N674UP

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A UPPER DECK CREW SERVICE DOOR EMERGENCY LIGHT WILL NOT TEST. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP AT CREW ESCAPE DOOR. REMOVED BATTERY POWER SUPPLY IAW AMM 33-51-04 RED A729592 TLS 86245. REINSTALLED SAME POWER SUPPLY MODULE IAW B747 MM 33-51-04. RELAMPED LIGHTED EXIT SIGN IAW B747 MM 33-51-02, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTS EXIT SIGN OVER CREW SERVICE DOOR INOP. REMOVED BATTERY POWER SUPPLY IAW MM 33-51-04. REINSTALLED SAME POWER SUPPLY MODULE IAW B747 MM 33-51-04. RELAMPED LIGHTED EXIT SIGN IAW B747 MM 33-51-02, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A CREW SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED CREW SERVICE DOOR LIGHT ASSY IAW B747 MM 33-51-07, OPS CHECKS GOOD.

Part: MODULE — DEFECTIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS COME ON WITH SWITCH IS OFF-POSITION. REPLACED EMERGENCY LIGHT MODULE AS PER MM 33-51-09. TEST OK AS PER MM 33-51-00. OK TO CONTINUE P/N ON, OFF 69B46010-24, S/N ON 001415 OFF-00 329.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C, FWD CARGO COMPT TIE DOWN TRACK FOUND CRACKED AT LBL 25 BS 560 - 570 AREA AS MARKED. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 5.

Part: SKIN — CORRODED (RT WING) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C, RHW FUEL TANK ACCESS PNL 652AB CUTOUT FOUND CORRODED. RHW FUEL TANK ACCESS PNL 652AB CUTOUT SKIN CORROSION REMOVED NDT CRACK CHECK CARRIED OUT, NIL CRACK, SHOT PEEN CARRIED OUT AS PER RS R57-26-34665.

Part: SKIN — CRACKED (L1 DOOR) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - L1 DR EXTERIOR SURFACE FOUND CRACKED AT APPROX BS 460 WL 220. SKIN REPAIRED AS PER SRM 52-10-02 FIG 9.

Part: RIB — CRACKED (RT WING) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C RHW NR 3 FUEL TANK WS 557.42 WING INTERSPAR RIB WEB CRACK. REPAIR C/OUT AS PER SRM 57-10-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D BS 380 STR 24R FRAME WEB FOUND CRACKED. M/D BS 380 STR 24R FRAME WEB REPAIRED AS PER RS R53-12-34662.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C FX - RT BODY FAIRING SUPPORT FOUND CORRODED AT BS 880 BL 0 - RBL 45. RT BODY FAIRING SUPPORT AT BS 880 BETWEEN BL 0 - RBL 45 REPAIRED PER SRM 53-50-04 FIG 2.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C FX - BODY FAIRING SUPPORT FOUND CORRODED AT BS 880 BL 0 - LBL 45. LT BODY FAIRING SUPPORT STA 880 BETWEEN LBL 30 - LBL 50 REPAIRED PER SRM 53-50-05 FIG 2.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1780 RBL 97 SEAT TRACK FOUND CRACK. M/D BS 1750 - 1950 RBL 98 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1893 - 1896 RBL 97 SEAT TRACK FLANGE FOUND CRACKED. M/D - BS 1750 - 1950 RBL 98 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIGURE 1. WORK DETAILS REF NRC 6282 CWS 326457, 334309 SRWS 918557.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 2180 - 2220 S2R STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1740 RBL 11 SEAT TRACK FLANGE CRACKED. M/D BS 1730 - 1790 RBL 11 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1960 - 1980 S2L STRINGER END FOUND CRACKED. M/D BS 1960 - 1980 STR 2L REPAIRED AS PER SRM 53-10-03 FIGURE 4.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C, M/D - BS 1562 - 1564 RBL 97 SEAT TRACK FOUND CRACKED. M/D BS 1550 - 1630 RBL 98 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIGURE 1.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1880 RBL 97 SEAT TRACK FOUND CRACKED. M/D BS 1750 - 1950 RBL 98 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIGURE 1. WORK DETAILS REF NRC 6282 CWS 326457, 334309 SRWS 918557.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C, M/D - BS 1800 RBL 97 SEAT TRACK FOUND CRACK. M/D BS 1750 - 1950 RBL 98 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIGURE 1. WORK DETAILS REF NRC 6282 CWS 326457, 334309.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C, M/D - BS 2170 LBL 11 O/B SEAT TRACK FLANGE CRACKED. M/D BS 2150 - 2190 LBL 11 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIGURE 14.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1598 - 1600 RBL 97 SEAT TRACK FOUND CRACKED. M/D BS 1550 - 1630 RBL 98 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIGURE 1 WORK DETAIL REF NRC 6286 CWS 303296 SRWS 918522.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1818 RBL 97 SEAT TRACK FOUND CRACK. M/D - BS 1750 - 1950 RBL 98 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIGURE 1. WORK DETAILS REF NRC 6282 CWS 326457, 334309.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1880 RT BETWEEN STR 13 - 14 FOUND SHEAR TIE CRACK. M/D BS 1880 STR 13R - 14R SHEAR TIE REPLACED AS PER SRM 51-10-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1990 RT STR 13 STRINGER CRACKED. HFEC INSPECTION C/OUT AS PER NTM PART 6 51-00-00 FIG 4 NIL CRACK FOUND.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 2160 - 2180 S2R STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1960 S12R STRINGER SPLICE FOUND CRACKED. STRINGER SPLICE REPLACED AS PER SRM 51-10-01 PG 8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 2260 RBL 22 FLOORBEAM CORROSION FOUND. M/D FLOORBEAM AT BS 2260 LBL 5 - RBL 48 REPAIRED PER SRM 51-40-04 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 2040 LBL 11 - RBL 11 FLOORBEAM FOUND CORRODED. M/D FLOORBEAM AT BS 2040 LBL 2 - RBL 11.33 REPAIRED PER SRM 51-40-04 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 2340 RBL 40 HAT SECTION FOUND CORRODED. M/D BS 2340 RBL 40 HAT SECTION REPLACED PER SRM 51-10-01 PG 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1904 TO 1910 RBL 97 SEAT TRACK FLANGE FOUND CORRODED. M/D BS 1750 - 1950 RBL 98 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1. REF NRC 6282 CWS 326457, 334309.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1580 LBL 85 FLOORBEAM CORROSION FOUND. M/D FLOORBEAM AT BS 1580 LBL 68 - LBL 123 REPAIRED PER SRM 51-40-04 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1603 TO 1610 RBL 97 SEAT TRACK FLANGE FOUND CORROSION. M/D BS 1550 - 1630 RBL 98 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIGURE 1. REF NRC 6286.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1580 LBL 114 FLOOR SUPPORT CORROSION FOUND. M/D BS 1580 LBL 114 FLOOR SUPPORT REPAIRED PER SRM 51-40-03 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C, M/D - BS 2010 RBL 11 SEAT TRACK O/B FLANGE CORROSION FOUND. BS 1970 TO 2050 RBL 11 SEAT TRACK REPLACEMENT PER SRM 51-10-01 PG 8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 1720 RBL 81 TO 95 FLOORBEAM UPPER CHORD UPPER AND LOWER SURFACE FOUND CORROSION. M/D FLOORBEAM AT BS 1720 RBL 68 - 120 REPAIRED PER SRM 51-40-04 FIG 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - BS 2120 - 2150 RBL106 FLOOR SUPPORT CORROSION FOUND. M/D BS 2140 - 2150 RBL106 FLOOR SUPPORT REPAIRED PER SRM 51-40-03 FIG 1.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C, NOSE W/W TOP PNL WEB FOUND CRACKED AT STA 285 - 290 RBL 10 BWL 190 UPPER SURFACE. NOSE W/W TOP PANEL STA 285 - 290 RBL 10 BWL 190 CRACKED WEB REPAIRED AS PER RS R53-18-34659.

Part: CLIP — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C, LT BS 320 NOSE WHEEL WELL VERTICAL BEAM CLIP FOUND CRACKED AT NR 1 COUNT FROM TOP AS MARKED. LT BS 320 NOSE W/W VERTICAL BEAM NR 1 CRACKED CLIP REPLACED AS PER SRM 51-10-01 AND EO B747-5310-0574 APPROX D.

Part: SKIN — CHAFED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C FX EXTERIOR SKIN FOUND CHAFING MARK AT S40R BS 1920 AREA. FX EXTERIOR SKIN AT BS 1920 STR 40R REPAIR AS PER SRM 53-30-03 FIGURE 17. WORK DETAIL REFER CWS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C, NOSE W/W BS 400 BHD PRESSURE PAN FOUND 2 CRACKS BY APPROX 1 X .5 INCH LONG AS MARKED. NOSE W/W BS 400 BULKHEAD PRESSURE PAN REPLACED AS PER DWG 624U0005 SHEET 7.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C, FWD CARGO STA 1000 RBL 60 CABIN FLOOR SUPPORT FOUND CRACKED. FWD CARGO STA 1000 RBL 60 CABIN FLOOR SUPPORT REPLACED AS PER SRM 51-10-01.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C, M/D - L5 DOOR FWD CUTOUT BETWEEN STR 24 & 25 CRACKED. REPAIRED AS PER SRM 53-10-04 FIG 34.

Part: STOP FITTING — CRACKED (L1 DOOR) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - L1 DOOR FWD LOWER STOP FITTING CRACK. STOP FITTING REPLACED AS PER SRM 51-10-01 PAGE 8. DOOR RIG AND OPERATION CHECK C/OUT SATISFACTORY.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C CRACK REVEALED AT LT NR 1 MED CUTOUT FRAME AT BS 434 FRAME WEB AREA AT NR 5 FASTENER HOLE BY APPROX .5 INCH LONG IAW ATTACH FIGURE. LT NR 1 MED CUTOUT FWD FRAME BS 434 WEB REPAIRED AS PER EO B747-5310-12889-A APPROX F.

Part: FASTENER — CRACKED (NR 4 PYLON) · airframe 74,753 hrs · 20,928 cycles

INSPECTION TYPE:C NR 4 PYLON ATTACH FITTING TAPER LOCK FASTENER FOUND 4EA CRACKED. REF ATTACHED SKETCH. LOCKS REPLACED AS PER EO 747-5740-12227-A.

Part: FIRE LOOP — INOPERATIVE (NR 4 ENGINE)

INSPECTION TYPE:N/A PREFLIGHT NR 4 ENGINE FIRE WARNING FAILED TO TEST WHEN MOVING TEST SWITCH TO UPPER POSITION NR 4 ENG NACELLE IND AND FIRE HANDLE INOP AND WHEN TO DOWN POSITION ONLY NR 1 FIRE HANDLE TESTS REPAIRED BROKEN TERMINAL ENDS ON LOWER NR 4 FWD FIRE LOOP REF WDM 26-11-04 ENG FIRE DETECTION SYS OPS CKS GOOD IAW M/M 26-11-04

Part: FIRE LOOP — INOPERATIVE (NR 4 ENGINE)

NR 4 FIRE LOOP INOP. REPLACED NR 4 ENG LOWER FWD SENSING ELEMENT AND OPS CHECK NORMAL PER M M 26-11-02 THIS CLEARS M212481

Part: CONNECTOR — DISCONNECTED (NR1 ENG FIREWALL)

INSPECTION TYPE:N/A DURING CLIMB TO FL300 NR 1 GEN TRIPPED NR 1 FIELD TRIPPED.CSD NR 1 ENG ABOVE REDLINE/180C IND. RAN CKLIST & DISCONNECTED CSD ATTEMPTED. CSD DISCONNECT NOT EFFECTIVE. CSD RPM0 & CSD PMG BETWEEN 75 AND 100. NR 1 ENG PRECAUTIONARY SHUTDOWN. CHECKED AND FOUND ELECTRICAL CONNECTOR D11P WAS DISCONECTED AT NR1 ENG HORIZONTAL FIREWALL. CLEANED AND INSTALLED CONNECTOR, PERFORMED OPS CK''D CSD DISCONNECT FUNCTION NORMAL. RECONNECTED CSD & NR 1 GEN OP''S NORMAL. OK FOR SERVICE. PERFORMED NR 1 ENG WINDMILLING INSPECTION NO CONTAMINATION NOTED AT FILTER & MAG TIP. OK TO OPERATE NR 1 ENG.

Part: CONNECTOR — FAULTY (NR1 ENGINE)

INSPECTION TYPE:N/A BTB- REJECTED T/O, NR 1 ENGINE FIRE WARNING. T/S FOUND UPPER AFT LOOP CONNECTORS BAD DEFERRED OK FOR SERVICE REF WIRING DIA 26-11-51.

Part: WARNING SYSTEM — ILLUMINATED (RT WING)

INSPECTION TYPE: ATB, RT WING OVERHEAT LIGHT ILLUM. REPAIRED WIRING.

Part: WARNING LIGHT — ILLUMINATED (RT WING OVERHEAT)

INSPECTION TYPE:C, RT WING OVERHEAT LIGHT ILLUMINATED.

Part: SUPPORT FITTING — CRACKED (NR 8 SPOILER) · airframe 71,893 hrs · 20,313 cycles

INSPECTION TYPE:S D-191245, NR 8 SPOILER SUPPORT FITTING WEB CRACKED. REMOVED AND REPLACED FITTING PER MM 27-61-01, 27-61-04, SRM 51-30-02 AND EO NR 747-57-0491.

Part: FITTING — CRACKED (WS 586)

INSPECTION TYPE:C 44, RT WING NR 3 MAIN FUEL TANK WS 586 REAR SPAR FITTING WAS CRACKED IN UPPER RADIUS. REPAIRED IAW EO B747-5720-10909 REF QUERY NOTE 12/2000, EFN 747-53-1095 AND ATTACHED 8110-3 NOTE, THIS IS A TIME LIMITED REPAIR, PERMANENT REPAIR WITHIN 18 MONTHS.

Part: SPLICE PLATE — CRACKED (BS 400)

INSPECTION TYPE:C 44, BS 400, STR 44 AREA LEFT AND RIGHT IN NOSE LANDING GEAR BAY, THE SPLICE PLATES AT BOTH LEFT AND RIGHT AFT CORNERS WERE CRACKED. REPAIR ACCOMPLISHED PER EO B747-5330-3520-D, SECTION 5, APPENDIX B. INSTALLED SKIN AND SPLICE STRAP DOUBLERS PER DRG 141U1099. CRACKED SPLICE PLATES REPLACED.

Part: FLOORBEAM — CORRODED (BS1040 - 1050)

INSPECTION TYPE:C 44, CORROSION ON LOWER CHORD FOR LONGITUDINAL FLOORBEAM WEB AT BS 1040 TO 1050, RBL 98. REPAIR ACCOMPLISHED IAW QUERY NOTE 21/2000 AND APPROVED 8110-3. REF EFN 747-57-0481.

Part: SKIN — CORRODED (BS 1140)

INSPECTION TYPE:C 44 MAIN DECK, CORROSION ON UPPER SURFACE OF CENTRE WING AT BS 1140 RBL 25. REMOVED CORROSION - EVALUATE AND REPROTECT. CORROSION REMOVED IAW SRM 51-10-01 AND REPROTECTED IAW 51-10-02. CORROSION DEPTH 0.004.

Part: RIB — CRACKED (VERTICAL STAB)

INSPECTION TYPE:C 44.TAIL.RIGHT HAND OUTBOARD ELEVATOR BALANCE WEIGHT SUPPORTS CRACKED AT STATIONS 261,285 AND 295.REPAIR SUPPORT STRUCTURE PER SRM. NEW SUPPORTS FABRICATED AND FITTED I.A.W SRM 51-10-01 AND 51-30-02.

Part: RIB — CRACKED (ELEVATOR)

INSPECTION TYPE:C 44, TAIL, LEFT INBOARD ELEVATOR UPPER RIB CRACKED AT STA 82. REPAIR AS PER SRM. RIB REPLACED IAW 51-30-02 AND 51-10-01.

Part: ANGLE — CRACKED (BS 260)

INSPECTION TYPE:C UNDER FLOOR ABOVE NOSE WHEEL WELL AT BS 260 AND 10 INCHES UNDER MAIN DECK FLOOR FOUND THREE ANGLES CRACKED AT RBL10, BL 0 AND LBL10 AS INDICATED. NEED TO REPLACE ALL THREE ANGLES IAW SRM 51-30-02. REF NON - ROUTINE 44230369. THREE ANGLES FABRICATED AND FITTED IAW SRM 51-30-02 AND 51-10-01.

Part: ANGLE — CRACKED (BS 260)

INSPECTION TYPE:C 44, UNDERFLOOR ABOVE NOSE WHEEL AT BS 260 AND 10 UNDER MAIN DECK FLOOR -3 ANGLES CRACKED AT RBL 10, BLO AND LBL 10 AS INDICATED. NEED TO REPLACE ALL THREE ANGLES IAW SRM 51-30-02, 3 ANGLES FABRICATED AND FITTED IAW SRM 51-30-02 AND 51-10-01 P/N BACB30FM6-3.

Part: SPLICE — CRACKING (BS 1480)

INSPECTION TYPE:C 44, ALSO REF 44229476, 44229857,44230096, 44230104, 44233476, 44234716 AND 44234895. REF EO 5310-10732A. REWORK RT BS 1480 HOLES AND SPLICE PLATES TO S/B B747543A2390 PLAN B. WORK ACCOMPLISHED IAW S/B 53A2390 AND Q/NOTE 16/2000 AND APPROVED 8 110-3. NOTE, FAA APPROVAL FOR THIS INSPECTION WILL BE REQUIRED.

Part: FRAME — CRACKED (BS 360)

INSPECTION TYPE:C 44, FUSELAGE FRAME WAS CRACKED AT BS 360 LHS, BETWEEN STRINGERS 24L AND 25L. REPAIR ACCOMPLISHED IAW QUERY NOTE 18/2000 AND APPROVED 8110-3. ALSO REF EFN 747-53-1098.

Part: FITTING — CRACKED (WS 586)

INSPECTION TYPE:C 44, LEFT HAND WING NR 2 MAIN FUEL TANK WS 586 REAR SPAR FITTING HAD A 2 INCH CRACK APPROX AT UPPER RADIUS. REPAIR PER QUERY NOTE 2/200 0 REPLY. ACCOMPLISHED TEMPORARY REPAIR IAW EO B747-5720-10909 AAENDUM TO UPS SRM. NOTE REPAIR MUST BE REPLACED WITH PERMANENT REPAIR WITHIN 18 MONTHS. PERMANENT REPAIR IS FITTING REPLACEMENT.

Part: BULKHEAD — CORRODED (BS 1241)

INSPECTION TYPE:C 44, SURFACE CORROSION IN LT WLG W/WELL AT BS 1241, BEHIND SPOILER MIXER. REMOVE, EVALUATE AND REPROTECT. CORROSION ON CANTED BULKHEAD AT STA 1241, RBL 5 TO 10. 2. WIDE SPREAD CORROSION ON CANTED BULKHEAD AT STA 1241, RBL 0-50. CORROSION REMOVED AND WAS FOUND TO BE OUT SIDE LIMITS IAW 51-10-01. QUERY NOTE 19/2000 ADDRESSES THIS REPAIR AND ATTACHING 8110-3. PREVIOUS REPAIR REMOVED/DOUBLERS AND TRIPLERS WERE INSTALLED/NEW SECTION OF CHORD WAS SPLICED IN AT THIS LOC AT THE RHS. Q/NOTE 20/2000, NEW WEB WAS FITTED AND DOUBLER INSTALLED LHS.

Part: DOOR FRAME — CRACKED (PAX DOOR)

INSPECTION TYPE:C 44, CRACK ON FORWARD FRAME BENEATH OUTER SKIN 6 INCHES LONG. HORIZON TAL MEMBER ALSO CRACKED AT NR 2 LEFT HAND DOOR. DOOR REMOVED TO WORK SHOP FOR REPAIR PER MM 52-10-20. REPAIR ACCOMPLISHED PER QUERY NOTE 1/2000. REPAIRED ANGLE PER SRM 52-10-02, FIG 10. HORIZONTAL MEMBER REPAIRED PER SRM 52-10-02, FIG 10.

Part: BULKHEAD — CORRODED (BS 1241)

INSPECTION TYPE:C 44, THERE WAS CORROSION ON THE CANTED BULKHEAD AT STA 1241, RBL 5 TO 10 ADJACENT REPAIR LOCATED AT THE SITE. REPAIR ACCOMPLISHED PER QUERY NOTE 19/2000 AND APPROVED 8110-3 REF N 747-53-1097.

Part: WINDOW BELT — CORRODED (BS 960 - 980)

INSPECTION TYPE:C 44, WINDOW FORGING STA 960-980 RIGHT HAND SIDE HAD EVIDENCE OF CORROSION BETWEEN FORGING AND OUTER SKIN. REMOVED FORGING FOR INVESTIGATION. REPAIRED PER QUERY NOTE 3/2000 ALSO REF 747-53-1093.

Part: WINDOW BELT — CORRODED (BS 920 - 940)

INSPECTION TYPE:C 44, WINDOW FORGING STA 920 - 940 HAD EVIDENCE OF CORROSION BETWEEN FORGING AND OUTER SKIN. REPAIR ACCOMPLISHED PER QUERY NOTE 5/2000 REF EFN 747-53-1091.

Part: WINDOW BELT — CORRODED (BS 900 - 920)

INSPECTION TYPE:C 44, WINDOW FORGING STA 900 - 920 RHS HAD EVIDENCE OF CORROSION BETWEEN FORGING AND OUTER SKIN. REMOVE FORGING FOR INVESTIGATION REF QUERY NOTE 06/2000. REPAIRED IAW QUERY NOTE 06/2000. ALSO REF UPS ENGINEERING FILE NUMBER 747-53-1090.

Part: WINDOW BELT — CORRODED (BS 920 - 940)

INSPECTION TYPE:C 44, WINDOW FORGING STA 920 - 940 LHS HAS EVIDENCE OF CORROSION BETWEEN FORGING AND OUTER SKIN. REMOVE FORGING TO INVESTIGATE. REFERENCE QUERY NOTE 4/2000 FOR REPAIR INSTRUCTIONS REF EFN 747-53-1 093.

Part: BRACKET — DAMAGED (BS 960)

INSPECTION TYPE:C 44, SUPPORT BRACKET FOR CTR GUIDE FOUND DAMAGED AT BS 960, BL0. NEW SUPPORT BRACKETS FABRICATED AND INSTALLED IAW SRM 51-20-01, AND 51-30-02.

Part: FRAME — DAMAGED (FUSELAGE)

FRAME DAMAGED AT PANEL 192, SUPPLEMENTAL MRR, TRANSFERRED TO C CHECK VISIT 1006 FLS AEROSPACE DUBLIN NRC 017.

Part: COMPUTER — INOP (AUTOPILOT)

INSPECTION TYPE:N/A, IN CRUISE AFTER AN ATC REQUIRED SPEED REDUCTION, B AUTOPILOT ABRUPTLY PITCHED A/C NOSE UP (ADDITIONAL 2.5 - 3 DEGREES. F/O PUSHED OVER BUT COULD NOT PREVENT AN ALTITUDE DEVIATION OF 300 FT NEITHER A/P OR ALTITUDE HOLD DISENGAGED AUTOMATICALLY. SUBSEQUENT A A/P OPS NORMAL. B A/P DISCREPANCY RECURRED WHEN RE-ENGAGED. *S/D* REMOVED AND REPLACED B SYSTEM PITCH COMPUTER PER MM 22-12-01, PERFORMED OPS CHECK AND AUTOPILOT CHECKS NORMAL.

Part: CONTROLLER — INOP (COCKPIT)

ATB - CREW REPORTED STRONG ACRID SMELL IN COCKPIT, COULD NOT LOCATE SMELL. CREW USED O2, RETURNED TO HKG. FOUND LEFT UPPPER DECK HEATER TEMP CONTROL AT FAULT. REMOVED AND REPLACED LEFT CONTROLLER.

Part: HEAT SYSTEM — INOP (CARGO COMMPT)

COMPUTER SHOWS FIRE WARNING, AFT CARGO HEAT SYSTEM WILL NOT TEST DI M1 76126. AFT CARGO HEAT SYSTEM WILL NOT TEST. CHECKED WIRING TO VALVES AND CHECK EXTENSION OVRD VALVES ACTUATOR AND OPS CHECKED GOOD MM 21-44-00.

Part: CONNECTOR — LOOSE (NR 4 CROSSFEED)

NR 4 FUEL CROSSFEED VALVE FAILED, CLOSED INFLIGHT. AIR TURNBACK TO ANC. LOCATED NR 4 FUEL CROSSFEED VALVE AND FOUND CANNON PLUG OFF OF ACTUATOR. INSTALLED SYSTEM WITH PRESSURE ON, NO LEAKAGE NOTED.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY LIGHT OUT MAIN DECK STA 600 RT. NO EMERGENCY LIGHTING SYSTEM INSTALLED THIS POSITION.

Part: SKIN — DAMAGED (AFT FUSELAGE)

INSPECTION TYPE-N/A, UPON ARRIVAL FOUND SKIN DAMAGE AND PUNCTURED I/B OF TAIL STAND BAIL FITTING PUNCTURE IS APPROXIMATELY 2 INCH LENGTH. TRANSFERRED TO L/P 319551 ITEM 1. REPAIRED DAMAGED SKIN AS PER EO B747-5330-10025A. CLOSED OUT NON-ROUTINE CARDS.

Part: SEAT TRACK — DAMAGED (NR 1 PIT)

INSPECTION TYPE-N/A, FWD LOWER PIT NR 1 POS SEAT TRACK DAMAGED. REMOVED OLD SECTION OF SEAT TRACK. INSTALLED NEW SECTION OF SEAT TRACK FWD LWR PIT NR 1 POS, REF M/M 51-00.

Part: AIR DISTR — ODOR (FLIGHT DECK)

STRONG FUEL ODOR ON FLIGHT DECK STARTING AT ROTATION AND INITIAL CLIMB ODOR DISSIPATED AFTER PACKS TURNED ON REPEAT WRITE UP SEE PAGE 992546. INSPECTED BEFORE, DURING AND AFTER FUELING E/E COMPARTMENT WING TO BODY FAIRINGS AIR CONDITIONING PACK BAYS NO FUEL SEAPS OR LEAKAGE NOTED. SUBMITTER STATES, SUSPECT ODOR FROM PREVIOUS MAINT.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE-N/A, STAIRWAY TO COCKPIT EMERGENCY LIGHTS INOP. REPAIRED WIRING TO LIGHT ASSY AND REPLACED LIGHT ASSY, (P/N SR356 B37) (S/N 11239-473) OFF, (S/N 143-10) ON, OPERATION NORMAL.

Part: POWER SUPPLY — INOPERATIVE (MAIN DECK)

INSPECTION TYPE-N/A, AFT EMERGENCY CEILING LIGHT ON MAIN CARGO AT ENTRANCE DOOR IS INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: PANEL — CRACKED (RT WING)

INSPECTION TYPE:N/A, UPPER RIGHT WING PANEL CRACKED FWD OF RT WING GEAR VISIBLE FROM UNDER WING. INTERIM REPAIR ACCOMPLISHED PER EO B747-5730-9327 D 131645.

Part: STRINGER — CORRODED (BS 818)

INSPECTION TYPE:C, FOUND STRINGER CORRODED ON BS 818 STR 46R. REPAIRED STRINGER ACC DFX 97-058 REV.2 DETAIL -1 AND DETAIL -2.

Part: STRINGER — CORRODED (BS 980-985)

INSPECTION TYPE-C, FOUND DURING INSPECTION STRINGER CORRODED FROM BS 980 TO 985 TR.46R CORROSION EXCEED LIMITATIONS ACC SRM53-10-01. REPAIRED STRINGER ACC DFX 97-058 REV 2 DETAIL 3 ENGINEERING FILE NUMBER 747-53-0818.

Part: TEE CHORD — CORRODED (BS 860)

INSPECTION TYPE-C, FWD CARGO COMPARTMENT FOUND ON FRAME BS 860 RBL 10 UPPER T-CHORD CORRODED AROUND ATTACHMENT HOLE. REPAIRED T-CHORD ACC DFX 97-075 ENGINEERING FILE NUMBER 747-53-0622.

Part: WEB — CRACKED (BS 1860/1910)

INSPECTION TYPE-C, FOUND CORROSION ON LOWER SIDE AND CRACKS ON UPPER SIDE OF CENTER BEAM WEBPLATE AT RBL/LBL 6 BETWEEN BS 1860/1910. LT UPPER CHORD AND WEB BETWEEN BS 1860 AND BS 1910 TRANSVERSE STIFFENER AT BS 1875, TWO WEB DOUBLERS AND CENTER GUIDE SUPPORT BRACKET AT BS 1864 REPLACED ACC DRAWING 65B06205 SHT 6 IN ACCORDANCE WITH SRM 51-30-05/02.

Part: STRINGER — CRACKED (BS 1730-1740)

INSPECTION TYPE:C, FOUND CRACK IN LOWER SIDE OF STRINGER, FROM SPLICE AT BS 1740 TO BS 1730 IN S-42LH. REMOVED DAMAGED SECTION OF STRINGER AND REPAIRED STRINGER ACC KLM DFX 97-062 REV 2 REPAIR APPROVED PER EFN 747-53-0823.

Part: SKIN — WORN (NR 4 PYLON)

INSPECTION TYPE-C, FOUND INNER SKIN WORN BY LATCHS AT ACCESS PANEL CUT OUT NAC STA 177 UPPER AND LOWER SIDE. REPAIRED INNER SKIN ON LATCH POSITIONS ACC KLM DFX 97-055 REV NR 1 APPROVAL EFN 747-54-0153.

Part: CHANNEL — CRACKED (BS 1683)

INSPECTION TYPE-C, FOUND CRACKS IN LOWER CHANNEL FOR CENTER GUIDE ATTACHMENT AT BS 1683, BL 0. LOGITUDINAL SUPPORT STIFFENER REPLACED ACC TELEFAX NO8817-6199 MARCH 04 1997 IN ACCORDANCE WITH DRAWING 65B09113-10, 32 SECTION OF TOP SKIN REPLACED ACC SRM 51-30-05/02.

Part: FLOORBEAM — CRACKED (BS 400)

INSPECTION TYPE-C, UPPER DECK FLOOR STRUCTURE FOUND LONGITUDINAL CHORD ON FLOORBEAM CRACKED DURING FLOOR PANEL INSTALLATION AT BS 400 RBL 75. REPAIRED T-CHORD FROM BS 400 TO 410 ACC SRM 53-10-04 FIG 76.

Part: FRAME — DENTED (BS 1820)

INSPECTION TYPE-C, FOUND DENT AT FRAME BS 1820 STR 16 RT DURING EO B747-5330-0843E. REPLACED FRAME FROM STR 17 TO STR 13 RT AT BS 1820 ACC SRM 51-40-03 FIG 2 AND SRM 51-30-02.

Part: FRAME — DENTED (BS 2040)

INSPECTION TYPE-C, FOUND DENT AT FRAME BS 2040 STR 16 RT DURING EO B747-5330-084E. FRAME AT BS 2040 BETWEEN STR 16 AND STR 17 REPAIRED ACCORDING SRM 53-10-04 FIG 87.

Part: FRAME — DENTED (BS 1780)

INSPECTION TYPE-C, FOUND DENT DURING EO B747-5330-0843E AT FRAME BS 1780 STR 19 RT. REPAIRED FRAME AT BS 1780 AT STR 19 RT ACC SRM 53-10-04 FIG 87.

Part: FRAME — CORROSION (BS 1600)

INSPECTION TYPE-C, AFT CARGO COMPARTMENT FOUND CORROSION ON LOWER AND UPPER SIDE OF FRAME UPPER CHORD AT BS 1600, RBL 36/44 AND LBL 36. REMOVED CORROSION ACC SRM 51-10-01, WITHIN LIMITS OF SRM 53-30-01 AT RBL 36/44. OUT OF LIMITS AT LBL 36 AND REPAIRED UPPER CHORD ACC SRM 51-40-04 FIG 2.

Part: SKIN — CORROSION (BS 1960-2080)

INSPECTION TYPE-C, FOUND CORROSION AT LAP JOINT FROM BS 1960 TO BS 2080 STR 12 RT. CORROSION AT STR 12 LAP JOINT BS 1960 BS 2080 REMOVED ACC SRM 51-10-01, WITHIN LIMITS ACC SRM 53-30-01. DELAMINATED LAP SPLICE REPAIRED ACC TO BS 2180 STR 12 RT.

Part: SKIN — CORROSION (BS 1880-1940)

INSPECTION TYPE-C, INTERNAL FUSELAGE FOUND CORROSION AT LAP JOINT FROM BS 1880 TO BS 1940 RT STR 4. REMOVED CORROSION FROM BS 1860 TO BS 1940 ACC TO SRM 51-10-01 WITHIN LIMITS ACC SRM 53-30-01. DELAMINATED LAP SPLICE REPAIRED ACC TO SRM 53-30-03 FIG 10 FROM BS 1860 TO BS 1940 STR 4 RT.

Part: DOUBLER — MISINSTALLED (NR 3 PYLON)

INSPECTION TYPE-C, PYLON 3 FOUND DURING SB54-2034R4 MODIFICATION THAT ALREADY DOUBLER WAS INSTALLED. ONLY DOUBLER IS NOT ACCORDING SB INSTALLED DOUBLER ON LT SIDE ACC, KLM DFX 97-046 REV 3 APPROVED EFN 747-54-0149R1.

Part: SHEAR TIE — CORROSION (BS 1740)

INSPECTION TYPE-C, AFT CARGO COMPARTMENT FOUND SHEAR TIE DELAMINATED DUE TO CORROSION AT BS 1740, BETWEEN S-48/47 RT. REMOVED DAMAGED SHEAR TIE AND REPAIRED SHEAR TIE ACC SRM 53-10-04, FIG 3A.

Part: SKIN — LIGHTNING STRIKE (BS 180)

INSPECTION TYPE-C, BS 140 TO BS 180 S14EL AND BS 160 TO BS 180 ABOVE PAX WINDOWS, SEVERAL LIGHTNING STRIKES IN THESE AREAS. LIGHTNING STRIKES AT BS 140 TO BS 180 S14EL AND BS 160 TO BS 180 ABOVE PAX WINDOWS OUT OF LIMITS ACC SRM 53-30-01, REPAIRED LIGHTNING STRIKES ACC SRM 53-30-03 FIG 3A PARAGRAPH 3.

Part: SKIN — LIGHTNING STRIKE (BS 280-400)

INSPECTION TYPE-C, BS 280 TO 400 S17L, AND ABOVE WINDOWS AT BS 320 TO BS 360 SEVERAL LIGHTNING STRIKES IN SKIN. LIGHTNING STRIKES AT BS 280 TO BS 380 AND BS 320 TO BS 360 ABOVE WINDOWS OUT OF LIMITS ACC SRM 53-30-01. REPAIRED LIGHTNING STRIKES ACC SRM 53-30-03 FIG 3A PARAGRAPH 3.

Part: CAM SHAFT — CORRODED (NR 7 TE FLAP)

INSPECTION TYPE-C, FOUND INSIDE THE GENEVA CAM SHAFT NR 7 CORROSION. GENEVA CAM SHAFT NR 7 REPLACED ACCORDING MM 27-51-23.

Part: LIGHTS — INOPERATIVE (CABIN)

INSPECTION TYPE DLY, MAIN DECK TWO EMERGENCY EXIT LIGHTS INOP, FWD AISLE LIGHT AND FWD LIGHT IN L1 DOOR SILL. PERFORMED OPS CHK OF EMERGENCY LIGHTS, LIGHTS CHECK GOOD.

Part: FLOORBEAM — CORRODED (BS 1060)

WHILE IN FOR C-CHECK AMS MAINTENANCE REPORTED, FLOORBEAM UPPER CHORD CORRODED AT BS 1580 LBL 0. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-04.

Part: KEEL BEAM — CORRODED (BS 1242)

WHILE IN FOR C CHECK AT AMS, MAINTENANCE, FOUND CORROSION ON CENTERLINE KEELBEAM WEB INSIDE BSTA 1242. REPAIRED AS REQUIRED PER SRM 51-10-01, AND KLM DTZ 96-011.

Part: SPAR — CORRODED (WS 1000)

AMS - WHILE IN FOR C-CHECK, CORROSION ON LWR FRONT SPAR CHORD BBSTA 1000 NEAR STA 38L. REMOVED CORROSION PER SRM 57-10-01 FIG 1, OUT OF LIMIT. REWORKED CORROSION SPOT PER KLM DFX 96-001 BOEING APPROVAL.

Part: SKIN — DELAMINATED (LT WING LE)

MAINTENANCE REPORTED LEFT WING L/E BEHIND LANDING LIGHT HAS DELAMINATION. REPAIRED IAW SRM 51-40-09.

Part: SKIN — DELAMINATED (LT WING LE)

WHILE ON GROUND, MAINTENANCE FOUND LEFT WING L/E INBOARD OF NR 2 PYLON HAS DELAMINATION. ACCOMPLISHED COMPOSITE REPAIR REF: SRM 51-40-09.

Part: SKIN — DELAMINATED (NR 2 PYLON)

MAINTENANCE REPORTED LEFT WING L/E INBOARD OF NR 2 PYLON HAS DELAMINATION. REPAIRED IAW SRM 51-40-09.

Part: EEL WIRE — FAILED (FLIGHT DECK)

WHILE ON GROUND, MAINTENANCE FOUND FORWARD EMERGENCY LIGHT OVER THE MAIN ENTRANCE WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED FUSE IN AFT BATTERY PACK AND REPAIRED WIRE TO FRONT DOOR EMERGENCY LIGHT. OPS CK NORMAL, WORK PERFORMED IAW MM 33-51-00.

Part: FIRE WARNING — ACTIVATED (FLIGHT DECK)

PILOT REPORTED, SHORTLY AFTER T/O FIRE WARNING BELL AND LIGHT ACTIVATED FOR APPROX .5 SECOND. DUE TO THE SHORT DURATION OF WARNING, COULD NOT PINPOINT WHICH ENGINE BUT JUMPSEAT MECHANIC SAID DEFINITELY NR 3 OR NR 4 FIRE WARNINGS TESTED AND ALL CK OK. NR 4 ENG COMPARISON RUNS PERFORMED UP TO TAKEOFF POWER, COULD NOT DUPLICATE FIRE WARNING DISCREPANCIES. REPLACED A7 AND A11 FIRE WARNING CARDS, SYSTEMS OPS CHECKED GOOD IAW MM 26-11-00.

Part: ENGINE — MALFUNCTIONED (NR 3)

PILOT REPORTED, ON FINAL APPROACH WITH ALL ENGINES AT IDLE, NR 3 ENGINE SURGED TO 1.25 EPR, N1 80 PLUS PERCENT N1 AND HIGH FUEL FLOW. ENGINE WAS SHUTDOWN.

Part: EEL — INOP (CREW DOOR)

WHILE ON GROUND, MAINTENANCE FOUND CREW SERVICE DOOR EMERGENCY EXIT LIGHTS FOR SLIDE INOP, DEFERED MEL 33-13.

Part: EEL — DIM (CABIN)

WHILE ON GROUND IN SDF, MAINTENANCE FOUND EMERGENCY LIGHT IN CREW SERVICE DOOR FRAME IS DIM. MAINTENANCE RELAMPED EMERGENCY EXIT AT RT FLIGHT DECK SERVICE DOOR.

Part: EEL — DIM (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND CREW SERVICE DOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE CLEANED THE CONNECTOR, LIGHT OPS CK OK.

Part: TE SKIN — DELAMINATED (RT ELEVATOR)

WHILE ON GROUND IN ONT, MAINTENANCE FOUND RT I/B ELEVATOR T/E DELAMINATED. REPAIRED IAW SRM 51-40-15.

Part: PANEL — DELAMINATED (RT HORIZ STAB)

MAINTENANCE REPORTED PANEL DELAMINATED ON RT HORIZONTAL STAB, LWR SURFACE, 2ND PANEL FROM OUTBOARD. INSTALLED REPAIR PER UPS EO B747-5510-6994A.