS PER BOEING DWG 65B00272.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C U/D - BS 340 LBL 10 - 20 FLOORBEAM SURFACE FOUND CORROSION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 300 S-13AR FRAME FOUND CRACKED. M/D BS 300 FRAME REPAIRED AS PER RS 53-12-34717.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 260 - 280 LBL 33 SEAT TRACK FLANGE CORRODED. SEAT TRACK REPAIRED AS PER SRM 51-10-05 FIG 1A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 220 RBL 57 FLOORBEAM SURFACE CORRODED. FLOORBEAM UPPER CAP REPAIRED AS PER SRM 53-10-07 FIG 10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 380 S-24AL FRAME FOUND CRACKED. FRAME REPAIRED AS PER RS R53-12-34720.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 490 RBL 75 SEAT TRACK FLANGE CORRODED. SEAT TRACK REPLACED AS PER SRM 51-10-01.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 360 RBL 92 FLOORBEAM WEB CRACKED. BS 360 MOST RT O/B WEB REPAIRED AS PER SRM 53-10-07 FIG 11.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 215 - 217 RBL 48 SEAT TRACK FLANGE CRACKED. SEAT TRACK REPAIRED SRM 53-10-05 FIG 1A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 380 S-24AR FRAME FOUND CRACKED. FRAME REPAIRED AS PER RS R53-12-34721.

Part: PANEL — CRACKED (CABIN) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - R3 DOOR CUTOUT FWD LOWER CORNER REVEAL FOUND CRACKED. CORNER REVEAL REPLACED PER SRM 51-10-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 360 S-23L FRAME FOUND CRACKED. SIDEWALL FRAME REPLACED AT BS 360 S-23L PER RS R53-12-3475.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C AFT CARGO COMPT - BS 1700 - 1725 S-49L STRINGER FOUND CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 423 LBL 10 SEAT TRACK FLANGE CORRODED. SEAT TRACK REPLACED PER SRM 51-10-01 PG 8.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C FX - STA 840 LBL 16-20 EXT SKIN FOUND BULGED. STA 840 LBL 16-20 EXT SKIN CORROSION REMOVED AS PER SRM 51-10-01 AND 51-10-02.

Part: DOOR FRAME — CRACKED (R4 DOOR) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D R4 DOOR AFT FRAME LOWER CORNER FOUND CRACKED. DOOR AFT FRAME LOWER CORNER REPAIRED AS PER SRM 52-10-02.

Part: STIFFENER — CRACKED (LT WING) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C L/W - L/E CAVITY FRONT SPAR 1 EA VERTICAL STIFFENER FOUND CRACKED AT LOWER END ABOUT 2 INCHES AT WS 382 JUST BEHIND NR 13 K/FLAP. STIFFENER IS REPAIRED AS PER HAECO RS R-57-21-34726.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 1265 CANTED BULKHEAD BL 0 SPLICE FOUND CRACKED. SPLICE REPLACED AS PER SRM 51-10-01.

Part: SKIN — CRACKED (R1 DOOR) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - R1 DOOR LOWER HINGE CUTOUT FOUND CRACKED. DOOR HINGE CUTOUT SKIN REPAIRED SRM 52-10-02 FIG 12.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C CRACK INDICATION REVEALED ON SKIN UNDERNEATH LT LOWER DRAG SPLICE FITTING AT BS 980 STR S-38L. CRACKED F/X SKIN IN BS 980 S-38L REPAIRED AS PER SRM 53-30-03 FIG 60.

Part: PANEL — BULGED (LT WING) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C L/W - LOWER L/E PNL FOUND BULGED UP AT WS 1270 AFT OF NR 5 V/C FLAP.

Part: SKIN — CRACKED (L1 DOOR) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - L1 DOOR UPPER HINGE CUTOUT FOUND CRACKED AS MARKED. HINGE CUTOUT SKIN REPAIRED AS PER SB 747-52-2144.

Part: PANEL — CRACKED (CABIN) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - R2 DOOR CUTOUT FWD LOWER REVEAL FOUND CRACKED. LOWER REVEAL REPAIRED AS PER SRM 53-10-04 FIG 84.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C AFT CARGO - CARGO DOOR FWD UPPER CORNER FOUND CRACKED AS MARKED.

Part: SKIN — BULGED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C FX - SKIN SLIGHTLY BULGED UP AT BS 2200 S-32L & S-32R. APPROX SKIN REPAIRED PER SRM 53-30-03 FIG 1.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,011 hrs · 20,052 cycles

INSPECTION TYPE:C M/D - BS 1240 RBL 99 BELOW FLOOR WING CTR TANK SURFACE FOUND CORROSION. CORROSION REMOVED PER SRM 57-30-01 FIG 1 & SHOT-PEENING CARRIED OUT AS PER BAC5884.

Part: HANDLE — BROKEN (L1 DOOR)

INSPECTION TYPE:N/A L1 DOOR INNER HANDLE BROKEN. REMOVED AND REPLACED HANDLE IAW 52-11-13. HANDLE OPS CHECKS OK.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A STAIRWAY OVERHEAD LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT IAW B747 MM 33-51-00, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A STA 350 RT CEILING LIGHT MISSING LENS AND INOP EMERGENCY EXIT LIGHT. REPLACED EMERGENCY LIGHT ASSY AT CEILING STA 350 RT CHKS GOOD.

Part: DOOR — LACK OF LUBE (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT DOOR FOR ESCAPE SLIDE AT COCKPIT BINDS WHEN OPENING OR CLOSING. ADJUSTED LATCH AND LUBED TRACK SLIDE OPERATES NORMAL NO BINDING.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A MAIN DECK ENTRY EMERGENCY LIGHTS ON LT SIDE HAS ONE INOP LAMP. R&R BOTH BULBS, OPS CHKS GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (FWD CARGO HOLD)

BTB-FWD CARGO COMPARTMENT SMOKE DET WARNING LIGHT ILLUMINATED. AWAITING LOG PAGE DEFERRED PER MEL

Part: CIRCUIT BOARD — DIRTY (FIRE DETECTION)

INSPECTION TYPE:PFLT CREW PREFLT NR 2 ENG FIRE BELL WILL NOT CUT OUT. CLEANED AND RE-RACK CARD A-6, OP CK NORMAL.

Part: FRAME — CORRODED (WINDOW)

INSPECTION TYPE:C, CORROSION WAS FOUND AT WINDOW FRAME CUTOUTS RT SIDE BETWEEN STA 560 - 580, 640 - 660 AND BETWEEN STA 860 - 1000. SEE NDT INSP REPORT NO U-209 8. WINDOW FRAME CUTOUTS AREA CORROSION REPAIRS ACCOMPLISHED IAW EO MF-M AN-B747-53-24-89306 AS INSTRUCTED BY BOEING MESSAGE NO IAI-TLV-00-00 33TH. REFERENCE NRCS 239317, 239432, 239720.

Part: OXYGEN MASK — FAILED (CABIN)

INSPECTION TYPE:C, PASSENGER O2 FAILED TO DROP AUTOMATICALLY WITH CABIN ALT AT 14.7. CLEARED O2 COMPT''S DOOR EDGES AND FRAMES FROM PANEL AND RECHECKED PER MM 35-20-00. FOUND OK.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY)

15 MIN AFTER TAKEOFF, LOWER AFT CARGO FIRE LIGHT ILLUMINATED. LOWER AFT CARGO FIRE CHECKLIST ACCOMPLISHED, BOTH BOTTLES DISCHARGED. REMOVED AND REPLACED NR 3 AND NR 6 AFT LOWER CARGO SMOKE DETECTORS PER 2 6-16-02 SYSTEM OPS CKS GOOD. ALSO REMOVED AND REPLACED BOTH CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLES IAW MM 26-23-01.

Part: LIGHT — INOPERATIVE (COCKPIT)

LIGHTS INOP IN NR 4 FIRE HANDLE DURING FIRE TEST IN BOTH.. HOWEVER, LIGHTS WILL TEST INDEPENDENTLY IN EITHER A OR B. T/S SYSTEM USING WDM 26-11-41 AND MM 26-11-00. REPLACED K13 RELAY ON FIRE DETECTION MODULE. SYSTEM OPS CHECKS OK PER MM 26-11-00.

Part: FIRE DETECTOR — INOP (CARGO BAY)

CREW PREFLIGHT FIRE WARNING LOWER AFT CARGO NO TEST. DEFERRED AND C/W DMP.

Part: SWITCH — MALFUNCTIONED (CARGO BAY)

INSPECTION TYPE:N/A, AFT CARGO FIRE WARNING. REMOVED AND REPLACED FIRE BOTTLES AND DISCHARGE SWITCH, SYSTEM TESTS NORMAL.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

AFT LOWER CARGO FIRE WARINING ILLUMINATED DURING FLIGHT. DETERMINED TO BE FALSE WARNING. MEL'D AFT LWR CARGO FIRE WARNING PER MEL 26-10-1-1, AND PLACARDED M 180936.

Part: SKIN — CRACKED (R3 EMER EXIT)

INSPECTION TYPE:N/A, R3 DOOR HAD A 5 INCH CRACK ON SKIN AND WAS LEAKING. FABRICATED AND INSTALLED DOUBLER PER SRM 52-00-03.

Part: SKIN — DELAMINATED (R1 DOOR)

INSPECTION TYPE:N/A, R1 DOOR SKIN PEELED BACK-DOOR LEAKING PROFUSELY ON LEADING EDGE BELOW FWD DOOR HINGE. DOOR BULGES OUT APPROX 1 INCH AND APPEARS TO BE IN ERNAL DAMAGE. *S/D* ASSIGNED ECA FORM 04927 TO IEM REPAIR ACCOMPLISHED IAW EO B747-520-1 1894A DISSIMIAL METAL REPAIR TO BE ACCOMPLISHED BY NEXT C CHECK D180 797 ASSIGNED.

Part: DRIVER CARD — DEFECTIVE (FIRE WARN SYS)

INSPECTION TYPE:N/A, ON DEPARTURE CLIMBOUT INTERMITTENT FIRE WARNINGS BEGAN. ALL FIRE WARNING SYSTEMS FOR CARGO COMPTS TESTED GOOD. LWR AFT CARGO FIRE WARNING CONTINUED EMERGENCY RETURN WAS INITIATED AND TOUCHDOWN WAS MADE OVERWEIGHT AND VERY SMOOTH AT APPROX 165 KTS AND 685,000 LBS. RESCUE CREWS REPORTED NO EVIDENCE OF FIRE. REMOVED AND REPLACED A-7 DRIVER CARD LWR CARGO (P/N 69B47519-3), (S/N AA27) ON, (S/N 208) OFF. REMOVED AND REPLACED A-8 DRIVER CARD NR 4 ENG AS PRECAUTION, (P/N 69B47519-3), (S/N FT2-7) ON, (S/N 267) OFF. OPERATIONAL CK OF FIRE WARINING SYSTEM ON LWR CARGO AND NR 4 ENG CKS GOOD PER MM 26-10-01.

Part: SKIN — CRACKED (NR 1 TR UNIT)

INSPECTION TYPE:N/A, 4 X 3 CRACKED OUT AREA AT NR 1 ENG EXHAUST OUTER SLEEVE SKIN O/B SIDE AT 1130. REMOVED TURBINE EXHAUST SLEEVE FRAME ASSY PER MM 78-1-01, INSTALLED NR 1 ENG THRUST REVERSER SLEEVE ASSY PER MM 78-11-00 (P/N 6SB97904-2 10) ON, (P/N 6SB97904-210) OFF, (S/N 000162) ON.

Part: FRAME — CRACKED (LT SERVICE DOOR)

REF LP 254182 ITEM 1 AND THIS LP ITEM 1, FOUND AFT LOWER CORNER OF NR 4 LEFT SERVICE DOOR, VERTICAL FRAME AND HORIZONTAL LOWER EDGE BEAM CRACKED IN RADIOUS. INSTALLED REPAIR DOUBLERS AS PER SRM 52-10-02. PRESSURE CHECK TO BE DONE ON LP 254184 ITEM 3, NO LEAKS NOTED.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT INOP UPPER DECK MOST FWD COVER. REMOVED LAMPS AND NEW BATTERY PACK, NO HELP. ASSY ON ORDER REQ NO A365680. FOUND BATTERY PACK LOW. RECHARGED WITH EXTERNAL PWR, OPS CK GOOD.

Part: GAUGE — MALFUNCTIONED (NR 3 ENGINE)

NR 3 ENG OIL QTY 5.3 PRIOR TO START. 4.3 GAL ON POWER PUSH FOR T/O; DURING CLIMB TO A 26000 LEVEL OFF OIL QTY OBSERVED TO SLOWLY DROP TO 2.6. WHEN POWER REDUCED OIL STOPPED AT 2.6 UNTIL SHUT DOWN. OIL QTY THEN CLIMBED TO 4.5 AFTER SHUTDOWN 2 MIN. RESET C/B ON NR 3 ENG OIL QTY. NR 3 ENG OIL QTY GA SHOWS 5.4, UNABLE TO DUPLICATE ON GROUND. FOR T/S SWAPPED ENG OIL QTY GA 3 AND 2 . BOTH OIL QTY IND WORK OK PER MM 79-31-00

Part: CONNECTOR — LOOSE (NR 1 ENGINE)

AFTER V1 ON TAKEOFF ROLL FIRE BELL WENT OFF BRIEFLY. AT ALTITUDE NR 1 A LOOP FAILED THE FIRE TEST. REFER TO LOG PAGE NR 996478. NR 1 ENGINE NACELLE B LOOP SELECTED. THE NR 1 A LOOP NACELLE INDICATOR CONTINUOUSLY JUMPED BETWEEN - 4 AND 8. FOUND LOOSE CONNECTION ON OUTBD SIDE OF ENG RESECURED OPS CK GOOD PER M/M 26-00 THIS CLEARS DEFERAL M141523 PLACARD REMOVED .

Part: FIRE WARNING — ACTIVATED (COCKPIT)

INSPECTION TYPE-N/A, FIRE BELL AND LIGHT ON TAKEOFF ROLL SOURCE UNKNOWN REPEAT (NOT ENGINES). REMOVED, CLEANED AND RESEATED FIRE DETECTION CHORD A8, OPS CHECKED GOOD PER MM 26-14-00.

Part: SMOKE DETECTOR — MALFUNCTIONED (COCKPIT)

ON TAKEOFF JUST PAST LIFTOFF, GOT MOMENTARY MASTER CAUTION AND FIRE BELL, SUSPECT CAUSED BY MAIN DECK SMOKE DET AS PER LOGPAGE 993132 WRITE UP. ALL SMOKE DETECTORS TEST OPS CK OK. NO FAULTS NOTED REF MM 26-14-00.

Part: FIRE BELL — FALSE WARNING (COCKPIT)

DURING T/O JUST PAST V1 MOMENTARILY FIRE WELL OCCURED, UNABLE TO DETERMINE SOURCE. RE-OCCURED ONCE MORE ABOUT 600' AGL, REPEAT REF PG 993135 NR 2. ALL FIRE WARNING SYS TEST NORMAL, NEED ADDITIONAL INFO AS TO SOURCE. OK FOR SERVICE.

Part: SMOKE DET — MALFUNCTIONED (CARGO COMPT)

INSPECTION TYPE-N/A, ON CLIMBOUT THE NR 4 MAIN DECK CARGO SMOKE DET LIGHT ILLUMINATED MOMENTARILY. THE LIGHT WAS ACCOMPANIED BY THE MASTER FIRE LIGHTS BELLS AND HORN ACTIVATING MOMENTARILY. SYSTEM WAS TESTED, OPS NORMAL. COMMENT NOTED BY MAINT ALL MAIN DECK SMOKE DETECTORS TEST GOOD WITH NO FALSE DETECTIONS.

Part: SKIN — LOOSE RIVETS (BS 2717-2742)

INSPECTION TYPE-C, THERE ARE SEVERAL RIVETS LOOSE AT EXTERNAL SKIN OF TAIL CONE AT STA 2417 AND 2742 ABOUT 25 INCH ABOVE LT APU ACCESS DOOR. SEVERAL RIVETS PULLED THROUGH SKIN, SKIN OUT OF LIMITS ACC SRM 53-30- 01. REPAIRED SKIN OF TAIL CONE AT STA 2717 AND STA 2742 ABOUT 25 INCH ABOVE LT APU, ACCESS DOOR IAW SRM 53-30-03 FIG 1A.

Part: FRAME — DAMAGED (BS 2716.6)

INSPECTION TYPE-C, FOUND DURING REPAIR ON NRC 764826 FRAME DAMAGE AT BS 2716.60 ABOUT 30 INCHES ABOVE LT APU ACCESS DOOR. REPAIRED FRAME DAMAGE AT BS 2716.60 ABOUT 30 INCHES ABOVE LT APU ACCESS DOOR IAW SRM 51-40-03 FIG 1.

Part: UPPER CHORD — CORRODED (BS 2360)

INSPECTION TYPE-C, MAIN DECK FLOOR STRUCTURE, UPPER CHORD CORRODED AT BS 2360 RBL 17. REPAIRED UPPER CHORD FROM LBL 9 TO RBL 55 ACC SRM 53-10-07.

Part: BULKHEAD CHORD — MISDRILLED (BS 2360)

INSPECTION TYPE-C, PRESS BULKHEAD BS 2360 DURING MOD OF BULKHEAD FOUND AT LOWER SIDE RT OF BL 0. CLOSE FASTENER SPACING (NOT IAW SRM) AT LOWER Y-CHORD AND WEB SIGMENTS. (NOT POSSIBLE TO MODIFY, PARTLY REPL OF CHORD NECESSARY). REPAIRED LOWER Y-CHORD AT RT OF BL 0 BS 2360 IAW EO B747-5310- 9485 (KLM DFX 97-194 REV 3).

Part: SEAT TRACK — CORRODED (BS 630-720)

INSPECTION TYPE-C, UPPERDECK: FOUND SEAT TRACK CORRODED AT RBL.27.99 FROM STA 630 TO 720. REPLACED SEAT TRACK AT RBL 27.99 FROM BS 650 TO BS 720 ACC SRM 53-10-05 FIG 1.

Part: SEAT TRACK — CORRODED (BS 640-720)

INSPECTION TYPE-C, UPPERDECK: FOUND SEAT TRACK CORRODED AT RBL 9.33 FROM STA 640 TO 720. REPLACED SEAT TRACK AT RBL 9.33 FROM BS 640 TO 740 ACC SRM 53-10-05 FIG 4.

Part: FIRE LIGHT — DEFECTIVE (CARGO COMP)

INSPECTION TYPE:N/A, DET CARGO FIRE LIGHT AND BELL ON INTERMITTENTLY. CLEANED CONTACTS ON A-8 LWR SMOKE DETECTOR CARD, RELAMPED NR 5 SMOKE DETECTOR SYS, OPS OK PER MM 26-00-00.

Part: BULB — FAILED (COCKPIT)

INSPECTION TYPE:N/A, FWD CTR PNL EMERGENCY LIGHTS INOP. RELAMPED, OPS CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHTS NOT WORKING PROPERLY. THEY STAY ON IN THE OFF POSITION. REMOVED AND REPLACED EMERGENCY LIGHT MODULE. OPS CHK GOOD. P/N ON/OFF 69B46010-24, S/N ON D00336, S/N OFF D00307.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT UPPER DECK OUT. REPLACED. CHECKS GOOD.

Part: FIRE BOTTLES — DISCHARGED (CARGO COMPT)

BOTH LOWER CARGO COMPT. FIRE BOTTLES DISCHARGED AND LIGHTS ARE ILLUMINATED. REPLACED BOTH FIRE BOTTLES PER MM 26-20. P/N ON 35207900M-11, OFF 35207920M-11, P/N ON 34907900M12, S/N ON 00691R1, OFF 00686R1, S/N OFF 02899531 OFF K87.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO COMPT)

AFT CARGO FIRE WARN LIGHT WITH BELL. ACCOMPLISHED AFT CARGO FIRE CHK LIST PRIOR TO LANDING. REMOVED AND REPLACED LWR CARGO COMPT NR 6 SMOKE DETECTOR PER B747MM. OPS CK NORMAL, THIS CLEARS M119730.

Part: FIRE WARNING — MALFUNCTIONED (NR 3 ENGINE)

INSPECTION TYPE, NR 3 ENGINE FIRE LIGHT AND FIRE WARNING BELL CAME ON BRIEFLY 1 TO 2 SECONDS, 4 TIMES DURING THE 7 HOUR FLIGHT. NACELLE TEMP, EGT AND ALL OTHER PARAMETERS NORMAL. INSPECTED NR 3 ENGINE FIRE LOOPS AND PERFORMED TEST IAW MM 26-11-00, NO FAULTS DETECTED AND OPS OK.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO COMPT)

INSPECTION TYPE-N/A, LOWER AFT CARGO FIRE WARNING DURING CLIMB, BOTH FIRE BOTTLES DISCHARGED AS PER AOM. AIR TURNBACK TO SEL. REMOVED AND REPLACED NR 4 SMOKE DETECTOR IN AFT LWR CARGO COMP, OPS CHK NORMAL PER B747 M/M. REMOVED AND REPLACED BOTH FIRE BOTTLES IAW MM 26-23-01, OPS SQUIB AND PRESS SYSTEM CHECK GOOD.

Part: FIRE DETECTOR — MALFUNCTIONED (CARGO COMP)

INSPECTION TYPE N/A, THE AFT LOWER CARGO FIRE PROTECTION WAS GIVING FALSE INDICATIONS PERIODICALLY DURING FLIGHT. PERFORM AFT CARGO LWR FIRE PROTECTION TEST PER MM 26-16-00, OPS CK NORMAL.

Part: SEAT TRACK — DAMAGED (BS 1720-1740)

INSPECTION TYPE: C. FOUND CROWN AREA FROM SEAT TRACK AT BSTA 1720 - 1740 LBL 25 DAMAGED. REPLACED SEAT TRACK IAW SRM 53-10-23 FIG 5/51-30-02.

Part: SHEAR TIE — CRACKED (BS 1740)

INSPECTION TYPE: C. FOUND SHEAR TIE CRACKED AT STA 1740 RT SIDE BETWEEN STR 50 AND STR 51. REPAIRED SHEARED TIE IAW SRM 53-10-04, FIG 3.

Part: FRAME — CORRODED (BS 1820)

INSPECTION TYPE: C. AFT CARGO FRAME TOP CAP AT STA 1820, BBL 26L - 42L. REPAIRED IAW SRM 51-40-03.

Part: SPLICE — CORRODED (BS 2350)

INSPECTION TYPE-C, CORROSION ON STRINGER SPLICE END STRAP AT STA 2350, S-50 LT. REPLACED STRINGER SPLICE END STRAP IAW SRM 51-30-02.

Part: STRINGER — CRACKED (BS 2100)

INSPECTION TYPE: C. FOUND CRACK IN FRAME STRINGER CUT-OUT AT BS 2100 S29R. REPAIRED FRAME IAW SRM 53-10-04.

Part: SPLICE — CORRODED (BS 2350)

INSPECTION TYPE-C, CORROSION ON STRINGER SPLICE END STRAP AT BS 2350 S-48R. STRINGER SPLICE END STRAP REPLACED IAW SRM 51-30-02.

Part: SHEAR TIE — CRACKED (BS 2160)

INSPECTION TYPE: C. BULK CARGO COMPARTMENT FOUND CRACKED IN FRAME SHEAR TIE AT STRINGER CUTOUT AT BS 2160, S42/44 LT. REPAIRED SHEAR TIE IAW SRM 53-10-01.

Part: FRAME — CRACKED (BS 1960)

INSPECTION TYPE: C. FOUND CRACK IN FRAME INNER FLANGE AT BS 1960, S40L. REPAIRED FRAME INNER FLANGE IAW 53-10-04, FIG 66 DETAIL 3.

Part: BRACKET — CRACKED (BS 1760)

INSPECTION TYPE: C. AFT CARGO COMPAARTMENT ATTACHMENT BRACKET FOR LOWER SILL JOINT WITH FRAME AT BS 1760 IS CRACKED IN TOP. REPLACED BRACKET IAW SRM 51-30-02.

Part: TORQUE BOX — CRACKED (BS 1840-1860)

INSPECTION TYPE: C. AFT CARGO COMP. WEB ON TOP OF TORQUE BOX IS CRACKED BETWEEN BS 1840/1860, LBL 63. WORKED OUT CRACK AND REPAIRED IAW SRM'S 51-40-02, 51-30-02.

Part: FRAME — CRACKED (BS 1740)

INSPECTION TYPE: C. AT BS 1740 RT STR 14, FRAME FORMED AND OLD FRAME REPAIR CRACKED. REPAIRED AT BS 1740 RT BETWEEN STR 12 AND STR 14 IAW ETN 747-53-0762.

Part: WEB — CRACKED (NLG WW)

INSPECTION TYPE: C. NLG WHEELWELL: WEB FROM PRESSURE PAN AT BULKHEAD STA 400 IS CRACKED. REPLACED WEB IAW SRM 51-30-02.

Part: STRINGER — CORRDED (BS 983)

INSPECTION TYPE: C. CORROSION FOUND DURING INSP. ON STR 46R BSTA 983 NEAR END FITTING. REPLACED CA. 1 FOOT OF STRINGER IAW SRM 53-10-01, FIG 1, DETAIL 1.

Part: SKIN — CORRODED (BS 987.5)

INSPECTION TYPE: C. FOUND FUSELAGE SKIN CORRODED ON BSTA 987.5 STR 41L AND STR 42L. CUT OUT PIECE OF CORRODED SKIN AND REPAIRED IAW SRM 53-30-03.

Part: FRAME — CRACKED (BS 1860)

INSPECTION TYPE: C. AFT CARGO COMPARTMENT, FOUND CRACK IN TOP OF FRAME BETWEEN STR 41/42 LBL 62 NEAR SIDE GUIDE BRACKET AT BS 1860. REPAIRED CRACK IN FRAME IAW SRM 51-40-03.

Part: SHEAR TIE — CRACKED (BS 1560)

INSPECTION TYPE-C, AFT CARGO COMPARTMENT FRAME SHEAR TIE CRACKED AT BS 1560, BETWEEN S-35/36 LT. REMOVED DAMAGED SHEAR TIE AND REPAIRED SHEAR TIE IAW SRM 53-10-04, FIG 4.

Part: FRAME — CRACKED (BS 1600)

INSPECTION TYPE: C. FOUND CRACK IN TOP OF FRAME RT AT BSTA 1600 NEAR FLOOR STUD STR 34. DRILLED OFF CRACK IAW SRM 51-10-01 AND REPAIRED IAW SRM'S 51-40-03 AND 51-30-02.

Part: FRAME — CRACKED (BS 1500)

INSPECTION TYPE-C, AFT CARGO COMP HAD CRACK IN FRAME INNER CHORD AT BS 1500 RT NEAR FLOOR. REMOVED DAMAGED SECTION OF FRAME INNER CHORD AND REPAIRED FRAME IAW SRM 51-40-03.

Part: EEL — INOPERATIVE (CARGO DECK)

MAINTENANCE REPORTED, EMERGENCY LIGHT ON MAIN CARGO DECK INOP AT POS 3L WEAK. REMOVED AND REPLACED LIGHT MODULE AT MAIN DECK STATION 600 LT PER MM 33-51-00.

Part: SKIN — CRACKED (RT TE MIDFLAP)

WHILE ON GROUND, MAINTENANCE FOUND RIGHT WING I/B MIDFLAP, O/B EDGE APPEARS TO HAVE A 3 INCH CRACK. AREA MARKED WITH RED TAPE. ACCOMPLISHED COMPOSITE REPAIR PER SRM 51-40-09.

Part: PANEL — CRACKED (RT HORIZ STAB)

WHILE ON GROUND, MAINTENANCE FOUND RT HORIZ STAB T/E CRACKED AT NAV LIGHT AREA. ACCOMP COMPOSITE REPAIR PER SRM 51-40-09.

Part: ESCAPE HATCH — NOT SECURE (FLIGHT DECK)

CREW REPORTED ON TAKEOFF ROLL, TOP ESCAPE HATCH OPENED, TAKEOFF ABORTED. SECURED TOP ESCAPE HATCH.

Part: BATTERY PACK — DISCHARGED (UPPER DECK)

WHILE ON GROUND, MAINTENANCE FOUND UPPER DECK EMERGENCY LIGHT ASSEMBLY INOPERATIVE. INSTALLED SERVICABLE BATTERY PACK ON UPPER DECK EMERGENCY LIGHT ASSEMBLY PER MM 33-50.

Part: COVER PLATE — LEAKED (NR 3 ENGINE)

PILOT REPORTED TWO HOURS INTO FLIGHT, NR 3 ENGINE OIL QUANTITY INDICATED 3.5 GALLON OIL LOSS. ENGINE WAS SHUTDOWN WITH 1 GALLON REMAINING. OIL TEMPERATURE AND PRESSURE NORMAL. MAINTENANCE FOUND OIL LEAK AT OIL PUMP COVER PLATE LOCATED ON ENGINE GEARBOX NR 3 ENGINE. REMOVED AND REPLACED PACKING ON COVER PLATES, BAGGED ALL OIL DRAIN LINES, RAN ENGINE. OPS AND LEAK CHECK GOOD.

Part: EEL — INOPERATIVE (UPPER DECK)

WHILE ON GROUND IN SDF, MAINTENANCE FOUND UPPER ESCAPE SLIDE DOOR AFT EMER LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW M/M 33-51-04. OPS CHECK GOOD.

Part: UPPER CHORD — CORRODED (BS 520)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON UPPER CHORD STA 520, LBL 33 TO 75. REPLACED PER SRM 51-30-02.

Part: SEAT TRACK — CRACKED (BS 600)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CRACKED FASTENR HOLE IN SEAT TRACK, STA 600, LBL 33.99. REPLACED PER SRM 53-10-05.

Part: STIFFENER — CORRODED (RT MLG WW)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION INSIDE RT WLG W/W STIFFENER RUNNING FROM STA 1241 TO 1255 ON CENTERLINE WEB. REPLACED PER SRM 51-30-02.

Part: KEEL BEAM — CORRODED (LT MLG WW)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION LT WLG, LWR SIDE OF CANTED PRESSURE DECK AND CORNER OF CENTER LINE KEEL BEAM WEB. INSTALLED REPAIR PER SRM 53-10-07.

Part: FLOORBEAM — CRACKED (BS 640)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM UPPER CHORD, RBL 45, STA 760. INSTALLED REPAIR PER SRM 51-10-01, 53-10-07.

Part: SEAT TRACK — CORRODED (BS 640)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK, STA 640, RBL 98. REPLACED PER SRM 53-10-05.

Part: SEAT TRACK — CORRODED (BS 880)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK LBL 33, BS 880. REPLACED PER SRM 53-10-05.

Part: FLOORBEAM — CORRODED (BS 800)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 800, LBL 75 TO 80. INSTALLED REPAIR PER SRM 53-10-07.

Part: SEAT TRACK — CORRODED (FS 870)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND A CORROSION CRACK AT THE SEAT TRACK AT STATION 870 AND LBL 98. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 53-10-05.

Part: WEB — CORRODED (FS 1245)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CENTERLINE WEB IN THE RIGHT HAND WLG WHEEL WELL AT STATION 1245. MAINTENANCE REMOVED CORROSION AND INSTALLED DOUBLER IAW EO 747-53-0711.

Part: FLOORBEAM — CORRODED (FS 860)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER CHORD OF THE FLOORBEAM AT STATION 860 AND LBL 75. MAINTENANCE REWORKED AND TREATED THE AREA ACCORDING TO SRM 51-10-01.

Part: SEAT TRACK — CORRODED (FS 520)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SEAT TRACK AT STATION 520 AND LBL 75. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 53-10-05.

Part: SEAT TRACK — CORRODED (FS 860)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND HEAVY CORROSION ON THE SEAT TRACK AT STATION 860 AND RBL 33.99. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 53-10-05.

Part: SEAT TRACK — CORRODED (FS 1300)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON THE SEAT TRACK BETWEEN STATION 1300 AND 1420 AND LBL 11.33. MAINTENANCE REMOVED AND REPLACED WITH NEW SEAT TRACK IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FS 860)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SEAT TRACK AT STATION 860 AND RBL 98. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 53-10-05.

Part: SEAT TRACK — CORRODED (FS 520)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SEAT TRACK AT STATION 520 AND LBL 33.99. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 53-10-05.

Part: SEAT TRACK — CORRODED (FS 680)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SEAT TRACK AT STATION 680. MAINTENANCE REPLACED THE TRACK PER SRM 53-10-05.

Part: SEAT TRACK — CORRODED (BS 1440-1495)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK HORIZONTAL FLANGE, RBL 33.99, BS 1440 TO 1490 AND 1495. REPLACED PER SRM 53-10-05.

Part: SEAT TRACK — CORRODED (BS 1496)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK HORIZONTAL FLANGE, RBL 75.92, BS 1496. REPLACED PER SRM 53-10-05.

Part: D-BEAM — CRACKED (NR 3 PYLON)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CRACK IN D-BEAM, FRONT SIDE, NR 3 PYLON. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 480-510)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK BS 480 TO 510, LBL 98. REPLACED PER SRM 53-10-05.

Part: FLOORBEAM — CORRODED (BS 520)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM UPPER CHORD, STA 520, LBL 11.33 TO LBL 55. REPLACED PER SRM 51-40-04.

Part: KEEL BEAM — CORRODED (BS 1241)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION RT WLG W/W BSTA 1241, CANTED PRESSURE DECK KEEL BEAM T-CHORD AT RBL 4, BETWEEN APU FUEL FEED CLOSE-OUT PANEL AND T-CHORD. INSTALLED REPAIR PER SRM 53-10-07.

Part: DOUBLER — CRACKED (PAX DOOR)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CRACK ON DOUBLER OF LWR HINGE ARM CUTOUT, ON MAIN RT MAIN ENTRY DOOR. INSTALLED REPAIR PER SB 747-52-2144.

Part: SEAT TRACK — CORRODED (FS 780)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SEAT TRACK AT THE LOWER SIDE OF STATION 780 TO 800 AND RBL 98. MAINTENANCE REPLACED THE SEAT TRACK AND INSTALLED NEW SPLICES IAW SRM 53-10-05.

Part: SEAT TRACK — CORRODED (FS 800)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON THE SEAT TRACK AT STATION 800 TO 840 AND WBL 98.58. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 53-10-05.

Part: INTERCOSTAL — CORRODED (FS 1327)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON THE INTERCOSTAL AT STATION 1327 BETWEEN LBL 11.33 AND RBL 11.33. MAINTENANCE REPLACED THE INTERCOSTAL IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FS 1300)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON THE SEAT TRACK BETWEEN STATION 1300 AND 1420, RBL 11.33. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 51-30-02.

Part: INTERCOSTAL — CORRODED (BS 1367)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL, BS 1367, LBL 11.33, AND LBL 33.99. REPLACED PER SRM 51-10-01.

Part: SKIN — CRACKED (BS 460)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CRACK AT BS 460, RT BETWEEN STR 14E AND 16. INSTALLED REPAIR PER UPS EO B747-5330-0661C.

Part: FLOORBEAM — CRACKED (BS 520)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CRACK IN FLOORBEAM WEB BS 520, LBL 11 TO 33. INTSALLED REPAIR PER SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (BS 1367)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL, BS 1367, LBL 11.33, AND RBL 11.33. REPLACED PER SRM 51-10-01.

Part: EEL — INOP (FLIGHT DECK)

MAINTENANCE REPORTED, UPPER RT PASSENGER CABIN EMER LIGHT INOP. REPLACED LIGHT, OPS CK GOOD.

Part: EEL — INOP (FLIGHT DECK)

(SUPPLEMENTAL MRR) MAINTENANCE REPORTED UPPER RT PASSENGER CABIN EMERGENCY LIGHT INOP. REPLACED EMER LIGHT. OPS CK GOOD.

Part: EEL — INOP (FLIGHT DECK)

MAINTENANCE REPORTED ONE EMERGENCY LIGHT OVER THE CREW SERVICE DOOR IS INOPERATIVE. DEFERRED CREW EMERGENCY EXIT (1) ONE LIGHT INOP PER MEL 33-13.