N676UP

Part: GENERATOR — INOPERATIVE (NR 3)

INSPECTION TYPE:N/A ATB FOR NR 3 BUSS TIE ON WITH FEEDER FAULT LT & CONST SPEED LIGHT. FIVE MIN LATER, CONST SPD LIGHT GEN 2 & GEN 4 W/LOSS OF BOOST PUMP IN TANKS 2 AND 3, NR 2 AFT, NR 3 FWD. NR 3 FAULT ANNUNCIATOR SHOWED GEN/FEEDER. INSPECTED FEEDERS IN PYLON. REPLACED NR 3 GEN PER MM. CHECKED FOR VOLTAGE DROP & VOLTAGES AT BTR & GCR AND ALL CHECKED GOOD.

Part: CSD — OVERHEATED (NR 2 ENGINE)

IFSD, NR 2 ENG CSD HAD HIGH OIL TEMP. FLIGHT CREW TRIED TO DISCONNECT BUT COULDN'T. FOLLOWED CHECK LIST AND SHUT DOWN ENGINE. MX INSPECTED NR 2 ENG CSD AND FOUND THAT OIL HAD LEAKED OUT AND CSD OVERHEATED. CSD REMOVED AND REPLACED AND GEAR BOX INSPECTION IN WORK.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS)

EMERGENCY LIGHTS ABOVE R1 DOOR DO NOT WORK. FOUND TERMINAL END ON EXIT SIGN BROKEN. REPLACED PER BOEING SSWD 20-30-11. FUSE BLOWN ON POWER PACK MODULE. REPLACED MODULE X328 MM 33-51-04/2. ALSO, FOUND WIRES AT PLUG DC228 BROKEN. REPLACED PLUG PER BOEING SSWD 20-61-11. EMERGENCY LIGHTS OPS NORMAL IAW MM 31-51-04.

Part: ACCUMULATOR — LEAKING (BRAKE SYSTEM)

INSPECTION TYPE:N/A PILOT REPORT - BRAKES SLOW TO RESPOND, FOUND BRAKE ACCUMULATOR LOW DURING ATTEMPTED SERVICE. FOUND LARGE AMOUNT OF HYD FLUID ON NITROGEN SIDE OF ACCUMULATOR. REMOVED AND REPLACED BRAKE ACCUMULATOR PER MM 32-41-09. SERVICED, OPS CHECK GOOD.

Part: SPAR — BROKEN (DAMAGED) · airframe 85,501 hrs · 23,519 cycles

INSPECTION TYPE:C RIGHT HORIZONTAL STABILIZER UPPER REAR SPAR AND SPLICE PLATE INSP BROKEN BOLTS INDICATION REVEALED ON BOLT 6 & 29. RIGHT HORIZONTAL STAB UPPER REAR SPAR AND SPLICE PLATE BROKEN BOLTS 6 & 29 POSITION REPLACED (BOLTS P/N ON:BACB30US6K17 & BACB30US7K20) WITH NON-MAGNETIC TYPE BOLTS PER B747-5510-16378-G APP 'D'.

Part: SWIVEL — LEAKING (NR 4 RESERVOIR)

INSPECTION TYPE:N/A COMPLETE LOSS OF HYD QTY IN FLIGHT, ON SYSTEM NR 4. NOTE: RESERVOIR NR 4 INDICATED 1 GALLON. FOUND RIGHT MAIN GEAR DOWNLOCK ACTUATOR FWD HOSE NEAR UPPER FITTING AT SWIVEL LEAKING. REMOVED AND REPLACED HOSE ASSY, SERVICED NR 4 HYD QTY PRESSURIZED & OPERATED SYSTEM REF MM 32- 32-15. NO LEAKS NOTED. RAN NR 4 ENG HYD PUMP & ADP OK.

Part: TERMINAL — CORRODED (R1 WINDOW)

INSPECTION TYPE: N/A, SMOKE SMELLS, ABOUT 1:30 INTO FLIGHT. FOUND COPILOT WINDSCREEN CONNECTION AT LOWER RT SIDE SMOKING SECURED RT 1 OVERHEAD WINDOW HEAT, SMOKE STOPPED. FOUND R1 WINDOW HEAT POWER TERMINAL (A) LOOSE AT CORRODED. CLEANED, RETORQUED AT PERFORMED OPERATIONAL CHECK OF R1 WINDOW HEAT SY SYSTEM. OPS CHECK NORMAL. OK FOR SEVICE, REF MM 20-11-14, 56-11-01, AT 30-41-00.

Part: LIGHT — WEAK (CABIN)

INSPECTION TYPE: N/A EMERGENCY LIGHT ON CEILING ON MAIN DECK POS NR 1 IS VERY DIM. REMOVED AND REPLACED EMERGENCY CEILING LIGHT IAW MM 33-51-00. OPS CK GOOD. OK FOR SERVICE.

Part: SKIN — PUNCTURED (RT TE FLAP)

RT OB FLAP LWR SKIN APPX 1 INCH PUNCTURE. REMOVED DAMAGED AREA OF SKIN AND CORE PER SRM 51-40-06. DAMAGE REMOVED OKAY TO INSTALL REPAIR. DRYED AREA-INSTALLED REPAIR CORE AND STARTED CURE PER SRM 51-40-20. COMPLETED REPAIR PER SRM 51-40-20. REF LOG PAGE 566736/2

Part: MODULE — INOPERATIVE (CABIN)

MAIN DECK EMERGENCY LIGHT IN CEILING AT STA 580R GOES OFF AFTER A FEW SECONDS OF TEST. REMOVED AND REPLACED CEILING LIGHT MODULE PER MM 33-51-07. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

MAIN DECK EMERGENCY LIGHT IN CEILING AT STA 340R DOES NOT COME ON DURING TEST. PERFORMED LIGHT TEST W/LIGHT CHECKING GOOD ON GROUND.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE: N/A EMERGENCY LIGHT IN CEILING (FWD OF STAIRS) ON MAIN CARGO DECK INOPERATIVE. MAIN DECK UPPER DOOR FRAME FWD EMERGENCY LIGHT IS TIED TO THIS LIGHT AND IS ALSO INOPERATIVE. REMOVED AND REPLACED CEILING LIGHT MODULE W/REF TO MM 33-51-07. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE: N/A MAIN DECK EMERGENCY LIGHT IN CEILING AT STA 58DL AND ENTRY DOOR AFT EMERGENCY LIGHT GO OFF AFTER A FEW SECONDS OF TEST. THESE LIGHTS ARE TIED TOGETHER IAW MM. SUSPECT CEILING LIGHT BATTERY PACK BAD. REMOVED AND REPLACED CEILING LIGHT MODULE W/REF TO MM 33-51-07. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

INSPECTION TYPE: ASE UPPER DECK DOOR FRAME EMEGENCY LIGHTS X 325 AND X 326 ARE INOP. REMOVED AND REPLACED UPPER DECK DOOR LIGHT POWER SUPPLY MODULE WITH REF TO MM 33-51-04. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 440) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C U/D BS440 FLOORBEAM WEB FOUND CRACKED AFTER UPPER CHORD REMOVED JUST AT LBL 4, CRACK LENGTH 1". U/D BS440 BETWEEN LBL24 AND RBL16 FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11.

Part: SKIN — CRACKED (BS 380 S6R) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE: C U/D FX SKIN AT BS 380 S6R REPAIR AREA FOUND 3 ADDITIONAL FASTENER HOLES CRACK AT OUTER SKIN. CRACK LENGTH 0.060" & 0.090" RESP. FX BS360-384 S6R OVERLAPPING SKIN REPAIRED AS PER RS R53-15-35543 ITEM D REFER NRC 7055 FOR WORKING DETAIL. POST REPAIR INSP FOR ALL SKIN DOUBLER ARE TO BE CONTINUED AT REPEAT INTERVALS AS GIVEN IN SB 747-53-2253 AFTER MOD FLIGHT SAFETY INSP AND PER UPS ENGINEERING FILE 747-53-20319.

Part: REVEAL — CRACKED (BS 2231) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D BS 2231 FRAME INNER CHORD S25R-26R FOUND REVEAL CRACK AND PREVIOUSLY STOP DRILLED, CRACK LENGTH 1.5". REPAIR DOUBLER REINSTALLED AS PER RS R53-62-35534 CONTINUE THE REPETITIVE INSPECTION ARE REQUIRED PER RS R53-62-35534 AND UPS EO B747-5310-24835-B.

Part: REVEAL — CRACKED (BS 2231) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D BS 2231 FRAME INNER CHORD S22L-S25L FOUND REVEAL CRACKED AT S22L AND S24L LOCATION AND PREVIOUSLY STOP DRILLED, CRACK LENGTH 1" AND 1.5". REPAIR DOUBLER REINSTALLED AND THE CRACK THAT ENDS AT A FASTENER HOLE OVERSIZED AS PER RS R53-62-35534 CONTINUE THE REPETITIVE INSPECTIONS ARE REQUIRED PER RS R57-62-35534 AND UPS EO B747-5310-24835-B.

Part: FRAME — CRACKED (BS 340 S6R) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FX BS340 FRAME FOUND 1 HOLE CRACK AT S6R LOCATION APPROX 0.030" LONG, CRACK LENGTH 0.030". FX BS 340 STR 6R AREA FRAME REPAIRED AS PER RS R53-15-35543 ITEM B AND UPS ENGINEERING FILE NR 747-53-20319.

Part: SKIN — CRACKED (BS 340-380 S6R) · airframe 83,907 hrs · 23,132 cycles

FX BS 340-380 S6R LAP SPLICE TOP ROW FASTENER HOLES FOUND CRACKS AT OUTER SKIN. FX BS340-360 S6R FASTENER REINSTALLED AS PER RS R53-15-35543 ITEM C. REFER NRC 7055 FOR WORKING DETAIL. FX BS360-384 S6R OVERLAPPING SKIN DOUBLERS ARE TO BE CONTINUE AT REPEAT INTERVALS AS GIVEN IS SB 747-53-2253 AFTER MODIFICATION FLIGHT SAFETY INSPECTION AND PER UPS ENGINEERING FILE 747-53-20319.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FX BS 340-360 S6R FOUND FASTENER HOLES CRACK AT STRINGER (CRACK LENGTH 0.030 INCH). FX BS 340-375 STR 6R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 3.

Part: FLOORBEAM — CORRODED (BS 520) · airframe 83,907 hrs · 23,132 cycles

BS 520 FLOORBEAM UPPER CHORD FOUND CORRODED. CORROSION BLEND OUT 0.030" BY 2" BY 3" EXCEED SRM 53-10-01 FIG 1 LIMIT AND U/D BS 520 FLOORBEAM UPPER CHORD REPAIRED AS PER HX RS NR R53-25-35537 REF NRC NR IB70247 FOR WORKING DETAIL AND REF UPS EO NR B747-5310-24843-A.

Part: FLOORBEAM — MISDRILLED (BS 520) · airframe 83,907 hrs · 23,132 cycles

BS 520 FLOORBEAM UPPER CHORD FOUND SHORT EDGE MARGIN FROM RBL 48 TO RBL 82. BS 520 FLOORBEAM REPAIRED AS PER HX RS NR R53-25-35537 REFER NRC NR IB70247 FOR WORKING DETAIL AND REF UPS EO NR B747-5310-24843-A.

Part: FLOORBEAM — MISDRILLED (BS 520) · airframe 83,907 hrs · 23,132 cycles

BS 520 FLOORBEAM UPPER CHORD FOUND SHORT EDGE MARGIN AT LBL 76" TO LBL 78" APPROX. U/D BS 520 FLOORBEAM REPAIRED AS PER HX RS NR R53-25-35537 REFER NRC NR IB70247 FOR WORKING DETAIL AND REF UPS EO NR B747-5310-24843-A.

Part: SKIN — CRACKED (BS 360-380 S6R) · airframe 83,907 hrs · 23,132 cycles

FX BS 360-380 S6R LAP SPLICE 6EA TOP ROW FASTENER HOLE FOUND CRACKS AT OUTER SKIN, CRACK LENGTH 1/16 APPROX. FX BS 340 TO BS 360 STR 6R FASTENER REINSTALLED AS PER RS R53-15-35543 ITEM C FX BS360-384 STR 6R OVERLAPPING SKIN REPAIRED AS PER RS R53-15-35543 ITEM D. POST REPAIR INSPECTION FOR ALL SKIN DOUBLER ARE TO BE CONTINUED AT REPEAT INTERVALS AS GIVEN IN SB 747-53-2253 AFTER MOD FLIGHT SAFETY INSPECTION AND US ENG FILE 747-53-20319.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C RT BLG W/W STA 1438 FRAME ATT HOLE FOUND CRACKED RBL 116 WL 156, CRACK LENGTH 3/8". RT BLG W/W BS 1438 RBL 116 WL 152 TO WL 165 FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C 1R MED FWD VERTICAL BEAM LOWER CORNER FOUND CRACK. CRACK LENGTH 1 INCH. 1R MED FWD VERTICAL BEAM LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FWD CARGO COMPT RT MAIN DECK FLOORBEAM LOWER CHORD SPLICE PLATE LOWER SURFACE FOUND SURFACE CORROSION AT STA 680 TO STA 700 RBL12. CORROSION BLEND OUT 0.019" BY 1/2" BY 1" EXCEED SRM LIMIT. FWD CARGO COMPT RT MAIN DECK FLOORBEAM LOWER CHORD SPLICE PLATE REPLACED AS PER SRM 51-10-01 PG 9 JUST AT STA 680-700 RBL 12 AREA.

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C 1L MED FWD VERTICAL BEAM LOWER CORNER CRACK FOUND AS MARKED. CRACK LENGTH 1 INCH. 1L MED FWD VERTICAL BEAM LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: ANGLE — CRACKED (BS 2231) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C RT SIDE BS2231 FRAME AT STR25 FOUND 2 HOLES CRACKED AT INTERCOSTAL TO FRAME WEB ATTACHED T-ANGLE AREA. CRACK LENGTH 1/8". RT SIDE BS 2231 FRAME AT STR 25 FRAME WEB ATTACHED T-ANGLE REPLACED AS PER SRM 51-10-01 PG 9.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

BS 820-840 STR -10R STRINGER ATT SHEAR WEB FWD END FOUND CRACKED, CRACK LENGTH 1/2". SHEAR WEB REPAIRED AS PER SRM 51-40-03 FIG 3.

Part: FLOORBEAM — CORRODED (BS 520) · airframe 83,907 hrs · 23,132 cycles

LT BS 520 UPPER DECK FLOORBEAM AFT FLANGE 5 FASTENER HOLES FOUND CRACK AND/OR CORROSION AT LBL 34, LBL 45, LBL 49, AND LBL 55" (CRACK LENGTH 0.060" , CORROSION BLEND OUT 0.075" X 1.5" X 2"). CORROSION EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 520 FLOORBEAM UPPER CHORD REPAIRED AS PER HX RS NR R53-25-35537, C/O INSPECTION PER AD 2005-20-29 AND RS NR R53-25-35537 REF E AND REF G WITHIN 15000 CYC AFTER CHORD REPLACEMENT AND REF UPS EO NR B747-5310-24843-A.

Part: STRAP — CRACKED (FLOORBEAM) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C U/D RT BS520 UPPER DECK FLOORBEAM FWD FLANGE AREA 1 FASTENER HOLE FOUND CRACK AT FLOOR CHORD STRAP AT RBL 35. CRACK LENGTH 0.030". STRAP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG9 AND SRM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 440) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C U/D RT BS440 UPPER DECK FLOORBEAM FWD FLANGE 1 FASTENER HOLE FOUND CORROSION AT RBL24. CORROSION BLEND OUT 0.048". FASTENER HOLE OVERSIZED TO 0.326" AS PER SRM 51-30-05 AS PER UPS EO B747-5310-23043 APP D WITHIN THE LIMITATION.

Part: FLOORBEAM — DAMAGED (BS 440) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C U/D RT BS 440 UPPER DECK FLOORBEAM FWD FLANGE 1 FASTENER HOLE FOUND OVAL AT RBL 48. U/DECK BS 440 LBL 68" TO RBL 68" FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 14.

Part: FLOORBEAM — CRACKED (BS 520) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C U/D LEFT BS 520 UPPER DECK FLOORBEAM FWD FLANGE 1EA FASTENER HOLE FOUND CRACK AT LBL 45. CRACK LENGTH 0.030 INCH. U/D BS 520 FLOORBEAM UPPER CHORD FWD FLANGE AT LBL45 AREA HOLE OVERSIZED TO 0.326 INCH AND C/D WAS MEASURED MORE THAN 1.3 PER UPS EO B747-5310-23043 APP D. NO MORE REPAIR IS NESESSARY.

Part: FLOORBEAM — DAMAGED (BS 440) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C U/D BS440 MOST OF FLOORBEAM FASTENER HOLE FOUND SHORT EDGE BELOW 0.44" AS MARKED AT BETWEEN LBL 44 TO LBL 53 AND RBL 44 TO RBL 53 AREA. U/D BS 440 BETWEEN LBL68 TO RBL68 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 14 REFER NRC7031 FOR WORKING DETAIL L/R BL44 TO L/R BL53 FLOORBEAM ATTACH GUSSETS REPLACED AS PER SRM 51-10-01 PG 9.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C U/D RIGHT BS 50 UPPER DECK FLOORBEAM AFT FLANGE 2EA FASTENER HOLE FOUND CORROSION AT RBL16 AND RBL 27. 0.310" & 0.326" OVERSIZED. FASTENER HOLE OVERSIZED TO 0.326" AT RBL 16 & 0.310" AT RBL 27 AS PER SRM 51-30-05 AS PER UPS EO B747-5310-23043 APP D WITHIN THE LIMITATION.

Part: FLOORBEAM — CORRODED (BS 440) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C U/D RT BS 440 UPPER DECK FLOORBEAM AFT FLANGE 1 FASTENER HOLE FOUND CRACK AND CORROSION AT RBL7. CORROSION BLEND OUT 0.032" FASTENER HOLE OVERSIZED TO 0.310" AS PER SRM 51-30-05 AS PER UPS EO B747-5310-23043 APP D WITHIN THE LIMITATION.

Part: FLOORBEAM — DAMAGED (BS 520) · airframe 83,907 hrs · 23,132 cycles

U/D RT BS 520 UPPER DECK FLOORBEAM FWD FLANGE 1 FASTENER HOLE FOUND OVAL AT RBL 70". U/D BS 520 FLOORBEAM REPAIRED AS PER HX RS NR R53-25-35537 REF NRC NR IB70247 FOR WORKING DETAIL AND REF UPS EO NR B747-5310-24843-A.

Part: GUSSET — CRACKED (FLOORBEAM) · airframe 83,907 hrs · 23,132 cycles

RT BS 520 UPPER DECK FLOORBEAM FWD FLANGE AREA 2 FASTENER HOLES FOUND CRACK AT GUSSET AT RBL 35 AND RBL 39.5 (CRACK LENGTH 0.060"). U/DECK BS 820 RBL 31" TO RBL 40" GUSSET REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C U/D RIGHT BS 520 UPPER DECK FLOORBEAM FWD FLANGE 2EA FASTENER HOLE FOUND CORROSION AT RBL 21 & RBL 25. FASTENER HOLE OVERSIZED TO 0.342" AT RBL 21 AND 0.310" AT RBL 25 AS PER SRM 51-30-05 AS PER UPS EO B747-5310-23043 APP D WITHIN THE LIMITATION.

Part: SHEAR WEB — CRACKED (BS 820-840) · airframe 83,907 hrs · 23,132 cycles

FOUND BS 820-840 STR -10L STRINGER ATT SHEAR WEB BOTH END FOUND CRACK (CRACK LENGTH 1"). SHEAR WEB REPLACED AS PER SRM 51-10-01 PG 9.

Part: REVEAL — CRACKED (BS 2231) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D BS2231 BETWEEN S25L AND 26L REVEAL CRACK, CRACK LENGTH 0.8". M/D BS 2231 BETWEEN STR 25L-STR 26L REVEAL PANEL REPAIRED AS PER RS R53-62-35536 AND UPS EO B747-5310-24836-B.

Part: FLOORBEAM — CORRODED (BS 520) · airframe 83,907 hrs · 23,132 cycles

BS 520 LBL 33-47 FLOORBEAM FOUND CORROSION AS MARKED. CORROSION BLEND OUT 0.051" BY 1.5" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, AND U/D BS 520 FLOORBEAM UPPER CHORD REPAIRED AS PER HX RS NR R53-25-35537 REFER NRC NR IB70247 FOR WORKING DETAIL AND REF UPS EO NR B747-5310-24843-A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FWD CARGO COMPT - LT STA 980 STR39 FRAME FOUND CRACKED. CRACK LENGTH 1/2". FWD CARGO COMPT LT STA980 STR39 FRAME REPAIRED AS PER RS R53-10-35553 JUST BETWEEN STR36L AND STR40L AREA CONTINUE INSP IS REQUIRED AS PER RS R53-10-35553 AND UPS EO B747-5310-24839-A.

Part: FLOORBEAM — CORRODED (BS 480) · airframe 83,907 hrs · 23,132 cycles

BS 480 LBL 10- RBL 32 FLOORBEAM UPPER FACE FOUND CORRODED. CORROSION BLEND OUT 0.021" BY 1" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 480 LBL 10" - RBL 32" FLOOR SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SPLICE PLATE — CRACKED (NLG WW) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C NWW LT AFT CORNER BS 400 S44L INTERNAL SPLICE PLATE FOUND CRACK FROM FWD EDGE AND PASS THRU 1ST FASTENER AND GO UNDERNEATH BULKHEAD CHORD (CRACK LENGTH 3.5 INCH). NWW LT AFT CORNER BS 400 S44L INTERNAL SPLICE PLATE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (BS 800) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE-C LT SIDE BS800 FRAME AT STR16 FOUND 1EA HOLE CRACKED AT FRAME STRAP APPROX .0625 INCH LONG RUNNING. CABIN LT SIDE BS800 FRAME ATTACH STRAP BETWEEN STR15L TI STR18L AREA REAIRED IAW RS R53-10-35541. CONTINUE INSPECTION AND SUPPLEMENTAL INSPECTION FOR THIS REPAIR IAW RS R53-10-35541 ARE REQUIRED AND IAW EO B747-5310-24842-A.

Part: SKIN — CORRODED (BS 565-622) · airframe 83,907 hrs · 23,132 cycles

RT BS 579 S44R LAP JOINT LOWEST FASTNENER HOLE FOUND CORROSION INDICATION AT OUTER SKIN AND INNER SKIN INTERFACE. CORROSION BLEND OUT AT INNER SKIN 0.009" BY 7/8" BY 1" AND OUTER SKIN 0.008" BY 3/4" BY 7/8". FX BS 565-622 BETWEEN STR 43R AND 45R OVERLAPPING AND OVERLAPPING SKIN REPAIRED WITH ZERO TIMED AT CRITICAL ROW FASTENER AS PER SRM 53-30-03 FIG 19. SUBSEQUENT INSPECTIONS ARE NECESSARY FOR CAT B REPAIR. REFER TO SRM 53-30-03 FIG19 TABLE 3 FOR INSPECTION REQUIREMENT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

BS 540 LBL 9-27 FLOORBEAM FOUND CORROSION AS MARKED. CORROSION BLEND OUT 0.020" BY 1.5" BY 1.5" EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 540 BL 0" TO LBL 35" FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 21.

Part: FRAME — CRACKED (BS 1283) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D BS 1283 RT S15-16 FRAME O/B FLANGE FOUND CRACK. CRACK LENGTH 1.25 INCH. M/D BS 1283 RT STR 15-16 FRAME O/B FLANGE REPAIRED AS PER SRM 53-10-04 FIG 1.

Part: FRAME — CRACKED (BS 360 S23R) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D BS360 S23R FRAME STRINGER CUTOUT CRACK, CRACK LENGTH 3/4". M/D BS360 STR23R FRAME REPAIRED AND ATTACH TIE CLIP REPLACED AS PER RS R53-11-35533 CONTINUE INSPECTION IS REQUIRED TO THE REPAIR AREA PER SB 747-53A2265 AND UPS EO B747-5310-24766-A.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D BS380 STR14ER FRAME ATTACH DOUBLER CRACK. CRACK LENGTH 0.5 APP. M/D BS380 STR14E RT FRAME ATTACH DOUBLER REPAIRED AS PER RS R53-11-35531 CONTINUE INSPECTION IS REQUIRED AS PER SB B747-53A2265 AND UPS EO B747-5310-24765-A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

FOUND BS 340 S13AL STRINGER CRACK, CRACK LENGTH 3/8", M/D BS 340-360 STR 13AL. REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: TIE CLIP — CORRODED (FWD CARGO BAY) · airframe 83,907 hrs · 23,132 cycles

FWD CARGO COMPT RT STA 940 STR 28 TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.015" BY 3/8" BY 1.5 IS EXCEED SRM 53-10-01 FIG 1 LIMITS, FWD CARGO COMPT BS 940 STR 28R TIE CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SUPPORT — CORRODED (TE FLAPS) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C RHW I/B T/E AFT FLAP INTERNAL REAR SUPPORT CHANNEL AT WBL135 FOUND CORROSION DAMAGED. CORROSION BLEND OUT 0.080" BY 1/2" BY 1/2" EXCEED SRM LIMIT. RHW I/B T/E AFT FLAP INTERNAL REAR SUPPORT CHANNEL AT WBL130-141 AREA REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: NUT PLATE — CORRODED (NLG WW) · airframe 83,907 hrs · 23,132 cycles

N/G W/W RT INTERNAL SIDE STA 360 BOTTOM AREA DOOR FITTING NUT PLATE FOUND CORROSION AS MARKED. CORROSION BLEND OUT 0.077" BY 1/2" BY 1/2" EXCEED SRM 53-10-01 FIG 1 LIMITS, AND THE NUT PLATE REPLACED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SUPPORT — CORRODED (RT WING FLAPS) · airframe 83,907 hrs · 23,132 cycles

RHW I/B T/E AFT FLAP INTERNAL REAR SUPPORT DAMAGED AT WBL 440 FOUND CORROSION DAMAGED. CORROSION BLEND OUT 0.080" BY 1/2" BY 1" EXCEED SRM 57-50-01 FIG 3 LIMITS, RHW I/B T/E AFT FLAP INTERNAL REAR SUPPORT AT WBL 423 TO 442. REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT RT STA1500 IN BETWEEN RBL 30 AND RBL 32 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.033" BY 1" BY 6". AFT CARGO COMPT BS1500 FLOORBEAM UPPER CHORD AT RBL 11 TO RBL 60 AREA REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: STRINGER — CORRODED (BS 1800) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT RT STA 1800 STRINGER 36 TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.019" BY 1/2" BY 3". AFT CARGO COMPT RT STA 1800 STR 36 TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.

Part: ANGLE — CORRODED (RT MLG WW) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C B/G RT W/W STA 1405 TOP PANEL CORROSION AS MARK AT RBL 85". CORROSION BLEND OUT 0.050" BY 1/2" BY 1/2" EXCEED SRM 53-10-01 FIG 1 LIMITS, B/G RT W/W BS 1405 TOP PANEL SPLICE ANGLE REPAIRED AT RBL 83-64" AS PER RS NR R53-48-35550 AND UPS ENGINEERING FILE NR 747-53-20307.

Part: INTERCOSTAL — CRACKED (BS 565 S30L) · airframe 83,907 hrs · 23,132 cycles

FWD CARGO COMPT BS 565 STR 30L FRAME INTERCOSTAL FOUND CRACK. CRACK LENGTH 1/2. INTERCOSTAL REPLACED AS PER SRM 51-10-01 PG 9.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C NLG WW RT INTERNAL SIDE STA348 WL173 WHEEL WELL SIDE FOUND CRACKED AS MARKED, CRACK LENGTH 2.215". NOSE W/W BS 350 RT SIDE PANEL BETWEEN WL160 AND WL170 REPAIRED AS PER RS R53-18-35532 CONTINUE INSPECTION ARE REQUIRED AS GIVEN IN SB 747-53A2349 R2 AND UPS EO B747-5330-24831-A.

Part: ANGLE — CORRODED (BLG W/W) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C B/G RIGHT W/W STA 1438 O/B AREA FRAME ATTACH ANGLE FOUND CORROSION AS MARK AT RBL 116. CORROSION BLEND OUT 0.047 X .5 X 5 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS. B/G RIGHT W/W STA 1438 O/B AREA FRAME ATTACH ANGLE AT RBL 116 REPLACED AS PER SRM 51-10-01 PG 9.

Part: STRINGER — CORRODED (BS 1500) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT RT STA 1500 STRINGER 29 TIE CLIP FOUND CORRODED. CORROSION BLEND OUT 0.017" BY 1/2" BY 2". AFT CARGO COMPT RT STA 1500 STR 29 TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.

Part: SUPPORT — CRACKED (BS 2598) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C EMP - BS 2598 BULKHEAD UPPER CENTER SECTION RT LOWER SUSPECT CRACK AT RBL 36. CRACK LENGTH 1.25 INCH. EMP - BS 2598 BULKHEAD UPPER CENTER SECTION RT LWR FLOOR SUPPORT REPAIRED AS PER RS R53-83-25547 JUST BETWEEN RBL 26 AND RBL 37 AND UPS ENGINEERING FILE 747-53-20310.

Part: SHEAR TIE — CORRODED (BS 1560) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT BS 1560 STR 28L FRAME TIE CLIP FOUND CORRODED. CORROSION BLEND OUT 0.019" BY 1" BY 2". AFT CARGO COMPT BS 1560 STR 28L FRAME TIE CLIP REPLACED AS PER SRM 51-10-01 P9.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D R1 DOOR AFT LOWER STOP FITTING FOUND CRACKED. CRACK LENGTH .5 INCH. STOP FITTING REPLACED AS PER SRM 51-10-01 PG 9.

Part: STRINGER CLIP — CORRODED (BS 1560) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT RT STA1560 STRINGER 28 TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.015" BY 1/2" BY 3". AFT CARGO COMPT RT STA 1560 STR 28 TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

AFT CARGO COMPT LT STA1560 IN BETWEEN LBL32 AND LBL45 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.033" 1/2" BY 8". AFT CARGO COMPT STA 1560 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2 JUST BETWEEN LBL 16 AND LT MOST O/B AREA.

Part: SHEAR TIE — CRACKED (BS 2040) · airframe 83,907 hrs · 23,132 cycles

BULK CARGO COMPT BS 2040 FRAME FOUND CRACK AT STA 29L CUTOUT. CRACK LENGTH 3/4", BULK CARGO CINOT BS 2040 STR 28L-29L FRAME SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: FRAME — CORRODED (BS 1438) · airframe 83,907 hrs · 23,132 cycles

B/G RT W/W STA 1438 O/B SIDE AREA NEAR TOP PANEL FOUND CORROSION AS MARK AT RBL 115". CORROSION BLEND OUT 0.070" BY 1" BY 1.5" EXCEED SRM 53-10-01 FIG 1 LIMITS, B/G RT W/W STA 1438 BETWEEN WL 183 AND WL190 S28R FRAME REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE: C AFT CARGO COMPT RT STA 1520 IN BETWEEN STR 38 AND STR 39 FRAME FOUND CRACKED. CRACK LENGTH 2 INCHES. FRAME REPAIRED IAW SRM 53-10-04 FIG 69.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT BS 1660 STR 35L FRAME ATT STIFFENER FOUND CRACK (CRACK LENGTH .375 INCH). AFT CARGO COMPT BS 1660 STR 35L FRAME ATTACHED CRACK STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: FRAME — CRACKED (BS 2060) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C BULK CARGO COMPT BS 2060 FRAME FOUND CRACK AT STA 29L CUTOUT. CRACK LENGTH 1 INCH. BULK CARGO COMPT BS 2060 STR 29L AREA FRAME REPAIRED AS PER SRM 53-10-04 FIG 39.

Part: CARGO TRACK — CORRODED (BS 1500-1520) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT RT STA 1500-1520 I/B TIE DOWN TRACK FOUND CORROSION. CORROSION BLEND OUT 0.047" BY 1/2" BY 10". TIE DOWN REPLACED AS PER SRM 51-30-02 AND 51-10-01 PG 9.

Part: STRINGER — CORRODED (BS 1500) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT RT STA1500 STRINGER 30 TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.025" BY 1/2" BY 3". AFT CARGO COMPT STA1500 STR30 TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.

Part: STRINGER CLIP — CORRODED (BS 1500) · airframe 83,907 hrs · 23,132 cycles

AFT CARGO COMPT RT STA 1500 STRINGER 33 TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.026" BY 1/2" BY 4". AFT CARGO COMPT RT STA 1500 STR 33 TIE CLIP FOUND CORROSION.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C NLG W/W RT INTERNAL SIDE STA352 WL181 W/W SIDE FOUND CRACK CROSS OVER STOP HOLE AS MARKED. CRACK LENGTH 2.37 NOSE W/W BS350 RT SIDE PANEL BETWEEN WL160 AND WL170 REPAIRED AS PER RS R53-18-35532 REFER NRC6739 FOR WORKING DETAIL. CONTINUE INSP ARE REQUIRED AS GIVEN IN SB 747-53A2349 R2 AND UPS EO B747-5330-24831-A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

AFT CARGO COMPT LT STA 1760 IN BETWEEN LBL45 AND LBL 58 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.035" BY 2" BY 3". AFT CARGO COMPT BS 1760 LBL16 TO LT MOST O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT LT STA1540 IN BETWEEN LBL 32 AND LBL 45 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.046" BY 1.5" BY 8". AFT CARGO COMPT LT STA 1540 IN BETWEEN LBL 16 TO LT O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FWD CARGO COMPT LT STA560 I/B TIE DOWN TRACK FOUND CORROSION. CORROSION BLEND OUT 0.055" BY 3/8" BY 1.5" EXCEED SRM LIMIT. FWD CARGO COMPT BS 510-570 LT I/B TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FWD CARGO COMPT STA 660 IN BETWEEN LBL 7 AND RBL 7 FLOORBEAM UPPER CHORD ATT PLATE FOUND CORROSION. CORROSION BLEND OUT 0.060" BY 1/2" BY 1.5" EXCEED SRM LIMIT. FWD CARGO COMPT BS 600 LBL 7 TO RBL 7 FLOORBEAM UPPER CHORD ATTACH PLATE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: RIB — CRACKED (WING) · airframe 83,907 hrs · 23,132 cycles

NR 1M FUEL TANK WS 862 RIB LOWER CHORD AT STR 6 FOUND CRACK, CRACK LENGTH 1/2"). LWR CHORD REPAIRED AS PER SRM 57-10-05 FIG 3

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FWD CARGO COMPT STA 640 BL0 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.090" BY 3/4" BY 1 1/4" EXCEED SRM LIMIT. FWD CARGO COMPT BS 640 LBL12.5 TO RBL 14 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG2.

Part: FRAME — CRACKED (BS 340) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C RT BS 340 UPPER DECK FLOORBEAM UPPER CHORD AREA 1 FASTENER HOLE FOUND CRACKED AT FRAME WEB LAYER THROUGH THICKNESS, CRACK LENGTH 3/32". CABIN U/D BS340 RT FRAME WEB AT WL310 AREA REPAIRED AS PER SRM 53-10-04 FIG 102 AND RS R53-10-35527 REPEAT INSPECTION IS REQUIRED AS PER RS R53-10-35527 ITEM 3 AND UPS EO B747-5310-24841-A.

Part: CARGO TRACK — WORN (CARGO BAY) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE: C FWD CARGO COMPT RT STA 620-640 OB TIE DOWN TRACK FOUND WORN. TIE DOWN TRACK REPLACED IAW SRM 51-10-01 PG 9 JUST AT OB BETWEEN BS 600 AND 690 RBL 45.

Part: FRAME — CRACKED (NR 3 PYLON) · airframe 83,907 hrs · 23,132 cycles

NR3 PYLON O/B SUPPORT FRAME LOWER PORTION FOUND CRACK AT NAC STA 252 AS MARKED, CRACK LENGTH 3/4". NR 3 PYLON NAC STA252 O/B SUPPORT FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

FWD CARGO COMPT, RT STA 820-840 STRINGER 47 FOUND CORRODED AND CRACKED, CRACK LENGTH 3/4". STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1, AT STR 47R BETWEEN BS 820 AND 850.

Part: STRINGER — CRACKED (RT WING) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C RHW NR 26 VC FLAP LOWER STR FOUND CRACKED AT 2 LOCATIONS. CRACK LENGTH 3/4" AND 3/8". LOWER STRINGER REPLACED AS PER SRM 51-30-02 AND 51-10-01 PG 9.

Part: RIB — CRACKED (WS 767RT) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C RT WING L/E SUPPORT RIB FOUND CRACKED AT WS 767 JUST BEHIND NR 17 VC FLAP I/B ROTARY, CRACK LENGTH 0.3" TO 4.5" RESP. RHW L/E SUPPORT RIB AT WS 767 BEHIND NR 17 VC FLAP O/B ROTARY ACTUATOR AREA REPAIRED AS PER RS R57-41-35530 CONTINUE INSPECTION IS REQUIRED AS PER RS R57-41-35530 AND UPS EO B747-5710-24821-A.

Part: SHEAR TIE — CRACKED (BS 1000) · airframe 83,907 hrs · 23,132 cycles

FWD CARGO COMPT, RT STA 1000 RBL 57 CENTER SECTION FRONT SPAR UPPER SECDTION SHEAR TIE FOUND CRACKED. CRACK LENGTH 1 3/8". SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D BS540 STR23-25R FRAME FWD FACE O/B AREA FOUND CRACK. CRACK LENGTH 1/2". M/D BS540 STR23R TO STR25R FRAME REPAIRED AS PER RS R53-10-35538 AND UPS EO B747-5310-24760-A.

Part: RIB — CRACKED (LT WING) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C LT WING L/E UPPER SUPPORT RIB FOUND CRACKED AT WS 970 BEHIND NR 7 VC FLAP I/B CRACK LENGTH 0.5 TO 3.5 INCH. LT WING L/E UPPER SUPPORT RIB AT WS 970 BEHIND NR 7 VC FLAP I/B AREA REPAIRED AS PER RS R57-41-35528 CONTINUE INSPECTION IS REQUIRED PER RS R57-41-35528 AND UPS EO B747-5710-24761-A.

Part: RETAINER — CORRODED (FRAME) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FX, LT LOWER FUSELAGE INTERIOR SUPPORT FRAME INNER CHORD ATT RETAINER FOUND CORROSION AT STA 2200 S-44L-46L AFT SURFACE. CORROSION BLEND OUT 0.050" BY 1/2" BY 2". RETAINER REPLACED AS PER SRM 51-10-01 PG 9.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D - L1 DOOR FWD CUTOUT REVEAL CRACK AT NR 5 STOP AREA (COUNT FROM LWR) CRACK LENGTH .375 INCH. CUT OUT REVEAL REPLACED AS PER SRM 51-10-01 PG 9 AND SRM 51-30-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FWD CARGO COMPT STA 640-650 BL 0 FLOORBEAM UPPER CHORD ATT PLATE FOUND CORROSION. CORROSION BLEND OUT 0.063" BY 1/2" BY 3/4" EXCEED SRM LIMIT. FWD CARGO COMPT BS 640-650 LBL5-RBL5 FLOORBEAM UPPER CHORD ATTACH PLATE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

AFT CARGO COMPT, LT STA1500 IN BETWEEN LBL30 AND LBL45 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.024" BY 1" BY 6". FLOORBEAM UPPER CHORD AT STA 1500 LBL 28 TO MOST O/B REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT RT STA 1620 IN BETWEEN RBL32 AND RBL45 FLOORBEAM CHORD FOUND CORROSION. CORROSION BLEND OUT 0.024" BY 1.5" BY 1.5". AFT CARGO COMPT RT STA 1620 IN BETWEEN RBL 32 AND RBL 45 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: CARGO TRACK — CORRODED (BS 1772) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT RT STA 1772 I/B TIE DOWN TRACK FOUND CORROSION. CORROSION BLEND OUT 0.055" BY 3/4" BY 2". TIE DOWN TRACK REPAIRED AT RT STA 1750-1772 AS PER SRM 53-10-05 FIG 5 WORK DETAIL REFER NRC 5988.

Part: FLOORBEAM — CORRODED (BS 1760) · airframe 83,907 hrs · 23,132 cycles

AFT CARGO COMPT RT STA 1760 IN BETWEEN RBL 7 AND RBL 25 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.025" BY 1.5" BY 10". AFT CARGO COMPT BS 1760 BETWEEN LBL 16 TO RBL 16 FLOORBEAM UPPER REPAIRED AS PER SRM 51-40-04 FIG 2 RBL 16 TO RBL 25 CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 BLEND OUT DEPTH 0.006" WIDTH 1" AND LENGTH 8" WITHIN SRM 53-10-01 FIG 1 LIMITATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

AFT CARGO COMPT RT STA1600 IN BETWEEN RBL 32 TO RBL45 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.030" BY 1" BY 2". AFT CARGO COMPT RT STA1600 COR BLEND OUT OF LIMIT UPPER CHORD FROM RBL 36-38 REPAIRED AS PER SRM 51-40-04 FIG 2 RBL32-36 AND RBL38-45 REPAIRED AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 OR THICKNESS 0.088 DEPTH 0.006" WIDTH 1" AND LENGTH 7" WITHIN SRM 53-10-01 FIG1 LIMITATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FWD CARGO COMPT LT STA 760 IN BETWEEN LBL40 AND LBL45 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.030" BY 3/4" BY 1 3/4" EXCEED SRM LIMIT. FWD CARGO COMPT BS760 LBL40 - LBL45 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: RETAINER — CORRODED (FRAME) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FX RT LOWER FUSELAGE INTERIOR SUPPORT FRAME INNER CHORD ATT RETAINER FOUND CORROSION AT STA2200 STR 44R TO 46R AFT SURFACE. CORROSION BLEND OUT 0.050" BY 1/2" BY 2". BS 2200 STR 44R TO STR 46R FRAME INNER CHORD ATT RETAINER REPLACED AS PER SRM 51-10-01 PG9 AND INSTALLED AS PER SRM 51-30-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

AFT CARGO COMPT LT STA1820 IN BETWEEN LBL 12 AND LBL 24 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.025" BY 1.5" BY 2". AFT CARGO COMPT BS 1820 LBL 12.5 TO LBL 14 AREA FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG2 AND FLOORBEAM UPPER CHORD LBL14 TO LBL24 AREA CORROSION. REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 BLEND OUT DEPTH 0.005" WIDTH 1/2" LENGTH 10" WITHIN SRM 53-10-01 FIG1 LIMITATION.

Part: CARGO TRACK — CRACKED (BS 1770) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT RT STA 1770 I/B TIE DOWN TRACK FOUND CRACKED CRACK LENGHT 7/8". TIE DOWN TRACK REPAIRED AT RT STA 1750-1770 AS PER SRM 53-10-05 FIG 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FWD CARGO COMPT RT STA 800 IN BETWEEN RBL 32 AND RBL 45 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.033" BY 5/8" BY 2" EXCEED SRM LIMIT. FWD CARGO COMPT RT STA 800 IN BETWEEN RBL 18 AND RT O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C AFT CARGO COMPT RT STA1740 IN BETWEEN RBL32 AND RBL45 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.028" BY 1" BY 1.5". AFT CARGO COMPT BS 1740 AT RBL 34-35.5 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2 AND RBL 32 TO RBL 34, RBL 35.5 TO RBL 45 CORROSION REMOVED AND REPORTED DEPTH 0.005" WIDTH 1" AND LENGTH 10" WITHIN SRM 53-10-01 FIG 1 LIMITATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C FWD CARGO COMPT LT STA 860 IN BETWEEN LBL32-45 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.030" BY 3/4" BY 2" EXCEED SRM LIMIT. FWD CARGO COMPT BS 860 LBL 32 TO LT O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG2.

Part: TENSION TIE — CRACKED (BS 800) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D BS 800R TENSION TIE FOUND 1 FASTENER HOLE SHORT OF EDGE MARGIN AT STEEL PLATE AND CHANNEL. M/D BS 800R TENSION TIE FWD AND AFT CHANNEL AT JUST O/B OF THE RT VERTICAL POST TO RT O/B END AREA AS PER RS R53-25-35525 STEEL PLATE RETAINS AS IS AND INSTALLED AS PER RS R53-25-35525 AND UPS EO B747-5310-24767-A. REFER NRC 5327 FOR WORKING DETAIL.

Part: PLATE — DAMAGED (BS 940) · airframe 83,907 hrs · 23,132 cycles

BS 940R TENSION TIE FWD STEEL PLATE FOUND 2 FASTENER HOLES SHORT OF EDGE MARGIN AND 1 FASTENER HOLE AT MOST O/B OF TENSION TIE SHORT OF EDGE MARGIN. BS 940R TENSION TIE FWD CHANNEL AND ATTACH STEEL PLATE REPAIRED AS PER RS R53-25-35523 REPEAT INSPECTION ARE REQUIRED AS PER RS R53-25-35523 REF C PER FAA 8100-9 FORM DATED 08/02/06 AND UPS EO B747-5310-24818-A.

Part: PLATE — DAMAGED (BS 800) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D, BS 800L TENSION TIE FWD STEEL PLATE FOUND 3 FASTENER HOLE SHORT OF EDGE MARGIN, CRACK LENGTH SEM. M/D BS 800L TENSION TIE FWD STEEL PLATE REPAIRED AS PER RS R53-28-35525 SHEET 2 ITEM 2 AND 3 AND UPS EO B747-5310-24767-A.

Part: FRAME — CRACKED (BS 820) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D LT BS 820 FRAME TENSION TIE ATTACHMENT AREA FOUND 1EA HOLE CRACK AT FRAME LAYER APPROX 1/16 INCH IN LENGTH RUNNING DOWNWARD. M/D LT BS 820 FRAME DOUBLER BETWEEN STR 8L TO 12L REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FRAME — CRACKED (BS 880) · airframe 83,907 hrs · 23,132 cycles

RT BS 880 FRAME TENSION TIE ATTACHMENT AREA 4 FASTENER HOLE FOUND CRACK AT FRAME WEB AND FRAME DOUBLER. CRACK LENGTH 0.125 AT DOUBLER AND 0.60 AT WEB. BS880 RT FRAME REPAIRED AS PER RS R53-25-35524 SHEET 1 AND 2 FRAME ATTACH DOUBLER REPLACED AS PER SRM 51-10-01 PG 9 AND RS R53-25-35524 SHEET 1 ITEM 3 AND UPS EO B747-5310-24758-A.

Part: BRACKET — CRACKED (BS 840) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE-C M/D LT BS840 FRAME TENSION TIE ATTACHMENT AREA FOUND 1 EA HOLE CRACK AT AFT BRACKET. M/D LT BS840 FRAME STR10L-10AL SUPPORT BRACKET REPLACED IAW SRM 51-10-01 PG9 AND RS R53-25-35526 ITEM3 AND UPS EO.

Part: FRAME — CRACKED (BS 860) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D RIGHT BS 860 FRAME TENSION TIE ATTACHMENT AREA FOUND 1EA HOLE CRACK AT FRAME WEB THRU THICKNESS RUNNING I/B UPPER. M/D RIGHT BS 860 FRAME REPAIRED BETWEEN STR 7R TO STR 12R AREA AS PER RS R53-25-35522 SHEET 1 ITEM 3 AND UPS EO B747-5310-24739-A.

Part: ATTACH ANGLE — CRACKED (BS 860) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D LEFT BS 860 FRAME TENSION TIE ATTACH AREA FOUND 2EA HOLE CRACK AT FWD CHANNEL. CRACK LENGTH 0.040 INCH. M/D LEFT BS 860 FRAME ATTACH TENSION TIE FWD CHANNEL 2EA HOLE OVERSIZED TO 0.216" AS PER EO B747-5310-23715 APP D, NO CRACK FOUND AFTER HFEC PER NTM PART 6 51-00-00 FIG 16.

Part: TENSION TIE — CRACKED (BS 800) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D RT BS 800 FRAME TENSION TIE ATTACHMENT AREA FOUND FWD TENSION TIE CHANNEL 5 HOLE CRACKED, CRACK LENGTH 0.040". M/D BS 800 RT TENSION TIE FWD AND AFT CHANNEL AT JUST O/B OF RT VERT POST TO RT O/B END AREA AS PER RS R53-25-35525 SHEET 2 ITEM 1 REPAIRED CARRIED OUT. CONTINUE INSPECTION ARE REQUIRED AS PER RS R53-25-35525 REFER NRC 5327 FOR WORKING DETAIL AND REF UPS EO B747-5310-24767-A.

Part: FRAME — CRACKED (BS 780) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D RH BS 780 TENSION TIE ATTACHMENT AREA FOUND 2 HOLES CRACK AT TENSION TIE FWD CHANNEL AND 2 HOLES AT TENSION TIE AFT CHANNEL. CRACK LENGTH 0.060" AND 1/8". M/D BS 780 TENSION TIE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER EO B747-5310-23715-A REFER NRC 5379 FOR WORKING DETAIL.

Part: FRAME — CRACKED (BS 780) · airframe 83,907 hrs · 23,132 cycles

LT BS 780 FRAME TENSION TIE ATTACHMENT AREA FOUND 1 HOLE CRACK AT TENSION TIE FWD CHANNEL AND 1 HOLE CRACK AT TENSION TIE AFT CHANNEL. CRACK LENGTH 1/8" AND 3/16". M/D BS 780 TENSION TIE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER EO B747-5310-23715-A.

Part: TENSION TIE — CRACKED (BS 880) · airframe 83,907 hrs · 23,132 cycles

RT BS 880 FRAME TENSION TIE ATTACHMENT AREA 4 FASTENER HOLE FOUND CRACK AT TENSION TIE AFT CHANNEL CRACK LENGTH 0.030" AND 0.060". BS 880 TENSION TIE AFTER CHANNEL REPLACED AS PER RS R53-25-35524 SHEET 1 ITEM 1. CONTINUE INSPECTION ARE REQUIRED AS PER RS R53-25-35524 REF A. REFER NRC 5326 FOR WORKING DETAIL AND REF UPS EO B747-5310-24758-A.

Part: FRAME — CRACKED (BS 840) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE-C M/D LT BS840 FRAME TENSION TIE ATTACHMENT AREA FOUND 2 EA FASTENER HOLES CRACKED AT FRAME AFT WEB. M/D BS840 FRAME AFT ATTACH WEB LHS AREA REPLACED AND INSTALLED IAW SRM 51-30-02 AND 51-10-01 PG9 AND RS R53-25-35526 ITEM 3 AND UPS EO B747-5310-24756-A.

Part: FRAME — CRACKED (BS 800) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D BS 800 FRAME TENSION TIE ATTACHMENT AREA FOUND FRAME WEB 1 HOLE CRACKED, CRACK LENGTH 0.117". M/D RT BS 800 FRAME TENSION TIE ATTACHMENT AREA HOLE FREEZE PLUG AND INSTALL FASTENER WITH A CAPTURE WASHER AS PER RS R53-25-35525 SHEET 2 ITEM 5 AND 6 AND REF UPS EO B747-5310-24767-A.

Part: FAILSAFE — CRACKED (BS 840) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE-C M/D LT BS840 FRAME TENSION TIE ATTACHMENT AREA FOUND 1 EA HOLE CRACKED AT FAIL SAFE CHORD. M/D LT BS840 FAIL SAFE CHORD REPAIRED AT S6L AND STR7L AREA IAW SRM 51-40-03 FIG2 AND RS R53-25-35526 SHEET 1 ITEM 4 AND UPS EO B747-5310-24756-A.

Part: TIE — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D RT BS820 FRAME TENSION TIE ATTACHMENT AREA FOUND 1EA HOLE CRACK AT AFT CHANNEL RUNNING UPWARD THRU THICKNESS. M/D BS820 RT AFT TENSION TIE AFT CHANNEL REPAIRED AT RT VERTICAL POST TO RT MOST O/B AREA AS PER RS R53-25-35520 CONTINUE INSPECTION REQUIRE AS PER RS R53-25-35520 AND UPS EO B747-5310-24764-A NOT TO EXCEED 3000 FLIGHT CYCLES.

Part: FAILSAFE — CRACKED (BS 880) · airframe 83,907 hrs · 23,132 cycles

RT BS 880 FRAME TENSION TIE ATTACHMENT AREA 1 FASTENER HOLE FOUND CRACK AT FAIL/SAFE CHORD. CRACK LENGTH THROUGH THICKNESS. BS 880 FAIL/SAFE CHORD REPAIRED AT STR 4R AND 5R AREA AS PER SRM 51-40-03 FIG2 AND RS R53-25-35524 SHEET 1 ITEM 4 AND UPS EO B747-5310-24758-A.

Part: SHEAR TIE — CRACKED (BS 880) · airframe 83,907 hrs · 23,132 cycles

RT BS 880 FRAME TENSION TIE ATT AREA 1 FASTENER HOLE FOUND CRACK AT SHEAR CLIP, CRACK LENGTH 0.060." RT BS 880 FRAME STR 9R TIE CLIP REPLACED AS PER SRM 51-10-01 P9.

Part: FRAME — CRACKED (BS 840) · airframe 83,907 hrs · 23,132 cycles

LT BS 840 FRAME TENSION TIE ATTACHMENT AREA FOUND 4 HOLE CRACK AT FRAME FWD WEB. BS 840 LT FRAME STR 8L TO STR 12L AREA FRAME REPAIRED AS PER RS R53-25-35526 AND UPS EO B747-5310-24756-A.

Part: FRAME — CRACKED (BS 860) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D RIGHT BS 860 FRAME TENSION TIE ATTACHMENT AREA FOUND 1EA HOLE CRACK AT TENSION TIE FWD CHANNEL AND 1EA HOLE CRACK AT TENSION TIE AFT CHANNEL CRACK LENGTH 0.030 INCH. M/D RIGHT BS 860 TENSION TIE FWD AND AFT CHANNEL REPAIRED AT RIGHT VERTICAL POST TO RIGHT MOST O/B AREA AS PER RS R53-25-35522 SHEET 1 ITEM 1 PERFORM SUPPLEMENTAL INSPECTIONS AS PER RS R53-25-35522 REF F AND UPS EO B747-5310-23739-A CONTINUE INSP IS REQUIRED.

Part: FRAME — CRACKED (BS 860) · airframe 83,907 hrs · 23,132 cycles

INSPECTION TYPE:C M/D BS 860 LEFT TENSION TIE AFT FACE CHANNEL FOUND CRACK APPROX .25 INCH. M/D BS 860 LEFT TENSION TIE AFT CHANNEL AT JUST O/B OF THE LEFT VERTICAL POST TO LEFT MOST O/B AREA AS PER RS R53-25-35522 SHEET 2 ITEM 1 PERFORM SUPPLMENTAL INSPECTIONS AS PER RS R53-25-35522 REF F AND UPS EO B747-5300-23739-A CONTINUE INSPECTION IS REQUIRED.

Part: TENSION TIE — CRACKED (BS 880) · airframe 83,907 hrs · 23,132 cycles

BS 880 LT TENSION TIE AFT CHANNEL CRACK 1/8 APPROX CRACK LENGTH 1/8". BS 880 TENSION TIE AFT CHANNEL REPLACED AS PER SRM 51-10-01 PG9 AND INSTALLED AS PER RO B747-5310-23715-A CONTINUE INSPECTION ARE REQUIRED AS PER RS R53-25-35524 REF A AND UPS EO B747-5310-24758-A.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

BS 800 RT TENSION TIE AFT CHANNEL FOUND CRACK, CRACK LENGTH 1". BS 800 RT TENSION TIE FWD AND AFT CHANNEL AT JUST O/B OF THE RT VERTICAL POST TO RT O/B END AREA AS PER RS R53-25-35525 SHEET 2 ITEM 1 REPAIR CARRIED OUT. CONTINUE INSPECTION REQUIRED AS PER RS R53-25-35525 AND UPS EO B747-5310-24767-A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 83,907 hrs · 23,132 cycles

FWD CARGO COMPT, MAIN DECK FLOOR SUPPORT BEAM UPPER CHORD LOWER SURFACE FOUND SURFACE CORROSION AT STA 705 TO STA 707 RBL12. CORROSION BLEND OUT 0.025" BY 0.5" BY 3/4" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG14 JUST AT RBL 12 BETWEEN STA 690 AND STA 754.

Part: SKIN — CHAFED (RT WING) · airframe 83,907 hrs · 23,132 cycles

RT WING, LOWER WING EXTERNAL SKIN SURFACE FOUND CHAFING MARKS AT I/B SIDE BODY FAIRING AREA STA 1130 TO STA 1180 WING ROOT JOINT (TOTAL 3 LOCATION) ORI 0.685" 0.598 REMAIN 3" BY 4.5" ORI 0.568" 0.482 REMAIN 4" BY 10", ORI 0.558" 0.506" REMAIN 3.5" BY 10". RT WING LOWER WING EXTERNAL SKIN SMOOTHED OUT REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 SELF CONTAINED SHOT PEEND CARRIED OUT AS PER SOPM 20-10-03 AND HFEC INSPECTION AS PER NTM PART 6 51-00-00 FIG 16. NO CRACK, FOUND BOLT INSTALLED AS PER RS 57-15-35548 AND UPS ENGINEERING FILE NUMBER 747-57-20094.

Part: DOOR — MALFUNCTIONED (RT MLG)

PILOT REPORT, AFTER LANDING BOTH RIGHT PRIM/ALT WING DOOR OPEN LIGHTS CAME ON. WING GEAR DOWNLOCK-OPERATED SEQUENCE VALVE REMOVED PER MM 32-32-04 RODEND BROKEN. INSTALLED WING GEAR DOWN LOCK. OPERATED VALVE PER MM 32-32-04 LEAK CHECK AND OPS CHECK NORMAL. OK FOR SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT)

FOUND 2 EMERG EXIT SIGNS INOP ONE OVER UPPER DECK ESC SLIDE DOOR; OTHER IN THE FWD GALLEY AREA. REACTIVATED EMERG EXIT SIGNS OPS NORMAL. THIS CLEARS M322490.

Part: LINK — CRACKED (NR 3 PYLON) · airframe 82,599 hrs · 22,823 cycles

NR 3 NACELLE REAR ENGINE MOUNT THRUST LINK, CRACK INDICATION REVEALED AT AFT END LUG LOWER EXIT LIMIT. NR 3 ENG REAR MOUNT THRUST LINK REPLACED PER EO B747-7120-22596-A WORK CARRIED OUT ON TASK CARD APPENDIX-H. NR 3 ENG REMOVED AND INSTALLED (FOR ACCESS) AS PER UPS TASK CARD TC 5000.

Part: LINK — CRACKED (NR 4 PYLON) · airframe 82,599 hrs · 22,823 cycles

NR 4 NACELLE REAR ENGINE MOUNT THRUST LINK, CRACK INDICATION REVEALED AT FWD END LUG UPPER EXIT LIMIT. NR 4 ENG REAR MOUNT THRUST LINK REPLACED PER EO B747-7120-22596-A WORK CARRIED OUT ON TASK CARD APPENDIX-I NR 4 ENG REMOVED AND INSTALLED (FOR ACCESS) AS PER UPS TASK CARD TC 5000.

Part: COWLING — OPEN (NR 4)

N/A RTO BTB NR 4 ENG OB CORE COWL OPEN ON TAKE-OFF ROLL. REPLACED OB NR 4 ENG CORE COWLS PER MM 71-10-00.

Part: WIRE — BURNED (BS 960)

WHILE T/S D311541 FOUND WIRE SPLICES BURNED REF WD W1210-014 BYR, W121 0-001 BYR, W1210-014BYR, W1210-024 BYR, W206-022 BYR, AND W1210-024 BYR. NOTE BYR IS BLUE, YELLOW, AND RED WIRE RUNS, SPLICE LOC IS STA 960 LT. REPLACED DAMAGED WIRES AND SPLICES WITH NEW MATERIAL AND OPS CHECK EAC SYSTEM.

Part: LIGHT — INOPERATIVE (COCKPIT)

EMERGENCY EXIT LIGHTS WILL NOT ARM WITH SAFETY SWITCH CLOSED. REPOSITIONED SWITCH ENGAGE HOOP. CHECKS OK.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 81,660 hrs · 22,628 cycles

AD LT NLG WW SIDE PANEL WEB FOUND 2 LOCATIONS CRACKED BETWEEN STA 265 AND 280, WL 160 AND 170. CRACK LENGTH APPROX 1 INCH. LT NLG WW SIDE PANEL WEB REPAIRED AT BETWEEN BS 265 AND 280 WL 160 AND 170 AREA AS PER SRM 53-10-04 FIG 116. SUBSEQUENT INSP NECESSARY FOR CAT B REPAIR. REFER TO SRM 53-10-04 FIG 116 TABLE II FOR REPEAT INSP REQUIREMENT.

Part: RIB — CRACKED (RT WING LE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C RIGHT W ILES 1057.55, 21 V/C FLAP I/B ARM O/B RIB MULTI CRACKS FOUND DURING RIB INSTALLATION WITH RIVET (CRACK LENGTH 1 TO 3 INCH). RIGHT WING 21 VC FLAP I/B ARM O/B RIB TOP FLANGE REPAIRED AS PER HX RS R-57-41-35262 AND UPS EO B747-5740-21822-A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C - BS 2060 - 2140 RBL 98 SEAT TRACK CORROSION FOUND. CORROSION BLEND OUT 0.042 X 1 X 3 EXCEED SRM 53-10-01 FIG 1, LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 2060 - 2140, RBL 90, TIE DOWN TRACK FLANGE FOUND CORROSION CRACK (CRACK LENGTH 1 INCH). TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C M/D BS 1960 RBL 60 FLOOR TRACK SUPPORT FITTING 2EA FOUND CRACKED. SUPPORT FITTINGS REPLACED PER SRM 51-10-01 PG 9.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

BS 1700 LBL 58 - 76 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.045 X 2 X 2 INCH, M/D BS 1700 BL 0 TO LBL 69 FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1700, RBL 11 - 33 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.050 X 2 X 2 EXCEED SRM 53-10-01 FIG 1, LIMIT FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C FX LAP JOINT AT BS 1867 TO 1877 STR 46L FOUND LOSS OF SKIN THICKNESS DUE PREVIOUSLY BLENDED 0.013 X .5 X 4 INCH. LAP JOINT OPENED UP FOR INSPECTION FOR DEFECTS FREE, LAP JOINT REINSTALLED PER HX RS R-53-60-35259 AND UPS EO B747-5330-21779-A.

Part: ATTACH FITTING — CORRODED (FLOORBEAM) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C - BS 2100 RBL 90 - 98 FLOORBEAM ATTACH SPLICE CORROSION FOUND CORROSION BLEND OUT 0.035 X 1 X 2.5 EXCEED SRM 53-10-01 FIG 1, LIMIT. SPLICE REPLACED AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSLEAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 2060 LBL 70 INCH SEAT TRACK CORROSION FOUND. CORROSION BLEND OUT 0.045 X 1 X 2 EXCEED SRM 53-10-01 FIG 1, LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.

Part: ATTACH ANGLE — CRACKED (INTERCOSTAL) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 420 RBL 55 INTERCOSTAL WEB ATTACH ANGLE CRACKED (CRACK LENGTH 1 INCH). ANGLE REPLACED AS PER SRM 51-10-01 PG 9.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 460 RBL 66 - 65 FLOORBEAM WEB CORROSION FOUND. CORROSION BLEND OUT 0.025 X 1 X 4 EXCEED SRM 53-10-01 FIG 1, LIMIT FLOORBEAM WEB REPAIR AS PER SRM 53-10-07 FIG 11.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C M/D- BS 480-500 LBL 68 TIE DOWN TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.039 X 1 X 2 EXCEED SRM 53-10-01 FIG 1, LIMIT TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 480-510 LBL 66 TIE DOWN TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.041 X 1 X 3 EXCEED SRM 53-10-01 FIG 1, LIMIT TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 160 - 180 RBL 13 TIE DOWN TRACK I/B FLANGE & LIP FOUND CORRODED. CORROSION BLEND OUT 0.040 X .5 X 3 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 190 - 240 RBL 11 - 33 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.046 X 1 X 5 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C, BS 440 RBL 55 INTERCOSTAL WEB ATTACH ANGLE CRACKED (CRACK LENGTH .75 INCH). ANGLE REPLACED AS PER SRM 51-10-01 PG 9.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 440 - 460 LBL 86 TIE DOWN TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.044 X 1 X 3 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 480 - 500 LBL 84 TIE DOWN TRACK I/B FLANGE & LIP FOUND CORRODED. CORROSION BLEND OUT 0.047 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 460, RBL 11 - 30 FLOORBEAM WEB CORROSION FOUND. CORROSION BLEND OUT 0.025 X 1 X 3 EXCEED SRM 53-10-01 FIG 1, LIMIT FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C M/D- BS 355 - 360, RBL 72, TIE DOWN TRACK FLANGE FOUND CORROSION CRACK (CRACK LENGTH 1 INCH). TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FITTING — CRACKED (RT WING) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 8 FOUND CRACKED AT SPLICE FITTING APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.

Part: FITTING — CRACKED (RT WING) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 NR 4 HOLE FOUND CRACKED AT INTERNAL SPLICE FITTING APPROX 0.060 INCH. HOLE REWORK PER SB 747-57A2314.

Part: FITTING — CRACKED (RT WING) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 6 FOUND CRACKED AT SPLICE FITTING APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, TIE DOWN TRACK BEAM LWR CHORD BS1000-1002 LBL 33 CORROSION CRACK FOUND. CRACK LENGTH 1 INCH AND CORROSION BLEND OUT 0.060 X 1 X 3 INCH, EXCEED SRM 53-10-01 LIMIT. M/D TIE DOWN TRACK BEAM LOWER CHORD REPAIRED AS PER HX RS R53-45-35264 & ENGINEERING FILE 747-53-20229.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, M/D BS 1500 RBL 5-10 FLOORBEAM FOUND CORROSION. CORROSION BLEND OUT 2 X 2 X 0.060 INCH FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 1.

Part: FITTING — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C M/D BS 1580 LBL 80 TIE DOWN SUPPORT FITTING CORROSION FOUND. CORROSION BLEND OUT 0.030 X 1 X 1 INCH, EXCEED SRM 53-10-01 LIMIT. FITTING REPLACED PER SRM 51-10-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, STA 1330, LBL 65 FLOOR SUPPORT SURFACE CORROSION. CORROSION BLEND OUT 0.035 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, INTERCOSTAL BS 1420, LBL 11-33 HEAVY CORRODED. CORROSION BLEND OUT 0.060 X 1 X 1. EXCEED SRM 53-10-01 LIMIT. INTERCOSTAL REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SUPPORT FITTING — CRACKED (CARGO TRACK) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, TIE DOWN TRACK / BS 1000 B/H VERTICAL SUPPORT FTG CRACKED AT LBL 33 (CRACK LENGTH 1 INCH). M/DECK TIE DOWN TRACK BS 1000 B/H VERTICAL SUPPORT FTG REPLACED AT LBL 33 AREA AS PER SRM 51-10-01 PG 9.

Part: SKIN — CRACKED (RT WING) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 11 FOUND CRACKED AT WING SKIN APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.

Part: FITTING — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1560, RBL 18 TIE DOWN SUPPORT FITTING CORROSION FOUND. CORROSION BLEND OUT 0.020 X 1 X 1 INCH, EXCEED SRM 53-10-01 FIG 1. LIMIT FITTING REPLACED PER SRM 51-10-01.

Part: SKIN — CRACKED (R3 DOOR) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1306 BETWEEN S24-25R R3 DOOR SKIN FOUND CRACK (CRACK LENGTH 1.25 INCH). M/D BS 1306 BETWEEN STR 24R-25R DOOR 3R SKIN REPAIRED PER SRM 52-00-03 FIG 4.

Part: SKIN — CRACKED (RT WING) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 FOUND HOLE NR 12 CRACKED AT WING SKIN APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1500 - 1560, LBL 98 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.045 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A AT BS 1480-1570 LBL 98 AREA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C M/D- BS 1600 - 1640 RBL 98 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.040 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. SEAT TRACK REPAIR AS PER SRM 53-10-05 FIG 1A.

Part: FITTING — CRACKED (RT WING) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 5 FOUND CRACKED .125 INCH. HOLE REWORKED PER BSB 747-57A2314.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C M/D- BS 1580 TO 1600 LBL 98 SEAT TRACK CRACKED (CRACK LENGTH 1 INCH). SEAT TRACK REPAIRED FROM BS 1570 TO BS 1630 LBL 98 AS PER SRM 53-10-05 FIG 1A.

Part: SKIN — CRACKED (RT WING) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C, RHW REAR SPAR UPPER SPLICE FITTING AT BS 1241 FOUND CRACKED AT HOLE NR 7 AT SKIN APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1480 - 1500 RBL 34, TIE DOWN TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.040 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1294, RBL 55-75 FLOOR SUPPORT U-CHANNEL UPPER FACE CORROSION FOUND CORROSION BLEND OUT 0.035 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOOR SUPPORT U-CHANNEL REPLACED AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C, BS 1580-1600 LBL 33 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.045 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPLACED AT BS 1480 TO BS 1600 LBL 33 AS PER SRM 51-10-01 PG 9.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1440, RBL 80-99 FLOOR SUPPORT U-CHANNEL ANCHOR NUTS AREA UPPER AND LOWER FACE FOUND CORROSION. CORROSION BLEND OUT 0.045 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOOR SUPPORT U-CHANNEL REPLACED AS PER SRM 51-10-01 PG 9.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, INTERCOSTAL BS 1300, LBL 11-33 RT O/B END CRACKED AT LWR SURFACE (CRACK LENGTH .75 INCH). INTERCOSTAL REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1500, RBL 78 TIE DOWN SUPPORT FITTING CORROSION FOUND. CORROSION BLEND OUT 0.025 X 1 X 1 EXCEED SRM 53-10-01 LIMIT. FITTING REPLACED PER SRM 51-10-01.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1660, RBL 78 TIE DOWN TRACK I/B FLANGE LWR FACE FOUND CORRODED. CORROSION BLEND OUT 0.035 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPAIR AS PER SRM 53-10-05 FIG 1A.

Part: FLOOR SUPPORT — CRACKED (FUSLEAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, STN 1094-1100 LBL 75 LONGITUDINAL FLOOR SUPPORT WEB & LOWER CHORD FOUND CRACKED (CRACK LENGTH 3.5 INCH). SUPPORT WEB REPLACED PER SRM 51-10-01 PG 9. LOWER CHORD REPAIRED PER HAECO RS R53-45-35260 & UPS ENG'R FILE 747-53-20227.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, SEAT TRACK BS 1497 - 1500 LBL 33 RT FLANGE CORRODED. CORROSION BLEND OUT 0.030 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1. TIE DOWN TRACK REPLACED AT BS 1480 TO BS 1600 LBL 33 AS PER SRM 51-10-01 PG 9.

Part: SKIN — CRACKED (LT WING) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, LT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 11 FOUND CRACKED AT WING SKIN APPROX 0.060 INCH. HOLE REWORKED AT BSB 747-57A2314.

Part: FLOORBEAM — CORRODED (M/D) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C - STA 1500, LBL 65 FLOORBEAM UPPER SURFACE CORROSION. CORROSION BLEND OUT 0.050 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1140 - 1160, RBL 34 TIE DOWN TRACK FLANGE FOUND CRACKED (CRACK LENGTH 2.75 INCH). BS 1070 TO BS 1210 RBL 34 INCH TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 34.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 996 TO 999 RBL 75 SEAT TRACK CRACKED (CRACK LENGTH 1.5 INCH). TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A AT BS 930 TO BS 1000 RBL 75 AREA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1110 RBL 75 SEAT TRACK WEB ATTACH STIFFENER FOUND CORRODED. CORROSION BLEND OUT 0.020 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CRACKED (FUSLEAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 994 TO BS 995 RBL 98 SEAT TRACK CRACKED (CRACK LENGTH 1 INCH). M/ DECK BS 970 TO BS 995 RBL 98 TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1480 BULKHEAD APU DUCT CUTOUT FOUND 3 FASTENER HOLES CRACKED. BS 1480 BULKHEAD REPAIRED PER SB 747-53-2309 UPS EO B747-5310-3100-C & DWG 144U2602.

Part: ATTACH BRACKET — CORRODED (FUSLEAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1020, RBL 75 FLOOR SUPPORT ATTACH BRACKET CORROSION FOUND. CORROSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. BRACKET REPLACED AS PER SRM 51-10-01 PG 9.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C M/D BS 1000 RBL 11 SEAT TRACK END SUPPORT FITTING FOUND CRACKED. SUPPORT FITTING REPLACED PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1165, RBL 75 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.030 X 1 X 1 EXCEED SRM 53-10-01 FIG 1, LIMIT SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, BS 1300, LBL 11- RBL 11, FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.035 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.

Part: WEB — CRACKED (NR 2 PYLON) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, NR 2 PYLON REAR LOWER WEB AT NAC STN 212 I/B EDGE UPPER SURFACE RIVETS HOLES FOUND CRACKED. NAC STN 212 REAR LOWER WEB REPAIRED PER SRM 54-10-03 FIG 2.

Part: RIB — CRACKED (RT WING LE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C RIGHT WING ILES 1057.55, 21 V/C FLAP I/B ARM O/B RIB FWD VERTICAL MOUNTING ATTACH FASTENER HOLES CRACKED (CRACK LENGTH 1 INCH). RIGHT WING 21 VC FLAP I/B ARM O/B RIB FWD VERTICAL FLANGE REPAIRED AS PER HX RS R-57-41-35262 AND UPS EO B747-5740-21822-A.

Part: RIB — CRACKED (RT WING LE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C RIGHT WING 17 VC FLAP O/B ARM O/B RIB MOST FWD FASTENER HOLE CRACKED (CRACK LENGTH 1.25 INCH). RIGHT WING 17 VC FLAP O/B ARM O/B RIB FWD FLANGE FASTENER HOLES REPAIRED AS PER HX RS R57-41-35263 AND UPS EO B747-5740-21796-A.

Part: RIB — CRACKED (RT WING LE) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE:C RIGHT WING 20VC FLAP I/B ARM O/B RIB I/B FACE AT ROTARY ACTUATOR AFT AREA FOUND CRACKED, CRACK LENGTH .5 INCH. RIGHT WING 20VC FLAP I/B ARM O/B RIB I/B FACE REPAIRED AS PER HX RS R57-41-35254 WITH CRACKED AREA TRIMMED OFF & INSPECTED BY NDT. NO CRACK FOUND & EO B747-5740-21781-A.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 80,944 hrs · 22,482 cycles

INSPECTION TYPE: C, LT BODY L/G W/W STA 1480 BULKHEAD APU BLEED AIR DUCT CUT OUT FOUND CRACKED AT LEFT O/B SIDE LBL 100. CRACK LENGTH 2.5 INCH, LT BODY L/G W/W BS 1480 BULKHEAD APU BLEED AIR DUCT CUTOUT REPAIRED AS PER SB B747-53-2309 R1, EO B747-5310-3100-C AND DWG 144U2602.

Part: PUMP — INOPERATIVE (NR 2 ENGINE)

CREW SHUTDOWN NR 2 ENGINE IN FLIGHT DUE TO ENGINE NOT RESPONDING. CREW RESTARTED AND ENGINE PERFORMED NORMALLY. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL PER MM 73-21-01 AND 73-11-01. PERFORMED ADJ AND TEST PER MM 71-00-00 OPS CK LEAK CK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

CREW SERVICE DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED AS NEEDED, OPS CK OK.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

AFT EMERGENCY EXIT LIGHT INOP AT ENTRY DOOR. RELAMPED, OP'S CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

EMERG EXIT LIGHTS INOP. FOUND BROKEN LT ASSY AT POS 580 RT R/R'D LT ASSY, C/B STILL OPENS. CONTROL PANEL NO HELP, FOUND 1 OHM TO GND AT D1561JP1N6. ACCOMPLISHED EO B747-3350-20943-A. LTS TEST GOOD.

Part: ENGINE — FLAMED OUT (NR 2)

DURING CRUISE NR 2 ENG FLAMED OUT AT 37K DURING CROSSFEED FROM NR 3 TANK. OIL PRESS REMAINED 10PSI, N1 25 PERCENT, N2 28 PERCENT ENG WAS SHUTDOWN FOR APPROX 25MIN. CREW ATTEMPTED RESTART AT 33K PER QRH - NO JOY, CREW COMPLETED ENG SEVERE DAMAGE CHECKLIST. COMPLIED WITH MM 71-00-42 AND MM 72-00-00 NO DEFECTS NOTED. REF. ITEM 3 LOGPG 195499 SUSPECT CROSSFEED VALVE AT FAULT RAN ENG NR 2 NO DEFECTS NOTED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

EMERGENCY LIGHTS UNARMED LAMPS OUT PILOT OVERHEAD RELAMPED 2 NR 387 BULBS FOR UNARMED STATUS ON EMERGENCY LIGHT PANEL.

Part: ENGINE — FLAMED OUT (NR 4)

AT 1330Z INTO FLIGHT NR 4 ENG FLAMED OUT. COMPLY WITHIN FLIGHT ENGINE FAILURE/SHUTDOWN CK LIST. TRIED INFLIGHT START CK LIST AS THE ENG INDICATION WAS NORMAL WITH EXCEPTION OF NR 4 OIL TEMP BEING AROUND 100 DEG. REMOVED AND REPLACED MAIN FILTER, INSPECTED PIR, PTT2 AND PT2 LINES FOR LEAKS AND SECURITY. VERIFIED FUEL PUMP PRESSURE (700 LBS) FUEL FLOW AT START NORMAL, ENGINE A/I OPS NORMAL MM 71-00-46, 71-00-42. RAN NR 4 ENGINE TO 1.51 EPR 18.8 F/F, 95 PERCENT N1 818 EGT, NO DEFECTS.

Part: REGULATOR — INOPERATIVE (OXYGEN SYSTEM)

02 REGULATOR DOES NOT SHOW FLOW INDICATION IN NORMAL/ON POSITION R/R S/O REGULATOR ASSY, IAW MM 35-11-07 OP CKD OK

Part: RIB — CRACKED (RT WING) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C RT WING LE NR 18 VC FLAP IB ARM OB RIB AT ILES 802 CRACKED. STOP DRILLED CRACK TRIMMED OFF STIFFENER THE REPAIR FTG AND THE REPAIR STRAP INSTALLED IAW HXRS NR R57-41-35055 AND EO B747-5740-19118-A ISSUED FOR REPLACE THE RIB WITHIN 18 MONTHS AND PERFORM REPEAT DETAIL VISUAL INSP. AT 77 DAY INTERVALS FOR GENERAL REPAIR INTEGRITY AND CRACK PROPAGATION.

Part: SKIN — CORRODED (BS1241 RBL24) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C INSTALL A NEW REPAIR DOUBLER AT BS 1241 - RBL 24 AS PER TELE UPS-HKG-03-001 FOR ACCOMPLISH SB 747-51A2054. CORROSION REMOVED AT RBL 16 AREA EXCEEDED SRM 53-10-01 FIG 1 LIMITATION AFTER DOUBLER REMOVED CORROSION BLEND OUT 0.045 INCH MAX NEW REPAIR CARRIED OUT AS PER RS R-53-48-35046 AT BS 1241 RBL 11.33 TO RBL 33.99 AREA AND EO B747-5310-16853.

Part: RIB — CRACKED (RT WING) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C RT WING NR 3 NACELLE RIB POST 2EA ATT HOLES FOUND CRACK INDICATION AT FRONT SPAR WEB. NR 3 NACELLE RIB REPAIRED AS PER B747-5720-11421-F AND RT FRONT SPAR WEB REPLACED AS PER B747-5720-11421-F

Part: RIB — CRACKED (LT WING) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C LT WING NR 2 NACELLE RIB POST 4EA ATT HOLES FOUND CRACK INDICATIONS AT FRONT SPAR WEB. NR 2 NACELLE RIB REPLACED AS PER EO B747-5720-11421-F AND LH FRONT SPAR WEB REPLACED AS PER EO B747-5720-11421-F

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C M/D: BS 1820 FRAME SHEAR TIE FOUND CRACKED AT LOWER RIVET HOLE AS MARKED BETWEEN S22R AND S23R. M/D- BS 1820 FRAME SHEAR TIE BETWEEN S22R - S23R REPLACED IAW SRM 51-10-01 P.8

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C M/D STA 1901 STR 23R TIE CLIP FOUND CRACKED. M/D STA 1901 STR 23R TIE CLIP REPLACED IAW SRM 51-10-01 P8.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C FWD CARGO COMPT - LT STA 740 - STA 820 STRINGER 44 FOUND CRACKED (3 LOCATION). FWD CARGO COMPT - LT STA 740 - STA 820 STR 44L REPAIRED PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C RT TUNNEL STA 320 - STA 340 STRINGER 42 FOUND CRACKED. STRINGER REPLACED AS PER SRM 51-10-01 PG 8.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C RT TUNNEL TORQUE BOX STA 340 IN BETWEEN STR 42 AND STA 43 CHORD FOUND CORRODED. THE CORD REPLACED IAW SRM 51-10-01 P8. (CORROSION REMOVED - BLEND OUT DEPTH 0.050 WIDTH 1 INCH LENGTH 1 INCH OUT OF SRM 53-10-01 FIG 1 LIMITS.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C FWD CARGO COMPT - RT STA 958-STA 960 STRINGER 44 FOUND CORROSION CRACKED. FORWARD CARGO COMPT - RT STA 950 - STA 970 S44 STRINGER REPAIRED IAW SRM 53-10-03 FIG.1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C FWD CARGO COMPT- LT STA 780 - STA 800 STRINGER 47L FOUND CORROSION. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1 DUE TO CORROSION CRACK LENTH WAS 1-45 INCH LENGTH WHICH EXCEEDED SRM 53-10-01 FIG 1 LIMITATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C FESC-LT STA 410 LBL 8- LBL 16 WEB FOUND CRACKED. FESC LT STA 410 LBL 8- LBL 16 FRAME WEB CRACK TRIMMED OFF IAW SRM 51-10-01 AND REPROTECTED IAW SRM 51-10-02.

Part: SKIN — DAMAGED (LH STR 19) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE: C, FX SKIN STR 19L STA 2280 - 2285 FOUND .25 INCH COUNTERSINK FASTENERS AT TOP ROW. FX SKIN AT STA 2280 - 2285 STR 19L AREA SKIN REPAIRED PER SRM 53-30-03 FIGURE 17. SKIN TRIMMED OFF PER SRM 53-30-03 FIG 17.

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE: C, NR 2 PYLON REAR MOUNT BULKHEAD FOUND CRACKED AT FORWARD AND AFT FRAME WEB AT STA 221. NR 2 PYLON REAR MOUNT BULKHEAD REPAIRED PER HX RS R54-53-35045 AND UPS ENGINEERING FILE NUMBER 747-54-20039.

Part: SUPPORT — CORRODED (ACTUATOR MOUNT) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE: C, LT WING NR 9 VC FLAP I/B ARM O/B ROTARY ACTUATOR SUPPORT RIB ACTUATOR MOUNTING SCREW HOLE NR 1 AND NR 4 FOUND SCRATCH MARK (LOOKING O/B AND COUNT FROM TOP CW). SCREW HOLE NR 4 CORROSION REMOVED IAW SRM 57-20-03, SCREW HOLE NR 1 REPAIRED IAW RS R57-41-35047 AND EO B747-5740-19059-A. REPEAT INSP REQ AT EVERY C-CHECK INTERVAL, NOT TO EXCEED 18 MONTHS IAW EO B747-5740-19059-A.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C M/D- BS 1780 STR 22R-23R FRAME ATT ANGLE CRACKED. ANGLE REPLACED IAW SRM 51-10-01 P 8.

Part: REVEAL — CRACKED (CABIN) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C M/D - R5 DOOR FWD CUTOUT BS 2231 BETWEEN 15R AND 16R STRINGER AREA UPPER REVEAL FOUND CRACKED. REVEAL PANEL REPAIRED AS PER SRM 53-10-04 FIG 91.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C NOSE WHEEL WELL COMPARTMENT TUNNEL - AT STA 240 CEILING AREA THE CABIN HORI FLOOR SUPPORT WEB AREA AFT SURFACE CORROSION FOUND AT BL 0. FLOOR SUPT WEB REPAIRED IAW SRM 51-40-02 FIG.1 DUE TO BLENDED DEPTH 0.043 INCH, WIDTH .7500 INCH AND LENGTH 2 INCH EXCEEDS SRM 53-10-01 FIG.1 LIMITATION.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE: C, FX - BODY FAIRING SUPPORT FRAME FOUND CORROSION AT STA 920 FROM BL 0 - LBL 10. CORROSION BLEND OUT 0.050 X 1 X 1 INCH. BODY FAIRING SUPPORT FRAME REPAIRED AS PER SRM 53-50-04 FIG 2.

Part: WEB — CRACKED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE: C, M/D - BS 360 - 380 STR 26R RBL 98 - 104 SUPPORT WEB CRACKED. SUPPORT WEB REPAIRED AS PER SRM 51-40-02.

Part: SUPPORT — CORRODED (FAIRING) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE: C, FX - BODY FAIRING SUPPORT FOUND SURFACE CORR AT STA 920 FROM LBL 30 - RBL 20. BODY FRG SUPPORTT COR REMOVED AT LBL 25 TO LBL 30 AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 WITHIN SRM 53-50-01 FIG 5 LIMITATION, BL 0 TO LBL 26 SUPPORT REPAIRED AS PER SRM 53-50-04 FIG 2 DUE TO EXCEEDED LIMITATION AS PER SRM 53-50-01 FIG 5 AFTER COR BLEND OUT 0.050 X 1 X 1 INCH BL 0 TO RBL 20 SUPPORTT REPAIRED REF NRC 5856 DETAIL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C M/D- BS 380 STR 25L FRAME CRACKED. FRAME REPLACED AS PER SB747-53-2272 DWG 624U0003 FROM S23L TO S44L AT BS380.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C NOSE WHEEL WELL COMPARTMENT TUNNEL - AT STA 240 CEILING AREA THE CABIN FLOOR SUPPORT BEAM FWD AND AFT LOWER AREA CORROSION FOUND FROM BL0 - LBL 24. FLOOR SUPPORT BEAM REPAIRED AS IAW SRM 51-40-04 FIG. 1 DUE TO COR BLENDED AREA DEPTH 0.050 INCH, WIDTH 1 INCH AND LENGTH 4 INCHES EXCEEDED SRM 53-10-01 FIG.1 LIMITATION.

Part: BULKHEAD — CRACKED (NR 1 PYLON) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C NR 1 PYLON REAR MOUNT BULKHEAD CRACK FOUND AT I/B FWD WEB EDGE NAS 221. NR 1 PYLON REAR MOUNT BULKHEAD REPAIRED IAW HX RS R54-53-35042 AND UPS ENGINEERING FILE NUMBER 747-54-20038.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE: C, FX - BODY FAIRING SUPPORT FRAME FOUND SURFACE CORR AT STA 1050, RBL 22 - 25 AND RBL 50 - 60 AS MARK. FX - BODY FAIRING SUPPORT FRAME STA 1050 RBL 22 - 25 SURFACE CORROSION AREA CORROSION CLEANED AS PER SRM 51-10-01 AND REPROTECTED AS PER SRM 51-10-02 AND BODY FAIRING SUPPORT STA 1050 RBL 50 - 60 AREA REPAIRED AS PER SRM 51-40-04 FIG 1. CORROSION BLEND OUT 0.050 X 1 X 1 WORK DETAIL REFER ATTACH CWS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE: C, FX - BODY FAIRING SUPPORT FRAME FOUND SURFACE CORROSION AT STA 920 FROM RBL 20 - 50. CORROSION BLEND OUT 0.056 X 1 X 1.5 INCH. BODY FAIRING SUPPORT FRAME REPAIRED AS PER SRM 53-50-04 FIG 2 AT STA 920 FROM RBL 0 - RBL 30 AREA. BODY FAIRING SUPPORT CORROSION AREA STA 920 RBL 30 - RBL 50 CORROSION CLEANED AND REPROTECTED AS PER SRM 51-10-01 AND SRM 51-10-02 WITHIN SRM 53-50-01 FIG 5 LIMIT.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C NLG W/W BOX STRUCTURE LT BS 300 VERTICAL BEAM WEB FOUND APPROX .125 INCH CRACK AT LOWER STAND OFF HOLE BETWEEN 1ST AND 2ND STIFFENER CLIP (COUNT FROM TOP). VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 PG 8.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 77,950 hrs · 21,828 cycles

INSPECTION TYPE:C NLG W/W BOX STRUCTURE LT BS 320 VERTICAL BEAM WEB FOUND APPROX .125 INCH CRACK AT LOWER STAND OFF HOLE BETWEEN 1ST AND 2ND STAND OFF HOLE (COUNT FROM TOP). VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 PG 8.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A MAIN DECK CARGO AREA HAS AFT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY EXIT LIGHT ASSY OPS CKS OK AS IAW MM 33-51-07.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

MAIN DECK AT STA 390 AND DOOR SILL FOR L1 EMERGENCY LIGHT DIMMED. REMOVED AND REPLACED EMERGENCY BATTERY, OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN)

FWD MAIN DECK RT STA 340 EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY, OPS CHECK OK.

Part: SIGN — INOPERATIVE (CABIN)

EMERGENCY EXIT SIGN ABOVE RT UPPER DOOR INOP REMOVED AND REPLACED LIGHT ASSY

Part: SIGN — INOPERATIVE (CABIN)

EMERGENCY EXIT SIGN ABOVE R/H DOOR UPPER DECK INOPERATIVE. DEFERRED EMERGENCY EXIT SIGN FOR UPPER DECK RT DOOR PER MEL 33-15. DEF #246761.REMOVED AND REPLACED LIGHT ASSY. OPS CHECKS GOOD

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO COMPT - BS 710 STR 29R STRINGER CORROSION FOUND. BS 670 - 740 STR STRINGER REPLACED AS PER SRM 51-10-01 PG 8.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO COMPT - AFTER STRINGER SPLICE REMOVED STRINGER END FOUND CRACK AT BS 740 STR 28R. STRINGER REPLACED AS PER SRM 51-10-01 PG 8.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO COMPT - BS 700 S28R WEB I/B ATT ANGLE CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS. FWD CARGO COMPT BS 690-730 S28R WEB I/B ATT ANGLE REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO COMPT - BS 700 S28R AREA FRAME I/B CHORD CORRODED. BS 700 RIGHT FRAME CRACK REPAIR AT S28R AS PER RS R-53-22-34798 & EA 747-53-20067.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C RT WLG CANTED BULKHEAD LWR CAP FOUND CORROSION AT RBL 53 BS 1241 TO 1241. THIS REPAIR IS CONSIDERED TIME - LIMITED FOR 24 MONTHS UNTIL AN IMPROVED DRAINAGE MODIFICATION CAN BE INSTALLED IAW BOEING SERVICE BULLETIN 747-51A2054 REV 1 AS PER UPS EO B747-5310-16853-A.

Part: BULKHEAD — CRACKED (NR 2 PYLON) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT AFT WEB APPROX 4 O'CLOCK (VIEW LOOKING FWD). NR 2 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER INSTRUCTION ON HAECO REPAIR SCHEME R-54-53-34787.

Part: RIB — CRACKED (L/E FLAP) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C DURING LHW NR 9 L/E FLAP GREASE LUBE AS NR 3 ROTARY ACTUATOR (COUNT FROM O/B) REMOVED, L/E RIB O/B FWD AREA FOUND CORROSION AT ILES 800. L/E RIB AT ILES 800 IS REPLACED AS PER SRM 51-10-01. CORROSION FOUND CRACKED THROUGH AT 2 LOCATIONS.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 1840 - 1860 RT BETWEEN S-20R AND S-22R WINDOW FORGINGS FOUND CORRODED AFTER NRC RECTIFICATION. REPAIR WINDOW FORGING AT M/D BS 1840 - 1860 RT BTN S20R - 22R.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 1220 LBL 96 LONGITUDINAL FLOOR SUPPORT TRACK SUPPORT WEB BOTTOM -T- CHORD HEAVY CORROSION. FLOOR LONGITUDINAL TRACK BOTTOM CHORD REPAIRED PER RS R53-45-34793. BEYOND SRM 53-10-01 ALLOWABLE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 1241 - 1265 RBL 34 SLOPE CANTED BULKHEAD LONGITUDINAL FLOOR TRACK SUPPORT BOTTOM -T- CHORD FINDING HEAVILY CORRODED. M/D BS 1241 - 1265 RBL 34 LONGITUDINAL FLOOR TRACK BOTTOM -T- CHORD REPLACED IAW SRM 51-10-01 PAGE 8.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D BS 2178 LT NR 1 STRINGER END CRACKED. BS 2178 S1L, STRINGER SEGMENT REPAIR AS PER SRM 53-10-03 FIG 4 AND FINISHED PAINT TOUCH UP PER MM 51-24-11.

Part: FITTING — CRACKED (CENTER WING) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C CRACK REVEAL ON THE FASTENER HOLE OF THE FITTING INSIDE WING CENTER TANK COMMON TO LT SIDE BATHTUB FITTING RUNNING UPWARD APPROX .125" LONG. LT SIDE STA 983 S38L INSIDE DRY BAY BATHTUB DRAG FITTING REPLACED AS PER SRM 51-30-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D BS 150-160 LBL 50 MOST O/B FLOOR SUPPORT CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C AFT CARGO COMPT - BS 1800 S-34R AREA FRAME ATT STIFFENER CORRODED. AFT CARGO COMPT BS 1800 S-34R AREA FRAME ATT STIFFENER REPLACED AS PER SRM 51-10-01 PG 8.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C LT BS 340 UPPER DECK FLOORBEAM ONE EACH FASTENER HOLE CRACK REVEALED AT UPPER CHORD LAYER THROUGH THICKNESS. U/D BS 340 FLOORBEAM UPPER CHORD PARTIALLY REPLACED FROM LBL 35 TO LT MOST O/B IAW HAECO RS R-53-15-34801 AND DWG 141U0044 SHEET 2 FOR REPAIR PARTS INSTALLATION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - NLG PRESSURE DECK UPPER SURFACE ANGLE FOUND CRACKED. ANGLE REPLACED AS PER SRM 51-10-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - NLG PRESSURE DECK UPPER SURFACE ANGLE FOUND CRACKED. ANGLE REPLACED AS PER SRM 51-10-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C 2 EACH FASTENER HOLES FOUND CRACK ON LT BS 980 S38L SKIN PANEL. FX BS 980 LT STR SKIN REPAIRED AS PER SRM 53-30-03 FIG 60 AT BS 975 - 983 LT BETWEEN STR 37 - 39L.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C 3 EA FASTENER HOLES FOUND CRACK ON THE BATH TUB FITTING OF LT SIDE BS 980 STR 38L. LT STA 980 S38L BATHTUB FITTING REPAIRED AS PER RS R53-23-34791. A PERMANENT REPAIR TO THE BATHTUB FITTING IS TO BE ACCOMPLISHED WITHIN 18 MONTHS. CONTINUE INSPECTION PLANS ON THE LT SIDE PER SB B747-53A2362 & SB 747-53A2444 AS PER UPS EO B747-5310-16873-A.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C, BULK CARGO BS 2120 RT FRAME WEB FOUND CORROSION BETWEEN STR 28R AND STR 29R. BS 2120 S28R S29R FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 39. BLEND OUT CORROSION DEPTH 0.030', WIDTH 1', LENGTH 1'.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C BULK CARGO - BS 2060 - 2080 RT STR 28 FOUND CORRODED. BS 2060 - BS 2090 S28R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C RT MLG W/W CANTED BULKHEAD LOWER CAP ANGLE UPPER EDGE CORRODED AT RBL 78 - 83 BS 1241 - 1242. THIS REPAIR IS CONSIDERED TIME - LIMITED FOR 24 MONTHS UNTIL AN IMPROVED DRAIN AGE MODIFICATION CAN BE INSTALLED IAW BOEING SERVICE BULLETIN 747-51A2054 REV 1 AS PER UPS EO B747-5310-16853-A.

Part: BULKHEAD — CORRODED (FUSELAEG) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 2141 RBL 76 CANT PRESSURE DECK FOUND CORRODED. BOND SKIN TRIMMED AS PER SRM 51-10-01. REPAIR PARTS FABRICATED AS PER RS R53-48-34796.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C RT BS 983 STR 38R LOWER DRAG SPLICE FITTING FOUND 1 EACH FASTENER HOLE CRACKED APPROX .125 INCH AS MARKED. RT BS 983 STR 38R LOWER DRAG SPLICE FITTING REPLACED AS PER SRM 51-10-01 AND BOEING SB 747-53-2064.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C LT MLG - BS 1241 BULKHEAD OVERRIDE JETTISON PUMP BONDING STRIP ATTACHMENT CORRODED. AS RS R-53-43-34797 IS TIME LIMITED REPAIR FOR 18 MONTHS, WAN 681694 RAISED AS FOLLOW - UP TO CARRY OUT PERMANENT REPAIR AS PER EO B747-5710-16852-A WITHIN 18 MONTHS OR THE NEXT C-CHECK WHICHEVER IS EARLIER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D - BS 780 S-7L AND S-8L FRAME FOUND CRACKED. FRAME REPAIRED IAW SRM 53-10-04 FIG 54.

Part: SPAR — CRACKED (CENTER WING) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C RT BS 990 FRONT SPAR WEB ONE EACH FASTENER HOLE COMMON TO BATH TUB FITTING CRACK REVEALED AT FRONT SPAR WEB LAYER FOR DETAIL PLS REFER ATTACHED SKETCH. RT BS 990 FRONT SPAR WEB CRACKED HOLE OVERSIZED TO 0.660" AND FREEZE PLUG INSTALLED AND DRILLED AS PER BS R53-43-34792.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C BS 2240 BETWEEN S49L AND S50L FRAME CRACK. FRAME REPAIRED AS PER SRM 53-10-04 FIG 71.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - L1 DOOR FWD FRAME FOUND CRACKED AT LOWER HINGE AREA. FRAME REPAIRED AS PER SRM 52-10-02 FIG 12.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C BULK CARGO - BS 2040 RT FRAME ATT TIE CLIP FOUND CORRODED AT STR 32R. TIE CLIP REPLACED AS PER SRM 51-10-01.

Part: WEB — CRACKED (R3 DOOR) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - R3 DOOR INNER WEB CRACKED. INNER WEB REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - R3 DOOR CUTOUT STOP FITTING FOUND CRACKED (NR 5). R3 DOOR FWD CUTOUT NR 5 STOP FITTING REPLACED AS PER SRM 51-10-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D - BS 960 S-5R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 54.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 780 S-7R AND S-8R FRAME FOUND CRACK. FRAME REPAIRED IAW SRM 53-10-04 FIG 54.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D - BS 760 STR 6-8R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - R3 DOOR FWD CUTOUT LOWER REVEAL FOUND DENT HOLE. R3 DOOR FWD CUTOUT LOWER REVEAL REPLACED AS PER SRM 51-10-01 PG 8.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C AFT CARGO - BS 1520 RTS FRAME ATT TIE CLIP FOUND CORROSION AT STR 29R. AFT CARGO - BS 1520 STR 29R TIE CLIP REPLACED AS PER SRM 51-10-01 PG 8.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 1241 RBL 76 CANT PRESSURE DECK FOUND CORRODED. BLEND OUT CORROSION DEPTH 0.015, WIDTH 4", LENGTH 6". THE BONDED DOUBLER REPAIRED AS PER HAECO RS R-53-48-34796. THIS REPAIR IS CONSIDERED TIME-LIMITED TO 24 MONTHS UNTIL AN IMPROVED DRAINAGE MOD SHOULD BE PERFORMED IAW BOEING SB 747-51A2054 REV 1 AS PER UPS EO B747-5310-16853-A.

Part: DOOR FRAME — CRACKED (R3 DOOR) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - R3 DOOR FWD FRAME FOUND CRACKED AT NR 1 STOP FITTING AREA. FRAME REPAIRED AS PER SRM 52-10-02 FIG 8.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C RT WLG W/W CANTED BULKHEAD WEB CORRODED AROUND DRAIN HOSE ADAPTOR AT BS 1241 - 1243 RBL 36 - 39. REPAIRED AS PER HAECO RS R-53-48-34796. THE REPAIR IS CONSIDERED TIME-LIMITED TO 24 MONTHS UNTIL AN IMPROVED DRAINAGE MODIFICATION CAN BE INSTALLED IAW BOEING SB 747-51A2054 REV 1 AS PER UPS EO B747-5310-16853-A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 1220 LBL 119 BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO DOOR BS 575 BETWEEN NR 1, NR 3 FRAME UPPER MASTER LATCH T/T INTERIOR AREA FOUND CORROSION (COUNT FROM FWD) AS MARKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT NOT WITHIN SRM LIMIT 52-00-02 FIG 1. FWD CARGO DOOR INTERIOR LWR BEAM REPAIRED AT BS 575 BETWEEN NR 1 & NR 2 FRAME AS PER SRM 51-40-02 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D - BS 990 S-9L STRINGER END SPLICE AREA FOUND CRACKED. STRINGER REPAIRED SRM 53-10-03 FIG 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C RT BS 990 AT STR 38 RING CHORD ONE EACH FASTENER HOLE FOUND TWO CRACKS AS MARKED. FOR DETAIL PLS REFER ATTACH SKETCH. LOWER CHORD SEGMENT REPAIRED PER SB 747-53-2362 FIG 9 AND CHORD LOCAL FABRICATED PER RS 53-43-34792 AREA REPAIRED FOR RT ONLY A PERMANENT REPAIR IS REQUIRED WITHIN 18 MONTHS OR NEXT C-CHECK WHICHEVER COMES FIRST.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C RT MLG W/W OVERRIDE JETTISON PUMP CUTOUT AND BONDING ATTACHMENT CORROSION FOUND AT STA 1241 RBL 90 - 96 WL 140 - 148. AS PER R-53-43-34797 IS THE LIMITED REPAIR FOR 18 MONTHS, WAN 681694 RAISED AS FOLLOW - UP TO CARRY OUT PERMANENT REPAIR AS PER EO B747-5710-16852-A WITHIN 18 MONTHS OR THE NEXT C-CHECK WHICHEVER IS EARLIER.

Part: STOP FITTING — CRACKED (R1 DOOR) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C R1 DOOR FWD LOWER STOP FITTING FOUND CRACKED. R1 DOOR FWD LOWER STOP FITTING REPLACED AS PER SRM 51-10-01 PG 8.

Part: FITTING — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C HEAVY CORROSION REVEALED AT UPPER AND LOWER FASTENER HOLES OF BATH TUB FITTING AT BS 990 S38R. PLEASE REFER FIG. RT SIDE STA 980 S38R BATHTUB FITTING PERMANENT REPAIR CARRIED OUT AS PER RS R53-23-34791. CONTINUE INSPECTION PLANS ON THE RT SIDE PER SB 747-53A2362 AND SB 747-53A2444 AS PER UPS EO B747-5310-16873-A.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 75,255 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - R2 DOOR FWD FRAME FOUND CRACKED AT LOWER HINGE CUTOUT AREA. R2 DOOR FWD FRAME LOWER HINGE CUTOUT AREA REPAIRED PER HAECO RS R-52-11-34782.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D - BS 630-640, LBL 46 SEAT TRACK CROWN FOUND CORRODED AS MARKED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C BS 2180 S-32R STRINGER END CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D BS 900 FRAME FOUND CRACKED AT S-11R. BS 900 SIDE FRAME AT STR 11R AREA REINFORCEMENT FRAME PATCH REPAIRED AS PER HX RS R53-22-34790.

Part: TIE — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 800 LT TENSION TIE FOUND CRACKED. BS 800 LT TENSION TIE REINFORCEMENT PATCH REPAIRED AS PER CUSTOMER EO B747-5310-5890 APPENDIX C FIG 2 AND AREA FINISHED PAINT PER MM 51-24-11.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 1241 RBL 35 CANTED PRESSURE BULKHEAD FOUND CRACKED. RT WLG W/W CANTED BULKHEAD WEB REPAIRED AT BS 1241 RBL 16 - RBL 47 AS PER RS R-53-48-34796.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C BULK CARGO - BS 2116 - 2120 RT STR 40 STR END FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS. BS 2110 - 2130 STR 40R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - L3 DOOR FWD CUTOUT NR 6 STOP FITTING FOUND CRACKED. L3 DOOR FWD CUTOUT NR 6 STOP FITTING REPLACED AS PER SRM 51-10-01 PAGE 8.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C RT WLG W/W PRESSURE DECK WEB CORROSION AT BS 1341 - 1343 RBL 54 - 56. CORROSION REMOVED IAW 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1.

Part: PANEL — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 1241 RT CLOSURE PNL FOUND CRACKED. CLOSURE PANEL REPLACED PER EO B747-5310-2758-E APPENDICES -E- AT RT SIDE ONLY.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 740 S-4L, S-3L AND S-2AL, S-3AR STRINGER END SPLICE AREA CRACKED. BS 790 S-4L, S-3L, S-2AL, S-3AR STRINGER REPAIRED IAW SRM 53-10-03 FIG 10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,255 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 960 S-5L FRAME FOUND CRACKED. SIDE FRAME REPAIRED AS PER SRM 53-10-04 FIG 54.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C RT WLG W/W PRESSURE DECK PANEL CORROSION AT RBL 56 - 58 BS 1342 - 1344. CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1. PRESSURE DECK WEB REPAIRED AS PER SRM 53-10-07 FIG 2.

Part: TIE — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 840 LT TENSION TIE FOUND CRACKED. BS 840 LT TENSION TIE REINFORCEMENT PATCH REPAIRED AS PER CUSTOMER EO B747-5310-5890 APPENDIX C FIG 2 AND AREA FINISHED PAINT TOUCH UP PER MM 51-42-11.

Part: SKIN — CORRODED (CENTER WING) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - WING CENTER SECTION SURFACE FOUND CORRODED. WING CENTER SECTION CORRODED SKIN REPAIRED AT BS 1220 LBL 97 AS PER RS R57-14-34799.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C BS 2180 BETWEEN S44R AND S46R AREA FRAME SHEAR TIE CRACK. BS 2180 SHEAR TIE BETWEEN STR 44R AND 46R REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D BS 960 S8L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 54.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C LWLG - BS 1241 BULKHEAD LBL 87 CENTER TANK TRANSFER VALVE BONDING JUMPER ATTACHMENT VERT STIFFENER CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 57-10-01 LIMITS. LWLG BS 1241 LBL 87 VERTICAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 8.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D - BS 990 S-7L AND S-8L STRINGER END SPLICE SUSPECT CRACKED. HFEC INSPECTION CUTOUT AS PER NTM PART 6 51-00-00 FIG 4. BS 970 - 990 S-7L AND S-8L STRINGER REPAIRED IAW SRM 53-10-03 FIG 4 AT TWO LOCATIONS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D - BS 540-600 AND 610-640 LBL 66, SEAT TRACK CROWN AND FLANGE FOUND CORROSION. BS 540-600 AND 610-640 LBL 66, SEAT TRACK CROWN AND FLANGE REPAIRED AS PER SRM 51-10-01. (P/N: BAC1520-1567-717876511RK).

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D - BS 760 S-7L AND S-8L AREA FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 54.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C BULK CARGO AFT COMPT BS 2180 S 44L STRINGER CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-41 FIG 1 LIMITS. BULK CARGO BS 2180 STR 44L REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: PANEL — CRACKED (CABIN) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - R5 DOOR FWD CUTOUT LOWER REVEAL FOUND CRACKED. REVEAL PANEL REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C BS 2180 S-51L STRINGER END CRACK. BS 2180 - 2210 S-51L STRINGER REPAIR IAW SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - STA 2182-2185 LT NR 1 STRINGER END FOUND CRACKED. BS 2172- BS 2188 S1L, STRINGER SECTIONAL REPAIRED AS PER SRM 53-10-03 FIG 4 AND FINISH PAINT APPLIED AS PER MM 51-24-11.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C BULK CARGO AFT COMPT COMPT BS 2200 S-42R AREA FRAME ATT STIFFENER CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS. BS 2200 STR 42R FRAME ATT STIFFENER REPLACED AS PER SRM 51-10-01 PG 8.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - R2 DOOR FWD CUTOUT REVEAL FOUND CRACKED. R2 DOOR FWD CUTOUT REVEAL REPAIRED IAW RS R53-22-34784.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - STA 1956-1960 LT NR 2 STRINGER END FOUND CRACK. TIE CLIP AT M/D BS 1960 S2L REPLACED AS PER SRM 51-10-01 PG 8.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C BS 2180 S-50R STRINGER END CRACKED. BS 2180 - 2210 S-50R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - STA 2186 STRINGER 1R STRINGER END CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FX - STA 400 S41L STIFFENER FOUND CRACKED. STIFFENER REPLACED AS PER SRM 51-10-01 PG 8.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - R4 DOOR FWD CUTOUT LOWER REVEAL FOUND CRACKED. R4 DOOR REVEAL REPAIRED AS PER SRM 53-10-04 FIG 84.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - R3 DOOR FWD CUTOUT LOWER CORNER REVEAL FOUND CRACKED. LOWER CORNER REVEAL FITTING REPLACED AS PER SRM 51-10-01 PG 8 & PAINT TOUCHED UP AS PER MM 21-24-11.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/ D- BS 2160 RBL 98 SEAT TRACK CRACK. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 8, P/N (BAC1520-1545-7178T6511RK).

Part: PANEL — CRACKED (CABIN) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - L2 DOOR FWD CUTOUT LOWER REVEAL CRACKED. L2 DOOR FWD CUTOUT LOWER REVEAL PANEL REPAIRED IAW SRM 53-10-04 PG 84.

Part: DOOR FRAME — DENTED (L1 DOOR) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - L1 DOOR FWD FRAME FOUND DENT AT UPPER HINGE AREA. FWD DOOR FRAME REPAIRED AS PER SRM 52-10-02 FIG 13.

Part: WEB — CRACKED (R3 DOOR) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D R3 DOOR INT WEB FOUND CRACKED AT FWD FRAME APPROX STOP FITTING NR 7 AREA. DOOR WEB REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D - BS 620 S-6R STRINGER CRACK. BS 610 - BS 630 STR 6R SEGMENT REPAIRED AS PER SRM 53-10-03 FIG 4 AND AREA FINISHED PAINT TOUCH UP PER MM 51-42-11.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C AFT CARGO COMPT - BS 1640- 1643 STR 35R FOUND CORRODED. AFT CARGO COMPT BS 1640-1643 STR 35R REPAIRED AS PER SRM 51-10-01 FIG 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C, BULK CARGO - BS 2140 RT FRAME CRACKED BTN STR 29R AND STR 30R. BS 2140 S-29R- 30R FRAME REPAIRED AS PER SRM 53-10-04 FIG 39.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - STA 2178 STR 1R STRINGER END CRACKED. BS 2178- BS 2150 S1R STRINGER SEGMENT REPAIR AS PER SRM 53-10-03 FIG 4 AND AREA FINISH PAINT TOUCH UP AS PER MM 51-24-11.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D - BS 400 RBL 80 MOST O/B FLOOR SUPPORT CRACK. FLOOR SUPPORT REPAIRED AS PER SRM 53-10-04 FIG 76 AND AREA FINISH PAINT TOUCH UP AS PER MM 51-24-11.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C, U/D - BTN BS 620 S-6L STRINGER CRACK. BS 610 - BS 630 S6L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO BS 520 - 540 STR S-29R STRINGER END FOUND CRACKED. BS 520 - 540 S-29R STRINGER SPLICE REPLACED AS PER SRM 51-10-01.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - STA 580 - 620 S20R TO 22R WINDOW FORGINGS MATING SURFACE EDGE FOUND CORRODED. BS 580 - BS 600 RT SIDE WINDOW FORGING REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D - BS 540 LBL 20-40 FLOORBEAM FOUND CORROSION AS MARKED. FLOORBEAM REPAIR AT BS 540 LBL 30 TO LBL 55 AS PER SRM 53-10-07 FIG 21.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - STA 400 - 420 S20R TO 22R WINDOW FORGING MATING SURFACE EDGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 56-20-01 LIMITS, STA 400 - 420 S20R-22R WINDOW FORGING REPLACED AS PER SRM 51-10-01 PG 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,255 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO - BS 880 RT FRAME I/B CHORD FOUND CRACKED BETWEEN STR 34R & STR 35R. FRAME I/B CHORD REPAIRED AS PER RS R-53-22-34785.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO BS 740 - 760 STR 28R FOUND CRACKED. BS 740 - 770 STR 28R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FX - STA 1063, LBL 9 KEEL BEAM PANEL SUPPORT BRACKET FOUND CORRODED. KEEL BEAM PNL SUPPORT BRACKET REPLACE JUST AT BS 1063 LBL 9.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - FRAME FOUND CRACK AT STA 540 S24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FX - STA 1063 AND STA 1103, RBL 9 KEEL BEAM PNL SUPPORT BRACKET FOUND CORRODED. KEEL BEAM PNL SUPPORT BRACKET REPLACE JUST AT BS 1063, 1103 RBL 9 (TOTAL 2 EA).

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - FRAME FOUND CRACK AT STA 940 S24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35.

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C U/D BS 330 LBL 0-40 FLOOR SUPPORT CORRODED. U/D BS 330 RBL 10 TO LBL 45 FLOOR SUPPORT REPAIR AS PER SRM 53-40-04 FIG 2.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FX - STA 1083 LBL 3 - RBL 3 KEEL BEAM PNL SUPPORT FOUND CORRODED. TWO EACH ATT ANGLE REPLACED AT FX STA 1083 LBL 3 - RBL 3 AS PER SRM 51-10-01 PG 8.

Part: SPAR — CHAFED (NR 1 PYLON) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C NR 1 PYLON - MID SPAR WEB CHAFING THROUGH AT NAC STA 238. MID SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 12.

Part: PANEL — CRACKED (CABIN) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 2231 LT NR 5 DOOR FWD CUTOUT BETWEEN STR 16 & 15 CUTOUT CRACK. CUTOUT REVEAL PANEL REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D- FRAME FOUND CRACK AT STA 560 S24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C, FWD CARGO COMPARTMENT LT STA 980 S38L STR END CRACKED AND ATTACHED SHIM DELAMINATED. STRINGER S-38L REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO - BS 840 LT STR 30 SUPPORT WEB I/B CHORD SPLICE FOUND CORRODED. FWD CARGO BS 840 LT STR 30 SUPPORT WEB I/B CHORD SPLICE REPAIRED AS PER SRM 51-10-01 FIG 1.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FX - LBL 9, STA 1177 AND 1223 KEEL BEAM PNL SUPPORT BRACKET FOUND CORRODED. KEEL BEAM PNL SUPPORT BRACKET REPLACE JUST AT BS 1177, 1223 LBL 9.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - FRAME FOUND CRACK AT STA 580 S24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - FRAME FOUND CRACK AT STA 600 S24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FX - STA 1177, 1201 AND 1223, RBL 9 KEEL BEAM PNL SUPPORT BRACKET FOUND CORRODED. KEEL BEAM PNL SUPPORT BRACKET REPLACE JUST AT RBL 1177, 1223, RBL 9.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - FRAME FOUND CRACK AT STA 920 S24L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35.

Part: PANEL — CRACKED (CABIN) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 2231 LT NR 5 DOOR FWD CUTOUT BETWEEN STR 22 & 23 CUTOUT CRACKED. BS 2231 L5 DOOR FWD CUTOUT REVEAL PANEL FROM STR 22L TO STR 25L REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C, FWD CARGO COMPARTMENT RT STA 980 S38R STR END CRACKED AND ATTACH SHIM DELAMINATED. FWD CARGO COMPARTMENT BS 950 - BS 980 S38R STRINGER REPAIRED IAW SRM 53-10-03 FIG 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - FRAME FOUND CRACK AT STA 640 S25L. FRAME REPAIRED AS PER SRM 53-10-04 FIG 35.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C, FWD CARGO - BS 880 RT FRAME I/B CHORD FOUND CRACKED AT STR - 38R. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO - BS 740 - 760 STR-29R FOUND CRACKED. FWD CARGO COMPT BS 740 - 790 STR 29R STRINGER REPAIRED IAW SRM 53-10 -03 FIG 1. BUTT JOINT SKIN REPAIRED FROM BS 740 - 752 BTN STR 28-30 PER SRM 53-30-03 FIG 47.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO - BS 680 RT FRAME FOUND CRACKED AT STR 34R. FRAME REPAIRED AS PER RS R-53-22-34783.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO - BS 660 LT FRAME ATT TIE CLIP FOUND CRACKED AT STR 38L. BS 660 STR 38L TIE CLIP REPLACED AS PER SRM 51-10-01 PG 8.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 900 AND 940-960 RBL 33 SEAT TRACK CROWN FOUND CHAFING MARK AS MARKED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. (P/N: BAC1520-1566-7178T6511RK)

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO - BS 520 RT FRAME WEB FOUND CRACKED BETWEEN STR 32R & STR 33R. FRAME WEB DOUBLER REPLACED AS PER SRM 51-10-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO - BS 840 - 844 STR 30L STR WEB UPPER FWD SUPPORT ANGLE FOUND HEAVY CORROSION AT STR 30L. SUPPORT ANGLE REPLACED PER SRM 51-10-01 PG 8.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C, FWD CARGO - BS 880 STR 35R FOUND CHIPPED AS MARKED. FWD CARGO COMPT BS 870 BS 890 STR 35R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,255 hrs · 21,257 cycles

INSPECTION TYPE:C AFT LOWER CARGO DOOR CUTOUT UPPER EDGE FORWARD CORNER FOUND CRACK AT BODY SKIN APPROX .375 INCH IN LENGTH FROM THE EDGE OF DOOR CUTOUT. DOOR CUTOUT FWD UPPER CORNER REPAIRED AS PER HAECO RS R-53-61-34789, SRM 53-30-03 FIG 62.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO - BS 830 - 846 STR 29R FOUND HEAVY CORROSION. CORROSION REMOVED IAW SRM 51-10-01. BS 790 - 870 STR 29R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C RT MLG W/W BS 1350 B/H LWR CHORD I/B UPPER SURFACE CORRODED AS MARKED. 3 EA 0.625 INCH HOLE INSPECTED, ALL WITHIN PRODUCTION TOLERANCES AND ARE CLEAN AND ROUND WITHOUT DAMAGE AS PER HX RAA 747-53-20057 REQUIREMENT.

Part: PANEL — CORRODED (RT WING) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C RHW - UPPER WING L/E AREA PNL BULGE UP AT WS 1410 - 1430. RHW UPPER SKIN AT OLES 1430 - 1450 L/E AREA IS REPAIRED AS PER RS R-57-25-34803.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO BS 480-500 LT STR 35 EDGE FOUND CRACKED. BS 480- BS 500 LT STR 35 SEGMENT REPAIRED AS PER SRM 53-10-03 FIG 3 AND AN AREA PAINT TOUCH UP PER MM 51-24-11.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO - BS 460 - 480 STR 36R FOUND CRACKED AS MARKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 3.

Part: BULKHEAD — CRACKED (NR 2 PYLON) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT FWD WEB APPROX 7 O'CLOCK (VIEW LOOKING FWD). NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACKED AREA REPAIRED AS PER HAECO RS R-54-53-34787.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FX - STA 1000, 1020, AND 1040 KEEL BEAM PNL SUPPORT BRACKET FOUND CORROSION AT LBL 9 & RBL 9 AREA. CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS. KEEL BEAM PNL SUPPORT BRACKET REPLACED JUST AT BS 1000 L/R, 1040 RT (TOTAL 3 EA) AS PER SRM 51-10-01 PG 8.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO - BS 840 LT FRAME I/B CHORD FOUND CORROSION AT STR 30L. FWD CARGO BS 840 LT FRAME I/B CHORD REPAIR AT STR 30L AS PER SRM 53-10-04 FIG 52.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO - BS 840 - 845 STR 30L STR WEB FOUND HEAVY CORROSION. FWD CARGO BS 840-845 STR 30L WEB REPAIRED AS PER SRM 51-10-01.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO BS 760 FRAME STR 30L ATT TIE CLIP FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 PG 8. FRAME STR-30L ATT TIE CLIP REPLACED AS PER SRM 51-10-01 PG 8.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C NWW TUNNEL - RT BS 300 VERTICAL BEAM WEB FOUND CRACKED AT LOWER STAND OFF HOLE BETWEEN FIRST AND SECOND CLIP (COUNT FROM TOP). NOSE W/W TUNNEL RT BS 300 VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 & BOEING DWG 624U0005.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - L3 DOOR CUTOUT FWD LOWER CORNER REVEAL FOUND CRACKED. M/D L3 DOOR CUTOUT FWD LOWER CORNER REVEAL REPLACED AS PER SRM 51-10-01 PG 8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO BS 720 LBL 25 LONGITUDINAL FLOOR SUPPORT AFT END FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 870 - 880 RBL 11 SEAT TRACK RT FLANGE FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS. M/D BS 870 - 1000 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C FWD CARGO - BS 920 - 940 STR 29R FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C LT SIDE TUNNEL BS 400 BULKHEAD O/B CORNER RADIUS FOUND CRACK AT S31L. LT SIDE TUNNEL BS 400 BULKHEAD O/B CORNER RADIUS REPAIRED AS PER SRM ADDENDUM 53-10 EO B747-5310-4659-B.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C BULK CARGO - BS 2020-2021 LBL 8 FLOOR SUPPORT FOUND CORRODED CRACKED. FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C AFT CARGO - BS 1840 - 1860 RBL 8 FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS. AFT CARGO BS 1850 RBL 8 FLOOR SUPPORT FLANGE REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C RT SIDE TUNNEL BS 400 BULKHEAD O/B CORNER RADIUS FOUND CRACK AT S31R. RT SIDE TUNNEL BS 400 BULKHEAD O/B CORNER RADIUS REPAIRED AS PER SRM ADDENDUM 53-10 EO B747-5310-4659-B.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C M/D - BS 800 FRAME S16L -17L LOCATION FOUND 2 EACH CRACKS AT REVEAL. BS 800 S16 TO S18L REVEAL REPAIR C/OUT IAW SRM 53-10-04 FIG 114 AND HX RS R53-22-34780.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C BULK CARGO - BS 1950-1960 S44R STRINGER SPLICE FOUND CORRODED AS MARKED. BS 1950-1960 S44R STRINGER SPLICE REPLACEMENT AS PER SRM 51-10-01.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C AFT COMPT - BS 1880 LBL 20 FLOORBEAM UPPER CHORD FOUND CORRODED CRACKED. AFT COMPT BS 1880 LBL 20 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-10-01 FIG 2.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 75,255 hrs · 21,257 cycles

INSPECTION TYPE:C FX - LT SIDE STA 1000 BULKHEAD AFT FACE ATTACH WEB O/B CORNER FOUND CORROSION AT S38L JUST BELOW DRAG SPLICE FITTING. CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS. BS 100 LT BULKHEAD WEB S-38L JUST BELOW DRAG SPLICE FITTING REPAIRED AS PER RS R-53-23-34786.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C AFT COMPT - BS 1880 LBL 26 FLOORBEAM UPPER CHORD FOUND CORRODED. AFT COMPT - BS 1880 LBL 26 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-10-01 FIG 01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C AFT COMPT - BS 1850 - 1856 RBL 8-16 FLOORBEAM UPPER SUPPORT PNL ATT PLATE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 51-10-01 PG 8. AFT CARGO BS 1840 - BS 1860 RBL 8 - 26 FLOORBEAM UPPER SUPPORT PANEL & ATT PLATE REPLACED AS PER SRM 51-10-01 PG 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,235 hrs · 21,257 cycles

INSPECTION TYPE:C AFT COMPT - BS 1800 S-41L TO 42L FRAME UPPER CHORD FOUND CRACKED. AFT COMPT BS 1800 BETWEEN STR 38L TO 42L FRAME REPAIRED AS PER SRM 53-10-04 FIG 66.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT OVER UPPER DECK STAIRS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AND BATTERY PACK OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (MAIN CARGO BAY)

INSPECTION TYPE:N/A EMERGENCY LIGHT MAIN CARGO CEILING FWD OF STAIRS INOP. RELAMPED MAIN CARGO CEILING LIGHT.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:IN EMERGENCY LIGHT INOP ON MAIN DECK. EMERGENCY LIGHT REPLACED.

Part: BATTERY — DISCHARGED (L1 DOOR)

INSPECTION TYPE:W/E AFT EMERG LIGHT AT L1 DOOR INOP. COMES ON THEN FADES OUT. REMOVED AND REPLACED BATTERY, OPS CK GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT AND EMERGENCY LIGHT IN AISLE IS OUT. REMOVED AND REPLACED EMERGENCY POWER PACK. OPS CK GOOD.

Part: WINDOW POST — CORRODED (FUSELAGE)

INSPECTION TYPE:C, (P/N 65B807077-07) WINDOW FRAME BETWEEN STA 620 - 640, STR 9 - 10 LT SIDE CORROSION WAS FOUND ON THE EXTERNAL SURFACE. TIME LIMITED REPAIR ACCOMPLISHED PER B747 SRM 56-20-07 FIG 7 IAW 1A1 EO MF-MAN-B47-56-00-89340 AS APPROVED FAA FORM 8110-3 9/22/00 AND UPS REPAIR/ALTERATION AUTH ENGIN FILE B747-56-0003. PERFORM DETAIL VISUAL/SURFACE HFEC INSP EVERY 6 MO OR 500 CYCLES. REPLACEMENT OF PART SHOULD BE ACCOMPLISHED WITHIN 18 MO OR 1500 CYCLES.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C, UPPER LOBE MAIN DECK - CRACK AND DISTORSION ON FRAME STA 360 AND STA 380, LT SIDE BETWEEN STR 23 - 24 CRACK REPAIR ACCOMPLISHED PER IAI EO MP-MAN-B47-53-10-89342 AND AS APPROVED ON FAA FORM 8770-3 DATED 9/29/00. NOTE: CONTINUED FRAME INSPECTONS EVERY 2000 FLIGHT CYCLES ARE REQUIRED PER FAA AD 97777.

Part: WIRE — SHORTED (COCKPIT)

INSPECTION TYPE:N/A, PASSING FL240 A STRONG ODOR STARTED IN COCKPIT. SMELLED SIMILAR TO A CETONE. ODOR WAS ISOLATED TO THE P7 CIRCUIT BREAKER PANEL. INSPECTED COCKPIT FOR BURNED WIRING, OVERHEAD PANEL OVERHEATING ETC. FOUND P-7, P-12, P-5 OVERHEAD PANELS IN GOOD CONDITION. FOUND L1 WINDOW LOWER LEFT PWR WIRE BURNED. SPLICED IN NEW WIRE, CKS OK. ANC FIRE DEPT INSPECTED, NO CHEMICALS, SMOKE FOUND WITH SNIFFENERS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,816 hrs · 20,292 cycles

INSPECTION TYPE: SP. RIGHT NR 3 DOOR NR 4 STOP FITTING IS CRACKED ON FUSELAGE SIDE. REMOVED AND REPLACED STOP FITTING I.A.W. DWG. 015U0579, AND SB. 747- 53-2358

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,816 hrs · 20,292 cycles

INSPECTION TYPE: AD, STA 1265 FWD LOWER CORNER OF L3 DOOR JUST BELOW NR 2 STOP FITTING IS CRACKED ON FRAME SEGMENT REPAIRED FRAME SEGMENT I.A.W. E.O.B747-5310-12070 APPENDIX E, AND 8110-3 APPROVED DH SK 676-257

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,816 hrs · 20,292 cycles

INSPECTION TYPE: AD, NR 3 DOOR, LT SIDE, NR 5 STOP FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG.015UO579,AND E.O. B747-5310- 11117C

Part: ENGINE — MALFUNCTIONED (NR 4 ENGINE)

INSPECTION TYPE:N/A, DURING DESCENT WITH NR 4 ENGINE AT IDLE THRUST EPR 1.17, NO-88.0 AND FUEL FLOW WAS 10,000. ACCOMPLISHED INFLIGHT ENGINE SHUTDOWN CHECKLIST. REMOVED AND REPLACED NR 4 ENGINE IAW TASK CARD 5000, OPS AND LEAK CHECK GOOD.

Part: OIL FILTER — CONTAMINATED (NR 2 ENGINE) · airframe 70,816 hrs · 20,292 cycles

INSPECTION TYPE:SP, NR 2 OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. SHUTDOWN NR 2 ENGINE IAW CHECKLIST. OIL PRESSURE REMAINED ABOVE 5 PSI. ENTIRE TIME ENGINE WINDMILLED FOR 40 MINUTES AFTER SHUTDOWN. CHECKED CHIP DETECTORS, NO DEFECT. DRAINED OIL FROM GEARBOX, NO DEFECT DRAINED OIL FROM TANK, SOME CARBON. FOUND OIL FILTER FULL OF CARBON, REPLACED FILTER IAW 72-61-05. REPLACED OIL QTY TRANSMITTER IAW 79-31-01, REPLACED OIL FILTER DIFF PRESS WARNING SWITCH IAW 79-35 -01, REPLACED LOW PRESSURE WARNING SWITCH IAW 79-33-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

CREW SERVICE DOOR EMERGENCY LIGHT BATTERY PACK IS DEAD. R&R BATTERY PACK PER MM 33-51-04 OPS CHECKED GOOD

Part: LIGHT — INOPERATIVE (BS 330)

EMERGENCY LIGHT INOP AT STA 330 MAIN CARGO DECK. REMOVED AND REPLACED EMERG LIGHT ASSP PER B747 MM 33-51-07, OPS CK GOOD.

Part: CONTROL — FAILED (LT WINDSHIELD)

INSPECTION TYPE:N/A, AFTER T/O CAPT'S WINDOW HEAT BEGAN TO EMIT WHITE SMOKE. TURNED HEAT OFF AND SMOKE STOPPED. REMOVED AND REPLACED WINDOW HEAT CONTROLLER AND SECURED CONNECTORS ON WINDOW CONTACTS, OPS CK NORMAL. (P/N 617154-5), (S/N 079C-188) OFF, (S/N 026C-1904) ON.

Part: DOUBLER — CRACKED (AFT FUSELAGE)

INSPECTION TYPE:N/A,TAIL SKID AREA SHOWS 2.25 INCH CRACK. REPAIRED CRACK PER SRM PAGE 53-30-03 PAGE 21 FIC/A SHEET 4. INSTALLED PERMANENT REPAIR DOUBLER.

Part: SIGN — INOP (SERVICE DOOR)

INSPECTION TYPE:IN, EXIT SIGN OVER CREW SERVE DOOR DOES NOT ILLUMINATE. RESET CANNON PLUG, OP CHECKS OK.

Part: ATTACH CHORD — MISRIGGED (DOOR SLIDE)

INSPECTION TYPE-N/A, DURING SHOP VISIT FOUND THE ATTACH CHORD TIED TO THE SHORT LOOP. PLACED THE ATTACHED CHORD THROUGH THE SHORT LOOP, ATTACHING THE ATTACH CHORD TO THE CONE AND REINSTALLING PIN PER BF GOODRICH OVERHAUL MANUAL 25-68-03.

Part: BULB — FAILED (CABIN)

INSPECTION TYPE-N/A, MAIN CARGO DECK EMERGENCY LIGHT INOP FWD OF CREW STAIRS. RELAMPED PER 747 MM, OPS CHECK GOOD.

Part: FIRE CARD — LOOSE (E/E COMPT)

IN FLIGHT TRANSIT MASTER FIRE WARNING LIGHT (FLASHED THREE). NO OTHER INDICATIONS. LIGHT TEST GOOD. RERACKED FIRE WARNING CARDS, OPS CK GOOD PER M/M 26-11-00 AND 26-15 -00, 26-14-00, 26-16-00. OK FOR SERVICE.

Part: FIRE LOOP — OUT OF POSITION (NR 1 ENGINE)

INSPECTION TYPE-N/A, NR 1 ENG LOOP 'A' FAULT DETECTOR ILLUMINATED INTERMITTENTLY FROM T/O UNTIL FL 180 DEG. NEEDLE WAS ERRATIC BOTTOM SCALE TO TOP OF SCALE EGDT OF NR 1 AT 855 DEG C ON T/O M29-15. REROUTED NR 1 FIRE LOOP, OPS CKD GOOD PER MM 26-10-00.

Part: BATTERY — DISCHARGED (L1 DOOR)

FWD EMERGENCY LIGHT AT L1 DOOR INOP. DOOR STILL OPERABLE DUE TO REMAINING EMERG LIGHT. REPLACED BATTERY ASSY, LIGHT TESTS GOOD. PN ON AND OFF S1356-10ASN ON TAG 00282916 NSN OFF.

Part: CIRCUIT BREAKER — MELTED (P-14 CTR MAIN)

INSPECTION TYPE N/A, FOUND ACCESS LEFT UPPER DECK C/B C338 BURNED. REPLACED C338 BREAKER, UPPER DECK LIGHTS TEST GOOD. DEFERRED P-14 C/B PANEL NEEDS HOLE REPAIRED, DEFERRAL NR D117075.

Part: FIRE LOOP — SHORTED (APU)

INSPECTION TYPE-N/A, ON SHORT FINAL APU A FAULT LIGHT CAME ON AND STAYED ON UNTIL SHUTDOWN, CHECKLIST INTERMITTENT FIRE BELL. FOUND APU A-LOOP SHORTED, REPOSITIONED.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE N/A, WALK WAY EXIT LIGHTS PRIOR TO CREW SERV DOOR CONTINUOUSLY FLASHED ON AND OFF. REMOVED AND REPLACED EMERGENCY UPPER DK CEILING LT ASSY, OP CK NORMAL PER MM 33-50-00 (P/N S1356B37) OFF, (S/N S1356B37) ON.

Part: CONNECTOR — LOOSE (FLIGHT CABIN)

INSPECTION TYPE N/A, EMERGENCY LIGHTS FLASH ON AND OFF CONTINUOUSLY. REMOVED EMERGENCY CEILING LIGHT, OPERATED AND CHECKED FOR LOOSE CONNECTIONS. NONE FOUND, OPS CK NORMAL. NOTIFIED MMOC TO PUT AN ALERT ITEM ON THIS REPEAT PROBLEM.

Part: CONNECTOR — DIRTY (COCKPIT)

INSPECTION TYPE: DLY. DURING FLIGHT, THE EMERGENCY LIGHTS SWITCH IN THE ARMED POSITION, THE EMERGENCY LIGHT MODULE IN THE CREW SERVICE DOOR HALLWAY CEILING FLICKERED ON AND OFF. CLEANED AND RESEATED CONNECTOR ON LIGHT ASSY, OPS CHK NORMAL.

Part: CONNECTOR — LOOSE (CABIN)

WITH THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION, THE EMERGENCY LIGHT MODULE IN THE CREW DOOR HALLWAY CEILING FLICKERED OFF AND ON. CLEANED AND RESEATED CONNECTOR ON LIGHT ASSY, CK O.K.

Part: LIGHTS — INOPERATIVE (MAIN DECK)

INSPECTION TYPE N/A REF D111137, EMERGENCY LIGHT AT STA 580 LT CEILING MAIN DECK DIM. REPLACED EMERGENCY LIGHT ASSM (P/N 1356837) (S/N 19732) ON, (P/N 1356-10A) (S/N UPS 5) OFF, ILLUMINATION CHECKS GOOD.

Part: BLKHD WEB — CORRODED (BS 2360)

INSPECTION TYPE 'C', FOUND ON WEB EDGE FASTENER SEM AT LT AT STR 38L WL 225 AT BS 2360 REAR PRESS BULK. REPAIRED DAMAGE IAW SRM 51-10-04 FIG 86 BOEING TELEX UPS-AMS-96-012 3RE APP DOC DFX 96-104, EFN 747-0761.

Part: SPAR WEB — CORRODED (WS 550)

INSPECTION TYPE 'C', LT WING REAR SPAR WEB OF LT WING REAR SPAR HAS CORROSION AT WS 550. REPAIRED CORROSION IAW UPS EFN 747-57-0323.

Part: STRINGER — CORROSION (BS 2200-2220)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED AREA AFT OF BULK CARGO COMP. FOUND CORROSION ON STR FLANGE S-36 RT BETWEEN BS 2200-2220. REMOVED CORRODED SECTION OF STRINGER AND REPAIRED STRINGER IAW SRM 53-10-3.

Part: TUBE — WORN (WS 1071)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED LT L/E INTERIOR I/B OF PYLON NR 1 FOUND WEAR HOLE IN SUPPORT TUBE ON AISLES 1071.25. REMOVED TUBE IAW MM 20-50-03, INSTALLED BUSHINGS IAW OHM 20-50-03 AND INSTALLED NEW TUBE IAW MM 20-50-03.

Part: SKIN — CORROSION (BS 2360)

INSPECTION TYPE 'C', FOUND CORROSION AT BS 2360 AFT PRESSURE SKIN PLATES AND Y-CHORD BETWEEN STR 46R AND STR 46L. REPLACED AFT PRESSURE WEB SEGMENT, PARTLY REPLACED Y-CHORD BETWEEN LBL 44 TO RBL 55. INSTALLED FASTENERS IAW SRM 51-30-02, APPR EFN 747-53-0760.

Part: ANGLE — CRACKED (BS 2200-S-40RH)

WHILE IN FOR C-CHECK AT AMS MAINTENANCE REPORTED - AREA AFT OF BULK CARGO COMP, FOUND CRACKED STIFFINER - ANGLE FROM INTERCOSTAL ON FORWARD SIDE OF FRAME BS 2200, S40R. REPLACED STIFFENER-ANGLE IAW SRM 51-30-02.

Part: BULKHEAD WEB — DAMAGED (BS 2160)

WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED BULK CARGO COMP. FOUND SEVERAL HOLE DAMAGES ON BULKHEAD WEB AT BS 2160, LT OF ACCESS DR. REMOVED DAMAGED SECTION OF BULKHEAD WEB AND REPAIRED WEB ACCORDING TO SRM 51-40-02.

Part: FRAME — CRACKED (BS 1580)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT CARGO COMP FOUND CRACKED IN FRAME UPPER FLANGE AT BS 1580 RT NEAR RT SIDE GUIDE. STOP DRILLED CRACK AND REPAIRED FRAME UPPER FLANGE ACC SRM 53-10-04, FIG 66.

Part: FRAME — CRACKED (BS 2220)

INSPECTION TYPE: C. AREA AFT OF BULK CARGO COMPARTMENT, FOUND CRACKS IN FRAME SHEAR TIE DUE TO CORROSION AT BS 2220 NEAR RIGHT OUTFLOW VALVE BETWEEN STR 40 AND STR 44R. REPLACED FRAME AT BS 2220 RIGHT BETWEEN STR 44 AND STR 36R IAW SRM 51-30-02.

Part: FRAME — CORRODED (BS 2220)

INSPECTION TYPE: C. AREA AFT OF BULK CARGO COMPARTMENT, FOUND CORROSION ON INNER FLANGE OF FRAME AT BS 2220 NEAR RIGHT OUTFLOW VALVE. CORROSION DAMAGES OUT OF LIMITS IAW SRM 51-10-01. REPLACED FRAME AT BS 2220 IAW SRM 53-10-01.

Part: FRAME — CRACKED (BS 1780 R/H)

WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1780, STR 10 - 15, DEFORMED AND CRACKED. REPAIRED FRAME IAW SRM 51-40-03, FIG. 2.

Part: FRAME — DEFORMED (BS 1800)

WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1800 STR 10 - 15, DEFORMED. REPAIRED FRAME IAW SRM 51-40-03, FIG. 2.

Part: FRAME — CRACKED (BS 1760)

WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1760, STR 10 - 15, DEFORMED AND CRACKED. REPAIRED FRAME IAW SRM 51-40-03.

Part: RIB — CRACKED (WS 1094.25)

WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED LT L/E INTERIOR INBOARD OF PYLON NR 1 RIB CRACKED UPPER CHORD AT ILES 1094.25. REPLACED RIB IAW SRM 51-30-02.

Part: FRAME — DEFORMED (BS 1740)

WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1740, STR 10 - 15, DEFORMED. REPAIRED FRAME IAW SRM 51-40-03, FIG. 2.4.

Part: FRAME — DEFORMED (BS 1900)

WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1900, STR 10 - 14, DEFORMED. REPAIRED FRAME IAW SRM 51-40-03, FIG. 2.4.

Part: FRAME — DEFORMED (BS 1880)

WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1880, STR 10 - 15, DEFORMED. REPAIRED FRAME IAW SRM 51-40-03, FIG. 2.

Part: FRAME — CRACKED (BS 1820)

WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1820, STR 10 - 16, DEFORMED AND CRACKED. REPAIRED FRAME IAW SRM 51-40-03, FIG. 2.

Part: STRINGER — CORROSION (BS 920-940)

MAINTENANCE REPORTED, BETWEEN STA 920 TO 940 STR 35 RT STRINGER IS CORRODED. CORROSION OUT OF LIMITS PER SRM 53-10-01. REPAIRED STR PER SRM 53-1003.

Part: TE SKIN — DELAMINATED (TE MIDFLAP)

WHILE ON GROUND, MAINTENANCE FOUND RT WING INBOARD MID-FLAP TRAILING EDGE OUTBOARD SECTION DELAMINATED. PERFORMED INTERIM REPAIR PER SRM 51-05, PG 21.

Part: EEL SWITCH — DIRTY (FLIGHT DECK)

MAINTENANCE FOUND EMERGENCY LIGHT SWITCH ON PILOTS OVERHEAD PANEL GOES TO ON VIA ARM WITH SWITCH CLOSED. CLEANED CONTACTS.

Part: SKIN — CRACKED (NAC STA 221)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND NR 4 PYLON OUTER SKIN CRACKED AT NAC STA 221. FABRICATED AND INSTALLED REPAIR PER SRM 54-30-03.

Part: WEB — CORRODED (STA 1000)

WHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND CORROSION ON SPAR WEB AT STA 1000. FABRICATED AND INSTALLED REPAIR PER UPS EO B747-5710-6859A.

Part: STRINGER — CRACKED (BS 1225)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND STRINGER 4L CRACKED AT BS 1225. REPLACED STRINGER PER SRM 51-10-3.

Part: RIB — CRACKED (NAC STA 163)

WHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND NR 4 PYLON RIB CRACKED AT NAC STA 163 O/B SIDE. REPLACED RIB PER SRM 51-30-2.

Part: FLOOR BEAM — CORRODED (BS 1580)

WHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND CORROSION ON TOP OF FRAME AT BS 1580. REPLACED UPPER CHORD PER SRM 51-30-2.

Part: FLOOR BEAM — CORRODED (BS 1660)

WHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND CORROSION ON TOP OF FRAME AT BS 1660. REPLACED UPPER CHORD PER SRM 51-30-2.

Part: FRAME — CRACKED (STA 1600)

WHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND CRACKED FRAME AT BS 1600, RBL 62. FABRICATED AND INSTALLED REPAIR PER UPS EO FILE NUMBER 747-53-0710.

Part: STRINGER — CRACKED (BS 970)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND VERTICAL FLANGE CRACKED ON STR 3A RT AT BS 970. REPLACED STRINGER PER SRM 51-10-3.

Part: SKIN — CORRODED (BS 2020-2040)

WHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND CORROSION ON LAP SPLICE BETWEEN BS 2020 AND BS 2040, STR 19L. FABRICATED AND INSTALLED REPAIR PER UPS EO B747-5330-1053E.

Part: FLOOR BEAM — CORRODED (STA 1760)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON UPPER CHORD FLOOR BEAM AT BS 1760, RBL 25-40. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3.

Part: FRAME — CORROSION (STA 1700)

WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON TOP OF FRAME AT STA 1700, STR 48R, LBL 25. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-4, 51-30-2.

Part: SEAT TRACK — CORRODED (BS 615)

MAINTENANCE REPORTED SEAT TRACK CORRODED BENEATH PALLET LOCK LOCATED AT RT SIDE O/B POS NR 1 CLOSEST TO CARGO DOOR IN FWD BELLY SECTION. REPLACED SEAT TRACK AS REQUIRED.