N683UP

Part: ELECTRONIC UNIT — SMOKE (FUEL FLOW)

FUEL FLOW ELECTRONICS UNIT SMOKING. REMOVED AND REPLACED FUEL FLOW ELECTRONICS UNIT PER MM 73-31-02. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

AF L1 DOOR ENTRY EMERGENCY LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT/BATTERY PACK ASSY WITH REF TO MM 33-51-07. OPS CHECK GOOD PER SAME.

Part: WEB — CRACKED (NLG WW) · airframe 91,449 hrs · 22,375 cycles

INSPECTION TYPE:C NWW RT SIDE PANEL STA 294 WL 170 SIDE PANEL WEB 1EA SUSPECT CRACK INDICATION FOUND ADJACENT LWR SIDE OF EXTERNAL STRAP APPROX. 0.5" LENGTH CRACK LENGTH 0.5" APPROX. NOSE WHEEL WELL SIDE PANEL REPAIRED AT BS 293 - BS 295 WL 170 AREA AS PER SRM 53-10-04 FIG 116 SUBSEQUENT INSPECTIONS ARE NECESSARY AS PER SRM 53-10-04 FIG 116 TABLE II.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT CONTROL SWITCH INDICATOR 1/2 INOP. RELAMPED EMERGENCY, OPS CHECK GOOD.

Part: MODULE — UNKNOWN (NR 3 HYD SYSTEM)

HYD SYSTEM 3 FAILURE PRESSURE & QUANTITY ZERO DURING FLAP RETRACTION. HYD SYSTEM PR & QT LIGHTS ON. REMOVED AND REPLACED MODULAR ASSY & LEAK CHECK IAW 29-11-23.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER CRACK REVEALED AT THE EDGE OF BEAR STRAP. CRACK LENGTH 2.5 INCHES APPROX. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782 AND UPS EO B747-5330-15047.

Part: FLOOR SUPPORT — CRACKED (BS 1220) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 1220 LBL 98.8 FLOOR WEB SUPPORT FOUND CRACK AS MARKED. CRACK LENGTH .375 INCH. M/D BS 1220 LBL 98.8 FLOOR WEB SUPPORT REPAIRED AS PER RS R53-15-35777 AND UPS ENGINEERING FILE 747-53-20406.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT I) FOUND CRACK THRU THICKNESS AT 5:00 O/C POSITION (LOOKING I/B) CRACK LENGTH 2.5 INCH. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT C) FOUND CRACKED AT BEAR STRAP .0625 INCH AT 11 O/C POSITION AND ANOTHER CRACK AT SKIN AND BEAR STRAP .0625 INCH AT 5 O/C POSITION (LOCKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER R R53-41-35782. WORK DETAIL REFER NRC51976 AND UPS EO B747-5330-15047.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT D) FOUND CRACKED AT SKIN .125 INCH APPROX RUNNING FWD AT 5 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC 51976 AND UPS EO B747-5330-15047.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT G) FOUND CRACKED AT BEAR STRAP .125 INCH TO UPWARD AT 11 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC51976 AND UPS EO B747-5330-15047.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1E FASTENER HOLE (IDENT F) FOUND CRACKED AT BEAR STRAP .125 INCH APPROX RUNNING UPWARD AT 12 O/C POSITION (LOOKING I/B). CRACK LENGTH .125 INCH. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC 51976 AND UPS EO B747-5330-15047.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD COVER CORNER 1EA FASTENER HOLE (IDENT B) FOUND CRACKED AT BEAR STRAP .0625 INCH TO FWD AT 5 O/C POSITION (LOOKING I/B). CRACK LENGTH .0625 INCH. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC 51916 AND UPS EO B747-5330-15047-A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C 1EA FASTENER HOLE (IDENT A) FOUND CRACKED AT RIGHT NR 3 PAX DOOR CUTOUT AREA FWD LOWER CORNER AT SKIN I/B FACE CRACK LENGTH 0.040 INCH APPROX WHICH RUNNING FWD AT 5 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC51976 AND UPS EO B747-5330-15047.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT E) FOUND CRACKED AT SKIN AND BEAR STRAP .125 INCH TO UPWARD AT 12 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC51976 AND UPS EO B747-5330-15047-A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT H) FOUND THROUGH THICKNESS CRACKED AT 7 O/C POSITION AND .0625 INCH CRACKED TO FWD AT BOTTOM OF HOLES BORE AT 5 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782. WORK DETAIL REFER NRC51976 AND UPS EO B747-5330-15047.

Part: STRINGER — CRACKED (BS 820-840 S10L) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 820-840 STR 10 LT STRINGER ATT WEB FOUND CRACKED. CRACK LENGTH .75 INCH. M/D BS 820-840 STR 10 LT ATTACH WEB REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: STRINGER — CRACKED (BS 820-840 S10R) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 820-840 S10 RIGHT STRINGER ATT WEB FOUND CRACK. CRACK LENGTH .625 INCH. M/D BS 820-840 STR 10R ATTACH WEB REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: FRAME — CRACKED (BS 820 S11-12R) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 820 STR 11-12R FRAME FOUND CRACK. CRACK LENGTH .875 - 1 INCH. M/D BS 820 STR 11-12R FRAME REPAIRED AS PER RS R53-12-35770. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-12-35770 AND UPS EO B747-5310-26322.

Part: WEB — CRACKED (BS 1500-1520) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C AFT CARGO COMPT LT VERTICAL WEB FOUND CRACKED AT STA 1500 TO STA 1520 STR 34L AFT EDGE AREA. CRACK LENGTH .75 INCH. VERTICAL WEB REPLACED PER SRM 51-10-01 PG 9.

Part: PRESSURE PANEL — CORRODED (LT MLG WW) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT BODY LANDING GEAR W/W PRESSURE DECK ATT WEB FOUND SURFACE CORROSION AT STA 1403 LBL 125. CORROSION BLEND OUT 0.034 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. LEFT BODY LANDING GEAR W/W PRESSURE DECK ATT WEB REPAIRED AT STA 1403 LBL 125 AREA AS PER SRM 53-10-07 FIG 2, SUBSEQUENT INSPECTION IS REQ'S AS PER SRM 53-10-07 FIG 2 SHT 7 TABLE 2.

Part: FLOOR SUPPORT — CORRODED (BS 1920-1940) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C BULK CARGO COMPT LEFT STA 1920 TO STA 1940 LBL 55" FLOOR SUPPORT UNDER ANCHOR NUT FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.025" X .5" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. BULK CARGO COMPT LEFT BS 1920 TO 1970 LBL 55" FLOOR SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: SKIN — CRACKED (R3 DOOR) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D R3 DOOR SKIN FOUND CRACKED APPROX AT CTR LOWER PORTION. CRACK LENGTH .375 INCH. M/D R3 DOOR SKIN AT CTR LOWER PORTION AREA REPAIRED AS PER SRM 52-10-02 FIG 9.

Part: SKIN — CRACKED (L3 DOOR) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D L3 DOOR SKIN FOUND CRACKED APPROX AT CTR LOWER PORTION. CRACK LENGTH .75 INCH. L3 DOOR SKIN REPAIRED AS PER SRM 52-10-02 FIG 9.

Part: SILL — CRACKED (BS 400) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C U/D RIGHT DOOR SILL BS 400 RBL TO FLOOR SUPPORT CHORD FOUND CRACKED. CRACK LENGTH: .75 INCH. FLOOR SUPPORT CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SUPPORT — CORRODED (BS 1940-2045) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C BULK CARGO COMPT SLOPE PANEL SUPPORT SEVERAL LOCATION FOUND SURFACE CORROSION AT STA 1940 TO STA 2045 LBL 60 ANCHOR NUT AREA. CORROSION BLEND OUT 0.025" X .5" X 2" EXCEED SRM 53-10-01 FIG 1 LIMITS. SLOPE PNL SUPPORT BS 1940-2010 COR REMOVED & REPROTECTED AS PER SRM 51-10-01 & 51-10-02 ORG 0.050" BLEND OUT 0.005" X .5" X 1" WITHIN SRM 53-10-01 FIG 1 LIMITS. BS 2010-2070 COR SUPPORT REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: SUPPORT — CORRODED (BS 1960) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C BULK CARGO COMPT - STA 1960 LEFT SIDEWALL SUPPORT ANCHOR NUT AREA FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.049" X .5" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. BULK CARGO COMPT - STA 1960 LEFT SIDEWALL SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: DOOR FRAME — CRACKED (L5 DOORWAY) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D L5 DOOR UPPER FRAME FOUND CRACKED AT SEVERAL FASTENER HOLE AREA. CRACK LENGTH .375 INCH. M/D L5 DOOR UPPER FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: SUPPORT FITTING — CRACKED (BS 980) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C FWD CARGO COMPT AFT FIXED END STOP SUPPORT FITTING FOUND CRACK AT STA 980 RBL 45. CRACK LENGTH .75 INCH. FWD CARGO COMPT AFT FIXED END STOP SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02, JUST AT STA 980 RBL 45.

Part: SHEAR TIE — CRACKED (LWS 469) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT WING WS 469.8 FWD OF UPPER STR 29 SHEAR TIES FOUND CRACKED AS MARKED. CRACK LENGTH .5 INCH. LEFT WING WS 469.8 FWD OF UPPER STR 29 SHEAR TIE REPAIRED AS PER SRM 57-10-05 FIG 7.

Part: FLOORBEAM — CRACKED (BS 1940) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C BULK CARGO COMPT M/D FLOORBEAM LOWER WEB FOUND CRACK AT 1940 RBL 64". CRACK LENGTH .5 INCH. BULK CARGO COMPT M/D FLOORBEAM LOWER WEB REPAIRED AS PER SRM 51-40-02 FIG 1, JUST AT STA 1940 RBL 64 AREA.

Part: STRINGER — CRACKED (BS 2185 S51R) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C BULK CARGO COMPT STRINGER FOUND CRACK AT STA 2185 STR 51R. CRACK LENTH .375 INCH. BULK CARGO COMPT BS 2185 STR 51R REPAIRED AS PER RS R53-11-35768 AND UPS ENGINEERING FILE NUMBER 747-53-20407.

Part: SUPPORT — CORRODED (BS 2080) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C BULK CARGO COMPT - STA 2080 LT SIDEWALL SUPPORT ANCHOR NUT AREA FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.038" X 1" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. BULK CARGO COMPT BS 2080 LEFT SIDEWALL SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: DOOR FRAME — CRACKED (BS 2231 S24-25R) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 2231 FRAME AT DOOR NR 5 BETWEEN S24R-25R FOUND 2EA HOLE CRACK. CRACK LENGTH .125 INCH, .25 INCH AND .1875 INCH. M/D RIGHT BS 2231 FRAME REVEAL, STRAP AND CHORD REPAIRED AS PER RS R53-62-35764. CONTINUE INSPECTION IS REQUIRED PER RS R53-62-35764 AND UPS EO B747-5310-26334.

Part: FRAME — CRACKED (R5 DOOR) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D R5 DOOR UPPER FRAME FOUND CRACKED AT SEVERAL FASTENER HOLE AREA. CRACK LENGTH .75 INCH. FRAME REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: STRINGER — CRACKED (BS 360-380) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 380 S14EL FOUND CRACK. CRACK LENGTH .25 INCH. M/D BS 360-380 STRINGER S14EL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FLOOR SUPPORT — CORRODED (BS 1940) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C BULK CARGO COMPT LEFT STA 1940 LBL 55 FLOOR SUPPORT FOUND CORRODED CRACK AS MARKED. CORROSION BLEND OUT 0.025" X .5" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. BULK CARGO COMPT FLOOR SUPPORT REPLACED WITH EXISTING SPLICE FROM BS 1920-1970 LBL 55 PER SRM 51-10-01 PG 9 & INSTALLED PER SRM 51-30-02 REF NRC NO AFQ516607 FOR DETAIL.

Part: WEB — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C U/D RIGHT CREW DOOR SILL AREA I/B VERTICAL WEB AND ANGLE FOUND CRACKED. CRACK LENGTH .5 INCH. VERTICAL WEB AND ANGLE REPLACED PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: SKIN — CORRODED (BS 1210-1220) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 1210-1220 LBL 97 WING CTR SECTION TOP SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.043 X .5 X 2 INCHES EXCEED SRM LIMIT. M/D BS 1210-1220 LBL 97 WING CTR SECTION TOP SKIN REPAIRED AS PER RS R57-14-35765 AND UPS EO B747-5730-15819.

Part: SUPPORT — CORRODED (BS 2080-1260) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C BULK CARGO COMPT RIGHT SLOPE PANEL SUPPORT SEVERAL LOCATION CORROSION AT STA 2080 TO STA 2160 RBL 60 ANCHOR NUT AREA. CORROSION BLEND OUT 0.026" X 1" X 1" EXCEED SRM LIMIT. BULK CARGO COMPT BS 2040 - 2160 RBL 60 SLOPE PANEL SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: ATTACH FITTING — CRACKED (RT WING) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT WING L/E RIB TO FRONT SPAR UPPER CHORD ATT FITTING AT ILES 340 FOUND CRACKED. CRACK LENGTH .375 INCH. RIGHT WING L/E RIB TO FRONT SPAR UPPER CHORD ATTACH AT ILES 340 REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: REVEAL — CRACKED (BS 2231) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 2231 FRAME AREA 2EA FASTENER HOLE CRACK FOUND AT REVEAL BETWEEN S25R AND S26R. CRACK LENGTH .25 INCH, .125 INCH, AND .1875 INCH. M/D RIGHT BS 2231 FRAME REVEAL, STRAP AND CHORD REPAIRED AS PER RS R53-62-3764. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-62-35764 AND UPS EO B747-5310-26334.

Part: WEB — MISREPAIRED (NR 1 NACLLE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C NR 1 PYLON LWR WEB CRACK PREVIOUS REPAIR DOES NOT APPEAR TO COVER ENTIRE CONDITION. CRACK LENGTH .75 INCH. WEB REPAIRED PER SRM 54-10-03 FIG 2.

Part: FRAME — CRACKED (R4 DOOR) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D R4 DOOR UPPER FWD FRAME FOUND CRACKED. CRACK LENGTH 1.25 INCH. FWD FRAME REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT WING L/E RIB TO FRONT SPAR UPPER CHORD ATT FITTING AT ISLES 270 FOUND CRACKED. CRACK LENGTH: .25 INCH. UPPER CHORD ATT CLIP REPLACED PER SRM 51-10-01 PG 9 & INSTALLED PER SRM 51-30-02.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D L4 DOOR LOWER AFT CORNER FRAME FOUND CRACKED. CRACK LENGTH 1.5 INCH. FRAME REPAIRED AS PER SRM 52-10-02 FIG 10 AT M/D L4 DOOR AFT VERTICAL FRAME CORNER AREA.

Part: STRINGER — CORRODED (BS 1620 S35L) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C AFT CARGO LEFT STA 1620 S35L FOUND CORROSION CRACK AS MARKED. CORROSION BLEND OUT 0.030" X .5" X .5" EXCEED SRM LIMIT. AFT CARGO COMPT BS 1610 TO BS 1630 STR 35L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: RIB — DAMAGED (BS 1500-1520) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C AFT CARGO LEFT STA 1500-STA 1520 S34L WEB 3 RIBS DAMAGED AT LOWER EDGE AS MARKED. REPLACED THE 3 RIBS AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 1960) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C BULK CARGO LT STA 1960 LBL 56" FLOOR SUPPORT CORRODED AS MARKED. CORROSION BLEND OUT 0.025" X .5" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS, BULK CARGO COMPT FLOOR SUPPORT REPLACED WITH EXISTING SPLICE FROM BS 1920-1970 LBL 55 - 57" PER SRM 51-10-01 PG 9 & INSTALLED PER SRM 51-30-02 REF NRC NO AFQ516607 FOR DETAIL.

Part: STRINGER — CRACKED (BS 1601 S34R) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C AFT CARGO RIGHT STA 1601 S34R STRINGER FOUND CRACKED. CRACK LENGTH .3125 INCH. AFT CARGO COMPT BS 1590 TO BS 1630 STR 34R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (BS 1652 S32R) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C AFT CARGO RIGHT STA 1652 STR 35R STRINGER FOUND CORROSION CRACKED. CRACK LENGTH .75 INCH. AFT CARGO COMPT BS 1650 TO BS 1670 STR 35R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: FRAME — CRACKED (BS 800) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 800 FRAME FOUND 2EA FASTENER CRACKS AT STRAP LAYER. CRACK LENGTH 0.125 INCH AND 0.025 INCH. FRAME REPAIRED AS PER RS R53-12-35762 AT BS 800 STR 16R TO STA 18R STRAP AREA AND REFER UPS EO B747-5310-26131.

Part: STRINGER — CRACKED (BS 1650) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C AFT CARGO RIGHT STA 1650 S38R STRINGER FOUND CRACK. CRACK LENGTH .375 INCH. AFT CARGO COMPT BS 1630 TO BS 1650 STR 38R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: INTERCOSTAL — CRACKED (BS 2220) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 2220 RBL 58 INTERCOSTAL WEB VERTICAL ANGLE FOUND CRACKED. CRACK LENGTH .5 INCH. M/D BS 2220 RBL 58 INTERCOSTAL WEB VERTICAL ANGLE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CORRODED (BS 1820) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C AFT CARGO LEFT STA 1820 FRAME LBL 90 FOUND CORRODED UNDER ANCHOR NUT AREA AS MARKED. CORROSION BLEND OUT 0.020" X .5" X .5" EXCEED SRM LIMIT. AFT CARGO LEFT BS 1820 FRAME LBL 90" AREA REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: FRAME — CORRODED (BS 1840) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C AFT CARGO LEFT STA 1840 FRAME LBL 90 FOUND CORRODED UNDER ANCHOR NUT AREA AS MARKED. CORROSION BLEND OUT 0.024" X .875" X 1" EXCEED SRM LIMIT. AFT CARGO BS 1840 LBL 90" FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: FLOORBEAM — CORRODED (BS 1940) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 1940 RBL 89 TO 92 FLOORBEAM UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.082" X 1" X 1" EXCEED SRM LIMIT. M/D BS 1940 RBL 70" TO 92" RIGHT O/B FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 3.

Part: BAFFLE — CRACKED (NR 2 PYLON) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C NR 2 PYLON NAC STA 180 VERT FLANGE L/R LOWER CLEATS BROKEN AND CRACKED. CRACK LENGTH .375 INCH. NR 2 PYLON NAC STA 180 VERTICAL BAFFLE AND CLEATS REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D R3 DOOR CUTOUT FWD LOWER CORNER SKIN AND STRAP FOUND CRACKED. CRACK LENGTH 2.5 INCHES. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782.

Part: STRINGER — CRACKED (BS 1650) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C AFT CARGO - RIGHT STA 1650 S37R STRINGER FOUND CRACKED. CRACK LENGTH .375 INCH. AFT CARGO COMPT BS 1630 TO BS 1670 STR 37R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: DOUBLER — CRACKED (R1 DOOR) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D - R1 DOOR SKIN ATT DOUBLER FOUND CRACKED AT LOWER LINK AREA. M/D - R1 DOOR SKIN DOUBLER REPLACED AND INSTALLED AS PER SRM 52-10-02 FIG 11.

Part: STRINGER — CRACKED (BS 1601) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C AFT CARGO RIGHT STA 1601 S37R STRINGER FOUND CRACKED. CRACK LENGTH .25 INCH. AFT CARGO COMPT BS 1590 TO BS 1630 S37R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: STRINGER — CRACKED (BS 1640 S32L) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C AFT CARGO LEFT STA 1640 STR 32L STRINGER FOUND CRACK APPROX .125 INCH AS MARKED. AFT CARGO LEFT STRINGER S32L REPAIRED AS PER SRM 53-10-03 FIG 1, JUST BETWEEN STA 1630 AND 1670.

Part: SKIN — CRACKED (LT WING) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT WING UPPER SURFACE I/B LEADING EDGE SKIN FOUND CRACKED AT WS 450 AFT NR 12 K/FLAP. LEFT WING UPPER SURFACE LEADING EDGE SKIN REPAIRED AS PER SRM 57-30-04 FIG 2.

Part: FLOORBEAM — CORRODED (BS 860) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 860 LBL 80-97 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.040 X 2 X 2 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 860 LBL 65 TO MOST LEFT O/B FLOORBEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FLOORBEAM — CRACKED (BS 860) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 860 LBL 47 TO 49 FLOORBEAM WEB FOUND CRACKED. CRACK LENGTH: .75 INCH. M/D FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FTG 11 JUST AT BS 860 BETWEEN LBL 39 & LBL 49.

Part: FRAME — CRACKED (BS 360 S14-16R) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 360 STR 14-16R FRAME AFT FACE O/B AREA FOUND CRACKED. CRACK LENGTH .375 & .25 INCH. M/D BS 360 STR 13R TO STR 18R FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: FRAME — CRACKED (BS 360 S17-18R) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 360 STR 17-18R FRAME AFT FACE O/B AREA FOUND CRACKED. CRACK LENGTH .25 & .3125 INCH. M/D BS 360 STR 13R TO STR 18R FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: ATTACH FITTING — CRACKED (BS 960-980) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 960 TO 980 RBL 11 INTERCOSTAL WEB FWD ATT FITTING FOUND CRACKED. CRACK LENGTH .375 INCH. M/D BS 960 TO 980 RBL 11 INTERCOSTAL WEB FWD ATT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: RIB — CRACKED (LWS 1349) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT WING - 3VC FLAP I/B ACTUATOR ATTACH L/E RIB AT OLES 1349.25 CD LINK PTD AREA FOUND CRACK. CRACK LENGTH 0.375 INCH. LEFT WING NR 3VC FLAP I/B ACTUATOR O/B RIB AT OLES 1349.25 REPAIRED AS PER HX RS R57-42-35766, & UPS EO B747-5740-15105.

Part: STIFFENER — CRACKED (BS 1500) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D STA 1500 RBL 58 FLOOR SUPPORT INTERCOSTAL WEB ATT STIFFENER FOUND CRACKED. CRACK LENGTH .25 INCH. SUPPORT STIFFENER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: REVEAL — CRACKED (L5 DOOR) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D L5 DOOR CUTOUT REVEAL FOUND CRACKED AT LOCK RELEASE LEVER AREA. CRACK LENGTH .5 INCH. M/D L5 DOOR CUTOUT REVEAL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (BS 360 S24-26L) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 360 STR 24AL-26L FRAME AFT FACE ATT DOUBLER FOUND CRACK. LENGTH .75 INCH. M/D BS 360 BETWEEN STR 24AL & 27L FRAME AFT FACE ATT DOUBLER REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (BS 380 S14-15L) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 380 STR 14-15L FRAME FWD FACE FOUND CRACK. CRACK LENGTH 1 INCH. M/D BS 380 STR 14-15L FRAME FWD FACE REPAIRED AS PER RS R53-10-35758. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-10-35758 AND UPS EO B747-5310-26303.

Part: FLOORBEAM — CRACKED (BS 960) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 960 RBL 9 TO 11 FLOORBEAM WEB FOUND CRACKED. CRACK LENGTH .75 INCH. M/D FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11, JUST AT BS 960 BETWEEN RBL 6 AND RBL16 AREA.

Part: SEAT TRACK — CORRODED (BS 2130-2140) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 2130-2140 LBL 85 SEAT TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.029" X .5" X 20" EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 2110-2150 LBL 85" SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: RIB — CRACKED (LT WING) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT WING NR 5 VC FLAP I/B ACTUATOR ATT L/E SUPPORT RIB AT OLES 1205 ORIGINAL CRACK EXTENDED TOWARD O/B. CRACK LENGTH .25 INCH. LEFT WING NR 5 VC FLAP I/B ACTUATOR L/E SUPPORT RIB AT OLES 1205 REPAIRED AS PER RS R57-42-35767. REPEAT INSPECTION IS REQUIRED AS PER RS R57-42-35767 AND UPS EO B747-5740-26319.

Part: SEAT TRACK — CORRODED (BS 908-910) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 908-910 LBL 11 SEAT TRACK BOTH SIDE FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.022" X .75" X 3" IS EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 890-930 LBL 11" SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: FLOORBEAM — CRACKED (BS 340) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 340 U/D FLOORBEAM UPPER CHORD TO FRAME CONNECTION AREA FOUND 1EA FASTENER HOLE CRACKED AT U/D FLOORBEAM WEB APPROX .125 INCH. RIGHT BS 340 U/D FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11, JUST BETWEEN RBL 52 AND RIGHT MOST O/B END.

Part: SEAT TRACK — CORRODED (BS 1520-1530) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D STA 1520-1530 RBL 96 SEAT TRACK I/B FLANGE CORRODED. CORROSION BLEND OUT 0.035" X .5" X 1" EXCEED SRM 53-10-09 FIG 1, LIMITS. M/D BS 1480-1570 RBL 96 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: CARGO TRACK — CORRODED (BS 480-500) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D LBL 33 BS 480-500 TIE DOWN TRACK I/B FLANGE CORRODED. CORROSION BLEND OUT 0.052" X .5" X 10" EXCEEDS SRM 53-10-01 FIG 1 LIMITS. M/D BS 460-530 LBL 33" TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 760) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D - LBL 75-97 BS 760 FLOORBEAM CORRODED. CORROSION BLEND OUT 0.044" X 1" X 2" EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 760 LBL 67 TO MOST LEFT O/B FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 3.

Part: SEAT TRACK — CORRODED (BS 400-420) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 400-420 LBL 90 SEAT TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.022" X .5" X 10" IS EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 410-460 LBL 90" SEAT TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 640 RBL 100-108 FLOORBEAM FOUND CORROSION. CORROSION BLEND 0.136 X 1 X 2 INCH EXCEED SRM LIMIT. M/D BS 640 RBL 100-108 FLOORBEAM FITTING REPAIRED AS PER RS R53-25-35757 AND UPS ENGINEERING FILE NUMBER 747-53-20405.

Part: SEAT TRACK — CORRODED (BS 1640) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 1640 LBL 11 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.019" X .5" X .5" EXCEED SRM LIMIT. M/D BS 1590-1690 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14, REFER NRC 50765 FOR DETAIL.

Part: SEAT TRACK — CORRODED (BS 1500-1520) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 1500-1520 LBL 97 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.028" X .5" X 8" EXCEEDS SRM 53-10-01 FIG 1 LIMITS, M/D BS 1483 - 1550 LBL 97 - 99" SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FRAME — CRACKED (BS 820) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LT BS 820 TENSION TIE TO FRAME CONNECTION NR 2, 4, 10 AND 13 FASTENER HOLE FOUND CRACK AT WEB RUNNING DOWN THRU THICKNESS. LT BS 820 FRAME WEB REPAIRED AT BETWEEN STR 8L AT STA 11.5L AS PER RS R53-25-35751 AND UPS EO B747-5310-26129.

Part: STIFFENER — CORRODED (BS 1241) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT WING RIGHT WLG WW CTR SECTION REAR SPAR STIFFENER BS 1241 AT RBL 85 30 INCHES BELOW CEILING FOUND CORRODED. CORROSION BLEND OUT 0.150 X .5 X 5 INCH EXCEED SRM LIMIT. RIGHT WING RIGHT WLG W/W CTR SECTION REAR SPAR STIFFENER AT BS 1241 RBL 85 REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND RS R53-43-35776 AND UPS EO B747-5710-16421.

Part: SEAT TRACK — CORRODED (BS 1595) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 1595 LBL 11 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.025" X .5" X 1" EXCEED SRM LIMIT. M/D BS 1590-1690 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: ATTACH FITTING — CRACKED (BS 260) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 260 LBL 11 NLG TOP BOX ATT CLIP FOUND CRACKED. CRACK LENGTH .25 INCH. M/D BS 260 LBL 11 NLG TOP BOX ATT CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT WING L/E NOSE BEAM WEB ATT ANGLE AT ILES 1117 FOUND CRACKED. CRACK LENGTH .375 INCH. LEFT WING L/E NOSE BEAM WEB ATT ANGLE AT ILES 1117 REPAIRED AS PER SRM 57-20-03 FIG 7.

Part: FLOOR SUPPORT — CRACKED (BS 340) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 340 RIGHT O/B FLOOR SUPPORT FOUND CRACKED. CRACK LENGTH .5 INCH. M/D BS 340 RIGHT O/B FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: FRAME — CRACKED (BS 820) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT BS 820 TENSION TIE TO FRAME CONNECTION NR 4 AND NR 10 FASTENER HOLE FOUND CRACK AT FRAME WEB DOUBLER RUNNING UP THRU THICKNESS. CRACK LENGTH .125 INCH. LEFT BS 820 TENSION TIE TO FRAME WEB ATT DOUBLER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (BS 780) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT BS 780 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 5 CRACK AT FWD CHANNEL RUNNING UPPER APPROX .125 INCH IN LENGTH. M/D BS 780 LT TO RT FRAME ATTACH TENSION TIE FWD CHANNEL REPLACED AND 51-30-02.

Part: CHANNEL — CRACKED (BS 780) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 780 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 5 FOUND CRACK AT FWD CHANNEL AT 12:00 O/C POSITION APPROX .125 INCH LONG. M/D BS 780 LT TO RT FRAME ATTACH TENSION TIE FWD CHANNEL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: PLATE — MISMANUFACTURED (BS 920) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 920 LEFT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 920 TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35761. CONTINUE INSPECTION IS REQUIRED AS PER R53-25-35761 AND UPS EO B747-5310-14932.

Part: FRAME — CRACKED (BS 820 S8-11R) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 820 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 10 CRACK AT FRAME LAYER RUNNING LOWER APPROX .0625 IN LENGTH. RIGHT BS 820 FRAME REPAIRED AT BETWEEN STR 8R AND STR 11.5R AS PER RS R53-25-35751 AND UPS EO B747-5310-26129.

Part: PLATE — MISMANUFACTURED (BS 820) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 820 RT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 820 RIGHT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35751. CONTINUE INSPECTION IS REQUIRED AS PER R53-25-35751 AND UPS EO B747-5310-26129.

Part: PANEL — DELAMINATED (RT WING TE FLAP) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT WING I/B FORE FLAP I/B LWR PANEL FWD AREA FOUND DELAMINATION. RIGHT WING I/B FORE FLAP I/B LWR PANEL REPAIRED AS PER RS R57-55-35769 AND UPS EO B747-5750-26318.

Part: PLATE — MISMANUFACTURED (BS 800) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 800 RIGHT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 800 RIGHT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35755. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35755 AND UPS EO B747-5310-14973.

Part: FILLER — CRACKED (BS 780) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 780 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 4 FOUND CRACK AT FILLER RUNNING 1:00 O/S POSITION APPROX .0625 INCH LONG. RIGHT BS 780 FRAME TENSION TIE ATT FILLER REPLACED AS PER SRM 51-10-01 PG 9.

Part: PLATE — MISMANUFACTURED (BS 780) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 780 RIGHT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 780 RIGHT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35745. CONTINUE INSPECTION IS REQUIRED AS PER R53-25-35745 AND UPS EO B747-5310-26128.

Part: PLATE — MISMANUFACTURED (BS 880) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 880 RT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 880 RT TENSION TIE ATTACH STEEL PLATE REPAIRED AS PER RS R53-25-35752. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35752 AND UPS EO B747-5310-26133.

Part: CHANNEL — CRACKED (BS 780) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT BS 780 FRAME TENSION TIE ATTACHMENT AT FASTENER HOLE NR 7 CRACK AT AFT CHANNEL RUNNING UPPER APPROX .0625 INCH IN LENGTH. M/D BS 780 LT FRAME ATTACH TENSION TIE AFT CHANNEL REPAIRED AS PER RS R53-25-35745. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35745 AND UPS EO B747-5310-26128.

Part: PLATE — MISMANUFACTURED (BS 800) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 800 LEFT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 800 LEFT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35755. CONTINUE INSPECTION IS REQUIRED PER RS R53-35-35755 AND UPS EO B747-5310-14973.

Part: PLATE — MISMANUFACTURED (BS 820) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 820 LEFT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 820 LEFT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35751. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35751 AND UPS EO B747-5310-26129.

Part: PANEL — DELAMINATED (LT WING) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT WING I/B MID FLAP UPPER PANEL 577LT INTERNAL FOUND DELAMINATION. LEFT WING I/B MID FLAP UPPER PANEL 577LT REPAIRED AS PER RS R57-55-35711 AND US EO B747-5730-15355.

Part: PLATE — MISMANUFACTURED (BS 920) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 920 RT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 920 RT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35761. CONTINUE INSPECTION IS REQUIRED AS PER R53-25-35761 AND UPS EO B747-5310-14932.

Part: PLATE — MISMANUFACTURED (BS 860) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 860 RT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 860 RT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35746. CONTINUE INSPECTION IS REQUIRED AS PER R53-25-35746 AND UPS EO B747-5310-26132.

Part: PLATE — MISMANUFACTURED (BS 880) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 880 LEFT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 880 LEFT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35752. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35752 AND UPS EO B747-5310-26133.

Part: CHANNEL — CRACKED (BS 820) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 820 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 4 CRACK AT FWD CHANNEL RUNNING UPPER AND LWR BOTH CRACK APPROX .0625 IN LENGTH. RIGHT BS 820 FRAME TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35751. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35751 AND UPS EO B747-5310-26129.

Part: FRAME — CRACKED (BS 820) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RT BS 820 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 11 CRACK AT FRAME UPPER APPROX .0625 INCH IN LENGTH RUNNING AT 5:00 O/C POSITION. RIGHT BS 820 FRAME REPAIRED BETWEEN STR 8R AND STA 11-5R AS PER RS R53-25-35751.

Part: FRAME — CRACKED (BS 900) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 900 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 1 THREE CRACKS FOUND AT FRAME LAYER. CRACK LENGTH .0625 AND 0.030 INCH. M/D BS 900 RIGHT FRAME BETWEEN STR 6R TO STR 11-5R REPAIRED AS PER RS R53-10-35750. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-10-35750 AND UPS EO B747-5310-26134.

Part: PLATE — MISMANUFACTURED (BS 860) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 860 LEFT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 860 LEFT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35746. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35746 AND UPS EO B747-5310-26132.

Part: FRAME — CRACKED (BS 780) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 780 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 1 AND NR 9 BOTH FOUND CRACK AT FAILSAFE CHORD AT 5:00 O/C POSITION. APPROX .0625 & .125 INCH LONG. M/D BS 780 RIGHT FRAME BELOW STR 11R FAILSAFE CHORD REPLACED AS PER RS R53-25-35745 AND UPS EO B747-5310-26128.

Part: PLATE — MISMANUFACTURED (BS780) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 780 LEFT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 780 LEFT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35745. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35745 AND UPS EO B747-5310-26128.

Part: PLATE — MISMANUFACTURED (BS 940) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 940 RT TENSION TIE ATT STEEL PLATE FOUND SHORT EDGE MARGIN. M/D BS 940 RIGHT TENSION TIE ATT STEEL PLATE REPAIRED AS PER RS R53-25-35756. CONTINUE INSPECTION IS REQUIRED AS PER R53-25-35756 AND UPS EO B747-5310-14767.

Part: FRAME — CRACKED (BS 940 S7-8L) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 940 STR 7-8L FRAME O/B FLANGE FOUND CRACK. CRACK LENGTH 0.875 INCH. M/D BS 940 LEFT BETWEEN STR 5L TO STR 12L FRAME REPAIRED AS PER RS R53-25-35756 AND UPS EO B747-5310-14767.

Part: CHANNEL — CRACKED (BS 800) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 800 TENSION TIE ATTACHMENT AREA NR 7 FASTENER HOLE CRACK FOUND AT AFT CHANNEL RUNNING UP APPROX .0625 INCH IN LENGTH. RIGHT BS 800 TENSION TIE ATT AFT CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: CHANNEL — CRACKED (BS 800) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 800 TENSION TIE ATTACHMENT AREA NR 5 AND NR 12 FASTENER HOLE CRACK AT FWD CHANNEL. CRACK LENGTH .125 INCH. RIGHT BS 800 TENSION TIE FWD CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: STRINGER CLIP — CRACKED (BS 880) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 880 TENSION TIE ATT NR 10 FASTENER HOLE CRACK AT TIE CLIP, CRACKS RUNNING UP .25 INCH AND RUNNING DOWN .1875 INCH APPROX. RIGHT SIDE BS 880 TENSION TIE ATT TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: CHANNEL — CRACKED (BS 800) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT BS 800 FRAME TENSION TIE ATTACHMENT AREA AT FASTENER HOLE NR 7 CRACK FOUND AT AFT CHANNEL RUNNING UPPER APPROX .0625 INCH IN LENGTH. LEFT BS 800 FRAME TENSION TIE ATT AFT CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (BS 880) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT BS 880 TENSION TIE ATTACHMENT AREA NR 13 FASTENER HOLE CRACK AT FRAME WEB THRU THICKNESS APPROX .0625 INCH. M/D RIGHT BS 880 TENSION TIE ATTACH FRAME AT STR 6R TO STR 12R REPAIRED AS PER RS R53-25-35752 AND UPS EO B747-5310-26133.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C EQUIPMENT COOLING OUTLET FOUND ONE EACH FASTENER HOLE CRACKED AT SKIN APPROX .125 INCH LONG RUNNING FWD & APPROX .375 INCH LONG RUNNING TO EDGE. FUSELAGE SKIN AT BS 575 EQUIPMENT COOLING OUTLET REPAIRED AS PER UPS EO B747-5330-6909 APPENDIX B.

Part: FRAME — CRACKED (BS 840) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT SIDE BS 840 TENSION TIE ATTACHMENT AREA NR 13 AND NR 14 FASTENER HOLE CRACK AT FRAME DOUBLER. CRACK LENGTH .25 INCH. M/D BS 840 LT FRAME ATTACH DOUBLER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: CHANNEL — CRACKED (BS 840) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C M/D BS 840 LEFT TENSION TIE AFT CHANNEL FOUND CRACK. CRACK LENGTH .5 INCH. M/D BS 840 LEFT TENSION TIE AFT CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: CHANNEL — CRACKED (BS 800) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C LEFT BS 800 FRAME TENSION TIE ATTACHMENT AREA AT HOLE NR 5 CRACK FOUND AT FWD CHANNEL RUNNING UPPER AND LOWER BOTH CRACK APPROX .125 INCH IN LENGTH. LEFT BS 800 FRAME TENSION TIE ATT FWD CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (BS 880) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C RIGHT SIDE BS 880 TENSION TIE ATTACHMENT AREA NR 10 FASTENER HOLE CRACK FOUND AT FRAME DOUBLER APPROX .0625 INCH IN LENGTH. M/D BS 880 RIGHT FRAME ATTACH DOUBLER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FIRESHIELD — DAMAGED (NR 2 PYLON) · airframe 90,184 hrs · 22,066 cycles

INSPECTION TYPE:C DMI D341139 - NR 2 PYLON FIRESHIELD DAMAGED AT NAC STA 261.5 AND STA 275.3. NR 2 PYLON FIRESHIELD REPAIRED AT NAC STA 261.5 TO NAC STA 290.5 AREA AS PER RS R54-54-35772 AND UPS ENGINEERING FILE 747-54-20058.

Part: SPAR — CRACKED (LT WING)

CRACKED LT WING REAR SPAR WING STA 1361. A/C FERRIED TO BFM FOR REPAIR. COMPLIED WITH EO B747-5710-25865-B

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

EMERG XIT LT AT UPPER RT EXIT DOOR INOP. DEFERRED PER MEL 33-15 M333108. REMOVED AND REPLACED UPPER DECK EMERG LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECKS GOOD. THIS CLEARS M333108. PLACARD REMOVED.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A CREW ENTRY DOOR EMERGENCY LIGHT FWD (UPPER SILL) DIM. R&R EMERGENCY LIGHT BATT ASSY PER MM 33-51-07, OPS CK GOOD.

Part: SKIN — CORRODED (FUSELAGE)

FUSE SKIN JUST RT OF AFT GALLEY DRAIN MAST PILLOWED. *S/D* REMOVED DE-ACT'D DRAIN MAST DAMAGE. FAB'D DOUBLER & FILLERS PER SRM 53-30-03. OK TO INSTALL REPAIR. COMPLETED DOUBLER & FILLERS INSTALLATION PER SRM 53-30-03. GALLEY DRAIN MAST DELETED PER EO B747 38-30-24809-A.

Part: LIFE VEST — MISSING (COCKPIT)

F/O LIFE VEST MISSING. REPLACE VEST.

Part: ZIPPER — BROKEN (SMOKE CURTAIN)

ZIPPER BROKEN ON RT SMOKE CURTAIN, EYE TO FWD CARGO. PO OA879126 PLACED ON DEFERRED MAINTENANCE. R & R SMOKE BARRIER BETWEEN E & E COMPARTMENT AND LWR FWD CARGO HOLD THIS CLEARS D317769.

Part: THRUST LINK — CRACKED (NR 4 ENGINE) · airframe 88,086 hrs · 21,555 cycles

AD NR 4 ENGINE REAR ENGINE MOUNT THRUST LINK FOUND CRACKED INDICATION ON FWD END LUG BORE LOWER AREA. NR 4 ENG THRUST LINK REPLACED IAW EO B747-7120-22596 APPENDIX I.

Part: THRUST LINK — CRACKED (NR2 ENG) · airframe 88,086 hrs · 21,555 cycles

AD NR 2 ENGINE REAR ENGINE MOUNT THRUST LINK FOUND CRACKED INDICATION ON AFT END LUG BORE LOWER AREA. NR 2 ENG THRUST LINK REPLACED IAW EO NR B747-7120-22596 APPENDIX G.

Part: RIB — DAMAGED (NR 2 PYLON)

L/T SIDE OF THE NR 2 PYLON, DAMAGED RIBS REPAIR. SHOW EVIDENCE OF CRACK INSIDE PYLON OPPOSITE PREVIOUS REPAIR. 11' FROM SLOT SEAL OPENIN G AND 8' FROM BOTTOM EDGE. ACCOMPLISED HI-FREQUENCY EDDY CURRENT SUSPECT AREA NO CRACKS DETECTED

Part: WARNING SYSTEM — INOPERATIVE (ALTITUDE)

ALTITUDE ALERTING SYSTEM INOP. RVSM A POSSIBILITY. R/R ALTITUDE A;ERTER COMPUTER PER MM 34-16-00-PG 207. SYSTEM TEST GOOD PER MM 34-16-00-OR.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C M/D BS 2180 FRAME WEB S24R STR CUTOUT FOUND CRACK (CRACK LENGTH 0.75" & 0.5"). M/D BS 2180 STR 23R TO STR 26R FRAME REPAIRED AS PER HX RS R53-62-35345 & UPS EO B747-5310-22631-A.

Part: SKIN — CRACKED (FX) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C FX SKIN S19R AT BS 388 TOP ROW FASTENER ROW 1EA FASTENER HOLE FOUND CRACK AT OUTER SKIN RUNNING FWD & AFT APPROX 0.030 INCH. FX SKIN BS 383 TO BS 399 STR 19R AREA OVERLAPPING SKIN REPAIRED WITH ZERO TIMING AT CRITICAL ROW FASTENERS AS PER SRM 53-30-03 FIG 17 REF NRC 5902 FOR DETAIL. PER MPI P18050 - LFEC INTIAL INSP AT 15000 FC & REPEAT AT 1500 FC THEREAFTER.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 87,225 hrs · 21,374 cycles

BULK CARGO DOOR CUTOUT AFT FRAME AREA AT BS 2034 STR 35-37 FOUND 2EA HOLE CRACK, CRACK LENGTH 0.020" AND 0.030". BULK CARGO DOOR CUTOUT AFT AREA BS 2034 BETWEEN STR 34/35R TO STR 37/38R AREA REPAIRED AS PER HX RS R-53-61-35359. REF NRC 6801 FOR DETAIL AND C/OUT CONTINUE INSPECTION PER HX RS R-53-61-35359.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 87,225 hrs · 21,374 cycles

LT WLG WW SIDEWALL PANEL FOUND CRACK AT BTN BS 260 AND 280 WL 170 APPROX 1 INCH. LT NLG WW SIDEWALL PANEL REPAIRED AT BS 260 TO BS 280 WL 170 AREA AS PER SRM 53-10-04 FIG 116.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 87,225 hrs · 21,374 cycles

BULK CARGO DOOR CUTOUT AFT FRAME AT BS 2034 STR 35-37 FOUND 7EA HOLE CRACK AT FRAME OUTER CHORD, CRACK LENGTH 0.020"/0.030". BULK CARGO DOOR CUTOUT AFT AREA BS 2034 BETWEEN STR 34/35R TO STR 37/38R AREA REPAIRED AS PER HX RS R-53-61-35359 AND C/OUT CONTINUE INSPECTION PER HX RS R-53-61-35359.

Part: DOUBLER — CORRODED (M/D) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C M/D BS 1980-2000 S20-22L WINDOW FORGING MATTING SURFACE SKIN FOUND CORROSION DUE FORGING REMOVED. CORROSION BLEND OUT 0.022" X 1.5" X 3" EXCEED SRM 53-30-01 FIG 1 LIMITS. M/D BS 1983 LT WINDOW CUTOUT DOUBLER CORROSION REPAIRED AS PER HX RS R53-61-35356 & UPS ENGINEERING FILE 747-53-20276.

Part: FRAME — CRACKED (U/D) · airframe 87,225 hrs · 21,374 cycles

BS 560 STR 10AL-11L FRAME O/B FOUND CRACK FLANGE. CRACK LENGTH 2" CORROSION BLEND OUT N/A. BS 560 BETWEEN STR 10AL-11L FRAME REPAIRED AS PER HX RS R53-12-35352 AND UPS EO B747-5310-22634-A.

Part: FRAME — CRACKED (L2 DOOR) · airframe 87,225 hrs · 21,374 cycles

L2 DOOR AFT FRAME LOWER CORNER CRACKED, CRACK LENGTH 1. L2 DOOR AFT FRAME LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 560 S9L STRINGER END FOUND CRACK, CRACK LENGTH 7/16". BS 560 STR 9L STR END REPAIRED AS PER SRM 53-10-03 FIG 2.

Part: PANEL — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 440 S14/S15 1R DOOR CUTOUT REVEAL CRACKED BETWEEN NR 8/9 DOOR STOP FTG, CRACK LENGTH 1". REVEAL PANEL REPLACED AS PER SRM 51-10-01 PG 9.

Part: FLOORBEAM — CORRODED (M/D) · airframe 87,225 hrs · 21,374 cycles

BS 1918 LBL 100 FLOOR SUPPORT CORROSION. CORROSION BLEND OUT 0.103" BY 1" BY 2". FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.

Part: TORQUE BOX — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

1R DOOR LATCH TORQUE BOX CUTOUT LWR BEAM CRACKED AND ATT 'T' BRACKET DEFORMED, CRACK LENGTH 5/16". SUPPORT BEAM AND BRACKET REPLACED AS PER SRM 51-10-01 PG 9.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 560, BETWEEN STR 6L - 8L FRAME AFT FACE O/B AREA 2EA CRACK FOUND, CRACK LENGTH 1.125 & 3/4". BS 560 FRAME REPAIRED AS PER SRM 53-10-04 FIG 54 AT BTN STR 6L TO 8L AREA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

STA 710 LBL 47 TO LBL 66 FLR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.023 BY .50 BY 1 EXCEED SRM 53-10-01 FIG 1 LIMITS, FLR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · airframe 87,225 hrs · 21,374 cycles

BS 340 LBL 40-50 FLOORBEAM FOUND CLR. CORROSION BLEND OUT 0.047 BY 2 BY 5 EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 340 LBL 8 TO LT O/B END FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 23.

Part: ANGLE — CORRODED · airframe 87,225 hrs · 21,374 cycles

INSIDE KEEL BEAM BOX AT BS 1329 LBL 9- RBL 9 ATT ANGLE FOUND CORROSION. CORROSION BLEND OUT 0.062" BY 1" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, ANGLE REPLACED AS PER SRM 51-10-01 PG 9.

Part: BULKHEAD — CRACKED (TUNNEL) · airframe 87,225 hrs · 21,374 cycles

FX BS 260 CANTED BULKHEAD WEB FOUND CRACKED AT WL 176 LBL 67, CRACK LENGTH 1/4". FX BS 260 CANTED BULKHEAD WEB REPAIRED AT WL 176 LBL 67 AREA AS PER SRM 53-10-04 FIG 6.

Part: FLOORBEAM — CRACKED (FUSLAGE) · airframe 87,225 hrs · 2,137 cycles

BS 360 FLOORBEAM FWD FLANGE 6EA MOUNTING HOLES CRACK. BS 360 FLOORBEAM UPPER CHORD HORIZ FWD FLANGE AT RBL 29 - 60 AREA REPAIRED AS PER UPS EO NR B747-5320-12407 APPENDIX 'D' PLAN 'C'.

Part: FRAME — CRACKED (BLG W/W) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE: C, LT BLG WW LT STA 1416 FRAME FOUND CRACKED IN BTN STR 29 AND STR 30, CRACK LENGTH 0.25". LT BLG W/W LT BS 1416 BETWEEN STR 29 AND 30 FRAME REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: FLOORBEAM — CRACKED (U/D) · airframe 87,225 hrs · 21,374 cycles

BS 360 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE ONE MOUNTING HOLE CRACK AT LBL 54, CRACK LENGTH 0.030". BS 360 LBL 21" TO LT O/B END AREA FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 23.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

U/D BS 400-402 RBL 76 LONGITUDINAL FLOOR SUPPORT FOUND CRACKED, CRACK LENGTH 2". U/D BS 400-402 RBL 76 LONGITUDINAL FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 415-420 BL 0 TO RBL 40 LATERAL SUPPORT FWD FLANGE FOUND CRACKED AT O/B AREA. BS 415-420 BL 0 TO RBL 40 LATERAL SUPPORT AT O/B AREA FWD FLANGE REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: KEELBEAM — CORRODED (FUSLEAGE) · airframe 87,225 hrs · 21,374 cycles

FX KEELBEAM PANEL SUPPORT FOUND CORROSION AT BS 1405. CORROSION BLEND OUT 0.054 BY .750 BY 1.5 EXCEED SRM 53-10-01 FIG 1 LIMITS, SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 380 LBL 30-40 FLOORBEAM FOUND CORROSION. CORROSION BLEND OUT 0.045 BY 1 BY 2.5 EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 380 LBL 24 TO LT O/B END FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 10.

Part: FLOORBEAM — CRACKED (U/D) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C U/D BS 380 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE 1EA MOUNTING HOLE CRACK (CRACK LENGTH 0.040"). U/D BS 380 FLOORBEAM UPPER CHORD REPAIRED AT BTN LBL 24" TO LT O/B AS PER SRM 53-10-07 FIG 10.

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 87,225 hrs · 21,374 cycles

BS 400-420 LBL 52 LONGITUDINAL FLOOR SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.042 BY 1 BY 2 EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

STA 700-710 LBL 66 SEAT TRACK FOUND CORRODED. CORROSION BLEND OUT 0.042 X 1 X 4 EXCEED SRM 53-10-01 FIG 1 LIMIT, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 360 FLOORBEAM UPPER STRUCTURE HORIZONTAL AFT FLANGE 1EA MOUNTING HOLE CRACK, CRACK LENGTH .125. BS 360 RBL 45 AFTER FLANGE OF FLOORBEAM UPPER STRUCTURE REPAIRED AS PER UPS EO NR B747-5320-12407 APPENDIX 'D' PLAN C.

Part: FLOORBEAM — CRACKED (U/D) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C U/D BS 360 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE 1EA MOUNTING HOLE CRACK AT LBL 46" (CRACK LENGTH 1/16"). U/D BS 360 LBL 21" TO LT O/B END AREA FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 23.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 340 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE ONE MOUNTING HOLE CRACK, CRACK LENGTH 1/16. BS 240 LBL 8" TO LT O/B CORRODED FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 23 REFER NRC NR 6532 FOR WORKING DETAIL.

Part: FLOORBEAM — CRACKED (U/D) · airframe 87,225 hrs · 21,374 cycles

BS 340 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE ONE MOUNTING HOLE CRACK, LENGTH 1/16". BS 340 LBL 8" TO LT O/B CORRODED FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 23.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 360 LBL 40 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.035 BY 2 BY 2 EXCEED SRM 53-10-01 FIG 1 LIMITS. BS 360 LBL 21" TO LT O/B END FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 23.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 400 RBL 3 TO 24 FLOORBEAM FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.043" BY 2" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS. BS 400 LBL 7" TO RBL 35" FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 10.

Part: RIB — CRACKED (LT WING) · airframe 87,225 hrs · 21,374 cycles

LT WING NR 2 VC FLAP I/B ARM I/B SUPT RIB TWO VERTICAL O/B FLANGE UPPER FASTENER HOLE CRACKED, CRACK LENGTH 3/8". SUPPORT RIB REPAIRED AS PER HX RS R-57-41-35350 AND C/OUT REPEAT INSPECTION PER UPS EO.B747-5740-22636-A.

Part: STRUCTURE — CORRODED (RT WING TE FLAP) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C RIGHT WING I/B MID FLAP T/E WEB UPPER CHORD CORROSION REVEALED AT 73" - 78" AS MARKED (COUNT FROM I/B). CORROSION BLEND OUT 0.083" X 3/4" X 3" EXCEED SRM 57-50-01 FIG 3 LIMITS. CHORD REPAIRED AS PER HX RS R57-55-35354 & UPS ENGINEERING FILE 747-57-20081.

Part: WEB — CORRODED (RT WING) · airframe 87,225 hrs · 21,374 cycles

RHW I/B MID FLAP T/E WEB UPR AREA SEVERAL AREA CORROSION REVEAL BETWEEN NR 3 AND NR 4 ARM, COUNT FROM O/B. CORROSION BLEND OUT 0.039" BY 0.5" BY 2" EXCEED SRM 57-50-01 FIG 3 LIMITS, WEB REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: WEB — CRACKED (LHW) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C LEFT WING UPPER WING L/E CAVITY NOSE L/E WEB CRACK AT WS 670-680 ABOVE NR 2 PYLON AREA, (CRACK LENGTH 1.25"). WEB FABRICATED & INSTALLED AS PER SRM 57-20-03 FIG 7.

Part: STRUCTURE — CORRODED (TE FLAP) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C RIGHT WING I/B MID FLAP T/E WEB UPPER CHORD CORRODED REVEALED AT 104"- 108" AS MARKED (COUNT FROM I/B). CORROSION BLEND OUT 0.054" X 3/4" X 3" EXCEED SRM 57-50-01 FIG 3 LIMITS, CHORD REPAIRED AS PER HX RS R57-55-35354 & UPS ENGINEERING FILE 747-57-20081.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 2160 BETWEEN STR 20-22L FRAME AFT FACE SHEAR TIE FOUND CRACK, CRACK LENGTH .750. SHEAR TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.

Part: SKIN — DAMAGED (NR 2 PYLON) · airframe 87,225 hrs · 21,374 cycles

NR 2 PYLON NAC STA 240 LOWER EDGE O/B SIDE DOUBLER HOLE CHAFED REVEALED AS MARK. NR 2 PYLON NAC STA 240 LOWER EDGE REPAIRED AS PER SRM 54-30-03 FIG 36.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C M/D BS 2180 BETWEEN S25-26L FRAME FOUND CRACK (CRACK LENGTH 1/2"). M/D BS 2180 BETWEEN STR 24L - 26L FRAME REPAIRED AS PER HX RS R53-62-35345 & UPS EO B747-5310-22631-A.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 1780 S-12R STRINGER TIE CLIP FOUND CRACKED, CRACK LENGTH .750. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.

Part: STRINGER — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

BS 1740-1760 S2R STRINGER END FOUND CRACK, CRACK LENGTH 2". M/DECK BS 1740-1760 STR 2R STRINGER END REPAIRED AS PER HX RS R53-61-35355 AND UPS EO.B747-5310-22662-A.

Part: STRINGER — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

BS 2180-2200 S25R STRINGER FOUND CRACKED, CRACK LENGTH 5/8". BS 2180 TO BS 2208 STR 25R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 87,225 hrs · 21,374 cycles

BULK CARGO DOOR CUTOUT FX SKIN EXTERNAL REPAIR PATCH AT BS 2034 STR 35R-37R REQUEST REMOVAL FOR ASSESSMENT PER BOEING MESSAGE 1-109528471-2. BULK CARGO DOOR CUTOUT AFT AREA BS 2034 BTN STR 34/35R TO STR 37/38R AREA REPAIRED AS PER HX RS R-53-61-35359. REF NRC 6801 FOR WORKING DETAIL AND C/OUT CONTINUE INSPECTION PER HX RS R-53-61-35359.

Part: SHEAR TIE — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

M/DECK BS 860 RT FRAME BTN STR 12-13R SHEAR TIE FOUND CRACKED, CRACK LENGTH 5/8". M/DECK BS 860 BETWEEN STR 12R-13R SHEAR TIE REPAIRED AS PER HX RS R53-22-35349 AND UPS EO B747-5310-22630-A.

Part: FRAME — CRACKED (FWD CARGO) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C FWD CARGO RT STA 760 FRAME UPPER FLANGE AT RBL 60 FOUND CRACKED (CRACK LENGTH 1/2", 5/8", 1.125"). FRAME REPAIRED AS PER HX RS R53-22-35341 & UPS EO B747-5310-22629-A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 1958-1960 STR 2L STRINGER END FOUND CRACK, CRACK LENGTH 1.5". STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR-2L BETWEEN BS 1930 AND 1960.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 1958-1960 STR 3L STRINGER END FOUND CRACKED, CRACK LENGTH 1.625 INCH. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR 3L BETWEEN BS 1930 AND 1960.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

M/D BS 980 BETWEEN S20-22R FRAME FWD FACE FOUND CRACK, CRACK LENGTH 0.5" AND 0.75". M/DECK BS 980 BTWEEN STR 20-22R FRAME REPAIRED AS PER HX RS R53-22-35344 AND UPS EO.B747-5310-22630-A.

Part: SHEAR TIE — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

BS 1780 S4-5R STRINGER SHEAR TIE FOUND CRACKED, CRACK LENGTH .3750. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 1958-1960 STR 1L STRINGER END FOUND CRACKED, CRACK LENGTH 3.875 INCH. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR - 1L BETWEEN BS 1930 AND 1960.

Part: FRAME — CRACKED (FWD CARGO) · airframe 87,225 hrs · 21,374 cycles

FWD CARGO LT STA 920 LBL 60" FRAME UPR FLANGE FOUND CRACKED, CRACK LENGTH 3". FWD CARGO COMPT BS 920 LBL 60" FRAME REPAIRED AS PER HX RS R53-22-35342 AND UPS EO.B747-5310-22635-A.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

BS 2180 STR 25R STRINGER AREA FRAME FOUND CRACK, CRACK LENGTH 0.75" AND 0.5". BS 2180 STR 23R TO STR 26R FRAME REPAIRED AS PER HX RS NR R53-62-35345 AND UPS EO NR B747-5310-22631-A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 1940-1960 STR 3R STRINGER END FOUND CRACKED, CRACK LENGTH 1.25 INCH. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR 3R BETWEEN BS 1930 AND 1960.

Part: STRINGER — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

M/D BS 1740-1760 S3R STRINGER END FOUND CRACKED, CRACK LENGTH 1.5". M/D BS 1740-1760 STR 3R STRINGER END REPAIRED AS PER HX RS R53-61-35355. FOLLOW UP INSPECTION FOR THIS REPAIR IS REQUIRED AS PER HX RS R53-61-35355 AND UPS EO.B747-5310-22662-A.

Part: SKIN — CORRODED (LHW) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C, LEFT WING UPPER WING SKIN L/E RABBIT AREA 2 PLACES BULGED UP AT WS 1470-1515 AFT OF NR 1 VC FLAP AREA. CORROSION THROUGH WHOLE THICKNESS AREA 7.3" X 4.3". LEFT WING UPPER WING SKIN REPAIRED AS PER HX RS R57-25-35357 & UPS ENGINEERING FILE 747-57-20080.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C M/D BS 2060 BETWEEN STR 25-26L FRAME FOUND CRACKED (CRACK LENGTH .375 INCH). M/D BS 2060 BETWEEN STR 26L - 26L FRAME REPAIRED AS PER HX RS R53-62-35347 & UPS EO B747-5310-22631-A7.

Part: SHEAR TIE — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

BS 1900 S23-24R STRINGER SHEAR TIE FOUND CRACKED, CRACK LENGTH 7/16". BS 1900 STR 23-24R STRINGER SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9.

Part: SHEAR TIE — CRACKED (FUSLEAGE) · airframe 87,225 hrs · 21,374 cycles

BS 1860 S10-11R STRINGER SHEAR TIE FOUND CRACKED, CRACK LENGTH .50. SHEAR TIE CLIP REPLACED AS PER SRM 51-10-01.

Part: WEB — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 1920-1940 S26R FLOOR WEB I/B EDGE FOUND CRACKED, CRACK LENGTH 0.75. WEB REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: FRAME — CRACKED (NR 4 PYLON) · airframe 87,225 hrs · 21,374 cycles

NR 4 PYLON NAC STA 240 I/B SIDE FWD OF ACCESS PANEL CUTOUT 483EL VERT FRAME LIGHTEN HOLE CRACKED, CRACK LENGTH 2". NR 4 PYLON NAC STA 240 I/B SIDE VERTICAL FRAME REPLACED AS PER SRM 51-10-01 PG 9.

Part: FRAME — CRACKED (RT MLG WW) · airframe 87,225 hrs · 21,374 cycles

RT MLG WW STA 1394-1416 LOWER FRAME AT WEB FOUND CRACKED, UPPER OF LONGERON BOX, CRACK LENGTH .750. WEB REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: FLOORBEAM — CORRODED (FWD CARGO) · airframe 87,225 hrs · 21,374 cycles

FWD CARGO RT STA 800 RBL 33 FLOORBEAM UPPER CHORD FOUND CORRODED AND CRACKED. CORROSION BLEND OUT 0.080" BY 1" BY 2.5" EXCEED SRM 53-10-01 FIG 1 LIMITS, FLOORBEAM REPAIRED AT BS 800 RBL 26 TO RBL 42" AREA AS PER SRM 51-40-04 FIG 2.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 2120 BETWEEN S13-14L FRAME ATT SHEAR TIE FOUND BROKEN, CRACK LENGTH .5. SHEAR TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 1940-1960 STR 11R STRINGER END FOUND CRACKED, CRACK LENGTH 1 INCH. BS 1930 TO BS 1960 STR 11R REPAIRED AS PER SRM 53-10-03 FIG 4.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 1940-1960 S1R STRINGER END FOUND CRACKED, CRACK LENGTH 1.125. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR 1R BETWEEN BS 1930 & 1960.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

BS 940 BETWEEN S14-15R FRAME FOUND CRACK, CRACK LENGTH 7/16". BS 940 BETWEEN STR 14-15R FRAME REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

BS 760 LT STR-14 FRAME FOUND CRACKED, CRACK LENGTH 3/4". FRAME REPAIRED AS PER HX RS R-53-22-35348 AND UPS EO. B747-5310-22632-A.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

M/DECK BS 580 LT STR 24L FRAME FOUND CRACKED, CRACK LENGTH 1". M/DECK BS 580 LT STR 23L TO 25L FRAME REPAIRED AS PER HX RS R53-22-35338 AND UPS EO.B747-5310-22626-A.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

BS 780 STR 20-22R FRAME FWD FACE FOUND CRACK. CRACK LENGTH 1.75" CORROSION BLEND OUT. M/DECK BS 780 BETWEEN STR 20R-22R FRAME REPAIRED AS PER HX RS R53-22-35346 AND UPS EO B747-5310-22632-A.

Part: WEB — CRACKED (NR 1 PYLON) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C NR 1 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT FWD FRAME WEB (CRACK LENGTH 7/16"). NR 1 PYLON REAR MOUNT BULKHEAD FRAME WEB REPAIRED AS PER HX RS R54-53-35353 & UPS ENGINEERING FILE 747-54-20052, CONTINUE TO CONDUCT DETAIL VISUAL & HFEC INSPECTION OF THE REAR ENGINE MOUNT LOWER B/H ASSY, PER THE REQUIREMENT OF SB 747-54A2202, EVERY 1200 FLT CYC OR 18 MONTHS.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C M/D BS 600 LT STR 25L - 24L FRAME FOUND CRACKED (CRACK LENGTH .75" & 1"). M/D BS 600 LT STR 23 TO STR 26 AREA FRAME REPAIRED AS PER HX RS R53-22-35339 & UPS EO B747-5310-22627-A.

Part: SKIN — CRACKED (FX) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C RIGHT WING AT BS 395 STR 19 UPPER FASTENER ROW FOUND 1EA FASTENER HOLE CRACK AT OUTER SKIN APPROX .125 INCH LONG RUNNING FWD AS MARKED. FX BS 383 TO BS 399 STR 19R AREA OVERLAPPING SKIN REPAIRED WITH ZERO TIMING AT CRITICAL ROW FASTENERS AS PER SRM 53-30-03 FIG 17. REFER NRC 5902 FOR DETAIL. PER MPI P18050- LFEC INTIAL INSP AT 15000 FC & REPEAT AT 1500 FC THEREAFTER.

Part: WEB — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BS 2320-2340 S26R WEB FOUND CRACKED AT AFT PORTION AREA, CRACK LENGTH .375. BS 2337 TO BS 2340 WEB REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: FRAME — CRACKED (AFT CARGO) · airframe 87,225 hrs · 21,374 cycles

AFT CARGO LT BS 1900 FRAME WEB FOUND CRACKED BETWEEN LT STR 36 AND LT STR 37, CRACK LENGTH .500. AFT CARGO LT BS 1900 FRAME REPAIRED AT BETWEEN LT STR 36 & 37 AREA AS PER SRM 53-10-04 FIG 4.

Part: FRAME — CRACKED (AFT CARGO) · airframe 87,225 hrs · 21,374 cycles

AFT CARGO RT BS 1520 FRAME WEB FOUND CRACKED AT RT STR 31, CRACK LENGTH .500. AFT CARGO RT BS 1520 FRAME REPAIRED AT STR 31 RT AREA AS PER SRM 53-10-04 FIG 4.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C M/D BS 740 RT STR 25R FRAME FOUND CRACK (CRACK LENGTH 0.75"). M/D BS 740 STR 24R-26R FRAME REPAIRED AS PER HX RS R53-22-35340 & UPS EO B747-5310-22628-A.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C M/D BS 640 LT STR 24L & 25L FRAME FOUND CRACKED (CRACK LENGTH 1/2" & 0.75"). M/D BS 640 LT STR 23 TO STR 26 AREA FRAME REPAIRED AS PER HX RS R53-22-35339 & UPS EO B747-5310-22627-A.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C M/D BS 620 LT STR 25 FRAME FOUND CRACKED (CRACK LENGTH 5/8"). M/D BS 620 LT STR 24 TO STR 26 AREA FRAME REPAIRED AS PER HX RS R53-22-35340 & UPS EO B747-5310-22628-A.

Part: SKIN — CRACKED (BS 395) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C, RIGHT SIDE AT BS 395 STR 19 UPPER FASTENER ROW FOUND ONE EACH FASTENER HOLE CRACKED AT OUTER SKIN APPROX .125 INCH LONG RUNNING FWD AS MARKED. FX BS 383 TO BS 399 STR 19R AREA OVERLAPPING SKIN REPAIRED WITH ZERO TIMING AT CRITICAL ROW FASTENERS PER SRM 53-30-03 FIG 17. SUBSEQUENT INSPECTION IS NECESSARY FOR CAT B REPAIR REF SRM 53-30-03 FIG 17 SHT 6 TABLE III FOR INSPECTION REQ WITH 15000 FC INSP THRESHOLD. MPI P18050 FOR LFEC INITIAL AT 15000 FC & REPEAT AT 1500 FC THERE AFTER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

AFT CARGO RT SIDEWALL BS 1620 FRAME WEB FOUND DENT AT RT STA 36 AREA AS MARKED, CRACK LENGTH .750. FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 66.

Part: SKIN — CORRODED (RT WING) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C RIGHT WING UPPER SURFACE RABBIT AREA FOUND BULGED BETWEEN WS 1375 AND WS 1395 (AFT NR 24 VC FLAP). CORROSION BLEND OUT 0.127" X 1.625" X 6" EXCEED SRM 57-30-01 FIG 1 LIMITS. RIGHT WING UPPER SURFACE RABBIT AREA REPAIRED AFTER CORROSION BLENDED OUT AS PER HX RS R57-25-35358 & UPS ENGINEERING FILE 747-57-20079.

Part: FRAME — CRACKED (M/D) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C M/D BS 940 S25L FRAME FOUND CRACKED (CRACK LENGTH 0.50"). M/D BS 940 STR 24L TO 26L AREA FRAME REPAIRED AS PER HX RS R53-22-35340 & UPS EO B747-5310-22628-A.

Part: FRAME — CRACKED (AFT CARGO) · airframe 87,225 hrs · 21,374 cycles

AFT CARGO RT BS 1500 FRAME WEB FOUND CRACKED BETWEEN RT STR 28 & STR 29, CRACK LENGTH .4375. AFT CARGO RT BS 1500 BETWEEN S28 TO S29 AREA FRAME REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: SUPPORT — CORRODED (FAIRING) · airframe 87,225 hrs · 21,374 cycles

INSPECTION TYPE:C AIR CONDITIONING BAY BODY FAIRING SUPPORT FOUND CORRODED AT BS 1155 LBL 65. CORROSION BLEND OUT 0.043" X 1" X 1.5" EXCEED SRM 53-50-01 FIG 5 LIMITS, SUPPORT REPAIRED AT LBL 65" AS PER SRM 51-40-04 FIG 1.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 87,225 hrs · 21,374 cycles

BELOW CENTER SECTION SURFACE BS 1241 RBL 104 'T' CHORD FOUND CRACKED, CRACK LENGTH 2.125". 'T' CHORD REWORKED AND INSTALLED AS PER SRM 51-10-01 AND 51-30-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

PS EMERGENCY EXIT LIGHT IN OVERHEAD FWD OF LAVATORY COMES ON ONLY MOMENTARILY THEN GOES OUT. REPLACED EMERGENCY LIGHT BATTERY PACK PER M/M 33-51-07. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

INSPECTION TYPE:A CHECK EMERGENCY LIGHT IN CIRCULAR CEILING LIGHT WILL NOT TAKE A CHARGE. REPLACED BATTERY PACK EMERGENCY LIGHT, OPS CHECKS OK.

Part: LIGHT — INOPERATIVE (COCKPIT)

F/E O2 REG INOP. *S/D* REMOVED AND REPLACED 02 REG BACKGROUND LIGHTS INOP. FOUND WIRES BROKEN BEHIND FE'S OXY GEN REGULATOR. REPAIRED WIRES WITH REF TO BOEING STD WIRING PRAC MANUA L 20-10-13. LIGHTS OPERATED NORMAL AND PLACARD REMOVED. THIS CLEARS M297824.

Part: DOOR FRAME — CRACKED (RT GEAR DOOR)

RT AFT BODY GEAR DOOR ATTACH FRAME CRACKED. REMOVED CRACKED CHANNEL; OK TO INSTALL REPLACEMENT FRAME; BEGAN INSTALLATION; OF NEW FRAME 8EA FASTENERS AT AFT BULKHEAD REQUIRE INSTALLATION; FINISHED INSTALLATION AS PER SRM 51-30-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE: C, EMERGENCY LIGHT INOP CREW SERVICE DOOR (ONE). REMOVED AND REPLACED BATTERY PACK X327 IAW 33-51-00, OPS NORMAL.

Part: COUPLER — LEAKING (02 BOTTLE)

INSPECTION TYPE:N/A CREW 02 INDICATOR F/E PANEL SLOWLY DECREASED FROM 1200 TO 0 AFTER 3.5 HOURS OF FLIGHT. SYSTEM PRESS GAUGE SIDE WALL WENT TO 0 PSI. REMOVED AND REPLACED LOWER & UPPER 02 BOTTLES AS PER MM 35-10-00, FOUND UPPER BOTTLES COUPING LEAKING. PART ON ORDER, REMOVED AND REPLACED UPPER CYLINDER 02 REGULATOR, LEAK CHECK C/W NORMAL.

Part: STRINGER — SCRATCHED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C COCKPIT - BS 340-360 LEFT STR 2 AFT END AREA FOUND SCRATCH MARK. COCKPIT - BS 340-360 LEFT STR 2 STRINGER REPLACED AS PER SRM 51-10-01 PG 8.

Part: RIB — CORRODED (NR 8 FLAP) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C LEFT WING - NR 8 VC FLAP I/B ARM I/B RIB ROTARY ACTUATOR NR 2, 8 MOUNTING BOLT HOLES CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 8 VC FLAP HOLES 878 I/B ARM I/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH AND NR 8 MOUNTING BOLT HOLE OVERSIZED TO 0.371 INCH, BUSHINGS FABRICATED & INSTALLED.

Part: RIB — CORRODED (NR 7 FLAP) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C LEFT WING - NR 7 VC FLAP I/B ARM O/B RIB ROTARY ACTUATOR NR 1, 3, 4, 5, 7, 8 MOUNTING BOLT HOLES CORRODED (LOOK O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 7 VC FLAP OLES 974 I/B ARM O/B RIB ROTARY ACTUATOR NR 1, 3, 4, 5, 7, 8 MOUNTING BOLT HOLES OVERSIZED TO 0.371 INCH, BUSHINGS FABRICATED & INSTALLED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE: C, AFT CARGO STA 1740 S42R STRINGER END CRACK. AFT CARGO COMPT BS 1740 STR 42R STRINGER REPAIR CARRIED OUT AS PER HX RS R53-61-35135, UPS ENGINEERING FILE NR 747-53-20181.

Part: RIB — CORRODED (NR 8 FLAP) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C LEFT WING - NR 8 VC FLAP I/B ARM O/B RIB ROTARY ACTUATOR NR 4 MOUNTING BOLT HOLE CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 8 VC FLAP HOLES 888 I/B ARM O/B RIB ROTARY ACTUATOR NR 4 MOUNTING BOLT HOLE OVERSIZED TO 0.328 INCH AS PER SRM 57-20-03 FIG 6 & NDT CHECKED NO CORROSION FOUND, REPAIR WITHIN SRM 57-20-03 FIG 6 LIMIT.

Part: RIB — CORRODED (NR 8 FLAP) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C LEFT WING - NR 8 VC FLAP O/B ARM I/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 8 VC FLAP HOLES 928 O/B ARM I/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH, BUSHINGS FABRICATED & INSTALLED.

Part: RIB — CORRODED (NR 10 FLAP) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C LEFT WING - NR 10 VC FLAP O/B ARM O/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE CORRODED (LOOK O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 10 VC FLAP OLES 766 O/B ARM O/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH & BUSHING FABRICATED & INSTALLED.

Part: RIB — CORRODED (NR 7 FLAP) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C LEFT WING - NR 7 VC FLAP O/B ARM O/B RIB ROTARY ACTUATOR NR 4, 5 MOUNTING BOLT HOLES CORRODED (LOOKS O/B COUNTS CLOCKWISE FROM TOP). LEFT WING NR 7 VC FLAP OLES 1024 O/B ARM O/B RIB ROTARY ACTUATOR NR 4, 5 MOUNTING BOLT HOLES OVERSIZED TO 0.388 INCH, BUSHINGS FABRICATED & INSTALLED.

Part: RIB — CORRODED (NR 4 FLAP) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C LEFT WING - NR 4 VC FLAP I/B RIB ROTARY ACTUATOR NR 3 & 4 MOUNTING BOLT HOLES CORRODED (LOOKS O/B COUNTS CLOCKWISE FROM TOP). LEFT WING NR 4 VC FLAP OLES 1277 I/B RIB ROTARY ACTUATOR NR 3 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH AND NR 4 MOUNTING BOLT HOLE OVERSIZED TO 0.371 INCH BUSHINGS FABRICATED & INSTALLED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C FUSELAGE BS 835 - 845 STR 39R FOUND PREVIOUSLY REPAIR PATCH LOWER ROW FASTENERS SHORT EDGE MARGIN. EXISTING SKIN CUTOUT ENLARGED PER SRM 51-10-01 AND REPROTECTED AS PER SRM 51-10-02 SKIN REPAIR CARRIED AS PER SRM 53-30-03 FIG 11 CATEGORY B REPAIR REQUIRE REPEAT INSPECTION AS PER SRM 53-30-03 FIG 11 TABLE II.

Part: RIB — CORRODED (NR 7 FLAP) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C LEFT WING - NR 7 VC FLAP O/B ARM I/B RIB ROTARY ACTUATOR NR 2, 3, 4, 5, 7 BOLT HOLES CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). DUE CORROSION BLEND OUT EXCEED MAX DIA 0.371 INCH, LEFT WING NR 7 VC FLAP OLES 1015 O/B ARM I/B RIB REPLACED AS PER SRM 51-10-01 PG 8, VC FLAP R & I PER MM 27-81-02, RIGGING & OPERATION CHECK C/OUT PER MM 27-81-00, BUSHING FABRICATED & INSTALLED.

Part: RIB — CORRODED (NR 8 FLAP) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C LEFT WING - NR 8 VC FLAP O/B ARM O/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 8 VC FLAP OLES 938 O/B ARM O/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH, BUSHING FABRICATED & INSTALLED.

Part: RIB — CORRODED (NR 5 FLAP) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C LEFT WING - NR 5 VC FLAP I/B RIB ROTARY ACTUATOR NR 3 & 4 MOUNTING BOLT HOLES CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 5 VC FLAP OLES 1205 I/B RIB ROTARY ACTUATOR NR 3 MOUNTING BOLT HOLE OVERSIZED TO 0.341 INCH & WITHIN SRM 57-20-03 FIG 6 LIMITS. NR 4 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH BUSHING FABRICATED & INSTALLED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C FWD CARGO LT STA 880 SLOPE PNL SUPPORT WEB CRACKED. FWD CARGO LT BS 880 BETWEEN S37L AND S38L FRAME REPAIR CARRIED OUT AS PER HX RS R53-22-35138, UPS ENGINEERING FILE NR 747-53-20176.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C NR 2 PYLON AFTER LOWER SPAR WEB NAC STA 240 AND NAC STA 256 I/B EDGE AREA CRACKS ARE FOUND AT 2 LOCATION AS MARK. NR 2 PYLON LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE: C, FWD CARGO FX 880 FRAME CRACKED BETWEEN STR 37-38R. FWD CARGO COMPT BS 880 RT BETWEEN S37R AND S38R FRAME REPAIR CARRIED OUT AS PER HX RS R-53-22-35139, UPS ENGINEERING FILE NR 747-53-20177.

Part: FRAME — CRACKED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE: C, M/D - STA 360 S17L POSITION FRAME CRACK. M/S BS 360 STR 17L FRAME REPAIR CARRIED OUT AS PER HX RS R-53-12-35134 AND UPS EO B747-5310-20297.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE: C, FX - KEELBEAM BOX INTERIOR LOWER WEB FOUND HEAVY CORROSION AT STA 1112 TO STA 1115 RBL 3 TO RBL 6. CORROSION BLEND OUT 0.039 X 2 X 2 INCH. KEEL BEAM BOX LOWER WEB REPAIRED AS PER HX RS R53-49-35142 AND UPS ENGINEERING FILE NR 747-53-20182, NRC 5728 FOR REPAIR DETAILS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C FWD CARGO LT STA 920 SLOPE PNL SUPPORT WEB CRACKED. FWD CARGO COMPT LT BS 920 BETWEEN STR 37L AND STR 38L FRAME REPAIR CARRIED OUT AS PER HX RS R53-22-35141, UPS ENGINEERING FILE NR 747-53-20178.

Part: FRAME — CRACKED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE:C FWD CARGO FS 900 FRAME CRACKED BETWEEN STR 37-38R. FWD CARGO COMPT BS 900 BETWEEN STR 37R AND 38R FRAME REPAIR CARRIED OUT AS PER HX RS R-53-22-35140 AND UPS ENGINEERING FILE NR 53-20179.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE: C, M/D - BS 270 LEFT VERTICAL WEB FOUND CRACKED AT I/B CHORD AREA AT STR 26. VERTICAL WEB DOUBLER REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: SKIN — CHAFED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE: C, TAIL FUSELAGE FWD OF 2360 S3L - S5L VERTICAL FIN LWR PANEL ATTACHMENT AREA CHAFE MARKS FOUND. BS 2335 - BS 2355 BETWEEN STR 4L AND STR 3L CHAFED SKIN REPAIRED PER SRM 53-30-03 FIG 1 CATEGORY B REPAIR REQUIRE REPEAT INSPECTION PER SRM 53-30-03 FIG 1 TABLE 4.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE: C, M/D BS 270 RIGHT VERTICAL I/B SUPPORT ATTACH WEB FOUND CRACKED AS MARKED AT S-26R. WEB DOUBLER REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE: C, M/D-CTR SECTION FLOOR SUPPORT WEB LWR CHORD FOUND CORROSION AS MARKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.055 X 1 X 3 INCH, EXCEED SRM 53-10-01 FIG 1 LIMITS. CHORD REPAIRED REFER SRM 51-40-04 FIG 3 CIC APPLIED IAW EO M-5100-2780E.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE: C, FX - KEELBEAM BOX LOWER EXTERNAL WEB ACCESS HOLE DOUBLER FOUND CORROSION CRACKED AT STA 1112 TO STA 1115 RBL 3 TO RBL 6. CORROSION BLEND OUT 0.050 X 2 X 2 INCH. DOUBLER, FILLER AND 2EA SPLICED ANGLE FABRICATED AND REPAIR PART INSTALLED AS PER RS 53-49-35142, UPS ENGINEERING FILE 747-53-20182.

Part: SKIN — BULGED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE: C, FX - LOWER FUSELAGE EXTERNAL SKIN FOUND BILGE UP AT STA 1000 STR 40L TO STR 41L. BS 980-998 BETWEEN STR 40L AND STR 41L SKIN REPAIR CARRIED OUT AS PER SRM 53-30-03 FIG 1 CATEGORY B REPAIR REQUIRE REPEAT INSPECTION PER SRM 53-30-03 FIG 1 TABLE 4.

Part: SKIN — DENTED (FUSELAGE) · airframe 84,505 hrs · 20,783 cycles

INSPECTION TYPE: C, VISUAL INSPECTION OF FUSELAGE DENT .110 INCH DEEP MINOR AXIS 2.5 INCH AT FX 270 30 INCH BELOW FIRST OFFICER'S WINDOW. FUSELAGE BS 265-275 BETWEEN STR 9R AND STR 10R SKIN REPAIR CARRIED OUT AS PER SRM 53-30-03 FIG 1 CATEGORY A REPAIR.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:ASV FORWARD L1 DOOR EMERGENCY LIGHT "L1853" INOP. RELAMPED L1 DOOR FORWARD EMERGENCY LIGHT OPS CHECKS GOOD

Part: REGULATOR — LEAKING (OXYGEN SYS)

ON PREFLIGHT CREW QXYGEN WAS 10 AT TOP OF CLIMB QUANTITY WAS 6.5 MONITORED FOR THE NEXT 25 MINUTES AND QUANTITY DROPPED TO 5.5 NOTIFIED DISPATCH AND RETURNED TO SDF. REMOVED AND REPLACED BOTH CREW O2 BOTTLES PER MM 12-15-08 REMOVED AND REPLACED 2ND OBS O2 REG. AND MASK PER MM 35-11-07 AND OPS CHECKED PER 35-11-07(MASK ASSY P/N 358-1510V S/N N/S/N LOC FIRST OBS

Part: LONGERON — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

DURING C CHECK, LT BLG OVERWING LONGERON BS 1413 FOUND TWO CRACKS BOTH CRACKS THROUGH THICKNESS ONE CRACK IS 5.5 INCH INLENGTH ANOTHER ONE CRACK IS 3 INCH IN LENGTH . BS 1413 LT OVERWING LONGERON ANGLE REPAIR CARRIED OUT AS PER HX RS R-53-43-34909 AND RA 747-53-20114.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

DURING C CHECK, CRACK FOUND AT RT SIDE OF BS 1350 OVERWING LONGERON, THE CRACK FOUND INITIATED FROM FWD EDGE OF VERTICAL FLANGE RUNNING TOWARD AFT TO I/B HORI FLANGE, TOTAL LENGTH OF CRACK 2 INCH LONG APPROXIMATELY. BS 1350 RT OVERWING LONGERON UPPER CHORD CRACKED AND CORRODED INTERIM REPAIR CARRIED OUT AS PER HX RS R-53-41-34906 & EA 747-53-20110 REPEAT INSPECTIONS EVERY 2000 FLTS PER REF 'F' SB747-53-2291 APPLY.

Part: PANEL — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C M/D BS 1241 RBL 6 FUEL LINE CLOSURE PANEL LOWER CUTOUT FOUND CRACK AFTER ATTACH PANEL REMOVED. BS 1241 RBL 6 CANTED BULKHEAD WEB FUEL LINE CLOSURE PANEL CUTOUT REPAIR CARRIED OUT AS PER HX RS R-53-48-34908, RA 747-53-20113

Part: SPLICE — CORRODED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C RT OVERWING LONGERON LWR INBOARD SPLICE FITTING AT BS 1460 - 1480 FOUND CORRODED AFTER SPLICE FITTING REMOVED FOR CORROSION CLEAN UP ACCESS (RBL 113). SPLICE FITTING REPLACED AS PER SRM 51-30-04 DUE CORROSION EXCEED SRM 53-10-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C CRACK FOUND AT LT OF BS 1480 UPPER BULKHEAD CHORD LOWER RADIUS AT FORWARD SIDE (BLG WHEEL WELL) CRACK LENGTH 1.25 INCHES APPROX WHICH INITIATED FROM LOWER EDGE EXTENDED UPWARD. (STR L32 TO L32) BS 1480 LT UPPER BULKHEAD CHORD LOWER RADIUS CRACK REPAIR CARRIED OUT AS PER HX RS R-53-43-34898 AND EO B747-5310-17628-A

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C M/D BS 320 BL 0 - RBL 1 FLOORBEAM LOWER CHORD CRACKED. FLOORBEAM LOWER CHORD CRACKED AREA REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: SKIN — MISREPAIRED (PAX DOOR) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C M/D- BS 460 - 480 WL 208 - 216, LT NR 1 DOOR EXTERIOR SKIN FOUND NON-STANDARD REPAIR. SKIN REPAIRED AS PER SRM 52-00-03 FIG 3 & MPI# 16130.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C M/D- BS 2230 - 2240, S17-18L, 5L CUTOUT FWD STOP FITTING REVEAL FOUND CRACK. REVEAL PANEL REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C RT BLG W/W STA 1360 TO STA 1372 S33R OVERWING LONGERON UPPER BONDED SKIN FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDED SRM 53-30-01 FIG 1 LIMITS, SKIN REPAIR CARRIED OUT AS PER HX RS NR R53-41-34906 AND RA NR 747-53-20110.

Part: FITTING — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C LT BS 1480 BULKHEAD LONGERON EXTENSION FITTING 1 FASTENER HOLE FOUND CRACK.(STR L33 TO L34). LH EXTENSION FITTING #1 BOLT HOLE REWORKED AS PER RS R53-43-34907 AND EO B747-5310-17618-A

Part: SPLICE — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

RT BS 1480 BULKHEAD AREA HOLE NR 23 CRACK FOUND AT OUTER CHORD SPLICE FITTING APPROX .125 INCH RUNNING INBOARD AND OUTBOARD STR R33 TO R34, RT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING HOLE NR 23 REWORKED AND CRACK FREE, OUT OF SB 'D' MAX LIMIT. NEW OUTER CHORD SPLICE FITTING REPLACED AS PER SRM 51-30-04.

Part: WEB — CORRODED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

U/D FLOOR WEB FOUND CORRODED AT FLANGE AREA. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT EXCEEDED SRM 53-10-01 LIMITS WEB REPAIR REFER SRM 51-40-03 FIG 3.

Part: RIB — CRACKED (RT WING) · airframe 81,157 hrs · 20,074 cycles

DURING C CHECK, RT W 22 V/C FLAP I/B ROTARY ACTUATOR MOUNTING RIB MOUNT BOLT HOLE SURFACE CORROSION REVEALED AT ALL MOUNT HOLES AND BORES. (RHW OLES 1205) RT W 22 V/C FLAP I/B ROTARY ACTUATOR RIB REPAIRED AS PER RS R57-41-34900 & EO B747-5740-17619-A. ROTARY ACTUATOR R + I PER MM 27-81-07 RIGGING AND OPERATION CHK C/OUT PER MM 27-81-00 EO B747-5740-17619-A ACCOMPLISHED.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C RT BS 1480 BULKHEAD AREA HOLE 23 CRACK FOUND AT WEB SPLICE PLATE APPROX .125 INCH RUNNING I/B AND O/B STR R33 TO R34. RT BS 1480 BULKHEAD WEB SPLICE PLATE REPLACED AS PER SRM 51-30-04 DUE CRACKED HOLE REWORKED AND OUT OF SB 747-53A2390 'D' MAX LIMIT.

Part: FRAME — CORRODED (RT MLG WW) · airframe 81,157 hrs · 20,074 cycles

C CHECK, RT WLG W/W OVERWING LONGERON I/B CHORD O/B SIDE CORROSION REVEALED AT STA 1250-1265 RBL 120. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.080 X 1 X 5 INCHES EXCEED SRM 53-10-01 LIMITS. CHORD REPAIRED PER FIG 51-40-04 FIG 3.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

LEFT BLG W/W O/B SIDEWALL BELOW LOWER CHORD ATTACH BRACKET CORROSION REVEALED AT STA 1394 LBL 122-130. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDED SRM 53-10-01 FIG 1 LIMITS. BRACKET REPLACED PER SRM 51-10 -01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C LT BS 1480 LONGERON EXTENSION FITTING NR 9 FASTENER HOLE FOUND CRACK. (STR L33 TO L34). LH EXTENSION FITTING 9 BOLT HOLE REWORKED AS PER RS R53-43-34907 AND EO B474-5310-17618-A

Part: SKIN — DENTED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C FX- EXTERNAL SKIN SURFACE FOUND DENTS AT BS 700 S40L TO S41L AREA AS MARKED. SKIN REPAIRED AT FX BS700 BETWEEN S40L TO S41L AS PER SRM 53-30-03 FIG 1 & MPI 16131

Part: WEB — CORRODED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C U/D- FLR SUPPORT ATT CURVE WEB FOUND HEAVY CORR AS MARKED. (BS 460, WL 307, RBL 24) CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.032" X 1" X 2" EXCEED SRM 53-10-01 LIMITS, WEB REPAIRED PER SRM 51-40-03 FIG 3

Part: PANEL — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

DURING C CHECK, M/D- BS 1238-1265 RBL 75-98 CLOSURE PANEL CRACKED. M/D RT BS 1241 CANTED PRESSURE DECK CLOSEOUT PANEL REPLACED AS PER EO# B747-5310-2758-E APPENDIX 'E'.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C RT WLG W/W KEEL BEAM TOP PANEL CORROSION REVEALED AT STA 1275-1350 RBL 0-10. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT EXCEEDED SRM 53-10-01 FIG 1 LIMITS. WEB REPAIRED AT STA 1345 RBL 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C CRACK FOUND ON LT BS 800 FRAME CHORD AT STR 16 AT FWD LOWER FASTENER HOLE BY APPROX 1/16 INCHES LONG RUNNING FWD LT BS 800 FRAME STRAP AND CHORD AT STR 16 FWD LWR FASTENER HOLE CRACKED. REPAIRED AS PERPER RS R53-022-34894 & EO B747-5310-17629- A

Part: STRAP — CRACKED (BS 800) · airframe 81,157 hrs · 20,074 cycles

DURING C CHECK, CRACK FOUND ON LT BS 800 FRAME STRAP AT STR 16 AREA AT FWD MOST LOWER FASTENER HOLE BY APPROX 3/8 LONG RUNNING AFT & FWD TO THE EDGE. LT BS 800 FRAME STRAP AT STR 16 & STR 17 MOST LWR FASTENERS HOLE CRACKED REPAIRED AS PER RS R53-22-34894 & EO B747-5310-17628A REPAIRED DETAILS REF NRC#UW59712 CONTINUE INSPECTIONS EVERY 3000 FLT CYCLES PER REF /A AS PER RS R53-22-34894 & EO B747-5310-17628A.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C LT WLG W/W FWD BULKHEAD UPPER AREA BELOW DRAIN V/V CORROSION REVEALED AT STA 1241 LBL 103. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDED SRM 57-10-01 LIMITS, WEB ANGLE REPAIR CARRIED OUT PER HX RS NR R53-43-34905, AND RA NR 747-53-20107.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C M/D- BS 2231, STR 24L REVEAL PANEL FOUND CRACK. M/D BS 2231 LT FRAME DOOR REVEAL AT S24L AREA REPAIR CARRIED OUT AS PER HX RS NR R-53-62-34896, AND EO B747-5310-17606-A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,157 hrs · 20,074 cycles

INSPECTION TYPE:C CRACK FOUND AT AFT CARGO DOOR CUTOUT FWD UPPER CORNER MOST AFT REMOVED FASTENER HOLE, TWO CRACKS FOUND ON SKIN OUTER SURFACE WITH LENGTH 1/16" AND 3/32" APPROX AT 1 AND 7 O'CLOCK RESPECTIVELY. (BS 1810, WL 199) AFT CARGO DOOR CUT-OUT FWD UPPER CRACKED SKIN REPAIRED AS PER SRM 53-30-03 FIG. 62 DETAIL II. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-30-03 FIG 62 TABLE III CATEGORY 'B' REPAIR.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 80,865 hrs · 20,019 cycles

INSPECTION TYPE:SP STA 720 STR 44L SHEAR TIE IS CRACKED. REMOVED DAMAGED SECTION OF SHEAR TIE, NDT VERIFIED NO CRACKS. AFTER DAMAGE REMOVAL, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-10-04.

Part: FIRE WARNING — FALSE INDICATION (COCKPIT)

INSPECTION TYPE:N/A ON T/O ROLL AND INITIAL CLIMB THE GLARESHIELD, BOTH MASTER FIRE LIGHTS FLICKERED 3 TIMES WITH NO INDICATION OF SOURCE. IN TESTING ALL FIRE DETECTION SYSTEMS WHEEL FIRE DID NOT TEST. AFTER RESET OF P-6 CB, ALL OPS NORMAL PER 26-11-00.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS UNARMED ANNUNCIATOR WILL NOT ILLUMINATE. RELAMPED UNARMED ANNUNCIATOR LIGHT, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS OVER ESCAPE SLIDE DOOR INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY PER AMM 33-51-04. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT CREW SERVICE DOOR CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED CEILING EMERGENCY LIGHT ASSY IAW B747 MM 33-51- 07, OPS CHECKS GOOD.

Part: STRUCTURE — CRACKED (PAX DOOR)

INSPECTION TYPE:C6 CRACK REVEALED ON R1 MAIN ENTRANCE DOOR LOWER CORNER BY APPROX. 1.5 INCH LONG AS MARKED. DOOR LWR CORNER REPAIRED AS PER SRM52-10-02 FIG 10.

Part: FITTING — CRACKED (FUSLEAGE)

INSPECTION TYPE:C6 CRACKS REVEALED ON AFT CARGO DOOR ROTARY ACTUATOR ATTACH FITTING AT BS 1820 AND 1900 AS PER ATTACHED FIGURE. REFER EO 747-5320-12180-A, AREA DEFECT RECTIFICATION CUTOUT.

Part: STRUCTURE — CRACKED (PAX DOOR)

INSPECTION TYPE:C6 M/D - R2 DOOR FWD LWR CORNER FOUND CRACKED. DOOR FWD LWR CORNER REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 M/D -BS 1352-1354 S18 RT, STRINGER END FOUND CRACK. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 FOR WORK DETAIL.

Part: SEAT TRACK — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 M/D - BS 2240 - 2280 LBL 11 SEAT FLANGE FOUND CHIPPED & CRACKED AS MARKED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.

Part: DOOR FRAME — CRACKED (PAX DOOR)

INSPECTION TYPE:C6 M/D - R2 DOOR FWD EDGE MOST UPPER STOP CUTOUT AREA FOUND CRACKED. DOOR CUTOUT EDGE REPAIRED AS PER SRM 52-10-02 FIG 8.

Part: FLOORBEAM — CORRODED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - M/D FLOORBEAM BS2220, RBL 57 UPPER CHORD CORRODED. FLOORBEAM REPAIRED AS PER SRM 53-10-01 FIG 1. BLEND OUT CORROSION. DEPTH 0.056 INCH , WIDTH 1 INCH , LENGTH 2 INCHES.

Part: SPLICE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 M/D - BS 1007 S1R , STRINGER END SPLICE FITTING FOUND CRACK. STRINGER END SPLICE FITTING REPLACED AS PER SRM 51-10-01.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 M/D - BS 1560, S24R-S25R FRAME O/B AREA FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 M/D - BS 742 - 744 , S23 RT STRINGER END FOUND CRACK. STRINGER REPAIRED.

Part: FLOORBEAM — CORRODED (CARGO BAY)

INSPECTION TYPE:C6 FWD CARGO COMPT BS 800 LBL 40 FLOORBEAM UPPER SURFACE ANCHOR NUT ATTACH AREA FOUND CORRODED AS MARKED. FLOORBEAMS REPAIRED AS PER 51-40-04 FIG 2. BLENDED OUT CORROSION. DEPTH 0.030 INCH , WIDTH 1 INCH , LENGTH 2 INCHES.

Part: FRAME — CORRODED (FUSELAGE)

INSPECTION TYPE:C6 FWD CARGO COMPT STA 800 S45L TO S46L FRAME CHORD & WEB FOUND CORRODED. BS 800 STR 45L - 45R FRAME ATTACH LWR ''T'' CHORD AND WEB REPLACED AS PER SRM 5101 P.8. BLEND OUT CORROSION DEPTH 0.050 , WIDTH 1 INCH , LENGHT 2 INCHES.

Part: SHEAR TIE — CORRODED (FUSELAGE)

INSPECTION TYPE:C6 FWD CARGO COMPT STA 820 STR 45L AND 46L SHEAR TIE CORRODED. DOME NUT PLATE REPLACED AS PER SRM 51-10-01 P.8.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 M/D - BS 1467 - 1478, STR 9R, STRINGER END FOUND CRACKED. STRINGER END ANGLE REPAIRED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

INSPECTION TYPE:C6 M/D - BS 1241-1265 LBL 116 O/B LONGITUDINAL FLOOR SUPPORT FOUND CORRODED. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01. CORROSION REMOVED IAW SRM 51-10-01. BLEND OUT COR. DEPTH 0.036 INCH, WIDTH 1INCH , LENGTH 2 INCH.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:C6 FWD CARGO COMPT BILGE AREA SKIN FOUND CORRODED AT FS 976-980 S45R- 46R AREA. FX SKIN REPAIRED AS PER SRM 53-30-03 FIG 1.

Part: SHEAR TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 M/D - BS 1220, STR 10R - 11R, FRAME ATTACH SHEAR TIE FOUND CRACK. SHEAR TIE ANGLE REPLACED AS PER ARM 51-10-01 P.8 AND 51-30-02.

Part: SHEAR TIE — CORRODED (FUSELAGE)

INSPECTION TYPE:C6 AFT CARGO COMPT - FRAME SHEAR TIE AFT FACE FOUND CORRODED AT STA 1680, BETWEEN STR 51 LT TO STR 51 RT. AFT CARGO COMPT SHEAR TIE CORROSION REMOVED & REPAIRED PER SRM 53-10-04 FIG 3A. BLEND OUT CORROSION DEPTH 0.030 INCH, WIDTH 1 INCH, LENGTH 2 INCH.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 800 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS1007 S-1L STRINGER END FOUND CRACKED. STRINGER END ANGLE REPAIRED.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN BS 880 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 880 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 920 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2.

Part: DOOR FRAME — CRACKED (PAX DOOR)

INSPECTION TYPE:C6 MAIN DECK - L3 DOOR LOWER FWD CORNER REVEAL FOUND CRACKED. CORNER REVEAL REPLACED AS PER SRM 51-10-01.

Part: TIE — CRACKED

INSPECTION TYPE:C6 CABIN - BS 920 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747310890 FIG 2.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 780 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG.2.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 987 S-15R STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 820 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 1007 S-3L STRINGER END FOUND CRACKED. STRINGER REPAIRED.

Part: ANGLE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 BODY CREASE BEAM STRUCTURE - FRAME ATTACH FWD ANGLE BEND RADIUS FOUND CRACKED AT BS 960 STRINGER 7L AS MARKED. ANGLE REPLACED AS PER SRM 51-10-01.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 940 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2.

Part: FITTING — CRACKED (PAX DOOR)

INSPECTION TYPE:C6 MAIN DECK - R3 DOOR FWD CUTOUT NR 5 DOOR STOP SUPPORT FITTING FOUND CRACKED. REFER NRC 6124 FOR FITTING REPLACEMENT DETAIL.

Part: DOOR FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 M/D - R3 DR LOWER FWD CORNER REVEAL FOUND CRACKED. CORNER REVEAL REPLACED AS PER SRM 51-10-01.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 1007 S-2L STRINGER END FOUND CRACKED. STRINGER END REPAIRED.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 940 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 1007 S-5L STRINGER END FOUND CRACKED. STRINGER END REPAIRED.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 820 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747 AS PER EO B747-5310-5890 FIG 2.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 800 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 780 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 860 RT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2.

Part: TIE — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 860 LT TENSION TIE FOUND CRACKED. TENSION TIE REPAIRED AS PER EO B747-5310-5890 FIG 2.

Part: FITTING — CRACKED (PAX DOOR)

INSPECTION TYPE:C6 MAIN DECK - R3 DOOR FWD CUTOUT NR 5 STOP SUPPORT FITTING FOUND CRACKED. R3 DOOR FWD NO.5 STOP FITTING REPLACED AS PER SRM 51-10-01.

Part: DOOR FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - R4 DOOR AFT LOWER FRAME CORNER CRACKED. DOOR LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 M/D FRAME CUP FOUND CRACKED AT BS 1660 JUST ABOVE STR 16R. FRAME CUP REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 MAIN DECK - FRAME CUP FOUND CRACKED AT BS 900 JUST ABOVE STR 22L. FRAME CUP REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS1007 S-1R STRINGER END FOUND CRACKED. STRINGER REPAIRED.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS987 S-15L STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 1007 S-3 RT STRINGER END FOUND CRACKED. STRINGER REPAIRED.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS1007 S-5R STRINGER END FOUND CRACKED. STRINGER REPAIRED.

Part: SEAT TRACK — CORRODED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - M/D FLOOR TIE DOWN TRACK (BS 1920-1940, LBL 97) CORRODED. SEAT TRACK REPLACED AS PER SRM 53-10-05 FIG 1A. BLEND OUT CORROSION DEPTH 0.038 INCH , WIDTH 1 INCH , LENGTH 3 INCHES.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 920 S-25L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 11.

Part: FITTING — CRACKED (BULKHEAD)

INSPECTION TYPE:C6 CRACKS REVEALED ON RT BS 1000 BULKHEAD ATTACHED BATH TUB FITTING AT SEVERAL FASTENER HOLES AS MARKED. RT BS 1000 BULKHEAD ATTACH BATH TUB FTG REPLACED AS PER SRM 51-10-01 P.8.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 560 S-24L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 11.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 900 S-25L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 4.

Part: STOP FITTING — CRACKED (PAX DOOR)

INSPECTION TYPE:C6 CABIN - L1 DOOR FWD LOWER STOP FITTING CRACKED. STOP FITTING REPLACED AS PER SRM 51-10-01 P.8.

Part: STRINGER — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 740 S-23R STRINGER END FOUND CRACKED. STRINGER REPAIRED.

Part: FRAME — CRACKED (BULKHEAD)

INSPECTION TYPE:C6 CRACK REVEALED ON R/H BS 1000 BULKHEAD CHORD VERTICAL FLANGE AT LWR TENSION BOLT HOLE AT S-38 RT AREA BY APPROX. 0.050 INCH LONG AS MARKED. RT BS 1000 BULKHEAD CHORD VERTICAL FLANGE AT LWR TENSION BOLT HOLE CRACK CLEARED. HFEC INSPECTED SATIS. NEW BOLT INSTALLED PER RS#R53-42-34640.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - MAIN DECK LT O/B FLOOR SUPPORT (BS2320-2342, LBL 66-70) CORRODED. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01.

Part: FITTING — CRACKED (PAX DOOR)

INSPECTION TYPE:C6 CABIN - R1 DOOR FWD LOWER STOP FITTING FOUND CRACKED. STOP FITTING REPLACED AS PER SRM 51-10-01 P.8.

Part: SEAT TRACK — CORRODED (FUSELAGE)

INSPECTION TYPE:C6 M/D - BS 320-340 RBL 11 SEAT TRACK FLANGE FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.

Part: FITTING — CRACKED (RT MLG)

INSPECTION TYPE:C6 TWO CRACKS REVEALED ON RT MLG ACTUATOR UPPER SUPPORT FITTING O/B LUG BORE BOTH BY APPROX. 1/8 INCH LONG AS MARKED. SERVICEABLE SUPPORT FITTING REPLACED IAW SRM 51-10-01 P.8 AND BOEING SB 747-53-2298 FIG 3.

Part: FITTING — CRACKED (BULKHEAD)

INSPECTION TYPE:C6 CRACKS REVEALED ON LT BS 1000 BULKHEAD ATTACHED BATH TUB FITTING AT SEVERAL FASTENER HOLE LOCATIONS AS MARKED. LT BS 1000 BULKHEAD ATTACH BATH TUB FTG REPLACED AS PER SRM 51-10-01 P.8.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 980 S-25R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG.11.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 920 S-24 RT TO S-25 RT FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 11.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 960 S-25R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG.11.

Part: INTERCOSTAL — CRACKED (SERVICE DOOR)

INSPECTION TYPE:C6 CABIN - R4 DOOR UPPER CENTER INTERCOSTAL WEB FOUND CRACKED, DOOR INTERCOSTAL WEB REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - BS 940 S-24R TO S-25R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG.11.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 AFT CARGO COMPT - FRAME ATTACH SKIN EDGE FOUND CRACKED AT RH STA 1520 STR 28R. THE SUBJECT FRAME PREVIOUS REPAIRED AS PER SRM 53-10-04 FIG 39 & CONFIRM NO CRACK BEYOND FASTENER HOLE BY NDT.

Part: DOUBLER — CRACKED (PAX DOOR)

INSPECTION TYPE:C6 CABIN - L1 DOOR LOWER HINGE DOUBLER FOUND CRACKED. DOUBLER REPLACED AS PER BOEING SB B747-52-2144.

Part: DOOR FRAME — CRACKED (SERVICE DOOR)

INSPECTION TYPE:C6 CABIN - L4 DOOR FWD FRAME LOWER CORNER FOUND CRACKED. L4 DOOR FWD FRAME LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 10.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - ABOVE MAIN DECK FLOOR BS 2320 LT FRAME (WL 20004) INNER FRAME CRACKED. FRAME REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6, FWD CARGO RT FLOOR AREA AT BS 980 STR 39 WEB UPPER FRAME CRACKED THROUGH 1 UPPER FASTENER HOLE. REPAIRED PER SRM 53-10-04 FIG 52.

Part: BRACKET — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 CABIN - MAIN DECK LONG. FLOOR SUPPORT BRACKET CRACKED. BRACKET REPLACED

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:C6 M/D BS 2320 LT FRAME INNER FRAME FOUND CRACKED. FRAME REPAIRED PER SRM 51-40-03 FIG 1.

Part: FITTING — CRACKED (FUSELAGE)

INSPECTION TYPE:C6, CRACK REVEALED AT BS 1265 LT NR 2 STOP FITTING AND FRAME INNER CHORD ATTACH HOLE APPROX .1875 INCH LONG. STOP FITTING REPLACED AS PER SRM 51-10-01.

Part: FITTING — CRACKED (FRAME)

INSPECTION TYPE:C6, CRACK AT BS 1265 RT NR 2 STOP AND FRAME INNER CHORD ATT FASTENER HOLE, APPROX .25 INCH LONG RUNNING I/B NR 2 STOP FITTING. REMOVED AND REPLACED PER SRM 51-10-01.

Part: SPOILER — INOPERATIVE (WING)

INSPECTION TYPE:N/A, NR 6 SPOILER INOP. PIREP - ROLLS RIGHT ON LANDING. *S/D* REMOVED NR 6 SPOILER PANEL AND ACT. INSTALLED NR 6 SPOILER PER MM 27-61-01. OPS CKS GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT EXIT)

INSPECTION TYPE:C, COCKPIT EMERGENCY EXIT DOOR FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED, OPS CHECKS GOOD.

Part: HINGE — CRACKED (MLG DOOR)

INSPECTION TYPE:N/A, RT BODY GEAR STRUT OUTBOARD DOOR HINGE FITTING CRACKED. *S/D* REMOVED DAMAGE IAW SRM 51-40-03, REMOVED SUPPORT FRAME FROM A/C FOR MAINTENANCE. FABRICATED AND INSTALLED SUPPORT FRAME FOR RT BODY GEAR STRUT DOOR HINGE POINTS AS REQUIRED.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT INOP AT EMERGENCY SLIDE DOOR. REMOVED AND REPLACED LAMP. SYS OPS CHECKS NORMAL.

Part: OIL CAP — MISSING (NR 4 ENGINE)

INSPECTION TYPE:N/A, ON CLIMBOUT NR 4 ENGINE OIL PRESSURE BEGAN TO FLUCTUATE BETWEEN 35 AND 45 PSI. ENGINE OIL PRESSURE 4 LIGHT ILLUMINATED TO CONFIRM, AT 0715Z , NR 4 ENGINE SHUT DOWN WHEN OIL PRESS BELOW RED ARE CONTINUOUSLY AND OIL PRESS LIGHT ON STEADY, WINDMILLING OIL PRESS. FOUND NR 4 ENGINE OIL TANK CAP MISSING. INSTALLED NEW OIL CAP AND INSPECTED MAIN OIL FILTER AND MAG PLUGS, FOUND NON DEFECT AND ENGINE WINDMILLING. INSPECTION C/W PER MM 72-00-00, PG 699.1 AND ENGINE RUN IDLE, CHECK OK PER 71-00-00.

Part: SIGN — INOP (L1 EMER EXIT)

INSPECTION TYPE:N/A, L1 DOOR EMERGENCY EXIT SIGN INOP. REPLACED EMERGENCY EXIT SIGN, OPS CHECK GOOD.

Part: HEAT DUCT — DIRTY (CARGO COMPT)

INSPECTION TYPE:N/A, AFT LWR CARGO COMPARTMENT FIRE WARNING ACCOMPLISHED LWR CARGO COMP SMOKE DET TEST, CKD OK. THOROUGHLY INSPECTED LOWER AFT CARGO COMP, NO EVIDENCE OF FIRE FOUND. WHEN INSPECTING CGO COMPT HEAT DUCT, FOUND PLASTIC TRASH STICKING TO THE DUCT. TRASH WAS PARTLY BURNED AND MOLTEN CAUSING FIRE ALARM GOING OFF. DEFERRED AFT LWR CARGO HEAT PER MEL.

Part: BULB — FAILED (CABIN)

INSPECTION TYPE N/A, EEL IN CREW ENTRY DOOR AND MAIN CARGO DOOR INOP. RELAMPED SAME AS REQUIRED, OPS CHECK NORMAL.

Part: REAR SPAR — CORRODED (RT STABILIZER)

INSPECTION TYPE:C, RT STABILIZER REAR SPAR LWR CHORD CORRODED AT STA 473-476. SECTION SPLICED AT LWR CHORD IAW 55-10-05.

Part: SKIN — DAMAGED (FUSELAGE)

INSPECTION TYPE-N/A, FUSELAGE SKIN HAS DAMAGE BELOW MAIN CARGO DOOR. ACCOMPLISHED B747-5310-9806A EO FOR RETURN TO SERVICE AND DEFERRED AS REQUIRES. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 30 DAYS DI 143360. TRANSFERRED TO C-CHECK TEAM AER LINGUS IRE NRC 666023 REFERS.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS AT L1 CREW DOOR FWD LIGHT INOP. ALSO, FWD CEILING LIGHT PNL NOT SECURED. REMOVED AND REPLACED EMERGENCY AISLE LIGHT ASSEMBLY.

Part: WIRE — LOOSE (CABIN)

INSPECTION TYPE-N/A, FWD ENTRY DOOR FWD EMERGENCY LIGHT OUT. RELAMPED TWO NEW BULBS, NO HELP. ALSO, FOUND FWD AND AFT LIGHT ASSY NOT ATTACHED TO BRACKETS. INSTALLED BOLTS IN FWD AND AFT LIGHT HOUSING. REMOVED AND REPLACED BATTERY PACK. FOUND GRD WIRE LOOSE, TIGHTENED. LIGHT OPS CKS OK, ON (S/N 589) OFF (S/N 16270).

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, FWD EMERGENCY EXIT LIGHT UPPER CREW SVC DOOR INOP. RELAMPED, OPS CKS OK.

Part: STRINGER — CORRODED (BS 1700)

INSPECTION TYPE-C, CORROSION ON LOWER SIDE OF STRINGER 60R AT BS 1700. REPLACED STRINGER PER SRM 53-10-03, 53-10-1.

Part: PRESSURE PAN — DELAMINATED (BS 2360)

INSPECTION TYPE-C, PRESSURE PAN DELAMINATED AT BS 2360, RT HYDRAULIC LINE, APU CUT OUT REINFORCEMENT. REPLACED PRESSURE PAN IAW SRM 51-30-2.

Part: SKIN — CORRODED (WS 1437-1462)

INSPECTION TYPE-C, CORROSION ON LT LOWER WING SKIN AT OLES 1437 TO 1462. REPAIRED PER UPS EFN 747-57-0338, BOEING DRAWING 65B22997-11.

Part: BULKHEAD WEB — CRACKED (BS 1480)

INSPECTION TYPE-C, CRACK IN BULKHEAD WEB AT BS 1480. INSTALLED REPAIR DOUBLER IAW UPS EO B747-5310-3100C.

Part: SKIN — CORRODED (WS 1386)

INSPECTION TYPE-C, CORROSION ON LT WING LOWER SKIN AT OLES 1386. REPAIRED PER UPS EFN 747-57-0338, BOEING DRAWING 65B22997-11.

Part: TRUSS FITTING — CRACKED (BS 1810)

INSPECTION TYPE-C, FORWARD TRUSS FITTING POS 9 CRACKED AT FWD LOWER FLANGE. REPLACED LATCH AND TRUSS FITTINGS IAW UPS EO B747-5340-0191.

Part: PRESSURE PAN — DELAMINATED (BS 2360)

INSPECTION TYPE:C PRESSURE PAN UPPER SIDE DAMAGED AT APU CUT OUT REINFORCEMENT BS 2360. REPLACED PRESSURE PAN IAW SRM 51-30-02, 51-40-00.

Part: SKIN — CORRODED (RT WING)

INSPECTION TYPE: C. RT LOWER WING SKIN, REPAIRED CORROSION INSIDE LEADING EDGE CAVITY FORWARD OF LOWER FRONT SPAR AT ILES 944.1015. REPAIRED LOWER SKIN ACC KLM DFX96-192. APPROVED PER UPS EFN 747-57-0339.

Part: SPLICE ANGLE — CRACKED (BS 1960)

INSPECTION TYPE: C. BULK CARGO COMPARTMENT, FOUND DURING REPAIR OF FRAME, CRACK BS 1360 NRC 7126 21, A CRACK IN SPLICE ANGLE AT BS 1960 FRAME/SPLICE S34L. REPLACED FRAME/SPLICE ANGLE ACC TO SRM 51-30-02.

Part: WEB — CORRODED (LT MLG WW)

INSPECTION TYPE-C, LT BLG WHEEL WELL CORNER OF PRESSURE DECK WEB STA 1372, LBL 127 IS CORRODED. PRESSURE DECK WEB REPAIRED ACC SRM 53-10-07.

Part: STIFFENER — CORRODED (LT MLG WW)

INSPECTION TYPE-C, LT WLG WHEEL WELL STA 1241 FOUND CORROSION ON THE 2ND STIFFENER I/B OF THE BULKHEAD FITTING LBL 80. CORROSION REMOVED IAW SRM 51-10-01, STIFFENER OUT OF LIMIT IAW 53-10-01, REPLACED STIFFENER ACC SRM 51-30-02.

Part: SPLICE — DAMAGED (BS 520)

INSPECTION TYPE: C. STRINGER SPLICE 16 FRAME STA 520 LT DAMAGED. REPLACED STRINGER SPLICE 16 AT STA 520 LT IAW SRM 51-30-02.

Part: SPLICE — DAMAGED (BS 520)

INSPECTION TYPE: C. STRINGER SPLICE DAMAGE AT STR 23 AND STR 24 STA 520 LT. REPLACED STRINGER SPLICE STR 23 AND STR 24 STA 520 LT IAW SRM 51-30-02.

Part: SKIN — MISDRILLED (BS 340-360)

INSPECTION TYPE: C. EXISTING HOLE PITCH ON STR 6 BETWEEN STA 340 AND STA 360 LT HAS A SHORT FASTENER SPACING BETWEEN 9 FASTENERS. INSTALLED BACR15BB6D8 ON STR 6 BETWEEN STA 340 AND STA 360 LT ACC BOEING FAX DFX95-167.

Part: FRAME — CRACKED (BS 360)

INSPECTION TYPE: C. CRACKS ON FRAME 360 RT AT STRINGER 15 CUT-OUT AND ON CABLE PULLEY CUT-OUT. REPAIRED FRAME AT STA 360 RT IAW SRM 53-10-04.

Part: FRAME — CRACKED (BS 360)

INSPECTION TYPE: C. FRAME 360 LT CRACKED ON CABLE CUT-OUT BETWEEN STR 15 AND STR 16. FRAME 360 LT ON CABLE CUT-OUT BETWEEN STR 15 AND STR 16 REPAIRED IAW SRM 53-10-04 FIG 18.

Part: INTERCOSTAL — CRACKED (BS 400-420)

INSPECTION TYPE: C. INTERCOSTAL BETWEEN STA 400/420 RT AT STR 3A CRACKED. INTERCOSTAL BETWEEN STA 400/420 RT AT STR 3A REPAIRED IAW SRM 51-40-03.

Part: ACTUATOR FITTING — CORRODED (RT MLG WW)

INSPECTION TYPE-C, RT WING DOOR ACTUATOR BEARING HAS TOO MUCH PLAY. REMOVED BEARING, FOUND CORROSION IN THE FITTING. REMOVED FITTING FOUND CORROSION AFT SIDE FITTING AND ON THE KEEL BEAM. REMOVED MLG DOORS ACC 32-12-01, REPLACED DOOR ACTUATOR FITTING IAW 53-43-02, REPAIRED KEEL BEAM WEB ACC SRM 53-10-09 FIG 4, INSTALLED MLG DOORS ACC MM 32-12-01.

Part: STRINGER — CRACKED (BS 434)

INSPECTION TYPE: C. CRACK ON STRINGER 23 STA 434 RT. CRACK REPAIRED ON STR 23 STA 434 RT IAW SRM 51-30-02.

Part: FRAME — DAMAGED (BS 1780)

INSPECTION TYPE: C. FOUND FRAME DAMAGE AT BS 1780 STR 13 RT. REPAIRED FRAME AT BS 1780 BETWEEN STR 11 AND STR 15 RT IAW SRM 51-40-03 FIG 2.

Part: FITTING — CORRODED (BS 1416.06)

INSPECTION TYPE: C. CORROSION AT FITTING AT BS 1416.06 BETWEEN RBL 11.33 TO LBL 11.33. FITTING OUT OF LIMITS AT BS 1416.06 BETWEEN RBL 11.33 TO LBL 11.33 ACC SRM 53-10-01. REPLACED FITTING IAW SRM 51-30-02.

Part: STRINGER — CRACKED (BS 180-200)

INSPECTION TYPE: C. STRINGER 5 CRACKED BETWEEN STA 180 AND STA 200 RT. REPLACED STRINGER 5 BETWEEN STA 180 AND STA 200 RT IAW SRM 51-30-02.

Part: WEB — CRACKED (BS 440-460)

INSPECTION TYPE: C. WEB BETWEEN STA 460 AND STA 440 LT AT STRINGER 14 CRACKED. REPLACED WEB BETWEEN STA 460 AND STA 440 LT IAW SRM 51-30-02.

Part: WEB — CRACKED (BS 1380)

INSPECTION TYPE: C. FOUND FOUR CRACKS IN WEB ASSY AT BS 1380 LBL 98 TO 117. REPLACED WEB ASSY IAW SRM 51-30-02.

Part: STRINGER — CRACKED (BS 1980)

INSPECTION TYPE-C, BULK CARGO COMPT FOUND STRINGER DENTED, CRACKED AND NOT PROPERLY REPAIRED, DUE TO OLD SKIN DAMAGE AT BS 1980, S39 LT. ALSO, FOUND SHEAR TIES BENT AT SAME LOCATION. REMOVED EXISTING REPAIR DOUBLER FROM SKIN. ENLARGED EXISTING SKIN CUTOUT TO REMOVE ALL DAMAGED SKIN AND REPAIRED SKIN ACC TO SRM 53-30-03 FIG 1. REMOVED DAMAGED STRINGER AND REPAIRED STRINGER ACC SRM 53-10-03 FIG 1, REMOVED DAMAGED SHEAR TIES AND REPAIRED ACC TO SRM 53-10-04 FIG 3.

Part: STIFFENER — CRACKED (BS 2220)

INSPECTION TYPE-C, AREA AFT OF BULK CARGO COMP FOUND CORROSION AND CRACK IN TOPSIDE OF FRAME STIFFENER AT BS 2220 S-40 LT. REPLACED FRAME STIFFENER ACC SRM 51-30-02. REMOVED REMAINING CORRROSION ON FRAME ACC SRM 51-10-01, WITHIN LIMITS OF SRM 53-10-10.

Part: FLOORBEAM — CORRODED (BS 1580)

INSPECTION TYPE-C, MAIN DECK FLOOR STRUCTURE FLOOR BEAM UPPER CHORD CORRODED AT BS 1580 BTWEEN LBL 60/108. CORROSION OUT OF LIMITS IAW SRM 53-10-01. REPLACED FLOOR BEAM IAW SRM 53-10-07.

Part: FRAME — CRACKED (BS 2120)

INSPECTION TYPE: C. BULK CARGO COMPARTMENT, FOUND CRACK IN FRAME WEB AT STRINGER CUTOUT CORNER AT BS 2120, S29L. REPAIRED FRAME WEB AT STRINGER CUTOUT CORNER ACC TO SRM 53-10-04, FIG 39.

Part: UPPERCHORD — CORRODED (BS 2140)

INSPECTION TYPE: C. UPPER CHORD CORRODED AT BS 2140 BETWEEN LBL 57 TO LBL 100. REMOVED CORROSION AT UPPER CHORD AT BS 2140 BETWEEN LBL 57 TO LBL 10 0 ACC SRM 51-10-01. CORROSION NOT IN LIMITS ACC SRM 53-10-01, REPLACED UPPER CHORD FROM LBL 48 TO LBL 108 ACC SRM 53-10-07 FIG 12.

Part: STIFFENER — CRACKED (BS 1860)

INSPECTION TYPE-C, AFT CARGO COMP FOUND FRAME STIFFENER BENT AND CRACKED AT BS 1860, S41 LT. REPLACED FRAME STIFFENER ACC SRM 51-30-02.

Part: FRAME — CRACKED (BS 1860)

INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME INNER FLANGE UNDER REINFORCEMENT STRAP AT BS 1860, S41. REMOVED DAMAGED SECTION OF FRAME INNER FLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-03.

Part: FRAME — CRACKED (BS 1360 S37)

INSPECTION TYPE-C, BULK CARGO COMP FOUND CRACKS IN FRAME INNER FLANGE, WEB AND REINFORCEMENT ANGLE AT BS 1960, S37 LT. REPAIRED FRAME INNER FLANGE, WEB AND REINFORCEMENT ANGLE. REPAIR APPROVED PER EFN 747-53-0790.

Part: PRESSURE PAN — DAMAGED (BS 2360)

INSPECTION TYPE: C. BS 2360 PRESS PAN ASSY APU DUCT MOUNT FLANGE AND UPPER SIDE, MAJOR DAMAGE. REPLACED PRESS PAN AT BS 2360 IAW SRM 51-30-02.

Part: SHEAR TIE — CRACKED (BS 1700)

INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME SHEAR TIE AT SKIN ATTACHMENT AT BS 1700, S 41 AND 42 RT. REMOVED DAMAGED SECTION OF SHEAR TIE AND REPAIRED SHEAR TIE ACC SRM 53-10-04 FIG 3.

Part: SHEAR TIE — CRACKED (BS 1680)

INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME SHEAR TIE AT SKIN ATTACHMENT BS 1680, S 41 AND 42 RT. REMOVED DAMAGED SECTION OF SHEAR TIE AND REPAIRED SHEAR TIE ACC SRM 53-10-04 FIG 3.

Part: HEAT SHLD BAFFLE — CRACKED (NR 1 PYLON)

INSPECTION TYPE C, AT THE FWD LOWER SPAR WEB PYLON NR 1 HEAT SHIELD BAFFLE CRACKED AT SEVERAL PLACES. REPLACED HEAT SHIELD BAFFLE AT THE FWD LOWER SPAR WEB ACC SRM 51-30 -02.

Part: SPAR WEB — CRACKED (NR 2 PYLON)

INSPECTION TYPE-C, AT THE FWD LOWER SPAR WEB PYLON NR 2 HEAT SHIELD BAFFLE CRACKED AT SEVERAL PLACES. REPLACED HEAT SHIELD BAFFLE AT THE FWD LWR SPAR WEB ACC SRM 51-30-02.

Part: HEAT SHLD BAFFLE — CRACKED (NR 3 PYLON)

INSPECTION TYPE-C, AT THE FWD LOWER SPAR WEB PYLON NR 3 HEAT SHIELD BAFFLE CRACKED AT SEVERAL PLACES. REPLACED HEAT SHIELD BAFFLE AT THE FWD LOWER SPAR WEB ACC SRM 51-30-02.

Part: STRINGR — CRACKED (BS 1650 S32)

INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN STRINGER FLANGE AT S32 LT BS 1650. REMOVED DAMAGED SECTION OF STRINGER FLANGE AND REPAIRED STRINGER FLANGE ACC TO SRM 53-10-03 FIG 2.

Part: HEAT SHLD BAFFLE — CRACKED (NR 4 PYLON)

INSPECTION TYPE-C, AT THE FWD LOWER SPAR WEB PYLON NR 4 HEAT SHEILD BAFFLE CRACKED AT SEVERAL PLACES. REPLACED HEAT SHIELD BAFFLE AT THE FWD LOWER SPAR WEB ACC SRM 51-3 0-02.

Part: FITTING — CRACKED (BS 488/500)

INSPECTION TYPE: C. FOUND CRACKS IN FITTING DUE TO INCORRECT RIVETING PRACTICE AT BS 488 - BS 500 STR 16 LT. REPLACED FITTING AT BS 488 - BS 500 STR 16 IAW SRM 51-30-02.

Part: FRAME — CRACKED (BS 1580)

INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME INNER FLANGE AT BS 1580, S29 RT. REMOVED DAMAGED SECTION OF FRAME INNER FLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-03.

Part: SKIN — CORRODED (BS 1670/1695)

INSPECTION TYPE-C, AFT CARGO COMP FOUND HEAVY CORROSION ON INTERNAL SKIN NEAR S30 RT AT BS 1678, BS 1690 AND BS 1695. REMOVED CORRODED SECTIONS OF SKIN PANEL BY MAKING A CUTOUT 21 BY 3.5 AND REPARED SKIN PANEL ACC SRM 53-30-03, FIG 1.

Part: DOOR — CRACKED (PAX DOOR)

INSPECTION TYPE C/D, DOOR STRUCTURE LWR HINGE ARM CUTOUT FOUND SMALL CRACK. REPAIRED SMALL CRACK AT MED 1 LT HINGE ARM CUTOUT IAW SRM 51-40-03.

Part: FRAME — CRACKED (BS 1520 S29)

INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME INNER FLANGE AT BS 1520 S29 RT. REMOVED DAMAGED SECTION OF FRAME INNER FLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-03 FIG 1.

Part: SKIN — CRACKED (LT NACELLE)

INSPECTION TYPE-C, CRACK IN SKIN .75 INCH AT ACCESS PANEL CUTOUT NAC STA 207 LT. REPAIRED SKIN AT ACCESS PANEL CUTOUT NAC STA 207 LT, ACC SRM 54-30-03, FIG 17B.

Part: SHEAR TIE — CRACKED (BS 1560)

INSPECTION TYPE-C, AFT CARGO COMPT FOUND CORROSION AND CRACKS IN FRAME SHEAR TIE AT SKIN ATTACHMENT BS 1560 BETWEEN S42/41 LT. REMOVED DAMAGED SHEAR TIE AND REPAIRED FRAME SHEAR TIE ACC SRM 53-20-04 FIG 3.

Part: FRAME — CRACKED (LT NACELLE)

INSPECTION TYPE-C, CRACK IN FRAME NAC STA 285, 7 INCHES ABOVE FIREWALL. REPLACED FRAME NAC STA 285 LT ACC SRM 51-30-02.

Part: SHEAR TIES — CRACKED (BS 1660)

INSPECTION TYPE: C. AFT CARGO COMPARTMENT, FOUND CRACK IN FRAME SHEAR TIES AT SKIN ATTACHMENTS BS 1660 RT, BETWEEN S 41/40 AND S 39/38 (3 EA). REMOVED CRACKED SHEAR TIES AND REPAIRED SHEAR TIES ACC SRM 53-10-04 FIG 3.

Part: SHEAR TIE — CRACKED (BS 1580)

INSPECTION TYPE-C, AFT CARGO COMPT FOUND CRACK IN FRAME SHEAR TIE AT SKIN ATTACHMENT BS 1580 BETWEEN S34/33 RT. REMOVED CRACKED SHEAR TIE AND REPAIRED FRAME SHEAR TIE ACC SRM 53-10-04 FIG 3.

Part: FRAME — CRACKED (BS 1680)

INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME INNER FLANGE AT BS 1680, S35 TO 34 RT. REMOVED CRACKED SECTION FROM FRAME INNERFLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-03.

Part: FRAME — CRACKED (LT NACELLE)

INSPECTION TYPE-C, FRAME CRACKED AT NAC STA 163 LT. REPLACED FRAME 163 LT ACC SRM 51-30-02.

Part: SHEAR TIE — CRACKED (BS 1520)

INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME SHEAR TIE AT STRINGER CUTOUT CORNER BS 1520, S27 RT. STOP DRILLED CRACK AND REPAIRED FRAME SHEAR TIE AT STRINGER CUTOUT CORNER ACC SRM 53-10-04 FIG 39.

Part: FRAME — CRACKED (BS 1760)

INSPECTION TYPE-C, AFT CARGO COMP FOUND INNER FLANGE OF FRAME CRACKED AT BS 1760, LBL 61, BETWEEN S41 AND 42 LT NEAR SIDE GUIDE. REMOVED CRACKED SECTION OF FRAME INNER FLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-03.

Part: FRAME — CRACKED (BS 1800)

INSPECTION TYPE-C, AFT CARGO COMP FOUND INNER FLANGE OF FRAME CRACKED AT BS 1800 BETWEEN S40 AND 39 RT. REMOVED CRACKED SECTION OF FRAME INNER FLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-03.

Part: INTERCOSTAL — CRACKED (BS2000/2020)

INSPECTION TYPE-C, BULK CARGO COMP FOUND THRESHOLD SUPPORT INTERCOSTAL CRACKED AT BS 2000 AND 2020 RBL 53. REPLACED THRESHOLD SUPPORT INTERCOSTAL ACC SRM 51-30-02.

Part: SHEAR TIES — CRACKED (BS 1600/1580)

INSPECTION TYPE-C, AFT CARGO COMP FOUND FRAME SHEAR TIE AT ATTACHMENTS CRACKED AT BS 1600 AND BS 1580, BETWEEN S40 AND S41 RT. REMOVED CRACKED FLANGES OF SHEAR TIES AND REPAIRED SHEAR TIE ACC SRM 53-10-04, FIG 3.

Part: BULKHEAD WEB — CRACKED (BS 2160)

INSPECTION TYPE-C, BULK CARGO COMP FOUND CRACK IN BULKHEAD WEB AT BS 2160, RBL 56 WL 168. REMOVED DAMAGED SECTION OF BULKHEAD WEB AND REPAIRED WEB ACC SRM 51-40-02 FIG 01.

Part: WEB — CRACKED (NLG WW)

INSPECTION TYPE-C, NLG WHEEL WELL TOP PANEL WEB UNDERNEATH LT SPINBRAKE INTERCOSTAL IS CRACKED. REPAIRED WEB ACC SRM 53-30-03 FIG 1.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO COMPT)

INSPECTION TYPE PIRE, NR 5 MAIN DECK CARGO SMOKE DETECTOR ILLUMINATED. REPLACED NR 5 SMOKE DETECTOR (P/N 2156-646) (S/N 140) OFF.

Part: RELEASE MECH — INOPERATIVE (ESCAPE HATCH)

MAINTENANCE REPORTED, FLIGHT DECK OVERHEAD ESCAPE HATCH WILL NOT UNLOCK AND OPEN. RESECURED LOOSE LINKAGE IN FLIGHT DECK OVERHEAD ESCAPE HATCH DOOR, OPS CHECKS NORMAL.

Part: RELEASE HANDLE — BROKEN (ESCAPE SLIDE)

MAINTENANCE REPORTED, ESCAPE SLIDE RELEASE HANDLE CLIP BROKEN AND PAWL BROKEN MAKING ESCAPE SLIDE ARMED AND NOT SAFE. REMOVED AND REPLACED RELEASE HANDLE CLIP AND PAWL. SLIDE SECURED AND OPERATES FROM SAFE TO ARM NORMALLY.

Part: LIGHT — INOPERATIVE (CABIN)

MAINTENANCE FOUND FWD L1 DOOR EMERGENCY LIGHT AND CEILING EMERGENCY LIGHT FWD OF CREW STAIRS ARE INOP. REPLACED CEILING AISLE LIGHT ASSY L1 AND AISLE EMERGENCY LIGHT OP NORMAL.

Part: EEL CONNECTOR — LOOSE (L1 ENTRY DOOR)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LT TEST FOUND INOP, EMERGENCY LT ON L-1 ENTRY DOOR INOP, FWD LIGHT AND ONE UPPER CARGO DECK CEILING LIGHT INTERMITTENT. RESECURED CONNECTOR AT M415 EMER LIGHT ASSY, OPS CHECKS GOOD.

Part: STRINGER — CRACKED (BS 340/400)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND SEVERAL CRACKS ON STR 6 LT AT BS 340/400 BY HFEC INSP. MAINTENANCE INSTALLED REPAIR DOUBLER ACC SB53-2253R2 AND DWR 65B28212-1 AND -2 PER UPS E.O. B747-5330-7466.

Part: SHEAR TIES — CRACKED (BS 1700)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND SHEAR TIES CRACKED AND CORRODED ON BS 1700 BETWEEN STRINGER 51 LT AND STRINGER 51 RT BETWEEN STRINGER 47 AND 46, RT AND BETWEEN STRINGER 48 AND 49 RT. MAINTENANCE FOUND CRACKS AND CORROSION OUT OF LIMITS AND REPAIRED SHEAR TIES IAW SRM 53-10-01 AND 53-10-04.

Part: SHEAR TIES — CRACKED (BS 1720)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND SHEAR TIES CRACKED AT BS 1720 RT BETWEEN STR 47/48 AND STR 48/49. MAINTENANCE FOUND CRACK OUT OF LIMITS AND REPAIRED IAW SRM 53-10-01, 53-10-04, FIGURE 3.

Part: SKIN — CORRODED (WS 780)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND RT WING LOWER SKIN CORRODED. REMOVED CORRODED PAD-UP AT LES STA 780. MAINTENANCE REPAIRED IAW UPS E.O. 747-57-0291.

Part: FRAME — CRACKED (BS 1900)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN UPPER FLANGE OF FRAME AT BS 1900 S42 LT NEAR SIDE GUIDE. MAINTENANCE REPAIRED IAW SRM 51-40-03.

Part: FRAME — CRACKED (BS 2000)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND FRAME AND REINFORCEMENT ANGLE CRACKED ON BS 2000 LBL 54 UNDER FLOOR STRUCTURE. MAINTENANCE REPAIRED CRACK IAW SRM 51-40-03.

Part: FRAME — CRACKED (BS 2060)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN FRAME JUST UNDER FLOOR STRUCTURE, BS 2060 LBL 54. MAINTENANCE REPAIRED IAW SRM 51-40-03.

Part: FITTING — CORRODED (BS 2360)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND STRINGER END FITTING OF STR S1 STA 236O IS CORRODED. MAINTENANCE REMOVED CORROSION, OUT OF LIMITS, REPLACED FITTING IAW SRM 51-30-05/02.

Part: STRINGER — CRACKED (BS 2000)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN THRESHOLD STRINGER IN BULK CARGO COMPARTMENT, AT BS 2000 RBL 52. MAINTENANCE FOUND THE DAMAGE TO BE OUT OF LIMITS, REMOVED CRACKED SECTION OF STRINGER AND REPAIRED IAW SRM 51-40-03.

Part: FRAME — CRACKED (BS 1780)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND FRAME WEB DEFORMED AND STIFFENERS CRACKED ON BS 1780 UPPER SIDE, AFT CARGO COMPARTMENT BETWEEN LBL 30 AND RBL 30. MAINTENANCE REMOVED DAMAGED SECTION AND STIFFENERS, FOUND TO BE OUT OF LIMITS AND REPAIRED IAW SRM 51-40-02 AND 51-30-02.

Part: CHANNEL — CRACKED (BS 140)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CHANNEL W/200 RT SIDE OF CENTER VERTICAL BEAM CRACKED AT LOWER POSITION. MAINTENANCE PRESSURE BULKHEAD CHANNEL BELOW W/200 RT SIDE OF CENTER VERTICAL BEAM. CRACK OUT OF LIMITS IAW SRM 53-10-01, REPAIRED IAW SRM 51-40-03.

Part: INTERCOSTAL — CORRODED (BS 1420)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACKS IN THE REINFORCING ANGLE AT BS 9360 BETWEEN STR 59 TO STR 8. MAINTENANCE REPAIRED ANGLE IAW SRM 51-40-03.

Part: SHEAR TIE — CRACKED (BS 1880)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND SHEAR TIE ON FRAME CRACKED AT BS 1880 RT, BETWEEN STRINGER 48 TO 49. MAINTENANCE REPAIRED IAW SRM 53-10-04 FIGURE 3.

Part: FRAME — CRACKED (BS 1960)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN REINFORCEMENT ANGLE UNDER FRAME UPPER FLANGE, BS 1960 LBL 55. THE CRACK WAS FOUND OUT OF LIMITS. MAINTENANCE REPAIRED IAW SRM 51-40-03.

Part: SHEAR TIE — CRACKED (BS 1820)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN SHEAR TIE AT BS 1820 LT, STR 45 AND 46. MAINTENANCE REPAIRED IAW SRM 53-10-04 FIGURE 3.

Part: TAIL SKID — DAMAGED (STA 2580)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND PERMANENT REPAIR OF TAIL SKID DAMAGED AT STA 2580 STRINGER 47R. MAINTENANCE MADE A PERMANENT REPAIR IAW SRM 53-30-03.

Part: SKIN — DENTED (BS 2520)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND DENT AT LAP SPLICE ON LT LOWER SIDE STA 2520. MAINTENANCE REPAIRED IAW SRM 53-30-03.

Part: FRAME — CRACKED (BS 2080)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN UPPER FLANGE OF FRAME, BS 2080 LBL 53. MAINTENANCE REPAIRED IAW SRM 51-40-03.

Part: SKIN — CRACKED (WS 499)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK AT UPPER SKIN OF D-BEAM. MAINTENANCE REPAIRED SKIN AT WS 499 IAW SRM 57-30-04 FIGURE 2.

Part: BULKHEAD — CRACKED (BS 2160)

WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND SMALL CRACKS ON BS 2160 BULKHEAD AT RBL 53, 10 INCHES ABOVE CARGO FLOOR AND RBL 37, 5 INCHES ABOVE CARGO FLOOR. MAINTENANCE REPAIRED IAW SRM 51-40-02.

Part: LATCH ASSY — LOOSE (FLIGHT DECK)

PILOT REPORTED OVERHEAD HATCH HANDLE POPS OUT IN FLIGHT. TIGHTENED LATCH ASSY, PRESSURIZED A/C AND FOUND NO DEFFECTS AT THIS TIME. OK FOR SERVICE.