N682UP

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING ARRIVAL SERVICE CK, FOUND A/C EMERGENCY LIGHTS INOP. REMOVED BATTERY PACK. REMOVED AND REPLACED MAIN ENTRY DOOR AFT LIGHT REF M/M CHAP 33-51-04 PG 205. OPS CK'D EMERGENCY LIGHT CKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS AT CREW SERVICE DOOR AND CABIN OVERHEAD INOP. CREW SVC DOOR SILL EMERG LT PWR PACK AND CABIN OVERHEAD CEILING EMERGENCY LT PWR PACK REPLACED. EMERGENCY LT SYSTEM, OPS CK NORMAL.

Part: FLOORBEAM — DAMAGED (BS 360) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C U/D RT BS 360 UPR DECK FLOORBEAM UPR CHORD AND FRAME ATTACHMENT AREA 1EA FASTENER HOLE FOUND OVAL AT UPR CHORD. U/D RT BS360 UPPER DECK FLOORBEAM UPPER CHORD REPAIRED AT LBL11 TO RT MOST OB AREA IAW SRM 53-10-07 FIG23.

Part: SKIN — CORRODED (CENTER WING) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D WING CTR SECTION UPPER SKIN CORROSION REVEAL AFTER PAINT STRIPPED AT ITEM 8,10,18A,18B,18D AND 19 PER BOEING ATTACHMENT. M/D WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35608 AND R57-14-35609 AND ENGINEERING FILE NUMBER 747-57-20121 AND 747-57-20118.

Part: SKIN — DENTED (BS 135-138) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C FX UPPER FUSELAGE EXTERNAL SKIN SURFACE FOUND DENT MARK AT STA135 TO STA138 STR9L TO STR14L. DENT 0.060 INCH X 1 INCH X 1INCH. FX BS135 TO BS138 BETWEEN STR9L TO STR14L AREA SKIN FLUSH REPAIRED IAW SRM 53-30-03 FIG 4 SUBSEQUENT INSPECTIONS ARE NOT NECESSARY FOR CATERGORY A REPAIR.

Part: DOUBLER — CRACKED (BS 840) · airframe 104,700 hrs · 26,436 cycles

M/D LT BS 840 TENSION TIE TO FRAME CONNECTION FOUND WEB DOUBLER 3 ADDITIONAL HOLES CRACKED, CRACK LENGTH 3/8". M/D LT BS 840 TENSION TIE TO FRAME ATTACHED DOUBLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 BETWEEN STR 9L TO STR 12L AREA.

Part: TEAR STRAP — CRACKED (BS 840) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D LT BS840 STR 10L SKIN AREA 1 FWD HOLE (JUST BELOW STR10L) FOUND CRACK AT TEAR STRAP APPROX 0.030" RUNNING FWD UPPER. M/D LT BS 840 STR 10L TEAR STRAP REPAIRED AS PER RS R53-25-35564 AND UPS EO B747-5310-25079-A.

Part: STRINGER — CRACKED (BS 840 S11L) · airframe 104,700 hrs · 26,436 cycles

LT BS 840 STR 11L STRINGER LWR HORIZ FLANGE CRACK AT AFT HOLE APPROX 0.030" RUNNING I/B. BS 830-850 STR11L REPAIRED AS PER SRM 53-10-03 FIG 4.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

MAIN E/E COMPT LT STRINGER S8L FOUND CRACKED AT STA 420 TO STA 440. CRACK LENGTH 2". STRINGER REPAIRED AS PER SRM 53-10-03 FIG 3.

Part: SKIN — CORRODED (BS 1180) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D CENTER SECTION UPPER SURFACE FOUND CORROSION AT BS 1180 RBL 98. CORROSION BLEND OUT 0.050" BY 2" BY 4" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35603 AND UPS ENGINEERING FILE NUMBER 747-57-20115.

Part: HINGE FITTING — CRACKED (RT WING SPOILER) · airframe 104,700 hrs · 26,436 cycles

RHW NR 11 SPOILER PANEL ACTUATOR HINGE FITTING AFT LOWER FLANGE I/B RADIUS, FOUND 1/8" CRACK. STOP HOLE DRILLED AS PER UPS EO# B747-5740-0511-B ITEM 8.2 (6)

Part: INTERCOSTAL — CRACKED (BS 1230) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C WING CENTER SECTION BS 1230 RBL 11 INTERCOSTAL FOUND CRACK, CRACK LENGTH 3/8". WING CENTER SECTION BS 1230 RBL 11" INTERCOSTAL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FRAME — DAMAGED (BS 340 S11-13AR) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C BS 340 RT FRAME WEB BETWEEN S11R AND S13A FASTENER HOLE IN POOR CONDITION AFTER SPLICE REMOVED. BS 340 RT FRAME POOR CONDITION HOLES AT THE EDGE OF THE FRAME CUTOUT AREA TRIMMED OFF AND FRAME REPAIRED AS PER RS R53-12-35567. CONTINUE INSPECTION ARE REQUIRED AS PER RS R53-12-35567 SHEET 2 ITEM C11 AND D3 AND UPS EO B747-5310-25138-A.

Part: FLOORBEAM — DAMAGED (BS 340) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C RT BS 340 UPPER DECK FLOORBEAM UPPER TEE O/B HOLE FOUND OVAL AT FRAME WEB. U/D RT BS 340 FLOORBEAM UPPER TEE ATTACHED FRAME OVAL HOLE OVERSIZED TO 1/4" AND REPAIRED AS PER RS R53-12-35567 (REFER NRC6234 FOR WORKING DETAIL) CONTINUED INSPECTION IS REQUIRED AS PER RS R53-12-35567 SHEET 2 ITEM C11 AND UPS EO B747-5310-25138-A.

Part: FITTING — BROKEN (R1 DOOR) · airframe 104,700 hrs · 26,436 cycles

R1 DOOR FWD LOWER STOP FTG BROKEN. R1 DOOR FWD LOWER STOP FTG REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 820 TO BS 840 TENSION TIE AT S10L ATT HORIZ SHEAR WEB FOUND CRACK, CRACK LENGHT 1". M/D BS 820 TO BS 840 TENSION TIE AT STR 10L ATTACH HORIZ SHEAR WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D - BS 820-840 TENSION TIE AT S10R AT HORIZ SHEAR WEB FOUND CRACK CRACK LENGTH 3/4". BS820-840 TENSION TIE AT STR 10R AREA AT HORIZ SHEAR WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SKIN — CORRODED (BS 1140-1143) · airframe 104,700 hrs · 26,436 cycles

BS 1140-1143 RBL 29-32 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.085" BY 2" BY 5" EXCEED SRM LIMIT. BS 1140-1143 RBL 29-32 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35604 AND UPS ENGINEERING FILE NUMBER 747-57-20103.

Part: SKIN — CORRODED (BS 1186-1214) · airframe 104,700 hrs · 26,436 cycles

BS 1186-1214 RBL 54-56 WING CTR SECTION UPPER SKIN CORROSION. CORROSION BLEND OUT 0.034' BY 1.5" BY 10" EXCEED SRM LIMIT. BS 1186-1214 RBL 54-56 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35594 FIG 7 AND UPS ENGINEERING FILE NUMBER 747-57-20100.

Part: SKIN — CORRODED (BS 1126-1130) · airframe 104,700 hrs · 26,436 cycles

BS 1126-1130 LBL103-107 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.074" BY 4" BY 4" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35586 AND UPS ENGINEERING FILE NUMBER 747-57-20114.

Part: SKIN — CORRODED (BS 1238-1240) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS1238-1240 RBL16-19 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.182" BY 2" BY 6" EXCEED SRM LIMIT. BS 1238-1240 RBL16-19 WING CTR SECTION UPPER SURFACE SKIN REPAIRED AS PER RS R57-14-35607 AND UPS EO B747-5730-25226-A.

Part: FITTING — DELAMINATED (BS 2598) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C EMP LT BS2598 B/H FRAME SUPPORT UNDER STAB HINGE SUPPORT FTG FOUND 1 HOLE WITH DELAMINATION AT FWD BACK UP FTG. HOLE REPAIRED AS PER RS R53-83-35558 AND UPS ENGINEERING FILE NUMBER 747-55-20003.

Part: SKIN — CORRODED (CENTER WING) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS1235-1238 RBL57-59 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.071" BY 2" BY 4" EXCEED SRM LIMIT. M/D BS 1235-1238 RBL57-59 WING CTR SECTION UPPER CORRODED AREA REPAIRED AS PER RS R57-14-35587 AND UPS ENGINEERING FILE NUMBER 747-57-20112A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C, AFT CARGO DOOR CUTOUT FWD DR HINGE 2EA HOLES CRACK AT FUSELAGE SKIN CRACK LENGTH : .0625 INCH AND 0.040 INCH. AFT CARGO DOOR CUTOUT FWD DOOR HINGE AREA. DOUBLERS REMOVED AND INSTALLED IAW SRM 51-30-02 FROM CRACKED SHIM REPLACED ONLY IAW SRM 51-10-01 PG9 AFT HFEC INSPECTION IAW NTM PART 6 51-00-00 FIG 16 AND 4. NO CRACK FOUND ON SKIN.

Part: WEB — CORRODED (BS 1160-1178) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS1160-1178 LBL11 WEB O/B FACE LWR AREA FOUND CORRODED. CORROSION BLEND OUT 0.020" X 3/4" BY 5" EXCEED SRM LIMIT. M/D BS 1140-1200 LBL11 WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

R5 DOOR FWD CUTOUT UPPER REVEAL CRACKED, CRACK LENGTH 1/2". R5 DOOR FWD CUTOUT UPPER REVEAL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG9 AND 51-30-02.

Part: SKIN — CORRODED (BS 1240) · airframe 104,700 hrs · 26,436 cycles

BS 1240 LBL60-66 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.063" BY 2" BY 2" EXCEED SRM LIMIT. BS 1240 LBL60-66 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35592 AND UPS ENGINEERING FILE NUMBER 747-57-20108.

Part: FITTING — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

M/D BS 802 LBL27 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.043" BY 1" BY 3" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.

Part: SKIN — CORRODED (BS 1080) · airframe 104,700 hrs · 26,436 cycles

BS 1080 LBL93 TO 96 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.073" BY 4" BY 4" EXCEED SRM LIMIT. BS 1080 LBL 93 TO 96 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35579 AND UPS ENGINEERING FILE NUMBER 747-57-20101.

Part: SKIN — CORRODED (BS 1195) · airframe 104,700 hrs · 26,436 cycles

BS 1195 LBL71-73 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.037" BY 3" BY 3" EXCEED SRM LIMIT. BS 1195 LBL71-73 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35576 AND UPS ENGINEERING FILE NUMBER 747-57-20099.

Part: SKIN — CORRODED (BS 1240) · airframe 104,700 hrs · 26,436 cycles

BS 1240 LBL49-53 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.161" BY 4" BY 7" EXCEED SRM LIMIT. BS 1240 LBL49-53 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35592 AND UPS ENGINEERING FILE NUMBER 747-57-20108.

Part: SKIN — CORRODED (BS 1182-1186) · airframe 104,700 hrs · 26,436 cycles

BS 1182-1186 RBL 67-70 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.047" BY 2.5" BY 4" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35616 AND UPS ENGINEERING FILE NUMBER 747-57-20123.

Part: SKIN — CORRODED (BS 1208-1210) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C BS 1208-1210 LBL26-28 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.056" BY 3" BY 3" EXCEED SRM LIMIT. BS 1208-1210 LBL 26-28 WING CTR SECTION UPPER SURFACE CORROSION AREA REPAIRED AS PER RS R57-14-35594 FIG 4 AND UPS ENGINEERING FILE NUMBER 747-57-20100.

Part: FITTING — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

M/D BS860 LBL55 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.026" BY 1/2" BY 3" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

M/D BS 900 LBL55 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.039" BY 1/2" BY 2" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.

Part: SKIN — CORRODED (BS 1140) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS1140 LBL106-108 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.028" BY 1" BY 3" EXCEED SRM LIMIT. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 ORIGINAL THICKNESS .0445" BLEND OUT DEPTH 0.028" BY 1" BY 3" WITHIN SRM 57-30-01 FIG 1 LIMITS. INSPECTION WITH 10X MAGNIFING GLASS.

Part: FLOORBEAM — CORRODED (BS 760) · airframe 104,700 hrs · 26,436 cycles

BS 760 LBL83-90 FLOORBEAM UPPER SURFACE CORROSION. CORROSION BLEND OUT 0.050" BY 1.5" BY 7" EXCEED SRM LIMIT. BS760 LBL65 TO LT O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 3.

Part: FITTING — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

M/D BS 978 RBL28 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.027" BY 0.5" BY 2" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.

Part: FLOORBEAM — CORRODED (BS 1020) · airframe 104,700 hrs · 26,436 cycles

BS 1020 LBL 13-26 FLOORBEAM UPPER SURFACE FOUND CORROSION BLEND OUT 0.031" BY 1" BY 10". BS 1020 L11"-L33" FLOORBEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SKIN — CORRODED (BS 1140-1144) · airframe 104,700 hrs · 26,436 cycles

FOUND BS 1140-1144 RBL12-14 WING CTR SECTION UPPER SKIN CORROSION. CORROSION BLEND OUT 0.120" BY 5" BY 5" EXCEED SRM LIMIT. BS 1140-1144 RBL12-14 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35591 AND UPS ENGINEERING FILE NUMBER 747-57-20102.

Part: FITTING — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

M/D BS980 RBL83 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.021" BY 1" BY 2" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.

Part: CHANNEL — CORRODED (BS 787) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS787 LBL11-RBL11 HAT SECTION AFT FLANGE CORROSION. CORROSION BLEND OUT 0.022 INCH X .8750 X 3 INCH EXCEED SRM LIMIT. HAT SECTION REPLACED IAW SRM 51-10-01 PG9. P/N:BAC1510-335-7075T6511.

Part: FLOORBEAM — CORRODED (BS 980) · airframe 104,700 hrs · 26,436 cycles

BS 980 LBL 60 FLOORBEAM UPPER SURFACE CORROSION. CORROSION BLEND OUT 0.068" BY 2" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS. BS 980 LBL 20" TO LBL 70" FLOORBEAM UPPER CHORD REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SKIN — CORRODED (BS 1140-1146) · airframe 104,700 hrs · 26,436 cycles

BS 1140-1146 LBL11-14 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.064" BY 4" BY 6" EXCEED SRM LIMIT. BS 1140-1146 LBL11-14 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35593 AND UPS ENGINEERING FILE NUMBER 747-57-20107.

Part: INTERCOSTAL — CRACKED (BS 1220) · airframe 104,700 hrs · 26,436 cycles

BS 1220 LBL110 FLOOR INTERCOSTAL WEB CRACK AT LWR AREA, CRACK LENGTH 3/8". M/D BS 1220 LBL 110 FLOOR INTERCOSTAL WEB REPAIRED AT LOWER AREA AS PER SRM 51-40-02 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

M/D BS 759 LBL75 SEAT TRACK LT FLANGE CORROSION. CORROSION BLEND OUT 0.021" BY 1/2" BY 1" EXCEED SRM LIMIT. M/D BS 750 TO BS 830 LBL 75 TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C EMP - BS2656 FUSELAGE EXTERNAL SKIN SURFACE FOUND DENT MARK AT STR3L-5L, CRACK LENGTH 3/16". SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A.

Part: SKIN — CORRODED (BS 1193) · airframe 104,700 hrs · 26,436 cycles

BS 1193 LBL100 TO 103 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.047" BY 2" BY 3" EXCEED SRM LIMIT. BS 1193 LBL100 TO 103 WING CTR SECTION UPPER SKIN REPAIRED AS PER RS R57-14-35597 AND UPS ENGINEERING FILE NUMBER 747-57-20104.

Part: SKIN — CORRODED (BS 1050-1054) · airframe 104,700 hrs · 26,436 cycles

BS 1050-1054 RBL116-122 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.079" BY 4" BY 6" EXCEED SRM LIMIT. BS 1050-1054 RBL116-122 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35590 AND UPS ENGINEERING FILE NUMBER 747-57-20105.

Part: SEAT TRACK — CORRODED (BS 896) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS 896 LBL 33 SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.022 INCH X .5 INCH X 2 INCH EXCEED SRM LIMIT. M/D BS890 TO BS1000 LBL33 TRACK REPAIRED IAW SRM 53-10-05 FIG 1A.

Part: FITTING — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

BS 842 LBL27-30 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.016" BY 1/2" BY 3" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.

Part: SKIN — CORRODED (BS 1237-1240) · airframe 104,700 hrs · 26,436 cycles

BS 1237-1240 LBL68-74 WING CTR SECTION UPPER SKIN CORROSION. CORROSION BLEND OUT 0.045" BY 3" BY 4" EXCEED SRM LIMIT. BS 1237-1240 LBL68-74 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35592 AND UPS ENGINEERING FILE NUMBER 747-57-20108.

Part: SKIN — CORRODED (BS 1161-1164) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 1161-1164 LBL101-104 WING CTR SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.043" BY 3" BY 4" EXCEED SRM LIMIT. BS 1161-1164 LBL101-104 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35581 AND UPS ENGINEERING FILE NUMBER 747-57-20106.

Part: PANEL — CRACKED (L3 DOOR) · airframe 104,700 hrs · 26,436 cycles

FOUND L3 DOOR FWD CUTOUT LOWER REVEAL PANEL CRACK, CRACK LENGTH 0.375". REVEAL PANEL REPAIRED ASP ER RS R53-42-35595 AND UPS ENGINEERING FILE NUMBER 747-53-20336.

Part: SKIN — CORRODED (BS 1185-1187) · airframe 104,700 hrs · 26,436 cycles

BS 1185-1187 LBL31-33 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.056" BY 2" BY 3" EXCEED SRM LIMIT. BS 1185-1187 LBL31-33 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35594 FIG 3 AND UPS ENGINEERING FILE NUMBER 747-57-20100.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 434 TO BS 440 RT S27AR TO S28AR FASTENER HOLES FOUND OVAL. BS 434 TO BS 440 STR 27AR AND STR 28AR STRINGER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SKIN — CORRODED (BS 1118-1120) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 1118 TO 1120 RBL70 TO 72 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.055" BY 3.5" BY 5" EXCEED SRM LIMIT. M/D BS 1118 TO 1120 RBL 70 TO 72 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35597 AND UPS ENGINEERING FILE NUMBER 747-57-20111.

Part: SKIN — CORRODED (BS 1138-1144) · airframe 104,700 hrs · 26,436 cycles

BS 1138 TO 1144 LBL9-11 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.064" BY 2" BY 2" EXCEED SRM LIMIT. BS 118 - 1144 LBL9-11 WING CTR SECTION UPPER SKIN REPAIRED AS PER RS R57-14-35593 AND UPS ENGINEERING FILE NUMBER 747-57-20107.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

FX AIR CONDITIONING BAY FAIRING SUPPORT FLOATING NUT AT SURFACE FOUND CORROSION AT STA 1013 TO 1017 O/B SIDE. CORROSION BLEND OUT 0.050" BY 1/2" BY 8" EXCEED SRM LIMIT. FX BS1005-1018 RBL75 FAIRING SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: FITTING — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

M/D BS 682 LBL15 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.017" BY 1.5" BY 3" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.

Part: SKIN — CORRODED (BS 1168-1170) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 1168-1170 LBL31-33 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.054" BY 3" BY 8" EXCEED SRM LIMIT. M/D BS 1168-1170 LBL31-33 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35594 FIG 2 AND UPS ENGINEERING FILE NUMBER 747-57-20100.

Part: SKIN — CORRODED (BS 1140-1142) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 1140 TO 1142 RBL106 TO 108 WING CENTER SECTION UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.044" BY 2" BY 4" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35594 FIG 6 AND UPS ENGINEERING FILE NUMBER 747-57-20100.

Part: SKIN — CORRODED (BS 1138-1142) · airframe 104,700 hrs · 26,436 cycles

BS 1138 TO 1142 RBL 85-98 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.128" BY 3.5" BY 6" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35617 AND UPS EO B747-5710-25225-A.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C FX FRONT BODY FAIRING SUPPORT LOWER SURFACE CORROSION AT STA983 LBL20 TO RBL10. CORROSION BLEND OUT 0.025" X 1/2" X 10" EXCEED SRM LIMIT. FX BS983 LBL22 TO RBL33 BODY FAIRING SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C FX AIR CONDITIONING BAY FAIRING SUPPORT FLOATING NUT AT SURFACE FOUND SURFACE CORROSION AT STA 1045 RBL 10 TO RBL 57. CORROSION BLEND OUT 0.029" BY 1/2" BY 20" EXCEED SRM LIMIT. FX BS 1045 BL0 - RBL57 FAIRING SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SKIN — CORRODED (BS 1182-1188) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 1182 TO BS 1188 RBL 75 TO 83 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.059" BY 2" BY 6" EXCEED SRM LIMIT. M/D BS 1175 TO 1198 RBL75 WCS UPPER SKIN REPAIRED AS PER RS R57-14-35616 AND UPS ENGINEERING FILE NUMBER 747-57-20123.

Part: FLOOR SUPPORT — CORRODED (BS 1220-1260) · airframe 104,700 hrs · 26,436 cycles

BS 1220-1260 LBL55 FLOOR SUPPORT UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.087" BY 1.5" BY 10" EXCEED SRM LIMIT. M/D BS 1220-1260 LBL55 FLOOR SUPPORT REPAIRED AS PER RS R53-45-35575 AND UPS ENGINEERING FILE NUMBER 747-53-20335.

Part: SKIN — CORRODED (BS 1185-1195) · airframe 104,700 hrs · 26,436 cycles

BS 1185-1195 RBL87-91 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.041" BY 6" BY 10" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35603 AND UPS ENGINEERING FILE NUMBER 747-57-20115.

Part: SEAT TRACK — CORRODED (BS 990-1000) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS990-1000 LBL33 SEAT TRACK IB FLANGE FOUND COR. CORROSION BLEND OUT 0.020 INCH X .5 INCH X 1 INCH EXCEED SRM LIMIT. M/D BS890-1000 LBL33 TRACK REPAIRED IAW SRM 53-10-05 FIG 1A REFER NRC 6587 FOR WORKING DETAIL.

Part: FLOORBEAM — CORRODED (BS 1220) · airframe 104,700 hrs · 26,436 cycles

BS 1220 LBL 83-95 FLOORBEAM UPPER TEE UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.046" BY 1.5" BY 10". BS 1220 LBL 75-95 FLOORBEAM UPPER TEE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SKIN — CORRODED (BS 1208-1212) · airframe 104,700 hrs · 26,436 cycles

BS 1208-1212 LBL9-13 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.041" BY 2" BY 10" EXCEED SRM LIMIT. BS 1208-1212 LBL9-13 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35594 FIG 5 AND UPS ENGINEERING FILE NUMBER 747-57-20100.

Part: SEAT TRACK — CORRODED (BS 980-1000) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS980-1000 LBL33 SEAT TRACK OB FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.033 INCH X .8750 INCH X 2 INCH EXCEED SRM LIMIT. M/D BS890 TO 1000 LBL33 TRACK REPAIRED IAW SRM 53-10-05 FIG 1A REFER NRC 6587 FOR WORKING DETAIL.

Part: SKIN — CORRODED (BS 1155) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 1155 RBL 92 TO 96 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.079" BY 4" BY 4" EXCEED SRM LIMIT. M/D BS 1155 RBL 92 TO 96 WING CTR SECTION UPPER SURFACE SKIN REPAIRED AS PER RS 57-14-35602 REFER NRC6353 FOR WORKING DETAIL AND UPS EO B747-5730-25246-A.

Part: WEB — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS1154-1160 RBL11 SEAT TRACK SUPPORT WEB LWR AREA CRACK. CRACK LENGTH 3.7500. M/D BS1140-1200 RBL11 SEAT TRACK SUPPORT WEB REPLACED AND INSTALLED IAW SRM 51-10-01 PG9 AND 51-30-02.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C NWW RT SIDEWALL PANEL BETWEEN BS 300-320 2 LOCATIONS CRACK FOUND ON WEB. CRACK ON BS305 APPROX 3/8" AND ON BS 313 APPROX 1/2" IN LENGTH. NWW RT SIDEWALL PANEL BETWEEN BS300-320 WL160 AREA REPAIRED AS PER SRM 53-10-04 FIG 116. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-10-04 FIG116 TABLE 2 FOR CATERGORY B REPAIR.

Part: SKIN — CORRODED (BS 1156-1160) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS1156-1160 RBL106-108 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.067" BY 2.5" BY 5" EXCEED SRM LIMIT. REPAIRED AS PER RS R57-14-35602 AND UPS EO B747-5730-25246-A.

Part: FLOORBEAM — CORRODED (BS 1020) · airframe 104,700 hrs · 26,436 cycles

BS 1020 LBL 25 FLOORBEAM UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.041" BY 2" BY 2". FLOORBEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 REFER NRC 6539 FOR WORKING DETAIL.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

BS 636-640 RBL75 SEAT TRACK CRACK, CRACK LENGTH 7/16". BS 610 TO BS 640 RBL75 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (BS 363-369) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS636-639 RBL11 SEAT TRACK CROWN CORROSION. CORROSION BLEND OUT 0.035 INCH X .7500 INCH X 3 INCH EXCEED SRM LIMIT. M/D BS630-690 RBL11 TRACK REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

BS 521 RBL14-20 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.022" BY 1/2" BY 3" EXCEED SRM LIMIT. TIE DOWN FTG ATTACH PLATE REPLACED AS PER SRM 51-10-01 PG 9.

Part: FLOORBEAM — CRACKED (BS 980) · airframe 104,700 hrs · 26,436 cycles

BS 980 LBL55 FLOORBEAM UPPER TEE FOUND CRACKED, CRACK LENGTH 3/8". BS 980 LBL20 TO LBL70 FLOORBEAM UPPER CHORD REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

BS 680 RBL12 FLOORBEAM UPPER CHORD LWR SURFACE CORROSION. CORROSION BLEND OUT 0.062" BY 2" BY 2" EXCEED SRM LIMIT. M/D BS 680 RBL13 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 3 REFER NRC 6712 FOR WORKING DETAIL.

Part: SEAT TRACK — CORRODED (BS 678) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS678 RBL11 SEAT TRACK LT FLANGE CORROSION. CORROSION BLEND OUT 0.017 INCH X .5 INCH X 3 INCH EXCEED SRM LIMIT. M/D BS630-690 RBL11 TRACK REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C FWD CARGO DOOR CUTOUT FWD DOOR HINGE 1 HOLE CRACK AT FUSELAGE SKIN RUNNING UP APPROX 0.030". SKIN REPAIRED AS PER RS R53-21-35571. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-21-35571 AND UPS B747-5320-25077-A.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C U/D RT BS340 UPR DECK FLOORBEAM UPR CHORD AND FRAME ATTACHMENT AREA 2EA FASTENER HOLES FOUND CRACK AT UPR CHORD VERTICAL FLANGE. CRACK LENGTH 0.060. U/D BS340 LBL11 TO RT MOST OB FLOORBEAM UPPER CHORD REPAIRED IAW SRM 53-10-07 FIG2.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

BS787 LBL11-33 HAT SECTION CRACKED, CRACK LENGTH 1/2". HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9, PART NUMBER : BAC1510-335-7075T6511.

Part: SKIN — CORRODED (CENTER WING) · airframe 104,700 hrs · 26,436 cycles

BS 1100 LBL85 WING CTR SECTION UPPER SKIN FOUND CORRODED. CORROSION BLEND OUT 0.067" BY 4" BY 5.5" EXCEED SRM LIMIT. BS 1100 LBL85 WING CTR SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35578 AND UPS ENGINEERING FILE NUMBER 747-57-20110.

Part: FLOORBEAM — DAMAGED (BS 340 S13AR) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C U/D RT BS 340 UPPER DECK FLOORBEAM UPPER TEE AND FRAME ATTACHMENT AREA 1 FASTENER HOLE FOUND TEE AT FRAME SPLICE. U/D RT BS 340 FLOORBEAM TEE ATTACHED FRAME SPLICE AT STR 13A AREA REPLACED AS PER RS R53-12-35567. CONTINUED INSPECTION IS REQUIRED AS PER RS R53-12-35567 SHEET 2 ITEM C11 AND UPS EO B747-5310-25138-A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

BS 640 RBL75 FLOORBEAM UPPER CHORD CORROSION. CORROSION BLEND OUT 0.062" BY 2" BY 2" EXCEED SRM LIMIT. M/D BS640 RBL40 TO 98 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 3.

Part: FITTING — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

M/D BS 681 RBL15 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.042" BY 1.5" BY 2" EXCEED SRM LIMIT. FTG REPLACED AS PER MM 20-51-01.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C FWD CARGO DOOR CUTOUT AFT DOOR HINGE FOUND ONE EA FASTENER HOLE CRACKED A TEE APPROX 0.040 INCH LONG AT 4 O/C POSITION. TEE REPLACED IAW SRM 51-10-01 PG9.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C FWD CARGO DOOR CUTOUT AFT DOOR HINGE FOUND 1 FASTENER HOLE CRACKED AT FRAME AT 4 O`CLOCK POSITION APPROX 0.030 LONG. REPAIRED AS PER RS R53-25-35580 AND UPS EO B747-5330-25123-A

Part: SEAT TRACK — CRACKED (BS 520 RBL 8) · airframe 104,700 hrs · 26,436 cycles

BS 520 RBL8 SEAT TRACK CRACK, CRACK LENGTH 4" AND 0.75" RESP. BS 520 RBL98 SEAT TRACK REPAIRED AS PER RS R53-25-35572 AND UPS ENGINEERING FILE NUMBER 747-53-20330.

Part: FRAME — CRACKED (BS 340) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C U/D LT BS 340 UPPER DECK FLOORBEAM UPPER TEE AND FRAME ATTACHMENT AREA 1 FASTENER HOLE FOUND CRACK AT FRAME WEB, CRACK LENGTH 0.060". U/D LT BS 340 UPPER DECK FLOORBEAM UPPER TEE ATTACHED FRAME REPAIRED AS PER RS R53-12-35567. CONTINUED INSPECTION IS REQUIRED AS PER RS R53-12-35567 SHEET 1 ITEM A3 AND UPS EO B747-5310-25138-A

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

BS 552 RBL11-33 HAT SECTION CORROSION. CORROSION BLEND OUT 0.020" BY 1" BY 10" EXCEED SRM LIMIT. HAT SECTION REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

BS 641 RBL 75 SEAT TRACK CRACK, CRACK LENGTH 3/8". BS 640 TO BS 670 RBL75 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FLOORBEAM — CRACKED (BS 340) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C U/D LT BS340 UPPER DECK FLOORBEAM UPPER TEE AND FRAME ATTACHMENT AREA 1 FASTENER HOLE FOUND CRACK AT STRAP, CRACK LENGTH 0.060". LT BS 340 FLOORBEAM UPPER TEE CRACKED STRAP REPLACED AS PER RS R53-12-35567. REPEAT INSPECTION IS REQUIRED AS PER RS R53-12-35567 SHEET 1 ITEM B3 AND UPS EO B747-5310-25138-A.

Part: FLOORBEAM — DAMAGED (BS 360) · airframe 104,700 hrs · 26,436 cycles

RT BS 360 UPPER DECK FLOORBEAM UPPER SECTION VERTICAL FLANGE AREA 3EA FASTENER HOLES FOUND OVAL AT STRAP AS MARKED. U/D RT BS 360 UPPER DECK FLOORBEAM UPPER SECTION VERTICAL FLANGE ATTACHED STRAP REPLACED AS PER RS R53-15-35573. REPEAT INSPECTION IS REQUIRED AS PER RS R53-15-35573 AND UPS ENGINEERING FILE NR 747-53-20332.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

BS 680 RBL13 FLOORBEAM UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.062" BY 1.5" BY 2" EXCEED SRM LIMIT. M/D BS 680 RBL13 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 3.

Part: SEAT TRACK — CORRODED (BS 532) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS 532 RBL11 SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.025 INCH X .5 INCH X 2 INCH EXCEED SRM LIMIT. M/D BS510-630 RBL11 TRACK REPLACED AND INSTALLED IAW SRM 51-10-01 P PG9 AND 51-30-02 REFER NRC 6163 FOR DETAIL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

FOUND BS 760 RBL 98 SEAT TRACK CROWN DAMAGED. CORROSION BLEND OUT EXCEED SRM LIMIT. M/D RBL98 BETWEEN BS 640 AND BS 770 SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: SKIN — CORRODED (BS 1140) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS1140 LBL 55 WING CTR SECTION UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.159" BY 3" BY 4" EXCEED SRM LIMIT. BS 1140 LBL 55 WING CTR SECTION UPPER SURFACE CORRODED AREA REPAIRED AS PER RS R57-14-35596 AND UPS ENGINEERING FILE NUMBER 747-57-20122.

Part: SPLICE PLATE — CRACKED (NLG WW) · airframe 104,700 hrs · 26,436 cycles

NWW LT AFT CORNER BS 400 S44L INTERNAL SPLICE PLATE FOUND CRACK FROM FWD EDGE AND RUNNING AFT UNDERNEATH BH CHORD, CRACK LENGTH 3/4". NWW LT AFT CORNER BS400 STR 44L INTERNAL SPLICE PLATE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS520-528 RBL11 SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.022 INCH X .5 INCH X 3 INCH EXCEED SRM LIMT. M/D BS510-630 RBL11 TRACK REPLACED AND INSTALLED INCH SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS556-560 RBL11 SEAT TRACK LT FLANGE CORROSION. CORROSION BLEND OUT 0.028 INCH X .5 INCH X 5 INCH EXCEED SRM LIMIT. M/D BS510-630 RBL11 TRACK REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02 REFER NRC 613 FOR DETAIL.

Part: SPLICE PLATE — CRACKED (NLG WW) · airframe 104,700 hrs · 26,436 cycles

NWW RT AFT CORNER BS 400 S44R INTERNAL SPLICE PLATE FOUND CRACK FROM FWD EDGE AND RUNNING AFT AND RUNNING O/B UNDERNEATH BH CHORD, CRACK LENGTH 1/2". NWW RT AFT CORNER BS400 STR 44R INTERNAL SPLICE PLATE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

BS 520 RBL90 SEAT TRACK CRACK, CRACK LENGTH 1/2". BS 480 TO BS 530 RBL90 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C FX, RT LOWER FUSELAGE INTERIOR STRUCTURE STRINGER SPLICE RETAINER ATT HOLE FOUND ELONGATED AT STA 2180 STRINGER 44R. FX BS 2180 STR 44R STRINGER SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FLOORBEAM — CRACKED (BS 340) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C U/D RT BS 340 UPPER DECK FLOORBEAM UPPER TEE AND FRAME ATTACHMENT AREA 2 FASTENER HOLE FOUND CRACK AT FRAME WEB, CRACK LENGTH .060". U/D RT BS 340 UPPER DECK FLOORBEAM UPPER TEE ATTACHED FRAME REPAIRED AS PER RS R53-12-35567. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-12-35567 SHEET 2 ITEM C11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

BS 680 LBL4 FLOORBEAM UPPER SURFACE CORROSION. CORROSON BLEND OUT 0.055" BY 2" BY 4" EXCEED SRM LIMIT. M/D BS680 LBL4 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 3.

Part: SEAT TRACK — CORRODED (BS 583-620) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS583-620 RBL11 SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.021 INCH X .5 INCH X 10 INCH EXCEED SRM LIMIT. M/D BS510-630 RBL11 TRACK REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02 REFER NRC 6163 FOR WORKING DETAIL.

Part: SKIN — CRACKED (NR 4 PYLON) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C NR 4 PYLON CAP SKIN SUSPECT CRACK AT SHEARED RIVET AREA, CRACK LENGTH 1/4". NR 4 PYLON CAP SKIN REPAIRED AS PER HX TOWS NO T-747-54-0224 AND RS R54-51-35569 AND UPS ENGINEERING FILE NUMBER 747-54-20055.

Part: DOOR FRAME — CRACKED (BS 488) · airframe 104,700 hrs · 26,436 cycles

LT BS 488 FRAME FOUND CRACK AT DOOR STOP NR 9 AREA AND TOOLING HOLE, CRACK LENGTH 1/16" AND 5/16" AND 3/16". LT BS 488 FRAME REPAIRED BETWEEN STR 16L TO STR 19L AREA AS PER SRM 53-10-04 FIG 121.

Part: SKIN — CRACKED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C FWD CARGO DOOR CUTOUT FWD HINGE FAIRING AREA 1 HOLE CRACK AT FX SKIN APPROX 1/16" LONG. SKIN REPAIRED AS PER RS R53-21-35571 AND REFER NRC 6304 FOR WORKING DETAIL AND UPS EO B747-5320-25077-A.

Part: SKIN — CORRODED (RT WING) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C RT WING L/E CAVITY LWR PANEL FOUND BULGED UP AFT OF NR 25 VC FLAP. CORROSION BLEND OUT 0.080" BY 2" BY 2" EXCEED SRM LIMIT. RT WING LOWER SKIN AT FS 1445 TO 1468 REPAIRED AS PER RS R57-26-35582 AND UPS ENGINEERING FILE NUMBER 747-57-20109.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

RT LOWER FUSELAGE EXTERNAL SKIN SURFACE FOUND BILGE UP AT STA 2180 TO STA 2183 STR 44R. FASTENER AND STRINGER 44R SPLICE AT BS 2180 AREA REMOVED AND REINSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 AFTER INSPECTION CARRIED OUT AS PER SRM 51-10-01. SKIN SURFACE NO CORROSION FOUND REFER NRC6340 FOR STR REPLACED WORKED DETAIL.

Part: STRINGER CLIP — CRACKED (BS 340) · airframe 104,700 hrs · 26,436 cycles

LT NLG W/W INTERNAL SIDE STA340 WL140 CLIP FOUND CRACK, CRACK LENGTH 1/4". BRACKET REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: SKIN — BULGED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C FX RT LWR FUSELAGE EXTERNAL SKIN SURFACE FOUND BULGED UP AT STA 1610-1613 STR 43R. SKIN REPAIRED AS PER SRM 53-30-03 FIG1 SUBSEQUENT INSPECTION ARE NECESSARY FOR CAT B REPAIR REFER SRM 53-30-03 FIG 1 TABLE 4 FOR REFERENCE.

Part: RIB — CRACKED (RT WING) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C RT WING, NR 21 VC FLAP I/B ARM I/B SUPPORT RIB FWD VERTICAL FLANGE FASTENER HOLES CRACKED, CRACK LENGTH 5/8". REPAIRED AS PER RS R57-41-35563 AND UPS EO B747-5710-25082-A.

Part: SPAR — CORRODED (BS 1241) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C FX, RT WING CENTER SECTION REAR SPAR WEB FOUND CORROSION AT BS 1241 RBL 105-106 B/H FTG BTN NR 15 AND NR 16 FASTENER HEAD (RT WING LT W/W) REMAIN THICKNESS 0.345" TO 0.389'. FX , RT WING CENTER SECTION REAR SPAR WEB CORROSION REMOVED AS PER UPS EO B747-5710-11129-G APP B FIG 5 JUST AT BS1241 RBL105-106.

Part: FRAME — CRACKED (BS 840) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D LT BS 840 FRAME TO TENSION TIE CONNECTION FOUND FRAME 1 HOLE CRACK, CRACK LENGTH 0.040". M/D LT BS 840 BETWEEN STR 8L TO STR 12L FRAME REPAIRED AS PER RS R53-25-35564 AND UPS EO B747-5310-25079-A.

Part: PLATE — DAMAGED (BS 840) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 840 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPPER AND LWR FASTENER HOLE. M/D BS840 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AS PER RS R53-25-35564. CONTINUE INSPECTION ARE REQUIRED AS PER RS R53-25-35564 AND UPS EO B747-5310-25079-A.

Part: TENSION TIE — CRACKED (BS 800) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS800 RT TENSION TIE TO FRAME CONNECTION ATTACHMENT FASTENER HOLE FOUND CRACK AT TENSION TIE FWD CHANNEL, CRACK LENGTH 0.040". M/D RT BS 800 FRAME TO TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35568. CONTINUE INSPECTION ARE REQUIRED AS PER RS R53-25-35568 AND UPS EO B747-5310-25023-A.

Part: PLATE — DAMAGED (BS 840) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 840 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B LOWER FASTENER HOLE. M/D BS 840 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AS PER RS R53-25-35564. CONTINUE INSPECTION ARE REQUIRED AS PER RS R53-25-35564 AND UPS EO B747-5310-25079-A.

Part: PLATE — DAMAGED (BS 920) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 920 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPPER I/B LOWER AND O/B LWER NR 2 (COUNT FROM O/B) FASTENER HOLE. M/D BS 920 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMINUM STRAP REPLACED AS PER RS R53-25-35566. CONTINUE INSP IS REQUIRED AS PER RS R53-25-35566 AND UPS EO B747-5310-25032-A.

Part: DOUBLER — CRACKED (FUSLEAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS840 RT TENSION TIE TO FRAME CONNECTION FASTENER HOLE FOUND CRACK AT WEB DOUBLER. CRACK LENGTH .0625 INCH. M/D BS840 BETWEEN S9R TO S12R FRAME ATTACHED DOUBLER REPLACED AND INSTALLED IAW SRM 51-10-01 PG9 AND 51-30-02.

Part: BEAM — CRACKED (NLG WW) · airframe 104,700 hrs · 26,436 cycles

RT NWW VERTICAL BEAM WEB AT BS 300 FOUND CRACK AT WL 171 INSULATION BLANKET STAND OFF, CRACK LENGTH 1/8". WEB REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED PER SRM 51-30-02.

Part: PLATE — DAMAGED (BS 800) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 800 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPPER NR 1, 3 AND I/B LOWER FASTENER HOLE AREA. M/D BS 800 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMINUM STRAP REPLACED AS PER RS R53-25-35568. CONTINUE INSP IS REQUIRED AS PER RS53-25-35568 AND UPS EO B747-5310-25023-A.

Part: PLATE — DAMAGED (BS 920) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS920 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPPER AND LOWER FASTENER HOLE. M/D BS 920 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMINUM STRAP REPLACED AS PER RS R53-25-35566. CONTINUE INSP IS REQUIRED AS PER RS R53-25-35566 AND UPS EO B747-5310-25032-A.

Part: STIFFENER — CRACKED (NLG WW) · airframe 104,700 hrs · 26,436 cycles

TOP PANEL LBL20 STIFFENER FOUND CRACKED AT BS 290, CRACK LENGTH 1/2". NWW BS 290 LBL20 TOP PANEL ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FRAME — CRACKED (BS 800) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 800 RT TENSION TIE TO FRAME CONNECTION ATTACHMENT FASTENER HOLE FOUND CRACK AT FRAME, CRACK LENGTH 0.040". M/D BS 800 RT FRAME CRACKED HOLE OVERSIZED TO 0.309" AND BOLT INSTALLED AS PER RS R53-25-35568 AFTER HFEC INSPECTION PER NTM PART 6 51-00-00 FIG16. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35568 AND UPS EO B747-5310-25023-A.

Part: PLATE — DAMAGED (BS 800) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 800 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) I/B UPPER 4EA FASTENER HOLE LOWER ROW NO.1,3,4,6 COUNT FROM I/B AND O/B LOWER FASTENER HOLE. M/D BS 800 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMINUM STRAP REPLACED AS PER RS R53-25-35568. CONTINUE INSP IS REQUIRED AS PER RS R53-25-35568 AND UPS EO B747-5310-25023-A.

Part: TENSION TIE — CRACKED (BS 800) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D LT BS 800 FRAME TO TENSION TIE CONNECTION FOUND TENSION TIE AFT CHANNEL 1 HOLE CRACK, CRACK LENGTH 1/16". M/D LT BS 800 TENSION TIE AFT CHANNEL REPAIRED AS PER RS R53-25-35568 CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35568 AND UPS EO B747-5310-25023-A.

Part: STIFFENER — CRACKED (NLG WW) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C NWW TOP PANEL RBL20 STIFFENER FOUND CRACKED AT BS 290, CRACK LENGTH 3/4". NWW BS290 RBL20 TOP PANEL ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: PLATE — DAMAGED (BS 880) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 880 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM)AT I/B UPPER I/B LOWER AND UPPER NR 2, NR 5 COUNT FROM O/B FASTENER HOLE. M/D BS 880 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMINUM STRAP REPLACED AS PER RS R53-25-35565. CONTINUE INSP IS REQUIRED AS PER RS R53-25-35565 AND UPS EO B747-5310-25025-A.

Part: PLATE — DAMAGED (BS 880) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 880 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPPER FASTENER HOLE. M/D BS 880 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE AND ALUMINUM STRAP REPLACED AS PER RS R53-25-35565. CONTINUE INSP IS REQUIRED AS PER RS R53-25-35565 AND UPS EO B747-5310-25028-A.

Part: PLATE — DAMAGED (FUSLEAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS860 RT TENSION TIE FWD CHANNEL 2EA HOLE OVAL AT S/STEEL PLATE OB UPR AND LWR FASTENER HOLE AREA. M/D BS860 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02 REFER NRC 5246 FOR DETAIL.

Part: FRAME — CRACKED (BS 780) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D RT BS780 FRAME AT TENSION TIE CONNECTION FOUND 2 HOLE CRACK AT FRAME, CRACK LENGTH 0.040". M/D RT BS 780 FRAME CRACKED HOLE OVERSIZED AS PER UPS EO B747-5310-23715. NO CRACK FOUND AFTER HFEC INSPECTED PER NTM PART 6 51-00-00 FIG 16. S/STEEL PLATE REPAIRED AS PER RS R53-25-35540. DUE TO SEM FOUND AFTER HOLE OVERSIZED OF WHOLE STACK UP. CONTINUE INSP IS REQUIRED AS PER RS R53-25-35540 AND UPS EO B747-5310-25071-A.

Part: PLATE — DAMAGED (BS 940) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D LT BS 940 TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN AT I/B UPPER AND LOWER FASTENER HOLE. M/D LT BS 940 TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AS PER RS R53-25-35491. CONTINUE INSPECTION ARE REQUIRED AS PER RS R53-25-35491 AND UPS EO B747-5310-25111-A.

Part: DOUBLER — CRACKED (BS 820) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C M/D BS 820 LT SIDE TENSION TIE TO FRAME CONNECTION FASTENER HOLE FOUND CRACK AT WEB DOUBLER. CRACK LENGTH 0.040 INCH. M/D BS820 LHS FRAME ATTACHED DOUBLER BETWEEN STR9L TO STR12L AREA REPLACED AND INSTALLED IAW SRM 51-10-01 PG9 AND 51-30-02.

Part: TENSION TIE — CRACKED (BS 900) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 900 LT SIDE TENSION TIE TO FRAME CONNECTION FASTENER HOLE FOUND CRACK AT AFT TENSION TIE. CRACK THROUGH THICKNESS. M/D BS 900 LT SIDE TENSION TIE AFTER CHANNEL REPAIRED AS PER RS R53-25-35559. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35559 AND UPS EO B747-5310-25022-A.

Part: TENSION TIE — CRACKED (BS 780) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D RT BS780 FRAME AT TENSION TIE CONNECTION FOUND 1 HOLE CRACK AT TENSION TIE AFT CHANNEL. CRACK LENGTH 1.25". M/D RT BS 780 TENSION TIE AFT CHANNEL REPAIRED AT O/B OF RT VERT POST TO RT MOST O/B AREA AS PER RS R53-25-35540. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35540 AND UPS EO B747-5310-25071-A.

Part: PLATE — DAMAGED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C, M/D LT BS780 TENSION TIE FWD CHANNEL ATTACHED STANLESS STEEL PLATE 4EA HOLE OVAL AT OB AREA. M/D LT BS 780 TENSION TIE FWD CHANNEL ATTACHED STANLESS STEEL PLATE REPLACED AND INSTALLED IAW SRM 51-10-01PG9 AND EO B747-5310-23715 APPENDIX C.

Part: PLATE — DAMAGED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE-C, M/D LT BS 900 TENSION TIE FWD CHANNEL ATTACHED STAINLESS STEEL PLATE OVAL HOLE 1EA FOUND AT UPPER ROW COUNT FROM IB NR 4. M/D BS 900 LT TENSION TIE FWD CHANNEL ATTACHED STAINLESS STEEL PLATE REPLACED AND INSTALLED IAW SRM 51-10-01 PG9 AND 51-30-02.

Part: TENSION TIE — DAMAGED (BS 940) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D LT BS 940 FRAME TO TENSION TIE CONNECTION FOUND FASTENER HOLE OVAL AT TENSION TIE FWD CHANNEL. M/D LT BS 940 FRAME TO TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35491. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35491 AND UPS EO B747-5310-25111-A.

Part: TENSION TIE — CRACKED (BS 900) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D LT BS900 FRAME TO TENSION TIE CONNECTION FOUND CRACK AT TENSION TIE FWD CHANNEL 1 HOLE, CRACK LENGTH 0.030". M/D LT BS 900 TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35559 CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35559 AND UPS EO B747-5310-25022-A.

Part: PLATE — DAMAGED (FUSELAGE) · airframe 104,700 hrs · 26,436 cycles

LT BS 860 TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE TO FRAME CONNECTION 1 FASTENER HOLE OVAL AT LOWER (COUNT FROM O/B NR 5). LT BS 860 TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 REFER NRC 5279 FOR DETAIL.

Part: TENSION TIE — CRACKED (BS 900) · airframe 104,700 hrs · 26,436 cycles

RT BS 900 FRAME AT TENSION TIE CONNECTION FOUND 1 HOLE CRACK AT TENSION TIE AFT CHANNEL, CRACK LENGTH 0.030". BS 900 FRAME ATTACHED TENSION TIE RT AFT CHANNEL CRACKED HOLE OVERSIZED TO 0.278" BY INCREMENT AS PER EO B747-5310-23715 APP D AND BOLT INSTALLED AS PER SRM 51-30-02 AND RS R53-25-35559 AND UPS EO B747-5310-25022-A.

Part: STRUCTURE — CORRODED (CENTER WING) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C FX WING CTR SECTION RT LOWER CHORD FOUND HEAVY CORROSION AT STA983 RBL 78 TO RBL 86 EXTERNAL SURFACE. CORROSION BLEND OUT 0.151" BY 1.5" BY 5" EXCEED SRM LIMIT. FX WING CTR SECTION RT LOWER CHORD REPAIRED AT RBL75 TO RBL87 AREA AS PER RS R57-11-35600 AND UPS ENGINEERING FILE NUMBER 747-57-20113.

Part: DOUBLER — CRACKED (BS 820) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D RT BS920 FRAME AT TENSION TIE CONNECTION FOUND 1 HOLE CRACK AT WEB DOUBLER, CRACK LENGTH 0.040". M/D BS 820 RHS FRAME ATTACHED DOUBLER BETWEEN STR 9R TO STR 12R AREA REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 AND RS R53-25-35562 AND UPS EO B747-5310-25070-A.

Part: PLATE — DAMAGED (BS 830) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D LT BS 860 TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN AT I/B LOWER FASTENER HOLE. BS 860 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE AND ALUMINUM STRAP REPLACED AS PER RS R53-28-35574. CONTINUE INSP ARE REQUIRED AS PER RS R53-25-35574 AND UPS EO B747-5310-25024-A.

Part: FLOORBEAM — CORRODED (BS 600) · airframe 104,700 hrs · 26,436 cycles

FWD CARGO COMPT RT STA600 RBL44-45 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.041" BY 1" BY 1" EXCEED SRM LIMIT. FWD CARGO COMPT BS 600 FLOORBEAM UPPER CHORD REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 JUST BETWEEN RBL30 AND RT MOST O/B.

Part: PLATE — DAMAGED (BS 940) · airframe 104,700 hrs · 26,436 cycles

BS 940 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B LOWER FASTENER HOLE AREA. BS 940 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AS PER RS R53-25-35491. CONTINUED INSPECTIONS ARE REQUIRED AS PER RS R53-25-35491 AND UPS EO B747-5310-25111-A.

Part: PLATE — DAMAGED (BS 820) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS 820 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPR FASTENER HOLE AREA. M/D BS 820 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AS PER RS R53-25-35562. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35562 AND UPS EO B747-5310-25070-A.

Part: PLATE — DAMAGED (BS 900) · airframe 104,700 hrs · 26,436 cycles

BS 900 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPPER 1 HOLE AND LOWER I/B 2 HOLE AREA. BS 900 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMINUM STRAP REPLACED AS PER RS R53-25-35559. CONTINUE INSP IS REQUIRED AS PER RS R53-25-35559 AND UPS EO B747-5310-25022-A.

Part: PLATE — DAMAGED (BS 860) · airframe 104,700 hrs · 26,436 cycles

INSPECTION TYPE:C M/D BS860 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN AT I/B LOWER FASTENER HOLE AREA AND AT NR 12 COUNT FROM O/B UPPER ROW FASTENER HOLE. M/D BS 860 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMINUM STRAP REPLACED AS PER RS R53-25-35574. CONTINUE INSP ARE REQUIRED AS PER RS R53-25-35574 AND UPS EO B747-5310-25024-A.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A MAIN DECK CEILING AND FWD DOOR SEAL EMERGENCY LIGHTS INOP. R&R AISLE EMERGENCY LIGHT AS REQUIRED. REF M/M 33-51-01. OPS CHECK NORMAL

Part: FLOORBEAM — CORRODED (BS 1265) · airframe 104,700 hrs · 26,436 cycles

BS 1265 LBL 11 TO 33 FLOORBEAM UPPER SURFACE FOUND CORROSION CORROSION BLEND OUT 0.050" X 1" X 10". M/D BS 1265 LBL 11 TO 33 FLOORBEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: PAN — CORRODED (LAV DUMP)

CORROSION FOUND AT LAV DUMP PAN AREA. RMVD CORRODED FRAMES & INTERCOSTALS. CKD INNER SKIN-NO DISCREPANCIES - OK TO REPLACE CORRODED PARTS. INSTALLED NEW FRAMES & INTERCOSTALS PER SRM 51-30-02 & EO B747-5330-23587A. DRILLED RT INTERCOSTAL FROM HOLES, DRILLED LH INCOSTAL FROM HOLES. INSTALLED RT & LH INTERCOSTAL PARTS ALSO INSTALLED DUMP CHUTE.

Part: THRUST LINK — CRACKED (NR 2 ENGINE) · airframe 103,615 hrs · 26,170 cycles

AD CRACK INDICATIONS FOUND AT NR2 ENG MOUNT THRUST LINK THE INDICATIONS LOCATED AT FWD AND AFT LUG BORE WHICH WERE EXCEEDED THE LIMITS. THRUST LINK REPLACED REF MM 71-21-03.

Part: THRUST LINK — CRACKED (NR 4 ENGINE) · airframe 103,615 hrs · 26,170 cycles

AD CRACK INDICATIONS FOUND AT NR 4 ENG MOUNT THRUST LINK THE INDICATIONS LOCATED AT FWD AND AFT LUG BORE WHICH WERE EXCEEDED THE LIMITS. THRUST LINK REPLACED. REF MM 71-21-03.

Part: ACM — INOPERATIVE (NR 1)

NR 1 PACK ELEC SMOKE, VIBRATION AFTER TAKEOFF. VIBRATION STOPPED WITH NR 1 PACK OFF. REMOVED AND REPLACED NR 1 PACK AIR CYCLE MACHINE IAW AMM 21-51-04, RAN PACK ON GROUND FOR 2 HOURS, ALL OPERATIONS NORMAL.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 102,404 hrs · 25,907 cycles

LT NWW SIDE PANEL FOUND CRACKED AT BTN BS 280 AND 300 WL 160 APPROX 2 INCH. REPAIRED AS PER SRM 53-10-04 FIG 116.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 102,404 hrs · 25,907 cycles

RT NWW SIDE PANEL FOUND 2 EA CRACK BOTH APPROX 1 INCH AT BTN BS 260 AND 280, WL 150, CRACK LENGTH 1 IN. RT NWW SIDE PANEL REPAIRED AS PER SRM 53-10-04 FIG 116.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 102,404 hrs · 25,907 cycles

LT NWW SIDE PANEL FOUND CRACK AT BTWN BS 280 AND 300, WL 170 APPROX 1 IN, CRACK LENGTH 1 IN. LT NWW SIDE PANEL REPAIRED AS PER SRM 53-10-04 FIG 11.

Part: WEB — CRACKED (FUSELAGE) · airframe 102,404 hrs · 25,907 cycles

RT NWW SIDE PANEL FOUND CRACKED AT BTN BS 260 AND 280 WL 170, CRACK LENGTH 2.5 IN. REPAIRED AS PER SRM 53-10-04 FIG 116.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 102,404 hrs · 25,907 cycles

LT NWW SIDE PANEL FOUND CRACKED AT BTN BS 280 AND 300 WL 150 APPROX 1 INCH CRACK LENGTH 1 INCH. REPAIRED AS PER SRM 53-10-04 FIG 116.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 102,404 hrs · 25,907 cycles

LT NWW SIDE PANEL FOUND CRACK AT BTN BS 260 AND 280 WL 150, CRACK LENGTH 1 INCH. REPAIRED AS PER SRM 53-10-04 FIG 116.

Part: SKIN — CORRODED (FUSELAGE) · airframe 102,404 hrs · 25,907 cycles

INTERIM REPAIR AFT OF ELECTRICAL ACCESS DOOR. CORROSION BLEND OUT 2 BY 5 IN , SKIN INTERNAL BONDED DOUBLER CORRODED. REMOVED PER HX RS NR R53-30-35332 AND UPS EA NR 747-53-20252 AND STRAP REPLACED PER SRM 51-10-01.

Part: FITTING — CRACKED (FLOOR SUPPORT) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/DECK BS 2019 RBL 60 BELOW FLOOR SUPPORT FTG FOUND CRACK AFTER BS 2020 FLOOR FTG REMOVAL, CRACK LENGTH 3/8 INCH. M/DECK BS 2019 RBL 60 INCH BELOW FLOOR SUPT FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 101,885 hrs · 25,799 cycles

M/DECK BS 1880 RBL 50 INCH TIE DOWN FTG ATT PLATE FOUND CORRODED. CORROSION BLEND OUT 0.025 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, BS 1880 RBL 50 INCH TIE DOWN FTG. REEPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D- BS 2130 TO 2140 LBL 75 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 X 1 X 1 INCH. CORROSION BLEND OUT 0.045 X 1 X 1 INCH, EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.

Part: CARGO TRACK — CORRODED (FUSLEAGE) · airframe 101,885 hrs · 25,799 cycles

M/DECK BS 1720 LBL 78 INCH AND 85 INCH TIE DOWN FTG ATTACH PLATE FOUND CORRODED. CORROSION BLEND OUT 0.030 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, TIE DOWN FTG AND PLATE REPLACED AS PER MM 20-51-01 FTG P/N: 69B62076-1, PLATE P/N: 69B62100-1.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE: C M/D- BS 1500 RBL 83-89 FLOORBEAM UPPER CHORD LWR SURFACE CRACKED CRACK, LENGTH .375 INCH. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: FITTING — CRACKED (FLOORBEAM) · airframe 101,885 hrs · 25,799 cycles

M/DECK BS 2020 RBL 60 INCH BELOW FLOORBEAM SUPPORT FTG FOUND CRACKED, CRACK LENGTH 3/4 INCH. M/DECK BS 2020 RBL 60 INCH BELOW FLOORBEAM SUPPORT FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D- BS 1800 TO 1920 RBL 11 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D - BS 2040-2050 LBL 88 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 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: SEAT TRACK — CORRODED (FUSLEAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D- BS 2040 - 2140 LBL 65 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D- BS 1780 RBL 95 SEAT TRACK CROWN FOUND CORRODED. CORROSION BLEND OUT 0.045 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

BS 1500-1580 LBL 11 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 P.9

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D - BS 1528-1532 RBL 75 SEAT TRACK LT FLANGE CORROSION. CORROSION BLEND OUT 0.045 X 1 X 1 INCH, EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D- BS 2160 L BETWEEN STR 13L & 14L SHEAR TIE CRACKED, LENGTH .25 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 101,885 hrs · 25,799 cycles

M/DECK BS 1500 LBL 75 INCH TIE DOWN FTG ATTACH PLATE FOUND CORRODED. CORROSION BLEND OUT 0.030 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C AREA AFT OF BULK CARGO STA 2180 S42R STRINGER END CRACKED, CRACK LENGTH .75 INCH. AFT OF BULK CARGO BS 2160 TO 2180 STR 42R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D- BS 1580 - 1600 LBL 118 FLOOR SUPPORT CORRODED. CORROSION BLEND OUT 0.035 X 1 X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: WEB — CRACKED (M/D) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D- STA 1220 LBL 116-118 BELOW FLOOR SUPPORT WEB CRACKED, LENGTH 2 INCHES. FLOOR SUPPORT WEB REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

BS 1700-1707 LBL 11 INCH SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.040 INCH BY 1 INCH BY 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, SEAT TRACK REPLACED AS PER SRM 51-10-01 P.9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE: C, M/D- BS 1920 - 2040 LBL 95 SEAT TRACK & FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 X 1 X 3 INCH, EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.

Part: FITTING — CORRODED (FUSLEAGE) · airframe 101,885 hrs · 25,799 cycles

BS 1680 LBL 55 TIE DOWN FIG ATT PLATE FOUND CORRODED. CORROSION BLEND OUT 0.025 INCH BY 1 INCH BY 1 INCH OUT OF SRM 53-10-01 FIG 1 LIMIT, TIE DOWN FIG PLATE REPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — CORRODED (FUSLEAGE) · airframe 101,885 hrs · 25,799 cycles

BS 1564-1570 RBL 98 INCH SEAT TRACK LEFT FLANGE CORROSION. CORROSION BLEND OUT 0.035 INCH BY 1 INCH BY 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, SEAT TRACK REPLACED AS PER SRM 51-10-01 P.9

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D- BS 1960 LT STR 2L TIE CLIP CRACKED, LENGTH .375 INCH. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 & SRM 51-30-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D- BS 1580 RBL 83-96 FLOORBEAM UPPER CHORD CORROSION. CORROSION BLEND OUT 0.060 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D BS 1580 RBL 83-96 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

M/DECK BS 1940 AND 1960 LBL 80 INCH TIE DOWN FTG ATT PLATE FOUND CORRODED. CORROSION BLEND OUT 0.020 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, M/D BS 1940 LBL 80 INCH TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D- STA 1500 RBL 117 FLOOR SUPPORT ANGLE CRACKED, LENGTH .75 INCH. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: FLOOR SUPPORT — CORRODED (M/D) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D-BS 1650 LBL 118 FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.035 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: PANEL — CRACKED (RT WING) · airframe 101,885 hrs · 25,799 cycles

RT WING L/E CAVITY AT FSSI 998 L/E MOST FWD D-SECTION ATT PANEL AND UPPER EDGE CHORD FOUND CRACKED, AFT OF NR 20 VC FLAP, CRACK LENGTH 1 INCH. PANELS AND CHORD REPAIRED AS PER SRM 57-20-03 FIG 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE4) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D- BS 2350 - 2360 RBL 55 FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.030 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: SHEAR TIE — CRACKED (M/D) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D - BS 1780 BETWEEN S10-11R FRAME ATTACH SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. M/D - BS 1780 BETWEEN S10-11R FRAME ATTACH SHEAR TIE REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C, BS 1278 STR 25R END FOUND CRACKED. CRACK LENGTH .75 INCH. M/DECK BS 2170-2180 STR 25R REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D- STA 1435 RBL 65 WHEEL WELL UPPER SKIN ATTACH STIFFENER FOUND CRACKED, LENGTH .375 INCH. STIFFENER REPLACED AS PER SRM 51-30-02 & SRM 51-10-01 PG 9.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D - BS 2300 RBL 52 FLOOR SUPPORT FOUND CRACKED, CRACK LENGTH 0.5 INCH. M/D - BS 2300 RBL 52 FLOOR SUPPORT REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 101,885 hrs · 25,799 cycles

AFT CARGO WALKWAY PANEL SUPPORT FOUND CORRODED BETWEEN BS 1580 AND 1600 RBL 36. CORROSION BLEND OUT 0.030 INCH BY 1 INCH BY 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, WALKWAY PANEL SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

BS 2180 STR 25R FRAME FOUND CRACKED, CRACK LENGTH 1 INCH. FRAME REPAIRED AT BS 2180 STR 25R AREA AS PER HX RS R-53-62-35275 AND UPS EO B747-5310-21972A.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D - BS 1560 LT BETWEEN STR 20L & 22L SHEAR TIE FOUND CRACKED, CRACK LENGHT .375 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D - BS 1580 S-19R FRAME ATTACH SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D - BS 1580 LT BETWEEN STR 20L & 22L SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C M/D - BS 1540 LT BETWEEN STR 20L & 22L SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (NR 3 NACELLE) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C NR 3 PYLON NAC STA 250 O/B FRAME LOWER TO WEB ATTACHMENT AREA CRACKED, LENGTH 1.5 INCH. FRAME REPAIRED AT LOWER PORTION AS PER SRM 54-10-03 FIG 1.

Part: SKIN — CRACKED (EMPENNAGE) · airframe 101,885 hrs · 25,799 cycles

TAIL FUSELAGE STA 2685 - 2705 WL 297 TO WL 334 LT MIDDLE AREA FOUND SKIN CRACKED, CRACK LENGTH 2.5 INCH. SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A.

Part: SKIN — CHAFED (VERTICAL FIN) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C VERTICAL FIN RT LWR EDGE FWD SECTION FX SKIN CHAFING MARK FOUND WITH ONE LOCATION OF SKIN BLEND OUT EXCEED EO LIMIT. CHAFE BLEND OUT 0.029 INCH. SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A AT STA 2360 TO 2394 STR 3R AREA.

Part: SKIN — CHAFED (VERTICAL FIN) · airframe 101,885 hrs · 25,799 cycles

INSPECTION TYPE:C VERTICAL FIN LT LWR EDGE FWD SECTION FX SKIN CHAFING MARK FOUND WITH 2 LOCATIONS CHAFE BLEND OUT EXCEED EO LIMIT. CHAFE BLEND OUT DEPTH 0.025 & 0.022 INCH. SKIN REPAIRED AT BS 2310-2360 STR 3L AREA AS PER SRM 53-30-03 FIG 1 & BS 2360 - 2380 STR 3L AREA AS PER SRM 53-30-03 FIG 1A.

Part: STRINGER — CRACKED (NR 3 PYLON)

INSPECTION TYPE:N/A FOUND CRACK ON NR 3 PYLON STRINGER, LT JUST FWD OF NAC STA 221, AREA MARKED IN RED. STRINGER IS CRACKED FROM TOP TO BOTTOM. STARTED DRILLING OUT FASTENERS IN STIFFENER & STRINGER REMOVED STIFFENER AND RIB FABRICATED REPAIR PARTS. ALODINED, PRIMED, INSTALLED AND PAINTED REPAIR PARTS AND REPAIR PER SRM 54-10-03.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT)

INSPECTION TYPE:N/A EMERGENCY LIGHT AT ESCAPE ABOVE EXIT SIGN INOP. TURNS ON MOMENTARILY THEN SHUTS. REMOVED AND REPLACED LIGHT ASSY PER 33-51-07. OPS CHECK OKAY PER SAME REF.

Part: BATTERY PACK — INOPERATIVE (L1 DOOR)

AFT EMERGENCY LIGHT IN L1 DOOR INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-04, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A AFT EMERGENCY LIGHT AT L1 DOOR INOP. PERFORMED OPS CHECK IAW MM 33-51-00, OPS CHECK NORMAL.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, DURING PERFORMING BS 1000 RT BATH TUB FITTING REPLACEMENT AS PER EO NR B747-5310-18579A, IT WAS FOUND 3 EA OF FASTENER HOLES SEAM AT I/B VERT FLANGE AND 6 EA OF FASTENER HOLES FOUND OVERSIZED DIAMETER .309 INCH IN O/B HORIZ FLANGE. THE BATH TUB FITTING REPAIRED AS PER RS NR R53-23-25077 AND AS PER EO B747-5310-17015-C FOR FURTHER INSPECTION.

Part: RIB — CRACKED (TE FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 5 VC FLAP O/B LINKAGE I/B RIB CRACKED AT LINKAGE BOLT HOLT HEAD SECTION. LT WING NR 5 VC FLAP O/B LINKAGE I/B RIB REPLACED AS PER SRM 51-10-01 PG 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, CRACK INDICATION REVEALED ON BS 2250 S28L FUSELAGE SKIN AREA AS MARKED UNDER REPAIR DOUBLER. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1 WITH FWD MOST EXISTING FASTENERS 7EA OVERSIZED .0625 INCH AND FASTENERS INSTALLED IAW SRM 51-00-06 AND 51-30-02 AFTER INSPECTED BY HFEC. SUBEQUENT INSPECTION ARE NECESSARY DUE TO THIS REPAIR CLASSIFY AS CATEGORY B REPAIR. REINSPECT IAW EO B747-5330-17977-B.

Part: WEB — CRACKED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, BS 1480 STR 41 RT ATT WEB FOUND CRACKED (BODY FAIRING LOCATIONS) DAMAGED SECTION TRIMMED OUT AND PERFORMED EXT PATCH REPAIRED IAW SRM 51-40-02 FIG 1.

Part: SKIN — DAMAGED (LAP JOINT) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, FX - LOWER FUSELAGE EXTERNAL SKIN LAP JOINT ATT RIVET HOLE FOUND OUT OF OVERSIZE CONTERSINK AT STA 2070 TO STA 2080 STRG 46L ( ONE EA ) ( DURING SKIN PANEL REMOVED ). SKIN REPAIRED IAW SRM 53-30-03 FIG 17 SUBSEQUENT INSPECTION ARE NECESSARY FOR THIS CATEGORY B REPAIR REFER TO SRM 53-30-03 FIG 17 TABLE III FOR INSP REQUIREMENT AND EO B747-5330-17977-B.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, BELOW FLOOR BILGE AREA STRINGER FOUND CORROSION CRACKED AT STA 2020 STRG 46R. CORROSION CRACKED STRINGER TRIMMED OFF IAW SRM 51-10-01 AND PERFORMED STRINGER REPAIRED IAW SRM 53-10-03 FIG 1 AT BTN STA 1980 AND STA 2030 AN AREA PAINT TOUCHED UP IAW MM 51-24-11.

Part: WEB — CORRODED (NLG WW) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, NLG W/W BAY RT STA 380 VERTICAL LOWER END ATTACH WEB AREA CORRODED. CORROSION BLEND OUT 0.40 X 1.25 X 4 INCH. NLG WW RT BS 380 VERT STRUCTURE & LOWER END ATTACH WEB REPAIRED AS PER RS R53-18-35076 DEFER THE NEW CRACK REPAIR UNTIL NEXT C-CHECK, REPEAT DETAIL EXTERNAL VISUAL INSPECTION AT 1500 FLIGHT. CYCLES INTERVALS UNTIL NEXT C-CHECK, BUT NOT TO EXCEED 3000 FLIGHT CYCLES. UPS EO B747-5310-19273-A RAISED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, BULK CARGO BAY BS 1920 FRAME ATT WEB ANGLE CRACKED AT STR 40L. ANGLE REPLACED IAW SRM 51-10-01 PG.8

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 986,492 hrs · 25,117 cycles

INSPECTION TYPE: C, L4 DOOR FWD CUT-OUT REVEAL UPPER CRACKED.BS1664 S-17 & S-18 M/D- L4 DOOR FWD CUT-OUT REVEAL REPAIRED AS PER RS R-53-62-35069 AND UPS ENGINEERING FILE NO 747-53-20153

Part: CLIP — CRACKED (AFT CARGO) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, AFT CARGO COMPT. RT STA 1780 STR STR 35 TIE CLIP FOUND CRACKED. TIE CLIP REPLACED AS PER SRM 51-10-01 PG8.

Part: CLIP — CRACKED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, M/D, BS 820 STR 6L FRAME ATT TIE CLIP CRACKED. M/D BS 820 STR 6L FRAME ATT TIE CLIP REPLACED AS PER SRM 51-10-01 P.8.

Part: CLIP — CRACKED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C M/D, BS 840 STR 6L FRAME ATT TIE CLIP CRACKED. M/D BS 840 STR 6L FRAME ATT TIE CLIP REPLACED IAW SRM 51-10-01 P.8.

Part: SHEAR TIE — CRACKED (AFT CARGO) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE:C AFT CARGO COMPT - BELOW FLOOR SUPPORT FRAME LOWER SHEAR TIE PLATE FOUND CRACKED AT STA 1880 LT SIDE STR 43 LT. DEFECT SHEAR TIE TRIMMED OUT IAW SRM 51-10-01 AND PERFORMED SHEAR TIE REPAIRED IAW SRM 53-10-04 FIG 41 AN AREA PAINT TOUCHED UP.

Part: SHEAR TIE — CRACKED (AFT CARGO) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, AFT CARGO COMPT- BELOW FLOOR SUPPORT FRAME LOWER SHEAR TIE PLATE FOUND CRACKED AT STA 1880 LT SIDE STR 44 LT. SHEAR TIE REPAIRED IAW SRM 53-10-04, FIG 41 AT AFT CARGO COMPT STA 1880, BETWEEN S44L.

Part: SHEAR TIE — CRACKED (AFT CARGO) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE:C AFT CARGO COMPT- BELOW FLOOR SUPPORT FRAME LOWER SHEAR TIE PLATE FOUND CRACKED AT STA 1880 LT SIDE STRG 45L. SHEAR TIE REPAIRED IAW SRM 53-10-04 FIG 41 AT AFT CARGO COMPT STA 1880 BETWEEN S45L.

Part: FRAME — CRACKED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, M/D BS 360 S-14 LT FRAME CRACKED. MAIN DECK BS 360 STR 14 LT FRAME REPAIRED AS PER RS R53-12-35070 AND AS PER EO B747-5310-19268-A.

Part: FLOOR SUPPORT — CHIPPED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, M/D - BS 340 STR 13R FRAME FLOOR SUPPORT ANGLE CHIPPED. CHIPPED AREA TRIMMED OFF AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02, HFEC INSPECTED NO CRACK FOUND INSPECTION CARRIED OUT IAW EO B747-5320-17558-B AND UPS-HKG-03-00217H, RESULT - N - CRACK REVEALED, CRES STRAPS INSTALLED IAW EO 747-5320-17558-B IAW RS R-53-15-35074 AND UPS EO B747-5320-17558-C.

Part: RIB — CORRODED (NR 4 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 4 V/C FLAP OB LINKAGE IB RIB NR 1 TO NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION. LT WING - NR 4 VC FLAP OB LINKAGE IB RIB ASSY REPLACED IAW SRM 51-10-01 P8 DUE ACTUATOR MOUNTING HOLES CORROSION REMOVAL EXCEED SRM 57-20-03 FIG 6 LIMIT.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE:C M/D - BS 540 - 541, STR 25R, STRINGER FOUND CRACK AS MARKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2.

Part: RIB — CORRODED (NR 5 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C LT WING NR 5 V/C FLAP IB LINKAGE OB RIB NR 1, NR 2 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM IB CLOCKWISE). NR 1, NR 2 AND NR 8 BOLT HOLES REPAIRED IAW RS 57-41-35066 AND REFER EO B747574019269A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 3 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 3 V/C FLAP I/B LINKAGE O/B RIB NR 2 TO NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM IB CLOCKWISE). NR 2 TO NR 7 BOLT HOLES REPAIRED IAW RS 574135066 AND REFER EO B747574019269A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 7 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 7 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 4 AND NR 6 ROTARY A ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 4 AND NR 6 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 6 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE:C LHW - NR 6 V/C FLAP OB UNKAGE IB RIB NR 4 ROTARY ACTUATOR MOUNTING HOLE FOUND PITTING CORROSION ( COUNT FROM IB CLOCKWISE ). NR4 MOUNTING HOLE REPAIRED IAW RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: DOOR FRAME — CRACKED (ESCAPE DOOR) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, M/D, RT NR 4 DOOR FORWARD FRAME MOST UPPER DOOR FITTING AREA FOUND CRACK. FORWARD FRAME CRACKED AREA REPAIRED IAW RS NR R52-11-35065 AND UPS AUTH NR 747-52-20006.

Part: RIB — CORRODED (NR6 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 6 V/C FLAP IB UNKAGE OB RIB NR 4 AND NR 5 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM IB CLOCKWISE). NR 4 AND NR 5 BOLT HOLES REPAIRED IAW RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 3 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 3 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 5 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 5 AND NR 8 BOLT HOLES REPAIRED AS PER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 8 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 8 V/C FLAP I/B LINKAGE I/B RIB NR 4 AND NR 5 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 4 AND NR 5 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 7 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 7 V/C FLAP O/B LINKAGE O/B RIB NR 1, NR 4 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1, NR 4 AND NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR19 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, RT WING NR 19 V/C FLAP O/B LINKAGE I/B RIB NR 1, NR 7 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION. NR 1, NR 7 AND NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTION.

Part: RIB — CORRODED (NR 9 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 9 V/C FLAP I/B UNKAGE O/B RIB NR 2, NR 3 AND NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2, NR 3 AND NR 7 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, M/D- R1 DOOR AFT UPPER STOP FITTING AREA DOOR FRAME FOUND CRACK. M/D - R1 DOOR AFT UPPER STOP FITTING AREA DOOR FRAME REPAIRED AS PER RS R52-11-35073 AND UPS ENGINEERING FILE 747-52-20007.

Part: RIB — CORRODED (NR 21 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, RT WING NR 21 V/C FLAP O/B LINKAGE IB RIB NR 7 ROTARY ACTUATOR MOUNTING AREA FOUND CORRODED ( COUNT FROM IB CLOCKWISE ). NR 7 BOLT AREA REPAIRED IAW RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 26 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, RT WING NR 26 V/C FLAP O/B LINKAGE I/B RIB NR 1 TO NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1 TO NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 8 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LEFT WING NR 8 V/C FLAP I/B LINKAGE O/B RIB NR 3, NR 5 AND NR 6 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 3, NR 5 AND NR 6 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 18 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, RIGHT WING - NR 18 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). FINAL HOLE SIZE 0.434 INCH AT HOLE NR 4. RIGHT WING NR 18 V/C FLAP O/B LINKAGE I/B RIB REPLACED IAW SRM 51-10-01 PG 8.

Part: RIB — CRACKED (NR 26 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, RT WING NR 26 V/C FLAP I/B LINKAGE I/B AND O/B SUPPORT RIBS FOUND CRACKED. RT WING NR 26 V/C FLAP I/B LINKAGE BOTH I/B AND O/B RIBS REPLACED IAW SRM 51-10-01 PG 8.

Part: RIB — CORRODED (NR 2 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 2 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 6 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 6 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CRACKED (TE FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 3 V/C FLAP O/B LINKAGE O/B SUPPORT RIB FOUND CRACKED. LT WING NR 3 V/C FLAP O/B LINKAGE O/B SUPPORT RIB REPAIRED AS PER RS R57-41-35067 & UPS CONTINUE EO B747-5740-19269-A RAISED.

Part: RIB — CORRODED (NR 9 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 9 V/C FLAP O/B UNKAGE O/B RIB NR 8 ROTARY ACTUATOR MOUNTING HOLE FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 8 BOLT HOLE REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 1 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 1 V/C FLAP O/B LINKAGE I/B RIB NR 2 TO NR 6 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 6 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 21 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, RT WING NR 21 V/C FLAP O/B LINKAGE O/B RIB NR 3 TO NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 3 TO NR 7 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

BS 554 RBL 46 TIE DOWN TRACK LT FLANGE CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.045 X 1 X 3 EXCEED SRM 53-10-01 FIG 1 LIMITS , FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 6. CIC APPLIED IAW EO M-5100-2780-E

Part: FRAME — CORRODED (MLG WW BLKHD) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WLG WHEEL WELL STA 1241 BULKHEAD UPPER SECTION AREA CORROSION REVEALED AT LBL 65, 70, 74 AND 90. UPPER SECTION REPAIRED AS PER RS 53-48-35072 REFER CWS FOR WORK DETAIL AND ENGINEERING FILE NO : 747-53-20158 DUE TO BLEND DEPTH 0.090 INCH X 2 INCHES X 3 INCHES AREA EXCEEDS SRM 53-10-01 FIG 1 LIMITATION.

Part: RIB — CORRODED (NR 18 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, RT WING NR 18 V/C FLAP I/B LINKAGE O/B RIB NR 1 TO NR 3, NR 5, NR 6 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1 TO NR 3, NR 5, NR 6 AND NR 8 BOLT HOLES REPAIRED AS PER RS 574135066 AND REFER EO B747574019269A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 1 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 1 V/C FLAP I/B LINKAGE O/B RIB NR 2 TO NR 5 ROTARY ACTUATOR MOUNTING HOLES FOUND FITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 TO NR 5 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 19 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, RT WING - NR 19 V/C FLAP O/B LINKAGE O/B RIB NR 1, NR 6 AND NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1, NR 6 AND NR 7 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CRACKED (NR 5 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 5 V/C FLAP O/B LINKAGE O/B SUPPORT RIB FOUND CRACKED. LT WING NR 5 V/C FLAP O/B LINKAGE O/B SUPPORT RIB REPAIRED AS PER RS NR R57-41-35067 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 4 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 4 V/C FLAP I/B LINKAGE O/B SUPPORT RIB FOUND CORROSION CRACKED. RIB ASSY REPAIRED IAW SRM 51-10-01 PG 8.

Part: RIB — CORRODED (NR 2 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 2 V/C FLAP I/B LINKAGE O/B RIB NR 2 TO NR 6 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). BOLT HOLES NR 2 TO NR 6 AND NR 8 REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 19 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, RT WING NR 19 V/C FLAP I/B LINKAGE O/B RIB NR 4 TO NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 4 TO NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 10 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING - NR 10 V/C FLAP I/B LINKAGE I/B RIB NR 1 TO NR 5 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1 TO NR 5 AND NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 20 V/C FLAP)

INSPECTION TYPE: C, RT WING - NR 20 V/C FLAP I/B LINKAGE O/B RIB NR 2, NR 3 AND NR 8 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2, NR 3 AND NR 8 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTION.

Part: RIB — CORRODED (NR 20 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, RT WING - NR 20 V/C FLAP O/B LINKAGE I/B RIB NR 8 ROTARY ACTUATOR MOUNTING HOLE FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 8 BOLT HOLE REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 8 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 8 V/C FLAP O/B UNKAGE I/B RIB NR 2 AND NR 3 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 2 AND NR 3 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CORRODED (NR 19 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, RT WING NR 19 V/C FLAP I/B LINKAGE I/B RIB NR 1 TO NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). NR 1 TO NR 7 BOLT HOLES REPAIRED AS PER RS 57-41-35066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: RIB — CRACKED (NR 4 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING - NR 4 V/C FLAP O/B LINKAGE O/B SUPPORT RIB FOUND CRACKED. LT WING NR 4 V/C FLAP O/B LINKAGE O/B SUPPORT RIB REPAIRED AS PER RS NR R57-41-35067 AND AS PER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

BS 400 FLOORBEAM UPPER SECTION UPPER FACE BTN RBL 0 / RBL 37 CORRODED. CORROSION REMOVED IAW SRM 51-10-01 CORROSION BLEND OUT 0.050 INCH X 1 INCH X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, FOR BS400 RBL 0" REPAIR REFER SRM 53-10-07 FIG 8. CIC APPLIED IAW EO M5100-2780-E. AND BS400 RBL 37 CORROSION BLEND OUT 0.005 X 1 X 1 WITHIN SRM 53-10-01 FIG 1 LIMITS.

Part: RIB — CORRODED (NR 10 V/C FLAP) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT WING NR 10 V/C FLAP I/B LINKAGE O/B RIB NR 4, NR 5 AND NR 7 ROTARY ACTUATOR MOUNTING HOLES FOUND PITTING CORROSION (COUNT FROM I/B CLOCKWISE). BOLT HOLE NR 4, NR 5 AND NR 7 REPAIRED AS PER RS 574135066 AND REFER EO B747-5740-19269-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, BS 500 - 520 RBL 46 TIE DOWN TRACK RT FLANGE CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 10 EXCEED SRM 53-10-01 FIG 1 LIMITS FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 6. CIC APPLIED IAW EO M5100-2780-E

Part: SKIN — CRACKED (FUSELAGE) · airframe 986,492 hrs · 25,117 cycles

INSPECTION TYPE: C, LOWER FUSELAGE EXTERNAL SKIN EDGE FOUND CRACKED AT STA 1480 RT SIDE STR 41 TO 42 RT. LOWER FUSELAGE EXTERNAL SKIN REPAIRED AS IAW RS NR R-53-61-35068 JUST AT STA 1480 RT SIDE STR 41R TO STR 42R AND REF UPS ENGINEERING FILE NR 747-53-20154.

Part: SKIN — CRACKED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, RT STA 2638 STR 8-9 SKIN CRACKED (ABOVE I/B ELEV). SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, ONE EACH FASTENER HOLE FOUND CRACK AT BS 1830 STR 4R APPROX 0.020 INCH LONG RUNNING TOWARD AFT. CRACKED PORTION AT TOP SKIN WERE TRIMMED OFF IAW SRM 51-10-01 AND 51-10-02 NDT INSP THE CUT-EDGE NO DEFECTS AND PERFORMED A EXT PATCH REPAIRED AT AFFECT AREA IAW SRM 53-30-03 FIG 17 AN AREA PAINT TOUCHED UP IAW MM51-24-11.

Part: BOLT — BROKEN (EMPENNAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, HORIZONTAL STAB BOX INTERIOR RT BL 43.5 WEB UPPER CORNER 2 EACH MOUNTING SCREW BROKEN. HORIZONTAL STAB BOX INTERIOR RT BL 43-5 WEB UPPER CORNER UPPER BOLT HOLE OVERSIZED AND BOLT REINSTALLED IAW SB 747-55A2050 R1 LWR BOLT REPLACED PER MM 20-51-01.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C U/D, BS 480 - 500 RBL 65 TIE DOWN TRACK LT FLANGE CORRODED. CORROSION BLEND OUT 0.045 INCH X 1 INCH X 12 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. CORROSION REMOVED IAW SRM 51-10-01. SEAT TRACK REPAIRED REFER TO SRM 53-10-05 FIG 6. CIC APPLIED IAW EO M5100-2780-E

Part: ANGLE — CORRODED (NLG WW) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, FX NOSE TUNNEL RT WW SIDEWALL ATTACH ANGLE CORRODED AT STA 380. CORROSION BLEND OUT 0.040 X 1.25 X 4 INCH. BS 380 RT VERT ANGLE REPAIRED AS PER RS R53-18-35076 AND UPS EO B747-5310-19273-A FOR REPEAT DETAIL EXTERNAL VISUAL INSPECTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, M/D SEAT TRACK FOUND CORRODED AT SEVERIAL LOCATIONS AS MARKED. REF WAN NR 796157. CORROSION BLEND OUT 0.039 INCH X 1 INCH X 4 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, CORROSION REMOVED IAW SRM 51-10-01 AND SEAT TRACK REPAIRED REFER TO SRM 53-10-05 FIG.1A. CIC APPLIED IAW EO M-5100-2780.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, FX - BS 2300 FRAME BELOW FLOOR SHEAR TIE FOUND CORRODED AS MARKED AT BL 0. CORROSION BLEND OUT 0.050 X 1 X 2 INCH. M/D BS 2300 BL SHEAR TIE REPAIRED PER SRM 53-10-04 FIG 3.

Part: FRAME — CRACKED (NR 1 PYLON) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, NR 1 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT FWD FRAME WEB. DETAILS PLS REFER ATTACHED FIGURE. FRAME WEBS REPLACED AND REPAIRED AS IAW RS NR R-54-53-35064 INSPECTIONS TO CONTINUE PER UPS EO B747-5410-13908 ( UPS ENGINEERING FILE NR 747-54 -20040) RAISED.

Part: WEB — CRACKED (NR 3 PYLON) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, SEVERAL CRACKS WERE FOUND AT NR 3 PYLON REAR MOUNT BULKHEAD FORWARD AND AFT FRAME WEB, DETAILS PLEASE REER ATTACHED FIGURE. FRAME WEBS REPLACED AND REPAIRED AS PER RS R54-53-35063 INSPECTIONS TO CONTINUE PER UPS EO B747-5410-13908 AND UPS ENGINEERING FILE NR 747-54-20040.

Part: FRAME — CRACKED (NR 4 PYLON) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE:C NR 4 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT OB FORWARD FRAME WEB. FRAME WEBS REPLACED AND REPAIRED AS IAW RS R-54-53-35064 INSPECTIONS TO CONTINUE IAW UPS EO B747-5410-13908 ( UPS ENGINEERING FILE NR 747-54 -20040 RAISED).

Part: ANGLE — CORRODED (NLG WW) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, FX NOSE TUNNEL LT WW SIDEWALL ATTACH ANGLE CORRODED AT STA 380. CORROSION BLEND OUT 0.040 X 1 X 4 INCH. THE ANGLE REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: PANEL — BULGED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, M/D BS 1241-1244, RBL 8 - 11 BELOW FLOOR CANTED BULKHEAD APU FUEL LINE CLOSEOUT PANEL FWD RT CORNER BULGE UP AND RIVET SHEARED. CORROSION BLEND OUT 0.035 X 1.5 X 4 INCH. EXISTING DOUBLER REMOVED AND NEW EXTENDED DOUBLER REPAIR AS PER RS R53-48-35075 AND ENGINEERING FILE NUMBER 747-53-20156.

Part: PANEL — CORRODED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, M/D BS 1241 LBL 75-79 BELOW FLOOR CANTED BULKHEAD CLOSEOUT PANEL CUTOUT CORRODED. CORROSION BLEND OUT 0.050 X 1 X 3 INCH. CLOSEOUT PANEL CUTOUT REPAIRED AS PER SRM 53-10-07 FIG 6.

Part: SKIN — CORRODED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, M/D BS 1239-1241 RBL 35-38 BELOW FLOOR WING CENTER SECTION UPPER SKIN UPPER FACE CORRODED. CORROSION BLEND OUT 0.056 X 3 X 4 INCH. REPAIR PARTS INSTALLED AS PER RS NR R57-14-35078 AND UPS ENGINEERING FILE NR 747-57-20047.

Part: SKIN — CRACKED (FUSELAGE) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, LT SIDE AT STA 570 EQUIPMENT COOLING OUTLET CUTOUT FWD FASTENER HOLE FOUND ONE EACH HOLE CRACKED APPROX .0625 INCHES IN LENGTH RUNNING AFT. PLS REEFR ATT. SKETCH. FX STA 560 TO 580 COOLING OUTLET CUTOUT WAS REPAIRED AS PER EO B747-5330-6909-D.

Part: SKIN — DEBONDED (THURST REVERSER) · airframe 98,649 hrs · 25,117 cycles

INSPECTION TYPE: C, DMI : D252292 - NR 4 ENG FAN THRUST REVERSER I/B SLEEVE DENTED, LOCATED 12 INCHES OF SEAM 6 O'CLOCK POS AND 11 INCHES FROM FWD EDGE 3 INCHES FROM AFT EDGE 4 W X 4 L X 0.032 D (REF EO B747-7830-18117). REPAIRED AS PER RS NR R-78-30-35071 AND AS PER EO B747-7830-19255-A FOR REPEAT INSPECTION INSTRUCTIONS.

Part: SKIN — DAMAGED (VERTICAL STAB)

ON WALKAROUND INSPECTION FOUND DAMAGE (FROM WING PANEL DEPARTING) ON VERTICAL FIN LT SIDE DAMAGE APPROX 24 X 15 INCHES. ACCOMPLISHED INTERIM REPAIR TO VERTICAL STABILIZER PER EO B747-5100-19 029.

Part: HYDRAULIC SYSTEM — FAILED (NR 2)

ATB - NR 2 HYD SYSTEM FAILURE. REMOVED & REPLACED NR 2 EDP AS REQUIRED DUE TO OVERHEAT IAW MM 29-11-05. OPS & LEAK CHECK REQUIRED. RAN NR 2 ENG FOR LEAK CHECK OF NR 2 HYD (EDP) PUMP GROUND CK'S NORMAL. OK FOR SERVICE. HYD PRESSURE CHECK NORMAL.

Part: COMPRESSOR — STALLED (NR 3 ENGINE)

AIR TURNBACK NR 3 ENG COMPRESSOR STALL IN CLIMB AT FL190 PAX REPORTED GLOW IN N1 SECTION. EGT RISING, ENG SHUTDOWN. REMOVED AND REPLACED NR ENGINE S/N OFF P685985CN, INSTALLED S/N P662942 PER TC 5000, 5001, 5016 & MM 71-00-00 OPS & LEAK CHECK GOOD. OK FOR CONTINUED SERVICE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 97,459 hrs · 24,873 cycles

INSPECTION TYPE: SPV, AFT CARGO BAY, STR 34L CRACKED AT BS 1660 (1 INCH) & BS 1720 (0.875 INCH) AT FRAME ATTACH AREA. STRINGER 34L AT BS 1660 & 1720 REPAIRED IAW SRM 53-10-03 FIG 2.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT FWD EMERGENCY EXIT LIGHT OUT MAIN ENTRY DOOR IS INOP. REMOVED AND REPLACED M415 ERF 33-15-05.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A MAIN DECK EMERGENCY LIGHT INOP. CHARGED EMERGENCY LIGHTS, OPS CHECK NORMAL

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C AFT CARGO COMPT- BS 1900 BETWEEN STR 51L TO 51R SHEAR TIE FOUND CRACKED. AFT CARGO COMPT- BS 1900 BETWEEN STR 51L TO 51R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A.

Part: RIB — CORRODED (RT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C RT WING- NR 20 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 5, NR 8 BOLT HOLE FOUND SURFACE CORROSION. RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02.

Part: RIB — CORRODED (RT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C RHW - NR 24 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 2, 3, 5 - 8 BOLT HOLE FOUND SURFACE CORROSION. CORROSION BLEND OUT FINAL SIZE NR 2 & 3 - 0.388", NR 7 & 8 - 0.498". RT WING - NR 24 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02.

Part: RIB — CORRODED (RT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C RT WING- NR 22 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 5 & 6 BOLT HOLE FOUND SURFACE CORRODED. CORROSION BLEND OUT AT BOLT HOLES FINAL DIAMETERS 0.371" TO 0.434" WITH NR 4, 5, 6 OVERSIZED ECCENTRICALLY. RT WING- NR 22 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02.

Part: RIB — CORRODED (RT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C RT WING- NR 25 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT BOLT HOLE FOUND SURFACE CORROSION. FROM NR 1 - NR 8 BOLT HOLE. RIB REPLACED IAW SRM 51- 10-01 PG 8 AND SRM 51-30-02.

Part: RIB — CORRODED (RT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C RT WING- NR 25 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1-NR 6 BOLT HOLE FOUND SURFACE CORROSION. RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02.

Part: RIB — CORRODED (RT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C RT WING- NR 18 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1-NR 8 BOLT HOLE FOUND SURFACE CORROSION. RIB REPLACED IAW SRM 51- 10-01 PG 8 AND SRM 51-30-02.

Part: RIB — CORRODED (RT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C RHW- NR 24 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1 - 8 BOLT HOLE FOUND SURFACE CORRODED. CORROSION BLEND OUT AT BOLT HOLES NR 1 & 8 - 0.434", NR 2 & 3 - 0.530", NR 7 - 0.465", NR 4 - 0.404", NR 5 - 0.437" , NR 6 - 0.404". RT WING- NR 24 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02.

Part: RIB — CORRODED (RT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C RT WING- NR 23 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1 - 8 BOLT HOLE FOUND SURFACE CORRODED. CORROSION BLEND OUT AT MOUNT BOLT HOLES FINAL DIAMETERS 0.434" - 0.500". RT WING- NR 23 L/E FLAP I/B ROTARY ACTUATOR MOUNT RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02.

Part: RIB — CORRODED (RT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C RT WING- NR 23 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB SUPPORT NR 1 - 8 BOLT HOLE FOUND SURFACE CORRODED. CORROSION BLEND OUT AT MOUNT BOLT HOLES FINAL DIAMETERS 0.371" TO 0.434". RT WING - NR 23 L/E FLAP O/B ROTARY ACTUATOR MOUNT RIB REPLACED IAW SRM 51-10-01 PG 8 AND SRM 51-30-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C, BS 980 RT FWD UPPER DRAG SPLICE FITTING FOUND MOST AFT HOLE AT SKIN ATTACH FLANGE CRACKED RUNNING FWD APPROX .0625 INCH LONG. HOLE OVERSIZED TO 0.278 INCH PER SRM 51-30-05 WITHIN SRM 53-30-03 FIG 60 LIMITATIONS.

Part: SPAR — CORRODED (RT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C, RT JETTISON PUMP ATT BONDING JUMPER ATT REAR SPAR BOLT HOLE SURFACE CORR AT WLG W/W STA 1241 RT AFT FACE RBL 91.8. CUTOUT RT WLG W/W BS 1241 REAR SPAR WEB JETTISON PUMP, CUTOUT ATT BONDING JUMPER ATT. FASTENER HOLE REPAIRED IAW RS R57-12-34823.

Part: FITTING — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C, BS 980 LT FWD UPPER DRAG SPLICE FITTING. FOUND HORIZONTAL FLANGE MOST FWD HOLE CRACKED RUNNING I/B APPROX .0625 INCH LONG STR L38 TO L38. BS 980 LT FWD UPPER DRAG SPLICE FITTING REPLACED AS PER SRM 51-10-01 PG 8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C, BS 980 LT FWD BATHTUB FITTING FOUND CHORD MOUNTING FLANGE 3 HOLES CRACKED. ONE HOLE AT UPPER BATHTUB FOUND 2 CRACKS RUNNING I/B APPROX .0625 AND .125 ANOTHER HOLE AT LOWER BATHTUB FOUND CRACK RUNNING I/B APPROX .1875, THE LOWEST HOLE OF THE FLANGE FOUND CRACK RUNNING DOWN APPROX .6250. CUTOUT BS 980 LT BATHTUB FITTING REPLACED IAW SRM 51-10-01 PG 8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C, BS 980 LT FWD LOWER DRAG SPLICE FITTING FOUND SKIN ATT FLANGE 6TH FASTENER HOLE CRACKED RUNNING DOWN APPROX .0625 INCH LONG. BS 980 LT FWD LWR DRAG SPLICE FITTING REPLACED AS PER SRM 51-10-01 PG 8.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C, BS 980 RT BULKHEAD WEB STR R38 1 HOLE COMMON TO BATHTUB UPPER FITTING FOUND CORROSION FROM 5 O/C TO 9 O/C POSITION (LOOK FROM FWD). BS 980 RT BULKHEAD WEB STR R38 HOLE COMMON TO BATHTUB UPPER FITTING REPAIRED AS PER RS R53-23-34817.

Part: FITTING — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C BS 980 RT FWD BATHTUB FITTING (STR R38) FOUND CHORD MOUNTING FLANGE 2 HOLES CRACKED. ONE HOLE AT UPPER BATHTUB FOUND CRACK RUNNING I/B APPROX .25 INCH LOWEST HOLE OF THE FLANGE FOUND 3 CRACKS APPROX .25 INCH LONG EACH. BS 980 RT FWD BATHTUB FITTING. REPAIRED AS PER RS R-53-23-34817.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT- RT BS 980 STR 37 FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: RIB — CORRODED (RT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C RHW- NR 22 L/E FLAP O/B ROTARY ACTUATOR MOUNTING RIB SURFACE CORRODED. CORROSION BLEND OUT AT SURFACE AT MOUNT BOLT HOLES NR 1 & 2 - 0.025" AT BOLT HOLES BORE NR 1 TO 6 - FINAL DIA 0.312" NR 7 - 0.371", NR 8 - 0. 312" RT WING NR 22 L/E FLAP O/B ROTARY ACTUATOR MOUNTING RIB REPAIRED AS PER RS R-57-41-34824.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT RT BS 980 STR 38 FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT - LT BS 960 BETWEEN S38L FOUND FRAME SHEAR TIE 2 EA HOLES CRACK. FWD CARGO COMPT LT BS 960 BETWEEN S38L - 39L FRAME SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT- BS 980 LT STR 38 FOUND CRACK. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT- RT BS 960 BETWEEN S38R - 39R FOUND FRAME SHEAR TIE 1 EA HOLE CRACK APPROX .25 INCH LONG. FWD CARGO RT BS 960 BETWEEN S38R-39R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D- FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLENDOUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER SRM FIG 51-40-04 FIG 1.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- STA 1480 KEEL BEAM PANEL SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT LBL 17 TO RBL 17 (AS MARK). CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01 PG 8.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX-KEEL BEAM PANEL SUPPORT LOWER CHORD UPPER AND LOWER SURFACE FOUND SURFACE CORROSION AT STA 1287 RBL 16 TO LBL 16. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS FOR REPLACEMENT REFER TO SRM FIG 51-10-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D-ZONE-E SEAT TRACK FOUND CORROSION AT BS 2190-2220 RBL 33. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 1A.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX-RT KEEL BEAM BOX SUPPORT PANEL ATT BRACKET FOUND SURFACE CORROSION AT BS 1098 RBL 9. CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- BS 1183 RT SIDE KEEL BEAM PANEL ATT BRACKET FOUND SURFACE CORROSION AS MARK. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D- ZONE-E FLOOR SUPPORT FOUND CORROSION AT BS 2200-2220 LBL 98. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX-KEEL BEAM PANEL SUPPORT LOWER CHORD UPPER AND LOWER SURFACE FOUND SURFACE CORROSION AT STA 1276 TO STA 1350 LBL 16. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 51-40-03 FIG 1.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- KEEL BEAM PANEL SUPPORT ATT BRACKET FOUND SURFACE CORROSION AT STA 1287 RBL 9 AND LBL 9 BOTH SIDE (TWO EA). CORROSION REMOVED IAW SRM 51-10-01. BLEND-OUT NOT WITHIN SRM 53-10-01 FIG 1, LIMITS FOR REPLACEMENT REFER TO SRM FIG 51-10-01 PG 8.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- BS 1227 RT SIDE KEEL BEAM PANEL ATT BRACKET FOUND SURFACE CORROSION. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D SEAT TRACK FOUND CORROSION AT BS 2224 LBL 90. CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR SRM FIG 53-10-05 FIG 1A.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- KEEL BEAM PANEL SUPPORT LOWER CHORD UPPER AND LOWER SURFACE FOUND SURFACE CORROSION AT STA 1307 LBL 16 TO RBL 16. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D- ZONE-E SEAT TRACK FOUND CORROSION AT BS 2240-2280 LBL 33. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 1A.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- BS 1205 RT SIDE KEEL BEAM PANEL ATT BRACKET FOUND SURFACE CORROSION AS MARK. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS FOR REPLACEMENT REFER TO SRM FIG 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX-KEEL BEAM PANEL SUPPORT LOWER CHORD UPPER AND LOWER SURFACE FOUND SURFACE CORROSION AT STA 1329 LBL 16 TO RBL 16. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS FOR REPLACEMENT REFER TO SRM FIG 51-10-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D- ZONE-E SEAT TRACK FOUND BULGE UP AT BS 2150 - 2163 LBL 98. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01 PG 8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D- FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D- SEAT TRACK FOUND SLIGHTLY CORRODED BS 510-BS 520, LBL 91. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 1A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D- FLOOR SUPPORT FOUND SLIGHTLY CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-07 FIG 8.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- BS 1078 RT KEEL BEAM PANEL SUPPORT ATT BRACKET FOUND CORROSION AT RBL 9. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPLACEMENT REFER TO SRM FIG 51-10-01.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D-BS 262 LBL 51 FLOOR FITTING ATT PLATE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 51-10-01, LIMITS FOR REPLACEMENT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- BS 440 STR 42L - 43L CORROSION. FOUND CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-30-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-30-03 FIG 1.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D- SEAT TRACK FOUND CRACK BS 460 RBL R88. SEAT TRACK REPLACED AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D- SEAT TRACK FOUND SLIGHTLY CORRODED BS 240 TO 260, RBL 50 TO RBL 53. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D SEAT TRACK FOUND CORRODED BS 406 TO 406, RBL R57. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-05 FIG 1A.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- LT SIDE AIR CONDITIONING BAY BS 1241 SLOPE PANEL. LOWER SURFACE SUPPORT RETAINER FOUND CORROSION AT LBL 90 TO LBL 94. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, REPLACEMENT REFER TO SRM FIG 51-10-01 PG 8.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C AFT CARGO BS 1900 BETWEEN STR 43L TO STR 47L SHEAR TIE FOUND CRACKED. AFT CARGO BS 1900 BETWEEN STR 43L TO STR 47L SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- LT BS 1480 BULKHEAD TO FX CHORD CRACKED AT STR 38L. CHORD REPAIRED AT BS 1480 STR 38L AS PER SRM 51-40-03.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C AFT CARGO - BS 1800 BETWEEN STR 47R & STR 48R SHEAR TIE FOUND CRACKED. AFT CARGO BS 1800 BETWEEN STR 47R & STR 48R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D-BS 360 STR 14- 14AL FRAME WEB FOUND CRACK. FRAME WEB REPAIRED AS PER SRM 51-40-03 FIG 3.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- LT BS 1480 BULKHEAD WEB CRACKED AT STR 34L AS MARKED. BULKHEAD WEB REPAIRED AS PER SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C NOSE W/W INTERIOR TOP SURFACE LONGITUDINAL BEAM FOUND CRACKED AT BS 320 LBL 22. ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 08 & 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D SEAT TRACK FOUND CORROSION CRACK. SEAT TRACK REPLACED AS PER SRM 53-10-05 FIG 1A.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C AFT CARGO - BS 1760 BETWEEN STR 48R & STR 49R SHEAR TIE FOUND CRACKED. AFT CARGO BS 1760 BETWEEN STR 48R & STR 49R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C, M/D - NR 1L DOOR FWD FRAME CUTOUT NR 1 STOP FITTING FOUND CRACKED (COUNT FROM LWR). M/D NR 1L DOOR FWD FRAME CUTOUT NR 1 STOP FITTING REPLACED AS PER SRM 51-10-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C AFT CARGO - BS 1680 BETWEEN STR 50R & STR 51R SHEAR TIE FOUND CRACKED AFT CARGO BS 1680 BETWEEN STR 50R & STR 51R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C AFT CARGO - BS 1680 BETWEEN STR 49R & STR 50R SHEAR TIE FOUND CRACKED. AFT CARGO - BS 1680 BETWEEN STR 49R & STR 50R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C AFT CARGO - BS 1900 - 1910 RBL 43 LONGITUDINAL FLOOR SUPPORT FOUND CORRODED AT UPPER AND LWR CHORD. CORROSION REMOVED IAW SRM 51-10-01, BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1, FOR REPLACEMENT REFER TO SRM FIG 51-10-01 P 8.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C AFT CARGO BS 1800 BETWEEN STR 48R & STR 49R SHEAR TIE FOUND CRACKED. AFT CARGO BS 1800 BETWEEN STR 48R & STR 49R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A.

Part: WEB — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C, NOSE W/W LT VERTICAL SIDEWALL WEB FOUND BULGE UP AT STA 380 WL 187. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPAIR REFER TO RS R53-18-34814.

Part: FITTING — DETERIORATED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C AFT CARGO - BS 1480 STR 51R STRINGER FWD FITTING FOUND DETERIORATED. STRING END FITTING REPLACED AS PER SRM 51-10-01.

Part: WEB — CORRODED (RT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- RT WING CTR SECTION FRONT SPAR LOWER CHORD ATT WEB EXTERIOR SURFACE FOUND HEAVY CORROSION AT BS 1000 RBL 65-73. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 57-10-01 LIMITS, FOR REPAIR REFER TO RS R53-43-34815.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D- RT BS 2231 FRAME REVEAL FOUND CRACK AT REVEAL CUTOUT BETWEEN S24R AND S25R. M/D- RT BS 2231 S24R & S25R FRAME REVEAL REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO - BS 720-740 STR - 33R FOUND CORRODED (2 LOCATION). CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-03 FIG 1.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C AFT CARGO - BS 1660-1680 LBL 20-40 FLOORBEAM SURFACE WEB FOUND CRACKED. AFT CARGO - BS 1660-1680 LBL 20-40 FLOORBEAM SURFACE WEB REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C NOSE WHEEL WELL LT WALL LONGERON BEAM FOUND CRACKED AT BS 320-340 NR 3 BEAM (COUNT FROM TOP). REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 08 & 51-30-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C M/D- BS 2188 S-3L STRINGER END FOUND CRACKED. CRACKED STRINGER REPAIRED PER RS R53-61-34819.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C AFT CARGO - BS 1660 BETWEEN STR 47R & STR 48R SHEAR TIE FOUND CRACKED. AFT CARGO - BS 1660 BETWEEN STR 47R & STR 48R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C RT BS 1480 BULKHEAD HOLE NR 5 CRACK FOUND ON EXTENSION FITTING APPROX .0625 INCH RUNNING AFT. REPAIR CARRIED OUT IAW SB747-53A2390 FIG 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C NOSE WHEEL WELL FWD BULKHEAD VERTICAL FRAME CHORD FOUND CRACKED AT BS 260 RBL 11 NR 2 LATERAL BEAM (COUNT FROM TOP). FRAME CHORD REPLACED AS PER SRM 51-10-01 PG 08 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO - BS 860 RT FRAME FOUND CRACKED AT STR 38R. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO - BS 680 RT FRAME FOUND CRACKED BETWEEN STR 39R AND STR 40R. FRAME REPAIRED AS PER RS R-53-22-34809.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO - BS 900 RT FRAME BETWEEN STR - 28R AND STR 29R FOUND CRACKED. FWD CARGO BS 900 RT FRAME BETWEEN STR -28R & 29R REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO- FRAME TIE CLIP FOUND CRACKED AT BS 840 STR 45L - 46L. FWD CARGO BS 840 STR 45L-46L FRAME TIE CLIP REPAIRED AS PER SRM 53-10-04 FIG 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO - BS 880 RT FRAME BETWEEN STR 30R AND STR 31R FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C COCKPIT - FLOORBEAM FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-07 FIG 23.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD WEB FASTENER HOLE NR 21 CRACK REVEALED APPROX 0.040 INCH IN LENGTH RUNNING O/B. REPAIR CARRIED OUT IAW SB747-53A2390 FIG 11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C, LT BS 1480 STR L33 BULKHEAD NR 9 HOLE FOUND TWO CRACKS AT EXTENSION FITTING. REPAIR CARRIED OUT IAW REPAIR SCHEME HX-RS NR R53-63-34822 FOR FABRICATION OF REPAIR BUSHING AND WASHER REFER TO CWPC CONTROL SEQ TEHI 0 12 - 108 AND TEHI 0 12 - 109.

Part: FITTING — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD NR 9 HOLE FOUND TWO CRACKS AT OUTER CHORD SPLICE FITTING. REPAIRED AS PER SB747-53A2390 FIG 11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C COCKPIT- FLOORBEAM FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REF SRM FIG 53-10-07 FIG 23.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C RT SIDE BS 800 FRAME FOUND ONE FASTENER HOLE CRACKED AT FRAME INNER CHORD ANGLE AND STRAP. FRAME CHORD AND STRAP REPAIRED AS PER RS R-53-22-34808.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C, LT BS 800 FRAME INNER CHORD AND STRAP, ONE FASTENER HOLE CRACK FOUND ON S16 AREA, CRACK THROUGH THICKNESS RUNNING FWD AND AFT DETAIL. LT BS 800 FRAME CHORD AND STRAP S15L-17L REPAIRED REFER RS R53-22- 34808.

Part: SPLICE — CRACKED (LT WING) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C LT WING REAR SPAR TO WING CTR SECTION UPPER SPLICE FITTING FOUND CRACKED AT RADIUS AREA. LT UPPER SPLICE FITTING REPLACED AS PER EO B747-5740-4366 APP H PG 46.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C, FWD CARGO - STRINGER END FOUND CRACKED AT BS 742 STR 40R. STRINGER END REPAIRED AS PER RS R53-21-34811.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT- BS 900 S43L AREA SHEAR TIE CRACK. SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3.

Part: CLIP — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C NWW TUNNEL - RT BS 280 VERTICAL BEAM NR 2 STIFFENER CLIP (COUNT FROM TOP) FOUND CRACKED. NR 2 STIFFENER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 8 AND 51-30-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT- BS 980 S39L FRAME CRACK. FRAME CRACK AREA REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C NWW TUNNEL - LT BS 300 VERTICAL BEAM NR 3 CLIP (COUNT FROM TOP ) FOUND CRACKED. CLIP REPLACED AS PER SRM 51-10-01.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT- BS 900 S46R TO S47R SHEAR TIE CORRODED. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT NOT WITHIN SRM 53-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO SRM FIG 53-10-04 FIG 3.

Part: ACCESS PANEL — CRACKED (NR 1 PYLON) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C NR 1 PYLON ACCESS PANEL NR 452 BL CUTOUT ARE CRACKED AT 2 LOCATIONS AS MARKED. CUTOUT NR 1 PYLON ACCESS PANEL NR 452 BL REAR CUTOUT TWO LOCATIONS REPAIRED IAW RS R54-51-34816.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C NWW TUNNEL - LT BS 320 VERTICAL BEAM WEB FOUND CRACKS AT NR 1, 2, 3 AND 6 STAND OFF HOLES (COUNT FROM TOP). VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C BS 400 PRESSURE PAN, ONE EA FASTENER HOLE CRACK INDICATION REVEALED. PRESSURE PAN BS 400 REPLACED AS PER SRM 51-10-01 AND DWG 624U0005 STEERING CABLE CONNECTED, RIGGING CHECK AND O/P CHECK AS PER MM 32-51-00 FOUND SATISFACTORY.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C NWW TUNNEL - LT BS 300 VERTICAL BEAM WEB FOUND CRACK AT NR 1 STAND OFF HOLE (COUNT FROM TOP). WEB REPLACED AS PER SRM 51-10-01 PG 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT - BS 980 S41L FRAME CRACK. FWD CARGO COMPT BS 980 S-41L FRAME CRACKED AREA REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT- BS 960 S46R AREA SHEAR TIE CRACKED. SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT - BS 980 S39R FRAME CRACK. FRAME CRACK AREA REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: CLIP — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C NWW TUNNEL - LT BS 320 VERTICAL BEAM NR 2 STIFFENER CLIP FOUND CRACKED. CLIP REPLACED AS PER SRM 51-10-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT - BS 900 S41L AREA SHEAR TIE CRACK. SHEAR TIE REPAIRED PER SRM 53-10-04 FIG 40.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C NWW TUNNEL - RT BS 320 VERTICAL BEAM WEB FOUND CRACK AT NR 1 STAND OFF HOLE (COUNT FROM TOP). WEB REPLACED AS PER SRM 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT-BS 920 S40R AREA SHEAR TIE CRACK. SHEAR TIE REPAIRED AS PER SRM 53-10-4 FIG 4.

Part: SKIN — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C AFT CARGO COMPARTMENT CUTOUT FWD UPPER CORNER FOUND CRACKS AT FUSELAGE SKIN AND SKIN DOUBLER BS 1820, STR R27. AFT CARGO COMPT DOOR CUTOUT FWD UPPER CORNER SKIN AND SKIN DOUBLER REPAIRED IAW RS R53-61-34807.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT - BS 1000 BULKHEAD BETWEEN S41L AND 42L LOWER CHORD CRACK. C/OUT FWD CARGO COMPT - BS 1000 BULKHEAD LOWER CHORD BETWEEN S401 TO S451 SECTION SEGMENT REPLACED IAW SRM 51-10-01 PG 8 AND DWG 65B10098-1 AND SB-747-53-2444.

Part: CLIP — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C NWW TUNNEL - LT BS 300 VERTICAL BEAM NR 4 STIFFENER CLIP FOUND CRACKED (COUNT FROM TOP). CLIP REPLACED AS PER SRM 51-10-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT - BS 980 S46L FRAME CRACK. FWD CARGO COMPT BS 980 S46L FRAME CRACKED AREA REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FWD CARGO COMPT- BS 960 41R AREA SHEAR TIE CRACK. SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 40.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 95,929 hrs · 24,524 cycles

INSPECTION TYPE:C FX- LT STA 780 - STA 800 STR 47 STRINGER FOUND WITH CORROSION CRACKED. STR 47L REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: KEELBEAM — CORRODED (FUSELAGE)

INSPECTION TYPE:PFLT KEEL BEAM CORROSION. REPAIRED IAW EO B747-5310-16631.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:PFLT SEVERAL EMERGENCY BACKGROUND LIGHTS ABOVE CENTER INSTRUMENT PANEL INOP. RELAMPED SEVERAL EMERGENCY BACKGROUND LIGHTS ABOVE INSTRUMENT PANEL IAW GMM 3-6-9. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY LIGHTS ABOVE STAIRS INOP. REPLACED BATTERY PACK, EMERGENCY LIGHTS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:IN UPPER DECK EMERGENCY LIGHT OVER STAIRWAY INOP. RELAMPED, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT L1854 INOP. CLEANED CONTACT AND RELAMPED. OPS CHECK OK.

Part: CONTROLLER — FAILED (COCKPIT)

INSPECTION TYPE:N/A, ATB-DURING CLIMB, UNABLE TO CONTROL PRESSURIZATION. FIRST IND- AUTO FAIL LT ILLUM, RAN CK LIST. UNABLE TO GAIN CONTROL, PRESS RELIEF LT ILLUM, DESCENDED TO 16,000 FT. GAINED PARTIAL CONTROL MOMENTARILY, RETURN TO NRT, DIFF PRESS STABILIZED AT APPRX 9.2 PSI UNTIL FURTHER DESCENT CABIN ALT IND 10,100 FT AT ON POINT. NEVER GOT WARNING HORN. CABIN DEPRESS CONDITION CK PERFORMED. NO DAMAGE FOUND. T/S FOUND AUTO PRESS CONTROL FAIL. MANUAL DEPRESS CNTRL WORKS NORMAL. M210343 CHECKED PRESS RELIEF VLVS. REMOVED AND REPLACED CABIN PRESS CONTROLLER IAW MM 21-31-02 ACC TEST ALL TESTS OK. THIS CLEARS MEL M210343 LOG PAGE 676680.

Part: HYDRAULIC LINE — BROKEN (NR 10 BRAKE)

INSPECTION TYPE:N/A LOSS OF NR 1 HYD SYSTEM ON CLIMB OUT LOSS OF ALL FLUID COMPLIED WITH APPROPRIATE UPS PROCEDURES ***SUPPLEMENTAL MRR*** FOUND NR 10 BRAKE TORQUE EQUALIZER ROD BROKEN R&R ROD OF NR 10 AND 11 BRAKE AS PER M/M 32-13-12

Part: ACTUATOR — FAILED (MLG)

INSPECTION TYPE:N/A ATB - RED GEAR & RED DR LIGHT ILLUM ON T/O S/O PANEL PRIMARY & ALT I ND RIGHT WING GEAR DR OPEN. ***SUPPLEMENTAL MRR*** REMOVED AND REPLACED RH WING RETRACT ACTUATOR PER MM 32-21. PERFORME D FUNCTIONAL CHECK GEAR SWING. INDICATIONS CHECK GOOD. PER MM 32-20- 00

Part: DOOR — OPEN (RT WING)

INSPECTION TYPE:C, FOLLOWING GEAR RETRACTION, RED DOOR OPEN LIGHT REMAINED ON. RIGHT WING DOOR CONFIRMED OPEN. AIR TURNBACK TO COLOGNE AFTER DUMPING FUEL.

Part: PRESSURE PANEL — CRACKED (CRACKED)

INSPECTION TYPE:C, CRACK FOUND ON SIDE WALL NLG-WW AT STA 270 LBL 30 WL 190 LT SIDE. CRACK LENGTH 27 CM. CRACK ON LT SIDE NLG WW STA 270 LBL 30 WL 190. REPAIRED ACCORDING TO KLM 747-2000-254 APPR BY FAA FORM 8110-3 IDENTIFCATION (A) UPS AMS-00-00010F. DATED 10/19/00 AS AMENDED BY UPSAMS 00-00032F. EFN NUMBER 747-53-1190.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

INSPECTION TYPE:C, LIGHT CORROSION IN FLOOR PANEL SUPPORT FLANGE. REWORKED WITHIN ALLOWABLE LIMITS.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C, FOUND FRAME BS 2260 RT CRACKED AT OUTER FLANGE BY FRAME SPLICE BETWEEN STR 11 AND 12. REPAIRED FRAME 2260 RT ACCORDING TO KLM 747-2000-274, APPROVED ACCORDING TO EFN 747-53-1191.

Part: FRAME — CORRODED (FUSELAGE FAIRING)

INSPECTION TYPE:C, FAIRING SUPPORT STRUCTURE AT BS 1460 IS CORRODED. REPLACED FAIRING FRAME.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:EO, FOUND FRAME 2920 RT CRACKED AT OUTER FLANGE BY FRAME SPLICE BETWEEN STR 11 AND 12. REPAIRED FRAME 2220 RT ACCORDING TO KLM 767-2000-273. APPROVED ACCORDING TO EFN 747-53-1195.

Part: SEAT TRACK — CORRODED (FUSELAGE)

INSPECTION TYPE:C, SEAT TRACK UPPER DECK RBL 65 HEAVY CORRODED AT SEVERAL LOCATIONS BETWEEN STA 480 AND 560. CORROSION FOUND OUT OF LIMITS OF SRM 53-10-01. REPLACED SEAT TRACK RBL 65 BETWEEN STA 480 AND 560 ACCORDING TO SRM 53-10-05 FIG 6.

Part: SEAT TRACK — CORRODED (FUSELAGE)

INSPECTION TYPE:C, SEAT TRACK UPPER DECK RBL 46 HEAVY CORRODED BETWEEN STA 480 AND 560. CORROSION OUT OF LIMITS OF SRM 53-10-01. REPLACED SEAT TRACK RBL 46 BETWEEN STA 400 AND 500 ACCORDING TO SRM 53-10-05 FIG 6.

Part: FLOORBEAM — CORRODED (FUSELAGE)

INSPECTION TYPE:C, FOUND CORRODED FLOORBEAM UPPER CHORD STA 480 RT AT RT OF STAIR CUTOUT. REPLACED EXISING PART OF UPPER DECK OF FLOORBEAM AT EXISTING SPLICE STA 480 BETWEEN RBL 57 AND 77 ACCORDING TO SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE)

INSPECTION TYPE:C, FOUND CORROSION IN SEAT TRACK FLANGE AT RBL 76 BS 760 - 800. FOUND CORROSION OUT OF LIMITS OF SRM 53-10-01. REPLACED SEAT TRACK RBL 76 BETWEEN STA 730 AND 850.

Part: FRAME — CORRODED (FUSELAGE)

INSPECTION TYPE:C, CHORD CORRODED STA 1170 LBL 9. REPAIRED CHORD ACCORDING TO SRM 51-40-03. REPLACED CHORD FAIRING ATTACH STA 1170 RBL 58/LBL 58.

Part: TRACK — CORRODED (LT FLAP)

INSPECTION TYPE:C, FOUND AFTER BEARING REMOVAL, CORROSION IN THE INNER RACE OF THE MOST INBOARD TRACK OF THE LT INBOARD MID FLAP (TRACK OF THE FORE FLAP). REPLACED MOST INBOARD TRACK ALL, OHM 97-52-35 PAGE 503.

Part: FRAME — CORRODED (FUSELAGE)

INSPECTION TYPE:C, CHORD STA 1045 CORRODED LBL 58 RBL 58. REPLACED CHORD ACCORDING SRM 51-30-02.

Part: WEB — CRACKED (FUSELAGE)

INSPECTION TYPE:C, CRACKS IN WEB. WEB REPLACED ACCORDING TO DRAWING.

Part: FRAME — CRACKED (1740 STR 11)

INSPECTION TYPE:C FRAME 1740 RT CRACKED AT FRAME INNER FLANGE STR 11 AND DENTS IN FRAM E FLANGE BETWEEN STR 15/16. REPAIRED FRAME STA 1740 RH ACC KLM-747-2000-263, APPROVED ACC EFN 74 7-53-1196

Part: FITTING — CORRODED (FUSELAGE)

INSPECTION TYPE:C, CORROSION IN INNER BORE FITTING. REPLACED FITTING ACCORDING TO SB 747-57-2262 REV 4.

Part: DOUBLER — CORRODED (WINDOW BELT)

INSPECTION TYPE:C, INTERNAL FUSELAGE AT BS 882-RT FOUND CORROSION ON FWD SIDE OF WINDOW BELT/SHIN DOUBLER BETWEEN STR 20 AND 22. CORROSION REMOVED ACC SRM 51-10-01, OUT OF LIMITS. ACCORDING TO EFN 747-53-1168, MAX BLEND OUT .055 INCH. SHIN PANEL REPAIRED ACCORDING EFN 747-53-1192.

Part: FORGING — CORRODED (WINDOW BELT)

INSPECTION TYPE:C, INTER FUSELAGE BS 2040 - 2060 RT FOUND CORROSION AROUND WINDOW FORGING. CORROSION REMOVED ACCORDING TO SRM 51-10-01, CORRODED AREA ON FWD SIDE OF WINDOW BELT WITHIN LIMITS, MAX DEPTH .02 INCH AND ON AFT SIDE OUT OF LIMITS MAX DEPTH .043 INCH ACCORDING TO EFN 747-53-1168. SKIN PANEL ON AFT SIDE OF WINDOW BELT REPAIRED ACCORDING TO EFN 747-53-1192.

Part: FORGING — CORRODED (WINDOW BELT)

INSPECTION TYPE:C, INTERNAL FUSELAGE STA 2140 AND 2160 LT. CORROSION BETWEEN WINDOW FORGING/FUSELAGE AT FWD AND AFT SIDE AND AFT LOWER CORNER. CORROSION REMOVED ACCORDING TO SRM 51-10-01, CORRODED AREA ON FWD SIDE OF WINDOW BELT WITHIN LIMITS AND ON AFT SIDE OUT OF LIMITS ACCORDING TO EFN 747-53-1168. SKIN PANEL ON AFT SIDE OF WINDOW BELT REPAIRED ACCORDING TO EFN 747-53-1192.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A, LIGHT SURFACE CORROSION AT LAP JOINT. REWORKED WITH ALLOWABLE LIMITS.

Part: LAP JOINT — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A, LIGHT SURFACE CORROSION AT LAP JOINT. REWORKED WITHIN ALLOWABLE LIMITS.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A, LIGHT SURFACE CORROSION AT LAP JOINTS. REWORKED WITHIN ALLOWABLE LIMITS.

Part: SEAT TRACK — CORRODED (FUSELAGE)

INSPECTION TYPE:C, SEAT TRACK AT UPPER DECK RBL 65, BETWEEN STA 560 AND 600 CORRODED AT SEVERAL LOCATIONS ON UNDERSIDE. REMOVED CORROSION ACCORDING TO SRM 51-10-01, FOUND OUT OF LIMITS OF SRM 53-10-01. REPLACED SEAT TRACK RBL 65 BETWEEN STA 560 AND 600 ACCORDING TO SRM 53-10-05 FIG 6.

Part: FITTING — CRACKED (CABIN) · airframe 91,662 hrs · 23,619 cycles

INSPECTION TYPE:SP, L3 DOOR, STOP FITTING NR 4 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 015U0579 AND SRM 51-30-2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 91,662 hrs · 23,619 cycles

INSPECTION TYPE:SP, INTERCOSTAL BETWEEN LONGERON 21R AND 22R, STATION 1241 TO 1241. REMOVED AND REPLACED T-ANGLE IAW DWG 65B08240 AND SRM 51-30-2.

Part: FITTING — CRACKED (PAX DOOR FRAME) · airframe 91,662 hrs · 23,619 cycles

INSPECTION TYPE:SP, L3 DOOR, STOP FITTING NR 2 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 015U0579, AND SRM 51-30-02.

Part: FITTING — CRACKED (PAX DOOR FRAME) · airframe 91,662 hrs · 23,619 cycles

INSPECTION TYPE:SP, L3 DOOR, STOP FITTING NR 3 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 015U0579, AND SRM 51-30-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,662 hrs · 23,619 cycles

INSPECTION TYPE:SP, LEFT FRAME STATION 1265 AND WEB APPROX 24 INCHES ABOVE FLOORLINE ARE CRACKED. REPAIRED FRAME AND WEB IAW B747-5310-12070-E.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,662 hrs · 23,619 cycles

INSPECTION TYPE:SP, RIGHT FRAME STATION 1265, 24 INCHES ABOVE FLOOR LINE BELOW NR 2 STOP FITTING IS CRACKED. REPAIRED FRAME IAW B747-5310-12070-E.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A REF: M193684, UPPER DECK EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY OPS CKS GOOD M-193684. CLEARED, PLACARD REMOVED.

Part: SIGN — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, CREW SERVICE DOOR EMERGENCY EXIT SIGN UNSERVICEABLE FRAME LATCH BROKEN CAUSING NON-POSITIVE ELECTRIC CONTACT. REPLACED LIGHT ASSY SIGN, OPS CHECK GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN)

INSPECTION TYPE:N/A, FLIGHT DECK EMERGENCY EXIT CEILING LIGHT VERY DIM. REMOVED AND REPLACED CEILING EMERGENCY LIGHT ASSY, OPS CHECKS NORMAL.

Part: LIGHT — BROKEN (CABIN)

INSPECTION TYPE:N/A, CREW SERVICE DOOR EMERGENCY EXIT SIGN FRAME LATCH BROKEN. REPLACED LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A M-193684 UPPER DECK EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECKS GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN)

INSPECTION TYPE:N/A, FLIGHT DECK EMERGENCY EXIT CEILING LIGHT VERY DIM. REPLACED CEILING EMERGENCY LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, UPPER DECK EMERGENCY EXIT LIGHT INOPERATIVE. REFERENCE M192189, RELAMPED AND OPS CHECK GOOD. DEFERRAL CLEARED.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP ON UPPER DECK EVACUATION SIDE DOOR. REMOVED AND REPLACED, OPS CK OK.

Part: FUEL TANK — CONTAMINATED (WING)

INSPECTION TYPE:N/A, NR 4 ENG FAILED AT FL390 M.845 SAT -52 NORMAL SHUTDOWN AND ALL CHECKLISTS COMPLETED. UNABLE TO AIR START DUE TO HIGH N2 AT CRUISE. ENGINE RESTARTED OK AT 13,000 FT WITH GND START PROCEDURE. ALL PARAMETERS SEEMED NORMAL. PERFORMED FLAME-OUT INSPECTION, FOUND 4M FUEL TANK WITH HEAVY WATER CONTAMINATION. DEFUELED TANKS 3M & 4M. REMOVED AND REPLACED NR 4 ENG FUEL PUMP FILTER. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, AFT EMERGENCY LIGHT L1854 AT DOOR L1 INOP. RELAMPED AFT LIGHT, OPS CHECKS GOOD.

Part: SAFETY VALVE — FAILED (MLG DOOR)

RIGHT BODY GEAR DOOR OPENED DURING DESCENT, 3000 FT, 220KTS. BOTH PRIMARY AND ALTERNATE SHOWED DOOR OPENED. THE DOOR DID CLOSE AFTER LANDING GEAR WAS EXTENDED. FOUND BODY RT BODY GEAR DOOR SAFETY VALVE BYPASSING TOG 36550. REMOVED AND REPLACED BODY GEAR DOOR SAFETY VALVE IAW B747 MM 32-33 -29, (NO HELP) NEEDS RIGG CHECK, PERFORMED CHECK PER MM 32-53-00, JACKED ACFT. GROUND OPS CHECK GOOD, OK FOR SERVICE.

Part: SKIN — DENT (FWD OF CARGO DOO)

INSPECTION TYPE:IN, DENT 3 FOOT FWD OF AFT CARGO DOOR. REMOVED DAMAGE IAW SRM 53-30-03. INSTALLED DOUBLER IAW SRM 53-30-03, PAINTED TO MATCH A/C COLOR SCHEME.

Part: MODULE — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS UNARMED ANNUNCIATOR ILLUMINATED WHEN SWITCH PLACED TO ARMED POSITION. REPLACED EMERGENCY LIGHT CONTROL PANEL PER M/M 33-51-09, OPS CKS OK.

Part: SKIN — CRACKED (CARGO DOORWAY)

AFT UPPER CORNER OF BULK CARGO DOOR FUSELAGE SKIN CRACKED. REPAIRING PER EO BH747-5330-10189.

Part: SEAL — FAILED (NR 3 ENGINE)

ON TAKEOFF CREW NOTICE SMOKE IN COCKPIT, TURN ON A/C PACKS SMOKE WENT AWAY RETURN TO KSDF. FOUND NR 3 ENGINE HAD BAD OIL SEAL REMOVED AND REPLACED ENGINE.

Part: ENGINE — DAMAGED (NR 2)

NR 2 ENGINE WOULD NOT MAKE TAKEOFF POWER. ABORTED TAKEOFF. FOUND LPT DAMAGED. REPLACED NR 2 ENGINE.

Part: BULB — FAILED (CABIN)

INSPECTION TYPE-N/A, REF DMI NR M-142426 FWD EMERGENCY EXIT LIGHT ON L-1 DOOR SILL INOP. FOUND SHORTED LIGHT BULB IN L1853. REPLACED BULB AND F1 FUSE IN M415, TEST GOOD REF WDM 33-51-01.

Part: BULB — FAILED (CABIN)

INSPECTION TYPE-N/A, MAIN CABIN DOOR EMERGENCY EXIT LTS INOP. RELAMPED DOOR EMER EXIT LIGHTS, OPS CK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-DLY, STAIR WELL EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY ASSY, OPS CHECKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, RT UPPER DECK EMERGENCY EXIT DOOR LIGHT UNSERVICEABLE. REMOVED AND REPLACED BATT PACK RT SIDE, F/C GOOD.

Part: FITTING — CRACKED (BS 1000)

INSPECTION TYPE-C, CENTER WING TANK FOUND FITTING CRACKED AT LOWER SPAR CHORD, LBL 78. REPLACED FITTING AT NAC STA 1000, IN CENTERWING AT LOWER SPAR CHORD LBL 78 ACC SRM 51-30-02.

Part: SKIN — CORRODED (RT WING)

INSPECTION TYPE-C, OLES 1545, CORRODED ON L/E UPPER CHORD SHOWS BULGE AND PULLED RIVET ON TOP OF WING. REMOVED FASTENERS FROM WING SKIN ACC SRM 51-30-02. REMOVED CORROSION FROM WING SKIN ACC SRM 51-10-01. SKIN OUT OF LIMITS ACC SRM 57-3 0-01 FIG 1. REPAIRED WING ACC KLM DFX 97-238. REPAIRED APPROVED PER UPS EFN 747-57-0392.

Part: SKIN — CORRODED (BS 1120)

INSPECTION TYPE-C, CENTER SECTION FUEL TANK CORROSION ON TOP SKIN PANEL AT BS 1120 RBL 120. REPAIRED CENTER WING UPPER PANEL AT BS 1120 STRINGER 17 RBL 120 ACC EFN 747-57-0391 KLM DFX 97-227. PERFORMED HFEC INSP ON UPS NRC 766739.

Part: FLOORBEAM — CORRODED (BS 400)

INSPECTION TYPE-C, MAIN CABIN A-ZONE BS 400, LBL 40 THRU RBL 40, WL 199.8 FLOORBEAM HEAVILY CORRODED AT UPPER AND LOWER SIDE. FLOORBEAM AT BS 400 LBL 40 THRU RBL 40 OUT OF LIMITS ACC SRM 53-10-01. REPAIRED FLOORBEAM ACC EFN 747-53-0844 KLM DFX 97-231.

Part: SKIN — CORRODED (BS 1140)

INSPECTION TYPE-C, CENTER SECTION FUEL TANK FOUND CORROSION ON TOP OF SKIN PANEL AT BS 1140 LBL 105. REPAIRED CENTER WING UPPER SKIN PANEL AT BS 1140 LBL 105 ACC EFN 7 47-57-0390 (KLM DFX 97-222). PERFORMED HFEC INSP ON UPS NRC 766740.

Part: WEB — CORRODED (FWD CARGO DOOR)

INSPECTION TYPE:C, FWD CARGO DOOR, FOUND ON LOWER CLOSURE WEB (CLOSE OUT BEAM) TWO CORROSION SPOTS, AFT SIDE BS 653 AND BS 662. REMOVED CORROSION ACC SRM 51-10-01. REMAINING THICKNESS ON BOTH SPOTS IS 0.015 INCH, FOUND NO LIMITS IN SRM. CONTACTED BOEING FOR ACTION. REPAIRED CLOSE OUT BEAM ACC. KLM D FX.97-224 AND UPS EFN 747-52-0064.

Part: WEB — CORRODED (BS 1394)

INSPECTION TYPE-C, THE LT BLG WHEEL WELL FOUND CORROSION AT THE PRESSURE DECK STA 1394 LBL 120. ACCOMPLISHED UPS EO B747-5320-2833-A APPROX 8.2.

Part: FRAME — CRACKED (BS 2701)

INSPECTION TYPE-C, FOUND CRACK AT FRAME AT BS 2701 ON WL 310 LT. REPAIRED FRAME AT BS 2701 ON WL 310 LT ACC SRM 51-40-03 FIG 1.

Part: FLOORBEAM — CORROSION (BS 460)

INSPECTION TYPE-C, MAIN DECK FLOOR STRUCTURE: FOUND CORROSION AT FLOORBEAM WEB AT BS 460 LBL 22 LOWER SIDE. REMOVED CORROSION AT MAIN DECK FLOOR STRUCTURE AT FLOORBEAM WEB BS 460 LBL 22 ACC SRM 51-10-01. OUT OFF LIMITS ACC SRM 53-10-01. REPAIRED ACC SRM 53-10-07 FIG 11.

Part: RETRACT MECH — MALFUNCTIONED (MLG DOORS)

INSPECTION TYPE-N/A, LANDING GEAR DOOR LIGHT CAME ON BELOW 5,000 FT ON CLIMBOUT. DOOR ACTUALLY CAME OPEN. VIBRATION, GEAR SEEMED TO BE SLOW EXTENDING. INSPECTED ALL GEAR DOORS, GEAR ACTUATORS, DOOR ACTUATORS, ASSOCIATED PLUMBING, AND DOOR SWITCHES. NO DEFECTS OR LEAKAGE FOUND. OPERATED ALL GEAR DOORS, ALL OPENED AND CLOSED AT NORMAL SPEED.

Part: SAFETY VALVE — DEFECTIVE (RT MLG DOOR)

AFTER TAKEOFF, RED DOOR OPEN LIGHT FRONT PANEL ILLUMINATED WITH GEAR HANDLE OFF. ASSOCIATED PRIMARY AND ALTERNATE RT BODY DOOR OPEN LIGHTS ILLUMINATED, SECOND OFFICER'S PANEL. REMOVED AND REPLACED BODY GEAR DOOR SAFETY VALVE. OPS CHECK AND LEAK CHECK GOOD PER MM 32-33-09. P/N OFF 2670112, S/N OFF 879. P/N ON 2670112. S/N ON 4563.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE, UPPER DECK DOOR EMERGENCY EXIT SIGN HAS DEAD BATTERY, FAILED DURING ROUTINE CHECK. REPLACED BATTERY.

Part: FRAME — DAMAGED (BS 1640)

INSPECTION TYPE: C. AFT CARGO COMP: FOUND DURING FRAME REPAIR BS 1640 LT STR 31/32 INNERFLANGE REINFORCEMENT CHORD DAMAGED AT SAME LOCATION. REPAIRED CHORD IAW KLM DFX96-129 ISSUE 5, APPROVED PER UPS EFN 747- 53-0766 IN COMBINATION WITH NCR 706450.

Part: FRAME — CRACKED (BS 1860)

INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACK ON FRAME STA 1860 LT ON UPPER FLANGE STR'S 40 AND 41. REPAIRED FRAME IAW KLM DFX96-122 ISSUE 2, APPRROVED PER EFN 747-53- 0769.

Part: STRINGER — CRACKED (BS 2160)

INSPECTION TYPE: C. BULK CARGO COMP: AT STA 2160, STR 46 LT CRACKED AT STRINGER CLIP. REPAIRED STRINGER IAW SRM 53-10-03, FIG 1.

Part: FRAME — CRACKED (BS 2160)

INSPECTION TYPE: C. BULK CARGO COMP: STA 2160 LT FRAME STRINGER CUTOUTS CRACKED AT STR 42 AND STR 44. REPAIRED FRAME IAW SRM 53-10-04, FIG 11.

Part: FRAME — CRACKED (BS 2040)

INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACK IN FRAME WEB AT FRAME SPLICE, BS 2040, STR 34 RT. REPAIRED FRAME IAW SRM 51-40-03, FIG 1.

Part: FRAME — CRACKED (BS 1640)

INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACK IN FRAME AT STA 1640 LT ON UPPER FLANGE BETWEEN STR 31 AND 32. REPAIRED FRAME IAW KLM DFX96-129 ISSUE 5, APPROVED PER UPS EFN 747-53-0766 IN COMBINATION WITH NCR 70660.

Part: FLANGE — CRACKED (BS 1580)

INSPECTION TYPE: C. AFT CARGO COMP: STA 1580 RT FLANGE CRACKED JUST AFT OF FLOOR SUPPORT. REPAIRED FRAME IAW SRM 51-40-03, FIG 1.

Part: STRINGER — ELONGATED HOLES (BS 1000)

INSPECTION TYPE: C. FORWARD CARGO COMP: FOUND DURING LOWER CHORD REPLACEMENT AT BS 1000, ELONGATED HOLES IN STR 46 RT. REPAIRED IAW TELEX UPS-AMS-95-0144RE / ATA 5321/20.

Part: BRACKET — CRACKED (BS 1980)

INSPECTION TYPE: C. FORWARD CARGO COMP: FOUND CARGO FLOOR STIFFENER ATTACHMENT BRACKET CRACKED AT BS 1980, RBL 54. REPLACED BRACKET IAW SRM 51-30-02.

Part: FRAME — CRACKED (BS 500)

INSPECTION TYPE: C. FORWARD CARGO COMP: FOUND TWO CRACKS IN TOP FLANGE FROM FRAME STA 500 LT ABOVE STR 38. REPAIRED FRAME IAW SRM 53-10-04, FIG 57.

Part: FRAME — CRACKED (BS 1520)

INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACKS ON FRAME STA 1520 LT AT STR 35 CUTOUT AND SHEAR TIE BETWEEN STR 34 AND 35. REPAIRED SHEAR TIE IAW SRM 53-10-04, FIG 3. REPAIRED UPPER FLANGE FRAME IAW SRM 51-40-03, FIG 1.

Part: STRINGER — CRACKED (BS 1635-1640)

INSPECTION TYPE: C. FOUND CRACK IN STRINGER 31 LT BSTA 1635 TO 1640. STRINGER 31 LT REPLACED BETWEEN STA 1635 - 1650. REPAIR CARRIED OUT IAW SRM 53-10-03, FIG 1.

Part: STRINGER — CRACKED (BS 2180)

INSPECTION TYPE: C. AFT CARGO COMP: AT STA 2180, STR 46 RT, STRINGER END CRACKED JUST IN FRONT OF SPLICE. STA 2180, STR 46, REPAIRED IAW SRM 53-10-03.

Part: STRINGER — CRACKED (BS 2140)

INSPECTION TYPE: C. BULK CARGO COMP: STA 2140 LT, FRAME STRINGER CUTOUT CRACKED AT STR 45. FRAME STR CUTOUT REPAIRED IAW SRM 53-10-04, FIG 41.

Part: SHEAR TIE — CRACKED (BS 2000)

INSPECTION TYPE: C. BULK CARGO COMP: BS 2000 LT SHEAR TIE CRACKED AT S-45. REPAIRED SHEAR TIE IAW SRM 53-10-04, FIG 3.

Part: STRINGER — CORRODED (BS 2060)

INSPECTION TYPE: C. BULK CARGO COMP: DURING ACCOMPLISHMENT OF FRAME REPAIR AT BS 2060, S-29 LT, FOUND CORROSION IN STRINGER AT FRAME/STRINGER-CLIP ATTACHMENT. REMOVED DAMAGED SECTION OF STRINGER FROM BS 2050 TO BS 2070 AND REPAIRED STRINGER IAW SRM 53-20-03, FIG 1.

Part: FRAME — CRACKED (BS 1780)

INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACKS ON FRAME BS 1780 LT ON UPPER FLANGE AT S-37 AND S-40. REMOVED DAMAGED SECTIONS FROM FRAME INNERFLANGE AND REPAIRED FRAME FLANGES AT S-37 AND S-40 IAW SRM 51-40-03, FIG 1.

Part: FRAME — DENTED (BS 1560)

INSPECTION TYPE: C. FRAME STA 1560. FOUND DENT IN WEB AT LBL 57. DENT OUT OF LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 1620)

INSPECTION TYPE: C. AFT CARGO COMP. FOUND CRACK IN FRAME AT BS 1620 LT ON UPPER FLANGE S-34. REMOVED DAMAGED SECTION FROM FRAME INNERFLANGE AND REPAIRED FRAME INNERFLANGE IAW SRM 51-40-03, FIG 1.

Part: INTERCOSTAL — CORRODED (BS 1850)

INSPECTION TYPE: C. AFT CARGO COMP: FOUND UNDER TWO ANCHOR NUTS, CORROSION, (ACCESS PANEL CUTOUT, TORQUE BOX) ON INTERCOSTAL AT BS 1850, RBL 7. REMOVED CORROSION ACC. SRM 51-10-01. DAMAGE OUT OF LIMITS IAW SRM 53-10-01. REPAIRED INTERCOSTAL IAW SRM 51-60-03. INSTALLED NEW ANCHOR NUTS IAW SRM 51-30-02.

Part: FRAME — CRACKED (BS 600)

INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACK ON FRAME BS 1600 LT ON UPPERFLANGE S-35. REMOVED DAMAGED SECTION FROM FRAME INNERFLANGE AND REPAIRED FRAME INNERFLANGE IAW SRM 51-40-03, FIG 1.

Part: BULKHEAD — CRACKED (BS 140)

INSPECTION TYPE: C. SEVERAL CRACKS AT BS 140 FORWARD PRESSURE BULKHEAD, CRACKS AROUND FASTENERS AT INNER RING. WEB CRACKS AT INNER RING CHORD REPAIRED IAW EO B747-5310-3279, APPENDIX B, FIG 3.

Part: SHEAR TIE — CRACKED (BS 2180)

INSPECTION TYPE: C. AREA AFT OF BULK CARGO COMP: FOUND CRACK IN SHEAR TIE AT STRINGER CUTOUT BS 2180, BETWEEN S-44/42 RT. REPAIRED SHEAR TIE AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 4.

Part: FRAME — CRACKED (BS 1500)

INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACK IN FRAME WEB NEAR INSULATION HOLE AT BS 1500, S-42 RT. STOP DRILLED CRACK AND REPAIRED FRAME WEB IAW KLM-DFX-96-127. REPAIRED APPROVED PER EFN-53-0767.

Part: FRAME — CRACKED (BS 2180)

INSPECTION TYPE: C. AREA AFT OF BULK CARGO COMP: FOUND CRACK IN FRAME WEB BSTA 2180, RBL 32 UNDER FLOOR SUPPORT. FRAME WEB REPAIRED IAW SRM 51-40-02, FIG 1.

Part: FRAME — CRACKED (BS 1660)

INSPECTION TYPE: C. AFT CARGO COMP: BS 1660 RT, TOP FLANGE CRACKED JUST ABOVE AND JUST BELOW FLOOR SUPPORT POST. REMOVED DAMAGED SECTIONS FROM FRAME INNERFLANGE AND REPAIRED FRAME INNERFLANGES IAW SRM 51-40-03, FIG 1.

Part: FRAME — CRACKED (BS 1540)

INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACKS ON FRAME BS 1540 LT AT UPPER FLANGE AT S29 AND S32. REMOVED DAMAGED SECTIONS FROM FRAME INNERFLANGES AT S29 AND S32, AND REPAIRED FRAME INNERFLANGES IAW SRM 51-40-03, FIG 1.

Part: FRAME — CRACKED (BS 1500)

INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACKS IN FRAME BS 1500 LT AT S35 CUTOUT AND ON UPPERFLANGE OF FRAME AT S-37. REPAIRED FRAME AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 4. REPAIRED FRAME UPPERFLANGE IAW SRM 51-40-03, FIG 1.

Part: FRAME — CRACKED (BS 1560)

INSPECTION TYPE: C. AFT CARGO COMP. FOUND CRACK IN FRAME BS 1560 LT AT S-35 LT CUTOUT. REPAIRED FRAME WEB AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 4.

Part: REPAIR DOUBLER — INCORRECT REPAIR (NR 3 PYLON)

INSPECTION TYPE: C. PYLON NR 3, FOUND REPAIR DOUBLER ON NAC STA 180 LT NOT INSTALLED IAW SRM (EDGE MARGINS ON MID SPAR TOO SMALL). FOUND DURING REMOVAL OF DOUBLER THAT DOUBLER WAS MADE FROM SOFT STEEL MAT: REWORK MID SPAR STIFFENER AND REPLACED GUSSET APPROVED BY TLX UPS-AMS 96-0137RE AND KLM DFX 96 117, ISSUE NR 2. INSTALLED NEW DOUBLER IAW S.B. 747 54-2034R4, FIGURES 3 AND 6.

Part: FRAME — CRACKED (BS 2220)

INSPECTION TYPE: C. FOUND CRACK IN FRAME LOWER FLANGE AT SKIN ATTACHMENT BS 2220. STR 42 LT, JUST BEHIND LEFT OUTFLOW VALVE. FRAME LOWER FLANGE REPAIRED IAW SRM 51-40-03, FIG. 1.

Part: BULKHEAD — CRACKED (BS 1000)

INSPECTION TYPE: C. FORWARD CARGO COMP: FOUND CRACKS IN BS 1000 BULKHEAD LOWER CHORD, BETWEEN S-47/46 LT AND RT. REPLACED LOWER CHORD PARTLY ACCORDING TO SB 747-53-2316R1.

Part: FRAME — CRACKED (BS 2120)

INSPECTION TYPE: C. BULK CARGO COMP: FOUND CRACK IN FRAME WEB AT STRINGER CUTOUT AT BS 2120, S-29 LT. REPAIRED FRAME WEB AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 39.

Part: FRAME — CRACKED (BS 2100)

INSPECTION TYPE: C. BULK CARGO COMP: FOUND CRACK IN FRAMEWEB AT STRINGER CUTOUT AT BS 2100, S-29 RT. REPAIRED FRAME WEB AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 39.

Part: FRAME — CRACKED (BS 2060)

INSPECTION TYPE: C. BULK CARGO COMP: FOUND CRACK IN FRAME WEB AT STRINGER CUTOUT AT BS 2060, S-29 LT. REPAIRED FRAME WEB AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 39.

Part: FRAME — CRACKED (BS 2040)

INSPECTION TYPE: C. FOUND CRACK IN FRAME WEB AT STRINGER CUTOUT AT BS 2040, S29 LT. FRAME WEB REPAIRED IAW SRM 53-10-04, FIG 39.

Part: FRAME — CRACKED (BS 2020)

INSPECTION TYPE: C. BULK CARGO COMP: FOUND CRACK IN FRAME WEB AT STRINGER CUTOUT AT BS 2020, S-29 RT. REPAIRED FRAME WEB AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 39.

Part: ENGINE — FAILED (NR 2)

CREW REPORTED EN ROUTE TO YQX, NR 2 ENGINE FAILED AT 16:21Z. N2 SEIZED, EGT PEAKED AT 935 DEGREES. CREW ACCOMPLISHED ALL APPLICABLE CHECKLIST PROCEDURES PER AOM. PERFORMED UNEVENTFUL LANDING AT GANDER, NEWFOUNDLAND, 17:47Z.

Part: TE SKIN — CRACKED (LT HORIZ STAB)

WHILE ON GROUND, MAINTENANCE FOUND 2 LT HORIZONTAL STAB T/EDGE CRACKED.

Part: EEL — INOP (CABIN)

WHILE ON GROUND IN ONTARIO, MAINTENANCE FOUND L-1 ENTRY DOOR FWD EMERGENCY LIGHT INOP. REPLACED A ZONE EMERGENCY LIGHT ASSY, OPS CHECK GOOD.

Part: FUEL FLOW MODULE — MALFUNCTIONED (NR 2)

WHILE EN ROUTE TO EWR FROM CGN AT FL 350 .84M APPROXIMATELY 5 HOURS INTO FLIGHT, THE NR 2 FUEL FLOW CIRCUIT BREAKER POPPED ACCOMPANIED BY AN ACRID BURNING SMELL FROM THE P6 PANEL. CREW ELECTED NOT TO RESET. FUEL FLOW MODULE REMOVED AND REPLACED IAW M/M 73-31-02.

Part: WATER FILL PANEL — CORRODED (FS 980)

WHILE IN AMSTERDAM FOR C CHECK, MAINTENANCE FOUND CORROSION AT THE WATER FILL PANEL, STA 980, RT LOWER SIDE, FUSELAGE. INSTALLED REPAIR PER SRM 51-20-01, 53-10-01, 51-10-01.

Part: FLOORBEAM — CORROSION (BS 76-90)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION FLOORBEAM, STA 866, BETWEEN LBL 76 TO 90, UNDER SIDE OF UPPER CHORD. INSTALLED REPAIR PER UPS EO 51-40-04.

Part: DOUBLER — CORRODED (RT MLG WW)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION AT BS 1241, CANTED PRESSURE DECK WEB AND DOUBLER, RT WHEEL WELL, RBL 20, BEHIND SPOILER MIXER. INSTALLED REPAIR PER UPS EO FILE NR B747-53-0713.

Part: FLOOR BEAM — CORRODED (FS 640)

WHILE IN AMSTERDAM FOR C CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM STA 640, RBL 99. INSTALLED REPAIR PER UPS EO FILE NR B747-53-0712.

Part: FLOOR BEAM — CORRODED (FS 980)

WHILE IN AMSTERDAM FOR C CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM UPPER CHORD AT BS 980, LBL80 AND 90. INSTALLED REPAIR PER SRM 51-40-04.

Part: FLOOR BEAM — CORRODED (FS 640)

WHILE IN AMSTERDAM FOR C CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM, BS 640, RBL 99. INSTALLED REPAIR PER UPS EO FILE NR B747-53-0712.

Part: DOUBLER — CORRODED (FS 1180-1200)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON WINDOW DOUBLER, STA 1180 TO 1200, STRINGER 14R. INSTALLED REPAIR PER UPS EO FILE NR B747-53-0715.

Part: SEAT TRACK — CORROSION (BS 810)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK, BS 810, LBL 76. REPLACED SEAT TRACK PER SRM 53-10-05.

Part: WEB — CRACKED (BS 1240)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION AND CRACK ON WEB AT BS 1240, LBL 105. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-02.