N677UP

Part: PANEL — DELAMINATED (RT WING)

RT WING UPPER INBD FIXED TRAILING EDGE PANEL DELAMINATED. REMOVED DISBONDED, DAMAGED SKIN FROM LEADING EDGE ACROSS PANEL TO LWR EDGE IAW 51-40-20. FABRICATED SKIN FILLER. REPLACED PANEL WITH SERVICEABLE PANEL.

Part: TUBE — CHAFED (OIL SYSTEM)

INSPECTION TYPE:N/A IFSD - CREW INFORMED FLIGHT CONTROL THAT THE OIL PRESSURE ON NR 1 ENG WAS RUNNING IN THE YELLOW BAND AND OCCASSIONALLY WAS HITTING THE RED LINE. IT WAS ALSO INDICATED THE OIL PRESSURE LIGHT WAS FLICKERING. CREW DELARED EMERGENCY, SHUT DOWN NR 1 ENGINE AND CONTINUED TO CTS. FOUND CHAFED OIL PRESS TUBE WITH PIN HOLE. C/W EO JT9D-7930-27881A. C/OUT ENG WINDMILLING INSP PER MM 72-00-01 FIG 3, SATIS. REMOVED AND REPLACED ENG MAIN OIL STRAINER AND RAN ENG PER MM 71-00-00. FOUND SATIS. NO LEAK NOTED. OIL ADDED 18 QTS. A/C OK FOR SERVICE.

Part: INTAKE — CLOGGED (INSTRUMENT PANEL)

LOUD HUMMING SOUND HEARD 5 TIMES FROM FORWARD INSTRUMENT PANEL, FIRST TWO TIMES WITH STRONG ODOR OF HOT ELECTRONICS. CLEARED CLOGGED AIR INTAKES ON NR 1 AND NR 2 INS CDU'S. INSPECTED FORWARD INSTRUMENTAL PANEL AREA. PERFORMED EQUIPMENT COOLING TEST. ALL CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY LIGHT INOP L1 DOOR FWD. RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD 747 MM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT INOP MCD CEILING FWD OF CREW ENTRY STAIRS. OPERATION CHECKS NORMAL 747 MM 33-51-00.

Part: PANEL — DELAMINATED (RT WING)

RT WING LEADING EDGE, TOP FILLER PANELS OF NR 3 ENGINE 4 INCH X 10 INCH DELAMINATED. DISCOVERED ADDITIONAL DELAM OF INNER SKIN OPPOSITE EXTERIOR SOFT SPOT. REMOVED PANEL FROM AIRCRAFT XZ 1227688, TRIMMED AND PICKED UP HOLES IN NEW PANEL IAW INSTALLED NEW PANEL, USED WAS STEEL SCREWS REF SRM 51-30-03.

Part: STIFFENER — CRACKED (RWS 405) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RIGHT WING REAR SPAR WEB WS 405 STIFFENER THE SECOND MOST UPPER HOLE FOUND CRACK RUNNING UP APPROX 1 INCH. RIGHT WING REAR SPAR WEB WS 405 STIFFENER UPPER PORTION REPAIRED AS PER SRM 51-40-04 FIG 3.

Part: SKIN — CORRODED (RWS 402) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RIGHT WING WS 402 CORROSION REVEAL AT MATTING SURFACE BETWEEN CHORD AND EXTENSION SKIN (DEFECT FOUND AFTER EXTENSION SKIN LIFT UP) FOR CHORD REPAIR. CORROSION BLEND OUT 0.124" X 2" X 2" & 0.137" X 1.5" X 6" EXCEED SRM 57-30-01 FIG 1 LIMITS, RIGHT WING WS 402 & WS 424 UPPER SKIN BLEND OUT AREA REPAIRED AS PER HX RS R57-22-35684 ITEM C AND UPS EO B747-5710-25565.

Part: SPAR — CRACKED (RT WING) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RIGHT WING REAR SPAR UPPER CHORD HORIZONTAL FLANGE FOUND 1EA FASTENER CRACKED AT WS 410 APPROX 0.030" RUNNING AFT. RIGHT WING REAR SPAR UPPER CHORD HORIZONTAL FLANGE AT WS 410 APPROX AREA CRACKED HOLE A REPAIRED AS PER HX RS R57-22-35684 ITEM D AND UPS EO B747-5710-25565.

Part: STRINGER — CRACKED (BS 744-745 S39R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C FWD CARGO COMPT RT STRINGER 39R SUSPECT CRACKED AT STA 744 TO STA 745, CRACK LENGTH 1". FWD CARGO COMPT BS 740-770 STR 39R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STIFFENER — CRACKED (L3 DOOR) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D L3 DOOR FWD LWR CORNER REVEAL ATTACH STIFFENER CRACK, CRACK LENGTH 3/8". L3 DOOR FWD LOWER CORNER REVEAL ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG9 AND 51-30-02.

Part: SEAT TRACK — CORRODED (BS 2040-2150) · airframe 97,105 hrs · 24,042 cycles

BS 2040 TO BS 2150 RBL 89 SEAT TRACK BOTTOM FLANGE CORRODED. CORROSION BLEND OUT 0.035" BY 1.5" BY 2" EXCEED SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 P9 JUST AT M/D RBL89 BETWEEN BS2040 AND 2150.

Part: FRAME — CRACKED (BS 2231 S23-25L) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C LEFT BS 2231 FRAME FOUND CRACKED AT REVEAL AT 3EA LOCATIONS BETWEEN S23L & 25L. CRACK LENGTH .125" & .375" & .625". LEFT BS 2231 FRAME BETWEEN S23L - S25L REVEAL REPAIRED AS PER HX RS R53-00-35672 WORKING DETAIL REF NRC 51422. CONTINUED INSPECTION IS REQUIRED AS PER HX RS R53-00-35672 AND UPS EO B747-5310-25584.

Part: WEB — CORRODED (L5 DOOR) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE-C M/D L5 DOOR LOWER HINGE LOWER WEB FOUND CORRODED. CORROSION BLEND OUT 0.063 INCH X 1INCH X 1.5 INCHES EXCEED SRM LIMIT. HINGE WEB REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02.

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE-C M/D NR 5R MED FWD LOWER INTERIOR CORNER FOUND VERTICAL BEAM PREVIOUSLY CRACKED. CRACK LENGTH 1.2500 INCH, M/D NR 5R MED FWD LOWER VERTICAL BEAM REPAIRED IAW SRM 52-10-02 FIG 10.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE-C M/D L1 DOOR LOWER HINGE CUTOUT FRAME FOUND CRACKED. CRACK LENGTH .3750 INCH, M/D L1 DOOR LOWER HINGE CUTOUT FRAME REPAIRED IAW SRM 52-10-02 FIG 12.

Part: SKIN — CRACKED (L3 DOOR) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D L3 DOOR EXTERIOR SKIN FOUND CRACKED AT CTR LOWER PORTION. CRACK LENGTH .875 INCH. M/D L3 DOOR EXTERIOR SKIN CTR LOWER PORTION REPAIRED WITH ZERO TIMED AT CRITICAL ROW FASTENER HOLES AS PER SRM 52-10-02 FIG 9 SUBSEQUENT INSPECTION REQUIRED AS PER SRM 52-10-02 FIG 9 SHEET 4 TABLE 3.

Part: FRAME — CRACKED (BS 2231 S24-25R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RIGHT BS 2231 FRAME FOUND CRACKED AT REVEAL AT 2EA LOCATIONS BETWEEN STR 24R & 25R. CRACK LENGTH .1875" & .5". M/D BS 2231 FRAME ATTACHED REVEAL REPAIRED AS PER HX RS R53-60-35673 REF NRC 51427 FOR WORKING DETAIL. CONTINUED INSPECTION IS REQUIRED AS PER HX RS R53-60-35673 AND UPE EO B747-5310-25592.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE-C M/D L3 UPPER HINGE EXT SKIN FOUND CRACKED. CRACK LENGTH .3750 INCH. M/D L3 DOOR UPPER HINGE EXT SKIN REPAIR IAW SRM 52-10-02 FIG 11 AND SB 747-52-2144.

Part: FRAME — CRACKED (BS 2231 S24-25R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RIGHT BS 2231 FRAME FOUND CRACKED AT CHORD AT 2EA FASTENER LOCATION STR 24R & 25R. CRACK LENGTH 0.040" & 0.060". M/D BS 2231 FRAME CHORD REPAIRED AS PER HX RS R53-60-35673 REFER NRC 51427 FOR WORKING DETAIL. CONTINUED INSPECTION IS REQUIRED AS PER HX RS R53-60-35673 AND UPS EO B747-5310-25592.

Part: BEAM — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

NR 4R MED FWD LWR INTERIOR CORNER FOUND VERTICAL BEAM CRACK BEYOND STOP HOLE AND HORIZONTAL BEAM CRACKED, CRACK LENGTH 7/8" AND 1". NR 4R MED FWD LOWER INTERIOR VERT AND HORIZ BEAM REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: PANEL — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

L1 DOOR FWD CUTOUT MID REVEAL PANEL FOUND CRACKED, CRACK LENGTH 3/8". L1 DOOR FWD CUTOUT MID REVEAL PANEL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS1920 RBL33 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.022" BY 1/2" BY 1" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 33 JUST AT M/D RBL33 BETWEEN BS 1810 AND BS 1950 (REFER NRC NO.51784 FOR DETAIL).

Part: FLOORBEAM — CORRODED (BS 2040) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 2040 RBL 60 FLOORBEAM FOUND CORROSION. CORROSION BLEND OUT 0.075" X 1/2" X 1" EXCEED SRM LIMIT. M/D BS 2040 RBL 60 FLOORBEAM REPAIRED AS PER RS R53-61-35674 AND UPS ENGINEERING FILE NUMBER 747-53-20364.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE-C M/D BS 2260 RBL13-20 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.023 INCH X 2 INCHES X 2 INCHES EXCEED SRM LIMIT. M/D BS 2260 LBL 8 TO RBL 66 FLOORBEAM REPAIRED IAW SRM 51-40-04 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1920 RBL74 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.090" BY 2" BY 2" EXCEED SRM LIMT. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 3 JUST AT M/D BS 1920 BETWEEN RBL33 TO RT MOST O/B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1920 - 1960 RBL 75 SEAT TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.030" BY 1" BY 1 1/4" EXCEED SRM LIMIT. BS 1870- 2010 RBL 75 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D SEAT TRACK FLANGE FOUND CORRODED BOTH I/B AND O/B. CORROSION BLEND OUT 0.043" BY 3/4" BY 1.5" EXCEED SRM LIMIT. M/D BS1890-2030 LBL 33 SEAT TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: WEB — CORRODED (BS 2160-2180) · airframe 97,105 hrs · 24,042 cycles

BS 2160-2180 LBL 97-100 FLOOR WEB FOUND CORROSION. CORROSION BLEND OUT 0.050" BY 5/8" BY 1" EXCEED SRM LIMIT. BS 2160-2180 LBL97-100 FLOOR WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS1880-1910 RBL11 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.021" BY 1/2" BY 10" EXCEED SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 P9 JUST AT M/D RBL11 BETWEEN BS 1870 AND 1910.

Part: CARGO TRACK — CORRODED (BS 1680) · airframe 97,105 hrs · 24,042 cycles

BS 1680 RBL86 TIE DOWN FTG FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.033" BY 1/2" BY 1/2" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 2060-2080 RBL75 SEAT TRACK O/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.030" BY 1/2" BY 1.5". SEAT TRACK REPLACED AS PER SRM 53-10-05 FIG 1A JUST AT M/D, RBL75 BETWEEN STA 2010 AND 2110.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C AFT CARGO DOOR COMPT CUTOUT FWD HINGE MOST FWD LWR FASTENER HOLE FOUND CRACK AT SKIN RUNNING UP. CRACKED SKIN TRIMMED OFF. FILLER FABRICATED & INSTALLED WITH INITIAL REPAIR DOUBLERS AS PER HX RS R53-61-35676. CONTINUED INSPECTIONS PER SSID ITEM F-39C IS REQUIRED AS PER HX RS R53-61-35676 AND UPS EO B747-5330-25568.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 2208 RBL 93 FLOOR SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.020" BY 1/2" BY 1" EXCEED SRM LIMIT. M/D BS 2200-2220 RBL 93 FLOOR SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 2190-2200 RBL89 SEAT TRACK FLANGE FOUND CORRODED. (BOTH SIDES) CORROSION BLEND OUT 0.035" BY 5/8" BY 10" EXCEED SRM LIMIT. BS 2150-2230 RBL89 SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 2140) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 2140 RBL 85 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.053" X 1" X 2" EXCEED SRM LIMIT. M/D BS 2140 RBL 45 TO RIGHT O/B MOST FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 2050-2130 LBL97 SEAT TRACK FLANGE FOUND CORRODED (BOTH SIDE). CORROSION BLEND OUT 0.035" BY 3/4" BY 1.5" EXCEED SRM LIMIT. M/D BS 2030-2150 LBL 98 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FLOOR SUPPORT — CORRODED (BS 1920-1940) · airframe 97,105 hrs · 24,042 cycles

BS 1930 RBL 118 FLOOR SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.021" BY 1" BY 1" EXCEED SRM LIMIT. BS 1920-1940 RBL 118 FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C FWD CARGO DOOR CUTOUT FWD HINGE MOST FWD LWR FASTENER HOLE FOUND CRACK AT SKIN RUNNING DOWN APPROX 0.040". FUSELAGE FWD CARGO DOOR CUTOUT FWD HINGE ATTACHED SKIN REPAIRED AS PER HX RS R53-21-35670. CONTINUED INSPECTION IS REQUIRED AS PER HX RS R53-21-35670 AND UPS EO B747-5330-25575-A.

Part: FLOOR PANEL — CORRODED (BS 2180-2200) · airframe 97,105 hrs · 24,042 cycles

BS 2180-2200 LBL99-100 FLOOR WEB FOUND CORROSION. M/D BS 2180-2200 LBL 99-100 FLOOR WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS1800-1820 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.057" BY 7/8" BY 1 7/8" EXCEED SRM LIMIT. M/D BS 1770-1830 LBL33 SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED WITH EXISTING SPLICE PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 2132 LBL89 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.035" BY 5/8" BY 1" EXCEED SRM LIMIT. M/D BS 2150-2230 LBL89 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 2280 LBL60-70 FLOORBEAM FOUND CORROSION. CORROSION BLEND OUT 0.045" X 1.5" 2" EXCEED SRM LIMIT. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1, JUST AT M/D BS2280 BETWEEN LBL 50 AND LT MOST O/B.

Part: SEAT TRACK — CORRODED (BS 1780-1850) · airframe 97,105 hrs · 24,042 cycles

BS 1780-1850 LBL11 SEAT TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.034" BY 3/4" BY 1 1/4" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14 JUST AT M/D LBL11 BETWEEN STA 1770 AND 1850 REFER NRC NR 50955 FOR WORKING DETAIL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1800-1860 RBL75 SEAT TRACK FLANGE AND CROWN FOUND CORRODED. CORROSION BLEND OUT 0.036" BY 5/8" BY 1 3/4" EXCEED SRM LIMIT. M/D SEAT TRACK AT BS 1730-1870 RBL75 REPAIRED AS PER SRM 53-10-05 FIG 1A REFER NRC50940 FOR WORKING DETAIL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS2160 RBL 65 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.022" BY 1/2" BY 3" EXCEED SRM LIMIT. M/D BS 2110-2240 RBL 65 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 520 LBL 26-28 FLOORBEAM UPPER CHORD FOUND CORRODED. CORROSION BLEND OUT 0.054" BY 1" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 3 REFER NRC NR 50665 FOR WORKING DETAIL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 2000 RBL33-50 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.086" BY 2" BY 10" EXCEED SRM LIMIT. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 3 JUST AT M/D BS 2000 BETWEEN RBL 33 AND RT MOST O/B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS1813 RBL33 SEAT TRACK I/B FLANGE LOWER FACE FOUND CORRODED. CORROSION BLEND OUT 0.040" BY 7/8" BY 1.5" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 33 JUST AT M/D RBL33 BETWEEN BS1810 AND BS 1950.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1880-1900 RBL33 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045" BY 7/8" BY 1 1/8" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 33 JUST AT M/D RBL 33 BETWEEN BS 1810 AND BS 1950 (REFER NRC NO.51784 FOR DETAIL).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 2220-2240 RBL65 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.026" BY 5/8" BY 20" EXCEED SRM LIMIT. M/D BS 2110-2240 RBL65 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A REFER NRC 51776 FOR WORKING DETAIL.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

TIE DOWN FITTING SUPPORT PLATE CORRODED AT STA 1861 LBL77-80. CORROSION BLEND OUT 0.017" BY 5/8" BY 2" EXCEED SRM LIMIT. TIE DOWN FITTING REPLACED AS PER MM 20-51-01.

Part: STRINGER — DENTED (BS 220-240 S47L) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C FWD OF E/E COMPT LT STA 220 TO STA 240 STRINGER 47 FOUND DENT MARK, FWD OF E/E COMPT BS 205 TO BS 240 S47L. REPAIRED AS PER SRM 53-10-03 FIG 3.

Part: CARGO TRACK — CORRODED (BS 1840) · airframe 97,105 hrs · 24,042 cycles

TIE DOWN FTG FLANGE PLATE FOUND CORROSION JUST AT BS1840 LBL30. CORROSION BLEND OUT 0.026" AND 1/2" AND 1/2" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1920 RBL13 TIE DOWN FTG FLANGE PLATE FOUND CORRODED. CORROSION BLEND OUT 0.020" BY 3/4" BY 1" EXCEED SRM LIMIT. TIE DOWN FITTING PLATE REPLACED AS PER MM 20-51-01.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1800 RBL 80 TIE DOWN FITTING FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.038" BY 1/2" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: SPLICE PLATE — CRACKED (BS 400) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C NWW RT AFT CORNER BS400 INTERNAL SPLICE PLATE FOUND CRACK FROM EDGE EXTENDING UNDERNEATH B/H CHORD, CRACK LENGTH 1 1/8". NWW RT AFT CORNER BS 400 INTERNAL SPLICE PLATE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG9 AND 51-30-02.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS1800 LBL75 TIE DOWN FTG FLANGE PLATE FOUND CORRODED. CORROSION BLEND OUT 0.025" BY 5/8" BY 1" EXCEED SRM LIMIT. TIE DOWN PLATE REPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS2050 RBL97 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.028" BY 5/8" BY 3" EXCEED SRM LIMIT. M/D BS 2010-2070 RBL97 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FRAME — CRACKED (BS 2231 S24-25L) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C LEFT BS 2231 FRAME BETWEEN S-24L & 25L ONE FASTENER HOLE CRACK FOUND ON REVEAL. CRACK LENGTH 0.030". FRAME REVEAL REPAIRED AS PER HX RS R53-00-35672 AT BS 2231 BETWEEN STR 23L TO STR 25L AREA. CONTINUED INSPECTION IS REQUIRED AS PER HX RS R53-00-35672 AND UPS EO B747-5310-25584.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C FX FUSELAGE FWD CARGO DOOR CUTOUT AFT UPPER CORNER HINGE FAIRING AREA FOUND 1EA FASTENER HOLE CRACKED AT SKIN APPROX 0.030" RUNNING AFT UPWARD. FUSELAGE FWD CARGO DOOR CUTOUT AFT UPPER CORNER HINGE FAIRING ATTACH SKIN REPAIRED PER RS R53-21-35669. CONTINUED INSPECTION IS REQUIRED AS PER RS R53-21-35669 AND UPS EO B747-5330-25580-A.

Part: PRESSURE PANEL — CORRODED (BS 1416) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C LEFT B/G WHEEL WELL STA 1416 I/B AREA LBL 6 UPPER PRESSURE FLOOR ATTACH SURFACE FOUND CORROSION AS MARK. CORROSION BLEND OUT 0.033" X 1/2" X 2" EXCEED SRM LIMIT. LEFT BLG WHEEL WELL BS 1416 I/B AREA PRESSURE WEB REPAIRED AS PER SRM 53-10-07 FIG 15. SUBSEQUENT INSP ARE NECESSARY FOR CAT B REPAIR REFER SRM 53-10-07 FIG 15 TABLE 2 FOR INSP REQUIREMENT.

Part: FLOORBEAM — CORRODED (BS 2260) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE-C M/D BS 2260 RBL 60 FLOORBEAM FOUND CORRODED. (CORROSION BLEND OUT 0.030 INCH X 2 INCH X 2 INCH EXCEED SRM LIMIT.) M/D BS 2260 LBL 8 INCH TO RBL 66 INCH FLOORBEAM REPAIRED IAW SRM 51-40-04 FIG 1. REF NRC 51769 FOR WORKING DETAIL.

Part: FRAME — CRACKED (BS 880 S39L) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C FWD CARGO COMPT LT STA 880 STRINGER 39 FRAME FOUND CRACK. CRACK LENGTH 7 INCH FWD CARGO COMPT BS 880 LEFT STR 36L TO STR 40L FRAME REPAIRED AS PER RS R53-00-35679 AND UPS EO B747-5310-25578-A.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1940 RBL77 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.018" BY 1/2" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C FX FWD CARGO DOOR CUTOUT FWD UPPER CORNER HINGE FAIRING AREA FOUND 1EA FASTENER HOLE CRACKED AT APPROX 0.040" IN LENGTH RUNNING DOWNWARD. FX FWD CARGO DOOR CUTOUT FWD UPPER CORNER HINGE FAIRING ATTACHED SKIN REPAIRED AS PER HX RS R53-21-35670. CONTINUED INSPECTION IS REQUIRED AS PER HX RS 53-21-35670 AND UPS EO B747-5330-25575-A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 2060 RBL60 FLOOR SUPPORT O/B FTG FOUND CRACKED, CRACK LENGTH 1.5". M/D BS 2060 RBL60 FLOOR SUPPORT O/B FTG REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1800 RBL35 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.080" BY 1/2" BY 1/2" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1880 RBL 55 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.018" BY 1/2" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: RIB — CRACKED (LT WING) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C LT WING UPPER L/E PANEL SUPPORT RIB FOUND CRACKED AT WS 1230 JUST BEHIND NR 5 VC FLAP O/B DRIVE I/B. CRACKED LENGTH 1/4 INCH. LT WING UPPER L/E PANEL SUPPORT RIB AT WS 1230 JUST BEHIND NR 5 VC FLAP O/B DRIVE I/B AREA REPAIRED AS PER HX RS R57-41-35666 DETAIL VISUAL INSPECTION THE AFFECTED AREA AT C-CHECK INTERVALS, NOT TO EXCEED 18 MONTHS PER HX RS R57-41-35666 IS REQUIRED AND AS PER UPS EO B747-5740-25561-A.

Part: FLOORBEAM — CORRODED (BS 2340) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D FLOORBEAM SUPPORT CHORD CORRODED AT STA 2340 LBL 43 - LBL 57. CORROSION BLEND OUT 0.058" X 1/2" X 10" EXCEED SRM LIMIT. M/D BS 2340 LBL 21 TO LEFT O/B FLOORBEAM SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1860 RBL55 TIE DOWN FITTIING FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.026" BY 3/4" BY 3/4" EXCEED SRM LIMIT. TIE DOWN FITTING REPLACED AS PER MM 20-51-01.

Part: CARGO TRACK — CORRODED (BS 1800) · airframe 97,105 hrs · 24,042 cycles

BS 1800 TIE DOWN FTG FLANGE PLATE FOUND CORROSION. CORROSION BLEND OUT 0.019" BY 3/4" BY 3/4" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-50-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1920 RBL82 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.080" BY 3/4" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: SILL — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

RT CREW DOOR SILL I/B VERT WEB FWD AND AFT ANGLE FOUND CRACKED, CRACK LENGTH 3/8" AND 1/2". RT CREW DOOR SILL I/B VERTICAL WEB FWD AND AFT ATTACHED ANGLES 2 REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS2020 RBL60 O/B FWD AND AFT VERTICAL SUPPORT FOUND CRACKED, CRACK LENGTH 7/8" AND 1 1/4". M/D BS2020 RBL60 O/B FWD AND AFT VERTICAL SUPPORT REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1880 RBL50 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.017" BY 1" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1900 RBL30 TIE DOWN FTG FLANGE PLATE FOUND CORRODED. CORROSION BLEND OUT 0.019" BY 3/4" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1820 RBL80 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.075" BY 1/2" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

TIE DOWN FTG PLATE CORRODED AT STA 2038 RBL26. CORROSION BLEND OUT 0.026" BY 1/2" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1920 RBL95 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.080" BY 1" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: FRAME — CRACKED (BS 880 S37-38R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C FWD CARGO COMPT RT STA 880 S37 AND S38 FRAME FOUND CRACKED, (2 LOCATION), CRACK LENGTH 4" AND 2.5" FRAME REPAIRED PER SRM 53-10-04 FIG 52.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D TIE DOWN FTG FLANGE PLATE FOUND CORRODED JUST AT BS 1920 LBL85. CORROSION BLEND OUT 0.080" BY 1" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: SPLICE PLATE — CRACKED (BS 400) · airframe 97,105 hrs · 24,042 cycles

NWW LT AFT CORNER BS 400 INTERNAL SPLICE PLATE FOUND CRACK FROM EDGE EXTENDING B/H CHORD, CRACK LENGTH 1". NWW LT AFT CORNER BS 400 INTERNAL SPLICE PLATE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1870-1920 RBL33 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.075" BY 1/2" BY 3" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 33 JUST AT M/D RBL33 BETWEEN BS 1810 AND BS 1950 (REFER NRC NO.51784 FOR DETAIL).

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 2276 BL0 HAT SECTION FOUND CORROSION. CORROSION BLEND OUT 0.025" BY 1/2" BY 3" EXCEED SRM LIMIT. HAT SECTION REPLACED AS PER SRM 51-10-01 P9 JUST AT M/D BS2276 BETWEEN LBL 11 AND RBL 11.

Part: CARGO TRACK — CORRODED (BS 1920) · airframe 97,105 hrs · 24,042 cycles

BS 1920 TIE DOWN FTG FLANGE PLATE FOUND CORROSION. CORROSION BLEND OUT 0.075" BY 1/2" BY 1/2" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1880 LBL50 TIE DOWN FTG FLANGE PLATE FOUND CORRODED. CORROSION BLEND OUT 0.080" BY 1/2" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: FRAME — CRACKED (BS 2231) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RT BS 2231 FRAME BETWEEN S24R & S25R ONE FASTENER HOLE CRACK FOUND ON CHORD I/B SURFACE APPROX 0.040" RUNNING FWD. M/D BS 2231 RT FRAME ATTACHED CHORD & REVEAL REPAIRED AS PER HX RS R53-60-35673. CONTINUED INSPECTION IS REQUIRED AS PER HX RS R53-60-35673 AND UPS EO B747-5310-25592.

Part: SILL — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C U/D BS 408 RBL 81 CREW DOOR CUTOUT SILL I/B LWR CHORD FOUND CRACKED, CRACK LENGTH 1/2". U/D BS 408 RBL 81 CREW DOOR CUTOUT SILL LOWER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: FLOOR SUPPORT — CORRODED (BS 2280-2300) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D FLOOR SUPPORT CORRODED AT STA 2280-2300 LBL 72. CORROSION BLEND OUT 0.064" X 1/2" X 8" EXCEED SRM LIMIT 53-10-01 FIG 1. M/D FLOOR SUPPORT AT BS 2280-2300 LBL 72 REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: SEAT TRACK — CORRODED (BS 2230-2240) · airframe 97,105 hrs · 24,042 cycles

BS 2230-2240 RBL 75 SEAT TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.017" BY 7/8" BY 10". SEAT TRACK REPLACED AS PER SRM 51-10-01 P9 JUST AT M/D RBL75 BETWEEN STA 2150 AND 2240.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1960 RBL77 TIE DOWN FTG FLANGE PLATE FOUND CORRODED. CORROSION BLEND OUT 0.020" BY 1" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: HOUSING — CHAFED (FLAP TRACK) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE-C RT WING - O/B MID FLAP OB FORE FLAP TRACK FWD HOUSING FOUND DEEP CHAFED. RHW OB MID FLAP O/B FORE FLAP TRACK FWD HOUSING FTG ASSY REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1820 RBL 35 TIE DOWN FTG PLATE FOUND CORRODED. CORROSION BLEND OUT 0.017" BY 1/2" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1900 RBL 13 TIE DOWN FITTING FLANGE PLATE FOUND CORRODED. CORROSION BLEND OUT 0.020" BY 3/4" BY 2" EXCEED SRM LIMIT. TIE DOWN FITTING PLATE REPLACED AS PER MM 20-51-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D FLOOR SUPPORT CORRODED AT STA 2350-2360 RBL17. CORROSION BLEND OUT 0.072" BY 1/2" BY 10" EXCEED SRM LIMIT. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 P9 JUST AT M/D RBL17 BETWEEN STA 2340 AND 2360.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1940 RBL 55 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.018" BY 7/8" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

SEAT TRACK O/B FLANGE CORRODED AT STA 1910-1920 LBL 75". CORROSION BLEND OUT 0.040" BY 5/8" BY 1.5" EXCEED SRM 53-10-01 FIG 1 LIMITS. CORRODED SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 1A FROM BS 1830 - 1950 LBL 75" AREA REFER NRC 51205 FOR WORKING DETAIL.

Part: CHANNEL — DEFORMED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

M/D BS2320-2340 LBL11 HAT SECTION SUPPORT FOUND DEFORMED. HAT SECTION SUPPORT REPLACED AS PER SRM 51-10-01 O9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 2040 RBL89 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.033" BY 1/2" BY 2" EXCEED SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 P9 JUST AT M/D RBL89 BETWEEN BS2040 AND BS2150 (REFER NRC NR 52060)

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1920 RBL27 TIE DOWN FTG FLANGE PLATE FOUND CORRODED. CORROSION BLEND OUT 0.025" BY 1" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1780 LBL85 TIE DOWN FTG FLANGE PLATE FOUND CORRODED. CORROSION BLEND OUT 0.022" BY 1" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: PLATE — CORRODED (BS 1920) · airframe 97,105 hrs · 24,042 cycles

BS 1920 LBL50 TIE DOWN FTG FLANGE PLATE FOUND CORROSION. CORROSION BLEND OUT 0.080" BY 1/4" BY 1/2" EXCEED SRM LIMIT. TIE DOWN FTG FLANGE PLATE REPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — CORRODED (BS 2150-2160) · airframe 97,105 hrs · 24,042 cycles

BS 2150-2160 LBL97 SEAT TRACK O/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.026" BY 7/8" BY 1.5" EXCEED SRM LIMIT. BS 2150-2200 LBL97 SEAT TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01, PG 9 AND 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 2060 LBL100 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.052" BY 1/2" BY 1/2" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1860 LBL60 TIE DOWN FTG FLANGE PLATE FOUND CORRODED. CORROSION BLEND OUT 0.035" BY 1" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1840 RBL 25 TIE DOWN FTG FLANGE PLATE FOUND CORRODED. CORROSION BLEND OUT 0.017" BY 5/8" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: FLOORBEAM — CRACKED (BS 1960) · airframe 97,105 hrs · 24,042 cycles

BS 1960 RBL60 I/B FLOOR FTG FOUND CRACKED, CRACK LENGTH 1.5". FLOOR SUPPORT FITTING REPLACED AS PER SRM 51-10-01 P.9 AND INSTALLED AS PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 2240-2260) · airframe 97,105 hrs · 24,042 cycles

BS 2240-2260 RBL33 SEAT TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.019" BY 1" BY 10" EXCEED SRM LIMIT. M/DECK BS 2230 TO BS 2280 RBL 33" TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 2000 RBL55 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.072" BY 1/2" BY 1/2" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 2200 RBL77 TIE DOWN FTG FLANGE PLATE FOUND CORROSION. CORROSION BLEND OUT 0.020" BY 1/2" BY 1/2" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: CARGO TRACK — CORRODED (BS 1880) · airframe 97,105 hrs · 24,042 cycles

TIE DOWN FLANGE PLATE FOUND CORROSION JUST AT BS 1880 LBL30. CORROSION BLEND OUT 0.016" BY 1/2" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — CORRODED (BS 2089-2096) · airframe 97,105 hrs · 24,042 cycles

FOUND SEAT TRACK FLANGE CORRODED AT STA 2089-2096 LBL89. CORROSION BLEND OUT 0.020" BY 0.5" BY 10". SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A JUST AT M/D LBL89 BETWEEN STA 2040 AND 2150.

Part: SEAT TRACK — CORRODED (BS 2086-2096) · airframe 97,105 hrs · 24,042 cycles

SEAT TRACK O/B FLANGE CORRODED AT STA 2086-2096 LBL89. CORROSION BLEND OUT 0.021" BY 7/8" BY 10". SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A JUST M/D LBL 89 BETWEEN STA 2040 AND 2150. REFER NRC NR 51200 FOR WORKING DETAIL.

Part: FRAME — CRACKED (BS 4900) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D FRAME FOUND CRACKED ON BS 4900 S13R, CRACK LENGTH 3/8". FRAME CRACKED ON BS 4900 STR 13R AREA REPAIRED AS PER SRM 53-10-04 FIG 87.

Part: FITTING — WORN (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1900 RBL55 TIE DOWN FTG FOUND WORN. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D FLOOR SUPPORT CORRODED AT STA 2280-2300 RBL63. CORROSION BLEND OUT 0.024" BY 1/2" BY 20" EXCEED SRM LIMIT. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 P9 JUST AT M/D RBL63 BETWEEN BS2280 AND 2300.

Part: FITTING — WORN (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

TIE DOWN FTG FOUND WORN JUST AT BS 1880 RBL 55. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: FLOOR SUPPORT — CORRODED (BS 1920-1940) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C BULK CARGO COMPT LT STA 1920-1940 LBL50 FLOOR SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.035" BY 2" BY 2" EXCEED SRM LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20 JUST AT LBL 50 BETWEEN STA1920 AND 1950.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D SEAT TRACK CORRODED AT STA 2040-2100 LBL33-34. CORROSION BLEND OUT 0.023" BY 1/2" BY 20" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A JUST AT M/D LBL 33 BETWEEN BS 2030 AND BS 2110.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

SEAT TRACK CORRODED AT STA 1861-1910 LBL 75. CORROSION BLEND OUT 0.035" BY 1/2" BY 25" EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AT BS 1830-1950 LBL 75" AREA AS PER SRM 53-10-05 FIG 1 A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D SEAT TRACK FLANGE CORRODED AT STA 2040-2140 LBL67. CORROSION BLEND OUT 0.043" BY 1/2" BY 20" EXCEED SRM LIMIT. M/D SEAT TRACK BS 2040-2150 LBL67 REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (BS 380-400) · airframe 97,105 hrs · 24,042 cycles

BS 380 TO 400 RBL95 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.029" BY 1/2" BY 10" EXCEED SRM LIMIT. SEAT TRACK REPLACED FROM BS 370-410 RBL 95 AS PER SRM 51-10-01 PG 9.

Part: FITTING — CHAFED (RT WING) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RIGHT WING O/B MID FLAP MOST I/B MOST FLAP SLIDING TRACK COMPT I/B WEB ATTACHMENT FOUND CHAFED. RIGHT WING O/B MID FLAP MOST I/B MOST FLAP SLIDING TRACK I/B WEB CHAFED AREA REPAIRED AS PER HX RS R57-58-35680 DETAIL VISUAL INSPECTION REPAIR AREA AT AN INTERVAL CONCURRENT WITH THE INSPECTION INTERVAL MANDATED BY AD 75-20-05 AND REF UPS EO B747-5740-25582.

Part: SEAT TRACK — CORRODED (BS 2040-2050) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D SEAT TRACK CORRODED AT STA 2040 - 2050 LBL 74. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A JUST AT LBL 74 BETWEEN BS 2050 AND 2090.

Part: SEAT TRACK — CORRODED (BS 1861-1920) · airframe 97,105 hrs · 24,042 cycles

SEAT TRACK CORRODED AT STA 1861-1920 LBL97. CORROSION BLEND OUT 0.026" BY 1/2" BY 20" EXCEED SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 53-10-05 FIG 1A.

Part: FLOORBEAM — CORRODED (BS 2139) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D FLOORBEAM CORRODED AT STA 2139 LBL 67 TO LBL 75. CORROSION BLEND OUT 0.059" X 2" X 3" EXCEED SRM LIMIT. M/D BS 2139 LBL 40 TO LEFT O/B MOST FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SPAR — CORRODED (RT WING) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RIGHT WING REAR SPAR UPPER CHORD FOUND CORRODED AT WS 400 W/W AREA. CORROSION BLEND OUT 0.420" X 3" X 6" EXCEED SRM 57-10-01 FIG 1 LIMITS. RIGHT WING REAR SPAR UPPER CHORD AT WS 400 AREA REPAIRED AS PER HX RS R57-22-35684 AND UPS EO B747-5710-25565.

Part: STRINGER CLIP — CORRODED (BS 1800) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C AFT CARGO COMPT, LT STA 1800 STRINGER 49 TIE CLIP FOUND CORROSION, CORROSION BLEND OUT 0.013" BY 3/4" BY 1/2" EXCEED SRM LIMIT. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. P/N : BAC1518-458-7075T6511.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1540 RBL28 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.019" BY 3/4" BY 1 1/2" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: CARGO TRACK — CORRODED (BS 1720) · airframe 97,105 hrs · 24,042 cycles

BS 1720 LBL66 TIE DOWN FTG FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.022" BY 1" BY 1" EXCEED SRM LIMIT. TIE DOWN FIG PLATE REPLACED AS PER MM 20-51-01.

Part: CARGO TRACK — CORRODED (BS 1800) · airframe 97,105 hrs · 24,042 cycles

BS 1800 LBL30 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.019" BY 3/4" BY 3/4" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-50-01.

Part: CARGO TRACK — CORRODED (BS 1720) · airframe 97,105 hrs · 24,042 cycles

BS 1720 LBL100 TIE DOWN FTG FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.019" BY 1/2" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: CARGO TRACK — CORRODED (BS 1780) · airframe 97,105 hrs · 24,042 cycles

BS 1780 LBL 95 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.019" BY 1" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1780 RBL95 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.081" BY 1/2" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — BROKEN (BS 1760) · airframe 97,105 hrs · 24,042 cycles

BS 1760 LBL97 SEAT TRACK CROWN FOUND BROKEN. SEAT TRACK REPLACED AS PER SRM 51-10-01 P9 JUST AT LBL 97 BETWEEN STA 1670 AND 1790.

Part: CARGO TRACK — CORRODED (BS 1800) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1800 RBL 60 TIE DOWN FITTING FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.038" BY 1/2" BY 1" EXCEED SRM LIMIT. TIE DOWN PLATE REPLACED AS PER MM 20-51-01.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 97,102 hrs · 24,042 cycles

INSPECTION TYPE:C AFT CARGO COMPT RT STA 1500 O/B TIE DOWN TRACK FOUND CORROSION. CORROSION BLEND OUT 0.020" BY 1/2" BY 2" EXCEED SRM LIMIT. AFT CARGO COMPT BS 1500-1530 MOST RT O/B TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 5.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS1780 RBL25 TIE DOWN FTG FLANGE FOUND COR. CORROSION BLEND OUT 0.080" X 1/2" X 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: CARGO TRACK — CORRODED (BS 1560) · airframe 97,105 hrs · 24,042 cycles

BS 1560 RBL 17 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.022' BY 5/8" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — CORRODED (BS 1720-1750) · airframe 97,105 hrs · 24,042 cycles

BS 1720-1750 LBL 97 SEAT TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.057" BY 1/2" BY 20". SEAT TRACK REPLACED AS PER SRM 51-10-01 P.9 JUST AT LBL 97 BETWEEN STA 1670 AND 1790 REFER NRC NR 508129 FOR DETAIL.

Part: CARGO TRACK — CORRODED (BS 1780) · airframe 97,105 hrs · 24,042 cycles

BS 1780 LBL66 TIE DOWN FTG FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.081" BY 0.5" BY 1". TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: CARGO TRACK — CORRODED (BS 1642) · airframe 97,105 hrs · 24,042 cycles

BS 1642 RBL93 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.033" BY 7/8" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG AND PLATE REPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS1780 - 1800 LBL11 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.020" BY 1/2" BY 20" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A JUST AT M/D LBL11 BETWEEN STA 1770 AND 1870.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1800 RBL25 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.025" BY 1" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — CORRODED (BS 1720-1725) · airframe 97,105 hrs · 24,042 cycles

BS 1720-1725 RBL 97 SEAT TRACK O/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.021" BY 1/2" BY 3" EXCEED SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 JUST AT RBL 97 BETWEEN STA 1650 AND 1730.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1780 RBL 90 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.029" BY 1" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: WEB — CORRODED (BS 1403) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RIGHT B/G WHEEL WELL STA 1403 RBL 17 TO RBL 123 UPPER PRESSURE FLOOR WEB ATTACH CHORD AREA FOUND CORROSION. CORROSION BLEND OUT 0.045" X 1" X 3" EXCEED SRM LIMIT. RIGHT BLG WHEEL WELL BS 1403 LATERAL SUPPORT CHORD AT UPPER PRESSURE WEB LOWER SURFACE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1800 RBL34 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.080" BY 2" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01 (REFER NRC.51381 FOR DETAIL).

Part: CARGO TRACK — CORRODED (BS 1660) · airframe 97,105 hrs · 24,042 cycles

BS 1660 RBL 77 TIE DOWN FTG FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.036" BY 1" BY 1". TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: FLOORBEAM — CRACKED (BS 1780) · airframe 97,105 hrs · 24,042 cycles

BS 1780 LBL 112-118 FLOOR SUPPORT FOUND CRACKED, CRACK LENGTH 3/4". BS 1780 LBL 112-118 FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS1730-1820 LBL75 I/B SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.025" BY 1" BY 20" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A FROM BS 1690 TO BS 1830 LBL75.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1780 LBL85 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.022" BY 5/8" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1780 RBL15 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.031" BY 3/4" BY 3/4" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: CARGO TRACK — CORRODED (BS 1700) · airframe 97,105 hrs · 24,042 cycles

BS 1700 RBL 55 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.031" BY 5/8" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: SUPPORT — BROKEN (FAIRING) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C FX BODY FAIRING SUPPORT CRACKED AT BS 1480 S29L AND 30L. FX BODY FAIRING SUPPORT AT BS 1480 STR 29L AND 30L AREA REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 1586 RBL55 TIE DOWN FTG FLANGE CORROSION. CORROSION BLEND OUT 0.018" BY 7/8" BY 2" EXCEED SRM LIMIT. TIE DOWN FTG REPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — CORRODED (BS 1720) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS1720 LBL11 SEAT TRACK FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.018" BY 1/2" BY 3" EXCEED SRM LIMIT. M/D BS 1690-1770 LBL11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: FLOORBEAM — CORRODED (BS 1700) · airframe 97,105 hrs · 24,042 cycles

BS 1700 LBL15 - 25 FLOORBEAM FOUND CORROSION. CORROSION BLEND OUT 0.070" BY 2" BY 2" EXCEED SRM LIMIT. BS 1700 LBL20 - BL0 FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 3.

Part: CARGO TRACK — CORRODED (BS 1680) · airframe 97,105 hrs · 24,042 cycles

TIE DOWN FTG FLANGE FOUND CORROSION JUST AT BS 1680 LBL40. CORROSION BLEND OUT 0.049" BY 3/4" BY 3/4" EXCEED SRM LIMIT. PLATE REPLACED AS PER MM 20-51-01.

Part: PLATE — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D TIE DOWN FTG SUPPORT PLATE CORRODED AT STA 1602 RBL16-18. CORROSION BLEND OUT 0.072" BY 3/4" BY 1" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1760 RBL90 TIE DOWN FTG FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.022" BY 1/2" BY 1/2" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: SEAT TRACK — CORRODED (BS 1640) · airframe 97,105 hrs · 24,042 cycles

BS 1640 RBL 98 SEAT TRACK CROWN CORROSION. CORROSION BLEND OUT 0.065" BY 1/2" BY 1.5" EXCEED SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 P9 JUST AT RBL 98 BETWEEN STA 1570-1650.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1790-1800 RBL75 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.024" BY 1/2" BY 10" EXCEED SRM LIMIT. M/D BS 1730-1870 RBL 75 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (BS 1500) · airframe 97,105 hrs · 24,042 cycles

SEAT TRACK STA 1500 LBL97 I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.021" BY 5/8" BY 2" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A, JUST AT M/D LBL97 BETWEEN BS 1480 AND 1550.

Part: CARGO TRACK — CORRODED (BS 1760) · airframe 97,105 hrs · 24,042 cycles

BS 1760 LBL66 TIE DOWN FTG FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.070" BY 1/2" BY 1/2" EXCEED SRM LIMIT. TIE DOWN FTG PLATE REPLACED AS PER MM 20-51-01.

Part: FLOOR SUPPORT — CORRODED (BS 1750-1760) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1750-1760 LBL 118 FLOOR SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.012" BY 1" BY 1" EXCEED SRM 53-10-01 FIG 1 LIMITS, M/DECK BS 1756-1768 LBL 118" FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: ATTACH FITTING — DEFORMED (BS 2000 S12R) · airframe 97,105 hrs · 24,042 cycles

FOUND BS 2000 S-12R FRAME ATT TIE CLIP FOUND DEFORMED. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — DAMAGED (BS 1614) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D STA 1614 RBL 11 SEAT TRACK AT GUIDE HOLE ELONGATED. M/DECK BS 1590-1650 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: STRINGER — CRACKED (BS 1485 S5R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1485 S5R STRINGER END FOUND CRACKED, CRACK LENGTH 0.75 INCH. M/D BS 1485 STR 5R REPAIRED AS PER RS R53-61-35649 AND UPS EO B747-5310-25537.

Part: FRAME — CRACKED (BS 1700 S12-16L) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C MD BS 1700 S13L FRAME FOUND CRACKED. M/D BS 1700 BETWEEN STR 12L - 16L AREA FRAME REPLACED AS PER RS R53-62-35644 AND UPS EO B747-5310-25536-A.

Part: STRINGER — CRACKED (M/D) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE-C M/D BS1485 S6R STRINGER END FOUND CRACKED. (CRACK LENGTH 0.45 INCH INCH 0.75 INCH). M/D BS1485 STR 6R REPAIRED IAW RS R53-61-35650 CONTINUE INSPECTION ARE REQUIRED IAW RS R53-61-35650 AND UPS EO B747-5310-25552-A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 520 RBL 50 TO 55 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.067" BY 2" BY 3" EXCEED SRM 53-10-01 FIG 1 LIMITS. BS 520 LBL 42" TO RT BL 62" EXISTING SPLICE FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 3.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 2220 S26L FRAME INNER EDGE FOUND PUNCH MARK. BS 2220 BETWEEN STR 24L TO 34L FRAME REPAIRED AS PER SRM 53-10-04 FIG 100.

Part: FLOORBEAM — CORRODED (BS 460) · airframe 97,105 hrs · 24,042 cycles

BS 460 LBL11 TO 33 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.054" BY 2" BY 10". FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1, JUST AT M/D BS460 BETWEEN RBL22 AND LBL52 REFER NRC NR 50645 FOR WORKING DETAIL.

Part: STRINGER — CRACKED (BS 1485 S11R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1485 STR 11R STRINGER END FOUND CRACK. CRACK LENGTH 1 INCH. M/D BS 1485 STR 11R STRINGER REPAIRED AS PER RS R53-61-35652 AND UPS E ENGINEERING FILE 747-53-20348.

Part: FRAME — CRACKED (BS 1740 S12-14R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1740 S13R FRAME INNER FLANGE FOUND CRACK. M/D BS 1740 BETWEEN STR 12R TO STR 14R AREA FRAME REPAIRED AS PER RS R53-62-35660 AND UPS EO B747-5310-25543-A.

Part: FRAME — CRACKED (BS 1760 S12R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1760 S12R FRAME INNER FLANGE FOUND CRACKED. CRACK LENGTH 1/2 INCH. FRAME REPAIRED PER HX RS R53-62-35659 AT BS 1760 STR 12R TO STR 14R AREA AND AS PER UPS EO B747-5310-25576-A.

Part: SEAT TRACK — CORRODED (BS 380-410) · airframe 97,105 hrs · 24,042 cycles

BS 380-410 LBL11 SEAT TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.029" BY 1/2" BY 10" EXCEED SRM LIMIT. BS 320-410 LBL 11 SEAT TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CORRODED (BS 460-480) · airframe 97,105 hrs · 24,042 cycles

BS 460-480 LBL11 SEAT TRACK I/B FLANGE FOUND CORRODED. FOUND CORROSION BLEND OUT 0.026" BY 1/2" BY 10" EXCEED SRM LIMIT. BS 410-510 LBL11 SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 REFER NRC50672 FOR WORKING DETAIL.

Part: FRAME — CRACKED (BS 1840 S13-14R) · airframe 97,105 hrs · 24,042 cycles

BS 1840 BETWEEN S13R AND S14R FRAME INNER FLANGE FOUND CRACKED, CRACK LENGTH 1/2". BS 1840 BETWEEN S13R AND S14R FRAME INNER FLANGE REPAIRED AS PER SRM 53-10-04 FIG 87.

Part: SEAT TRACK — CORRODED (BS 460-480) · airframe 97,105 hrs · 24,042 cycles

BS 460-480 RBL 11 SEAT TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.036' BY 7/8" BY 10" EXCEED SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 P9, JUST AT RBL 11 BS 410 AND 510 (REFER NRC50679 FOR DETAIL).

Part: CHANNEL — CORRODED (BS 480) · airframe 97,105 hrs · 24,042 cycles

BS 480 LBL4-RBL4 FLOOR SUPPORT HAT SECTION FWD FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.025" BY 1/2" BY 4" EXCEED SRM LIMIT. HAT SECTION REPLACED AS PER SRM 51-10-01 P9.

Part: SEAT TRACK — CORRODED (BS 480-500) · airframe 97,105 hrs · 24,042 cycles

BS 480-500 RBL95 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.025" BY 1/2" BY 20" EXCEED SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 P9 JUST AT RBL 95 BETWEEN STA 480 AND 510.

Part: SEAT TRACK — CORRODED (BS 470-490) · airframe 97,105 hrs · 24,042 cycles

BS 470-490 LBL33 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.023" BY 1/2" BY 10" EXCEED SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 P9 JUST AT LBL 33 BETWEEN STA 460 AND 510.

Part: SHEAR TIE — DEFORMED (BS 1580 S16R) · airframe 97,105 hrs · 24,042 cycles

BS 1580 S-16R FRAME ATT TIE CLIP FOUND DEFORMED. TIE CLIP REPLACED AS PER SRM 51-10-01 P9 AND INSTALLED AS PER SRM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 480) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 480 LBL 11 TO 22 FLOORBEAM FOUND CORROSION. CORROSION BLEND OUT 0.067" BY 2" BY 10" EXCEED SRM 53-10-01 FIG 1 LIMITS, M/D BS 480 LBL 47 TO RBL 22" FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SEAT TRACK — CORRODED (BS 440) · airframe 97,105 hrs · 24,042 cycles

BS 440 LBL70 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.080" BY 1/2" BY 2" EXCEED SRM LIMIT. CORRODED TRACK REPLACED FROM BS 410-460 LBL 70 AS PER SRM 51-10-01 PG 9.

Part: CARGO TRACK — CORRODED (BS 420-440) · airframe 97,105 hrs · 24,042 cycles

BS 420-440 RBL 66-72 TIE DOWN TRACK O/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.023" BY 7/8" BY 10" EXCEED SRM LIMIT. CORRODED TIE DOWN TRACK REPLACED FROM BS 410-460 AS PER SRM 51-10-01 PG 9.

Part: CARGO TRACK — CORRODED (BS 460-480) · airframe 97,105 hrs · 24,042 cycles

BS 460-480 RBL 11 TIE DOWN TRACK O/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.025" BY 1/2" BY 10" EXCEED SRM LIMIT. TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9 JUST AT RBL 11 BETWEEN STA 410 AND 510 (REFER NRC 50679).

Part: SEAT TRACK — CORRODED (BS 440) · airframe 97,105 hrs · 24,042 cycles

BS 440 LBL11 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.023" BY 1/2" BY 3" EXCEED SRM LIMIT. BS410-510 LBL11 SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 REFER NRC50672 FOR WORKING DETAIL.

Part: FLOORBEAM — CORRODED (BS 460) · airframe 97,105 hrs · 24,042 cycles

BS 460 LBL11 - RBL 11 FLOORBEAM ANCHOR NUTS AREA FOUND CORROSION. FLOOR BEAM REPAIRED AS PER SRM 51-40-04 FIG 1 JUST AT M/D, BS 460 BETWEEN RBL 22 AND LBL 52.

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 97,105 hrs · 24,042 cycles

BS 480-520 RBL75 SEAT TRACK I/B AND O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.024" BY 1/2" BY 10" EXCEED SRM LIMIT. CABIN BS480-520 AND BS 520-550 RBL75 SEAT TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: STRINGER — CRACKED (BS 1485 S7R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1485 STR 7R STRINGER END FOUND CRACKED. CRACK LENGTH .75 INCH. M/D BS 1485 STR 7R STRINGER REPAIRED AS PER RS R53-61-35651 AND UPS EO EO B747-5310-25550.

Part: FRAME — DENTED (BS 1800 S11R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1800 S11R FRAME INNER FLANGE FOUND DENT MARK. DENT LENGTH 0.875 INCH. M/D BS 1800 STR 11R FRAME REPAIRED AS PER HX RS R53-62-35665. CONTINUED INSPECTION REQUIRED PER HX RS R53-62-35665 AND UPS EO B747-5310-25583-A.

Part: SEAT TRACK — CORRODED (BS 420) · airframe 97,105 hrs · 24,042 cycles

BS 420 LBL11 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.028" BY 1/2" BY 3" EXCEED SRM LIMIT. BS 410-510 LBL11 SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — DAMAGED (BS 2220 S26R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 2220 S26R FRAME INNER EDGE FOUND PUNCH MARK. M/D BS 2220 STR 24R TO STR 34R FRAME REPAIRED AS PER SRM 53-10-04 FIG 100 WITH NEW SEGMENT FRAME FABRICATED AS PER HX RS R53-62-35677 CONTINUE INSPECTION ARE REQUIRED AS PER HX RS R53-62-35677 AND UPS EO B747-5310-25574-A.

Part: SEAT TRACK — CORRODED (BS 490) · airframe 97,105 hrs · 24,042 cycles

BS 490 LBL11 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.035" BY 1/2" BY 3" EXCEED SRM LIMIT. BS 410 - 510 LBL11 SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02 REFER NRC 50672 FOR WORKING DETAIL.

Part: SEAT TRACK — CORRODED (BS 480-500) · airframe 97,105 hrs · 24,042 cycles

BS 480-500 LBL75 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.028" BY 1/2" BY 10" EXCEED SRM LIMIT. CORRODED TRACK REPLACED FROM BS 480-510 LBL75 AS PER SRM 51-10-01 PG 9.

Part: CARGO TRACK — CORRODED (BS 470-480) · airframe 97,105 hrs · 24,042 cycles

BS 470-480 RBL 33 TIE DOWN TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.021" BY 1" BY 6" EXCEED SRM LIMIT. BS 460-510 RBL33 TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9.

Part: CARGO TRACK — CORRODED (BS 410-460) · airframe 97,105 hrs · 24,042 cycles

BS 410-460 RBL 11 TIE DOWN TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.029" BY 1" BY 9" EXCEED SRM LIMIT. TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9 JUST AT RBL 11 BETWEEN STA 410 AND 510.

Part: FRAME — CRACKED (BS 1560 S14L) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1560 S14L FRAME FOUND CRACKED. CRACK LENGTH 3/8 INCH. FRAME REPAIRED PER HX RS R53-62-35667 AT BS 1560 STR 14L AREA. CONTINUED INSPECTION REQUIRED AS PER HX RS R53-62-35667 AND UPS EO B747-5310-25581-A.

Part: CARGO TRACK — CORRODED (BS 230-240) · airframe 97,105 hrs · 24,042 cycles

BS 230 TO 240 RBL74 TO 76 TIE DOWN TRACK O/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.032" BY 1/2" BY 10" EXCEED SRM LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A JUST AT RBL75 BETWEEN BS 230 AND 330.

Part: CARGO TRACK — CORRODED (BS 400-405) · airframe 97,105 hrs · 24,042 cycles

BS 400-405 RBL11 TIE DOWN TRACK O/B A/NUT AREA LOWER FACE FOUND CORROSION. CORROSION BLEND OUT 0.030" BY 7/8" BY 5" EXCEED SRM LIMIT. TIE DOWN TRACK AT RBL 11 BS 320-410. REPLACED AS PER SRM 51-10-01 PG9 WORKS DETAIL REF NRC 50350.

Part: SUPPORT — CORRODED (BS 1287) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C FX STA 1287 IN BETWEEN LBL16" AND RBL 16" KEEL BEAM PANEL SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.036" BY 1" BY 3" EXCEED SRM LIMIT. FX BS 1287 KEEL BEAM PANEL SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 P9 AND 51-30-02.

Part: FLOOR SUPPORT — DEFORMED (BS 420-440) · airframe 97,105 hrs · 24,042 cycles

BS 420 TO 440 RBL 95 FLOOR SUPPORT WEB UPR ATTACH 'L' ANGLE FOUND DEFORMED. SUPPORT WEB UPR ATT 'L' ANGLE REPLACED AS PER SRM 51-10-01 P9 AND INSTALLED AS PER SRM 51-30-02.

Part: CARGO TRACK — CORRODED (BS 230-240) · airframe 97,105 hrs · 24,042 cycles

BS 230-240 LBL25 TIE DOWN TRACK O/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.030" BY 1/2" BY 10" EXCEED SRM LIMIT. OUT OF LIMIT TIE DOWN TRACK REPAIRED AS PER SRM 51-10-01 PG 9, BETWEEN BS 140 AND BS 250.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

BS 360 TO 410 LBL11 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.023' BY 1/2" BY 10" EXCEED SRM LIMIT. BS 320-410 LBL11 SEAT TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 REFER NRC 50681 FOR WORKING DETAIL.

Part: SUPPORT — CORRODED (BS 1308) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C FX STA 1308 IN BETWEEN LBL 16" AND RBL 16" KEEL BEAM PANEL SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.043" BY 1.5" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, FX BS 1308 KEEL BEAM PANEL SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SEAT TRACK — CORRODED (BS 185-230) · airframe 97,105 hrs · 24,042 cycles

BS 185 TO 230 LBL40 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.021" BY 1/2" BY 7" EXCEED SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG9 JUST AT LBL40 BETWEEN BS 160 AND 230.

Part: SUPPORT — CORRODED (BS 1265) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C FX STA 1265 IN BETWEEN LBL 9" AND RBL 9" KEEL BEAM PANEL SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.046" BY 1" BY 2" EXCEED SRM LIMIT. FX BS 1265 KEEL BEAM PANEL SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 P9 AND 51-30-02.

Part: FLOOR SUPPORT — CORRODED (BS 360-370) · airframe 97,105 hrs · 24,042 cycles

BSL 360 TO 370 LBL90 TO 91 FLOOR SUPPORT O/B L ANGLE FOUND COROSION. CORROSION BLEND OUT 0.013" BY 1/2" X 5" EXCEED SRM LIMIT. SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: SEAT TRACK — CORRODED (BS 270-280) · airframe 97,105 hrs · 24,042 cycles

BS 270 TO BS 280 RBL40 SEAT TRACK FLANGE CORRODED. CORROSION BLEND OUT 0.038" BY 1/2" BY 10" EXCEED SRM LIMIT. CORRODED SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A BETWEEN BS 250 AND BS 290.

Part: SEAT TRACK — CORRODED (BS 260-320) · airframe 97,105 hrs · 24,042 cycles

BS 260 TO 320 RBL75 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.024" BY 1/2" BY 20" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A JUST AT RBL75 BETWEEN BS 230 AND 330.

Part: FLOOR SUPPORT — DEFORMED (BS 500-520) · airframe 97,105 hrs · 24,042 cycles

BS 500-520 RBL 5 FLOOR SUPPORT WEB FOUND DEFORMED. FLOOR SUPPORT WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 P9 AND SRM 51-30-02

Part: SHEAR TIE — DEFORMED (BS 1840 S15R) · airframe 97,105 hrs · 24,042 cycles

BS 1840 S-15R FRAME ATTACH TIE CLIP FOUND DEFORMED. TIE CLIP REPLACED AS PER SRM 51-10-01 P9 AND INSTALLED AS PER SRM 51-30-02.

Part: WEB — CRACKED (BS 300-320) · airframe 97,105 hrs · 24,042 cycles

BS 300 TO 320 RBL 10 FLOOR WEB FOUND CRACKED, CRACK LENGTH .7500. FLOOR WEB REPLACED AND INSTALLED AS PER SRM 51-10-01 P9 AND SRM 51-30-02.

Part: FRAME — DEFORMED (BS 1820 S14R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 1820 S14R FRAME FOUND DEFORMED. M/D BS 1820 STR 14R FRAME REPAIRED AS PER RS R53-62-35661 AND UPS EO B747-5310-25562-A.

Part: SKIN — CORRODED (RWS 1540) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RIGHT WING L/E CAVITY LWR EXTENSION SKIN FOUND CORRODED AT WS 1540 JUST BEHIND NR 26 VC FLAP. CORROSION BLEND OUT 0.053" X 1" X 2" EXCEED SRM LIMIT. RIGHT WING L/E CAVITY LWR EXTENSION SKIN AT WS 1512 AREA REPAIR PER RS R57-26-25675 AND UPS ENGINEERING FILE 747-57-20129.

Part: FITTING — CRACKED (FUSELAGE) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RIGHT BLG ACTUATOR SUPPORT FITTING O/B LUG FOUND CRACK. CRACK LENGTH: 1/8 INCH APPROX. RIGHT BLG ACTUATOR SUPPORT FITTING REPLACED PER EO B747-5340-0994.

Part: CARGO TRACK — CORRODED (BS 1880-1900) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C AFT CARGO COMPT LT STA1880-1900 I/B TIE DOWN TRACK FOUND CORROSION. CORROSION BLEND OUT 0.044" BY 2" BY 4". AFT CARGO COMPT BS 1865-1915 LT O/B TIE DOWN TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 P9 AND 51-30-02.

Part: CARGO TRACK — CRACKED (BS 402-404) · airframe 97,105 hrs · 24,042 cycles

BS 402-404 RBL11 TIE DOWN TRACK CROWN ATT LIP FOUND BROKEN, CRACK LENGTH 1/4". BS 320-410 RBL 11 TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9.

Part: SKIN — CORRODED (RWS 1400) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RIGHT WING L/E CAVITY LOWER EXTENSION SKIN FOUND CORROSION AT WS 1400 JUST BELOW NR 1 L/E FLAP PDU. CORROSION BLEND OUT 0.103" X 7/8" X 1.5" EXCEED SRM LIMIT. RIGHT WING L/E LOWER EXTENSION SKIN AT WS 1400 REPAIRED AS PER SRM 57-30-03 FIG 4.

Part: FLOORBEAM — CORRODED (BS 1500) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C AFT CARGO COMPT RT STA1500 IN BETWEEN RBL45 AND RBL58 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.033" BY 1" BY 8". AFT CARGO COMPT BS 1500 RBL 20 TO RT MOST O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: PLATE — DAMAGED (BS 920) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE-C M/D BS 920 RT TENSION TIE ATTACH STEEL PLATE 8EA RIVET HOLES FOUND ELONGATED. M/D BS 920 RT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE REPLACED IAW SRM 51-10-01 PG 9 AND INSTALLED IAW SRM 51-30-02.

Part: SHEAR WEB — CRACKED (BS 820-840 S10L) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE-C M/D BS820-840 STR10L STRINGER ATT SHEAR WEB FOUND CRACKED. CRACK LENGTH .7500 INCH AND .8750 INCH. M/D BS820-840 STR10L AREA SHEAR WEB REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02.

Part: SHEAR WEB — CRACKED (BS 820-840 S10R) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE-C M/D BS820-840 STR10R STRINGER ATT SHEAR WEB FOUND CRACK. CRACK LENGTH .7500 AND .5 INCH. M/D BS820-840 STR10R AREA SHEAR WEB REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02.

Part: TENSION TIE — CRACKED (BS 800) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C LEFT BS 800 FRAME TENSION TIE ATTACHMENT AREA 1EA FASTENERS HOLE FOUND CRACK AT AFT CHANNEL APPROX .125 INCH LONG AS MARKED. CRACK LENGTH .125 INCH. M/D BS 800 LEFT TENSION TIE AFT CHANNEL REPAIR AS PER RS R53-25-35643. CONTINUED INSPECTION IS REQUIRED AS PER RS R53-25-35643 AND UPS EO B747-5310-25512.

Part: ATTACH FITTING — CRACKED (BS 840) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C LEFT BS 840 FRAME TENSION TIE ATTACHMENT AREA ONE EACH FASTENER HOLE CRACK AT WEB DOUBLER APPROX .0625 INCH LONG RUNNING I/B AND LWR. M/D BS 840 LT FRAME ATTACH DOUBLER CRACKED HOLE OVERSIZED & FASTENER INSTALLED AS PER UPS EO B747-5310-23715 APP C AFTER CRACK FREE INSP BY HFEC INSP PER NTM PART 6 51-00-00 FIG 16. STEEL PLATE AND ALU STRAP REPAIRED AS PER R53-25-35653 REFER NRC50086 FOR DETAIL. CONTINUE INSP REQ'D PER RS R53-25-35653 & UPS EO B747-5310-25541-A.

Part: TENSION TIE — CRACKED (BS 840) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RT BS 840 FRAME TENSION TIE ATTACHMENT AREA FOUND 1EA FASTENER HOLE CRACK AT AFT CHANNEL APPROX 1/16 INCH LONG. M/D BS 840 RT TENSION TIE AFT CHANNEL O/B PORTION REPAIRED AS PER HX RS R53-25-35653 CONTINUE INSPECTION IS REQUIRED AS PER HX RS R53-25-35653 AND UPS EO B747-5310-25541-A.

Part: TENSION TIE — CRACKED (BS 820) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RT BS 820 FRAME TENSION TIE ATTACHMENT AREA ONE EACH FASTENER HOLE FOUND CRACK AT FWD CHANNEL APPROX 1/16 INCH IN LENGTH RUNNING I/B & LWR. M/D BS 820 RT TENSION TIE FWD O/B CHANNEL REPAIRED AS PER HX RS R53-25-35639. CONTINUED INSPECTION REQUIRED AS PER HX RS R53-25-35639 AND UPS EO B747-5310-25513-A.

Part: TENSION TIE — DAMAGED (BS 880) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 880 LEFT TENSION TIE O/B FWD CHANNEL 9 EA RIVET HOLES FOUND ELONGATED. *S/D* BS 880 LEFT TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35638 CONTINUE INSPECTION IS REQUIRED AS PER RS HX RS R53-25-35638 AND UPS EO B747-5310-25548-A.

Part: TENSION TIE — DAMAGED (BS 880) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 880 LT TENSION TIE O/B AFT CHANNEL 5EA RIVET HOLES FOUND ELONGATED. M/D BS 880 LT TENSION TIE AFT CHANNEL REPAIRED AS PER RS R53-25-35638 CONTINUE INSPECTION IS REQUIRED AS PER HX RS R53-25-35638 AND UPS EO B747-5310-25548-A.

Part: TENSION TIE — CRACKED (BS 780) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C BS 780 LT FRAME TENSION TIE ATTACHMENT AREA FASTENER HOLES FOUND CRACK AT AFT CHANNEL. CRACK LENGTH 1/16 INCH. M/D BS 780 LT TENSION TIE O/B AFT CHANNEL REPAIRED AS PER HX RS R53-25-35637. CONTINUED INSPECTION REQUIRED AS PER HX RS R53-25-35637 AND UPS EO B747-5310-25511-A.

Part: TENSION TIE — DAMAGED (BS 840) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 840 RT TENSION TIE O/B FWD CHANNEL 3EA RIVET HOLES FOUND ELONGATED. M/D BS 840 RT TENSION TIE O/B FWD CHANNEL REPAIRED AS PER HX RS R53-25-35653. CONTINUE INSPECTIONS ARE REQUIRED AS PER HX RS R53-25-35653 AND UPS EO B747-5310-25541-A.

Part: TENSION TIE — DAMAGED (BS 920) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 920 RT O/B TENSION TIE FWD CHANNEL 8 EA RIVET HOLES FOUND ELONGATED. M/D BS 920 RT TENSION TIE O/B FWD CHANNEL REPAIRED AS PER HX RS R53-25-35640. CONTINUED INSPECTION IS REQUIRED AS PER HX RS R53-25-35640 AND UPS EO B747-5310-25517-A.

Part: TENSION TIE — DAMAGED (BS 920) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE-C M/D BS 920 LT TENSION TIE OB FWD CHANNEL 1EA RIVET HOLE FOUND ELONGATED. M/D BS920 LT TENSION TIE OB FWD CHANNEL ELONGATED HOLE OVERSIZED TO 0.247 INCH DIA FASTENER INSTALLED IAW UPS EO B747-5310-23715 APP D AFTER HFEC INSPECTION IAW NTM PART 6 51-00-00 FIG 16 CRACK FREE.

Part: PLATE — MISMANUFACTURED (BS 840) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 840 LT TENSION TIE FWD STEEL PLATE UPPER AND LOWER ROW MOST I/B FASTENER HOLES SHORT OF EDGE MARGIN (2EA). M/D BS 840 LT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE & ALUMINUM STRAP REPAIRED AS PER HX RS R53-25-35653. CONTINUED INSP ARE REQUIRED AS PER HX RS R53-25-35653 AND UPS EO B747-5310-25541.

Part: TENSION TIE — CRACKED (BS 940) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 940 LT TENSION TIE O/B AFT CHANNEL O/B EDGE FOUND CRACK. CRACK LENGTH 3/8 INCH. M/D BS 940 LT TENSION TIE O/B AFT CHANNEL REPAIRED AS PER HX RS R53-25-35642 CONTINUE INSPECTION IS REQUIRED AS PER HX RS R53-25-35642 AND UPS EO B747-5310-25518-A.

Part: TENSION TIE — DAMAGED (BS 800) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 800 LEFT TENSION TIE O/B AFT CHANNEL 5EA RIVET HOLES FOUND ELONGATED. M/D BS 800 LEFT TENSION TIE AFT CHANNEL REPAIRED AS PER RS R53-25-35643, REFER NRC 50143 FOR WORKING DETAIL AND IAW UPS EO B747-5310-25512.

Part: PLATE — MISMANUFACTURED (BS 880) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 880R TENSION TIE FWD STEEL PLATE UPPER AND LOWER ROW MOST I/B FASTENER HOLE SHORT OF EDGE MARGIN (2EA). M/D BS 880 RT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE REPAIRED AS PER HX RS R53-25-35638 CONTINUE INSPECTIONS ARE REQUIRED AS PER HX RS R53-25-35638 AND UPS EO B747-5310-25548-A.

Part: PLATE — MISMANUFACTURED (BS 920) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 920 TENSION TIE FWD STEEL PLATE UPPER AND LOWER ROW MOST I/B FASTENER HOLE SHORT OF EDGE MARGIN (2EA). M/D BS 920 RT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE REPAIRED AS PER HX RS R53-25-35643 CONTINUED INSPECTION REQUIRED AS PER HX RS R53-25-35640 AND UPS EO B747-5310-25517-A.

Part: PLATE — MISMANUFACTURED (BS 840) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 840R TENSION TIE FWD STEEL PLATE UPPER & LOWER ROW MOST I/B FASTENER HOLE SHORT OF EDGE MARGIN (2EA). M/D BS 840 RT TENSION TIE FWD CHANNEL ATTACH STEEL PLATE REPAIRED AS PER HX RS R53-25-35653. CONTINUE INSPECTIONS ARE REQUIRED AS PER HX RS R53-25-35653 AND UPS EO B747-5310-25541-A.

Part: PLATE — MISMANUFACTURED (BS 800) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 800 RT TENSION TIE FWD STEEL PLATE UPPER AND LOWER ROW MOST I/B FASTENER HOLE SHORT OF EDGE MARGIN (SEM) 2 EACH. M/D BS 800 RT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE REPAIRED AS PER RS R53-25-35643. CONTINUED INSPECTION ARE REQUIRED AS PER RS R53-25-35643 AND UPS EO B747-5310-25512.

Part: SKIN — DENTED (LT MLG DOOR) · airframe 97,102 hrs · 24,042 cycles

INSPECTION TYPE:C LT LG O/B W/W DOOR SURFACE DENT MARK REVEALED. LT LG O/B W/W DOOR SKIN DENTED AREA REPAIRED AS PER SRM 52-80-02 FIG 1.

Part: TENSION TIE — DAMAGED (BS 800) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 800 LT TENSION TIE O/B FWD CHANNEL 8 EACH RIVET HOLES FOUND ELONGATED. M/D BS 800 LT TENSION TIE FWD CHANNEL REPAIRED PER RS R53-25-35643. CONTINUED INSPECTION REQUIRED AS PER RS R53-25-35643 AND UPS EO B747-5310-25512.

Part: FRAME — CRACKED (BS 820) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C RIGHT BS 820 FRAME TENSION TIE ATTACH AREA TWO EA FASTENER HOLE FOUND CRACK AT FRAME LAYER FOR DETAIL. CRACK LENGTH 0.040" CRACK LENGTH 0.040". M/D BS 820 RIGHT FRAME CRACKED TWO HOLES OVERSIZED BY 1/64" INCREMENT UP TO 0.309" DIA AS PER EO B747-5310-23715 APP D STEEL PLATE AND ALUMINUM STRAP REPAIRED AS PER RS R53-25-35639 REFER NRC 500289 FOR DETAIL. CONTINUED INSPECTION ARE REQUIRED AS PER RS R53-25-35639 AND EO B747-5310-25513-A.

Part: TENSION TIE — DAMAGED (BS 900) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 900 RT TENSION O/B FWD CHANNEL 4 EA RIVET HOLES FOUND ELONGATED. M/D BS 900 RT TENSION TIE FWD CHANNEL O/B PORTION REPAIRED AS PER HX RS R53-25-35641. CONTINUED INSPECTION IS REQUIRED AS PRE HX RS R53-25-35641 AND UPS EO B747-5310-25516-A.

Part: TENSION TIE — DAMAGED (BS 900) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 900 RT TENSION TIE O/B AFT CHANNEL 12 EA RIVET HOLES FOUND ELONGATED. M/D BS 900 RT TENSION TIE O/B AFT CHANNEL REPAIRED AS PER HX RS R53-25-35641. CONTINUED INSPECTION IS REQUIRED AS PER HX RS R53-25-35641 AND UPS EO B747-5310-25516-A.

Part: PLATE — MISMANUFACTURED (BS 860) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 860 LT TENSION TIE FWD STEEL PLATE LOWER ROW MOST I/B FASTENER HOLE SHORT OF EDGE MARGIN (1EA). M/D BS 860 LT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE REPAIRED AS PER HX RS R53-25-35645. CONTINUED INSPECTION REQUIRED AS PER HX RS R53-25-35645 AND UPS EO B747-5310-25514-A.

Part: PLATE — MISMANUFACTURED (BS 860) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 860 RT TENSION TIE FWD STEEL PLATE UPPER AND LOWER ROW MOST I/B FASTENER HOLE SHORT OF EDGE MARGIN (2EA). M/D BS 860 RT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE REPAIRED AS PER HX RS R53-25-35645. CONTINUED INSPECTION REQUIRED AS PER HX RS R53-25-35645 AND UPS EO B747-5310-25514-A.

Part: TENSION TIE — CRACKED (BS 780) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 780 LT TENSION TIE O/B AFT CHANNEL EDGE FOUND CRACK. CRACK LENGTH 3/8 INCH. M/D BS 780 LT TENSION TIE O/B AFT CHANNEL REPAIRED AS PER HX RS R53-25-35637. CONTINUED INSPECTION IS REQUIRED AS PER HX RS R53-25-35637 REFER NRC 500743 FOR WORKING DETAIL AND REF TO UPS EO B747-5310-25511-A.

Part: PLATE — MISMANUFACTURED (BS 900) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 900 RT TENSION TIE FWD STEEL PLATE UPPER AND LOWER ROW MOST I/B FASTENER HOLE SHORT OF EDGE MARGIN (2EA). M/D BS 900 RT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE REPAIRED AS PER HX RS R53-25-35641. CONTINUE INSPECTION ARE REQUIRED AS PER HX RS R53-25-35641 AND UPS EO B747-5310-25516-A.

Part: PLATE — MISMANUFACTURED (BS 900) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 900 LT TENSION TIE FWD STEEL PLATE LOWER ROW MOST I/B FASTENER HOLE SHORT OF EDGE MARGIN (1EA). M/D BS 900 LT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE REPAIRED AS PER HX RS R53-25-35641. CONTINUE INSPECTIONS ARE REQUIRED AS PER HX RS R53-25-35641 AND UPS EO B747-5310-25516-A.

Part: TENSION TIE — DAMAGED (BS 940) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 940 RT TENSION TIE O/B AFT CHANNEL 3 EA RIVET HOLES FOUND ELONGATED. M/D BS 940 RT TENSION TIE O/B AFT CHANNEL REPAIRED AS PER HX RS R53-25-35642. CONTINUE INSPECTION IS REQUIRED AS PER HX RS R53-25-35642 AND UPS EO B747-5310-25518-A.

Part: PLATE — MISMANUFACTURED (BS 940) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 940 RT TENSION TIE FWD STEEL PLATE UPPER ROW MOST I/B FASTENER HOLE SHORT OF EDGE MARGIN (1EA). M/D BS 940 RT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE REPAIRED AS PER HX RS R53-25-35642. CONTINUED INSPECTION REQUIRED AS PER HX RS R53-25-35642 AND UPS EO B747-5310-25518-A.

Part: PLATE — MISMANUFACTURED (BS 820) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 820 LT TENSION TIE FWD STEEL PLATE UPPER AND LOWER ROW MOST I/B FASTENER HOLE SHORT OF EDGE MARGIN (2EA). M/D BS 820 LT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE REPAIRED AS PER HX RS R53-25-35639. CONTINUED INSPECTION REQUIRED AS PER HX RS R53-25-35639 AND UPS EO B747-5310-25513-A.

Part: TENSION TIE — DAMAGED (BS 940) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 940 RT TENSION TIE O/B FWD CHANNEL 7 EA RIVET HOLES FOUND ELONGATED. M/D BS 940 RT TENSION TIE O/B FWD CHANNEL REPAIRED AS PER HX RS R53-25-35642 CONTINUE INSPECTION IS REQUIRED AS PER HX RS R53-25-35642 AND UPS EO B747-5310-25518-A.

Part: PLATE — MISMANUFACTURED (BS 820) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 820 RT TENSION TIE FWD STEEL PLATE LOWER ROW MOST I/B FASTENER HOLE SHORT OF EDGE MARGIN. M/D BS 820 RT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE REPAIRED AS PER HX RS R53-25-35639. CONTINUED INSPECTION REQUIRED AS PER HX RS R53-25-35639 AND UPS EO B747-5310-25513-A.

Part: TENSION TIE — MISMANUFACTURED (BS 820) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 820 RT TENSION TIE O/B FWD CHANNEL 5 EACH RIVETS HOLES FOUND ELONGATED. M/D BS 820 RT TENSION TIE O/B FWD CHANNEL REPAIRED AS PER HX RS R53-25-35639 REFER NRC 500735 FOR WORKING DETAIL. CONTINUED INSPECTION REQUIRED AS PER HX RS R53-25-35639.

Part: PLATE — MISMANUFACTURED (BS 780) · airframe 97,105 hrs · 24,042 cycles

INSPECTION TYPE:C M/D BS 780 RT TENSION TIE FWD STEEL PLATE UPPER ROW MOST I/B FASTENER HOLE SHORT OF EDGE MARGIN (1 EA). M/D BS 780 RT TENSION TIE FWD CHANNEL ATTACHED STEEL PLATE REPAIRED AS PER HX RS R53-25-35637. CONTINUED INSPECTION REQUIRED AS PER HX RS R53-25-35637 AND UPS EO B747-5310-25511-A.

Part: LIGHT — INOPERATIVE (CABIN)

STAIRWELL DOME EMERGENCY LIGHT INOP IN UPPER DECK. DEFERRED PER MEL 33-13. R&R BATTERY ASSY. STAIRWELL DOME EMERGENCY LIGHT. OPS CHECK GOOD. THIS CLEARS M334472.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

AFT SECTION EMERGENCY LIGHTS INOP UPPER DECK STATION 405. REPLACED EMERGENCY LIGHT BATTERY ASSY ON X328 (UPPER DECK LIGHT ASSY). OPS CHECK GOOD.

Part: ODOR — DETECTED (CABIN)

AFTER TURNING PACKS ON AFTER T/O BOTH CREW AND ACMS SMELLED AN ODOR. CREW CHECKED. UPPER AND MAIN DECK, FOUND NOTHING ABNORMAL. NOTICED NR 1 PK SHOWING NO AIR FLOW OR COMP DISCHARGE. WHEN NR 1 PK OFF, ODOR WENT AWAY. PLACED NR 1 PK CONTROL TO MANUAL. OPERATED NR 1 PACK, NO ODORS FOUND. FOUND AIR FLOW INDICATION FLUCTUATING W/PACKS OFF. DEF PACK AIRFLOW INDICATION PER MEL 21-11. ALL OTHER PARAMETERS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

N/A EMERG LIGHT AT CREW SERVICE DOOR INOP. EXIT LIGHT AT SLIDE WORKS NORMAL. REPLACED BATTERY PACK FOR EMER EXIT LIMITS. OPS CK OK. THIS CLEARS M331019. CLOSING LP 585036/2.

Part: ODOR — DETECTED (COCKPIT)

NEAR TOP OF DESCENT, STRONG BURNING SMELL IN COCKPIT. UNABLE TO FIND SOURCE, AND IT DISSIPATED (ELECTRICAL). GENERAL VISUAL INSPECTION OF COCKPIT, E/E AREA PERFORMED PER GMM-2 -2, NO IRREGULARITIES NOTED.

Part: RIB — CRACKED (RT WING)

FOUND 8 INCH CRACK ON LEADING EDGE OF RT WING ON FIRST RIB CAP OUTBD FUSELAGE. EXTERNAL DOUBLER REPAIR PER SRM 57-30-04 FIG 1. TIME LIMITED REPAIR PERMANENT FLUSH REPAIR NO LATER THAN 6 MONTHS.

Part: LANDING GEAR — INOPERATIVE (LEFT)

ATB - LEFT BODY GEAR WOULD NOT RETRACT. L BODY TILT LIGHTS, BOTH PRIM AND ALT ON. ALSO L/BODY GEAR DOOR LIGHTS BOTH PRIM AND ALT. ON GEAR WA S EXTENDED. NO CHAFED OR PINCHED WIRE REF WDM 32-61-21 PG 2 & 32-6 1-22 PG 1. COMPLIED W/ TECH BOW NO STEERING FAULTS OR LEAK. CYCLED L&R MAIN BODY GEAR 6 TIMES GOING TO OFF POS. & SHAKING WIRES & CARD FILE. NO FAULTS R&R L/H BODY MM32-13-15. AC OK FOR SERVICE. PRI & ALT SYS CK IN ALL SITUATIONS NOTED ABOVE. AC JACKED & LOWERED PER MM 07-11-01.

Part: PANEL — DELAMINATED (LEFT WING)

LEFT WING LOWER PANEL DELAMINATED OUTBOARD OF NR 3 CANOE. UNDER NR 5 SPOILER ACT, AREA MARKED. COMPLIED WITH EO B747-5720-23353A EXCEPT FOR INSTALLING FASTENERS ON LE OF PANE. REMOVED TEMP REPAIR PANEL SH 1199928 DRILLED UP NEW PANEL. INSTALLED RIVETS AND LOCK FASTENERS FWD EDGE AND SCREWS ON OB EDGE. REF SRM 51-30-12 SH 199928. INSTALLED BULB SEAL ON REAR OF PANEL 1439884. INSTALLED TIE REELS, THIS CLEARS D314807.

Part: LINK — CRACKED (NR 3 PYLON) · airframe 95,393 hrs · 23,626 cycles

INSPECTION TYPE:AD NR 3 ENGINE REAR MOUNT THRUST LINK CRACK INDICATION REVEALED AT FWD LUG UPPER SURFACE 80 PERCENT FSH & AFT UPPER SURFACE 50 PERCENT FSH BOTH EXCEED LIMIT. NR 3 ENG REAR MOUNT THRUST LINK CHANGED REF MM 71-21-03.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C NWW RT SIDE WALL PNL BS 300 WL 140-160 FOUND 3 EA FASTENER HOLES CRACKED AT VENT. BEAM INNER CHORD ALL APPROX .0625 INCH IN LENGTH. NWW RT SIDE WALL PNL BS 300 WL 140 TO 160 VERTICAL BEAM INNER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C NWW RT SIDE WALL PNL BS 300 TO BS 320 NR 4 HORIZONTAL STIFFENER (COUNT FROM TOP) 1 EA FASTENER HOLE FOUND CRACKED AS MARKED (CRACK LENGTH .0625 INCH). NWW RT SIDE WALL PNL BS 300 TO BS 320 NR 4 HORIZONTAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C NWW LT SIDE WALL PANEL BS 280 TO 300 NR 4 HORIZONTAL STIFFENER (COUNT FROM TOP) 1 EA FASTENER HOLE FOUND CRACKED (CRACK LENGTH .0625 INCH). NWW LT SIDE WALL PANEL BS 280 TO 300 NR 4 HORIZONTAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C NWW RT SIDE WALL PNL BS 280 TO BS 300 NR 3 HORIZONTAL STIFFENER (COUNT FROM TOP) 2 EA FASTENER HOLES FOUND CRACKED AS MARKED (CRACK LENGTH .0625 INCH). NWW RT SIDE WALL PNL BS 280 TO BS 300 NR 3 HORIZONTAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C NWW LT SIDE WALL PNL BS 300 WL 140-160 4 EA FASTENER HOLES FOUND CRACKED AT VERTICAL BEAM INNER CHORD ALL CRACKS APPROX .0625 INCH IN LENGTH. NWW LT SIDE PANEL BS 300 WL 140-160 VERTICAL BEAM INNER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C NWW LT SIDE WALL PANEL BS 280 TO 300 NR 3 HORIZONTAL STIFFENER (COUNT FROM TOP) 1 EA FASTENER HOLE FOUND CRACKED (CRACK LENGTH .0625 INCH). NWW LT SIDE WALL PANEL BS 280 TO 300 NR 3 HORIZONTAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C NWW LT SIDE WALL PANEL BS 300 TO 320 NR 3 HORIZONTAL STIFFENER (COUNT FROM TOP) 1 EA FASTENER HOLE FOUND CRACKED (CRACK LENGTH .0625 INCH). NWW LT SIDE WALL PANEL BS 300 TO 320 NR 3 HORIZONTAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C NWW RT SIDE WALL PNL BS 300 TO BS 320 NR 3 HORIZONTAL STIFFENER (COUNT FROM TOP) 1EA FASTENER HOLE FOUND CRACKED AS MARKED (CRACK LENGTH .0625 INCH). NWW RT SIDE WALL PNL BS 300 TO BS 320 NR 3 HORIZONTAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C U/D - STA 600 FRAME CRACKED AT STRINGER S-8R AREA (CRACK LENGTH .5 INCH). U/D STA 600 AT STRINGER S-8R FRAME REPAIRED AS PER SRM 53-10-04 FIG 54.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D-BS 742, S 3AL STRINGER END FOUND CRACK AS MARKED. ( CRACK LENGTH 1.5 INCHES ) M/D BS 742 STR 3AL STRINGER REPAIRED IAW SRM 53-10-03 FIG 10.

Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C CABIN - U/D BS 380 FWD FLANGE OF FLOORBEAM FLOOR PANEL ATT HOLES SHORT EDGE MARGIN FOUND AT RBL 39, 40 & 41 AREA. CABIN - U/D BS 380 FWD FLANGE OF FLOORBEAM RBL 39, 40 & 41 AREA REPAIRED AS PER UPS EO B747-5320-12407 APPENDIX D PLAN C.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE: C, M/D BS 700 LBL 78 TIE DOWN FITTING FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.020 X 1 X 1.25 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 700 LBL 78 TIE DOWN FITTING REPLACED AS PER MM 20-51-01.

Part: CARGO TRACK — CORRODED (FUSELAEG) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE: C, M/D BS 800 LBL 55 TIE DOWN FITTING FLANGE CORRODED. CORROSION BLEND OUT 0.026 X .875 X 1.125 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 800 LBL 55 TIE DOWN FITTING REPLACED AS PER MM 20-50-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C U/D STA 640 STRINGER S-9R END CRACKED. (CRACK LENGTH .4375 INCH). U/D - BS 640 STRINGER 9R REPAIRED IAW SRM 53-10-03 FIG 2.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C U/D - LT SIDE BS 620 STR END S-9L CRACKED. ( CRACK LENGTH .4375 INCH ) U/D - LT SIDE BS 620 STR - 9L REPAIRED IAW SRM 53-10-03 FIG 2.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C M/D BS 742 STR 8L STRINGER END FOUND CRACK AS MARKED. ( CRACK LENGTH 3 INCHES). M/D BS 741 TO BS 770 STR 8L AREA STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C U/D STA 560 STRINGER S-9R END CRACKED. ( CRACK LENGTH .4375 INCH ) U/D - BS 560 STR -9R REPAIRED IAW SRM 53-10-03 FIG 2.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C U/D - LT SIDE BS 640 STR END S-9L CRACKED ( CRACK LENGTH 1INCH ) U/D LT SIDE BS 640 STR 9L REPAIRED IAW SRM 53-10-03 FIG 2.

Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C CABIN - U/D BS 380 FWD FLANGE OF FLOORBEAM FLOOR PANEL ATT HOLES SHORT EDGE MARGIN FOUND AT RBL 55 & 65 AREA. CABIN - U/D BS 380 FLOORBEAM FWD FLANGE RBL 55 & 65 REPAIRED AS PER UPS EO B747-5320-12407 APPENDIX D PLAN -C-.

Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C CABIN - U/D FLR BEAM BS 340 FWD FLANGE RBL 40 INCHES SHORT EDGE MARGIN FOUND AT CLIP NUT HOLES AREA. CABIN - U/D BS 340 FLR BEAM FWD FLANGE RBL 40 INCH AREA REPAIRED IAW EO B747-5320-12407-D PLAN C.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C M/D BS 742 STR 10L STR END FOUND CRACK AS MARKED, (CRACK LENGTH 2.75 INCHES). M/D BS 741 TO BS 770 STR 10L AREA STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C CABIN- U/D BS 380 FWD FLANGE OF FLOORBEAM FLOOR PANEL ATT. HOLES SHORT EDGE MARGIN FOUND AT RBL 20 INCHES AND 24.5 INCHES. CABIN - U/D BS 380 FLOORBEAM FWD FLANGE RBL 20 INCHES AND 24.5 INCHES AREA REPAIRED IAW EO B747-5320-12407-D PLAN C.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 860 LBL 84 FLOORBEAM CORROSION. CORROSION BLENDED OUT, EXCEED SRM 53-10-01 FIG 1 LIMITS, REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 800 RBL 75-80 FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION BLENDED OUT. EXCEEDED SRM 53-10-01 FIG 1 LIMITS, M/D BS 800 RBL 75-80 FLOORBEAM UPPER TEE REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 770- 800 RBL 11 SEAT TRACK I/B FLANGE CORROSION. CORROSION BLENDED OUT. EXCEEDED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D BS 550 LBL 11 - 33 FLOOR SUPPORT HAT SECTION FOUND CORROSION. CORROSION BLEND OUT 0.012 X .875 X 1.75 INCH HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (NLG WW) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C RT SIDE NWW SIDE PANEL AT BS 280-300 NR 2 STIFFENER (COUNT FROM TOP) FOUND RADIUS CRACKED APPROX 1.25 INCH LONG RUNNING FROM FWD EDGE (CRACK LENGTH 1.25 INCH). STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D - BS 756 RBL 33 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLEND OUT 0.039 X .875 X 1.25 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, M/D BS 670 - 770 RBL 33 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C, M/D BS 640 RBL 40-60 FLOORBEAM CORROSION. CORROSION BLEND OUT 0.063 BY 1.0 BY 2.0. EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D BS 640 RBL 43 TO RBL 66 FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D BS 909 LBL 11 - 33 HAT SECTION SUPPORT CORRODED. CORROSION BLEND OUT: 0.015 X .875 X 1.25 INCH. HAT SECTION SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D BS 570 LBL 11 - 33 FLOOR SUPPORT HAT SECTION FOUND CORRODED. CORROSION BLEND OUT: 0.011 X 1 X 1.5 INCH HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C, BS 860 RBL 60 CARGO HANDLING FITTING SUPPORT PLATE FOUND CORROSION. CORROSION BLEND OUT 0.023 X .875 X 1.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 860 RBL 60 TIE DOWN FITTING REPLACED AS PER MM 20-51-01.

Part: SKIN — CRACKED (RT WING) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C RIGHT WING BS 1241 UPPER REAR SPAR BOLT HOLE NR 5 UPPER SKIN AND CHORD FOUND CRACKED (CRACK LENGTH 0.030 / 0.060 INCH). HOLE REWORKED AS PER EO B747-5740-17032-C.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D - BS 860 LBL 75 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLEND OUT: 0.021 X 1 X 1.75 INCH. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A FROM BS 850 - 870 LBL 75 INCH.

Part: SEAT TRACK — CORRUPTED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D- BS 520-540 LBL 86 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLEND OUT 0.018 X .5 X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A FROM BS 480-570 LBL 86.

Part: RIB — CRACKED (RT WING) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C RIGHT WING BS 1241 UPPER REAR SPAR SPLICE BOLT HOLE NR 9 FOUND CRACKED AT RIB CHORD (CRACK LENGTH 0.040 INCH). HOLE REWORKED AS PER EO B747-5740-17032-C.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C, RT SIDE NWW SIDE PANEL AT BS 320 - 340 NR 6 STIFFENER (COUNTED FROM TOP) FOUND RADIUS CRACKED (CRACKED LENGTH .375 INCH). RT SIDE NWW SIDE PANEL AT BS 320 - 340 NR 6 STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C LT SIDE NWW SIDE PANEL AT BS 300-320 NR 4 STIFFENER (COUNT FROM TOP) FOUND RADIUS CRACKED APPROX .5625 INCH LONG RUNNING FROM FWD EDGE AS MARKED. LT SIDE NWW SIDE PANEL AT BS 300-320 NR 4 STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 830 RBL 11 SEAT TRACK FLANGE CORRODED. CORROSION BLENDED OUT. EXCEEDED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 890-910 RBL 11 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLEND OUT 0.025 BY 0.5 BY 3.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, M/D BS 890 - BS 1000 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14 WORK DETAIL REF NRC NR 6392.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D - BS 520, LBL 11, TIE DOWN TRACK FOUND HEAVY CORROSION CRACK (CRACK LENGTH 2.5 X 1 INCH). TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D BS 742 S-9L STRINGER END FOUND CRACKED. CRACK LENGTH 2.875 INCH. M/D BS 742 STR -9L TO BS 770 STR 9L AREA STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4.

Part: STRINGER — CORRODED (AFT CARGO) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C AFT CARGO COMPT BS 1645 STR 35R STRINGER CORRODED. CORROSION BLENDED OUT 0.039 INCHES BY 0.25 INCHES BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. AFT CARGO COMPT BS 1645 STR 35R REPAIRED AS PER SRM 53-10-03 FIG 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D - BS 630-670 RBL 11 TIE DOWN TRACK CROWN & FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.025 X .5 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 630-770 RBL 11 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE: C M/D - BS 782 RBL 33 SEAT TRACK IB FLANGE COR. CORROSION BLEND OUT 0.022 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D - RBL 33 INCH SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 1A BTN BS 770-810.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D- BS 760-780 RBL 75 TIE DOWN TRACK FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.029 X .5 X 4 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 750-870 RBL 75 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 720-740 LBL 75 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLENDED OUT. EXCEEDED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A FROM BS 670-770 LBL 75.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D - BS 728, RBL 11 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLEND OUT 0.025 X .75 X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D - BS 630 - BS 770 RBL 11 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 94,338 hrs · 23,406 cycles

BS 550- 570 LBL 32 TIE DOWN TRACK FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.048 BY 0.4375 BY 1.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D- BS 640 - 660 RBL 75 SEAT TRACK I/B FLANGE CORROSION CRACKED (CRACK LENGTH 1 INCH CORROSION CRACK). M/D BS 640-670 RBL 75 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SPLICE — CRACKED (LT WING) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C LEFT BS 1241 WING REAR SPAR UPPER SPLICE BOLT HOLE NR 8 CRACKED AT CHORD (CRACK LENGTH 0.08 INCH). HOLE REWORKED AS PER EO B747-5740-17032-C.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D - BS 550 LBL 11 - RBL 11 FLOOR SUPPORT HAT SECTION FOUND CORROSION BLEND OUT: 0.016 X 1 X 1.5 INCH. HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D - BS 860-980 RBL 97 SEAT TRACK I/B FLANGE CORRODED. CORROSION BLEND OUT: 0.028 X 1 X 2 INCH. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A FROM BS 850-990 RBL 97 INCH.

Part: SEAT TRACK — CORRODED (MAIN DECK) · airframe 94,338 hrs · 23,406 cycles

BS 778 LBL 33 SEAT TRACK I/B FLANGE CORRODED. CORROSION BLEND OUT 0.026 BY 0.5 BY 0.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A FROM BS 770-810 LBL 33.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 525-610 RBL 11 TIE DOWN TRACK FLANGE ANCHOR NUTS AREA FOUND CORROSION. CORROSION BLEND OUT 0.025 BY 1.0 BY 9.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D BS 510- BS 630 RBL 11 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: SEAT TRACK — CORRODED (FUSLEAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE: C M/D - BS 600-640 LBL 90 SEAT TRACK OB FLANGE COR. CORROSION BLEND OUT 0.034 INCH X .8750 INCH X 0.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 1A AT BS 570-640 LBL 90.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D BS 570 RBL 11-33 FLOOR SUPPORT HAT SECTION FOUND CORRODED. CORROSION BLEND OUT: 0.026 X .875 X 1.25 INCH. HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9.

Part: STRINGER — CRACKED (CARGO BAY) · airframe 94,338 hrs · 23,406 cycles

BS 2185 S35R STRINGER CORROSION CRACK. STRINGER 35R REPAIRED AS PER SRM 53-10-03 FIG 1 AND SPLICE REINSTALLED AS PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D - BS 680-700 RBL 11 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLEND OUT 0.024 X .5 X 5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 630-770 RBL 11 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: STRINGER CLIP — CRACKED (CARGO BAY) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C AFT CARGO COMPT BS 1920 S40L TIE CLIP CRACKED. (CRACK LENGTH .3750 INCH) AFT CARGO COMPT BS 1920 STR 40L TIE CLIP REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9.

Part: STRINGER — CORRODED (AFT CARGO) · airframe 94,338 hrs · 23,406 cycles

AFT CARGO COMPT, BS 1737 S-35R STRINGER END CORRODED. CORROSION BLEND OUT 0.020 BY 1.0 BY 1.75 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER SPLICE REPLACED AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D- BS 1000-1100 LBL 11 SEAT TRACK SURFACE CORRODED AS MARKED. CORROSION BLEND OUT 0.036 X .875 X 2.25 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D- BS 1000-1110 AND BS 1110-1150 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34.

Part: SPLICE PLATE — CORRODED (FLOORBEAM) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D- BS 860 LBL 95 - 113 FLOORBEAM UPPER SURFACE SPLICE PLATE CORRODED. CORROSION BLEND OUT 0.015 X 1.5 X 1.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, SPLICE PLATE REPLACED AS PER SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (FWD CARGO) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C FWD CARGO COMPT BS 400 RBL 1 INCH BULKHEAD STIFFENER CRACKED BELOW MEC FLR (CRACK LENGTH .375 INCH). FWD CARGO COMPT BS 400 RBL 1 INCH BULKHEAD STIFFENER REPLACED AS PER SRM 51-10-01 PG 9, (JUST BELOW MEC FLOOR).

Part: STRINGER — CRACKED (CARGO BAY) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C FWD CARGO COMPT STR 39L CRACKED AT BS 745 (CRACK LENGTH 1.25 INCH). FWD CARGO COMPT BS 755 TO 770 STR 39L REPAIRED AS PER SRM 53-10-03 FIG 1 & STRINGER SPLICE REINSTALLED AFTER REPAIRED AS PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 910-940 RBL 11 SEAT TRACK FLANGE CORROSION. CORROSION BLEND OUT 0.022 BY 1.0 BY 4.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D BS 890 - BS 1000 RBL 11 SEAT TRACK. REPAIRED AS PER SRM 53-10-05 FIG 14 WORK DETAIL REF NRC 6392.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C U/D- BS 420-440 BL 0 FLOOR (L) SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.033 INCH X .7500 INCH X 1INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, U/D BS 420-440 BL 0 FLOOR (L) SUPPORT REPLACED IAW SRM 51-10-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 980 LBL 75-98 BELOW FLOOR VERT WEB BASE FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.019 BY 0.5 BY 1.75 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, BS 980 FLOORBEAM LOWER CAP ATTACH ANGLE REPLACED AT LBL 75 - LBL 117. AREA AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D- BS 862 RBL 74 SEAT TRACK FLANGE CORROSION. CORROSION BLEND OUT 0.035 X 1.5 X 1.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 750-870 RBL 75 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FRAME — CRACKED (CARGO BAY) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C FWD CARGO COMPT BS 660 S37L - 38L FRAME CRACKED (CRACK LENGTH 8.25 INCH). FWD CARGO COMPT - BS 660 BETWEEN S37L AND S38L FRAME REPAIRED AS PER SRM 53-10-04 FIG 52.

Part: SHEAR TIE — CORRODED (FWD CARGO) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C FWD CARGO BS 900 STR 46R- 47R FWD SHEAR TIE FOUND CORRODED. CORROSION BLEND OUT 0.036 INCH BY 0.75 INCH BY 2.0 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. FWD CARGO BS 900 STR 46R - 47R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A.

Part: STIFFENER — CORRODED (FUSLEAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C FWD CARGO COMPT - BS 295 WL 130 LT NWW VERTICAL WALL STIFFENER CORRODED. CORROSION BLEND OUT 0.058 X 0.5 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.

Part: STRINGER — CORRODED (FWD CARGO) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C FWD CARGO COMPT STR 47L CORRODED AT BS 745. CORROSION BLEND OUT 0.021 INCH BY 0.875 INCH BY 2.0 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, FWD CARGO COMPT - BS 740 - BS 760 STR 47L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 1090 LBL 11 - RBL 11 FLOOR SUPPORT CORROSION. CORROSION BLEND OUT 0.052 BY 1.125 BY 1.75 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, M/D BS 1090 LBL 11 - RBL 11 FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE: C FWD CARGO BS 960-980 STR 47R FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.075 INCH X .7500 INCH X 1.75 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, FWD CARGO COMPT - BS 970-980 STR 47R STRINGER REPAIRED IAW SRM 53-10-03 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 1170 LBL 11- RBL 11 FLOOR SUPPORT CORROSION. CORROSION BLEND OUT 0.036 BY 1.215 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D - BS 1170 LBL 11 - RBL 11 FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.

Part: WEB — CORRODED (AFT CARGO) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C AFT CARGO COMPT BS 1794 S34R CLOSURE WEB CORRODED. CORROSION BLEND OUT 0.019 INCH BY 0.75 INCH BY 1.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, WEB REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: SEAT TRACK — CORRODED (MAIN DECK) · airframe 94,338 hrs · 23,406 cycles

BS 1000-1060 RBL 10 SEAT TRACK FLANGE CORROSION. CORROSION BLEND OUT 0.028 BY 1.0 BY 1.0. EXCEED SRM 53-10-01 FIG 1 LIMIT, M/D BS 1000-1130 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 980-1000 RBL 11 INCH SEAT TRACK FLANGE CORROSION. CORROSION BLEND OUT 0.060 BY 0.875 BY 2.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, M/D BS 890 - BS 1000 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C BULK CARGO COMPT - BS 1924 S32R STRINGER END CORRODED. CORROSION BLEND OUT 0.040 INCH X .8750 INCH X 1INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. BULK CARGO COMPT - BS 1924 S-32R STRINGER REPAIRED IAW SRM 53-10-01 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

BS 900-920 RBL 12 SEAT TRACK FLANGE CORROSION. CORROSION BLEND OUT 0.020 BY 1.0 BY 3.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMIT, M/D BS 890- BS 1000 RBL 11 SEAT TRACK. REPAIRED AS PER SRM 53-10-05 FIG 14 WORK DETAIL REF NRC 6392.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C U/D BS 660-710 RBL 48, SEAT TRACK CROWN HI-LOCK AREA FOUND CORROSION. CORROSION BLENDED OUT 0.045 INCH BY 0.5 INCH BY 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. U/D BS 650 TO 720 RBL 48 INCH TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: SPAR — CORRODED (RT WING) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C RIGHT BS 1241 WING UPPER REAR SPAR NR 3 BOLT HOLE FOUND CORROSION. HOLE REWORKED AS PER EO B747-5740-17032-C. HOLE OVERSIZED TO 1 INCH.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE: C U/D - BS 520-530 RBL 82, FLR SUPPORT (L) ANGLE LWR FACE FOUND CORROSION. CORROSION BLEND OUT 0.025 INCH X .8750 INCH X 2 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 520-530 RBL 82 INCH FLR SUPPORT (L) ANGLE REPAIRED IAW SRM 51-40-04 FIG 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C AFT CARGO COMPT BS 1560 STR 34L FRAME INNER CHORD CRACKED (CRACK LENGTH 10.5 APPROX). AFT CARGO COMPT BS 1560 STR 32L TO STR 38L FRAME REPAIRED AS PER HX RS R53-62-35312 CONTINUED INSPECTION REQUIRE TO THE REPAIR AREA PER SB 747-53A2349 REV 2 & UPS EO B747-5310-22293-A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D- BS 1040-1090 LBL 10 SEAT TRACK FLANGE CORROSION. CORROSION BLEND OUT 0.040 X 1 X 1.75 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 1000-1110 LBL 10 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D - BS 2180 - 2200 STR 11L STRINGER END FOUND CRACKED (CRACK LENGTH .75 INCH). M/D - BS 2180 - 2210 STR 11L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C, M/D BS 660 STR 24L CUTOUT CRACKED, (CRACK LENGTH 0.5 IN). M/D BS 660 STRINGER 24L, CUTOUT FRAME REPAIRED AS PER SRM 53-10-04 FIG 35.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C FWD CARGO COMPT - LT TUNNEL BS 295 WL 130 NWW VERTICAL WALL ANGLE FWD SURFACE CORROSION. CORROSION BLEND OUT 0.015 X 1 X 4 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, FWD CARGO COMPT - LT TUNNEL BS 295 WL 130 VERTICAL WALL ANGLE REPLACED AS PER SRM 51-10-01 PG 9.

Part: WEB — CRACKED (BLEED AIR DUCT) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C LT BS 1480 APU BLEED AIR DUCT CUTOUT CRACK FOUND 1EA FASTENER HOLE APPROX 0.0625 INCH IN LENGTH . LT BS 1480 APU BLEED AIR DUCT CUTOUT REPAIRED AS PER UPS EO NR B747-5310-3100-C AND DWG 144U2602.

Part: PLATE — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D BS 1100 RBL 75 TIE DOWN FTG ATT PLATE FOUND CORRODED. CORROSION BLEND OUT 0.028 INCH X 1.5 INCH X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, M/D BS 1100 RBL 75 INCH TIE DOWN FTG ATT PLATE REPLACED IAW SRM 51-10-01 PG 9.

Part: FRAME — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C AFT CARGO COMPT BS 1500 STR 33L FRAME INNER FLANGE CRACKED (CRACK LENGTH 9 INCH APPROX). AFT CARGO COMPT BS 1500 STR 32L TO 38L INNER FLANGE REPAIRED AS PER HX RS R53-62-35311 CONTINUED INSPECTION REQUIRE TO THE REPAIR AREA PER SB 747-53A2349 REV 2 & UPS EO B747-5310-22294-A.

Part: SEAT TRACK — CORRODED (MAIN DECK) · airframe 94,338 hrs · 23,406 cycles

M/D BS 1130-1140 RBL 11 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.063 BY 1.5 BY 2.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 1130 TO 1265 RBL 11 TRACK REPAIRED AS PER SRM 53-10-05 FIG 34.

Part: SEAT TRACK — CORRODED (MAIN DECK) · airframe 94,338 hrs · 23,406 cycles

BS 1140 - 1265 RBL 11 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.052 BY 1.5 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, M/D -BS 1130-1265 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34.

Part: FLOORBEAM — CRACKED (FUSLEAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C M/D BS 1220 RBL 105 FLOORBEAM WEB FOUND CRACKED. ( 0.5 INCH) M/D - BS 1220 RBL 105 INCHES FLR BEAM WEB REPAIRED IAW SRM 51-40-02 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE: C, BS 1100 RBL 80-95 FLOORBEAM, FOUND CORRODED. CORROSION BLENDED OUT FLOORBEAM UPPER TEE REPLACED AS PER SRM 51-10-01 PG 9.

Part: LAP JOINT — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C FX SKIN LAP JOINT FOUND CORROSION AT BS 398 - 400 STR 19L AROUND 2 EA FASTENERS AS MARKED (APPROX 15 PERCENT MATERIAL LOSS). CORROSION BLEND OUT 0.016 X 1.125 X 2.25 INCH EXCEED EO B747-5330-20503-D LIMITS. FX BS 388 TO BS 400 STR 19L SKIN REPAIRED AS PER HX RS R53-11-35313 & UPS EO B747-5330-22315-A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C FX- SKIN LAP JOINT FOUND CORRODED AT BS 379-381 STR 23L AROUND 2EA FASTENERS AS MARKED (APPROX 15 PERCENT MATERIAL LOSS). CORROSION BLEND OUT 0.011 BY 0.875 BY 1.75 INCHES. EXCEED EO NR B747-5330-20503-D LIMIT. FX SKIN LAP JOINT REPAIRED AS PER SRM 53-30-03 FIG 26 FROM BS 375-38L BTN STR 22L - STR 23L.

Part: SKIN — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE: C EMP - STA 2638 BETWEEN S-7L AND S-8L EXT. SKIN CRACKED APPROX 10 INCHES ( CRACK LENGTH 10 INCHES ) EMP - BS 2638 BETWEEN S-7L & S-8L SKIN REPAIRED IAW SRM 53-30-03 FIG 1A.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C, M/D - BS 460 RT FLOORBEAM WEB FOUND CRACKED AT STR 13R RBL 98 AREA, (CRACK LENGTH 0.3750 IN). FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11.

Part: SUPPORT — CRACKED (AFT CARGO) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE: C AFT CARGO COMPT - BS 1914 LBL 25 AND LBL 47 AFT FIXED END STOP LWR SUPPORT CRACKED. ( CRACK LENGTH .7500 INCH TO 1INCH ) AFT CARGO COMPT - BS 1914 LBL 25 AND LBL 47 AFT FIXED END STOP LWR SUPPORT REPAIRED IAW SRM 51-40-03 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C LT WING NR 7 VC FLAP O/B ARM I/B SUPPORT RIB FWD VERTICAL FLANGE FASTENER HOLE CRACKED (CRACK LENGTH 1 INCH). LT WING NR 7 VC FLAP O/B ARM I/B SUPPORT RIB FWD VERTICAL FLANGE REPAIRED AS PER HX RS R57-41-35307 DETAIL VISUAL INSPECT AT 6 MONTH INTERNAL FOR CRACKING, ELONGATED HOLES MISSING OR LOSE FASTENERS CORROSION OR OTHER SIGN OF DAMAGE.

Part: RIB — CRACKED (LT WING) · airframe 94,338 hrs · 23,406 cycles

INSP TYPE: C, LT WING UPPER T/E PANEL SUPPORT RIB UPPER CHORD CRACKED REVEALED AT WBL 445.8 INCHES FWD OF I/B AILERON I/B EDGE (CRACK LENGTH 0.5 INCH). LT WING UPPER T/E PANEL SUPPORT RIB UPPER CHORD REPLACED AS PER SRM 51-10-01 PG 9.

Part: SKIN — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

SKIN AT BS 396-397 S23R FOUND 1 TOP ROW FASTENER AREA FOUND CORRODED. CORROSION BLENDED OUT. EXCEEDED EO B747-5330-20503-D LIMITS. FX SKIN BS 388 TO BS 400 STR 23R SKIN REPAIRED AS PER SRM 53-30-03 FIG 26.

Part: RIB — CRACKED (LOT WING) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C LT WING NR 5 VC FLAP O/B ARM O/B SUPPORT RIB I/B FACE D-HOLE CRACKED. (CRACK LENGTH .5 INCH). LT WING NR 5 VC FLAP O/B ARM O/B SUPPORT RIB I/B AREA REPAIRED AS PER HX RS R57-41-35308 DETAIL VISUAL INSPECT AT EALIER OF C-CHECK OR 18 MONTH INTERNALS REQUIRE REF UPS EO B747-5740-22314-A.

Part: RIB — CRACKED (RT WING) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C RT WING NR 19 VC FLAP I/B ARM O/B SUPPORT RIB FWD VERTICAL FLANGE FASTENER HOLES FOUND CRACKED (CRACK LENGTH 1 INCH). RT WING NR 19 VC FLAP I/B ARM O/B SUPPORT RIB FWD VERTICAL FLANGE REPAIRED AS PER HX RS R57-41-35307. DETAIL VISUAL INSPECT AT 6 MONTH INTERVALS FOR CRACKING, ELONGATED HOLES MISSING OR LOSE FASTENERS CORROSION OR OTHER OF DAMAGE.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C NLG W/W RIGHT SIDEWALL NR 2 STRIP BLUGED AT BS 280 AS MARK (COUNT FROM TOP, CRACK LENGTH 1.5 INCH). NLG W/W RIGHT SIDEWALL BS 270 TO BS 290 WL 170 WEB REPAIRED AS PER SRM 53-10-04 FIG 116.

Part: BULKHEAD — CORRODED (RT MLG WW) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE:C, RT WLG W/W FWD BULKHEAD LOWER AREA CORROSION REVEALED AT STA 1241 RBL 75-99. CORROSION BLEND OUT 0.063 X .875 X 1.25 INCH EXCEED SRM 57-10-01 FIG 1 LIMITS. RT WLG W/W FWD BULKHEAD LOWER AREA RBL 75-99 AREA CORROSION REMOVED & REPAIRED AS PER HX RS R57-12-35310 & UPS EO B747-5710-22305-A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 94,338 hrs · 23,406 cycles

INSPECTION TYPE: C, AT BS 1681 STR 46R LAP JOINT MID ROW FASTENER (ONE EACH) FOUND SKIN BULGE UP (CORROSION BLEND OUT 0.019 X 0.5 X 1.5 INCH). FUSELAGE BS 1676 TO BS 1688 STR 46R AREA SKIN REPAIRED WITH ZERO-TIME FASTENER HOLES OVERSIZED AT CRITICAL ROW AREA AS PER SRM 53-30-03 FIG 17. SUBSEQUENT INSPECTION ARE NECESSARY FOR CATEGORY-B REPAIR REF TO SRM 53-30-03 FIG 17.

Part: STIFFENER — CRACKED (KEELBEAM) · airframe 94,338 hrs · 23,406 cycles

FX AIR CONDITIONING BAY LT KEELBEAM BOX EXTERNAL SURFACE VERTICAL WEB ATTACH STIFFENER FOUND CRACKED AT STA 983 LBL 9 WL 95 INCH (CRACK LENGTH .500) FX AIR CONDITIONING BAY LT KEELBEAM BOX EXTERNAL SURFACE VERTICAL WEB ATTACH STIFFENER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 94,338 hrs · 23,406 cycles

LT MLG WW APU BLEED AIR DUCT CUTOUT CRACKED AT 2 AND 7 O'CLOCK POSITION AT STA 1480 (CRACK LENGTH 2.5 IN). LT MLG WW AREA BLEED AIR DUCT CUTOUT REPAIRED AS PER UPS EO B747-5310-3100-C AND DWG 144U2602.

Part: LIGHT — INOPERATIVE (MAIN DECK)

MAIN DECK FWD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECKED OK.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

INSPECTION TYPE:A CHECK, EMERGENCY LIGHT AT STA 570 LT AND L1 DOOR AFT SILL LIGHT IS EXTREMELY DIM. REPLACED BATTERY PACK LIGHT, OPS CHECK OK.

Part: CRASH AX — DAMAGED (EMERGENCY EQUIP)

CRASH AX NEEDS TO HAVE DEFECTS BLENDED. REMOVED AND REPLACED CRASH AX WITH SERVICEABLE PART OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A CREW SERVICE DOOR EMERGENCY SILL LIGHTS INOPERATIVE. REPLACED X327 EMERGENCY LIGHT BATTERY POWER UNIT FOR X-326 AND X325, LIGHTS OPS CHECKS GOOD.

Part: ACM — DAMAGED (NR 3)

ATB - SMOKE & FUMES FROM CASPER FOLLOWED BY VIBRATION WHICH CONTINUED AFTER PACKS SECURED UNTIL ACFT DEPRESSURATION. FOUND NR 3 ACM HEAVELY DAMAGED & CAUSE SMOKE. REMOVED AND REPLACED NR 3 ACM AND OPS CHECK OK IAW AMM 21-51-04 P401.

Part: BATTERY PACK — INOPERATIVE (ESCAPE SLIDE)

EMERGENCY EXIT LIGHTS IN RIGHT ESCAPE SLIDE DOOR FRAME INOP. REMOVED AND REPLACED BATTERY PACK PER MM 33-51-04, OPS CHECK GOOD.

Part: RIB — CORRODED (LT WING TE FLAP) · airframe 91,214 hrs · 22,751 cycles

LEFT WING L/E NR 2 VC FLAP O/B ROTARY ACTUATOR SUPPORT RIB MOUNTING HOLE NR 2, 3, 4 AND NR 1 BORE FOUND SURFACE CORRODED (LOOKING O/B). LEFT WING L/E NR 2 V/C FLAP O/B ROTARY ACTUATOR SUPPORT RIB REPLACED PER SRM 51-10-01 PG 8. NR 2 V/C FLAP REF MM 27-81-02 RIGGING AND OPERATION CHECK CARRIED OUT PER MM 27-81-00. CORROSION BLEND OUT FINAL SIZE 0.434 INCH DIA OUT HOLES NR 2 TO NR 4 OLES 1453 .25.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE:C- BS 680 - 700 LBL 78 LONGITUDINAL FLOOR SUPPORT WEB FOUND CRACKED AS MARKED. DEFECTIVE AREA WEB REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C - AFT FUSELAGE SKIN AT BS 2365 - 2385 LT STR 3. THE DEPTH OF WEAR IN FUSELAGE SKIN HAS EXCEEDED EO B747-5330-18431 LIMIT AFT BLEND OUT. DEFECTIVE AREA SKIN REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1A.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, FWD CARGO COMPT BILGE SKIN SHEAR T/E FOUND CORRODED AT THE AREA BETWEEN STR 46 - 47 APPROX RBL 7 FRAME BS 540. SHEAR TIE REPLACED AS PER SRM 51-10-01. THE CORRODED AREA OF THE SHEAR TIE WAS DEPTH 0.050 INCH X LENGTH 3 INCH X WIDTH 2 INCH OUT OF LIMIT PER SRM 53-10-01 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, UPPER DECK - BS 340 RBL 4 - 40 LATERAL FLOORBEAM FOUND SERVICE CORROSION. FLOORBEAM UPPER SECTION REPAIRED PER SRM 53-10-07 FIG 23. CORROSION BLEND OUT 0.050 X 1 X 1 INCH.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE:C EMP - AFT FUSELAGE SKIN AT BS 2348 - 2355 STR 3 (RT). THE DEPTH OF WEAR IN FUSELAGE SKIN HAS EXCEEDED EO B747-5330-18431 LIMIT AFT BLEND OUT. DEFECTIVE AREA SKIN REPAIR CARRIED OUT AS PER SRM 53-30-03 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, UPPER DECK, BS 400 RBL 30 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.050 X 2 X 2 INCH. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 4.

Part: SHEAR TIE — CRACKED (RT WING RIB) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, RT WING, NR 3 MAIN TANK INTERNAL RIB 469.82 FWD SHEAR TIE FOUND CRACKED. RIB REPAIRED AS PER SRM 57-10-05 AND CWS FOR WORK DETAIL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE:C EMP - AFT FUSELAGE SKIN AT BS 2340 - 2355 LT STR 3. THE DEPTH OF WEAR IN FUSELAGE SKIN HAS EXCEEDED EO B747-5330-18431 LIMIT AFT BLEND OUT. DEFECTIVE AREA SKIN REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE:C EMP - AFT FUSELAGE SKIN AT BS 2365 - 2390 RT STR 3, THE DEPTH OF WEAR IN FUSELAGE SKIN HAS EXCEEDED EO B747-5330-18431 LIMIT AFT BLEND OUT. DEFECTIVE AREA SKIN REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1A.

Part: FLOORBEAM — CORRODED (COCKPIT) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, COCKPIT - BS 340, LBL 8 - 44, FLOORBEAM UPPER SECTION FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 3 INCH. FLOORBEAM UPPER SECTION REPAIRED PER SRM 53-10-07 FIG 23.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, U/D - BS 530 - 590 LBL 66, TIE DOWN TRACK CROWN AND FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.040 X 0.5 X 2.5 INCH. U/D BS 480 TO BS 620 LBL 66 CARGO TRACK REPLACED AS PER SRM 53-10-05 FIG 1A.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, UPPER DECK, BS 530 - 590, RBL 66. TIE DOWN TRACK FLANGE AND CROWN AREA FOUND CORROSION. CORROSION BLEND OUT 0.053 X 0.5 X 2.5 INCH. BS 500 TO BS 590 RBL 66 CARGO TRACK REPLACED AS PER SRM 53-10-05 FIG 1A.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, UPPER DECK, BS 510 - 530, LBL 66 TIE DOWN TRACK CROWN AREA FOUND CORRODED. CORROSION BLEND OUT 0.045 X 0.5 X 2 INCH. U/D BS 480 TO BS 620 LBL 66 CARGO TRACK REPLACED AS PER SRM 53-10-05 FIG 1A.

Part: WEB — CRACKED (MLG WW) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, LT BLG W/W O/B SIDE LOWER FAIRING SUPPORT WEB CRACKED AT STA 1438. WEB REPLACED PER SRM 51-40-03 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, MAIN DECK - BS 555 RT STR 26 STR WEB I/B FLANGE FOUND CRACKED AS MARKED. MAIN DECK - BS 555 RIGHT STR 26 STR WEB I/B FLANGE REPAIRED AS PER SRM 51-40-03 FIG 3.

Part: FLOORBEAM — CORRODED (COCKPIT) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, COCKPIT BS 380, LBL 22-24, FLOORBEAM UPPER TEE AFT FLANGE FOUND CORRODED. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 1. CORROSION BLEND OUT 0.050 X 1 X 1 INCH.

Part: SPAR — CRACKED (NR 3 PYLON I/B) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, NR 3 PYLON I/B AFT LOWER SPAR WEB FASTENER FOUND CRACKS JUST AFT OF REAR ENGINE MOUNT BULKHEAD. NR 3 PYLON I/B AFT LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 22 AT NAC STA 221.9.

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, NR 1 PYLON I/B AFT LOWER SPAR WEB FOUND CRACKED JUST AFT OF REAR ENGINE MOUNT BULKHEAD. NR 1 PYLON LOWER SPAR WEB I/B EDGE AREA REPAIRED AS PER SRM 54-10-03 FIG 23.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, COCKPIT BS 340-360 BL 0, FLOOR SUPPORT UPPER CHORD FOUND CRACKED. BS 340-360 BL 0 FLR SUPPORT UPPER CHORD REPLACED PER SRM 51-10-01.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE:C M/D - BS 805 BETWEEN LT STR -24 & STR -25 CUTOUT REVEAL FOUND CRACKED AS MARKED. CUTOUT REVEAL PANEL, REPLACED AS PER SRM 51-10-01.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, BS 1220 LBL 110 FLOORBEAM WEB FOUND CRACKED AS MARKED. FLOORBEAM WEB REPLACED PER SRM 51-40-02 FIG 1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, MAIN DECK - BS 1236, RBL 116. LONGITUDINAL FLOOR SUPPORT I/B FLANGE FOUND CRACKED AS MARKED. FLOOR SUPPORT REPAIRED PER SRM 51-40-02 FIG 02.

Part: REVEAL — CRACKED (L5 DOOR FRAME) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE:C M/D - L5 DOOR FWD CUTOUT REVEAL FOUND CRACK BETWEEN STRINGER S17L TO S18L. CUTOUT REVEAL PANEL, REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: REVEAL — CRACKED (R5 DOORWAY) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE:C M/D - R5 DOOR FWD CUTOUT REVEAL FOUND CRACK BETWEEN STRINGER S17R - S18R. M/D - R5 DOOR FWD EDGE BS 2231 STR 16R TO STR 19R FRAME STRAP AND REVEAL REPAIR CARRIED OUT IAW HX RS R-53-61-35096. (UPS EO NO B747-5310-19827-A).

Part: SUPPORT — CRACKED (RT MLG WW) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, RIGHT BLG WHEEL WELL O/B SIDE UPPER SKIN SUPPORT WEB CRACKED AT STA 1416. RIGHT BLG WHEEL WELL O/B BS 1416 STR 29R TO STR 31R FRAME REPAIR CARRIED OUT IAW HX RS R-53-42-35097. (RA 747-53-20163).

Part: SKIN — DEFORMED (CARGO DOOR) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, BULK CARGO DOOR FWD LOWER EXT SKIN DEFORM. DEFECTIVE AREA DOOR SKIN REPAIRED IAW SRM 52-00-03 FIG 3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, MAIN DECK - BS 2340, S44R STRINGER CLIP FOUND CRACK. STRINGER CLIP REPLACED AS PER SRM 51-10-01 PG 8.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE: C, MAIN DECK - BS 240-250, RBL 56 TIE DOWN TRACK CROWN LIP FOUND CRACK. CARGO TRACK REPLACED AS PER SRM 51-10-01 PG 8.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 91,214 hrs · 22,751 cycles

INSPECTION TYPE:C - BS 1664, BETWEEN STR 24 - 26R R4 DOOR CUTOUT FWD LWR REVEAL FOUND CRACK. DOOR CUTOUT REVEAL REPLACED AS PER SRM 51-10-01 PG 8.

Part: CIRCUIT CARD — INOPERATIVE (NR 1 FIRE WARN)

INSPECTION TYPE:N/A FIRE AND FAULT ON NR 1 ENGINE. B-NACELLE ILLUMINATED INTERMITTENTLY ON CLIMB AND APPROACH. CLEANED 3 RESEATED FIRE WARNING CARDS A-13 A-10. OPS TEST GOOD PER 26-10-00.

Part: LIGHT — MISSING (COCKPIT)

TRANSFERRED FROM NONROUTINE 596216 MAIN DECK EMERGENCY LIGHT M385 AT STA 350 RT IS INOP FOUND NO LIGHT ASSY INSTALLED REF WD 35-51-01 SNT 2, PG 2, NOTE 1 LIGHT ASSY AT THIS POSITION WAS DEACTIVATED BY EO 33-50-301A LABELED CEILING PANEL ACCORDINGLY.

Part: BATTERY — INOPERATIVE (MAIN CARGO BAY)

SEVERAL EMERGENCY LIGHT BULBS INOP AT MAIN CARGO COMPARTMENT CEILING NEAR MAIN ENTRY DOOR AND ONE BULB INOP AT MAIN ENTRY DOOR OVERHEAD REPLACED BATTERY ASSY IN EMERGENCY LIGHT ASSY M325 AT STATION 580 LT. LIGHT OPERATION CKS OK & 21 DOOR AFT SILL LIGHT. CK OK EMERGENCY LIGHT M385 AT STATION 350 RT TRANSFERRED TO NON ROUTINE 596229

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT AFT L1 DOOR EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK NORMAL.

Part: SWITCH — FAULTY (CABIN)

INSPECTION TYPE:PFLT EMERGENCY LIGHT SWITCH WILL NOT STAY IN ARMED POSITION WITH GUARD CLOSED. GUARD PUSHES SWITCH INTO ON POSITION. REPLACED EMERGENCY LIGHT CONTROL MODULE IAW MM 33-51-09 PG 401/402.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, BS 1480 BULKHEAD TOTAL 6 STRINGER FOUND SHORT EDGE MARGIN S34L, S35L , S36L, S34R, S35R & S36R. BS 1480 BULKHEAD STRINGER SHORT EDGE MARGIN CONDITION AT S34L, S35L, S36L , S34R, S35R & S36R ARE CONSIDERED AS STRUCTUALLY ACCEPTABLE AS PER HX RS R-53-43-34841 ITEM 4 PER FIG 5 & 6. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, CRACK FOUND AT 1 FASTENER HOLE AT BS 340 LT SIDE UPPER DECK FLOORBEAM UPPER CHORD AREA (VERTICAL FLANGE). CHORD REPAIRED AS PER RS R-53-25-34834 & UPS REPAIR/ALTERATION AUTHORIZATION 747-53-20085.

Part: FITTING — CRACKED (ROTARY ACTUATOR) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, FWD ROTARY ACTUATOR SUPPORT FITTING FOUND CRACK AT HOLE NR 8 (LOOKING FWD) APPROX 0.030 INCH LONG AS MARKED. CRACKED HOLE OVERSIZED TO 0.688 INCH AND CRACK / CORROSION FREE. BUSHING FABRICATED AND INSTALLED AS PER RS R53-65-34855 WITH ENGINEERING FILE NUMBER : 747-53-20096.

Part: FITTING — CRACKED (CENTER WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, RIGHT BS 1241 WING REAR SPAR UPPER SPLICE FITTING NR 8 HOLE CRACK FOUND APPROX 0.030 INCH, RUNNING I/B AND NR 3 HOLE CRACK FOUND AT FWD AND AFT DIRECTION. RIGHT BS 1241 WING REAR SPAR TO WING CENTER SECTION SPLICE FITTING REPLACED AS PER UPS EO B747-5740-4366-F APPENDIX A, C, D, F, H AND I.

Part: FITTING — CRACKED (ROTARY ACTUATOR) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C FWD ROTARY ACTUATOR SUPPORT FITTING FOUND CRACK AT HOLES NR 6 (LOOKING FW) APPROX 0.030 INCH LONG AS MARKED. CRACKED HOLE OVERSIZED TO 0.541 INCH AND CRACK / CORROSION FREE. BUSHING FABRICATED AND INSTALLED AS PER RS R53-65-34855 WITH ENGINEERING FILE NUMBER : 747-53-20096.

Part: SKIN — CORRODED (RT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C RIGHT WING - FRONT SPAR LOWER CHORD FOUND CORROSION AT WS 1100 - 1110 AFTER LOWER PANEL, REMOVED JUST AT NR 4 PYLON AREA. CORROSION BLEND OUT 0.104 INCH X 2 INCH X 4 INCH EXCEED SRM LIMIT. WING LOWER SKIN REPAIRED AS PER HX RS R-57-26-34853 (UPS RA ENGINEERING FILE NUMBER 747-57-20030).

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, LT BS 1480 BULKHEAD S35L FOUND CRACK AT CHORD I/B SURFACE, RUNNING FWD .0625 INCH, RUNNING .25 INCH LONG, AND CRACK AT STRINGER END FITTING O/B SURFACE RUNNING FWD .125 INCH LONG.

Part: SKIN — CRACKED (BS 1480 RH) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C R/H OF BS 1480 BULKHEAD S34R STRINGER END FITTING COMMON TO SKIN AREA, 1 EA FASTENER HOLE FOUND CRACK AT INNER SKIN AT FWD AND AFT DIRECTION CRACK LENGTH UNDETERMINED DUE COVERED BY OVERLAPPING SKIN. RH BS 1480 B/H AT STR 34R AREA SKIN 1 EA CRACK HOLE CRACK FREE FINAL SIZE 0.625" & REPAIR BUSHING INSTALL PER HX RS R-53-43-34841 ITEM 3 FIG 4. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06.

Part: SKIN — CRACKED (BS 1480 LH) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C CRACK FOUND AT BS 1480 LHS B/H ATTACHED SKIN AT 1 EA FASTENER HOLE OF S34L STRINGER ENG FTG LOWER HOLE. THE CRACK LOCATED AT 8 O'CLOCK POSITION AND WITH LENGTH 0.050" APPROX. LH BS 1480 B/H FX SKIN AT STR 34 AREA AT HOLE #9 CRACK FREE FINAL SIZE 0.500" AND REPAIR BUSHING INSTALL PER HX RS R-53-43-34841 ITEM '1' & '3' FIG '1'. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & 2001-11-06.

Part: LONGERON — CRACKED (BS 1460 - 1470) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C FX LH OVERWING LONGERON AFT SPLICE END AT STA 1460 - 1470, FWD HOLE FOUND CRACKED 1/4" LONG & 1/4" DEPTH FROM TOP SURFACE WITH NDT AND MID & AFT HOLES BORE CORROSION IS REVEALED. BS 1350 - 1480 RH OVERWING LONGERON REPAIRED IAW RS R-53-43-34843. (UPS EO# B747-5310-17206-A)

Part: BRACKET — CRACKED (M/D B2231 S26R) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C M/D - BS 2231, S26R FRAME ATT BRACKET CRACKED. ( AT FLOOR LEVEL AREA ). M/D BS 2231 S26R FLOOR LEVEL AREA FRAME ATT BRACKET REPLACED AS PER SRM 51-10-01. P.8.

Part: BULKHEAD (BS 1480 L/R) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C CARRY OUT BS 1480 BULKHEAD AND SPLICE COMPONENT MODIFICATION AS PER SB 747-53A2390 R1 PLAN B. BS 1480 L/R B/H & SPLICE COMPONENT MOD C/OUT AS PER SB 747-53A2390 R.1 PLAN B AS PER FIG 2,3,4,6,7,8,14,17,19,20,23 & 28, APPENDIX 'A', 'C' & 'D', REFER HX RS R-53-43-34841 & UPS EO B747-5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, M/D - BS 1241 LBL 30 CANTED BULKHEAD FOUND CORRODED CRACKED DUE SEALANT REMOVED FOUND. M/D BS 1241 CANTED BULKHEAD REPAIRED FROM BL 0 - LBL 45 AS PER RS R53-48-34842 AND REF NRC 7643 FOR WORK DETAIL.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, LT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING FOUND NR 2, 3, 4, 5, 6, 7, 8, 9, 11 HOLES ELONGATED AFTER FITTING REMOVED. LT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING CHANGED AS PER BOEING SB 747-53A2390.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C M/D - BS 1241 LBL 40 CANTED BULKHEAD FOUND CORRODED CRACKED, DUE SEALANT REMOVED FOUND. M/D - BS 1241 CANTED BULKHEAD REPAIRED FROM BL 0 - LBL 45 AS PER RS R53-48-34842 AND REFER NRC 7643 FOR WORK DETAIL.

Part: BULKHEAD — CRACKED (BS 1480 LH) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C CRACK FOUND AT UPPER BULKHEAD FORGING RADIUS AREA, CRACK RUNNING UPWARD 1.5" IN LENGHT APPROX. L/H BS 1480 B/H CHORD FWD RADIUS CRACKED AREA TRIMMED OFF & REPAIRED PER HX RS R-54-43-34841 ITEM '14' & '15'. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06.

Part: STRAP — CRACKED (BS 2231 S24R-25R) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C R/H BS 2231 STR 24-26 AT REPAIR AREA FASTENER HOLES FOUND 1 EA FASTENER HOLE CRACK AT STRAP LAYER APPROX 3/16" INCH IN LENGTH AND CRACK END AS MARKED. FOR DETAIL PLS REFER ATTACHED SKETCH. REVEAL & STRAP REPAIRED AT BS 2231 RH FRAME BETWEEN STR 24-26 AREA AS PER RS R-52-61-34845.(UPS EO B747-5310-17209-A, APPENDIX A) REFER HAECO NRC#6215 FOR DETAIL.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, RT BLG W/W AT BS 1438 RBL 110 ON TOP OF OVERWING LONGERON AND VERT SUPPORT FRAME CORROSION REVEALED. CORROSION BLEND OUT 0.168 INCH X .5 INCH X 2.5 INCH EXCEED SRM LIMIT. BS 1350 - 1480 RT OVERWING LONGERON REPAIRED IAW RS R-53-43-34843, (UPS EO B747-5310-17206-A).

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, CORROSION AND CRACK REVEALED ON LT BS 1480 BULKHEAD CHORD AT STR 36 END FITTING AREA BY APPROX 0.040 INCH AND .1875 INCH LONG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C DURING THE REPAIR ASSESSMENT PROGRAM INSPECTION - BS 960 - 980 STR 3L - 4L EXISTING REPAIR DOUBLER THICKNESS AT THAT AREA OUT OF SRM REPAIR LIMIT. BS 960 - 980 STR 3L - 4L NEW REPAIR DOUBLER REPLACED AS PER SRM 51-30-02 AND 53-30-03 FIG 1.

Part: PRESSURE PANEL — CORRODED (LT MLG WW) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, LEFT BLG W/W - CEILING PRESSURE DECK CORRODED AT LBL 55, FS 1350 - 1370. LEFT BLG W/W CEILING PRESSURE DECK WEB REPAIRED AT BS 1335 - 1375 LBL 55 - 80 REFER NRC 7975. CORROSION BLEND OUT 0.060 X 1 X 2 INCH EXCEED SRM LIMIT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, CRACK REVEALED ON LT BS 1480 BULKHEAD CHORD AT STR 34 STRINGER END FITTING AREA BY APPROX .125 INCH RUNNING AFT AS PER FIGURE ATTACHED.

Part: SEAT TRACK — CORRODED (M/D FLR PNL) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C M/D - AFTER FLOOR PANEL REMOVED, BS 1940 RBL 11" SEAT TRACK FOUND HEAVY CORRODED. CORROSION BLEND OUT 0.044" X 1" X 1" EXCEED SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, DURING THE REPAIR ASSESSMENT PROGRAM INSPECTION - BS 560 - 566 STR 38R - 39R EXISTING REPAIR DOUBLER THICKNESS AT FWD CARGO DOOR FWD LOWER CORNER AREA OUT OF SRM REPAIR LIMITS. FWD CARGO DOOR FWD LOWER CORNER AREA REPAIRED AS PER SRM 52-00-03 FIG 4 REFER RAP - SEQUENCE 42 - 17 FOR DETAIL INSTRUCTION.

Part: LONGERON — CRACKED (BS 1460 LBL 110) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C LH BLG W/W - FS 1460 OVERWING LONGERON AFTER SPLICE FTG REMOVAL & CORROSION CLEAN UP, FOUND 3" LONG CRACK AT LONGERON. BS 1460 LH OVERWING LONGERON REPAIRED AS PER HX RS R-53-43-34843. (UPS EO# B747-5310-17206-A) REFER HAECO NRC# 6792 FOR DETAIL.

Part: WEB — CRACKED (LH BLG W/W) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C LH BLG W/W - CEILING COR CRACK AT FS 1355, LBL 76. PRESSURE WEB REPAIRED AT BS 1335-1375 LBL 55 - LBL 80 AS PER SRM 53-10-07 FIG 2.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX - KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1227 LT SIDE LBL 9. CORROSION BLEND OUT EXCEEDS SRM LIMITS. BRACKET REPLACED AS PER SRM 51-10-01.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX - KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1122 RBL 9. CORROSION BLEND OUT EXCEEDS SRM LIMITS. BRACKET REPLACED AS PER SRM 51-10-01.

Part: PRESSURE PANEL — CORRODED (WHEEL WELL) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RIGHT WLG W/W PRESSURE DECK O/B AFT CORNER ABOVE BRAKE METERING V/V AREA CORRODED AS MARKED. CORROSION BLEND OUT 0.030 X 1 X 2 INCH EXCEED SRM LIMIT. BS 1315 TO 1380 RBL 98 TO RBL 128 PRESSURE DECK WEB REPAIRED AS PER 53-10-07 FIG 2 REFER NRC 7774.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX - KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1183 RT SIDE RBL 9. CORROSION BLEND OUT EXCEEDS SRM LIMITS. KEELBEAM PANEL SUPPORT BRACKET REPLACED AS PER SRM 51-10-01.

Part: RIB — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX - KEELBEAM BOX LOWER EXTERIOR LOWER CHORD ATT RIB FOUND SURFACE CORROSION AT STA 1360 RBL 7 TO LBL 7. CORROSION BLEND OUT EXCEEDS SRM LIMITS. RIB REPLACED AS PER SRM 51-10-01.

Part: WEB — CORRODED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C FX - KEELBEAM BOX LOWER EXTERIOR LOWER KEELBEAM FIXED PANEL UPPER SURFACE AND HINGE FITTING AREA FOUND SURFACE CORROSION AT STA 1255 TO STA 1275 LBL 7 TO LBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMIT. WEB REPLACED AS PER SRM 51-10-01 PG 8.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX - KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1122 RBL 9. CORROSION BLEND OUT EXCEEDS SRM LIMITS. BRACKET REPLACED AS PER SRM 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C FX - KEELBEAM PANEL SUPPORT LOWER CHORD SURFACE FOUND SURFACE CORROSION AT STA 1112 LBL 9 TO RBL 9. CORROSION BLEND OUT EXCEEDS SRM LIMIT. PANEL SUPPORT REPLACED A PER SRM 5101 PG 8.

Part: FITTING — CORRODED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C FX - KEELBEAM BOX LOWER EXTERIOR LOWER FIXED PANEL UPPER SURFACE AND HINGE FITTING AREA FOUND SURFACE CORROSION AT STA 1255 TO 1275 RBL 7 TO RBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FITTING REPLACED AS PER SRM 51-10-01 PG 8.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX - KEELBEAM PANEL SUPPORT BRACKET FOUND SURFACE CORROSION AT STA 1000 LBL 9. CORROSION BLEND OUT EXCEEDS SRM LIMITS. SUPPORT BRACKET REPLACED AS PER SRM 51-10-01.

Part: PANEL — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX - KEELBEAM BOX LOWER EXTERIOR KEELBEAM FIXED PANEL UPPER SURFACE AND HINGE FITTING AREA FOUND SURFACE CORROSION AT STA 1440 TO STA 1470 RBL 7 TO RBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. WEB REPLACED AS PER SRM 51-10-01.

Part: PRESSURE PANEL — CORRODED (WHEEL WELL) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C RT WLG W/W PRESSURE DECK LWR BONDED SKIN CORRODED AT BS 1375 O/B AREA AS MARKED. CORROSION BLEND OUT 0.050 X 1 X 2 INCH EXCEED SRM LIMIT. BS 1315 TO 1380 RBL 94 TO RBL 128 PRESSURE DECK WEB REPAIRED AS PER SRM 53-10-07 FIG 2.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RT WLG PX DECK AT O/B BS 1340 AREA HEAVY CORROSION FOUND AS MARKED. CORROSION BLEND OUT 0.060 INCH X 1 INCH X 1 INCH EXCEED SRM LIMIT, BS 1315 - 1380 RBL 94 - 128. PRESSURE DECK WEB REPAIRED AS PER SRM 53-10-07 FIG 2. UPS MPI 15830 RAISED FOR EXTERNAL INSPECTION AS PER SRM 53-10-07 PG 5.

Part: FITTING — CRACKED (BS 1480 LH) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C L/H BS 1480 B/H AREA, HOLE #9 CRACKS FOUND AT EXTENSION FITTING RUNNING UPPER & FWD, CRACK THROUGH THICKNESS. LH BS 1480 B/H LONGERON EXTENSION FTG HOLE #9 CRACK FREE FINAL SIZE 0.8745" & PLAN B REPAIR BUSHING INSTALL PER SB 53A2390 R1 PLAN B. REFER HX RS R-53-43-34841 & UPS EO 5310-17028-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06.

Part: PRESSURE PANEL — CORRODED (WHEEL WELL) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RT BLG W/W AT BS 1416 RBL 6 - 9 TOP CEILING / CHORD MATING SURFACE CORRODED AS RED MARKED. CORROSION BLEND OUT 0.050 X 1 X 2 INCH EXCEED SRM LIMIT. PRESSURE DECK WEB REPAIRED AS PER SRM 53-10-07 FIG 15.

Part: RIB — CORRODED (RT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, RT WING L/E RIB AT ILES 852.45 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.065 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX - KEELBEAM BOX LOWER EXTERIOR PANEL SUPPORT LOWER CHORD FOUND SURFACE CORROSION AT STA 1470 LBL 16 TO RBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX KEELBEAM BOX LWR EXTERIOR LWR PANEL SUPPORT LOWER CHORD FOUND SURFACE CORROSION AT STA 1392 TO 1440 LBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01.

Part: PRESSURE PANEL — CORRODED (WHEEL WELL) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RT BLG W/W AT BS 1410, RBL 0 - 3 TOP CEILING / CHORD MATING SURFACE CORROSION FOUND AS RED MARKED. CORROSION BLEND OUT 0.016 X .5 X 1 INCH EXCEED SRM LIMIT. PRESSURE WEB REPAIRED AT RT BLG W/W BS 1402 - 1422 BL 0 TO RBL 33 AS PER SRM 53-10-07 FIG 15. (REFER HAECO NON ROUTINE CARD NR 7522).

Part: LONGERON — CORRODED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RT BLG W/W AT BS 1416 RBL 110 ON TOP OF OVERWING LONGERON VERTICAL SUPPORT FRAME MATING SURFACE CORROSION FOUND AS RED MARKED AND ON TOP OF THIS DEFECT THE CROSS-OVER STRINGER CORROSION FOUND AS RED MARKED. CORROSION BLEND OUT DEPTH THROUGH THICK, WIDTH .25 INCH, LENGHT 2.125 INCH EXCEED SRM LIMIT. BS 1350 - 1480 RT OVERWING LONGERON REPAIRED IAW RS R-53-43-34843, (UPS EO B747-5310-17206-A).

Part: RIB — CORRODED (RT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RT WING L/E RIB AT OLES 1493.45 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.038 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.

Part: RIB — CORRODED (RT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RT WING L/E RIB AT OLES 1349.29 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.026 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.

Part: RIB — CORRODED (RT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RT WING L/E RIB AT OLES 1308.15 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.020 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C LT BS 1480 BULKHEAD AREA, HOLE NR 11 CRACK FOUND AT SKIN RUNNING FWD AND AFT, CRACK THROUGH THICKNESS, PLS REFER ATT FIG. SKIN REPAIRED AS PER SB 53A2390 FIG 28 STEP 13 - 17.

Part: SPLICE — CRACKED (BS 990 S10L) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C U/D - BS 990 S-10L STRINGER SPLICE FOUND CRACKED. BS 990 S10L SPLICE REPLACED AS PER SRM 51-10-01 PG 8.

Part: PANEL — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX KEELBEAM BOX LWR EXTERIOR LWR FIXED PANEL UPPER SURFACE FOUND SURFACE CORRODED AT LT SIDE STA 1440 TO 1460 LBL 7 TO 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. FIXED PANEL REPLACED PER SRM 51-10-01.

Part: PRESSURE PANEL — CORRODED (MLG WW) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, LT WLG W/W - FS 1241 CANTED BULKHEAD CORROSION FOUND AT LBL 21 - 23. CORROSION BLEND OUT 0.050 INCH X 1 INCH X 2 INCH EXCEED SRM LIMIT. BS 1241 - 1265 BL 0 TO LBL 45 CANTED BULKHEAD WEB REPAIRED IAW RS R-53-48-34842 (UPS RA ENGINEERING FILE NUMBER: 747-53-20092).

Part: RIB — CORRODED (RT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RT WING L/E RIB AT OLES 1381.25 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.030 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX KEELBEAM BOX LWR EXTERIOR LWR PANEL SUPPORT LWR CHORD FOUND SURFACE CORROSION AT STA 1276 TO 1353 RBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX - KEELBEAM BOX LOWER SURFACE LOWER PANEL SUPPORT LOWER CHORD SURFACE FOUND SURFACE CORROSION AT STA 1480 RBL 16 TO LBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX KEEL BEAM BOX LWR EXTERIOR LWR SUPPORT LWR CHORD FOUND SURFACE CORROSION AT STA 1329 RBL 16 TO LBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX KEELBEAM BOX LWR EXTERIOR PANEL SUPPORT LWR CHORD FOUND SURFACE CORROSION AT STA 1353 RBL 16 TO LBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:C FX - KEELBEAM BOX LOWER EXTERIOR PANEL SUPPORT LOWER CHORD FOUND SURFACE CORROSION AT STA 1405 LBL 16 TO RBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, LT BS 1480 BULKHEAD AREA, HOLE NR 11 CORROSION FOUND AT BULKHEAD CHORD, LOCATED AT HOLE FWD O/B.

Part: RIB — CORRODED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C FX KEELBEAM BOX LWR EXTERIOR LWR CHORD SUPPORT LWR RIB FOUND SURFACE CORROSION AT STA 1308 RBL 2 AFT SURFACE. CORROSION BLEND OUT EXCEEDS SRM LIMIT. RIB REPLACED AS PER SRM 51-10-01 PG 8.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,099 hrs · 88,072 cycles

INSPECTION TYPE:N/A FX KEELBEAM BOX LWR EXTERIOR PANEL SUPPORT LWR CHORD SURFACE FOUND SURFACE CORROSION AT STA 1276 RBL 16 TO LBL 16. CORROSION BLEND OUT EXCEEDS SRM LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01.

Part: SKIN — CRACKED (BS 1480 RH) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C R/H OF BS 1480 FUSELAGE SKIN AT EXTENSION FITTING SRES FOUND CRACK AT HOLE #11 RUNNING AT 5 O'CLOCK POSITION ( VIEW LOOKING I/B )WITH 1/16" IN LENGTH APPROX AT I/B SURFACE. RH BS 1480 FX SKIN AT HOLE #11 CRACK FREE FINAL SIZE 0.6875" & PLAN B REPAIR BUSHING INSTALL PER SB 53A2390 R.1 FIG 14. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06.

Part: SKIN — CRACKED (BS1480 R/H) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C R/H BS 1480 FUSELAGE SKIN AT EXTENSION FITTING AREA CRACK AT HOLE #1 , 9 O'CLOCK POSITION AT I/B SURFACE APPROX 0.100" IN LENGTH (LOOKING I/B). R/H BS 1480 FX SKIN CRACK AT HOLE #1, HOLE FINAL SIZE 0.6875" & PLAN B REPAIR BUSHING INSTALL PER SB 747-53A2390 R.1 FIG 14. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, RT BS 1480 BULKHEAD AT HOLE NR 3 FOUND 3 CRACKS AT EXTENSION FITTING RUNNING FWD AND AFT.

Part: FITTING — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, RT BS 1480 BULKHEAD AT HOLE NR 1, 3 CRACKS FOUND AT EXTENSION FITTING RUNNING FWD AND AFT DIRECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C M/D - R3 DOOR LWR HINGE CUTOUT SKIN CRACKED. SKIN REPAIRED AS PER SRM 52-10-02 FIG 11.

Part: ANGLE — CORRODED (LT MLG DOOR) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, LEFT BLG W/W - O/B STRUT DOOR ATTACHMENT FAIRING ANGLES INNER FACE SURFACE CORRODED AT FS 1438 TO 1480 LBL 120. CORROSION BLEND OUT 0.050 X 1 X 2 INCH EXCEED SRM LIMIT. FAIRING CHORD REPLACED IAW SRM 51-10-01 PG 8.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, LT BLG W/W - OVERWING LONGERON AT W/W CORRODED AT MULTI SPOTS FROM FS 1360 - 1470 LBL 123 - 109. CORROSION BLEND OUT DEPTH THROUGH THICK, WIDTH .25 INCH, LENGTH 3.625 INCH EXCEED SRM LIMIT. BS 1350 - 1480 RT OVERWING LONGERON REPAIRED IAW RS R-53-43-34843 (UPS EO B747-5310-17206-A).

Part: SPLICE PLATE — CRACKED (BS 1480 RH) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C R/H OF BS 1480 B/H WEB SPLICE PLATE FOUND CRACK AT HOLE #15 LOCATED AFT SIDE SURFACE APPROX 1/16" IN LENGTH. RH BS 1480 BULKHEAD WEB SPLICE PLATE AT HOLE #15 FINAL SIZE 0.500" & PLAN B REPAIR BUSHING INSTALL PER SB 53A2390 R.1 FIG 14. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RT BS 1480 BULKHEAD LONGERON EXTENSION FITTING FOUND CRACK AT NR 5 AT 8 O'CLOCK POSITION (VIEW LOOKING I/B), .0625 INCH IN LENGTH APPROX. RT BS 1480 BULKHEAD LONGERON EXTENSION FITTING AT HOLE NR 5 CRACK, HOLE FINAL SIZE 0.6875 INCH & PLAN B REPAIR BUSHING INSTALL PER SB 53A2390 R1 FIG 14. HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06.

Part: FITTING — CORRODED (FUSLEAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RT OF BS 1480 BULKHEAD LONGERON EXTENSION FITTING FOUND CORROSION AT HOLE NR 11 BORE SURFACE SURFACE .0625 INCH IN DEPTH APPROX. RT BS 1480 BULKHEAD LONGERON EXTENSION FITTING AT HOLE NR 11 FINAL SIZE 0.6875 INCH & PLAN B REPAIR BUSHING INSTALL PER SB 53A2390 R.1 FIG 14. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, M/D - BS 1320 RBL 75-97 FLOOR SUPPORT ATT PLATE CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOOR SUPPORT ATT PLATE AT M/D BS 1320 RBL 75-97 REPLACED AS PER SRM 51-10-01 PG 8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, RT OF BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING FOUND CRACK AT HOLE NR 9 RUNNING FWD AT O/B SURFACE .0625 INCH IN LENGTH APPROX.

Part: RIB — CORRODED (LT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, LT WING L/E RIB AT ILES 755.05 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.008 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.

Part: FITTING — CRACKED (BS 1480 RH) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C R/H OF BS 1480 B/H LONGERON EXTENSION FTG FOUND CRACK AT HOLE #9 AT 3 O'CLOCK POSITION ( VIEW LOOKING I/B ), THE CRACK 1/16" IN LENGTH APPROX AT I/B SURFACE. RH BS 1480 BULKHEAD LONGERON EXTENSION FITTING AT HOLE #9 CRACK FREE FINAL SIZE 0.8125" & PLAN B REPAIR BUSHING INSTALL PER SB 53A2390 R1 PLAN B & HX RS R-53-43-34841. REFER HX RS R-53-43-34841 & UPS EO 5310-17208-A, A TIME LIMIT REPAIR FOR 12 MONTHS. POST MOD INSP PLAN PER SB 53A2390 & AD 2001-11-06.

Part: FRAME — CRACKED (BS 2231 S24R-26R) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C R/H BS 2231 FRAME FOUND TWO CRACK AT REVEAL AND STRAP BETWEEN STR TO STR 26 AND CRACKS END MARKED. REVEAL & STRAP REPAIRED AT BS 2231 RH FRAME BETWEEN STR 24-26 AREA AS PER RS R-53-61-34845.(UPS EO B747-5310-17029-A, APPENDIX A)

Part: FRAME — CRACKED (BS 2231 S24L-25L) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C LH BS 2231 FRAME TWO EACH FASTENER HOLES CRACK FOUND AT REVEAL AND STRAP. REVEAL AND STRAP REPAIRED AS PER RS R-53-61-34845. (UPS EO B747-5310-17209-A, APPENDIX A)

Part: RIB — CORRODED (LT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, LT W L/E RIB AT OLES 1277.15 FOUND CORROSION AT ROTARY ACTUATOR MOUNT BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.022 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.

Part: WEB — CRACKED (BS 2231 S26L) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C M/D - BS 2231 S26L BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. M/D BS 2231 S26L BELOW FLOOR INTERCOSTAL WEB REPLACED AS PER SRM 51-10-01 P.8.

Part: RIB — CORRODED (RT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RT WING L/E RIB AT OLES 1277.15 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.050 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-..

Part: RIB — CORRODED (RT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C RT WING L/E RIB AT ILES 1014.95 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.017 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.

Part: RIB — CORRODED (LT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C LT WING L/E RIB AT ILES 802.5 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR C/OUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-. CORROSION BLEND OUT 0.022 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT.

Part: RIB — CORRODED (LT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, LT WING LEADING EDGE RIB AT ILES 842.05 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.024 INCH X 0.5 INCH X 0.5 INCH, EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERIM CORROSION REPAIR CUTOUT AS PER EO B747-5740--17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.

Part: RIB — CORRODED (RT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, RT WING L/E RIB AT OLES 1421.35 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.031 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.

Part: RIB — CORRODED (LT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, LT WING L/E RIB AT ILES 765.45 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.018 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX B.

Part: SKIN — CRACKED (RH SIDE STA 392) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C FX - EXTERIOR SKIN FOUND CRACKED AROUND RIVET FASTENER AT RH SIDE STA 392 STR 44R. NOSE WHEEL WELL RH AFTER CORNER SKIN REPAIRED AS PER EO B747-5330-3520E AND DWG 141U1099 AND HX RS R53-11-34838 WITH UPS ENGINEERING FILE NUMBER 747-53-20090.

Part: STRINGER — CRACKED (BS 990 S-10L) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C M/D - BS 990 S-10L STRINGER END FOUND CRACKED. BS 990 S10L STR REPAIRED AS PER RS R53-21-34835. ( UPS REPAIR / ATERATION AUTHORIZATION #747-53-20088 ).

Part: SPLICE — CRACKED (BS 1301 S12L) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C M/D - BS 1301 S12L FRAME ATTACH SPLICE FOUND CRACKED. M/D - BS 1301 S12L FRAME ATT SPLICE REPLACED AS PER SRM 51-10-01 P.8 .

Part: RIB — CORRODED (RT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, RT WING L/E RIB AT ILES 1523.45 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.032 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIRS TO BE DETAIL VISUALLY INSPECTED AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.

Part: RIB — CORRODED (LT WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, LT WING L/E RIB AT OLES 1308.15 FOUND CORROSION AT ROTARY ACTUTOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.017 INCH X 0.5 INCH X 1 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PER EO B747-5740-17207 APPENDIX -A-. COMPLETED REPAIR TO BE DETAIL VISUALLY INSPECTION AT EVERY C-CHECK NOT TO EXCEED 18 MONTHS AS PER EO B747-5740-17207 APPENDIX -B-.

Part: FRAME — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, CRACK REVEALED AT BS 800 LT SIDE S16L FWD FASTENER HOLE, CRACK FOUND THRU THICKNESS AT FRAME BS 800 LT S16L FRAME REPAIRED AS PER RS R-53-22-34840. (UPS EO 13747-5310-17235-A & EO B747-5310-17198-A).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C, FWD CARGO COMPARTMENT STA 560 RBL 45 PALLET LOCK FLOOR SUPPORT CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: FITTING — CRACKED (CENTER WING) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, CRACK REVEALED AT RT OF BS 1241 REAR SPAR TO WING CENTER SECTION SPLICE FITTING SIGNAL INDICATION GREATER THAN 50 PERCENT FSH. RIGHT BS 1241 WING REAR SPAR TO WING CENTER SECTION SPLICE FITTING REPLACED AS PER UPS EO B747-5740-4366-F APPENDIX A, C, D, F, H AND I.

Part: STRAP — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, CRACK FOUND AT BS 800 RT SIDE ABOVE S17R FWD FASTENER HOLE, THE CRACK FOUND 1 INCH LONG AT THE STRAP. BS 800 RT SIDE ABOVE STR 17R THE STRAP REPAIRED AS PER HX RS R53-22-34839 AND REFER NRC 5908 FOR WORK DETAIL. (UPS EO B747-5310-17165-A).

Part: REVEAL — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C M/D - R5 DR FWD CUTOUT REVEAL CRACKED. REVEAL REPAIRED AT BS 2231 S25R AREA AS PER RS R-53-61-34845, (UPS EO B747-5310-17209-A, APPENDIX A) REFER HAECO NRC 6215 FOR DETAIL.

Part: WEB — CRACKED (#2 PYLON) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C NO.2 PYLON - LOWER SPAR BOTTOM AREA FOUND CRACK AT NAC STA 228 AS MARKED. LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 2 AND SRM 54-10-03 FIG 22.

Part: STRAP — CRACKED (FUSELAGE) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE: C, CRACK FOUND AT BS 800 RT SIDE ABOVE S16R AFT FASTENER HOLE CRACK FOUND AT STRAP .125 INCH AT FWD AND .0625 INCH RUNNING AFTWARD. BS 800 RT BETWEEN STR 15 TO STR 17 AREA STRAP REPAIRED AS PER RS R-53-22-34839 (UPS EO B747-5310-17165-A).

Part: FRAME — CRACKED (BS 2231 S26R) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C M/D - R5 DOOR FWD CUTOUT REVEAL CRACKED. BS 2231 STR 26R FRAME REVEAL REPAIRED A PER RS R-53-61-34845, (UPS EO B747-5310-17209-A, APPENDIX A) REFER HAECO NRC# 6215 FOR DETAIL.

Part: SKIN — CRACKED (BS 1800-1920) · airframe 88,072 hrs · 22,099 cycles

INSPECTION TYPE:C AFT LOWER CARGO DOOR CUTOUT UPPER CORNER ( FWD SIDE AND AFT SIDE ) FOUND FASTENER HOLES ( TOTAL : 3 EA ) CRACKED AT SKIN. AFTER LOWER CARGO DOOR CUTOUT UPPER CORNER ( FWD SIDE & AFT SIDE ) REPAIRED AS PER RS R-53-61-34833.(UPS RA ENGINEERING FILE NUMBER# 747-53-20086)

Part: ENGINE — FLAMED OUT (NR 3)

INSPECTION TYPE:N/A ENGINE NR 3 FLAME-OUT AT FL350 APPROXIMATELY 15 MINUTES AFTER LEVEL OFF, CAUSE UNKNOWN. AOM PROCEDURES ACCOMPLISHED AND ENGINE RESTARTED. AS PER MM T/S TREE 71-00-42 PG 219 AND 131 ACCOMPLISHED ALL CORRECTIVE ACTIONS FOR FLAME-OUT. NO DISCREPANCIES NOTED. RAN ENGINES AT PP, ALL ENGINE PARAMETERS CHECK NORMAL.

Part: SWITCH — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT SWITCH INOP. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH MODULE. OPS CHECK GOOD.

Part: CONTROL PANEL — FAULTY (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL PANEL IAW B747-33-51-09.

Part: COVER — BROKEN (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT SWITCH COVER BROKEN. REMOVED AND REPLACED EMERGENCY LIGHTS MODULE AND OPS CHECK OK PER MM 33-51-09.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A FOUND EXIT LIGHT INOP AT UPPER DECK CREW SERVICE DOOR CEILING. REMOVED AND REPLACED BATTERY PACK ASSY RT-SIDE EXIT LIGHT, OPS TEST OK. PER MM 33-51- 00, P/N OFF/ON 9008-3-5A, S/N OFF 5941, SN ON 75833.

Part: ENGINE — MALFUNCTIONED (NR 3)

INSPECTION TYPE:N/A THRUST LEVERS CLOSED INSIDE BRUCK 1200 AGL. NR 3 ENG OIL PRESS LIGHT ON, EGT 952 GEN LIGHT ON AIRSPEED 165 KTS. FF 0 N2 & N1 LOW (NEAR 0). INSPECTED 3.5 BLEED VLVS FOR FOD, FUEL PUMP FP12 PRESSURE CHECKED AND REPLACED FUEL PUMP FILTER PER MM 73-11-02. REPLACED FUEL CONTROL MAIN FILTER PER MM 73-21-02. CHECKED FUEL CONDITION ACTUATOR PER MM 71-00-42. OPERATED ENGINE AT IDLE AND T/O PWR PER MM 71-00-00. NO FAULTS FOUND. BORESCOPED ENG PER 72-00-00. WINDMILL INSP PER 72-00-00, NO FAULT

Part: PLATE — FAULTY (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHT PNL SWITCH DOES NOT AGREE WITH PANEL POSITION INDICATION. REMOVED AND REPLACED LIGHT PLATE AS PER EO B747-3350-14819, SWITCH AND LIGHT PLATE AGREE.

Part: CARD — DEFECTIVE (AUTOPILOT)

INSPECTION TYPE :W/E, ON DEPARTURE THE CREW BEGAN TO NOTICE A SLIGHT ELECTRICAL SMELL, NOTHING OUT OF ORDINARY WAS NOTICED, APPROACHING LEVEL OFF SMELL DISAPPEARED. SHORTLY AFTER ''B'' A/P DISENGAGED FOR NO APPARANT REASON. COULD NOT REENGAGE A/P B, NOTE: B A/P PADDLESTICK SWITCH W/ENGAGE BUT A/P W/NO T HOLD ALT. OR COURSE, PULLED B A/P CB & CONTINUED FLT. REPLACED MONITOR & LOGIC UNIT AS PER MM 22-11-07, OPS CKS GOOD, PERF ORMED T/S TREE IN 22-15-00 WITH NO DEFECTS NOTED NO ABNORMAL SMELL N OTED IN COCKPIT

Part: EXTINGUISHER — INOPERATIVE (APU)

INSPECTION TYPE:PFLT, APU FIRE EXTINGUISHER INOP. *S/D* REMOVED AND REPLACED APU FIRE EXTINGUISHER BOTTLE. OPS CK NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, CORROSION AND PULLED RIVETS AT BS 1000 STR 41R. REPAIRS ACCOMPLISHED TO SKIN AND CHORD IAW Q/NOTE 4/01 AND SRM 53-30 -03. REFERENCE ALSO NRCS 44374471, 44370677 AND 44374732.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, 2 INCH CRACK FOUND BS 260 CANTED BULKHEAD AT UPPER EDGE LT SIDE. REPAIR ACCOMPLISHED IN ACCORDANCE WITH QUERY NOTE 17 / 01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, CORROSION ON PALLET LOCK TIE DOWN FITTING AT BS 2080 LBL 60. FITTING REPLACED IAW SRM 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, FWD CARGO CRACK FOUND IN SHEAR TIE AT BS 960- STR 37 & 38 LT. SHEAR TIE REPLACED IAW SRM 53-10-04.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, FWD CARGO RT SIDE SHEAR TIE CRACKED AT BS 940 STR 38 & 39 RT. REPAIR CARRIED OUT IAW SRM 53-10-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, CORROSION ON UPPER SURFACE OF HORIZ FLANGE MAIN CABIN FLOORBEAM AT BS 260 BETWEEN RBL 35 AND RBL 48. REPAIRS ACCOMPLISHED PER FLS QUERY NOTE 17 / 01 REFERENCE ALSO QUERY NOTE 19 / 01.

Part: PANEL — CRACKED (NR 6 SPOILER) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, LT WING CRACK ON T/E PANEL FWD OF SPOILER NR 6 I/B HINGE. REPAIRED IAW SRM 51-40-09 MATERIAL USED BMS 8-301TY2.

Part: SHUTOFF VALVE — LEAKING (CREW OXYGEN) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, DURING CREW OXY SYS LEAK CHECK. FOUND CREW OXY SYS SHUT OFF VALVE LEAKING. REPLACED CREW OXYGEN SHUTOFF VALVE.

Part: BRACKET — DAMAGED (APU BAY) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, APU AREA DAMAGED BRACKET ON UPPER DETECTOR U-BRACKET. NEW BRACKET FABRICATED IAW SRM 51-20-01.

Part: STIFFENER — CRACKED (NR 2 PYLON) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 2 PYLON CRACK OTBD PYLON STIFFENER NAC 286. REPAIRED STIFFENER IAW SRM 54-14-03.

Part: FITTING — CRACKED (PAX DOORWAY) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 1 RT MAIN ENTRY DOORWAY FWD EDGE JUST ABOVE LOWER HINGE IS CRACKED. ALSO, CLOSURE PANEL CRACKED FITTING REPLACED IAW SRM 51-30-02. CLOSURE PANEL REPLACED IAW SRM 51-30-02.

Part: CASTING — CRACKED (RT TE FLAP) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, RIGHT I/B MIDFLAP O/B DEFLECTOR ROLLER SUPPORT CASTING CRACKED. CRACKED CASTING REPLACED IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK CORROSION ON SEAT TRACK INNER FLANGE BS 1765, 1785 AND 1820 LBL 76 REPAIR REQUIRED. REPAIRED IAW SRM 53-10-05.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK CANTED PRESSURE BULKHEAD WEB IS CRACKED UNDER LWR CREASE BEAM WEB STR 26 LT BS 260 (CPCP TASK C53-210-07-1B ). CANTED PRESSURE BULKHEAD REPAIRED, WEB REPAIR IAW QUERY NOTE 19/01.

Part: BRACKET — CRACKED (E/E BAY DOOR) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, E&E COMPARTMENT DOOR CRACK ON OUTER FRAME AT RT SUPPORT BRACKET MOUNT BOLT HOLE AND SUSPECT CRACK ON OUTER CHORD OF FRAME 3 LHS. REPAIRS CARRIED OUT IAW SRM 51-40-03. HFEC INSP CARRIED TO DETERMINE CRACKING PER D67170 PART 6 CH 51-00-00 FIG 4.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C AFT CARGO HOLD FUSELAGE FRAMES AT BS 1520 - AND 1560 ARE CRACKED BETWEEN STRS 39 AND 40 LT. FRAMES AT BS 1520 & 1560 REPAIRED IAW QUERY NOTE 10/01 BOEING APPROVED REPAIRS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, CORROSION BEYOND LIMITS AT FLOORBEAM BS 1720 BETWEEN LBL 85 AND LBL 98. NEW SECTION SPLICED IN PER Q / NOTE 9/01.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, FRAME SUPPORT STA 987 LT LOWER WING TO BODY SUPPORT FRAME HAS CORROSION. WING TO BODY FRAME REPAIRED IAW QUERY NOTE 15/91 AND SRM 51-40-04 FIG 1. INSTALLED REPAIR SECTION.

Part: FITTING — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK CORROSION ON SUPPORT PLATE UNDER PALLET LOCK TIE DOWN FITTING AT BS 1980 RBL 58. FITTING REPLACED IAW SRM 51-30-02.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, LOWER BILGE AREA AFT CORROSION ON STR AT CLIP FRAME BS 2320 STR 50 RHS. STRINGER REPAIRED IAW SRM 53-10-03 FIG 9.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK CORROSION ON AFT CARGO HOLD CEILING SUPPORT ANGLES BS 1840 - 1860 LBL 7 AND RBL 7. NEW SUPPORT ANGLES FABRICATED AND FITTED IAW SRM 51-20-01 AND SRM 51-30-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK ON AFT CARGO HOLD CEILING ANGLES AT BS 1840 - 1860 LBL 7 AND RBL 7 CORRODED. NEW SUPPORT ANGLES FABRICATED AND FITTED IAW SRM 51-20-01 AND SRM 51-30-02.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, UPPER DECK SEAT TRACK BS 600 - 630 LBL 47 CORRODED. CORRODED SECTION REMOVED AND NEW SECTION FITTED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN CABIN UPPER DECK FLOOR SEAT TRACK AT BS 540 - 670 LBL 66 CORRODED. CORRODED SECTION OF SEAT TRACK REMOVED AND NEW SECTION FITTED IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK CORROSION ON PALLET LOCK TIE DOWN FITTING AT BS 2040 RBL 80. FITTING REPLACED IAW SRM 51-30-02.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK T-CHORD OF LOWER CREASE BEAM WEB IS CRACKED STR 26 AT BS 1241 LT. DAMAGED T-CHORD REMOVED AND NEW SECTION FITTED IAW SRM 51-30-02 NDT USED TO MARK CRACK ENDS.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, CABIN MAIN DECK INNER T-CHORD OF LOWER CREASE BEAM WEB IS CRACKED STR 26 AT BS 1241 LT SIDE. DAMAGED T-CHORD REMOVED AND NEW SECTION FITTED IAW SRM 51-30-02.

Part: BALLSCREW — CORRODED (TE FLAP) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 1, 5, & 8 FLAP BALLSCREWS CORRODED AND NR 7 HAS WORN BOLT HOLE. BALLSCREWS 1, 5, 7 & 8 REPLACED IAW MM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK CORROSION ON SEAT TRACK AT BS 1660 - 1680 RBL 34. SEAT TRACK REPLACED AT BS 1660 - 1680 RBL 34 REPLACED IAW SRM 53-10-05.

Part: STRAP — WORN (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, WEAR AT FUSE STA 2568 WHERE FRONT END OF APU DOORS CONTACT FUSELAGE STRAP WORN. REPLACED STRAP WITH NEW PART IAW SRM & QUERY NOTE 12/01.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK FLOOR INTERCOSTAL IS CRACKED AT BS 440 - 460 RBL 60 AND ATTACH BRACKET TO FLOOR WEB IS CRACKED AT BS 440. INTERCOSTAL RE-WORKED AND NEW BRACKETS FITTED IAW SRM 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, CORROSION ON PALLET LOCK TIE DOWN FITTING. FITTING REPLACED REF SRM 51-30-02.

Part: SKIN — WORN (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, TAIL AT STA 2742 ON LT SIDE OF FUSE WHERE APU DOOR SITS ON FUSE SKIN REPLACE ANGLE SKIN ANGLE WORN AWAY. NEW FRAME FITTED IAW SRM 51-30-02.

Part: GUARD — CRACKED (THROTTLE CABLE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, FWD CARGO COMPARTMENT SEVERAL CRACKS ON THROTTLE CABLE CIVER GUARDS BS 980 LT AND RT. CABLE COVER GUARDS REPLACED IAW MM 76-11-00.

Part: WEB — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK FLOOR INTERCOSTAL WEB IS CRACKED AND UPPER CHORD DAMAGED AT BS 500 - 520 LBL 60. NEW WEB AND UPPER CHORD FABRICATED IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK LIGHT CORROSION ON INNER FLANGE OF SEAT TRACK AT BS 485 - 495 RBL 66. SEAT TRACK REPLACED IAW SRM 51-80-02.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, CABIN MAIN DECK CORROSION ON UPPER CHORD OF CANTED PRESS BULKHEAD AT BS 260 RBL 35-48. UPPER CHORD REPAIRED IAW QUERY NOTE 17/01 AND SRM 53-10-04.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK SHEAR TIE IS CRACKED AT BS 1295 BETWEEN STRS 14 &15 LT SIDE. SHEAR TIE FABRICATED IAW SRM 51-30-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK SHEAR TIE CRACKED AT BS 1295 BETWEEN STRS 14 AND 15 LT. SHEAR TIE FABRICATED IAW EO 206671 AND INSTALLED IAW SRM 51-30-02.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK CORROSION ON UPPER CHORD BS 400 BULKHEAD RBL 15 TO 46. UPPER CHORD AT BS 400 RBL 15 - 46 REPAIRED IAW QUERY NOTE 6/01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK CORROSION ON UPPER CHORD OF BS 400 BULKHEAD RBL 15 TO 46. UPPER CHORD AT BS 400 RBL 15-46 REPAIRED IAW QUERY NOTE 6/01, ANGLES FABRICATED. HEAT TREATED 15-5 PH X.071 AND INSTALLED.

Part: BOLT — CORRODED (NR 4 FLAP TRACK) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 4 FLAP TRACK AFT LOCATING MOUNT BOLTS AND SHIMS CORRODED. NR 4 FLAP TRACK AFT MOUNT BOLTS AND SHIMS REPLACED IAW MM 27-51-22.

Part: FITTING — CRACKED (NR 3 ENTRY DR) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 3 ENTRY DOOR RT SIDE HINGE FITTING FOUND CRACKED AT BS 1265. FITTING REPLACED IAW SRM 51-30-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 3 ENTRY DOOR BS 1265 RT SIDE HINGE FITTING CRACKED. HINGE FITTING REPLACED IAW SRM 51-30-02.

Part: FITTING — CRACKED (PAX DOOR) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 3 ENTRY DOOR BS 1265 LT SIDE HINGE FITTING CRACKED. FITTING REPLACED IAW SRM 51-30-02.

Part: ANGLE — CRACKED (RT WING) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, RT WING FEAR STRUT DOOR I/B FAIRING SUPPORT ANGLE IS CRACKED. SUPPORT ANGLE REPLACED IAW SRM 51-30-02.

Part: FITTING — CRACKED (PAX DOORWAY) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, DOOR 3 RT STOP FITTINGS FWD NR 2 & 5 CRACKED. NOTE DOORWAY STOP FITTINGS NOT DOOR. FITTINGS REPLACED IAW SRM 51-30-02.

Part: ANGLE — CRACKED (RT MLG DOOR) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, RT WING GEAR STRUT DOOR I/B FAIRING SUPPORT ANGLE IS CRACKED. SUPPORT ANGLE REPLACED IAW SRM 51-30-02.

Part: SHAFT — CORRODED (FLAP TRACK) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 4, 2, 5, 6 AND 8 FLAP TRACK GENEVA SHAFTS CORRODED AND CHROME CHIPPED ON BRGS. FLAP TRACK ROLLER SHAFTS REPLACED, ALSO BEARINGS IAW MM 27-51-40.

Part: STOP — CRACKED (PAX DOORWAY) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 3 DOORWAY LT STOP FITTINGS NR 2 & 4 FWD STOP FITTINGS CRACKED. FITTINGS REPLACED IAW SRM 51-30-02.

Part: FITTING — CRACKED (PAX DOORWAY) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 3 LT DOORWAY FITTING NR 2 AND 4 CRACKED. REPLACED FITTINGS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK FUSELAGE FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 929 STR 24 LT. REPAIRED IAW SRM 53-10-04.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, DOOR 5 RT BOTTOM FWD CORNER OF DOOR FOUND CRACKED. REPAIR PLATE FABRICATED AND CAD PLATED. REPAIRED IAW SRM 52-10-00. ENDS OF CRACKS MARKED USING NDT HFEC NDTM PT 6 51-00-00 FIG 23.

Part: FRAME — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C MAIN CABIN CRACKING IN OUTER FLANGES OF FRAME AT BS 260 - 280 RT SIDE. REPAIRED IAW SRM 51-40-03.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN CABIN DOOR 2 RT BOTTOM FWD CORNER CRACKED. BOTTOM FWD CORNER REPAIRED VERTICAL FRAME IAW SRM 52-10-02, USING AI SI301X0.050 2024T3. ALSO, REPLACED PULLED RIVETS. NDT CARRIED OUT ON CRACKS TO DETERMINE ENDS IAW B747 NDTM D6-7170 PART 6 51-00-00 FIG 23.

Part: STOP — CRACKED (PAX DOOR) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C MAIN ENTRY DOOR NR 2 LT SIDE LOWER FWD STOP CRACKED. DOOR 2 LT CRACK IN FWD LOWER CORNER REPAIRED IAW SRM 52-10-02 STOP FITTING REPLACED.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C DOOR 1 LT BOTTOM FWD L/E CORNER OF DOOR CRACKED. DOOR 1 LT FWD LWR CORNER CRACK REPAIRED IAW SRM 52-10-02. NDT ACCOMPLISHED TO CONFIRM CRACK ENDS IAW SRM 52-10-02 FIG 10. CRACK REPAIRS IN VERTICAL FRAME.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, DOOR 1 RT BOTTOM FWD L/E CORNER FOUND CRACKED. BOTTOM FWD CORNER CRACK REPAIRED IAW SRM 52-10-02, REPAIR PARTS FABRICATED IAW BAC 5300 AND VERTICAL FRAME REPAIRED IAW 52-10-02 FIG 10. CRACK NDT INSPECTED TO MARK CRACK ENDS. ALSO, BLIND FASTNERS ON PREVIOUS REPAIR REPLACED WITH SOLIDS.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C DOOR 4 LT BOTTOM AFT L/E CORNER FOUND CRACKED. DOOR 4 FWD AND AFT LOWER CORNERS CRACK REPAIRED IAW SRM 52-10-02. TWO REPAIR PIECES CAD PLATED AND INSTALLED, CRACK ENDS CONFIRMED WITH NDT HFEC D6-7170 PT 6 CH 51-00-00 FIG 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK CABIN FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 920 STR 24 LT FOR REPAIR. FRAME WEB REPAIR CARRIED OUT IAW SRM 53-10-04.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, DOOR 4 LT BOTTOM L/E CORNER OF DOOR FOUND CRACKED. DOOR 4 LT FWD AND AFT LOWER CORNERS CRACKED, REPAIRED IAW SRM 52-10-02. ENDS OF CRACKS MARKED USING NDT ON HORZ BEAMS IAW SRM 52-10-02 FIG 10. CRACKS FOUND IN VERTICAL ANGLES.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C DOOR 4 RT BOTTOM FWD CORNER OF DOOR FOUND CRACKED. BOTTOM FWD CORNER OF DOOR CRACK REPAIRED IAW SRM 52-10-02 FIG 10. DOOR SKIN REPAIRED AT HINGE CUTOUTS PREVIOUS REPAIRS HAD BLIND FASTENERS. BLIND FASTENERS REMOVED AND SOLIDS INSTALLED IAW SRM 51-30 -02. FASTENERS MS 2024D6. REPAIR PARTS FABRICATED IAW BAC 53 00.

Part: CHANNEL — CRACKED (NR 5 FLAP TRACK) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, RT WING DIAPHRAM SUPPORT CHANNEL CRACKED IN TWO PLACES LOCATED ABOVE FLAP TRACK NR 5 AND AFT OF MOUNT. SUPPORT CHANNEL REPLACED IAW SRM 51-30-02. ANGLE FABRICATED PER BAC 5300 AND SOLUTION HEAT TREATED AND INSTALLED.

Part: BRACKET — CRACKED (RT WING) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, RT WING LOWER T/E SUPPORT BEAM CLIP CRACKED AT FWD SIDE OF LDG BEAM AT WS 500. BRACKET REMOVED AND REPLACED IAW SRM 51-30-02.

Part: CHANNEL — CRACKED (LT WING LE FLAP) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, LT WING L/E LEADING EDGE FLAP DRIVE UNIT SUPPORT CHANNEL CRACKED AT POSITION NR 2 LEFDU. SUPPORT CHANNEL REPAIRED IAW SRM 51-40-03.

Part: MOUNT — CRACKED (LE FLAP) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, R WING L/E KRUEGER FLAP NR 15 INBOARD HINGE MOUNT CRACKED. NEW FLAP ASSY FITTED IAW MM 27-81-01.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, RT WING LOOSE FASTENERS ON JOINT IN L/E BULL NOSE SECTION O/B AT WS 320. REPAIRED IAW SRM 57-30-04 FIG 1 AND Q/NOTE 5/01.

Part: DOUBLER — CRACKED (RT WING) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, RT WING L/E CRACK ON INNER STRUCTURE OF WING BULLNOSE JUST I/B OF NR 4 ENGINE. REPAIRED IAW SRM 51-40-03.

Part: FITTING — CRACKED (RT WING) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, RT WING L/E INBOARD UPSTOP FITTING IS CRACKED ON INBOARD LINKAGE OF VCF 20. UP STOP FITTING REPLACED IAW SRM 51-30-02.

Part: PANEL — DELAMINATED (NR 12 SPOILER) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 12 SPOILER PANEL IS DELAMINATED. SPOILER PANEL REPLACED AT NR 12 POSITION.

Part: FITTING — CRACKED (RT WING) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, RT WING L/E INBOARD SWAN NECK HINGE FITTING ON BULL NOSE OF VCF 20 IS CRACKED. REPLACED SWAN NECK HINGE FITTING INBOARD NR 20 VCF IAW MM 27-81-02.

Part: HINGE — CRACKED (LE FLAP) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, RT WING L/E NR 15 KRUEGER FLAP O/B FOLDING FAIRING ATTACH HINGE FITTING IS CRACKED. P/N 65B02471-10. DUE TO ADDITIONAL DAMAGE ON FLAP, FLAP REPLACED.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, KEEL BEAM CORROSION ON FAIRING SUPPORT BEAM AT BS 1000 BBL .0. BRACKET REPAIRED IAW SRM 51-20-01 AND SRM 51-30-02.

Part: SKIN — CORRODED (RT WING) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, RT WING L/E CORROSION ON L/E LWR IN SPAR SKIN AT OLES 833 RT. NDT INSPECTION OF AREA ACCOMPLISHED, DAMAGED REMOVED AND REPROTECTED IAW QUERY NOTE 2/01, BLEND OUTS PER INSTRUCTIONS.

Part: GUARD — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK CARGO PROFILE INDICATORS ARE CRACKED AT BS 1720 LT AND RT SIDES, LT MAX CARGO PROFILE INDICATOR CENTER ATTACH BRACKET TO FUSELAGE FRAME IS CRACKED. NEW PROFILE GUARDS FABRICATED IAW SRM 51-20-01 AND SRM 51-30-02.

Part: STRUCTURE — CORRODED (TE FLAP) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 1, 5 & 8 FLAP BALLSCREWS CORRODED AND NR 7 POSITION HAS WORN MOUNT BOLT HOLES. REPLACED 1, 5, 7, AND 8 BALLSCREWS.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK FRAME WEB IS CRACKED AT CUTOUT FOR STR AT BS 920 STR 24 RT. FRAME WEB REPAIRED IAW SRM 53-10-04.

Part: DOUBLER — DAMAGED (NR 3 PYLON) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, NR 3 ENGINE INBOARD LOWER PYLON SKIRT AREA DAMAGED ON THE INSIDE AFT OF REAR ENGINE MOUNT. REPAIRED SKIRT IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, MAIN DECK CABIN CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 1720 LBL 85-98. UPPER CHORD AT BS 1720 LBL 85-98 REPAIRED IAW QUERY NOTE 9/01 SPLICED IN A NEW SECTION OF UPPER CHORD FLOORBEAM PER SRM 51-40-04.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,872 hrs · 21,406 cycles

INSPECTION TYPE:C, DEFERRED DEFECT ITEM D18497 ACCOMPLISHED A TIME LIMITED REPAIR TO FUSE SKIN STA 1745-1794 PER EO B747-5330-10180A. RT SIDE OF A/C PERMANENT REPAIR TO BE ACCOMPLISHED. PERMANENT REPAIR ACCOMPLISHED PER UPS EO B747-5330-10810.

Part: MODULE — LEAKING (HYDRAULIC SYSTEM)

INSPECTION TYPE:N/A, ATB - NR 4 HYDRAULIC SYSTEM FLUID LOSS ON TAKEOFF. REMOVED AND REPLACED O/B FLAP CONTROL MODULE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 83,514 hrs · 21,115 cycles

INSPECTION TYPE:SP, INTERNAL SKIN IS CORRODED AT PREVIOUS REPAIR STA 972 - 976 ABOVE STRINGER 39R. REPAIRED SKIN IAW SRM 53-30-3 FIG 11.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A FOUND EMGY EXIT LIGHT OVER UPPER DECK DOOR INOP RECYCLED CIRCUIT BREAKERS FOR EMEGERENCY LIGHTING, LIGHTS OP CK NORM AL

Part: SKIN — CRACKED (WINDOW FRAME)

INSPECTION TYPE:N/A, NR 3 LT WINDOW FRAME CRACKED. REPAIRED CRACK IN SKIN PER B747 SRM 53-30-03.

Part: CONTROLLER — FAILED (COCKPIT)

INSPECTION TYPE:N, DURING CRUISE OBSERVED SMOKE IN COCKPIT. FOUND SMOKE COMING FROM LT WINDOW. TURNED OFF WINDSHIELD HEAT, SMOKED STOPPED. REMOVED AND REPLACED LOWER AFT WIRE TERMINAL. REMOVED AND REPLACED WINDOW HEAT CONTROLLER PRECAUTIONARY. OPS CK NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS BY MAIN DECK L5 DOOR INOP. REPLACED LIGHT ASSEMBLY, OPS CHECK OK REF MM 33-51-07.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:3-A, EMERGENCY LIGHTS BY MAIN DECK DOOR L-5 INOP. REPLACED LIGHT ASSEMBLY AND OPS CK GOOD.

Part: ACTUATOR — FAILED (NR 4 ENGINE)

INSPECTION TYPE:N/A, NR 4 ENG IN FLIGHT SHUTDOWN DUE TO S/O VLV CLOSED AND C/B POPPED. REPAIRED PIN CONNECTOR D2316J AND REMOVED AND REPLACED S/O VLV.

Part: COMPUTER — INOP (TE FLAP)

INSPECTION TYPE:N/A, AFTER TAKEOFF WHEN SELECTING FLAPS UP FROM FLAPS 1, CREW GOT WARNING HORN. AIR TURNBACK DUE TO WARNING HORN. REMOVED AND REPLACED AURAL WARNING CONTROL LOGIC MODULE. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, NR 1 LT DOOR EMERG LIGHT INOP (REF ITEM M 150853). FOUND PIN 9 PUSHED BACK INTO CONECTOR D1561J. REINSTALLED PIN PER 33-51-12, CHECKED NORMAL CLEARING M 150853.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP ENTRY DOOR AND THE CEILING MAIN DECK FWD OF STAIR AND AFT OF STAIR A370200 370204. REPLACED STA 600 BATTERY PACK (P/N S1356B37), (S/N 19553) ON, (S/N 1849 2359045) OFF, AFT OF STAIR REPLACED STA 600 BATTERY PACK (P/N 13J6B37) (S/N 25613) ON, (S/N 34035) OFF, BOTH CEILING AND ENTRY LIGHTS CHECKED OK.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE-1A, EMERGENCY LIGHT INOP ENTRY DOOR AND THE CEILING MAIN DECK FWD OF STAIR AND AFT OF STAIR. REPLACED BOTH BATTERY/LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN)

CREW UPPER DECK SLIDE DOOR EMERGENCY FWD LIGHT WILL NOT ILLUMINATE (DOOR SILL FRAME). REPLACED CARTRIDGE ASSY.

Part: LIGHT — INOPERATIVE (CREW DOOR)

INSPECTION TYPE-N/A REF M 146611, FWD SLIDE LIGHT CREW DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATT PACK AT FWD SLIDE, OPS GOOD THIS CLEARS M 146611 PLACARD REMOVED.

Part: DOUBLER — CORRODED (BS 1781-1841)

INSPECTION TYPE-N/A, STRINGER DOUBLER CORRODED FS 1781 TO 1841 STR 48R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-30-3 FIG 37.

Part: DOUBLER — CORRODED (BS 1781-1841)

INSPECTION TYPE-N/A, STRINGER DOUBLER CORRODED FS 1781 TO 1841 STR 51L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-30-2.

Part: DOUBLER — CORRODED (BS 1781-1841)

INSPECTION TYPE-N/A, STRINGER DOUBLER CORRODED FS 1781 TO 1841 STR 50R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-30-02.

Part: DOUBLER — CORRODED (BS 1781-1841)

INSPECTION TYPE-N/A, STRINGER DOUBLER CORRODED FS 1781 TO 1841 STR 49R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-30-2.

Part: DOUBLER — CORRODED (BS 1781-1841)

INSPECTION TYPE-N/A, STRINGER DOUBLER CORRODED FS 1781 TO 1841 STR 51R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-30-02.

Part: SHEAR TIE — CRACKED (BS 1820)

INSPECTION TYPE-N/A, FS 1820 BETWEEN STR 51L AND 50L SHEAR TIE CRACKED. REPAIRED IAW SRM 53-10-4 FIG 3.

Part: SHEAR TIE — CRACKED (BS 1780)

INSPECTION TYPE-N/A, FS 1780 BL 0 SHEAR TIE CRACKED. REPAIRED IAW SRM 53-10-04 FIG 3.

Part: SHEAR TIE — CRACKED (BS 1780)

INSPECTION TYPE-N/A, SHEAR TIE CRACKED FS 1780 BETWEEN STR 48R AND 49R. REPAIRED IAW SRM 53-10-04 FIG 3.

Part: SHEAR TIE — CRACKED (BS 1840)

INSPECTION TYPE-N/A, SHEAR TIE CRACKED FS 1840 BETWEEN STR 51R AND 50R. REPAIRED IAW SRM 53-10-4 FIG 3.

Part: SHEAR TIE — CRACKED (BS 1800)

INSPECTION TYPE-N/A, CRACKED SHEAR TIE FS 1800 BL 0. REPAIRED IAW SRM 53-10-04 FIG 3.

Part: SHEAR TIE — CRACKED (BS 1840)

INSPECTION TYPE-N/A, SHEAR TIE CRACKED FS 1840 BETWEEN STR 47R AND 48R. REPAIRED IAW SRM 53-10-04 FIG 3.

Part: SHEAR TIE — CRACKED (BS 1840)

INSPECTION TYPE-N/A, SHEAR TIE CRACKED FS 1840 BETWEEN STR 50R AND 49R. REPAIRED IAW SRM 53-10-04 FIG 3.

Part: SHEAR TIE — CRACKED (BS 1780)

INSPECTION TYPE-N/A, SHEAR TIE CRACKED FS 1780 BETWEEN STR 50L AND 51L. REPAIRED IAW SRM 53-10-04 FIG 3.

Part: STRINGER — CORRODED (BS 1800-1820)

INSPECTION TYPE-N/A, FS 1800 TO 1820 STRINGER 48R HAS EVIDENCE OF CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 8.

Part: SHEAR TIE — CRACKED (BS 1820)

INSPECTION TYPE-N/A, SHEAR TIE CRACKED FS 1820 BL 0. REPAIRED IAW SRM 53-10-04 FIG 3.

Part: SKIN — CORRODED (BS 1740-1770)

EXT LOWER BELLY SKIN CORROSION APPOX 20 INCHES IN DIAMETER AT BL 0 AND BS 1740-1770. DEFERRED FOR ONE TIME FERRY FLIGHT. FERRY PERMIT NR 9029/DMI NR 145983. TRANSFERRED TO NRC 735004. REMOVED CORROSION ON LWR BELLY SKIN IAW SRM 51-10-1. UT THICKNESS PER B747 NTM PT.1, 51-04-00, NOMINAL THICKNESS .065- .070. AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-30-01 FIGS 1 AND 2. TREATED AREA IAW SRM 51-10-02. LOG PAGE 412 ITEM 3.

Part: FASTENERS — CRACKED (BS 1830-1850)

INSPECTION TYPE-N/A, EVIDENCE OF CORROSION AND CRACKED FASTENER HEADS FROM STA 1830 TO 1850 AT STRINGER 48R. *S/D* DEFERRED FOR ONE TIME FERRY FLIGHT. FERRY PERMIT NR 9029/DMI NR 145981, REF CONTROL NR UPS98425665 FOR CORRECTIVE ACTION.

Part: STRINGER — CORRODED (BS 1820-1840)

INSPECTION TYPE-N/A, EVIDENCE OF CORROSION FROM STA 1820 TO 1840 AT STRINGER 51R. *S/D* INSTALLED TEMPORARY REPAIR DOUBLER FOR FERRY FLIGHT TO HAVE PERMANENT REPAIR INSTALLED. TEMP REPAIR WAS INSTALLED PER SRM 53-30-03. FERRY PERMIT NR 9029, REF CONTROL NR UPS98425677 FOR CORRECTIVE ACTION.

Part: SKIN — CORRODED (BS 1830-1850)

INSPECTION TYPE-N/A, FROM DEFERRED ITEM D145981 - EVIDENCE OF CORROSION AND CRACKED FASTENER HEAD FROM FS 1830 TO 1850 STR 48R. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-03.

Part: LIGHTS — INOPERATIVE (CABIN)

MAIN DECK EMERGENCY LIGHTS IN CEILING AND L1 DOOR FRAME ARE INOP. INSTALLED MAIN DECK EMERGENCY LIGHT ASSY IN POSITIONS STA 550 AND STA 350. ALL EMERGENCY LIGHTS OPERATE NORMALLY IAW M/M 33-50.

Part: FITTING — CRACKED (L 1 DOORWAY)

INSPECTION TYPE:C FROM BODY DOOR TORQUE TUBE CUTOUT AT MED 1L IS UPPER FITTING CRACKED. REPLACED FITTING AT BODY TORQUE TUBE DOOR CUTOUT UPPER FITTING ACC SRM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 440)

INSPECTION TYPE-C, UPPERDECK FLOOR STRUCTURE FOUND CORROSION ON TOP OF FLOORBEAM AT BS 440 RBL 48. REPAIRED UPPER CHORD AT BS 440 RBL 48 ACC EFN 747-53-0859 AND KLM DFX 97-304.

Part: SKIN — CORRODED (RT WING)

INSPECTION TYPE-C, FOUND CORROSION AT RT WING LOWER SKIN AT BOOST PUMP HOUSING INBD ACCESS OPENING (BETWEEN HOUSING AND SKIN). REMOVED CORROSION FROM LOWER WING SKIN ACC SRM 51-10-01. LOWER SKIN OUT OF LIMITS ACC SRM 57-30-03 FIG 3. REPAIRED LOWER SKIN ACC KLM DFX-97-288. REPAIR APPROVED PER UPS EFN 747-57-0405.

Part: SKIN — CORRODED (RT WING)

INSPECTION TYPE-C, FOUND CORROSION AT RT WING LOWER SKIN AT OUTB BOOST PUMP HOUSING ACCESS OPENING, (BETWEEN HOUSING AND SKIN). REMOVED CORROSION FROM LOWER WING SKIN ACC SRM 51-10-01. LOWER SKIN OUT OF LIMITS ACC SRM 57-30-03 FIG 3. REPAIRED LOWER SKIN ACC KLM-DFX-97-288. REPAIR APPROVED PER UPS EFN-747-57-0405.

Part: SKIN — CORRODED (RT WING)

INSPECTION TYPE-C, FOUND CORROSION RT WING AT UPPER SKIN EXTENSION LOWER SIDE ILES 762. REMOVED FASTENERS FROM UPPER WING SKIN ACC SRM 511-30-02. REMOVED CORROSION FROM UPPER SKIN ACC SRM 51-10-01. UPPER SKIN OUT OF LIMITS ACC SRM 57-30-01 FIG 1. REPAIRED UPPER SKIN ACC KLM DFX97-285. REPAIR APPROVED PER UPS EFN-747-57-0406. INSTALLED FASTENERS FROM UPPER SKIN ACC SRM 51-30-02.

Part: BULKHEAD ANGLE — CRACKED (BS 2360)

INSPECTION TYPE-C, FOUND CRACK AT PRESS BULKHEAD ANGLE JUST BELOW STR 5 LT BS 2360. REPLACED ANGLE AT PRESS BULKHEAD BS 2360 STR 5 LT ACC SRM 51-30-02.

Part: FRAME — CRACKED (BS 320)

INSPECTION TYPE-C, S-41 MOD REPLACEMENT OF FRAME 320 FLIGHTDECK BETWEEN STR 0-1 RT EXISTING T-PROFILE CRACKED. REPAIRED T-PROFILE ON FRAME 320 FLIGHT DECK ACC KLM DFX-97-294 R3, EFN 747-53-0853.

Part: WEB — CORRODED (BS 1320)

INSPECTION TYPE:C FOUND CORROSION ON PRESS DECK WEB AT LOWER SIDE AT BS 1320 BETWEEN LBL 108/115. REPAIRED PRESSURE DECK WEB LOWER SIDE ACC EFN 747-53-0856 AND KLM DFX 97-281 AT BS 1320 BETWEEN LBL 108/115.

Part: SKIN — CORRODED (BS 1000)

INSPECTION TYPE:C, CORROSION FOUND ON SKIN CENTER WING BS 1000 LBL 90. REMOVED CORROSION ACC SRM 57-10-01. OUT OF LIMITS ACC SRM 53-10-01. REPAIRED ACC KLM DFX 97-290 REV 2 AND UPS EFN 747-57-0408.

Part: CLIP — CRACKED (WS 543.93)

INSPECTION TYPE-C, FOUND CLIP CRACKED ON LE RIB TO FRONT SPAR UP CHORD AT ILES 543.93. REPLACED CLIP IN ACC WITH SRM 51-30-02 AND DWG 65B15969.

Part: BULKHEAD DOUBLER — MISINSTALLED (BS 2360)

INSPECTION TYPE-C, FOUND DOUBLER INSTALLED ON AFT PRESSURE BULKHEAD WHO HAS INTERFERENCE WITH EO B747-5310-1332-C APU CUTOUT REINFORCEMENT. REPAIRED PRESSURE BULKHEAD AT BS 2360 ACC EFN 747-53-0849 (KLM DFX 97-270).

Part: RIB — CRACKED (WS 1140)

INSPECTION TYPE-C, RT WING AT WS 1140 RIB, FWD UPPER STRINGER CUTOUT RIB CRACKED. CRACK LENGTH APPROX 1.25 INCH. RT WING STA 1140 RIB REPAIRED ACC TLX UPS-AMS-97-0376RE,-0388RE, -0394RE AND 811-3 NM 1518, UPS EFN 747-57-0407, KLM DFX 97-287.

Part: WEB — CORRODED (BS 1410-1430)

INSPECTION TYPE:C, FOUND CORROSION IN PRESS DECK WEB BETWEEN BS 1410-1430 LBL 98.58. REPAIRED PRESS DECK AT BS 1410 - 1430 LBL 98.58 ACC UPS EFN 747-53-0855 AND KLM DFX 97-284 REV. 3.

Part: WEB — DAMAGED (BS 1380)

INSPECTION TYPE-C, FOUND DURING PERFORMING SB 53-2224, 3 X .4375 HOLES IN PRESSURE DECK WEB THAT SHOULD BE .25 HOLES BS 1380 RBL 99. REPAIRED PRESSURE DECK WEB AT RBL 99 BS 1380 ACC EFN 747-53-0403. (KLM DFX 97-275).

Part: FRAME — CORRODED (BS 1416)

INSPECTION TYPE-C, RBLG BS 1416 FAIRING FRAME CORRODED AT FWD SIDE. REPAIRED FRAME IN ACC WITH KLM-DFX-97-282 AND APPROVED PER UPS-EFN-747-53-0851.

Part: WEB — CRACKED (BS 1440)

INSPECTION TYPE-C, DURING PERFORMING SB 53-2224 FOUND CRACK IN PRESSURE DECK WEB BS 1440 LBL 33.99. REPAIRED PRESSURE DECK WEB CRACK AT BS 1400 LBL 33.99 ACC SRM 53-10-07 FIG 2.

Part: T-FITTING — CRACKED (VERT STAB)

INSPECTION TYPE-C, FOUND T-FITTING CRACKED AT FIN STA 143 2ND RIB FROM BELOW. INTERNAL LT SIDE JUST AFT OF FRONT SPAR FROM VERT STAB. REPLACED T-FITTING AT FIN STA 143 LT ACC SRM 51-30-02.