N680UP

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHT INOPERATIVE, PASSENGER AREA. REPLACED BATTERY PACK, OPS CHECK GOOD.

Part: SWITCH — JAMMED (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY LIGHTING SWITCH JAMS. INSTALLED NEW EMERGENCY CONTROL MODULE PER AMM 33-51-09 AND EO B747-3350-20899A, OPS CHECKED NORMAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, BELOW FLOOR INTERCOSTAL WEB CRACKED AT BS 2220 S-37R AS MARKED. BS 2220 S-37R BELOW FLOOR INTERCOSTAL WEB REPLACED AS PER SRM 51-10-01 PG 8.

Part: STRAP — CORRODED (LT WNG REAR SPAR) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, BS 1241 LEFT WING REAR SPAR LOWER SPLICE FOUND CORROSION AT HOLE -A- ALL LAYERS APPROX 12 O/C POSITION AND APPROX 0.030 INCH DEEP. CORROSION REMOVED AND BOLT HOLE FINAL OVERSIZE TO 0.907 INCH PER EO B747-5710-12138-G, HFEC INSPECTED RESULT, NO CRACK AND CORROSION FOUND. BOLT BACB30US14K50Y INSTALLED PER EO B747-5710-12138-G APPENDICES -D- ITEM 7, FUEL LEAK CHECK CARRIED OUT SATISFACTORY.

Part: FITTING — CRACKED (RT WNG SPAR) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE:C RIGHT WING REAR SPAR LOWER KICK FITTING HOLE -C- FOUND CRACKED APPROX 0.040 INCH. KICK FITTING HOLE -C- OVERSIZED TO 0.937 INCH TO REMOVE CRACK. HFEC INSPECTED CONFIRM CRACK FREE FASTENER HOLE BUSHING REPAIRED AND BOLT BACB30US14K45X INSTALLED PER RS R57-12-35122 AND EO B747-5710-20137-A REF UPS-HKG-04-00063F, UPS-HKG-04-00065H.

Part: FITTING — CRACKED (LT WING SPAR) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE:C LLEFT WING REAR SPAR LOWER KICK FITTING HOLE -C- FOUND CRACKED APPROX 0.040 INCH. LOWER KICK FITTING HOLE -C- OVERSIZED TO 1.000 INCH TO REMOVE CRACK. HFEC INSPECTED CONFIRM CRACK FREE. FASTENER HOLE BUSHING REPAIRED PER RS R-57-12-35122. BOLT P/N BACB30US14K45X INSTALLED. REF UPS-HKG-04-00063F, UPS-HKG-04-00065H, EO B747-5710-20137-A.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, REF EO B747-5310-1093M LEFT BS 1241 FWD HOLE FOUND A BUSHING IN BULKHEAD FORGING. LEFT BS 1241 FWD HOLE FORGING OLD BUSHING REMOVED. HFEC INSPECTED, RESULT NO CRACK FOUND. BUSHING FABRICATED AND INSTALLED PER RS R53-43-35119. BOLT BACB30US12K46 INSTALLED PER RS R53-43-35119 AND EO B747-5310-20150-A, REF SB 747-53-2283 REV 4, UPS-HKG-04-00059H.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, REF EO - B747-5310-1093M LT BS 1241 AFT HOLE FOUND A BUSHING IN SKIN. LEFT BS 1241 AFT HOLE SKIN OLD BUSHING REMOVED. HFEC INSPECTED RESULT, NO CRACK FOUND. BUSHING FABRICATED AND INSTALLED PER RS R53-43-35119. BOLT BACB30US12K40 INSTALLED REF: SB747-53-2283 REV 4 FIG 14, EO B747-5310-1093-M AND EO B747-5310-20150-A, UPS-HKG-04-00059H.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, AFT OF BULK CARGO COMPT - RT STA 2240 STRINGER 46 TIE CLIP FOUND CRACK. DEFECTIVE AREA STRINGER TIE CLIP REPLACED AS PER SRM 51-10-01 PAGE 8.

Part: BUSHING — CRACKED (FUSELAGE) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, REF EO B747-5310-1093-M RT SIDE BS 1241 FWD HOLE HAS BEEN OVERSIZED TO 1 INCH AND HAS A BUSHING INSTALLED. OLD BUSHING REMOVED AND HFEC INSPECTED RESULT CONFIRM CRACK FREE ON ALL LAYERS. BUSHING REPAIRED ON LONGERON AND ON SKIN. SPLICE STRAP AND FORGING PER RS R53-43-35119 AND BOLT BACB30US12K46, INSTALLED AS PER RS R53-43-35119, UPS-HKG-04-00059H EO B747-5310-1093-M AND EO B747-5310-20150-A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE:C AFT OF BULK CARGO COMPT- RT STA 2240 FRAME CRACKED BETWEEN STR R38 & STR R40 AREA. AFT OF BULK CARGO COMPT - RT STA 2240 FRAME STR 35R TO STR 40R REPLACED AS PER RS R53-62-35127 AND ENGINEERING FILE 747-53-20173.

Part: FITTING — CRACKED (LT WING) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, BS 1241 LT WING REAR SPAR UPPER SPLICE FITTING FOUND CRACKS AT HOLE NR 5. BS 1241 LT WING REAR UPPER SPLICE FITTING HOLE NR 5 REAMED TO REMOVE CRACKS. HFEC INSPECTED RESULT CRACK FREE. FINAL HOLE DIAMETER IS 1.000 INCH AND BUSHING INSTALLED AS PER EO B747-5740-17032-A APPENDIX -E-.

Part: SPAR — CORRODED (WING) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE:C BS 1241 WING REAR SPAR LEFT UPPER CHORD FOUND CORROSION AT HOLE NR 9 APPROX 0.030 INCH DEPTH. BS 1241 WING REAR SPAR LEFT UPPER CHORD BOLT HOLE NR 9 CORROSION REMOVED NDT INSPECTED RESULT CORROSION FREE. BOLT HOLE BUSHING REPAIRED AS PER EO B747-5740-17032-A APPENDIX -E-. SEPARATE BUSHING INSTALLED IN INTERNAL SPLICE FITTING AND UPPER CHORD.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, AFT CARGO COMPT - STA 1840 IN BETWEEN STR 51L AND STR 51R SHEAR TIE FOUND CRACKED. DEFECTIVE AREA SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3.

Part: FITTING — CRACKED (NR 1 DIA BRACE) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, CRACK FOUND AT NR 1 DIA BRACE UNDERWING ATTACHED FITTING'S MOST AFT HOLE OF THE O/B ROW, CRACK LENGTH .125 INCH LONG APPROX AT THE UPPER SURFACE. CRACKED HOLE REPAIRED PER RS R57-04-35118 AND EO B747-5740-20132-A.

Part: BEAM — CRACKED (NOSE WHEEL WELL) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, NOSE WHEEL WELL, VERTICAL BEAM WEB RT BS 280 BETWEEN 1ST AND 2ND STIFFENER ONE INSULATION BLANKET STAND OFF HOLE CRACK FOUND APPROX 2 INCHES LONG AS MARKED (WL 160 TO 170). BEAM WEB REPAIRED AND REPAIRED PART INSTALLED AS PER SRM 51-40-02 FIG 1.

Part: FITTING — CRACKED (RT WING) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE:C RT WING BS 1241 WING REAR SPAR UPPER SPLICE PLATE NR 4 FASTENER HOLE WAS CRACKED APPROX 0.040 INCH LONG RUNNING TOWARDS AFT (WL 180). BUSHING REPAIRED AS PER EO B747-5740-17032-A FINAL OVERSIZE FASTENER HOLE WAS 1.000 INCH AS PER APPENDIX -E-.

Part: STRINGER — DENTED (FUSELAGE) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, FWD CARGO COMPT, LT STA 580 - STA 600 STR 46 FOUND DENT MARK. FWD CARGO COMPT LT BS 580 - BS 600 STR 46L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: SEAL — CHAFED (FUSE TO VERTICAL) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE:C EMP AFT FUSELAGE TOP SKIN LT SIDE VERT FIN SEAL INTERFACE AREA FOUND MINOR CHAFE MARK FROM BS 2284-2360. BS 2284-2360 SKIN WEAR DAMAGE AREA SMOOTHED OUT AS PER SRM 51-10-01 & REPROTECTED AS PER SRM 51-10-02 WITHIN SRM 53-30-01 FIG 1. FLAGNOTED & EO 5330-18431-A ITEM 8 ALLOWABLE DAMAGE LIMITS. EXCEPT BS 2300-2320 & BS 2330-2360 EXCEEDED LIMITS. SKIN REPAIR C/O AS PER SRM 53-30-03 FIG 1 CATEGORY B REPAIR REPEAT INSPECTION REQ PER SRM 53-30-03 FIG 1 SHT 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, FWD CARGO COMPT, LEFT STA 980 FRAME FOUND CRACKED AT STRINGER 39 AREA. FRAME REPAIRED PER SRM 53-10-04 FIG 64.

Part: ANGLE — CORRODED (FAIRING) · airframe 66,233 hrs · 33,562 cycles

INSPECTION TYPE: C, FX- AIRCON BAY FAIRING SUPPORT UPPER SURFACE CORROSION AT STA 1040 FROM RBL 15 - 57. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM 53-50-01 FIG 5 LIMITS, FAIRING SUPPORT REPLACED PER SRM 51-10-01 PG 8 & CIC APPLIED IAW EO M5100-2780-E.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A UPPER DECK CEILING RIGHT EMERGENCY LIGHT INOP. RELAMPED CEILING EMERGENCY LIGHT CHECKS GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,386 hrs · 33,383 cycles

INSPECTION TYPE: SP, SKIN EXFOLIATED ON AFT BELLY SKIN AT STA 1964 STR 45L 3.5. CUT OUT CORRODED AREA PER SRM 53-30-03. REMOVED LITE SURFACE CORROSION ON INTERNAL TEAR STRAP, FOUND WITHIN LIMITS, NDT HFEC PER NDTSOM 06 10-01.001, NO CRACKS NOTED AT CUTOUT. FABBED DOUBLER AND FILLER FROM 2 024T3 .071, TREATED AND PRIMED PARTS, INSTALLED COUNTER SINK WASHERS, INSTALLED REPAIR PARTS PER SRM 53-30-03 FIG 47 SRM 51-30-02.

Part: SKIN — CRACKED (FWD ENTRY DOOR) · airframe 65,385 hrs · 33,382 cycles

INSPECTION TYPE: SPV, COMPLY WITH D266098 L1 DOOR OUTER AFT SKIN IS CRACKED AT APPROX STA 472 AT APPROX WATER LINE 210. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 52-10-02 FIG 9, 51-10-02, 51-30-08.

Part: FORGING — CORRODED (BULKHEAD) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE: C CORROSION REVEALED ON RT BS 1241 BULKHEAD FORGING AT UPPER KICK FITTING ATTACH FASTENER HOLE BY APPROX 0.030" DEEP AS PER ATTACH FIGURE. R/H BS 1241 B/H KICK FTG ATTACH FORGING UPPER HOLE REPAIRED AS PER HX RS R-53-43-34916 & UPS EO B747-5310-17698-A. NOTE : L/R BS 1241 FAILSAFE STRAP IS TO BE INSPECTED PER SB 747-53-2283 'CRACK SAFE' PROCEDURE EVERY 3000 FLIGHTS. THE SPLICE STRAPS & SOLID FILLERS REQUIRED TO CHANGE WITHIN 2 YEARS.

Part: FORGING — CRACKED (BULKHEAD) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE: C CRACK FOUND ON LT BS 1241 BULKHEAD FORGING AT LWR KICK FITTING FASTENER HOLE BY APPROX 0.050" LONG RUNNING AT FWD DIRECTION. LH BS 1241 BULKHEAD KICK FTG ATTACH FORGING LOWER BOLT HOLE REPAIRED AS PER HX RS R-53-43-34916 & UPS EO B747-5310-17698-A. NOTE : L/R BS 1241 FAILSAFE STRAP TO BE INSPECTED PER SB 747-53-2283 'CRACKED STRAP' PROCEDURE EVERY 3000 FLIGHTS. THE SPLICE STRAPS & SOLID FILLERS TO CHANGE WITHIN 2 YEARS.

Part: WEB — CRACKED (#2 PYLON) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C #2 PYLON MID SPAR WEB HAS CRACK AT PREVIOUS REPAIR NAC STA 205 APPROX. #2 PYLON MID SPAR WEB CRACK AT NAC STA 205 REPAIRED REF SRM 54-10-03 FTG.12 / SRM 51-30-02.

Part: WEB — CRACKED (BS 260 B/H WEB) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C LH TUNEL AREA 7 BS 260 B/H WEB INNER UPR CORNER AROUND FASTENER HEAD AT LBL 35". B/H WEB REPAIRED AS PER SRM 53-10-04 FIG.48.

Part: WEB — CRACKED (RH TUNNEL BS 260) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C RH TUNEL AREA 7 BS 260 B/H WEB INNER UPPER CORNER CRACK AROUND FASTENER HEAD AT RBL 35". BULKHEAD WEB REPAIRED AS PER SRM 53-10-04 FIG 48..

Part: SUPPORT — CORRODED (FX BS 880) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C FX- BS 880 RBL 30 - LBL 30 BODY FAIRING SUPPORT SURFACE CORROISON FOUND. CORROSION BLEND OUT 0.046"X1"X3", EXCEED SRM LIMIT, REPAIRED AS PER SRM 53-50-04 FIG.2

Part: BEAM — CRACKED (NLGWW) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C NOSE WHEEL WELL BODY STRUCTURE CRACK FOUND AT R/H VERTICAL BEAM STAND-OFF HOLE AT BS 300 BETWEEN #5 & #6 VERTICAL BEAM CLIP (COUNT FROM LOWER) REFER FIGURE ATTACHED. VERTICAL BEAM WEB REPLACED PER SRM 51-10-01 P.8.

Part: WEB — CRACKED (NOSE W/W) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C NOSE W/W BODY STRUCTURE CRACK FOUND AT LH BS 320 VERTICAL BEAM WEB, ONE EACH STAND-OFF HOLE WAS CRACKED BTN #2 & #3 VERTICAL BEAM CLIPS AND 2 STAND-OFF HOLES CRACKED BTN #5 & #6 CLIPS REFER FIG ATTACHED. VERT BEAM WEB REPLACED PER SRM 51-10-01 P.8.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C BS 540 UPPER DECK FLOORBEAM UPPER HORIZONTAL FLANGE, 1 EA FASTENER HOLE CRACK FOUND AT RBL 42, 1/8 INCHES LONG RUNNING AFT. FLOORBEAM AT BS 540 RBL 42 REPAIRED AS PER SRM 53-10-07 FIG 21.

Part: BEAM — CRACKED (NLG WW) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE: C NOSE WHEEL WELL BODY STRUCTURE CRACK FOUND AT RT VERTICAL BEAM WEB STAND-OFF HOLE AT BS 320 BTN 2 & 3 ( COUNTED FROM LOWER) VERTICAL BEAM CLIPS & ANOTHER CRACKED STAND-OFF HOLE FOUND BTN NR 5 & 6 CLIPS PLEASE REFER FIGURE ATTACHED. VERTICAL BEAM WEB REPLACED PER SRM 51-10-01 P8.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C FX BS 1620 RBL 50-56 BODY SUPPORT FRAME CORRODED. CORROSION BLEND OUT 0.039 X 1 X 2 INCHES EXCEED SRM LIMIT, REPAIRED AS PER SRM 53-50-01.

Part: PANEL — CRACKED (NOSE W/W) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C NOSE W/W TOP PNL WEB FOUND CRACK AT BS 291 LBL 15 JUST FWD OF INTER- COSTAL. NOSE W/W TOP PANEL REPAIRED AS PER SRM 53-10-04 FIG.117.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE: C RT BS 1810 STR 27 AFT CARGO DOOR UPPER DOOR UPPER FWD CORNER 1 EA FASTENER HOLE CRACK FOUND AT SKIN , APPROX 1/8 INCH RUNNING DOWNWARD. PLS REFER ATT FIG. AFT CARGO DOOR CUTOUT UPPER FWD CORNER REPAIRED AS PER SRM 53-30-03 FIG 62. REPEAT INSPECTION IN 3000 CYCLES INTERVAL.

Part: SKIN — CORRODED (LHW LWR SURFACE) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C LHW LWR SKIN SURFACE CORROSION IS FOUND AT FUEL TANK ACCESS DR 522BB CUTOUT. CORROSION BLEND OUT 0.06"X0.5"X8"EXCEED SRM LIMIT 57-30-03. CORROSION REMOVED REFER SOPM 20-20-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE: C LT SIDE BS 1241 SPLICE STRAP 2 EACH CRACKS REVEALED OF AFT HOLE RUNNING AFT THE THICKNESS. REF HX RS R-53-43-34916 & UPS EO B747-5310-17698A. THE CRACKED STRAPS MUST BE INSPECTED EVERY 3000 FIGHTS PER EO B747-5310-0323 & SB 747-53-2283 UNTIL SPLICE STRAPS & SOILID FILLERS REPLACED WITHIN 2 YEARS.

Part: STRAP — CRACKED (BULKHEAD) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE: C LT SIDE BS 1241 BULKHEAD SPLICE STRAP AREA, CRACK REVEALED AT AFT HOLE AT SKIN RUNNING FWD APPROX 1/8" IN LENGTH. LH BS1241 B/H SKIN AFT HOLE REPAIRED AS PER HS RS R-53-43-34916 INSTRUCTION 'A' & UPS EO B747-5310-17698-A. (NOTE : L/R FAILSAFE STRAP IS TO BE INSPECTED PER SB 747-53-2283 'CRACKED STRAP' PROCEDURE EVERY 3000 FLIGHTS. THE SPLICE STRAPS & SOLID FILLERS REQUIRED TO REPLACE WITHIN 2 YEARS)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C LT BS 1480 AREA FOUND HOLE NR 26 CRACKED AT BULKHEAD WEB. LT BS 1480 BULKHEAD SPLICE WEB NR 26 BOLT HOLE OVERSIZED TO 0.660 INCH & CONFIRMED CRACK FREE. REPAIR BUSHING FABRICATED & INSTALLED AS PER BOEING SB 747-53A2390 FIG 11 & HAECO RS R-53-43-34911 & UPS EO B747-5310- 17623-A. THE REPEAT INSPECTION OF BS 1480 BULKHEAD & SPLICE COMPONENT WILL BE REDUCED TO 4800 FLIGHT CYCLES AS PER UPS EO B747-5310-10732.

Part: STRAP — CRACKED (BULKHEAD) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE: C RT SIDE BS 1241 BULKHEAD SPLICE STRAP CRACK REVEALED AT AFT HOLE RUNNING FWD & AFT. REFER HX RS R-53-43-34916 & UPS EO B747-5310-17698-A. THE CRACKED STRAPS MUST BE INSPECTED EVERY 3000 FLIGHTS PER EO B747-5310-0323 & SB 747-53-2283 UNTIL STRAPS AND SOILD FILLERS REPLACED WITHIN 2 YEARS.

Part: FRAME — CRACKED (M/D BS 380 S24AR) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C M/D BS 380 S24AR FRAME CRACKED. RH FRAME AT BS 380 S24AR REPAIRED AS PER HX RS R53-12-34913 & UPS EO B747-5310-17674-A. TO BE CONTINEOUS TO INSPECT THE REPAIR AREA UNTIL SB 747-53-2272 MOD IS COMPLETED.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE: C LT BS 2231 STR 25 1 EA FASTENER HOLE CRACK FOUND AT REVEAL RUNNING FWD APPROX 0.040 INCH AND RUNNING AFT APPROX 0.020 INCH. PLS REFER ATT FIG. BS 2231 S25L STRAP REPAIRED AS PER SRM 53-10-04 FIG 115. ** REPEAT INSPECTION PER BSB 53A2450 AT 3000 FLT CYCLES INTERVAL.**

Part: STRUCTURE — DAMAGED (RT WING) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE: C RT WING LE CAVITY FRONT SPAR LOWER CHORD VERTICAL FLANGE THICKNESS FOUND BLENDED PREVIOUSLY AT OLES 1322, PLS CHK LIMITATION. (20 INCHES O/B WING JACK AREA) RT WING L/E FRONT SPAR LWR CHORD VERTICAL FLANGE AT OLES 1322 IS REPAIRED AS PER HX RS R-57-21-34917. (UPS AUTH # 747-57-20036)

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE: C M/D - BS 2231 S25R FRAME CHORD FOUND CRACKED. BS 2231 FRAME CHORD REPAIRED AT STR 24R-26R AS PER HX RS R53-62-34918 (UPS EO B747-5310-17697-A).TO BE CARRY OUT REPEAT INSPECTION IN THE REPAIR AREA AT 3000 CYCLE INTERVALS PER SB 747-53A2450.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C AFT BULK CARGO - BS 2231 S33R FRAME ATTACH ANGLE FOUND COR DAMAGED. COR BLEND OUT 0.63" X 1" X 1" EXCEED SRM LIMIT. ANGLE REPLACED AS PER SRM 51-10-01 P.8.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE: C DURING RAP MOD ACCOMPLISH, BS 970-975 STR 40L-41L PREVIOUS REPAIR DOUBLER IS LESS THAN EXISTING SKIN THICKNESS & SHORT EDGE MARGIN FOUND AT CUTOUT AREA. FX SKIN REPAIRED AT BS 970-975 STR 40L-41L AREA AS PER SRM 53-30-03 FIG 1.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE:C LT BS 800 FRAME S16 AREA, ONE FASTENER HOLE FOUND CRACKED AT STRAP 1/8 INCHES RUNNING FWD AND AFT, CRACK AT ANGLE 0.040 INCH RUNNING FWD REF ATT SKETCH FOR DETAILS. BS 800 FRAME CRACKED AREA REPAIRED PER RS R53-22-34910. ** TO BE CONTINUEOUS PERFORMING REPEAT INSPECTION PER SB 747-53A2451 EVERY 3000 FLIGHT CYCLES. **

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 63,455 hrs · 32,969 cycles

INSPECTION TYPE: C RT BS 800 FRAME AREA FOUND 5 EA FASTENER HOLES CRACKED. REF ATT SKETCH FOR DETAILS. STRAP AND CHORD REPAIRED AS PER RS R53-22-34910 & UPS EO NR B747-5310-17666-A. ** TO BE CONTINUEOUS PERFORMING REPEAT INSPECTION PER SB 747-53A2451 EVERY 3000 FLIGHT CYCLES.**

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A FORWARD MOST LEFT SIDE EMERGENCY LIGHT IN COURIER COMPARTMENT IS INOP. REMOVED AND REPLACED LEFT SIDE EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (NR 1 PYLON) · airframe 62,902 hrs · 32,847 cycles

INSPECTION TYPE:SPC NR 1 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT AFT WEB DOUBLER APPROX .25 INCH IN LENGTH. NR 1 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER HX RS 54-53-34828.

Part: BULKHEAD — CRACKED (NR 2 PYLON) · airframe 62,902 hrs · 32,847 cycles

INSPECTION TYPE:SPC NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT AFT WEB DOUBLER APPROX .1875 INCH IN LENGTH. NR 2 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER R54-53-34828.

Part: BULKHEAD — CRACKED (NR 4 PYLON) · airframe 62,902 hrs · 32,847 cycles

INSPECTION TYPE:SPC CRACK REVEALED AT NR 4 PYLON REAR ENGINE MOUNT BULKHEAD FWD SIDE I/B DOUBLER, THE CRACK INITIATED FROM ONE FASTENER HOLE PROPAGATED UPWARD TO THE EDGE CRACK LENGTH .1875 INCH. NR 4 PYLON REAR MOUNT BULKHEAD REPAIRED AS PER HX RS R-54-53-34828.

Part: FITTING — CRACKED (T/E FLAP)

INSPECTION TYPE:A LT INBOARD FORE FLAP CENTER SUPPORT FITTING HAS A CRACK AROUND IT. REPLACED LT INBOARD FORE FLAP PER MM 27-51-02.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A 2 EMERGENCY EXIT DOOR SLIDE LIGHTS INOP. REMOVED AND REPLACED CREW DOOR BATTERY PACK IAW B747 MM 33-51-04, OPS CHECKS GOOD.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 CABIN - R5 DOOR FWD LOWER CORNER FOUND CRACKED. R5 DOOR FWD LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 1B.

Part: RIB — CRACKED (RT WING) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 RT - CORROSION CRACK IS REVEALED AT ILES 630.72 RIB AS MARKED. RT RIB WAS REPAIRED AS PER SRM 51-40-02 AFTER CORROSION REMOVED AS PER SRM 51-10-01.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 NOSE WHEEL WELL VERTICAL BEAM LT BS 300 FRAME WEB FOUND NR 2 STAND OFF HOLE CRACK (COUNT FROM TOP APPROX. 1/4 INCH IN LENGTH AT 7 O/C POSN AS MARKED. (LOOKING FWD) VERTICAL BEAM WEB REPLACED IAW BOEING SB 747-53A2293, PROCEDURE 3 PART IV PER DRAWING 624U0005 SHEET 1 & 13.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 FX - STA 1404 LBL 16 - RBL 16 KEEL BEAM PANEL SUPPORT FIND WITH CORRODED. SUPPORT REPLACED AS PER 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 AFT CARGO - STA 1913 BALLMAT SUPPORT SURFACE CORR AT RBL 30, RBL 40 & RBL 60. REPAIR AS PER SRM 51-40-03 FIG 1.

Part: BEAM — CRACKED (EMERGENCY DOOR) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C6 CRACK REVEALED ON THE FWD BOTTOM OF HORIZONTAL BEAM OF DOOR 2L. 2L DOOR FWD BOTTOM OF HORIZONTAL BEAM REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 M/D - BS 2240 LBL 40-75 FLOORBEAM UPPER SURFACE FOUND CORROSION FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 9.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 M/D - R2 DOOR FWD CUTOUT REVEAL FOUND CRACKED. NR 2 RT DOOR LWR REVEAL AND FRAME INNER CHORD STRAP REPAIRED AS PER SRM 53-10-04 FIG 84.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 FX - BODY FAIRING SUPPORT UPPER & LWR SURFACE CORR AT STA 1480 FROM LBL 55 - RBL 40. STA 1480 LBL 55 - RBL 40 BODY FAIRING SUPPORT REPLACED AS PER SRM 51-10-01 P.8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 CABIN - FRAME FOUND CRACK AT STA 560 BETWEEN STR 23L TO STR 24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 11.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 FX - BODY FAIRING SUPPORT SURFACE CORROSION AT LBL 58 FROM STA 1170-1230. LT STA 1170-1230 LBL 58 BODY FAIRING SUPPORT SURFACE REPLACED AS PER SRM 51-40-04 FIG 1.

Part: FITTING — CRACKED (PAX DOORWAY) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 M/D - R3 DOOR FWD CUTOUT NR 6 STOP FITTING CRACKED. NR 6 STOP FITTING REPLACED AS PER SRM 51-10-01. `

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 FX - STA 1426 LBL 16 - RBL 16 KEEL BEAM PANEL SUPPORT FOUND WITH CORRODED. SUPPORT REPLACED AS PER SRM 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 FX - STA 1465 LBL 16 - RBL 16 KEEL BEAM PANEL SUPPORT FOUND WITH CORRODED. ***CPCP*** SUPPORT REPLACED AS PER SRM 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 FX - AFT BODY FAIRING SUPPORT SURFACE CORROSION AT STA 1540 FROM LBL 40 - RBL 60 AS MARKED. SUPPORT REPAIRED AS PER SRM 53-50-04 FIG 2.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 BULK CARGO COMPT - FLOOR SUPPORT CORROSION REVEALED AT STA 1940, LBL 55 AS MARKED. FLOOR SUPPORT BETWEEN STA 1920 TO STA 1950 LBL 55 REPAIRED AS PER 53-10-07 FIG 20.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 AFT CARGO - BILGE AREA STA 1750 STR 51R SURFACE CORROSION. AFT CARGO - BS 1750-1770 STR 51R REPAIRED AS PER SRM 53-10-03 FIG 8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 BULK CARGO COMPT - FLOOR PANEL SUPPORT LOWER SURFACE FOUND CORROSION AT STA 1920 LBL0 AS MARKED. FLOOR PANEL SUPPORT REPAIRED AT BULK CARGO COMPTMENT BETWEEN STA 1920 TO 1925 BL 0.

Part: BEAM — CRACKED (PAX DOOR) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 CRACK REVEALED ON THE FWD BOTTOM OF HORIZONTAL BEAM OF DOOR 4L. 4L DOOR FWD BOTTOM OF HORIZONTAL BEAM REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: FRAME — CRACKED (NR 4 PYLON) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 NR 4 PYLON PYLON AFT TORQUE BULKHEAD O/B VERTICAL CHORD, CRACK FOUND AT 2ND FASTENER HOLE (FROM LOWER) RUNNING O/B APPROX. 0.100 INCH LONG. NR 4 PYLON AFT TORQUE BULKHEAD O/B VERTICAL CHORD CRACKED HOLE O/SIZE FASTENER INSTALLED WITH FREEZE PLUG IAW UPS-HKG-01-00015H AND UPS-HK-01-00016.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 FX - EXTERIOR SKIN STA 2160 STR 46R CORR CRACK REVEALED ***CPCP*** FX - EXTERIOR SKIN AT STA 2160 STR-46R REPAIRED AS PER SRM 53-30-03 FIG 1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3, AFT CARGO BAY- FLOOR PANEL SUPPORT FOUND CRACK AT STA 1976 RBL 30 AS MARKED. FLOOR PANEL SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 CABIN - ''U'' CHANNEL I/B FLANGE FOUND CRACKED AT STA 994-995 LBL 75. U CHANNEL REPLACED AS PER SRM 51-10-01.

Part: SHAFT — CORRODED (RT FLAP TRACK) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 RT WING NR 8 FLAP TRACK GENEVA CAM ROLLER SUPPORT ROD CORRODED. RT WING NR 8 FLAP TRACK AFT ROLLER SUPPORT SHAFT & ROLLER REPLACED IAW MM 27-51-40.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 M/D - BS 1350-1370 LBL 116 MOST O/B LONGITUDINAL FLR SUPPORT FOUND CRACKED AS MARKED. M/D BS 1350-1370 LBL 116 FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: SHAFT — CORRODED (LT WING TE FLAPS) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 LT & RT WING T/E I/B AFT FLAP DRIVE GENEVA CAM ROLLER SHAFTS NR 3,5 & 6 PITTING CORROSION FOUND. ROLLER SHAFTS REPLACED IAW MM 27-51-39.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 CABIN - SHEAR TIE FOUND CRACK AT STA 1800 S-4R TO S-5R. SHEAR TIE REPLACED AS PER SRM 51-10-01.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 L3 DR CUTOUT FWD LOWER CORNER REVEAL CRACKED AS MARKED. L3 DR CUTOUT FWD LOWER CORNER REVEAL REPLACED AS PER AS PER SRM 51-10-01.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 R3 DR CUTOUT FWD LOWER CORNER REVEAL CRACKED AS MARKED. R3 DR CUTOUT FWD LOWER CORNER REVEAL REPLACED AS PER SRM 51-10-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 CABIN - SHEAR TIE FOUND CRACK AT STA 1920 S-4R TO S-5R. SHEAR TIE REPLACED AS PER SRM 51-10-01.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 CRACK REVEALED ON THE BOTTOM FORWARD CORNER VERTICAL BEAM OF DOOR 5L, DOOR 5L FWD CORNER VERTICAL BEAM REPAIRED AS PER SRM 52-10-02 FIG 10

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 CABIN - SHEAR TIE FOUND CRACK AT STA 1820 S-4R TO S-5R. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 CABIN SEAT TRACK I/B FLANGE FOUND CRACKED AT STN 996-997 RBL 33. SEAT TRACK REPAIRED PER SRM 53-10-05 FIG. 1A

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 U/D - BS 560-580 LBL 28 SEAT TRACK CORRODED. U/D BS 560-580 LBL 28 SEAT TRACK REPAIRED AS PER SRM 53-10-01 FIG.1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 U/D - BS 600-660 LBL 64 SEAT TRACK FLANGE CORRODED. SEAT TRACK REPAIR AT LBL 65 FROM BS 600-660 AS PER SRM 53-10-05 FIG 1A

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 UPPER DECK FLOORBEAM UPPER CHORD AT BS 380 LBL 32-36 FOUND TWO EACH , FLOOR PANEL ATTACHMENT HOLES CRACKED AS MARKED. REPAIRED FLOOR BEAM CRACKED HOLES PER SB 747-53A2431 FIG 7.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 UPPER DECK FLOORBEAM UPPER CHORD AT BS 380 RBL 32-36 FOUND PANEL ATTACHMENT HOLES CRACKED AS MARKED. REPAIRED FLOOR BEAM CRACKED HOLES AS PER SB 747-53A2431 FIG 9 .

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 U/D - BS 620-660 LBL 48 SEAT TRACK FLANGE CORRODED. U/D BS 620-660 LBL 48 SEAT TRACK REPAIRED AS PER SRM 53-10-01 FIG.1

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 U/D - BS 540 LBL 28 SEAT TRACK CROWN CORRODED. U/D BS 540 LBL 28 SEAT TRACK CROWN REPAIRED AS PER SRM 53-10-01 FIG.1

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 U/D - BS 660-680 LBL 28 SEAT TRACK CROWN AND FLANGE CORRODED. U/D BS 660-680 LBL 28 SEAT TRACK CROWN REPAIRED AS PER SRM 53-10-01 FIG.1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 U/D - BS 660 LBL 38 FLOORBEAM FOUND CORROSION. U/D BS 660 LBL 38 FLOORBEAM REPAIR AS PER SRM 53-10-01 FIG.1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 U/D - BS 710 LBL 28 SEAT TRACK FLANGE CORRODED. U/D BS 710 LBL 28 SEAT TRACK REPAIRED AS PER SRM 53-10-01 FIG.1.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 BULK CARGO COMPT - FLOOR PANEL SUPPORT LOWER SURFACE FOUND CORROSION AT FS LBL 30 AS MARKED. FLOOR PANEL SUPPORT REPAIRED AT BULK CARGO COMPT FX 1920- FS 1926 LBL 30 AS PER SRM 53-10-07 FIG 20.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 UPPER DECK FLOORBEAM UPPER CHORD AT BS 340 LBL 32 FOUND ONE EACH FLOOR PANEL ATTACHMENT HOLE CRACKED AS MARKED. REPAIRED CRACKED HOLES AS PER SB 747-53A2431 FIG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 U/D - BS 600-660 LBL 28 SEAT TRACK FLANGE CORRODED. U/D BS 600-660 LBL 28 SEAT TRACK FLANGE REPAIRED AS PER SRM 53-10-01 FIG.1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 U/D - BS 590 LBL 48 SEAT TRACK FLANGE CORRODED. U/D SEAT TRACK REPAIR AT LBL 48 BS 590 AS PER SRM 53-10-01 FIG.1.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 UPPER DECK FLOORBEAM UPPER CHORD AT BS 360 RBL 18-58 FOUND EIGHT FLOOR PANEL ATTACHMENT HOLES CRACKED AS MARKED. REPAIRED FLOORBEAM CRACKED HOLES PER SB 747-53A2431 FIG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 U/D - BS 580 - 600 LBL 48 SEAT TRACK FLANGE CORRODED. U/D BS 580-600 LBL 48 SEAT TRACK REPAIRED AS PER SRM 53-10-01 FIG.1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 U/D - BS 520-530 LBL 48 SEAT CROWN FOUND CORRODED. U/D SEAT TRACK REPAIR AT LBL 48 FROM BS 520- BS 530 AS PER SRM 53-10-01 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 COCKPIT LATERAL FLOORBEAM UPPER CHORD CORRODED AROUND FASTENER HOLES. U/D BS 420 LBL 11 TO LBL 30 FLOORBEAM REPAIR AS PER SRM 53-10-07 FIG.8

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 UPPER DECK FLOOR BEAM UPPER CHORD AT BS 360 LBL 24-54 FOUND FOUR FLOORBEAM PANEL ATTACHMENT HOLES CRACKED AS MARKED. REPAIRED CRACKED HOLES PER SB 747-53A2431 FIG 9. THE REPETITIVE INSPECTION TO BE FOLLWED BY UPS & TO BE BODIED IN 3000 FLT CYCLES PER EO B747-5320-12407-B (CUSTOMER HAD BEEN INFORMED).

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 UPPER DECK FLOORBEAM UPPER CHORD AT BS 340 RBL 44-55 FOUND THREE EACH FLOOR PANEL ATTACHMENT HOLES CRACKED AS MARKED. REPAIRED FLOORBEAM UPPER HCORD (AFT SIDE) CRACKED HOLES AS PER SB 747-53A2431 FIG.9.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 M/D - L5 DOOR FWD CUTOUT REVEAL FOUND CRACKED AT UPPER HINGE LOWER AREA. REPLACED L5 DOOR FWD CUTOUT REVEAL AS PER SRM 51-10-01 DOOR RIGGING & OPERATIONAL TEST DONE PER MM 52-11-01 FOUND SATIS.

Part: FITTING — CRACKED (PAX DOOR) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 M/D- L3 DOOR FWD CUTOUT NR 6 STOP FITTING FOUND CRACKED. REPLACED NR 6 DOOR STOP FITTING AS PER SRM 51-10-01; DOOR ADJUSTMENT & RIGGING AS PER MM 52-11-01 BE COMPLIED WITH FOUND SATIS.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 M/D - L2 DOOR FWD CUTOUT LOWER REVEAL FOUND CRACKED. L2 DOOR FWD CUTOUT LOWER REVEAL AND FRAME REPAIRED AS PER SRM 53-10-04 FIG.84.

Part: STRINGER — CRACKED (CABIN) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 CABIN - STRINGER END FOUND CRACK AT 1730 - 1731 STR-8L. STRINGER REPAIRED AS PER SRM 53-10-03 FIG.5

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 CABIN - SHEAR TIE FOUND CRACKED AT STN 2340 STR- 4R TO 5R. SHEAR TIE REPLACED PER SRM 51-10-01

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 CABIN - FRAME FOUND CRACKED AT STA 1416 BETWEEN STR 24L TO STR 25L. REPAIRED FRAME AS PER SRM 53-10-01 FIG 11.

Part: HINGE — CRACKED (PAX DOOR) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 M/D - L1 DOOR BODY T/T LOWER HINGE UPP BEARING SUPPORT FTG FOUND CRACKED AT BS 440 WL 178. REPLACED L1 DOOR HINGE BODY TORQUE TUBE LOWER HINGE FTG PER SRM 51-10-01 DOOR RIGGING & OPERATIONAL TEST DONE PER MM FOUND SATIS.

Part: FRAME — CRACKED (PAX WINDOW) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 FX - COCKPIT R3 WINDOW FRAME FOUND CRACKED AT AFT EDGE LOWER AREA. SKIN REPAIED AS PER SRM 53-30-03 FIG 49.

Part: FITTING — CRACKED (PAX DOOR) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 M/D- L3 DOOR FWD CUTOUT NR 2 STOP FTG FOUND CRACKED. REPLACED NR 2 STOP FITTING PER SRM 51-10-01 DOOR ADJUSTMENT & RIGGING PER MM BE COMPLIED WITH FOUND SATIS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE:C3 M/D - BS 140 BULKHEAD RING FOUND CRACKED AT STR 20R. M/D BS 140 BULKHEAD OUTER RING CHORD REPAIRED IAW UPS EO 747-5310-3079-D APPENDIX B FIG 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,103 hrs · 32,223 cycles

INSPECTION TYPE: C3 U/D - BS 670-690 LBL 65 SEAT TRACK LIPS CORRODED. SEAT TRACK REPAIR AT LBL 65 FROM BS 670-690 AS PER SRM 53-10-05 FIG 1A.

Part: ENGINE — FAILED (NR 4)

NR 4 ENGINE SHUTDOWN IN FLIGHT ON FINAL APPROACH HAD A COMPRESSOR STALL WITH DESCENT POWER ON WITH A IMMEDIATE RAPID RISE IN EGT. SHUTDOWN EGT SHOWS MAX 914. FELT COMPRESSOR STALL AND HEARD LOW RUMBLE AFTER THRUST LEVER RETARDED TO FLIGHT IDLE. REMOVED AND REPLACED NR 4 ENGINE PER B747 TC 50 00.

Part: STRUCTURE — CORRODED (BS 2160)

INSPECTION TYPE:N/A, 1 FT X 2 FT AREA OF CORROSION FOUND AT STATION 2160. *S/D* REMOVED CORRODED SKIN AND STRINGER DOUBLER. INSTALLED AND TREATED DOUBLER IAW SRM 53-30-03.

Part: WARNING SYST — MALFUNCTIONED (COCKPIT)

ON SEVERAL OCCASIONS INFLIGHT MASTER WARNING BRIEFLY FLASHED AND FIRE BELL BRIEFLY SOUNDED. ALL OTHER INDICATIONS NORMAL. FUNCTION TEST APU FIRE TEST OPS TEST NORMAL PER MM26-22-00.

Part: FIRE CARD — NOT SEATED (APU)

1.5 HRS INTO FLT THE APU FIRE WARNING LIGHT ILLUMINATED VERY DIMLY AND THE FIRE BELL SOUNDED, BUT SILENTLY FOR 10 SECONDS. THIS SITUATION DID NOT HAPPEN THE REST OF FLT. RESEATED THE A-5 AND A-8 CONTROL CARDS. APU FIRE TEST GOOD PER M/M 26-10-00.

Part: RIVET — POPPED (BELLY SKIN)

INSPECTION TYPE-N/A, SEVERAL RIVETS POPPED JUST FWD OF RT OUTFLOW VALVE ON BELLY SKIN. REPAIR COMP AS PER EO B747-5310-9815B.

Part: STRINGER — CORRODED (BS 2160)

INSPECTION TYPE-N/A, STR 46 RT CORRODED STA 2160 AT PRODUCTION SPLICE. REMOVED AND REPLACED CORE SECTION OF STRINGER IAW 53-10-03.

Part: FORMER RING — CORRODED (BS 2180)

INSPECTION TYPE-N/A, AFT FORMER RING CORRODED AT STA 2180 BETWEEN STR 46 AND 43R. REMOVED AND REPLACED CONFORMER RING IAW 51-10-00.

Part: DOUBLER — CRACKED (RT OUTFLOW VALVE)

INSPECTION TYPE-N/A, RT OUT FLOW VALVE, LOWER FWD, CORNER TANG OF INTERNAL DOUBLER HAS 2 EA SUSPECTED CRACKS. NDT REQ, FOUND 4 EA FASTENER HOLE CRACKED. USING NDT M-20 (M) REF LOGBOOK PAGE 000230 ITEM 1, INST REPAIR AS PER EO 747-5310-9815-B.

Part: SKIN — DAMAGED (BS 1975/1990)

INSPECTION TYPE-C, EXTERNAL FUSELAGE SKIN, PREVIOUS REWORK ON SKIN LAPSPLICE STR 46 BETWEEN BS 1975 TO 1990 IS OUT OF LIMITS ACC TO SRM 53-30-01 FIG 1. LAPSPLICE ON STR 46 BETWEEN BS 1975 AND 1990 LT REPAIRED ACC SRM 53-30-03 FIG 17.

Part: SKIN — CRACKED (BS 2035-2055)

INSPECTION TYPE-C, PREVIOUS REWORK ON SKIN LAP SPLICE STR 46 BETWEEN BS 2035 AND 2055 LT IS OUT OF LIMITS ACC SRM 53-30-01 FIG 1. SKIN LAP SPLICE ON STR 46 BETWEEN BS 2035 AND 2055 REPAIRED ACC SRM 53-30-03 FIG 17.

Part: SKIN — DAMAGED (BS 1855/1925)

INSPECTION TYPE-C, EXTERNAL FUSELAGE SKIN, PREVIOUS REWORK ON SKIN LAPSPLICE BETWEEN BS 1855 TO 1925 AT STR 46 LT IS OUT OF LIMITS ACC TO SRM 53-30-01 FIG 1. REPAIRED SKIN LAPSPLICE BETWEEN BS 1855 TO 1925 AT STR 46 LT IAW SRM 53-30-03 FIG 17.

Part: SPAR WEB — CRACKED (WS 453)

INSPECTION TYPE-C, MID-SPAR WEB INSPECTION, EO 747-5710-7893 FOUND CRACK IN WEB AT WS 453. CRACK IS APPROX 7 MM, STARTING AT FASTENER HOLE FROM SECOND ROW OF FASTENERS THAT ATTACH THE WEB TO THE UPPER CHORD. REPAIRED MID-SPAR WEB AT WS 453 ACC EO B747-5710-7893, APPNDIX C.

Part: HINGE ARM — CRACKED (PAX DOOR)

INSPECTION TYPE: C. M.E.D. 1-L LWR HINGE-ARM: FOUND SMALL CRACK ON FWD FRAME. REPAIRED CRACK AT M.E.D. 1L LWR HINGE-ARM CUTOUT IAW SRM 52-10-02 FIG 12.

Part: FRAME — CRACKED (BS 2200)

INSPECTION TYPE-C, AREA AFT OF BULK CARGO COMP DURING REPLACEMENT OF FILLER FOUND CRACK IN FRAME INNERFLANGE REINFORCEMENT ANGLE AT BS 2200, NEAR FRAME STIFFENER AT S-42 RT. REPLACED REINFORCEMENT ANGLE ACCORDING TO SRM 51-30-02.

Part: HANDLE PAN — CRACKED (PAX DOOR)

INSPECTION TYPE: C. FOUND AT MAIN ENTRY DOOR 1 LT, A CRACK IN THE PAN OF THE OUTSIDE DOOR HANDLE. REPLACED PAN OF THE OUTSIDE DOOR HANDLE 1 LT IAW SRM 51-30-02.

Part: SKIN — CORROSION (BS 1600-1740)

INSPECTION TYPE-C, EXTERNAL SKIN, FOUND BLEND OUT SPOTS AND CORROSION AROUND FASTENER HEADS FROM BS 1600 TO 1740 STR 42 TO 46 LT. SKIN PANEL REPAIRED IAW UPS APPROVAL ENGINEERING FILE NR 747-53-0792.

Part: SPAR WEB — CRACKED (NAC STA 193/196)

INSPECTION TYPE-C, CRACK IN LOWER SPAR WEB, NAC STA 193/196 LT, AT PNU DUCT SUPPORT STIFFENER. REPAIRED LOWER SPAR WEB AT NAC STA 193/196 LT ACC SRM 54-10-03 FIG 2.

Part: STIFFENER — CORRODED (BS 2200)

INSPECTION TYPE-C, AREA AFT OF BULK CARGO COMP FOUND CORROSION ON TOP OF FRAME STIFFENER BS 2200 NEAR S-42 RT, JUST IN FRONT OF RT OUTFLOW VALVE. CORROSION DAMAGE OUT OF LIMITS ACC TO SRM 53-10-01. REPLACED SAME STIFFENER ACC TO SRM 51-30-02.

Part: LIGHT — INOPERATIVE (CABIN)

MAINTENANCE REPORTED EMERGENCY LIGHT OUT IN CEILING INBOARD 5L DOOR. REMOVED AND REPLACED LIGHT ASSY. OPS NORMAL.

Part: BATTERY PACK — DISCHARGED (UPPER DECK)

MAINTENANCE REPORTED EMERGENCY AISLE EXIT LIGHT INOP UPPER DECK RT SIDE. REMOVED AND REPLACED BATT. PACK. OP CK GOOD.

Part: SENSOR — SHORTED (NR 4 PYLON)

CREW REPORTED, RT WING LE OVERHEAT LIGHT ILLUMINATED. RAN ALL ABNORMAL CHECKLISTS AND OVERHEAT LIGHT FAILED TO EXTINGUISH. LIGHT REMAINED ILLUMINATED FOR OVER TWO HRS AFTER ENG SHUTDOWN. FOUND SENSOR S1048 IN PYLON NR 4 SHORTED TO GND.

Part: SKIN — PUNCTURED (RT TE MIDFLAP)

WHILE ON GROUND, MAINTENANCE FOUND RT I/B MIDFLAP LOWER SURFACE HAS TWO HOLES AT 2 FEET AND 5 FEET FROM THE I/B, COVE LIP AREA. ACCOMPLISHED COMPOSITE REPAIR PER SRM 51-40-09.

Part: CORNER — CRACKED (RT TE MIDFLAP)

WHILE ON GROUND, MAINTENANCE FOUND RT I/B MIDFLAP COVE LIP OB CORNER CRACKED AND DELAMINATED. ACCOMPLISHED COMPOSITE REPAIR REF SRM 51-40-09.

Part: SPAR WEB — CRACKED (WING)

WHILE IN AMSTERDAM FOR C-CK, MAINT FOUND AT WING NR 2, 6 CRACKS AT THE FRONT SPAR WEB, BETWEEN THE INBD AND OUTBD UPPER LINK FITTING. REPAIRED IAW EO B747-5400-6500A.

Part: SPAR WEB — CRACKED (WING)

WHILE IN AMSTERDAM FOR C-CK, MAINT FOUND AT WING NR 3, 8 CRACKS AT THE FRONT SPAR WEB, BETWEEN THE INBD AND OUTBD UPPER LINK FITTING. REPAIRED IAW EO B747-5400-6500A.

Part: T-CHORD — CRACKED (TE FLAP)

WHILE IN AMSTERDAM FOR C-CK, MAINT FOUND RT OUTBD MIDFLAP ASSY UPPER REAR SPAR T-CHORD (P/N G5BCB532-4), IS CRACKED AND HAS LOCAL CORROSION. REPLACED IAW OHM 57-52-55.

Part: FRAME — CORRODED (BS 960)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON OUTER CHORD OF FAIRING FRAME AT BS 960, LBL 07. REPAIRED THE OUTER CHORD OF THE FAIRING FRAME IAW SRM 53-40-04.

Part: SKIN — DAMAGED (BS 560)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LOWER FUSELAGE EXTERNAL SKIN DAMAGED AT STA 560 LT SIDE STRINGER 43. REPAIRED IAW SRM 53-30-03.

Part: SKIN — DAMAGED (NR 4 PYLON)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND DAMAGE ON OUTER SKIN OF PYLON NR 4 AT STA 210. REPAIRED IAW SRM 54-30-03.

Part: SKIN — CRACKED (NR 4 PYLON)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON OUTER SKIN OF PYLON NR 4 OF ACCESS PANEL AT STA 195, LT. REPAIRED IAW SRM 54-30-03.

Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED, EMER CEILING LIGHT, UPPER DECK MOST AFT INOP ON TEST. REPLACED BATTERY PACK, OPS CK OK.

Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED, LT UPPER DECK AISLE EMER LIGHT INOP. REPLACED EMER LIGHT ASSY, OPS CK OK.

Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED, STAIRWELL EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPS CHECK OK.

Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED, THE TWO EMER LIGHTS ABOVE UPPER DECK CREW EMER DOOR EXIT INOP. REPLACED BATTERY PACK.

Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED, EMER EXIT SIGN ABOVE CREW EMER DOOR EXIT LIGHTS INOP. REPLACED BATTERY PACK, OPS CHECK OK.

Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)

MAINTENANCE REPORTED, UPPER DECK CREW EMER EXIT DOOR SILL/SLIDE LIGHTS (2 EA) INOP. REPLACED BATTERY PACK, OPS CHECK OK.

Part: EEL — INOPERATIVE (CABIN)

MAINTENANCE REPORTED EMER EXIT LIGHTS INOP, BY FWD ENTRY DOOR AND AFT ENTRY DOOR 2 EA.

Part: EEL — INOP (FLIGHT DECK)

MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS (INCANDESCENT LIGHTS) UNDER THE INST GLARESHIELD ARE BURNED OUT: CAPTAIN'S SIDE 2ND FROM LEFT, CENTER 2ND FROM LEFT, F/U SIDE LEFT MOST BULB. REPLACED BULBS. OPS CHECK GOOD.