N520UP

Part: BATTERY PACK — DISCHARGED (BS 420)

INSPECTION TYPE:N/A EMERGENCY LIGHT ON MCD AT STA 420 LT DOES NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT/BATTERY ASSY WITH REF TO MM 33-51 51-07. OPS CHECK GOOD PER SAME.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CRACK FOUND AT 1EA FASTENER HOLE BELOW STR 15ER AT BS 420 FWD INNER CHORD (P/N: 65B01835-34) CRACKED THROUGH THICKNESS 0.040 INCH LONG RUNNING O/B AT 3 O`CLOCK POSITION (LOOKING FWD), (CRACK LENGTH 0.040 INCH). CABIN BS 420 FRAME ATTACH INNER CHORD BETWEEN STR 10AR TO STR 16R REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CRACK FOUND AT 1EA FASTENER HOLE BELOW STR 15ER AT BS 420 AFT INNER CHORD (P/N: 65B01835-7) THROUGH THICKNESS CRACK 0.040 INCH LONG RUNNING O/B AT 3 O`CLOCK POSITION (LOOKING FWD). CABIN BS 420 FRAME ATTACH INNER CHORD BETWEEN STR 10AR TO STR 16R REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: RIB — CORRODED (LT WING) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C LEFT WING L/E UPPER PANEL AT WS 970 FOUND BULGED UP. CORROSION BLEND OUT 0.030 X 1 X 2 INCHES LT WING L/E UPPER WS 970 UPPER CHORD REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (BS 420) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C M/D BS 420 S14ER FRAME FOUND CRACKED AS MARKED. CRACK LENGTH 5.5". BS 420 BTN S13AR TO S17R FRAME REPAIRED AS PER RS R53-12-35815. CONTINUED INSPECTIONS ARE REQUIRED AS PER RS R53-12-35815 AND UPS EO B747-5310-27050.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C FWD CARGO COMPT STR 39L AT BS 740 SPLICE CORROSION FOUND. REMOVED (CORROSION BLEND OUT 0.029" X .5 X .75 INCH OUT OF LIMITS SRM 53-10-01 FIG 1) FWD CARGO COMPT BS 740 LT STR 39 STRINGER SPLICE, REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C FWD CARGO COMPT STR 40L AT BS 740 SPLICE CORROSION FOUND. REMOVED CORROSION BLEND OUT 0.025 X .375 X .625 INCH OUT OF SRM 53-10-01 FIG 1 LIMITS. FWD CARGO COMPT BS 740 AT LT STR 40 STRINGER SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FRAME — CRACKED (BS 480 S15L) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CABIN BS 480 S15L FRAME FOUND CRACK. CRACK LENGTH 2 1/4" CABIN BS 480 STR 13AL TO STR 16L FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CABIN BS 420 S14ER FRAME DOUBLER FOUND CRACKED. (CRACK LENGTH 6 INCHES) CABIN BS 420 STR 13AR TO STR 15R FRAME ATTACH DOUBLER AND BETWEEN STR 10AR TO STR 16R FRAME ATTACH INNER CHORD & INNER ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CABIN BS 460 S14R FRAME DOUBLER FOUND CRACKED (CRACK LENGTH 1.5 INCH). CABIN BS 460 BETWEEN STR 11R TO STR 14ER AREA FRAME ATTACH DOUBLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CABIN R1 DOOR CUTOUT FWD UPPER CORNER ATTACH ANGLE FOUND CRACK (CRACK LENGTH .375 INCH). CABIN R1 DOOR CUTOUT FWD UPPER CORNER ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CABIN BS 480 S15R FRAME FOUND CRACK. CRACK LENGTH 2.5 INCHES. CABIN BS 480 STR 13AR TO STR 16R FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CABIN L1 DOOR CUTOUT FWD UPPER ATTACH ANGLE FOUND CRACKED APPROX AT BS 440 S16L (CRACK LENGTH .5 INCH). CABIN L1 DOOR CUTOUT FWD UPPER CORNER ATTACH ANGLE AT BS 440 S16L REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SKIN — DAMAGED (NR 1 PYLON) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C NR 1 PYLON STRUT O/B LOWER EDGE SKIN FOUND DAMAGED AT STA 236. NR 1 PYLON STRUT O/B LOWER EDGE SKIN REPAIRED AT STA 236 AS PER SRM 54-34-03 FIG 25.

Part: FRAME — CRACKED (BS 800) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C NR 2 DOOR FWD FRAME AT BS 800 RT SIDE FOUND CRACKED AT NR 5 AND NR 6 FAST HOLE BELOW STR 16 BOTH HOLE CRACKED AT STRAP WITH LENGTH 0.040" RUNNING AFTWARD. BS 800 RT SIDE FRAME FWD INNER CHORD AND STRAP REPAIRED AT BTN STR 15T TO STR 18R AREA AS PER RS R53-21-35812. POST REPAIR INSPECTION ARE REQUIRED AS PER RS R53-21-35812. WORKING DETAIL REFER NRC50958 AND REFER UPS EO B747-5310-27072.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C FWD CARGO COMPT S40L STRINGER FOUND CORROSION AT STA 740. (CORROSION BLEND OUT 0.040 X .75 X 1 INCH OUT OF SRM 53-10-01 FIG 1 LIMITS). FWD CARGO COMPT BS 710 TO BS 740 STR 40L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: FRAME — CRACKED (BS 800) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C BS 800 RT SIDE AT STR16 INNER CHORD 1 HOLE FOUND CRACKED AT 9 O/C POSITION WITH LENGTH 0.125" LENGTH. M/D BS 800 RT SIDE FRAME FWD INNER CHORD AND STRAP REPAIRED AT BETWEEN STR 15R TO STR 18R AREA AS PER RS R53-21-35812. POST REPAIR INSPECTION ARE REQUIRED AS PER RS R53-21-35812 AND UPS EO B747-5310-27072.

Part: STRINGER — CORRODED (BS 740 S36L) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C FWD CARGO COMPT S36L STRINGER FOUND CORROSION AT STA 740. CORROSION BLEND OUT 0.045" BY 1/2" BY 2" EXCEED SRM LIMIT. FWD CARGO COMPT BS 740 TO BS 770 STR 36L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: WEB — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C FX LOWER FUSELAGE OF INTERIOR SUPPORT WEB FOUND CRACKED AT STA 2220 TO STA 2240 STR 42L (CRACK LENGTH 2 INCHES). FX LOWER FUSELAGE OF INTERIOR SUPPORT WEB AT STA 2220 TO STA 2240 STR 42L REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C FWD CARGO COMPT S39L STRINGER FOUND CORROSION AT STA 745. (CORROSION BLEND OUT 0.063 X .875 X 1.25 INCH OUT OF SRM 53-10-01 FIG 1 LIMITS). FWD CARGO COMPT BS 740 TO BS 770 STR 39L REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: WEB — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C M/D HORIZONTAL SUPPORT WEB FOUND CRACKED JUST AT BS 820 STR 10L. (CRACK LENGTH .75 INCH). M/DECK BS 820 STR 10L HORIZONTAL SUPPORT WEB REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: WEB — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C M/D HORIZONTAL SUPPORT WEB FOUND CRACKED JUST AT BS 820 STR 10L (CRACK LENGTH .5 INCH). M/DECK HORIZONTAL SUPPORT WEB AT BS 820 STR 10L AREA REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: DOUBLER — CRACKED (BS 820) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CRACK FOUND AT DOUBLER AT LT SIDE OF BS 820 STR 10A ATTACHED TENSION TIE NR 4 HOLE CRACK LENGTH 3/16" APPROX AT 8 O/C POSITION. M/D BS 820 LT SIDE STR 10A FRAME ATTACH DOUBLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C FWD CARGO COMPT STRINGER FOUND CRACKED AT STA 280 S41R (CRACK LENGTH .375 INCH). FWD CARGO COMPT STA 260-280 STR 41R STRINGER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FILLER — CRACKED (BS 820) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CRACK FOUND AT FILLER AT LT SIDE OF BS 820 STR 10A ATTACHED TENSION TIE NR 12 HOLE AT 4 AND 7 O/C POSITION. CRACK LENGTH 3/32" AND 1/16". M/D BS 820 LT STR 10A TENSION TIE ATTACH FILLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND UPS EO B747-5310-23715-C.

Part: PLATE — DAMAGED (BS 940) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C M/D BS 940 LT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN AT MOST O/B. M/D BS 940 LT TENSION TIE ATT STEEL PLATE REPLACE AND INSTALLED AS PER RS R53-25-35811 AND UPS EO B747-5310-23715-C.

Part: CHANNEL — CRACKED (BS 940 S8L) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CRACK FOUND AT AFT CHANNEL OF BS 940 S8L TENSION TIE AT HOLE NR 16, THE CRACK WAS FOUND IN FWD FACE WITH LENGTH 0.030" APPROX. M/D BS 940 LT SIDE FRAME ATTACH TENSION TIE AFT CHANNEL REPAIRED AS PER RS R53-25-35811. SUPPLEMENTAL INSPECTIONS ARE REQUIRED AS PER RS R53-25-35811 AND UPS EO B747-5310-26946.

Part: CHANNEL — CRACKED (BS 860) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CRACK FOUND AT FWD CHANNEL OF BS 860 RBL80 TENSION TIE AT HOLE NR 6, THE CRACK WAS FOUND RUNNING AT 5 O/C POSITION WITH LENGTH 0.0625" APPROX. BS 860 RT TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35810 AND UPS EO B747-5310-26948. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35810 AND UPS EO B747-5310-26948.

Part: CHANNEL — CRACKED (LT WING) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C LT WING NR 4 L/E PDU AFT SUPPORT CHANNEL FOUND CRACKED AT MOUNT BOLT AREA. (CRACK LENGTH .375 INCH). LT WING NR 4 L/E PDU AFT SUPPORT CHANNEL REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: FILLER — CRACKED (BS 940 S8L) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CRACK FOUND AT BS 940 S8L TENSION TIE AT HOLE NR 11 THE CRACK WAS FOUND THROUGH THICKNESS AT THE FILLER. CRACK LENGTH 3/8". M/D BS 940 LT FRAME TENSION TIE ATTACH FILLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND UPS EO B747-5310-23715-C.

Part: CHANNEL — CRACKED (BS 820) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C CRACK FOUND AT FWD CHANNEL AT BS820 S10AR TENSION TIE AT HOLE NR 4 THE CRACK WAS FOUND RUNNING AT 12 O/C POSITION WITH LENGTH 0.040" APPROX. BS 820 RT FRAME ATTACH TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35809. SUPPLEMENTAL INSPECTION IS REQUIRED AS PER RS R53-25-35809 AND UPS EO B747-5310-26947.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C THROUGH THICKNESS CRACK FOUND AT BS 880 STR 9R TENSION TIE AT NR 10 FASTENER HOLE OF FRAME DOUBLER THE CRACK RUNNING AT UPWARD DIRECTION (CRACK LENGTH .25 INCH). M/DECK BS 880 RIGHT STR 9R FRAME ATTACH DOUBLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: PLATE — DAMAGED (BS 840) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C M/D BS 840 RT TENSION TIE ATTACH STEEL PLATE SHORT EDGE MARGIN FOUND AT UPPER ROW NR 4 COUNT FROM O/B. M/D BS 840 RT TENSION TIE ATTACH S/STEEL PLATE REPLACED AND INSTALLED AS PER RS R53-25-35808. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35808 AND UPS EO B747-5310-26949.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 83,127 hrs · 18,423 cycles

INSPECTION TYPE:C THROUGH THICKNESS CRACK FOUND AT BS 880 STR 9R TENSION TIE AT AFT ATTACHED TIE CLIP THE CRACK RUNNING AT UPWARD DIRECTION (CRACK LENGTH .125 INCH). M/DECK BS 880 STR 9R STRINGER ATTACH TIE CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT MODULE M306 INOP. LOCATED AT UPPER DECK STA 590. ITEM DEFERRED REFERENCE M343595. REPOSITIONED CEILING PANEL TO CORRECT PANEL POSITION. OPS CHECKED GOOD. THIS CLEARS M343595.

Part: PANEL — MISINSTALLED (CABIN)

FOUND EMERGENCY LIGHT M301 INOP. FOUND CEILING PANEL INSTALLED IN WRONG LOCATION. SWAP TO CORRECT. SWAPPED CEILING PANELS, HOOKED UP CORRECT C/P TO EMERG LIGHT MODULE. OPS CK GOOD.

Part: WINDOW FRAME — CORRODED (FUSELAGE)

FOUND CORROSION ON UPPER RT (F/O'S) R1 WINDOW FRAME. BEGAN REMOVAL OF CORROSION BY MECHANICAL MEANS AS PER SRM 56-10-01 & 51-10. REMOVED FILLER AND FAB'D NEW PART PER DWG 69B10705-1. OK TO INSTALL FILLERS. INSTALLED FILLERS PER SRM AND B747 52-30-02.

Part: BEAM — CRACKED (LT WING)

AC FERRIED FOR REPAIR, CRACK IN LT WING LEADING EDGE UPPER CHORD AT STA 952. CRACK HAS BEEN STOP DRILLED IAW MFG ENG INSTRUCTIONS. DEACTIVATED GROUP A LEADING EDGE FLAPS, NR D331311. R/R LE BULLNOSE SKIN IAW SRM 57-20-03, FIG 7; RMVD DMGD PART OF UPR. CHORD IAW SRM 57-20-3, STEP 4, FIG 7; FAB. UPR CHORD FILLER;ALODINED PRIMED TO RPR. PARTS IAW SRM 57-20-03; INSTLD FASTNERS IAW SRM 57-20 -03; R/R FAST. AT L/W #2 PDU SUPPORT FTG. IAW SRM 51-30-2; CLOSED CIRC. BRKS ON P6 PNL AFT L/E FLAP 1,2,3,4 & PRIMED L/E FLAPS.

Part: O-RING — WORN (L1 WINDOW)

INSPECTION TYPE:N/A ATB - IMMEDIATELY AFTER T/O SMOKE WAS SENSED IN C/P. SMOKE WAS COMING FROM THE AREA OF WINDOW L1. WINDOW HEAT WAS TURNED OFF. RAN CHECKLIST. FUEL WAS JETTISONED TO LANDING WT AND FLIGHT RETURNED TO ANC. FOUND TERMINAL-A LOOSE. REMOVED OLD O-RING. INSTALLED ALTERNATE O-RING PER GMM 3-6-9. OPS CHECK NORMAL IAW MM 30-41-01.

Part: STRUCTURE — CRACKED (CARGO DOOR)

FOUND CRACK IN FWD LWR CARGO DOOR STRUCTURE. A/C WILL FERRY TO PAE. STOP DRILLED END OF CRACK TO .250 DIA HOLE. ROUTED OUT CRACK. RE- WORK OUTER SKIN TO INITAL CONTOUR IAW SRM 52-30-06. HFEC THE STOP DRILL HOLE. FABRICATED WEB REPAIR DOUBLER. ALODINE/PRIMED ALL BARE METAL. PRIMED DOUBLER IAW MM 41-24-11. INSTALLED REPAIR DOUBLER. OPS TEST CARGO DOOR & WARNING SYSTEM-OPS GOOD. D326253 CLEARED

Part: ANGLE — CORRODED (CARGO DOOR)

AFT LWR CARGO PIT DOOR OPENING AND FWD LWR CORNER HAS CORRODED ANGLE REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE IAW BOEING DRAWING 65B04642. OK TO INSTALL. INSTALLED ANGLE AND FASTENERS IAW 51-10-01.

Part: STIFFENER — CRACKED (NLG WW) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NWW, RT SIDEWALL PANEL BS 280-300 1ST STIFFENER (COUNT FROM TOP) FOUND CRACK AT RADIUS APPROX 1/4" LONG. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (NLG WW) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NWW, LT SIDEWALL PANEL BS 300-320 4TH STIFFENER (COUNT FROM TOP) FOUND 9 INTERMITTENT CRACKS AT RADIUS (CRACK LENGTH 3/8" AND 1/2" 9 LOCATIONS) STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: WEB — CRACKED (NR 3 PYLON) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NR 3 PYLON REAR MOUNT B/H FWD AND AFT OB FRAME WEB FOUND CRACKS. ( FWD FRAME .3125 INCH AND 1.375 INCHES ) ( AFT FRAME .1875 INCH AND 1INCH ) NR 3 PYLON REAR MOUNT B/H REPAIRED IAW HX RS NR R54-53-35416 AND UPS ENGINEERING FILE NR 747-54-20053.

Part: FLOORBEAM — CRACKED (BS 340) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C U/D BS 340 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE 6 FLOOR PNL ATTACH HOLES FOUND CRACKED BETWEEN RBL 10" - RBL 45" (CRACK LENGTH 0.060" ). U/D BS 340 RBL 3" TO RBL 50" FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE CRACK HOLES REPAIRED AS PER EO NR B747-5320-12407 FIG 3 PLAN C.

Part: STIFFENER — CRACKED (NLG WW) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NOSE W/W LT SIDEWALL PANEL BS 280-300 2ND STIFFENER (COUNT FROM TOP) FOUND CRACK AT RADIUS APPROX 9" LONG (CRACK LENGTH 9"). NOSE W/W LT SIDEWALL PANEL BS 280-300 2ND STIFFENER REPLACED IAW SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (NLG WW) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NWW, RT SIDEWALL PANEL BS 300-320 4TH STIFFENER (COUNT FROM TOP) FOUND CRACK AT RADIUS APPROX 1/4" LONG. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (NLG WW) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NWW, LT SIDEWALL PANEL BS 300-320 3RD STIFFENER (COUNT FROM TOP) FOUND CRACKS AT RADIUS APPROX 1/2" AND 1/8" LONG. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (NLG WW) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NOSE W/W RT SIDEWALL PANEL BS 280-300 4TH STIFFENER (COUNT FROM TOP) FOUND CRACK AT RADIUS APPROX 1/4" LONG. NOSE W/W RT SIDEWALL PANEL BS 280-300 4TH STIFFENER REPLACED IAW SRM 51-10-01 PG 9.

Part: FLOORBEAM — CRACKED (BS 380) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C U/D BS 380 FLOORBEAM UPPER CHORD FWD HORIZONATAL FLANGE 1EA FLOOR PANEL ATT HOLE FOUND CRACKED, CRACK LENGTH 0.060". U/D BS 380 RBL 61" TO RBL 71" FLOORBEAM UPPER CHORD FWD HORIZONATAL FLANGE REPAIRED AS PER EO NR B747-5320-12407 FIG 3 PLAN C.

Part: FLOORBEAM — DAMAGED (BS 340) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C COCKPIT BS 340 LBL 49" LBL 55" AND LBL 61" FLOORBEAM UPPER CHORD AFT FLANGE ANCHOR NUT SHORT EDGE MARGIN. COCKPIT BS 340 LBL 41" TO LBL 64" FLOORBEAM UPPER CHORD AFT FLANGE REPAIRED AS PER EO NR B747-5320-12407 FIG 2 PLAN B.

Part: STIFFENER — CRACKED (NOSE W/W) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NWW RT SIDE WALL PANEL BS 320-340 5TH (COUNT FROM TOP) STIFFENER FOUND CRACK AS RADIUS APPROX 5/8" LONG. NWW RT SIDEWALL PANEL BS 320-340 5TH STIFFENER REPLACED IAW SRM 51-10-01 PG 9.

Part: FLOORBEAM — DAMAGED (BS 340) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C COCKPIT BS 340 RBL 61" FLOORBEAM UPPER CHORD AFT FLANGE ANCHOR NUT HOLE FOUND SHORT EDGE MARGIN. COCKPIT BS 340 RBL 56 TO RBL 64 FLOORBEAM UPPER CHORD AFT FLANGE REPAIRED AS PER EO NR B747-5320-12407 FIG 2 PLAN B.

Part: STIFFENER — CRACKED (NLG WW) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NOSE W/W RT SIDEWALL PANEL BS 300-320 5TH STIFFENER (COUNT FROM TOP) FOUND CRACK AT RADIUS APPROX 3/16" LONG. NOSE W/W RT SIDE WALL PANEL BS 300-320 5TH STIFFENER REPLACED IAW SRM 51-10-01 PG 9.

Part: FLOORBEAM — DAMAGED (BS 380) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C COCKPIT BS 380 LBL 66" LBL 72" FLOORBEAM UPPER CHORD AFT FLANGE FOUND SHORT EDGE MARGIN, ANCHOR NUT HOLES. COCKPIT BS 380 LBL 61" - LBL 75" FLOORBEAM UPPER CHORD AFT FLANGE REPAIRED AS PER EO NR B747-5320-12407 FIG 2 PLAN B.

Part: FLOORBEAM — CRACKED (BS 340) · airframe 80,484 hrs · 17,793 cycles

U/D BS 340 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE 1 FLOOR PANEL ATTACHED HOLE FOUND CRACKED AT LBL 48". U/D BS 340 LBL 41" TO LBL 53" FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE CRACK HOLE REPAIRED AS PER EO NR B747-5320-12407 FIG 3 PLAN 'C'.

Part: FLOORBEAM — CORRODED (BS 400) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C U/D BS 400 RBL 40" - RBL 68" FLOORBEAM UPPER CHORD ANCHOR NUTS AREA FOUND CORROSION. CORROSION BLEND OUT 0.055" BY 2" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 400 RBL 33 TO MOST RT O/B FLOORBEAM UPPER CHORD REPAIRED IAW SRM 53-10-07 FIG 8.

Part: FLOOR SUPPORT — CRACKED (BS 340-360) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C COCKPIT BS 340-360 BL 0 FLOOR SUPPORT 'L' ANGLE FOUND CRACK, CRACK LENGTH 4". COCKPIT BS 340-360 BL 0 FLOOR SUPPORT 'L' ANGLE REPLACED AS PER SRM 51-10-01 PAGE 9.

Part: FLOORBEAM — CORRODED (BS 360) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C COCKPIT BS 360 LBL 12" - LBL 34" FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.065" BY 2" BY 3" EXCEED SRM 53-10-01 FIG 1 LIMITS, COCKPIT BS 360 LBL 4" TO LBL 42" FLOORBEAM UPPER CHORD REPAIRED IAW SRM 53-10-07 FIG 23.

Part: FLOORBEAM — SCORED (BS 360) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C COCKPIT BS 360 RBL 50" - RBL 54" FLOORBEAM UPPER CHORD SEVERAL SCORE MARK. COCKPIT BS 360 RBL 42" TO RBL 62" FLOORBEAM UPPER CHORD REPAIRED IAW SRM 53-10-07 FIG 23.

Part: FITTING — CRACKED (RT WING) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C RT WING, NR 8 SPOILER SUPPORT 'H' FTG I/B LOWER FLANGE CRACK 1" LONG. RHW NR 8 SPOILER SUPPORT 'H' FTG REPLACED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FRAME — CRACKED (NR 1 PYLON) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NR 1 PYLON NAC STA236 I/B VERTICAL FRAME BOTTOM CRACKED, CRACK LENGTH 2.75". VERTICAL FRAME REPLACED AS PER SRM51-10-01 P.9 AND INSTALLED AS PER SRM 51-30-02.

Part: CLIP — CRACKED (NLG W/W) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NLG W/W INTERNAL VERTICAL BEAM NR 6 CLIP CRACKED AT BS 320 RT (COUNT FROM TOP) CRACK LENGTH 3/4". NLG W/W INTERNAL VERTICAL BEAM ATTACH CLIP REPLACED AT BS 320 RT NR 6 (COUNT FROM TOP) IAW SRM 51-10-01 PG 9.

Part: INTERCOSTAL — CORRODED (BS 2300) · airframe 80,484 hrs · 17,793 cycles

BS 2300 RBL 60" FLOOR SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.034" BY 1" BY 1" EXCEED SRM 53-10-01 FIG 1 LIMITS, M/D BS 2300 TO BS 2320 RBL 60" FLOOR SUPPORT REPLACED IAW SRM 51-10-01 PAGE 9.

Part: FRAME — CRACKED (NR 4 PYLON) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NR 4 PYLON I/B SIDE OF NAC STA 236 VERTICAL FRAME CRACKED, JUST FWD OF PYLON VALVE, CRACK LENGTH : 2.5". VERTICAL FRAME REPLACED AS PER SRM 51-10-01 P.9 AND INSTALLED AS PER SRM 51-30-02.

Part: PANEL — BLISTERED (RH WING) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C RHW - IB MID FLAP LWR FLAP FOUND BULGED UP AT 95 INCHES - 135 INCHES FROM IB SIDE AS MARKED. TIME LIMITED REPAIR ACCOMPLISHED IAW HX RS NR R-57-55-35418 AND UPS EO NR B747-5750-23648-A.

Part: STIFFENER — CRACKED (KEELBEAM BOX) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C FX AIR CONDITIONING BAY KEEL BEAM BOX LT EXTERNAL VERTICAL STIFFENER FOUND CRACKED AT BS 983 LBL 9" LOWER AREA, CRACK LENGTH 2". FX AIR CONDITIONING BAY KEEL BEAM BOX AT BS 983 LBL 9" VERTICAL STIFFENER REPLACED IAW SRM 51-10-01 PG 9.

Part: VERTICAL BEAM — CRACKED (NLG WW) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NWW RT BS 280 VERTICAL BEAM WEB ONE EA STAND OFF HOLE FOUND CRACK JUST ABOVE WL 170, 3/16" RUNNING O/B 1/16" RUNNING I/B. NWW RT BS 280 VERTICAL BEAM WEB REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: SKIN — CORRODED (FWD CARGO DR) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C FWD CARGO DOOR EXTERNAL SURFACE NR 821FR ACCESS PANEL CUTOUT AREA BILGE UP AT UPPER HALF TOP AREA. CORROSION BLEND OUT 0.070 INCH X 1INCH X 4 INCHES FWD CARGO DOOR NR 821FR ACCESS PANEL CUTOUT INTEGRAL FLANGE TRIMMED OUT AND REPAIRED IAW HX RS NR R52-34-35419 AND UPS EO NR B747-5230-23649-A.

Part: STIFFENER — CRACKED (KEELBEAM BOX) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C FX- AIR CONDITIONING BAY KEEL BEAM BOX AT BS 983 RBL 9" VERTICAL STIFFENER CRACKED AT LOWER AREA, CRACK LENGTH 1.5". FX- AIR CONDITIONING BAY KEEL BEAM BOX AT BS 983 RBL 9" VERTICAL STIFFENER REPLACED IAW SRM 51-10-01 PG 9.

Part: PRESSURE BLKHD — CRACKED (NLG WW) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C NOSE W/W BS 400 BULKHEAD PRESSURE PANEL FOUND CRACKED, CRACK LENGTH 1/4". NOSE W/W BS 400 B/H PRESSURE PANEL REPLACED AS PER SRM 51-10-01 PAGE 9 AND INSTALLED AS PER BOEING DWG NR 624U0005 SHT 1 AND SHT 9.

Part: SKIN — CRACKED (EMPENNAGE) · airframe 80,484 hrs · 17,793 cycles

INSPECTION TYPE:C REF DMI# D305601 - INTERIM REPAIR TO FUSELAGE SKIN PUNCTURE AT FS 2565 (CRACK LENGTH 13"). SKIN AT BS 2553 - 2575 BETWEEN S46R AND S49R PERMANENT REPAIRED AS PER EO# B747-5330-22469-B APPENDIX B AND ZERO, TIME ALL FASTENER HOLES CARRIED OUT IAW SRM 51-10-01 PG 12.

Part: STRAP — BROKEN (O2 MASK)

CAPT'S O2 MASK SUPPORT STRAP BROKEN. REPLACED CAPT'S O2 MASK STRAP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY BATTERY PACK INOP FOR AFT 2 CEILING LIGHTS IN UPPER DECK. REPLACED EMERGENCY BATTERY PACK M335. OPS CHECK GOOD PER 33-51-00 PG 501.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY EXIT)

INSPECTION TYPE:N/A, EMERGENCY EXIT SIGN ABOVE UPPER DECK EMERGENCY EXIT DOOR INOP. REMOVED AND REPLACED BATTERY PACK (M312), OPS CHECK GOOD, MM 33-51-04.

Part: BATTERY PACK — FAULTY (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT SIGN ABOVE ESCAPE SLIDE INTERMITTENT REQ A829506. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD PER 747 MM 33-51-04.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

AFT 2 EMERGENCY LIGHT IN CEILING PASSENGER SEAT AREA COMES ON MOMENTARILY THEN GO OUT WHEN SWITCH PLACED IN ON POSITION. REMOVED AND REPLACED POWER SUPPLY MODULE IAW MM 33-51-00 AND MM 33-57-04. OPS CHECK GOOD. EMERGENCY POWER SUPPLY INSTALLED STA 650.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, RT BS 1241 REAR SPAR UPPER SPLICE PLATE CRACK FOUND AT HOLE NR 6, APPROX 0.090 INCH IN LENGTH RUNNING AFT ( STR R28 TO R28) CRACKED HOLE REAMED TO 1.000 INCH IAW EO B747-5740-17032.

Part: PLATE — CRACKED (RT WING) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE PLATE (BS 1241)FOUND CRACK AT HOLE NR 5 APPROX 0.060 INCH. RT WING REAR SPAR UPR SPLICE PLATE HOLE NR 5 CRACK FREE AT 1.00 INCH WAS REPAIRED IAW EO B747-5740-17032.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, U/D- BS 420-440 LBL 36 INCH SEAT TRACK CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 1 INCH X 4 INCHES, EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPLACED IAW SRM 51-10-01 PG 8. AND CIC APPLIED IAW EO NR M-5100-2780E.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, U/D STA 744-745 RT 2A STRINGER END FOUND CRACKED. U/D STA 744-745 RT STRINGER 2A REPAIRED IAW SRM 53-10-03 FIG.10

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C U/D- STA 545-560 RBL 28 SEAT TRACK IB FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 1 INCH X 3 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED REF SRM 53-10-05 FIG 1A. AND CIC APPLIED IAW EO NR M5100-2780-E.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, U/D BS 420-460 LBL 56 INCHES SEAT TRACK CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 2 INCH X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPLACED IAW SRM 51-10-01 PG 8, AND CIC APPLIED IAW EO NR M-5100-2780E.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, U/D BS 405-440 LBL 75-78, FLOOR SUPPORT ANGLE CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.050 INCH X 2 INCHES X 2 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 435- BS 440 FLR SUPPORT ANGLE REPAIRED REF SRM 51-40-04 FIG 3, CIC APPLIED IAW EO M-5100-2780-E.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, U/D: BS 630-760 LBL 28 INCH SEAT TRACK CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.060 INCH X 1 INCH X 20 INCHES, EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS630 - BS650 LBL 28 INCH SEAT TRACK REPAIRED REF. SRM 53-10-05 FIG 1A. AND CIC APPLIED IAW EO NR M-5100-2780-E.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, U/D- STA 595-602 RBL 47 INCHES SEAT TRACK FOUND CRACK. U/D- STA 590- STA 650 RBL 47 INCHES SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE:C U/D BS 613 RBL 9 INCHES, SEAT TRACK LIP 2EA BROKEN. U/D BS 610-650 RBL 9 INCHES, SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 4.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, U/D STA 516-517 LT NR 4 STRINGER END FOUND CRACK. U/D STA 516-517 LT NR 4 CRACKED STRINGER REPAIRED IAW SRM 53-10-03 FIG 3.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, M/D- BS 1350-1370 RT STR 6 FOUND CRACKED AS MARKED. M/D- BS 1350-1370 RT STR 6 REPAIRED IAW SRM 53-10-03 FIG.5.

Part: STRAP — CORRODED (FUSELAGE) · airframe 771,311 hrs · 7,128 cycles

INSPECTION TYPE: C, FX- BS 1241 LEFT WL 174-170 BETWEEN FX EXTERNAL INTERNAL LONGERON AREA FITTING ATTACH SPLICE STRAP FOUND CORROSION AS MARKED. CORROSION BLEND OUT WITH REMAIN THICKNESS 0.100 INCH REFER SB 747-53-2283 R4 SPLICE STRAP REPLACED EO B747-5310-1093-N.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, M/D BS 980-1000 RT STR 14 STR END FOUND CRACKED. M/D BS 980-1000 STR 14R REPAIRED IAW SRM 53-10-03 FIG. 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE:C U/D BS 560-590 LBL 29 INCH SEAT TRACK FLANGE CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 1 INCH X 20 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED REF SRM 53-10-05 FIG 1A. CIC APPLIED IAW EO NR M5100-2780-E.

Part: CLIP — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, BS 2040 LT FRAME ATT TIE CLIP FOUND CRACKED AT STR 24. M/D BS 2040 LT FRAME ATTACH CRACKED TIE CLIP AT STR 24 REPLACED IAW SRM 51-10-01 P8.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, BS 1520 RT FRAME SHEAR TIE FOUND CRACKED AT STR 21. SHEAR TIE REPLACED IAW SRM 51-10-01 P8 AT M/D BS 1520 RT FRAME STR 21R.

Part: SHEAR TIE — CRACKED (CENTER TANK) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C CTR TANK FRONT SPAR LOWER CHORD SHEAR TIE FOUND CRACKED AT LBL 65. SHEAR TIE REPLACED IAW SRM 51-10-01 PG 8.

Part: SHEAR TIE — CRACKED (CENTER TANK) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE:C CTR TANK FRONT SPAR LOWER CHORD SHEAR TIE FOUND CRACKED AT RBL 80 IN. SHEAR TIE FTG REPLACED IAW SRM 51-10-01 PG8.

Part: SHEAR TIE — CRACKED (CENTER TANK) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT RBL 35. SHEAR TIE FTG REPLACED IAW SRM 51-10-01 P. 8.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, M/D- BS 2160 STR 2L, FRAME ATT. TIE CLIP FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 1 INCH X 2 INCHES, EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE CLIP REPLACED REF. SRM 51-10-01 P.8 , AND CIC APPLIED IAW EO NR M-5100-2780-E.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, M/D BS 2180-2200 LT STR 10 STR END FOUND CRACKED. M/D BS 2180-2200 LT STR 10 REPAIRED IAW SRM 53-10-03 FIG 13.

Part: SHEAR TIE — CRACKED (CENTER TANK) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE:C CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT LBL 75. SHEAR TIE REPLACED IAW SRM 51-10-01 P8.

Part: SHEAR TIE — CRACKED (CTR TANK) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT LBL 35 INCH CTR TANK FRONT SPAR UPPER CHORD, SHEAR TIE REPLACED AT LBL 35 INCH IAW SRM 51-10-01 PG 8.

Part: SHEAR TIE — CRACKED (CENTER TANK) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT RBL 10 IN. SHEAR TIE REPLACED IAW SRM 51-10-01 PG 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, M/D BS 380 STR 17L FRAME CRACKED. FRAME REPAIRED AS PER HX RS R53-12-35186 & UPS EO B747-5310-20989-A.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, M/D BS 400, STR 13-14R FRAME OB ATTACH, SHEAR TIE FOUND CRACKED. BS 400 STR 13-14R FRAME OB ATTACH SHEAR TIE REPLACED IAW SRM 51-10-01 PG 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, M/D- BS 500, STR 14R FRAME FOUND CRACKED. M/D BS 500 STR 14R CRACKED FRAME REPAIRED AS PER HX RS R53-12-35185 & UPS EO B747-5310-20988A.

Part: FRAME — CRACKED (M/D) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, M/D: BS 400 STR 15L FRAME CRACKED. M/D- BS 400 STR 15L CRACKED FRAME REPAIRED AS PER HX RS R53-12-35187 & UPS EO B747-5310-20990-A.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, LT BS 340 UPPER DECK FLOORBEAM FOUND TWO EACH FASTENER HOLES CRACKED AT FRAME WEB BS 340 LT UPPER DECK FLOORBEAM CRACKED FRAME WEB REPAIRED AS PER HX RS R53-12-35182 & UPS EO B747-5310-20986-A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE: C, LT BS 360 UPPER DECK FLOORBEAM FOUND ONE EACH FASTENER HOLE CRACKED AT FRAME WEB. FRAME REPAIRED AS PER HX RS R53-12-35184 & UPS EO B747-5310-20987-A.

Part: FLOORBEAM — CRACKED (FUSLEAGE) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE:C, RIGHT BS 340 UPPER DECK FLOORBEAM FOUND ONE FASTENER HOLE CRACKED AT FRAME WEB. FLOORBEAM REPAIRED AS PER HX RS R53-12-135182 & UPS EO B747-5310-20986-A.

Part: LONGERON — CORRODED (RT MLG) · airframe 77,131 hrs · 17,128 cycles

INSPECTION TYPE:C, RT MLG WW OVERWING LONGERON UPPER SURFACE CORROSION REVEALED AT STA 1335, RBL 126. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.230 X 3.5 X 3.5 INCH, EXCEED SRM 53-10-01 FIG 1 LIMITS, LONGERON REPAIRED PER HX RS R53-41-35194 & UPS EO B747-5310-21016-A. CIC APPLIED IAW EO M5100-2780-E.

Part: FIRE WARNING — FALSE INDICATION (NR 3 ENGINE)

FIRE INDICATION ON NR 3 ENGINE. EXECUTED FIRE IN FLIGHT SHUTDOWN. BOTH FIRE BOTTLE DISCHARGED. INITIALLY OBTAINED FIRE DETECTION LIGHT ON FWD PANEL COUPLED W/FAULT LIGHT ON DET PANEL. ENG FIRE TEMP SENSOR IN ORANGE, INCREASING EMERGENCY RED FIRE HANDLE ILLUMINATED. T/S PER WDM 26-11-03 PG A1. CLEANED UP CONN DM219. NR 3 ENG FIRE INDICATION BACK TO NORMAL. REMOVED AND REPLACED NR 3 ENG BOTH FIRE BOTTLE & SQUIB PER MM 26-21-03. A/C OKAY FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT AFT OF LAV DOOR INOP. DEF M283794. REPLACED BATTERY PACK LIGHT, OPS CHECK NORMAL. THIS CLEARS M238794.

Part: COVER — BROKEN (EMERGENCY LIGHT)

EMERGENCY LIGHT JUST AFT OF LAV DOOR ON CEILING IS INOP. FOUND LIGHT COVER ASSEMBLY BROKEN. ORDERED LIGHT COVER ASSEMBLY EMERGENCY LIGHT DEFERRED PER MEL 33013. PLACARD INSTALLED.

Part: CHECK VALVE — STUCK (CABIN PRESSURE)

DECOMP LIGHT AND ALT WARNING HORN 10000 ALT CAME ON AT ALT 22000. ACCOMPLISHED RAPID DECOMP AND EMERGENCY DESCENT. CHECK LIST BUMP PUEL ATB FOUND PNEU GROUND CONNECT CHECK VALVE INTERMITTENT, STUCK OPEN POS. REMOVED AND REPLACED PNEU GND CONNECT CHECK LEFT VALVE AND CHECKED O.K. IAW MM 36-11-14ALL DOOR SEALS AND PERFORMED EXCESSIVE CABIN PRESSURE LEAKAGE CONDITION INSP COMPLETE IAW AMM 05-51-08 P201. AND PRESS CONT SYS TEST O.K IAW AMM 21-31-00P 501

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE :AS BOTH UPPER DECK SERVICE DOOR UPPER SILL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ASSY. RELAMPED AS REQUIRED IAW 33-00.

Part: FUSE — BLOWN (EMERGENCY LIGHT)

INSPECTION TYPE: AS-E, EMERGENCY LIGHT FIXTURE L1854 IN L1 DOOR SILL INOPERATIVE. RELAMP NO HELP. REPLACED FUSE IN EMERGENCY LIGHT ASSY AND OPS CHECKED NORMAL IAW MM33-51 -07.

Part: SKIN — CORRODED (PAX DOOR) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C, MAIN DOOR - R4 DOOR UPPER HINGE CUTOUT LOWER WEB FOUND CORROSION CRACKED. M/D - R4 DOOR UPPER HINGE CUTOUT LWR WEB REPLACED AS PER SRM 51-10-01 P8.

Part: DOOR FRAME — CRACKED (R5 DOOR) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C, R5 DOOR FWD LOWER CORNER CRACK FOUND AT VERTICAL RADIUS AS MARKED. LWR CORNER REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C L4, DOOR FWD LOWER CORNER CRACK FOUND AT VERTICAL RADIUS AS MARKED. LWR CORNER REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C, FWD CARGO BAY, STA 720 - 740 STRINGER 47 RT FOUND CORROSION CRACK. CORROSION BLEND OUT 0.030 INCH X 1 INCH X 1 INCH EXCEED SRM LIMIT. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD CORNER HINGE FITTING ATTACH FASTENER HOLES ONE EACH HOLE FOUND CRACK AT SKIN 5 O'CLOCK POSITION .125 INCH LENGTH THRU THICKNESS REFER ATTACHED DRAWING FOR DETAILS. AFT CARGO DOOR CUTOUT FWD CORNER SKIN REPAIRED AS PER HX RS R-53-61-34990 & UPS EA B747-53-20128.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C, RIGHT BS 2231 2 EA FASTENER HOLE CRACK REVEALED ON STRAP BELOW STR 25R REFER FIGURE ATTACHED. M/D - RIGHT BS 2231 STR 25 REVEAL PANEL STRAP REPAIRED AS PER SRM 53-10-04 FIG 115.

Part: SPAR — CORRODED (LT WING MLG WW) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C, LT WING MLGWW BS 1241 LBL 'O' PRESSURE BULKHEAD REAR SPAR ATT T-CHORD FOUND SURFACE CORROSION. T-CHORD REPLACED AS PER SRM 51-10-01 PG 8. (DEPTH 0.060 INCH, WIDTH 1 INCH, LENGTH 1 INCH).

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,562 hrs · 16,470 cycles

KEEL BEAM BOX EXTERIOR LOWER I/B SURFACE FOUND SURFACE CORROSION AT STA 1383 TO STA 1405 LBL 7. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND SRM 51-10-02, BLEND OUT DEPTH 0.008 INCH, WIDTH 1 INCH, LENGTH 3 INCHES WITHIN SRM 53-10-01 LIMITS. (DEPTH 0.040 INCH, WIDTH 1 INCH, LENGTH 2 INCHES).

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE:N/A FX - KEEL BEAM BOX EXTERIOR I/B SURFACE FOUND SURFACE CORROSION AT STA 1416 TO STA 1456 LBL 7. (DEPTH 0.055 INCH, WIDTH .75 INCH, LENGTH .75 INCH). CORROSION REMOVED AND REPROTECTED AS PER SRM AND SRM 51-10-02 BLEND OUT DEPTH 0.009 INCH, WIDTH 1 INCH, LENGTH 3 INCHES WITHIN SRM 53-10-01 LIMITS.

Part: FITTING — CRACKED (LH BS 1480 B/H) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE:C LH BS 1480 B/H - CRACKS REVEALED ON THE OUTER CHORD SPLICE FITTING HOLE #23 RUNNING I/B & O/B & ALL GREATER THAN 0.100" LONG. PLS REFER FIGURE ATTACH. OUTER CHORD SPLICE FITTING HOLE #23 CRACK OUT OF SB 747-53A2390 LIMIT FITTING REPLACED AS PER 747-53A2390 AND EO B747-5310-10732-I.

Part: FITTING — CRACKED (BULKHEAD) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C, LT BS 1480 BULKHEAD CRACK REVEALED ON EXTENSION FITTING HOLE NR 5 APPROX 0.06 INCH LONG RUNNING UPWARD. PLS REFER FIGURE ATTACH. LT 1480 BULKHEAD EXTENSION FITTING HOLE NR 5 REWORKED TO 0.800 AND BUSHING INSTALLED AS PER RS 53-34989.

Part: LONGERON — CORRODED (FWD CARGO COMPT) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE:C FWD CARGO COMP - STA 740 S47R STINGER SPLICE HEAVY CORROSION REVEALE D STRINGER SPLICE REPLACED AS PER SRM 51-10-01 P.8. (DEPTH 0.040", WIDTH 1", LENGTH 2")

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE:C U/D - SEAT TRACK FOUND HEAVY CORR. CORROSION BLEND OUT 0.048"X1"X2" SEAT TRACK REPAIRED AT U/D BS 570 - BS 710 LBL 47" AS PER SRM 53-10-05 FIG 1A.

Part: STRAP — CRACKED (FUSELAGE) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C, CRACKS FOUND AT BS 2231 RT INBOARD ATTACHED STRAP, THE CRACKS RUNNING FWD AND AFT DIRECTION OF ONE EACH FASTENER HOLE AND CRACKED THROUGH THICKNESS. M/D - RIGHT BS 2231 STR 24-25 REVEAL PANEL STRAP REPAIRED AS PER SRM 53-10-04 FIG 115.

Part: BRACKET — CRACKED (STR 25L BS 2231) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE:C FWD CRACKS WITH THROUGH THICKNESS FOUND AT ONE EACH FASTENER HOLE AT TIE CLIP AT THE I/B CHORD AT STR 25L OF BS 2231. TIE CLIP REPLACED AT BS 2231 STR 25L AREA AS PER SRM 51-10-01 PG.8.

Part: BULKHEAD — CORRODED (LT MLG WW) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C, LT WING MLGWW - BS 1241 LBL 1 TO LBL 8 PRESSURE BULKHEAD WEB FOUND CORROSION AT BRACKET ATT SURFACE. CORROSION BLEND OUT (0.068 X 2 X 8 INCH) NOT WITHIN SRM 57-10-01 LIMITS, FOR REPAIR REER HX RS NR R53-43-34986 & UPS EA 747-53-20125.

Part: BULKHEAD — CORRODED (RT MLG WW) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C, RT WING MLG WW - BS 1241 WING CENTER SECTION REAR SPAR PRESSURE BULKHEAD WEB SURFACE FOUND CORROSION AT RBL 1 TO RBL 6 BRACKET ATT SURFACE. CORROSION BLEND OUT (0.070 X 2 X 8 INCH) NOT WITHIN SRM 57-10-01 LIMITS FOR REPAIR REFFER RS NR R53-43-34986 & UPS EA 747-53-20125.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE:C U/D SEAT TRACK FOUND HEACY CORR AS MARKED. CORROSION BLEND OUT 0.055"X1"X3" SEAT TRACK REPLACED AT U/D BS 480 - BS 530RBL 65 AS PER SRM 51-10-01 P.8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C U/D - FLOOR SUPPORT FOUND HEAVY CORROSION. FLOOR SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 8. (DEPTH 0.060 INCH, WIDTH 1 INCH, LENGTH 2 INCH).

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C, AFT LOWER CARGO DOOR CUTOUT UPPER CORNERS TWO FASTENER HOLES FOUND CRACK REVEALED FWD CORNER CRACKED HOLE AT SKI AND BEAR STRAP LAYER. AFT CORNER CRACKED HOLE AT BEAR STRAP LAYER. FOR DETAIL PLS REFER ATTACHED SKETCH. FWD UPPER CORNER REPAIRED AS PER HX RS R53-61-34990 & AFT UPPER LOWER REPAIRED AS PER HX RS R53-61-34981 & UPS EA 747-53-20127 & B747-53-20128.

Part: BRACKET — CORRODED (LT MLG WW) · airframe 73,562 hrs · 16,470 cycles

INSPECTION TYPE: C, LT MLG WW - BS 1241 LBL 1 TO 8 HORIZONTAL BRACKET FOUND CORROSION CRACKED. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM LIMIT. BRACKET REPLACED AS PER SRM 51-10-01 PAGE 8 TOTALLY 2 EA (P/N: 65B82011-3 AND 69B11570-1).

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,143 hrs · 15,580 cycles

INSPECTION TYPE: C, M/D - BS 1840 BETWEEN STR 12R AND 14R ATT FRAME FOUND CRACKED. BS 1840 BETWEEN STR 12R AND 14R FRAME I/B CRACKED AREA REPAIRED PER SRM 53-10-04 FIGURE 87.

Part: SKIN — CORRODED (STA 975-987) · airframe 65,143 hrs · 15,580 cycles

INSPECTION TYPE:C FX - LOWER FUSELAGE EXTERNAL SKIN EDGE FOUND CORRROSION CRACKED AT STA 983 STRG 42L. FX - LOWER FUSELAGE STA 975 TO STA 987 S42L EXTERNAL SKIN REPAIRED AS PER SRM 53-30-03 FIG.1.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT EMERG LIGHTS UNARMED LIGHT INOP RELAMPED. OPS CK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

INSPECTION TYPE: PFLT, UPPER DECK PASSENGER AREA 3 EA CEILING EMERGENCY LIGHTS INOP. REF L/P 914473, M249145. REPAIRED GROUND WIRE W894-L4734-20 PULLED FROM SOCKET CONTACT AT D5127P. TEST OK. THIS CLEARS M249145

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE: PFLT, UPPER DECK CEILING EMERGENCY LIGHTS AT STA 590 AND STR 710 INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK M335. OPS TEST NORMAL.

Part: SKIN — CRACKED (NR 3 PYLON)

INSPECTION TYPE: ASV NR 3 PYLON INBD SIDE AFT AND BELOW "TEXAS" DOUBLER PREVIUOS REPAIR SHO WS EVIDENCE OF CRACK EXTENDING UPWARD FROM REPAIR.(MARKED). VERIFIED END OF CRACK WITH HFEC G. BUCHERT QC 10445. REMOVED DOUBLER . HS 86801 11 10 02. STOPDRILLED CRACK, H.S. 86801 11-10-02. VERIFIE D STOP DRILL G. BUCHERT QC 10445. INSTALLED A REPAIR DOUBLER AS PER SRM 54-34-03.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A MAIN CARGO DECK CEILING EMERGENCY LIGHT JUST OUTBD OF FWD ENTRY INOP ALSO FWD DOOR FRAME EMERG LIGHT INOP REMOVED AND REPLACED LT ASSY PER AMM33-51-04 AND RELAMPED LIGHT OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE: ASV EMERGENCY LIGHT ON UPPER DECK ABOVE STAIRS INOP. RELAMPED OPS CHECKED GOOD.

Part: BULKHEAD — CRACKED (#3 NACELLE) · airframe 72,032 hrs · 16,183 cycles

INSPECTION TYPE:SPC NR 3 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD CRACK REVEALED AT O/B FWD & AFT WEB AREA APPROX AT 5 O'CLOCK POSTION. NR 3 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD CRACKED AREA REPAIRED PER HX RS R-54-53-34827 WITH REPAIR KIT INSTALLED PER REPAIR DWG 65B07 582 SHT 8.

Part: LIGHT — INOPERATIVE (EXTERIOR)

INSPECTION TYPE:N/A EXTERIOR ESCAPE SLIDE LIGHT INOP.

Part: FLAP — CRACKED (RT WING)

INSPECTION TYPE:PFLT RT I/B TRAILING EDGE OF AFT FLAP HAS CRACK IN COMPOSITE POSSIBLE DELAMINATION O/B OF I/B CANOE, MARKED. INSPECTED AREA AND SPEED TAPED PER EO B747-5750-15750-A. REINSPECT AT 50 DAY INTERVALS AND PERMANENT REPAIR NO LATER THAN C-CHECK.

Part: FITTING — CRACKED (R1 DOOR) · airframe 69,723 hrs · 15,709 cycles

INSPECTION TYPE:C M/D - R1 DOOR, DOOR AFT CUTOUT MOST LOWER STOP FITTING CRK. R1 DOOR AFT CUTOUT MOST LOWER STOP FITTING REPLACED AND DR STOP ADJUSTMENT AS PER MM 52-11-01, LOW GATE ASSY INSTALLATION AND RIGGING PER MM 52-09-00 AND SRM 51-10-01

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,383 hrs · 14,839 cycles

INSPECTION TYPE:C2 U/D BS 320 BETWEEN STR 2L AND 3L WEB CRACKED. REPAIRED FRAME WEB PER SRM 51-40-02. (NDT CONFIRM NO CRACK BEYOND STOP HOLE AFTER STOP HOLE DRILLED PER SRM 51-10-01).

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,383 hrs · 14,839 cycles

INSPECTION TYPE:C-2 M/D L5 DOOR FWD CUTOUT BETWEEN STR 15 & 16 CUTOUT CRACKED. REPAIRED L5 DOOR FWD UPPER CUTOUT AS PER SRM 53-10-04 FIG 91.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,383 hrs · 14,839 cycles

INSPECTION TYPE:C2 U/D BS 380 STR 6L AND 7L FRAME INNER CHORD CRACKED. REPAIRED FRAME INNER CHORDS & WEB AS PER SRM 53-10-04 FIG 98 (NDT C/OUT PER NDT MANUAL PT.6, 51-00-00 FIG04 CONFIRMED; RESULT: NO CRACK REVEALED AT TRIM OFF AREA NO CRACK BEYOND STOP HOLE ).

Part: WEB — CRACKED (FUSELAGE) · airframe 61,383 hrs · 14,839 cycles

INSPECTION TYPE:C-2 U/D BS 330 STR 12L ATT WEB CRACKED. REPAIRED WEB AS PER SRM 51-40-02.

Part: STRINGER — CRACKED (BS 280) · airframe 69,723 hrs · 15,709 cycles

INSPECTION TYPE:C NOSE - W/W TUNNEL BS 280 STR 41R STRINGER FOUND CRACKED. NOSE W/W TUNNEL BS 280 STR 41R REPLACXED AS PER SRM 51-10-01

Part: DOUBLER — CRACKED (R4 DOOR) · airframe 69,723 hrs · 15,709 cycles

INSPECTION TYPE:C M/D- R4 DOOR FWD CUTOUT BTN STR 24 X 25 CUTOUT CRK. FABRICATED / REPAIRED / INSTALLED DOUBLERS PER SRM 53-10-04 FIG 84.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 69,723 hrs · 15,709 cycles

INSPECTION TYPE:C NLG WW, BS 400 PRESSURE PAN CRACK FOUND APPROX 1 INCH LONG. NLG WW BS 400 BULKHEAD PRESSURE PAN REPLACED AS PER SRM 51- 10-01 AND INSTALLED AS PER BOEING DWG 624U0005 SHT 1 - 9.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,723 hrs · 15,709 cycles

INSPECTION TYPE:C M/D L1 DOOR FWD CUTOUT FRAME LWR REVEAL FOUND CRACKED AS MARKED. FASTENERS OF L1 DOOR FWD CUTOUT FRAME LWR REVEAL INSTALLED AS PER MM 52-11-01 AND SRM 51-10-01 FOR LWR REVEAL REPLACEMENT DONE, DR RIGGING AND OPERATIONAL TEST DONE FOUND " SATIS " PER MM 52-11-01.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,723 hrs · 15,709 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,723 hrs · 15,709 cycles

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

Part: HANDLE — MALFUNCTIONED (EMERGENCY DOOR)

INSPECTION TYPE:N/A UPPER DECK EMERGENCY ESCAPE DOOR HANDLE INTERMITTENTLY DOES NOT STOW ONCE OPENED, THIS DOES NOT LET THE DOOR OPEN NORMALLY. THE EXTERIOR HANDLE JAMS INTO DOOR SILL. OPS CHECKED DOOR PER MM 52-130 PG 9, CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A AFT EMERGENCY EXIT LIGHT AT CREW ENTRY DOOR L1 IS INOP R&R BATTERY ASSY PER 33-50-00 OPS CK OK

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A AFT EMERGENCY LIGHT AT CREW ENTRY DOOR L1 IS INOP EMERGENCY LIGHT BY CREW STAIRS (AFT) INOP R/R BATTERY ASSY ONLY, PER 33-50-00 OPS CHK OK

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:C, L1 DOOR EMERGENCY LIGHT INOP. REPLACED LAMP, OP CHECK NORMAL IAW MM CHAPTER 33.

Part: BATTERY PACK — MISSING (CABIN)

INSPECTION TYPE:N/A, AFT TWO CEILING MOUNTED EMERGENCY LIGHTS INOP ON UPPER DECK. FOUND POWER PACK MISSING. INSTALLED NEW POWER PACK. OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT OVER UPPER RT ESCAPE DOOR INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 31-51-04. OPS CHECK GOOD.

Part: LINE — NOT CLOSED (E/E BAY)

INSPECTION TYPE:C, AIR TURNBACK DUE TO FAILURE OF AIRSPEED AND ALTIMETER SYSTEM. AFTER DEBRIEF WITH CREW, FLS COMPLETED AN INSPECTION OF A/C, FOUND CAPT''S AND F/O''S PITOT DRAIN LINES UNCAPPED IN THE E & E BAY. THE FLAP SYS WAS OVERSPED. *S/D* CAPPED PITOT DRAIN LINES, OPS CHECK GOOD. COMPLETED INSPECTION OF OVERSPED FLAPS. REMOVED AND REPLACED BAD COMPONENTS ACCORDINGLY. A/C OK FOR SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, FRAME CRACKED AT STRINGER CUTOUT AT STA 500 LT, STR 11L. PLEASE REPAIR/RECTIFY. REPAIR ACCOMPLISHED IAW APPROVED REPAIR PER 8110-3. ALL THE ACTIVE CRACK TIPS WERE ELIMINATED. REINFORCING DOUBLERS AND FILLERS WERE INSTALLED PER SRM GUIDE LINES, REF SRM 53-10-04 FIG 22.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, FWD CARGO, EVIDENCE OF CORROSION FOUND ON STRINGER AT BS 984 STR 38 LT. STRINGER FABRICATED PER WORK SHOP ORDER E0169804 AND INSTALLED IAW SRM 51-30-02. REPAIR ACCOMPLISHED IAW SRM 53-10-03.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, CORROSION REMOVED FROM INNER SURFACE OF SKIN AT BS 2160 BETWEEN STR 48 - 49 RT. PLEASE CARRY OUT NDT INSPECTION OF AREA TO ENSURE REMOVAL OF CORROSION. CORRODED AREA CUT AWAY AND REPAIRED IAW SRM 53-30-03.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, CRACK IN FRAME WEB AT CUTOUT ,BS 460 STR 11 LT. REPAIR ACCOMPLISHED IAW SRM 53-10-04 AND APPROVED 8110-3 AS FOLLOWS. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, CRACK IN FRAME WEB AT STR CUT OUT, BS 480, STR 12 LT. PLEASE RECTIFY REPAIR AS FOLLOWS. REPAIR CARRIED OUT IAW SRM 53-10-04, FIG 22 AND APPROVED 8110-3 REP AIR SCHEME ALL ACTIVE CRACK TIPS WERE ELIMINATED. REINFORCING DOUBLERS AND FILLERS WERE INSTALLED PER SRM GUIDELINES.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK - CRACK IN FRAME WEB AT STR CUTOUT BS 480 STR 12 LT. REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 22, AND APPROVED 8110-3 REP AIR. ALL ACTIVE CRACKS WERE ELIMINATED. REINFORCING DOUBLERS AND FILLERS WERE INSTALLED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 360 STR 3 RT. REPAIR ACCOMPLISHED IAW SRM 53-10-04 AND APPROVED 8110-3 REPAIR AS DETAILED. THE CRACKED FRAME WAS REPAIRED BY STOP DRILLING BOTH CRACKS AND INSTALLING A REPAIR DOUBLER.

Part: BOLT — CORRODED (NR 3 FLAP TRACK) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, FLAP TRACK FWD FUSE BOLT CORRODED. REPLACED BOLT. NUMBER 3 FLAP TRACK FWD FUSE BOLT REPLACED IAW MM 27-51-25.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 500 STR 10 RT. REPAIR ACCOMPLISHED IAW SRM 53-10-04, FIG 22 AND APPROVED 8110-3 REPAIR SCHEME - ALL ACTIVE CRACKS ELIMINATED, REINFORCING DOUBLERS AND FILLER WERE INSTALLED PER THE SRM GUIDE LINES.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, FUSELAGE FRAME WEB IS CRACKED AT BS 480 STR 12 RT. REPAIR CARRIED OUT IAW SRM 53-10-04 AND APPROVED 8110-3 REPAIR, CRACK STOP DRILLED PER SRM 51-10-01, INSTALLED REPAIR DOUBLER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, FUSELAGE FRAME WEB IS CRACKED AT BS 360 BETWEEN STR 4 AND 5 LT. REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 8 AND APPROVED 8110-3 REPAIR. ALL ACTIVE CRACK TIPS WERE ELIMINATED BY STOP DRILLING. A REINFORCING DOUBLER WAS INSTALLED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 480 STR 13 LT. REPAIRED IAW SRM 53-10-04 FIG 22, AND APPROVED 8110-3, CRACKS STOPPED DRILLED AND REPAIR DOUBLER INSTALLED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, FUSELAGE FRAME WEB IS CRACKED AT CUT FOR STR AT BS 500 STR 11 RT. REPAIR ACCOMPLISHED IAW SRM 53-10-04, FIG 22 AND REPAIR DETAILED IN APPROVED 8110-3. ALL ACTIVE CRACK TIPS WERE ELIMINATED. REINFORCING DOUBLERS AND FILLERS WERE INSTALLED PER SRM GUIDE TO RESTORE THE ORIGINAL CAPABILITY.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 480 STR 10A RT. REPAIR CARRIED OUT IAW SRM 53-10-04, AND APPROVED 8110-3 AS FOLLOWS. STOPPED DRILLED IAW 51-10-01 AND INSTALLED REPAIR DOUBLER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C, UPPER DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 40 0 STR 11 LT. REPAIRED IAW SRM 53-10-04, FIG 20 AND APPROVED 8110-3 REPAIR AS DETAILED, THESE CRACKED FRAMES WERE REPAIRED BY STOP DRILLING CRACKS AND INSTALLING REPAIR DOUBLERS.

Part: BEAM — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, REF NRC''S 44269701, 44270124, 44269086, PLEASE REPAIR CRACKING IN LOWER CREASE BEAM CHORD. RT AND LT SIDES IN AREAS LISTED ON ABOVE NRC, CRACKING AT BS 320 - BS 360, STR 26 RT. TYPICAL FORM REPAIR ACCOMPLISHED IAW 51-40-01 AT BS 320 TO 360 STR 26 RT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 460 STR 11 RT. REPAIRED IAW SRM 53-10-04 FIG 20. STOP DRILLED IAW 51-10-01 AND REPAIR DOUBLER FITTED PER APPROVED 8110-3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, FUSELAGE FRAME WEB IS CRACKED AT CUT OUT FOR STR AT BS 420 STR 11 LT. REPAIR CARRIED OUT IAW SRM 53-10-04, AND APPROVED 8110-3 AS DETAILED. THESE CRACKED FRAMES WERE REPAIRED BY STOP DRILLING CRACKS AND INSTALLING REPAIR DOUBLERS.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 520 STR 11 RT. REPAIRED CRACKS AT BS 520 SRM 53-10-04, FIG 20. THE CRACKED FRAMES WERE REPAIRED BY STOP DRILLING CRACKS AND INSTALLING REPAIR DOUBLERS AND CLIPS. DETAILED IN APPROVED 8110-3 FOR SAID REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, UPPER DECK, FUSELAGE FRAME WEB CRACKED AT CUTOUT FOR STR AT BS 48 0 STR 11 RT. REPAIR CARRIED OUT IAW SRM 53-10-04, AND APPROVED 8110-3, REPAIR AS FOLLOWS. STOPPED DRILLED IAW 51-10-01 AND REPAIR DOUBLER INSTALLED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, FWD CARGO CRACK FOUND IN STRINGER 38 LT AT BS 500. NEW STRINGER SECTION FABRICATED IAW WORK SHOP ORDER E0098286, AND INSTALLED IAW SRM 51-30-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, FWD CARGO, CRACK FOUND IN STRINGER 37 LT BS 520. NEW STRINGER SECTION FABRICATED IAW E0098287 AND INSTALLED IAW SRM 51-30-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, MAIN DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 200 STR 14. REPAIR CARRIED OUT IAW SRM 53-10-04 AND APPROVED 8110-3, DETAILS OF REPAIR TEXT AS FOLLOWS. THESE CRACKED FRAMES WERE REPAIRED BY STOP DRILLING CRACKS AND INSTALLING REPAIR DOUBLERS AND CLIPS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, MAIN DECK, FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 240 STR 14 LT. REPAIR CARRIED OUT IAW SRM 53-10-04, FIG 14 AND CONTINUE WITH INSPECTIONS IN ACCORDANCE WITH SB 53A2265.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44, MAIN DECK, FUSELAGE FRAME WEB CRACKED AT CUTOUT FOR STR AT BS 200 STR 14 RT. REPAIR CARRIED OUT IAW SRM 53-10-04 AND APPROVED REPAIR DETAILED I N 8110-3.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 66,582 hrs · 15,080 cycles

INSPECTION TYPE:C 44 STR 39R AT STA 280 FOUND DAMAGED. STRINGER SECTION REPLACED IAW SRM 51-30-02.

Part: PANEL — CRACKED (RT WING)

INSPECTION TYPE:N/A, CRACK UPPER WING PANEL L/E RIGHT WING. *S/D* REPAIRED PER SRM 51-40-15.

Part: FAN — INOP (COCKPIT)

CREW PREFLIGHT, ELECTRIC ODOR UPPER DECK EQUIP COOLING FAN INOP. SWAPPED LEFT MAIN EQUIP COOL FAN WITH UPPER DECK AND DEFERRED.

Part: ENGINE — FAILED (NR 3)

INSPECTION TYPE:N/A, NR 3 ENGINE IN-FLIGHT SHUT DOWN DUE TO LOW OIL PRESSURE AND QUANTITY. ENGINE OIL QUANTITY WAS FULL AT TAKEOFF, AS FLIGHT PROGRESSED QUANTITY CONSUMPTION GREATER THAN 1 QUART PER HOUR. OIL PRESSURE DROPPED INTO YELLOW BAND. SHUT DOWN ENGINE AS PER AOM. REMOVED AND REPLACED NR 3 ENGINE IAW UPS TC 5000. OPS AND LK CHECKS GOOD.

Part: RETRACT MECH — MALFUNCTIONED (RT TE FLAP)

INSPECTION TYPE:N/A, ATB-OUTBOARD FLAPS RETRACTED UNCOMMANDED.

Part: PANEL — CRACKED (NR 4 PYLON)

INSPECTION TYPE:N/A, NR 4 PYLON PANEL CRACKED. REPAIRED PANEL IAW B747-5430-11517.

Part: BRAKES — OUT OF ADJUST (LANDING GEAR)

INSPECTION TYPE-N/A, MAIN A/C BRAKES VERY WEAK FROM BOTH CAPTS AND F/O'S POSITION. NORMAL BRAKE SOURCE SELECT SW, NO HELP. BRAKE PEDALS, CAPT AND F/O BOTTOM OUT WHEN TRYING TO STOP. ALL HYD SYS PRESSURES NORMAL. INSPECTED MAIN BRAKE SYS, FOUND CABLES TENSION ON LOW, ADJ CABLE SYS PER 32-41-00 PG 501, BRAKES OPS CHKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, TWO AFT EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACKS, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, ONE EMERGENCY LIGHT AT CREW SERVICE DOOR INOP. REMOVED AND REPLACED LIGHT AT CREW SERVICE DOOR, OPS CHECK GOOD.

Part: BULKHEAD CLIPS — CRACKED (BS 340)

INSPECTION TYPE-C, FOUND CRACK ON BULKHEAD ATTACH CLIPS AT STA 340 LT (3) MARKED ATTACHED TO NWW SIDE PANEL. CRACKED CLIPS REMOVED AND NEW CLIPS FABRICATED AS PER SRM 51-40-03 AND INSTALLED AS PER SRM 51-30-02, OBTAINED FROM STA STOCK.

Part: BULKHEAD CLIP — CRACKED (BS 340)

INSPECTION TYPE-C, FOUND CRACK ON BULKHEAD ATTACH CLIP AT STA 340 RT (2) MARKED. CRACKED CLIPS REMOVED AND NEW CLIPS FABRICATED AS PER SRM 51-40-03 AND INSTALLED AS PER 51-30-02.

Part: STRINGER — CRACKED (BS 1744)

INSPECTION TYPE-C, AFTER SPLICE REMOVED (NR 469307) CRACK FOUND ON STRINGER 10 RT AT STA 1744 APPROX 1 INCH LENGTH. TYPICAL SPLICE REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 5, NEW PORTION REPLACED.

Part: SUPPORT — CORRODED (BS 2260-2300)

INSPECTION TYPE-C, CORROSION ON SUPPORT FLOOR BETWEEN STA 2260 TO 2300 RBL 90 AT 5 RT DOOR AREA. TYPICAL SPLICE REPAIR CARRIED OUT IAW SRM 51-40-03.

Part: CLIP — CORRODED (BS 1680)

INSPECTION TYPE-C, CORROSION ON TIE CLIP IN STA 1680 AT STR 1 RT AREA. CORRODED TIE CLIP REMOVED, NEW TIE CLIP (P/N 65B38600-160) INSTALLED PER SRM 51-30-02, OBTAINED FROM STA STOCK.

Part: CLIP — CORRODED (BS 1640)

INSPECTION TYPE-C, CORROSION ON TIE CLIP IN STA 1640 AT STR 3 RT AREA. CORRODED TIE CLIP REMOVED, NEW TIE CLIP (P/N 65B38600-160) INSTALLED PER SRM 51-30-02, OBTAINED FROM STA STOCK.

Part: CLIP — CORRODED (BS 1540)

INSPECTION TYPE-C, CORROSION ON TIE CLIP IN STA 1540 AT STR 3 RT AREA. CORRODED TIE CLIP REMOVED, INSTALLED NEW TIE CLIP (P/N 65B38600-160) PER SRM 51-30-02, OBTAINED FROM STA STOCK.

Part: STRINGER — CORRODED (BS 2120-2140)

INSPECTION TYPE-C, CORROSION ON STR 3 LT BETWEEN STA 2120 TO 2140. DAMAGED SECTION OF STRINGER REMOVED. AREA CHECKED AND CLEANED. TYPICAL SPLICE REPAIR DONE IAW SRM 53-10-03 FIG 5 ANF FIG 6. FASTENERS OBTAINED FROM STA STOCK.

Part: STRINGER — CORRODED (BS 2100-2140)

INSPECTION TYPE-C, DEEP CORROSION ON STR 2 LT BETWEEN STA 2100 TO 2140. TYPICAL SPLICE REPAIR CARRIED OUT AS PER SRM 53-10-03 FIG 5 MATERIAL OBTAINED FROM STA STOCK.

Part: TIE CLIP — CORRODED (BS 2100)

INSPECTION TYPE-C, DEEP CORROSION ON TIE CLIP STA 2100 STR 2, 3 LT CORRODED TIE CLIP REMOVED. NEW TIE CLIP (P/N 65B38600-160) PER SRM 51-30-02, OBTAINED FROM STA STOCK.

Part: CLIP — CRACKED (BS 400)

INSPECTION TYPE-C, CRACK ON CLIP IN FLOORBEAM AT STA 400 LBL 20 AREA. CRACKED CLIP REMOVED, FABRICATED NEW CLIP IAW SRM 53-10-20 FIG 12 AND INSTALLED IAW SRM 51-30-02.

Part: SKIN — CRACKED (BS 440)

INSPECTION TYPE-C, CRACK AT 1 LT DOOR ON STA 440 AT STR 26 AREA. CRACKED ANGLE REMOVED, FABRICATED NEW ANGLE SAME AS ORIGINAL PER SRM 53-10-21, NEW ANGLE INSTALLED PER SRM 51-30-02, OBTAINED FROM STA STOCK.

Part: STRINGER — CORRODED (BS 1720-1760)

INSPECTION TYPE-C, DEEP CORROSION ON STR 3 LT INSTALLED NEW PORTION OF STRINGER (P/N 65B04368-129) AND TYPICAL SPLICE REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 5, FASTENERS OBTAINED FROM STA STOCK.

Part: WEB — CRACKED (BS 2240)

INSPECTION TYPE-C, CRACK ON WEB AT STA 2240 BETWEEN STR 16 TO 17, NR 5 PAX RT PAX DOOR AREA. CRACKED WEB REMOVED A NEW WEB MADE IAW SRM 53-10-23 FIG 1.

Part: STRINGER — CORRODED (BS 1680-1740)

INSPECTION TYPE-C, CORROSION ON STR 3 LT BETWEEN STA 1680 TO 1740. INSTALLED NEW PORTION OF STRINGER (P/N 65B04368-129) AND TYPICAL SPLICE REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 5, FASTENERS OBTAINED FROM STA STOCK.

Part: STRINGER — CORRODED (BS 2160)

INSPECTION TYPE-C, WEB OF STA 2160 BETWEEN STR 27L TO 27R IS DAMAGED. FABRICATED NEW WEB PER SRM 53-10-23 FIG 9, INSTALLED PER SRM 51-30-02, OBTAINED FROM STA STOCK.

Part: FRAME — CORRODED (BS 1920)

INSPECTION TYPE-C, S/M DEEP CORROSION ON UPPER CHORD FRAME STA 1920 RT SIDE BETWEEN STR 42 TO 43. UPPER CHORD REMOVED, FABRICATED NEW CHORD PER SRM 53-10-23, CHORD INSTALLED PER SRM 51-30-02, OBTAINED FROM STA STOCK.

Part: WEB FITTING — CRACKED (BS 1420)

INSPECTION TYPE-C, CRACK IN WEB FITTING RBL 10 STA 1420. NEW WEB FITTING INSTALLED IAW SRM 51-30-02, (P/N 654U6075-169).

Part: SKIN — CORRODED (BS 1060)

INSPECTION TYPE-C, CORROSION ON C/S UPPER SKIN STA 1060 UNDER RT STUB FRAME RBL 106 APPROX STUB FRAME. REMOVED CORROSION AND AREA ANTI-CORROSION TREATMENT. INSTALLED O/S HI-LOCKS BN R3836/96 WORK ACCOMPLISHED PER IAI EO MF-MAN-B747-57-14-84866 AND SRM 51-30-02.