N522UP

Part: BATTERY PACK — LOOSE (CABIN)

INSPECTION TYPE:N/A EMERGENCY -EXIT- SIGN AT CREW SERVICE DOOR INOP. FOUND BATTERY PACK LOOSE. SECURED, OPERATIONAL NORMAL PER AMM 33-51-02.

Part: SUPPORT — CRACKED (BS 930-940) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D BS 930-940 LBL30 TENSION TIE SUPPORT FOUND CRACK, CRACK LENGTH 3/8". M/D BS 920-940 LBL30 TENSION TIE SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SUPPORT — CRACKED (BS 920-940) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D BS920-940 RBL30 TENSION TIE SUPPORT FOUND CRACK, CRACK LENGTH 5/16". M/D BS 920-940 RBL30 TENSION TIE SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FLOORBEAM — CORRODED (BS 1920) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C AFT CARGO COMPT CARGO FLOORBEAM UPPER TEE FOUND CORROSION AT STA 1920 CARGO NET ATT HOOK RBL4 TO LBL4. CORROSION BLEND OUT 0.045" BY 1.5" BY 2". AFT CARGO COMPT BS 1920 LBL 42 TO RBL 42 FLOORBEAM UPPER CHORD REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SILL — CRACKED (BS 434-440) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D L1 DOOR SILL FOUND CRACK, CRACK LENGTH 1" APPROX. M/D L1 DOOR SILL AT BS 434 TO BS 440 WEB REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: SILL — CRACKED (BS 434-440) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D RT BS434 TO BS 440 FLOOR SILL WEB CORROSION CRACK REVEALED, CRACK LENGTH 1" APPROX. M/D BS 434 TO BS 440 DOOR 1R SILL WEB REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: FRAME — CRACKED (BS 2231 S23-26R) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D AFTER FURTHER FASTENER REMOVED, RT BS 2231 FRAME INNER CHORD AREA S23R-26R FOUND TOTAL 4 HOLES CRACK AT DIFFERENT STACK UP STRUCTURES (FRAME STRAP, INNER CHORD) (CRACK LENGTH 0.040",1/16", THROUGH THICKNESS). M/DECK BS 2231 FRAME ATTACH INNER CHORD AND STRAP AT BETWEEN STR 22R TO STR 26R AREA REPAIRED AS PER SRM 53-10-04 FIG 115, CONTINUE INSP ARE REQUIRED AS PER SRM 53-10-04 FIG 115 (UPS MPI NR P19305 RAISED FOR CONTINUE INSP.)

Part: SHEAR TIE — CORRODED (BS 2200 S42-34L) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C AFT OF BULK CARGO COMPT SKIN ATT ANGLE FOUND BULGE AT STA 2200 BTN S42L AND S37L. CORROSION BLEND OUT EXFOLIATION THROUGH WHOLE THICKNESS. AFT OF BULK CARGO COMPT BS 2200 STR 37L TO STR 42L FRAME ATTACH SUPPORT ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: DOOR FRAME — CRACKED (BS 2231 S23-26L) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D AFTER FURTHER FASTENER REMOVED INNER CHORD AREA S23L - 26L FOUND TOTAL HOLES CRACK AT DIFFERENT STACK UP STRUCTURES (FRAME,STRAP, INNER CHORD OR REVEAL) (CRACK LENGTH 0.050" & THROUGH THICKNESS) M/D BS2231 FRAME ATTACH REVEAL REPAIRED AT BETWEEN STR 21.5L TO STR 25L AREA AS PER SRM 53-10-04 FIG 34. FRAME ATTACH INNER CHORD & STRAP REPAIRED BETWEEN STR 22L TO STR 26L AREA AS PER SRM 53-10-04 FIG 115. CONTINUE INSP. AREA REQUIRED AS PER SRM 53-10-04 FIG 115.

Part: REVEAL — CRACKED (DOOR FRAME) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D L3 DOOR FWD CUTOUT LWR CORNER REVEAL FTG FOUND CRACK, CRACK LENGTH 3/4" APPROX. M/D L3 DOOR FWD CUTOUT LWR CORNER REVEAL FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: REVEAL — CRACKED (R3 DOORWAY) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D R3 DOOR FWD LOWER CUTOUT CORNER REVEAL FOUND CRACK AS MARKED, CRACK LENGTH 1/2" APPROX. M/D R3 DOOR FWD LOWER CUTOUT CORNER REVEAL FTG REPLACED AN INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FRAME — CRACKED (BS 2231 S23-25R) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D RT BS 2231 FRAME INNER CHORD S23R-25R FOUND 2 HOLES CRACK AT FRAME STRAP, CRACK LENGTH 1/16" AND 0.040". M/D BS 2231 FRAME ATTACH INNER CHORD AND STRAP AT BEN STR 22R TO STR26R AREA REPAIRED AS PER SRM 53-10-04 FIG 115. CONTINUE INSP REQUIRED AS PER SRM 53-10-04 FIG 115. REFER NRC51555 FOR WORKING DETAIL. UPS MPI#P19305 RAISED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C NR 3R MED CUTOUT FWD LOWER CORNER FOUND SKIN AND BEARSTRAP EDGE CRACKED. NR 3R MED CUTOUT FWD LOWER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO B747-5310-24674 APP N.

Part: INTERCOSTAL — CRACKED (BS 340-350) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C LT FUSELAGE SKIN AREA AT BS 340-350 STR 5A 1 FASTENER HOLE FOUND CRACKED AT INTERCOSTAL. (1ST LAYER FROM I/B) RUNNING DOWNWARD APP 0.030" IN LENGTH (REFER SKETCH FOR DETAIL). LT FUSELAGE SKIN BS 340-360 STR 5A ATTACHED INTERCOSTAL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C NR 3L MED CUTOUT AFT UPPER CORNER FOUND SKIN AND BEARSTRAP EDGE FOUND CRACKED, CRACK LENGTH 1/8" APPROX. NR 3L MED CUTOUT AFT UPPER CORNER AND BEARSTRAP REPAIRED AS PER UPS EO B747-5330-24674 APP I AND O.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C NR 3R MED CUTOUT AFT UPPER CORNER FOUND SKIN AND BEARSTRAP EDGE CRACKED, CRACK LENGTH 1/8" TO 2". NR 3R MED CUTOUT AFT UPPER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO B747-5330-24674 APPENDIX P & L.

Part: STRINGER CLIP — CRACKED (AFT CARGO) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C AFT CARGO COMPT S33L STRINGER CLIP FOUND CRACKED AT STA 1760, CRACK LENGTH 5/16". AFT CARGO COMPT BS 1760 STR 33L STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FRAME — CRACKED (BS 2231 S24-25L) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D LT BS2231 FRAME INNER CHORD S24L-25L FOUND 1 HOLE CRACK AT FRAME STRAP RUNNING FWD APPROX 1/8". M/D BS2231 FRAME ATTACH INNER CHORD AND STRAP REPAIRED BTN STR22L TO 26L AREA AS PER SRM 53-10-04 FIG 115. CONTINUE INSPECTION ARE REQ AS PER SRM 53-10-04 FIG 115. REFER NRC51556 FOR WORKING DETAIL. (UPS MPI#P19306 RAISED FOR CONTINUE INSPECTION)

Part: INTERCOSTAL — CRACKED (BS 290) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C NWW TOP PANEL LBL20 INTERCOSTAL FOUND CRACK AT 1 FASTENER LOCATION AT BS290 AS MARKED, CRACK LENGTH 1/2". NWW TOP PANEL AT BS 290 LBL20 INTERCOSTAL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C NR 3L MED CUTOUT FWD LOWER CORNER FOUND SKIN AND BEARSTRAP EDGE CRACKED, CRACK LENGTH 1/16" TO 5/8" RESP. NR 3L MED CUTOUT FWD LOWER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO B747-5330-24674 APP M.

Part: STRINGER — DEFORMED (BS 485) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C FWD CARGO COMPT S38L STRINGER FOUND DEFORM AT STA 485, FWD CARGO COMPT BS 484 TO BS 496 STR38L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 3.

Part: PANEL SUPPORT — CRACKED (BS 1540) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C AFT CARGO COMPT SLOPE PANEL LT SIDE UPPER SUPPORT FOUND CRACKED AT STA 1540, CRACK LENGTH 1/2". AFT CARGO COMPT BS 1530 TO BS 1550 LT SIDE SLOPE PANEL UPPER SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: SUPPORT ANGLE — CRACKED (BS 1000) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C FWD CARGO COMPT STA 1000 BULKHEAD 1 SUPPORT ANGLE FOUND CRACKED AT LBL 100 WL 155, CRACK LENGTH 1/2". FWD CARGO COMPT BS 1000 BULKHEAD AT LBL 100 WL 155 SUPPORT ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: STIFFENER — CORRODED (BS 1241) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C RT W/G W/W STIFFENER CORROSION AT STA 1241 RBL 85, CORROSION BLEND OUT 0.105" BY 2" BY 4" EXCEED SRM 57-10-01 FIG 1 LIMITS. RT W/G W/W AT BS 1241 RBL 85" VERT STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: STRINGER CLIP — CRACKED (BS 780) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C FWD CARGO COMPT S33L STRINGER CLIP FOUND CRACKED AT STA780, CRACK LENGTH 1/4". FWD CARGO COMPT BS 780 STR 33L STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 3 AND 51-30-02.

Part: CREASE BEAM — CRACKED (BS 960-980) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C RT FX CROWN BS 960-980 UPPER CREASE BEAM FWD FRAME ATTACH ANGLE RADIUS FOUND CRACK APPROX 1/2" LONG. FX CROWN BS 960-980 RT UPPER CREASE BEAM FWD FRAME ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SHEAR TIE — CORRODED (RT WING) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C RT W/G REAR SPAR WS 375 UPPER FIXED PANEL SUPPORT APPEARED CORRODED. CORROSION BLEND OUT EXFOLIATION THROUGH WHOLE THICKNESS 2" BY 3/4" EXCEED SRM LIMIT. RT W/G REAR SPAR WS375 UPPER FIXED PANEL SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.

Part: SUPPORT — CORRODED (RT WING) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C RT WING WS500 L/E MOST FWD INTERIOR LOWER SUPPORT CHORD BULGED AS MARK. CORROSION BLEND OUT EXFOLIATION THROUGH WHOLE THICKNESS EXCEED SRM LIMIT. RHW WS 492 TO WS 508 L/E MOST FWD INTERIOR LOWER SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: STRINGER CLIP — CRACKED (BS 1680 S33L) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C AFT CARGO COMPT S33L STRINGER CLIP FOUND CRACKED AT STA1680, CRACK LENGTH 3/8". AFT CARGO COMPT BS 1680 STR33L STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: CREASE BEAM — CRACKED (BS 960-980) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C RT FX CROWN BS960-980 LOWER CREASE BEAM FWD FLANGE FOUND CRACK APPROX 1/2" LONG. FX CROWN BS 960-980 RT LOWER CREASE BEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: DOOR FRAME — CHAFED (APU DOOR) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C APU COMPT AFT DOOR CUTOUT SUPPORT FRAME LWR FLANGE LWR SURFACE FOUND CHAFED MARKED. APU COMPT AFT DOOR CUTOUT SUPPORT FRAME LWR FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: STIFFENER — CORRODED (RT MLG WW) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C RT W/G W/W STIFFENER APPEAR CORRODED AT STA1241 RBL 63. RT W/G W/W AT BS 1241 RBL63 VERTICAL STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-10 PG 9 AN 51-30-02.

Part: CREASE BEAM — CRACKED (BS 940-960) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C FX CROWN BS 940-960 LOWER CREASE BEAM FWD FLANGE RADIUS FOUND CRACK APPROX 3/8" LONG. FX CROWN BS 940-960 LOWER CREASE BEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SKIN — CHIPPED (THRUST REVERSER) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C NR 3 ENGINE AFT EXHAUST SLEEVE EXTERNAL SKIN FWD EDGE CHIPPED AT 5 O`CLOCK POSITION. CRACK LENGTH .1875 INCH. NR 3 ENGINE AFT EXHAUST SLEEVE EXTERNAL SKIN FWD EDGE AT 5 O`CLOCK POS REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD UPPER CORNER SKIN REPAIRED AS PER HX RS NR R53-61-35822, CRACK LENGTH 0.030" AND 0.090"). AFT CARGO DOOR CUTOUT FWD UPPER CORNER SKIN REPAIRED AS PER HX RS NR R53-61-35822. CONTINUE INSPECTION ARE REQUIRED AS PER HX RS NR R53-61-35822 AND UPS EO NR B747-5330-27287.

Part: CREASE BEAM — CRACKED (BS 980-1000) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C RT FX CROWN BS980-1000 UPPER CREASE BEAM FWD RADIUS FOUND CRACK APPROX 1" LONG. FX CROWN BS 980-1000 RT UPPER CREASE BEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: CREASE BEAM — CRACKED (BS 960-980) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C LT FX CROWN BS 960-980 UPPER CREASE BEAM FWD FRAME ATTACH ANGLE RADIUS FOUND CRACK APPROX 1/2" LONG. FX CROWN BS960-980 LT UPPER CREASE BEAM FWD FRAME ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FLOORBEAM — CRACKED (BS 2300) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D BS 2300 LBL50 FLOORBEAMS WEB REAR SIDE STIFFENER FOUND CRACKED AS MARKED, CRACK LENGTH 3/8". M/D BS 2300 LBL50 FLOORBEAM WEB REAR SIDE STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FLOOR SUPPORT — CORRODED (BS 2300-2320) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D STA2300-2320 LBL34 FLOOR SUPPORT FOUND SEVERAL CORROSION. CORROSION BLEND OUT 0.023" BY 1" BY 4" EXCEED SRM LIMIT. M/D BS 2300-2320 LBL34 FLOOR SUPPORT REPLACED AND INSTALED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: STRINGER — CRACKED (BS 550 S30L) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C FWD CARGO COMPT S30L STRINGER FOUND DAMAGED AT STA 550, CRACK LENGTH 7/16". FWD CARGO COMPT BS 550 STR 30L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-10-03 FIG 2 SHEET 4 TABLE 3. UPS MPI NR P109303 RAISED.

Part: FLOORBEAM — CORRODED (BS 2340) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D BS2340 LBL40-59 FLOORBEAM UPPER CHORD FOUND SEVERAL AREAS OF CORROSION. CORROSION BLEND OUT 0.040" BY 1" BY 3" EXCEED SRM LIMIT. M/D BS 2340 LBL 25 TO LT MOST O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: STRINGER SPLICE — CRACKED (BS 738 S31R) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C FWD CARGO COMPT S31R STRINGER SPLICE FOUND CRACKED AT STA738. CRACK LENGTH 1/4". FWD CARGO COMPT BS 738 STR 31R STRINGER SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG9 AND 51-30-02.

Part: FLOORBEAM — CORRODED (BS 2360) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D BS 2360 LBL 55 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.047" BY 1" BY 2" EXCEED SRM LIMIT. M/D BS 2360 LBL25 TO LT MOST O/B AREA FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SKIN — DENTED (TAILCONE) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C EMP RIGHT TAIL CONE SKIN SURFACE FOUND A DENT MARK AT STA 2755 BETWEEN 17R & 18R. EMP RIGHT TAIL CONE SKIN BS 2750 TO 2762 STR 17R - 18R AREA REPAIRED AS PER SRM 53-30-03 FIG 1A.

Part: PANEL — BULGED (LT WING) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C LWS 888 L/E LOWER FIXED PANEL FWD BULGED AS MARKED. CORROSION BLEND OUT 0.040" BY 1" BY 2". LHW L/E WS888 LOWER FIXED PANEL FWD SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SUPPORT — CRACKED (BS 1920) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C AFT CARGO COMPT DIVIDER SUPPORT HOOK AREA FOUND CRACKED AT STA 1920 LBL 4 TO RBL 4 FLOOR AREA, CRACK LENGTH 2". AFT CARGO COMPT DIVIDER SUPPORT AT BS 1920 LBL 42 TO RBL 42 REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: SKIN — CRACKED (BS 340-350 S5-5A) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C U/D FX SKIN AT BS340-350 S5-5A FOUND CRACKS AT 3 FASTENER HOLES, CRACK LENGTH 1/16, 1/2 AND 9/16". FX BS 340 TO 350 STR5L SKIN REPAIRED WITHOUT ZERO TIMING AT CRITICAL ROW FASTENERS AS PER SRM 53-30-03 FIG 1 AND TAR S/N 127807 REV A REPEAT INSP IS REQUIRED AS PER SRM 53-30-03 FIG 1. UPS MPI#P19298 RAISED FOR CONTINUE REPEAT INSPECTION.

Part: SKIN — DENTED (BS 2725) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C EMP LT TAIL CONE SKIN FOUND DENT MARK AT STA 2725 BTN S0L AND S1L. EMP LT TAIL CONE SKIN AT BS2725 BTN STR 0 AND STR 1L SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A.

Part: FLOORBEAM — CRACKED (BS 2280) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D STA2280 LBL39 FLOORBEAMS WEB REAR SIDE FOUND SEVERAL CRACKS, CRACK LENGTH 1/4". M/D BS 2280 LBL 39 FLOORBEAM WEB REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: SKIN — CRACKED (BS 340 S5-5AR) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C U/D FX SKIN AT BS 340 S5-5A FOUND CRACK AT 1 FASTENER HOLE CRACK LENGTH 1/16". FX BS 340 BETWEEN STR 5R TO 5 AR SKIN REPAIRED WITHOUT ZERO TIMING AT CRITICAL ROW FASTENERS AS PER SRM 53-30-03 FIG 1 AND TAR S/N 127808 REV A REPEAT INSP IS REQUIRED AS PER SRM 53-30-03 FIG 1. UPS MPI NR P19299 RAISED FOR CONTINUE REPEAT INSP AND MPI NR P19300 RAISED FOR PERM REPAIR.

Part: FRAME — CRACKED (BS 940) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C LT BS 940 TENSION TIE NR 1 FASTENER HOLE FOUND CRACK AT WEB DOUBLER RUNNING 5 O/C POSITION APPROX 1/16" IN LENGTH. M/D BS 940 LT SIDE FRAME DOUBLER THROUGH FRAME TENSION TIE, STEEL PLATE AND FAIL/SAFE CHORD HOLE OVERSIZED AND FASTENER INSTALLED AS PER UPS EO B747-5310-23715 APP D AND C.

Part: FRAME — CRACKED (BS 940) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C LT BS 940 TENSION TIE NR 1 FASTENER HOLE FOUND CRACK AT FRAME RUNNING 7 O/C POSITION APPROX 0.040" IN LENGTH (LOOKING AFT). M/D BS 940 LT SIDE FRAME THROUGH FRAME DOUBLER, TENSION TIE, STEEL PLATE AND FAIL/SAFE CHORD HOLE OVERSIZED AND FASTENER INSTALLED AS PER UPS EO B747-5310-23715 APP D AND C.

Part: CHANNEL — CRACKED (BS 940) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C RT BS940 TENSION TIE TO FRAME CONNECTION AREA FOUND 2 FASTENER HOLES CRACKED AND 3 FASTENER HOLES OVAL AT AFT CHANNEL. M/D BS 940 RT TENSION TIE AFT CHANNEL LT TO RT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 AND EO B747-5310-23715-C.

Part: PLATE — MISINSTALLED (BS 940) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/ BS940 LT TENSION TIE FWD ATT STEEL PLATE UPPER ROW MOST I/B FASTENER HOLE FOUND SHORT EDGE MARGIN. M/D BS 940 LT TENSION TIE FWD ATTACH STEEL PLATE REPLACED AND INSTALLED AS PER RS R53-25-35824 AND EO B747-5310-23715-C. CONTINUED INSPECTIONS ARE REQUIRED AS PER RS R53-25-35824 AND UPS EO B747-5310-27295.

Part: CHANNEL — CRACKED (BS 880) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C LT BS 880 TENSION TIE NR 6 HOLE FOUND CRACK AT AFT CHANNEL APPROX 0.040" RUNNING UP. M/D BS 880 TENSION TIE AFT CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER UPS EO B747-5310-23715-C AND SRM 51-30-02 REFER NRC 50076 FOR WORKING DETAIL.

Part: CHANNEL — CRACKED (BS 820) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C LT BS 820 TENSION TIE NR 4 FASTENER HOLE FOUND CRACK AT FWD CHANNEL APPROX 1/16" IN LENGTH RUNNING UP. M/D BS 820 TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35817 AND UPS EO B747-5310-27264-A. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35817 AND UPS EO B747-5310-27264.

Part: PLATE — MISINSTALLED (BS 820) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D BS 820 RT TENSION TIE FWD ATT STEEL PLATE LOWER ROW MOST O/B FASTENER HOLE FOUND SHORT EDGE MARGIN. M/D BS820 RT TENSION TIE FWD ATTACH STEEL PLATE REPAIRED AS PER RS R53-25-35817 AND UPS EO B747-5310-27264. CONTINUED INSPECTION IS REQUIRED AS PER RS R53-25-35817 AND UPS EO B747-5310-27264.

Part: FRAME — CRACKED (BS 820) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C RT BS 820 TENSION TIE TO FRAME CONNECTION AREA FOUND HOLE NR 4 CRACK AT FRAME WEB DOUBLER APPROX 0.040". M/ BS 820 RT TENSION TIE TO FRAME WEB ATTACH DOUBLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND EO B747-5310-23715-C AND SRM 51-30-02.

Part: PLATE — MISINSTALLED (BS 900) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D BS 900 RT TENSION TIE FWD ATT STEEL PLATE UPPER ROW NR 5 FASTENER HOLE (COUNT FROM I/B) FOUND SHORT EDGE MARGIN. M/DECK BS 900 RT TENSION TIE FWD ATTACH STEEL PLATE REPAIRED AS PER HX RS NR R53-25-35819 CONTINUE INSPECTION IS REQUIRED AS PER UPS EO NR B747-5310-27294.

Part: PLATE — MISINSTALLED (BS 940) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE: C M/D BS 940 RT TENSION TIE FWD ATT STEEL PLATE UPPER ROW MOST IB FASTENER HOLE FOUND SHORT EDGE MARGIN. M/DECK BS 940 RT TENSION TIE FWD ATTACH STEEL PLATE REPLACED AND INSTALLED IAW HX RS NR R53-25-35824 AND UPS EO NR B747-5310-23715-C CONTINUE INSPECTION ARE REQUIRED IAW RS NR R53-25-35824 AND UPS EO NR B747-5310-27295.

Part: PLATE — MISINSTALLED (BS 900) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D BS 900 LT TENSION TIE FWD ATT STEEL PLATE UPPER ROW MOST O/B FASTENER HOLE FOUND SHORT EDGE MARGIN. M/DECK BS 900 LT TENSION TIE FWD ATTACH STEEL PLATE REPAIRED AS PER HX RS NR R53-25-35819 AND CONTINUE INSPECTION IS REQUIRED AS PER UPS EO NR B747-5310-27294.

Part: CHANNEL — CRACKED (BS 860) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C RT BS 860 TENSION TIE TO FRAME CONNECTION AREA FOUND HOLE NR 5 CRACK AT FWD CHANNEL APPROX 0.030". M/D BS 860 RT TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35820 AND UPS EO B747-5310-27253. CONTINUED INSPECTIONS ARE REQUIRED AS PER RS R53-25-35820 AND UPS EO B747-5310-27253.

Part: KEELBEAM — CORRODED (BS 1460) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C FX KEEL BEAM BOX LOWER EXTERNAL PANEL SUPPORT ATT SHIM FOUND CORROSION AT STA 1460 LBL4 TO LBL5 AND RBL4 TO RBL5 UPPER SURFACE TO STIFFENER AREA AS MARKED. CORROSION BLEND OUT 0.065" BY 3/4" BY 1 1/4" EXCEED SRM LIMIT. FX KEEL BEAM BOX LOWER EXTERNAL PANEL SUPPORT ATT SHIM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: CHANNEL — CRACKED (BS 940) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C RT BS 940 TENSION TIE TO FRAME CONNECTION AREA FOUND 1 FASTENER HOLE CRACKED AND 3 FASTENER HOLES OVAL AT FWD CHANNEL, CRACK LENGTH 0.090" APPROX. M/D BS 940 RT TENSION TIE FWD CHANNEL LT TO RT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 AND EO B747-5310-23715-C.

Part: KEELBEAM — CORRODED (BS 1445-1448) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C FX KEEL BEAM RT LOWER CHORD UPPER SURFACE FOUND CORROSION AT STA 1445-1448 RBL8. CORROSION BLEND OUT 0.091" BY 2" BY 3" EXCEED SRM LIMIT. FX KEEL BEAM RT LOWER CHORD BS 1445-1448 RBL8 LWR FLANGE UPPER SURFACE CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND 51-10-02 AN RS R53-49-35827 AND UPS ENGINEERING FILE NR 747-53-20424.

Part: CHANNEL — CRACKED (BS 880 S9R) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C CRACK FOUND AT BS 880 RT SIDE S9R TENSION TIE ATTACHED AFT CHANNEL CRACK LOCATED AT NR 6 FASTENER HOLE 0.040" APPROX RUNNING UPWARD DIRECTION. M/D BS 880 TENSION TIE AFT CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER UPS EO B747-5310-2371-C AND SRM 51-30-02.

Part: FRAME — CRACKED (BS 840) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C CRACK FOUND AT BS 840 RT SIDE S10R TENSION TIE ATTACHED FRAME DOUBLER CRACK LOCATED AT NO.4 FASTENER HOLE THROUGH THICKNESS RUNNING O/B DIRECTION, CRACK LENGTH 0.060" APPROX. M/D BS 840 RT SIDE FRAME DOUBLER THROUGH FRAME TENSION TIE AND STEEL PLATE HOLE OVERSIZED AT FASTENER INSTALLED AS PER UPS EO B747-5310-23715 APP D AND C.

Part: CHANNEL — CRACKED (BS 880 S9R) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C CRACK FOUND AT BS 880 RT SIDE S9R TENSION TIE ATTACHED FWD CHANNEL CRACK LOCATED AT NR 14 FASTENER HOLE 0.030" APPROX RUNNING DOWNWARD DIRECTION. M/D BS 880 TENSION TIE FWD CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER UPS EO B747-5310-23715-C AND SRM 51-30-02.

Part: FRAME — CRACKED (BS 840 S10R) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C CRACK FOUND AT BS 840 RT SIDE S10R TENSION TIE ATTACHED FRAME CRACK LOCATED AT NR 4 FASTENER HOLE 0.030" APPROX RUNNING O/B DIRECTION. M/D BS 840 BETWEEN STR 8R TO STR 12R FRAME REPAIRED AS PER RS R53-25-35818 AND UPS EO B747-5310-27272-A. CONTINUED INSPECTIONS ARE REQUIRED AS PER RS R53-25-35818 AND UPS EO B747-5310-27272.

Part: CHANNEL — CRACKED (BS 880 S9R) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C CRACK FOUND AT BS 880 RT SIDE S9R TENSION TIE ATTACHED FWD CHANNEL CRACK LOCATED AT NR 16 FASTENER HOLE 0.040" APPROX RUNNING UPWARD DIRECTION. M/D BS 880 TENSION TIE FWD CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER UPS EO B747-5310-23715-C AND SRM 51-30-02 REFER NRC 50073 FOR WORKING DETAIL.

Part: STRINGER CLIP — CRACKED (BS 880 S9R) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C CRACK FOUND AT BS 880 RT SIDE S9R TENSION TIE ATTACHED STRINGER CLIP CRACK LOCATED AT NR 10 FASTENER HOLE 0.030" APPROX RUNNING UPWARD DIRECTION. M/D BS 880 RT SIDE STR 9R TENSION TIE ATTACHED STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 AND EO B747-5310-23715-C.

Part: CHANNEL — CRACKED (BS 880 S9R) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C CRACK FOUND AT BS 880 RT SIDE S9R TENSION TIE ATTACH FWD CHANNEL CRACK LOCATED AT NR 9 FASTENER HOLE 0.030" APPROX. RUNNING UPWARD DIRECTION, M/D BS880 TENSION TIE FWD CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER UPS EO B747-5310-23715-C AND SRM 51-30-02 REFER NRC 50073 FOR WORKING DETAIL.

Part: PLATE — MISINSTALLED (BS 920) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D BS 920 RT TENSION TIE FWD ATT STEEL PLATE TOP ROW NR 5 FASTENER HOLE (COUNT FROM I/B) FOUND SHORT EDGE MARGIN. M/D BS 920 RT TENSION TIE FWD ATTACH STEEL PLATE REPAIRED AS PER RS R53-25-35821 AND UPS EO B747-5310-27268. CONTINUED INSPECTION IS REQUIRED AS PER RS R53-25-35821 AND UPS EO B747-5310-27268.

Part: PLATE — MISINSTALLED (BS 920) · airframe 74,820 hrs · 17,560 cycles

INSPECTION TYPE:C M/D BS 920 LT TENSION TIE FWD ATT STEEL PLATE LOWER ROW MOST O/B FASTENER HOLE FOUND SHORT EDGE MARGIN, M/D BS 920 LT TENSION TIE FWD ATTACH STEEL PLATE REPAIRED AS PER RS R53-25-35821 AND UPS EO B747-5310-27268. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35821 AND UPS EO B747-5310-27268.

Part: SKIN — DELAMINATED (NR 5 SPOILER)

INSPECTION TYPE:N/A NR 5 FLT SPOILER HAS UPPER SURFACE SKIN PEELING BACK AND DELAMINATED APPROX 25 PERCENT OF SURFACE AREA. REMOVED AND REPLACED NR 5 FLT SPOILER IAW AMM 27-61-01. OPS CHECKS GOOD.

Part: SKIN — DAMAGED (HORIZONTAL STAB)

HOLE IN FUSELAGE TAIL SECTION LEFT SIDE ABOVE HORIZONTAL STABILIZIER/ ELEVATOR APPROX 5 X 7 INCHES. FABRICATED AND INSTALLED SHEET METAL DOUBLER PER 747 SRM 53-30-03.

Part: WARNING LIGHT — FALSE ACTIVATION (L1 DOOR)

L1 DOOR INDICATION LIGHT CAME ON DURING CLIMB-OUT. LOUD AIR NOISE IN C CARGO AREA. INSPECTED L1 DOOR SEAL. NO DAMAGE. CYCLE L1 DOOR 5 TIMES. NO FAULT FOUND, PRESSURIZING AIRCRAFT TO 2.0, DOOR WARNING LIGHT DID NOT COME ON. OPS CHECK L1 ENTRY DOOR. OK PER MM 52-11-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

UPPER DECK DOOR AISLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AISLE LIGHT AND BATTERY PACK ASSY MM 33-51-02.

Part: LIGHT — ILLUMINATED (L1 DOOR)

INSPECTION TYPE:N/A ATB - FWD L1 DOOR LIGHT ILLUMINATED. DOOR VERY NOISY AND APPEARED TO BE OFF LOCKS. PRESSURE 3.0 ALT 10,000 FT DEPRESSURIZED. RETURNED TO ANC. FOUND AFT SIDE LATCH ROLLER AND CAM UNSECURED. PERFORMED GVI, NO DEFECTS NOTED. PERFORMED OPERATIONAL PROCEDURE 52-11-00 PG 13-18.

Part: CONNECTOR — LOOSE (COCKPIT)

FIRE DETECTION LIGHT ON FWD ANNUNCIATOR PANEL FLICKERED FOR A FEW SECONDS AFTER TAKEOFF. DEFERRED PER MEL 26-15; PERFORMED T/S IAW WDM 26-11-61 AND RESECURED LOOSE CONNECTION ON REAR OF PILOT'S PANEL. FIRE DET LIGHT OPS TEST NOW NORMAL. M332692 CLOSED AND PLACARD REMOVED.

Part: CONTROLLER — SMOKE (CABIN TEMP)

ZONE TEMP CONTROLLER NR 1 SMELLS OF SMOKE. REMOVED AND REPLACED CONTROLLER IAW MM 21 61 01.

Part: CRANK ASSY — BROKEN (L1 DOOR)

CLIMBING THRU 20,000 FT HEARD & FELT THUMP L ENTRY DOOR 1 LIGHT CAME ON. DUMPED FUEL. FOUND L1 DOOR UPPER & LOWER CRANKS BROKEN ON AT SIDE OF DOOR. R/R'D CRANK ASSY, RE-RIGGED PER MM 52-11-01. DOOR OPS NORMAL.

Part: RIB — CRACKED (LT WING) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C LT WING O/B MID FLAP SLIDING TRACK RIB FOUND CRACKED, CRACK LENGTH 1 INCH. LT WING O/B MID FLAP SLIDING TRACK RIB REPLACED AS PER SRM 51-10-01 PG 9.

Part: DOUBLER — CRACKED (BS 480) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C U/D BS 480 BTN S11L & S12L FRAME DOUBLER FOUND CRACKED, CRACK LENGTH .5 INCH. U/D BS 480 BTN S11L - S12L FRAME DOUBLER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C COCKPIT BS 360 STR 10AL FRAME INNER CHORD FOUND CRACKS FROM 1EA FASTENERS HOLE AS MARKED, CRACK LENGTH .125 INCH. COCKPIT BS 360 STR 10-15L FRAME INNER CHORD REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: PANEL — DEBONDED (T/E FLAP) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C RIGHT WING O/B AFT FLAP TOP PNL 688KT AFT EDGE MIDWAY AREA DEBONDED. DEBONDED AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-24 FIG 2.

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C U/D - BS 420-425 STR 10L STRINGER SPLICE FASTENER HOLES FOUND ELONGATED. BS 420-425 STR 10L STRINGER SPLICE REPLACED AS PER SRM 51-10-01 PG 9.

Part: FITTING — WORN (BS 1000) · airframe 72,217 hrs · 16,929 cycles

FOUND FUS BS 1000 S39R END FTG CROSS MOUNT BOLT AREA WORN OUT. BS 1000 STR 39R END FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND EO B747-5310-18579-F FIG 10.

Part: FITTING — WORN (BS 1000) · airframe 72,217 hrs · 16,929 cycles

FOUND BS 1000 S37R END FTG CROSS MOUNT BOLT AREA WORN OUT. BS 970- BS 983 STR 37R REPAIRED AS PER SRM 53-10-03 FIG 1 AND STR 37R END FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & EO NR B747-5310-18579 APPENDIX 'F' FIG 10.

Part: CLIP — CRACKED (BS 480) · airframe 72,217 hrs · 16,929 cycles

BS 480 STR 11L FRAME FWD AND AFT FACE ATT CLIP FASTENER HOLES FOUND ELONGATED. CRACK LENGTH 3/8". FWD AND AFT ATT CLIPS 2 REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C U/D BS 380 FWD FLANGE RBL 51, 52.5, 53.5 AND 55 SHORT EDGE MARGIN FOUND. U/D BS 380 FLOORBEAM UPPER CHORD FWD FLANGE AT RBL 51". REPAIRED AS PER EO B747-5320-12407 FIG 2 PLAN B & RBL 52.5", 53.5" AND 55" AREA. REPAIRED AS PER EO B747-5320-12407 FIG 4 PLAN D AFTER NDT INSPECTED PER NTM PART 6 51-00-00 FIG 4 CRACK FREE.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C FWD CARGO COMPT - REAR STOP FITTING SUPPORT FRAME FOUND CRACKED AT STA 960 TO STA 970 RBL 25 SEAT TRACK ATT SURFACE, CRACK LENGTH 5 INCHES. SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: STRINGER CLIP — CRACKED (BS 500) · airframe 72,217 hrs · 16,929 cycles

BS 500 STR12L FRAME FWD FACE ATT TIE CLIP FOUND CRACK. CRACK LENGTH 1/4". TIE CLIP REPLACED AS PER SRM 51-10-01 PG9 AND INSTALLED AS PER SRM 51-30 -02.

Part: SPLICE — CRACKED (BS 500) · airframe 72,217 hrs · 16,929 cycles

FOUND BS 500 STR12L STRINGER SPLICE FOUND CRACKED. CRACK LENGTH 3/8". STRINGER SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.

Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C U/D BS 380 FWD FLANGE RBL 61, 66 AND 71 SHORT EDGE MARGIN FOUND. U/D BS 380 FLOORBEAM UPPER CHORD FWD FLANGE RBL 56" TO RBL 76" AREA REPAIRED AS PER EO NR B747-5320-12407 FIG 2 PLAN B.

Part: PANEL — DENTED (T/E FLAP) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C RIGHT WING - I/B AFT FLAP UPPER O/B FLAP PANEL 678IT FOUND DENT MARK AT LOWER SURFACE. DENT AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-22 FIG 3.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C BS 980-1000 S38L FOUND CRACK AT STRINGER 3EA FASTENER HOLES APPROX 1/16" LONG. FWD CARGO COMPT BS 970 TO BS 1000 S38L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.

Part: SPAR — CRACKED (RT WING) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C RT WING FRONT SPAR WEB AT FSSI 688 FOUND 2EA FASTENER HOLES CRACKED, CRACK LENGTH .5 INCH & .125 INCH. RT WING FRONT SPAR WEB REPAIRED AS PER RS R57-21-35443 JUST BETWEEN FSSI 670 & FSSI 695 AND UPS EO B747-5720-23833-A.

Part: SUPPORT — CRACKED (RT WING FLAP) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C RT WING - O/B MID FLAP ACCESS PANEL 687NT AFT SUPPORT O/B AREA CRACKED, CRACK LENGTH 12 INCHES. RT WING - O/B MID FLAP ACCESS PANEL 687NT AFT SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 3.

Part: FITTING — CORRODED (BS 983) · airframe 72,217 hrs · 16,929 cycles

FWD CARGO COMPT REF NRC NR 5726 LT BATH FITTING ATT SURFACE FOUND HEAVY CORROSION AT STA 983 STR 38L PRESSURE BULKHEAD (AFTER FTG REMOVED ). CORROSION BLEND OUT 0.100" BY 2" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, BS 1000 STR 38L UPPER BATH TUB FTG REPLACED AS PER SRM 51-10-01 PG 9 & EO NR B747-5310-18579 APPENDIX G FIG 11.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD HINGE MOST FWD LOWER FASTENER HOLE FOUND CRACK AT SKIN RUNNING FWD APPROX 0.030 INCH. AFT CARGO DOOR CUTOUT FWD HINGE MOST FWD LOWER FASTENER HOLE AT SKIN AREA REPAIRED AS PER RS R53-61-35445 CONTINUE OPEN HOLE INSPECTION PER RS R53-61-35445 IS REQUIRE AND REF UPS EO B747-5330-23856-A.

Part: DOUBLER — CRACKED (BS 500) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C COCKPIT - BS 500 STR 11L FRAME DOUBLER FOUND CRACK AT O/B AREA, CRACK LENGTH .5 INCH. COCKPIT BS 500 STR 11L TO STR 16L FRAME DOUBLER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: PLATE — CRACKED (INTERCOSTAL) · airframe 72,217 hrs · 16,929 cycles

E/E COMPT BS 400 BL0 FX INTERCOSTAL SPLICE PLATE FOUND CRACKED. CRACK LENGTH 1.75". SPLICE PLATE REPLACE AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30- 02

Part: ACCESS PANEL — CORRODED (TE FLAP) · airframe 72,217 hrs · 16,929 cycles

L/W O/B AFT FLAP ACCESS PANEL NR 588KT AFT SUPPORT I/B AREA CORROSION CRACK REVEALED. CORROSION BLEND OUT 0.055" BY 1" BY 3" EXCEED SRM 57-50-01 FIG 3. LIMIT AFT SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 4 AND HFEC INSP C/OUT AS PER NTM PART6 51-00-0 FIG 4. RESULT NO CRACK FOUND AT CUT LINE AND FIBERGLASS T/E WEDGE REPAIRED AS PER SRM 51-40-12 PART 4D FIG 11.

Part: ANGLE — CRACKED (E/E BAY) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C E/E COMPT BS 400 LBL 27 NWW REAR PANEL INTERCOSTAL VERTICAL ANGLE FOUND CRACKED, CRACK LENGTH .3125 INCH. VERTICAL ANGLE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: ANGLE — CRACKED (E/E BAY) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C E/E COMPT - BS 400 RBL 27 NWW REAR PANEL INTERCOSTAL VERTICAL ANGLE FOUND CRACKED, CRACK LENGTH .375 INCH. VERTICAL ANGLE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: FLAP TRACK — CHAFED (RT WING) · airframe 72,217 hrs · 16,929 cycles

O/B MID FLAP I/B SLIDE TRACK I/B WEB AFT AREA DEEP CHAFING REVEALED. RHW O/B MID FLAP O/B SLIDE TRACK I/B WEB REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 300-320 WL 170 STIFFENER RADIUS INTERMITTENT CRACK APPROX TOTAL : 6 INCHES LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 300-320 WL 170 AREA.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 280-300 WL 180 STIFFENER RADIUS FOUND CRACK APPROX .375 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 280-300 WL 180 AREA.

Part: TANK — CRACKED (LT WING) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C LT WING SURGE TANK WS 1516 LWR AREA STR 5 & 6 FOUND CRACKED, CRACK LENGTH .4375 INCH AND PIECE BROKEN. LT WING SURGE TANK WS 1516 FULL LENGTH LOWER CHORD REPAIRED AS PER HX RS R57-22-35446 AND UPS ENGINEER FILE 747-57-20088.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - LEFT SIDEWALL PANEL BS 265-280 WL 180 STIFFENER RADIUS FOUND CRACK APPROX .3125 INCH IN LENGTH. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW LEFT SIDEWALL PANEL BS 265-280 WL 180 AREA.

Part: FRAME — CRACKED (BS 500) · airframe 72,217 hrs · 16,929 cycles

BS 500 STR 11L FRAME O/B AREA FOUND CRACK. CRACK LENGTH 3/4". BS 500 BETWEEN STR 8L TO STR 13L FRAME REPAIRED AS PER SRM 51-40-03 FIG2.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 300-320 WL 180 STIFFENER RADIUS FOUND CRACK APPROX .25 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RT SIDEWALL PANEL BS 300-320 WL 180 AREA.

Part: STRUCTURE — CRACKED (BS 1000) · airframe 72,217 hrs · 16,929 cycles

FWD CARGO COMPT BS 1000 B/H CHORD COMMON TO UPPER BATH TUB FTG AFT FASTENER HOLE FOUND CRACK AT CHORD RUNNING FWD APPROX 1/16" LONG. FWD CARGO COMPT BS 1000 BULKHEAD CHORD REPAIR AS PER EO# B747-5310-18579-F AT BETWEEN STR 36 / 37L TO STR 40 / 41L AREA.

Part: FRAME — CRACKED (BS 400) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C U/D BS400 STR10L FRAME O/B AREA FOUND CRACK. CRACK LENGTH 1/2" U/D BS400 STR9L TO STR10AL FRAME REPAIRED AS PER RS R53-10-35442 CONTINUED INSPECTIONS REQUIRE WHILE PERFORMING SB 747-53A2265 INSPECTIONS & REPLACEMENT WITH SB747-53-2272 AT OR BEFORE 20000 FLIGHT CYCLES REF UPS EO B747-5310-23830-A.

Part: FRAME — CRACKED (BS 420) · airframe 72,217 hrs · 16,929 cycles

BS 420 STR 10L FRAME O/B AREA FOUND CRACK, CRACK LENGTH 1/2". BS420 STR9/10 TO STR 11 FRAME REPAIRED AS PER RS R53-10-35441 CONTINUED INSPECTION REQUIRE WHILE PERFORMING SB 747-53A2265 INSPECTIONS AND REPLACEMENT WITH SB747-53-2272 MOD AT OR BEFORE 20000 FLIGHT CYCLES REF UPS EO B747-5310-23839-A.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - RT SIDEWALL PANEL BS 280-300 WL 150 STIFFENER RADIUS FOUND CRACK APPROX .25 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 280-300 WL 150 AREA.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 320-340 WL 130 STIFFENER 1EA FASTENER ADJ AREA FOUND CRACK, CRACK LENGTH .25 INCH. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 320-340 WL 130 AREA.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 300-320 WL 160 STIFFENER RADIUS FOUND 2EA CRACKS APPROX .25 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 300-320 WL 160 AREA.

Part: PANEL — DEBONDED (T/E FLAP) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C RIGHT WING - I/B AFT FLAP I/B LWR FIXED PANEL FOUND DEBOND AT PANEL I/B PORTION (AFTER PANEL REMOVAL). DEBONDED AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-24 FIG 2.

Part: STRUCTURE — CRACKED (BS 1000) · airframe 72,217 hrs · 16,929 cycles

FWD CARGO COMPT BS 1000 B/H CHORD FOUND CRACK ALONG RADIUS JUST EXTEND BEYOND LOWER BATH TUB FTG APPROX 1/4" (CRACK LENGTH 1/4") FWD CARGO COMPT BS 1000 BULKHEAD CHORD REPAIRED AS PER EO# B747-5310-18579-F AT BETWEEN STR 36/37R TO STR 40/41R AREA.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 280-300 WL 170 STIFFENER RADIUS FOUND CRACKS APPROX 2 INCHES LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 280-300 WL 170 AREA.

Part: FRAME — CRACKED (BS 480) · airframe 72,217 hrs · 16,929 cycles

BS480 STR 11L FOUND O/B AREA FOUND CRACK. CRACK LENGTH 7/8" TO 1". BS 480 S10L AND ABOVE U/B FLOORBEAM AREA FRAME REPAIRED AS PER RS R53-10-35447 CONTINUED INSPECTION REQUIRE WHILE PERFORMING SB747-53A2265 INSPECTIONS AND REPLACEMENT WITH SB747-53-2272 MOD REF UPS RO B747-23852-A.

Part: FRAME — CRACKED (BS 360) · airframe 72,217 hrs · 16,929 cycles

COCKPIT BS 360 STR 10L TO STR 10AL FRAME O/B AREA FOUND CRACK, CRACK LENGTH 1" & 0.125". COCKPIT BS360 STR9L TO STR10AL FRAME REPAIRED AS PER RS R53-12-35434 CONTINUED INSPECTIONS REQUIRE WHILE PERFORMING SB 747-53A2265 INSPECTIONS AND REPLACEMENT WITH SB747-53-2272 MOD AT OR BEFORE 20000 FLIGHT CYCLES REF UPS EO B747-5310-23812-A.

Part: CLIP — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C U/D BS 440 STR 10R FRAME FWD & AFT ATT -L- CLIPS FOUND CRACK (TOTAL 2EA), CRACK LENGTH .375 INCH. TIE CLIPS TOTAL 2EA REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 280-300 WL 160 STIFFENER RADIUS FOUND 2EA CRACKS APPROX .375 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 280-300 WL 160 AREA.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - LT SIDEWALL PANEL BS 320-340 WL 130 STIFFENER RADIUS FOUND CRACK APPROX .375 INCH IN LENGTH. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW LEFT SIDEWALL PANEL BS 320-340 WL 130 AREA.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 300-320 WL 150 STIFFENER RADIUS FOUND INTERMITTENT CRACK APPROX 7 INCHES. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 300-320 WL 150 AREA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C FX- BS 420 STR 27AR FX STRINGER SPLICE FOUND CRACKED, CRACK LENGTH 3/4". FX- BS 420 STR 27AR FX STRINGER SPLICE REPLACED AS PER SRM 51-10-01 PG 9.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 265-280 WL 180 STIFFENER RADIUS FOUND CRACK APPROX .25 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT BS 265-280 WL 180 AREA OF NWW RIGHT SIDEWALL PANEL.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - LT SIDEWALL PANEL BS 300-320 WL 180 STIFFENER RADIUS FOUND CRACK APPROX .5 INCH IN LENGTH. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW LT SIDEWALL PANEL BS 300-320 WL 180 AREA.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW - LEFT SIDEWALL PANEL BS 320-4 WL 150 STIFFENER RADIUS FOUND CRACK APPROX .125 INCH IN LENGTH. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW LEFT SIDEWALL PANEL BS 320-340 WL 150 AREA.

Part: FRAME — CRACKED (BS 380) · airframe 72,217 hrs · 16,929 cycles

COCKPIT BS 380 STR10L, 10AL AND 11L FRAME O/B AREA FOUND CRACK. COCKPIT BS 380 STR 0 TO STR 13AL FRAME REPLACED AND INSTALLED AS PER RS R53-12-35444 CONTINUED SB747-53A2265 INSPECTIONS REQUIRE AND WHEN SB 747-53-2272 MOD IS DONE AT THIS FRAME LOCATION, THE REPAIR 141U1009-32 FRAME WEB IS TO BE REPLACED REF UPS EO B747-5310-23680-A

Part: STIFFENER — CRACKED (NOSE W/W) · airframe 72,217 hrs · 16,929 cycles

NOSE W/W TOP PANEL BS 265-280 LBL 20 STIFFENER RADIUS FOUND CRACK APPROX 3/4" LONG. NOSE W/W TOP PANEL BS 265-280 LBL 20" STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: STIFFENER — CRACKED (NLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NWW TOP PANEL BS 260-280 LBL 10 STIFFENER RADIUS FOUND CRACK APPROX .25 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT BS 265-280 LBL 10" AREA OF NWW TOP PANEL.

Part: FRAME — CRACKED (BS 480) · airframe 72,217 hrs · 16,929 cycles

BS480 STR11-12R FRAME O/B AREA FOUND CRACKED. CRACK LENGTH 5/8" TO 1". BS480 BETWEEN STR 10R AND ABOVE U/D FLOORBEAM AREA FRAME REPAIRED AS PER RS R53-10-35447. CONTINUED INSPECTION REQUIRE WHILE PERFORMING SB747-53A2265 INSPECTIONS AND REPLACEMENT WITH SB747-53-2272 MOD REF EO B747-5310-23852-A FOR CONTINUED INSPECTION.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C M/D RIGHT NR 5 DOOR LWR HINGE AREA UPPER BEARING ATT AREA FOUND CORROSION. EXFOLIATION CORROSION 2 X 3 INCH. M/D RIGHT NR 5 DOOR LWR HINGE UPPER WEB REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: STRINGER — CRACKED (BS 400-426) · airframe 72,217 hrs · 16,929 cycles

BS 420 STR 34R STRINGER FOUND CRACKED, CRACK LENGTH 3/4". BS 400-426 STR -34R, REPAIRED AS PER SRM 53-10-03 FIG 3.

Part: STRINGER CLIP — CRACKED (BS 440 S36R) · airframe 72,217 hrs · 16,929 cycles

BS 440 STR 36R STRINGER FOUND CRACKED AT STR TIE CLIP, CRACK LENGTH 5/8". BS 434 TO BS 453 STR 36R REPAIRED AS PER SRM 53-10-03 FIG 3.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C M/D RIGHT NR 5 DOOR LWR HINGE LWR SUPPORT WEB FOUND CORROSION CRACK, CRACK LENGTH .75 INCH. M/D RIGHT NR 5 DOOR LWR HINGE LWR SUPPORT WEB REPLACED AS PER SRM 51-10-01 PG 9.

Part: FRAME — CRACKED (BS 360) · airframe 72,217 hrs · 16,929 cycles

COCKPIT BS 360 STR8-9R FRAME O/B FLANGE FOUND CRACK, CRACK LENGTH 0.19" TO 1 1/4". COCKPIT BS 360 STR8-9R FRAME O/B FLANGE REPAIRED AS PER RS R53-12-35433 CONTINUED INSPECTIONS REQUIRE WHILE PERFORMED SB 747-53A2265 INSPECTIONS AND REPLACEMENT WITH SB747-2272 MOD AT OR BEFORE 20000 FLIGHT CYCLES.

Part: WEB — CRACKED (CARGO DOOR) · airframe 72,217 hrs · 16,929 cycles

RT NR 5 DOOR LWR WEB FOUND CRACK. CRACK LENGTH 2". LWR WEB REPLACED AS PER SRM 51-10-01 P9.

Part: GATE — CORRODED (SERVICE DOOR) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C M/D - RIGHT NR 5 DOOR LWR GATE FACE AND PUSH ROD ATT BRACKET FOUND CORROSION. CORROSION BLEND OUT 0.095 X 2 X 2 INCH. LWR GATE REPLACED & DOOR RIGGING CHECK PERFORMED AS PER MM 52-11-09.

Part: FRAME — CRACKED (BS 440) · airframe 72,217 hrs · 16,929 cycles

BS 440 STR9-10R FRAME O/B FLANGE FOUND CRACK. CRACK LENGTH 1.5". BS440 STR9-10R FRAME O/B FLANGE. REPAIRED AS PER RS R53-12-35438 AND UPS RO B747-5310-23800-A.

Part: SUPPORT TUBE — CORRODED (RT WING TE FLAPS) · airframe 72,217 hrs · 16,929 cycles

RHW I/B FORE FLAP I/B LEVER SUPPORT TUBE FOUND CORRODED AT FWD FACE INSIDE THE FORE FLAP, EXFOLIATION CORROSION. SUPPORT TUBE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: FRAME — CRACKED (NR 3 PYLON) · airframe 72,217 hrs · 16,929 cycles

NR 3 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT FWD AND AFT FRAME MOST O/B CRACK LENGTH 3/8" AND 1/4". NR 3 PYLON REAR MOUNT BULKHEAD BOTH SIDES FWD AND AFT FRAMES REPLACED AND REPAIRED AS PER RS R54-53-35431 DETAIL VISUAL AND HFEC INSPECTION OF THE BULKHEAD LWR ASSY PER RS R54-53-35431 REF /E/ EVERY 1200 FLIGHT CYCLES OR 18 MONTHS WHICHEVER IS EARLIER AND UPS EA ENGINERING FILE NUMBER C-54-20024.

Part: FRAME — CRACKED (BS 287) · airframe 72,217 hrs · 16,929 cycles

COCKPIT BS 287 S10-10A RHS FRAME O/B AREA FOUND CRACK. CRACK LENGTH 0.25" AND 1". COCKPIT BS 287 S10-10A FRAME REPAIRED AS PER RS R53-12-35435 AND UPS EO B747-5310-23811-A.

Part: RIB — CRACKED (NR 2 PYLON) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NR 2 PYLON, RT INTERIOR RIB CRACKED AT NAC STA 210 BELOW MID SPAR, CRACK LENGTH 2.5". NR 2 PYLON RT INTERIOR RIB AT NAC STA 210 BELOW MID SPAR AREA REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C EMP - BS 2658 FIREWALL BULKHEAD FORWARD SIDE WL 350 RBL 10 FOUND CRACKED, CRACK LENGTH .875 INCH. BS 2658 BULKHEAD WL 350 RBL 10" FWD SIDE AREA REPAIRED AS PER SRM 53-10-04 FIG 30.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C M/D LEFT NR 2 DOOR FWD CUTOUT LWR REVEAL FOUND CRACKED, CRACK LENGTH .5 INCH. LEFT NR 2 DOOR FWD CUTOUT LOWER REVEAL REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: PANEL — CHAFED (T/E FLAP) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C LHW, O/B AFT FLAP UPPER CENTER FLAP PANEL NR 588JT FOUND CHAFE MARKS. CHAFED AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-24 FIG 2.

Part: WEB — CORRODED (BS 2240-2260) · airframe 72,217 hrs · 16,929 cycles

BS 2240-2260 WL206 R NR 5 DOOR INTERIOR LWR WEB FOUND CORROSION. CORROSION BLEND OUT 0.060" BY 2" BY 2". LWR WEB REPLACED AS PER SRM 51-10-01 P9 (REFER NRC 6509 FOR WORKING D DETAIL).

Part: SKIN — CORRODED (RT WING) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C RT WING T/E CAVITY REAR SPAR LOWER SKIN FOUND CORRODED BETWEEN WS 510 & WS 515 (ACCESS FROM T/E PNL 671AB). CORROSION BLEND OUT 0.074 X 2 X 5 INCH EXCEED SRM LIMIT. RT WING T/E CAVITY REAR SPAR LOWER SKIN UPPER SURFACE AT WS 516.5 REPAIRED AS PER RS R57-26-35436 AND REF UPS EO B747-5720-23814-A.

Part: SKIN — DENTED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C EMP - BS 2680 TO BS 2690 SKIN ABOVE LT APU COOLING EXHAUST FOUND 1EA DENT MARK AS MARKED. DAMAGED SKIN TRIMMED OFF AT BS 2680 - BS 2690 ABOVE LT APU COOLING EXHAUST AS PER SRM 53-30-03 FIG 1A & REPAIRED AS PER SRM 53-30-03 FIG 1A AFTER NDT INSPECTED AT CUTOUT AREA AS PER NTM PT6 51-00-00 FIG 4. CRACK FREE.

Part: SPLICE — CRACKED (BS 500) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C M/D LEFT STA 500 FRAME ATT SPLICE CRACKED BETWEEN STR 13L & STR 14L, CRACK LENGTH .375 INCH. M/D BS 500 BTN S11L - 16L FRAME ATT SPLICE ANGLE REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.

Part: PANEL — DELAMINATED (T/E FLAP) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C RIGHT WING: O/B AFT FLAP PANEL 688IT UPPER SURFACE FOUND DELAMINATED. DELAMINATED AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-24 FIG 1.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C M/D BS 400 STR 23-25R FRAME I/B CHORD ATT SPLICE FOUND CRACK,CRACK LENGTH .375 INCH. BS 400 STR 23-25R FRAME I/B CHORD ATT SPLICE ANGLE REPLACED AS PER SRM 51-10-01 PG 9.

Part: FRAME — CRACKED (BS 240) · airframe 72,217 hrs · 16,929 cycles

BS240 FRAME CRACKED AT S11L CUTOUT. CRACK LENGTH 0.75". M/D BS240 S11L FRAME REPAIRED AS PER RS R53-12-35440 AND UPS EO B747-5310-23825-A AFTER CRACK FREE CONFIRMED BY NDT INSPECTION PER NTM PT6 51-00-00 FIG4.

Part: FRAME — CRACKED (BS 500) · airframe 72,217 hrs · 16,929 cycles

FOUND LT STA 500 FRAME CRACKED AT BETWEEN STR 13L & 14L U/D FLOORBEAM LOWER CHORD ATTACHMENT AREA, CRACK LENGTH 7/8". BS 500 BETWEEN STR 13L TO STR 16/17L AREA FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C M/D, LT STA 400 FRAME SPLICE ANGLE FOUND CRACKED AT STR 24L (CRACK LENGTH 7"). M/D LT BS 400 FRAME SPLICE ANGLE REPLACED AT STA 24L AREA AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: SKIN — CRACKED (BS 980) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C FX - SKIN AT BS 980 STR 38L 1EA FASTENER HOLE COMMON TO FWD LWR DRAG SPLICE FTG FOUND CRACK AT SKIN RUNNING DOWN, CRACK LENGTH .125 INCH. SKIN REPAIRED AS PER SRM 53-30-03 FIG 60 AND MPI P18440 ISSUED TO CONTROL THE REPEAT INSEPCTION INTERVALS.

Part: SKIN — CORRODED (BS 1240) · airframe 72,217 hrs · 16,929 cycles

BS 1240 LBL 90-94 WING CENTER SECTION SKIN UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.078 X 3 X 3" EXCEED SRM 57-30-01 LIMIT. BS 1240 LBL 88.5-94 WING CENTER SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35432 AND UPS EO B747-5710-23803-A.

Part: SKIN — CRACKED (NR 4 PYLON) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C NR 4 PYLON - SKIN / DOUBLER CRACKED FOUND 3EA FASTENER HOLES ON LEFT LWR EDGE BESIDE AFT UPPER ENG MOUNT FITTING NAC STA 220, (CRACK LENGTH .5 INCH). NR 4 PYLON LEFT LOWER EDGE SKIN REPAIRED AS PER SRM 54-34-03 FIG 24. AFTER STOP HOLES DRILLED CRACK FREE CONFIRMED BY NDT INSPECTION AS PER NTM PT6 51-00-00 FIG 4.

Part: STIFFENER — CORRODED (MLG WW) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C RIGHT BLG W/W TOP PANEL SUPPORT STIFFENER SURFACE CORROSION REVEALED AT STA 1403 RBL 96-98. CORROSION BLEND OUT 0.033 X 2 X 4 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SUPPORT STIFFENER REPAIRED AS PER SRM 51-40-04 FIG 1.

Part: SKIN — CORRODED (AFT CARGO DOOR) · airframe 72,217 hrs · 16,929 cycles

AFT CARGO COMPT CARGO DOOR EXTERNAL SKIN SURFACE FOUND BILGE UP AT FWD MIDDLE ACCESS PNL FWD LOWER CUTOUT, CORROSION BLEND OUT 0.065" BY 2" BY 2". DOUBLER REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02 AFTER CORROSION CLEANED AT THE MATING SURFACE AS PER SRM 51-10-01 & REPROTECTION AS PER SRM 51-10-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C FX AIR CONDITIONING BAY KEEL BEAM BOX LT EXTERNAL VERTICAL SURFACE ATT STIFFENER FOUND CRACKED AT BS 1000 LBL 9, CRACK LENGTH .375 INCH. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C FX- AIR CONDITIONING BAY KEEL BEAM BOX RT EXTERNAL VERTICAL SURFACE ATT STIFFENER FOUND CRACKED AT STA 1000 RBL 9, CRACK LENGTH .5 INCH. FX- AIR CONDITIONING BAY KEEL BEAM BOX RT EXTERNAL VERTICAL SURFACE ATT STIFFENER REPLACED PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 72,217 hrs · 16,929 cycles

FWD CARGO COMPT, BS 830-970 RT I/B FLOOR TRACK FOUND CORRODED. CORROSION BLEND OUT 0.035" BY 0.5" BY 10"). FLOOR TRACK REPAIRED AS PER SRM 53-10-05 FIG 5, JUST AT RBL 25" BETWEEN BS 930 AND 970.

Part: DOUBLER — CRACKED (BS 250) · airframe 72,217 hrs · 16,929 cycles

INSPECTION TYPE:C FX LWR FX LEFT EXTERNAL SKIN ATT DOUBLER FOUND CRACKED AT STA 250 STR 32L TO S33L NOSE L/G FWD CORNER, CRACK LENGTH 3 INCHES. FX BS 250 S41L NWW FWD CORNER CUTOUT SKIN & EXTERNAL DOUBLER REPAIRED AS PER HX RS R53-18-35439 AND REFER UPS ENGINEERING FILE 747-53-20285.

Part: ODOR — DETECTED (COCKPIT)

STRONG ODOR ON APP AFTER LDG WITH SMOKE CAME FROM EYE BALL OUTLETS. LOCKED OUT NR 1 PACK PER DMP 21-1-2-1-1, DUE TO DUCT BLOWN -NOTE PREVIOUSLY DEF M313988. RAN ALL ENG PER MM 71-00-00, ALL PACKS (EXPT NR 1), APU-NO SMOKE OR ODOR SMELL OR VISUAL FOUND (NOTE:PRESSURIZE AIRCRAFT). ALL PER AMM 21-00-00, 49-. C/W MM 05-51-30 DUCT RUPTURE, NO DAMAGE NOTED.

Part: LINK — CRACKED (NR 3 PYLON MOUNT) · airframe 71,851 hrs · 16,829 cycles

NR 3 ENG REAR ENG MOUNT THRUST LINK AFT LUG UPPER AND LOWER OF BORE FOUND SUSPECTED CRACK INDICATIONS WHICH WERE GREATER THAN 40 PERCENT FSH, EXCEEDED LIMIT. REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CARD NR 5000.

Part: LINK — CRACKED (NR 3 PYLON MOUNT) · airframe 71,851 hrs · 16,829 cycles

NR 3 ENG REAR ENGINE MOUNT THRUST LINK FWD LUG LOWER OF BORE FOUND SUSPECTED CRACK INDICATION WHICH WAS GREATER THAN 40 PERCENT FSH, EXCEEDED LIMIT. REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CARD NR 5000.

Part: LINK — CRACKED (NR 3 PYLON MOUNT) · airframe 71,851 hrs · 16,829 cycles

NR 3 ENG MOUNT THRUST LINK SUSPECTED CRACK INDICATION REVEALED AT FWD LUG UPPER SIDE, THE INDICATION GREATER THAN 40 PERCENT FSH, EXCEEDED LIMIT. REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CARD NR 5000.

Part: LINK — CRACKED (NR 2 PYLON MOUNT) · airframe 71,851 hrs · 16,829 cycles

NR 2 ENG MOUNT THRUST LINK SUSPECTED CRACK INDICATION REVEALED AT BOTH FWD AND AFT END LUG, BOTH INDICATION GREATER THAN 40 PERCENT FSH (EXCEEDED LIMIT). REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CARD NR 5000.

Part: LINK — CRACKED (NR 1 PYLON MOUNT) · airframe 71,851 hrs · 16,829 cycles

NR 1 ENG MOUNT THRUST LINK SUSPECTED CRACK INDICATION REVEALED AT BOTH FWD AND AFT END LUG, BOTH INDICATION GREATER THAN 40 PERCENT FSH (EXCEEDED LIMIT). REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CARD NR 5000.

Part: UNKNOWN — FUMES (COCKPIT)

AFTER TAKEOFF THERE WERE STRONG FUMES IN COCKPIT. CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN SDF. RAN ALL 3 PACKS, NO DEFECTS NOTED. OK FOR CONTINUED SERVICE

Part: BATTERY PACK — INOPERATIVE (R1 DOOR)

EMERGENCY LIGHTS INOP OVER R-1 DOOR. REPLACED BATTERY PACK PER MM 33-51-02.

Part: BATTERY PACK — INOPERATIVE (R1 EMER EXIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER R1 DOOR INOP. REMOVED AND REPLACED BATTERY PACK ASSY AS PER AMM 33-51-04. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EXIT SIGN AT UPPER DECK EMERGENCY EXIT IS INOP AND MARKED AS DEACTIVATED. REMOVED DEACTIVATED LABEL, NO POWER AT EXIT SIGN REQUIRES FURTHER T/S. REPLACED BATTERY PACK IAW B747 MM 33-51-04, OPS CHECK GOOD.

Part: POWERPACK — INOPERATIVE (EMERGNECY LIGHT)

2 AFT MOST O/H EMERGENCY LIGHTS IN UPPER DECK INOP. FOUND POWER PACK RIGHT SIDE STA 630 MAIN DECK INOP. PANEL LOWERED, PACK NTS. REF REQ A822639 JP VAUGHN 95768. CHARGED BATTERY PACK, CHECKS GOOD.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C FX- LEFT BS 1241 AREA EXTERNAL LONGERON FITTING NR 12 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. FX - LEFT BS 1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 12 MOUNT BOLT HOLE CORROSION CLEANED BY OVERSIZE .0156 INCH AS PER SRM 51-30-05 PG 13 AND MOUNT BOLT, ALSO REPLACED AS PER MM 20-51-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, LT BS 1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 5 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. LT BS 1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 5 MOUNT BOLT HOLE CORROSION CLEANED BY OVERSIZE BOLT HOLE .0156 INCH IAW SRM 51-30-05 PAGE 13 AND MOUNT BOLT ALSO REPLACED IAW MM 20-51-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C FX - LEFT BS 1241 AREA EXTERNAL LONGERON FITTING NR 11 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. FX - LEFT BS 1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 11 MOUNT BOLT HOLE CORROSION CLEANED BY OVERSIZE BOLT HOLE .0156 INCH AS PER SRM 51-30-05 AND MOUNT BOLT, ALSO REPLACED AS PER MM 20-51-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, LT BS 1241 AREA EXTERNAL LONGERON FITTING NR 10 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. LT BS1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 10 MOUNT BOLT HOLE CORROSION CLEANED BY OVERSIZE BOLT HOLE .0156 IAW SRM 51-30-05 PAGE 13 AND MOUNT BOLT ALSO REPLACED IAW MM 20-51-01.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, LT BS 1241 AREA EXTERNAL LONGERON FITTING NR 17 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. ( BS 1241 BULKHEAD SPLICE STRAP AFT HOLE) NR 17 MOUNT BOLT HOLE CORRODED, CLEANED BY OVERSIZE BOLT HOLE .0156 INCH IAW SRM51-30-05 BUT FOUND SPLICE STRAP CRACKED RUNNING FWD AND AFT BY HFEC INSP. IAW NTM PART 6.51-00-00 FIG 1 FURTHER REFER UPS RECORD SPLICE STRA WERE PREVIOUSLY INSPECTED AND CRACK DOCUMENTED RE-INSP. NOT DUE FOR ANOTHER 1600 CYC AND SCHEDULED SPLICE STRAP REPLACEMENT.

Part: SHEAR TIE — CRACKED (BULKHEAD) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, AFT CARGO COMPT - BS 1480 LT PRESSURE BULKHEAD LOWER CHORD ATTACH SHEAR TIE FOUND CRACKED AT STR 35L TO STR 36L. AFT CARGO COMPT BS 1480 LT BULKHEAD LOWER CHORD ATTACH SHEAR TIE AT S35L TO S36L AREA REPLACED AS PER SRM 51-10-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, BS 420 LT FRAME TIE CLIP FOUND CRACKED AT STR 7. BS 420 LT FRAME STR 7 TIE CLIP REPLACED AS PER SRM 51-10-01 PG 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, BS 610-650 LBL 46 SEAT TRACK LIP FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.060 X 2 X 4 EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 6.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, COCKPIT - BS 360 LT FRAME ATTACH SUPPORT ANGLE FOUND CRACKED AT STR 2A. COCKPIT BS 360 LT FRAME STR 2A SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 8.

Part: REVEAL — CRACKED (L5 DOORWAY) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, M/D- BS 2231-2240, S16-17L, L5 DOOR CUTOUT FWD UPPER CORNER REVEAL FOUND CRACK. M/D BS 2231-2240 STR 16-17L L5 DOOR CUTOUT FWD UPPER CORNER REVEAL CRACKED AREA REPAIRED AS PER SRM 53-10-04 FIG 91.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, U/D- BS 740-760 LEFT STR 3 STR END FOUND CRACKED. STRINGER REPAIR AS PER SRM 53-10-03 FIG 10 AT BS 740-760 LT STR 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C U/D - BS 420 - 460 LBL 60 - 64 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK SECTION REPLACED AND INSTALLED AS PER SRM 51-10-01 PAGE 8 A AND 51-30-02.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, COCKPIT - BS 360 LT FRAME ATTACH SUPPORT ANGLE FOUND CRACKED AT STR 1. COCKPIT BS 360 LT FRAME STR 1 SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, BS 400-420 BL 0 LONGITUDINAL FLOOR SUPPORT FOUND CORRODED AT UPPER & LOWER FACE. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.063 X 2 X 4 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, FLOOR SUPPORT REPLACED PER SRM 51-10-01 PG 8, CIC APPLIED IAW EO M-5100-2780-E.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, COCKPIT - BS 360 RIGHT FRAME WEB FOUND CRACKED BETWEEN STR 6 AND STR 5. FRAME WEB REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, BS 400-420 LT STR - 9 LWR STIFFENER FOUND CRACKED. BS 400-420 LT STR 9 LOWER STIFFENER REPLACED AS PER SRM 51-10-01 PG 8.

Part: SHEAR TIE — CRACKED (COCKPIT) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, COCKPIT - BS 340 LT FRAME TIE CLIP FOUND CRACKED AT STR 8. COCKPIT BS 340 LT FRAME STR 8 TIE CLIP REPLACED AS PER SRM 51-10-01 PG 8.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, L1 DOOR AFT LOWER CORNER FRAME FOUND CRACKED. LWR CORNER FRAME REPAIRED IAW SRM 52-10-02

Part: FRAME — CRACKED (FUSLEAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, U/D - BS 400 LEFT FRAME WEB FOUND CRACKED BETWEEN STR 9 AND STR 10A AS MARKED. FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 11 AT M/D BS 400 LEFT BETWEEN STR 9 TO STR 10A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, BS 400 LT FRAME I/B CHORD FOUND CRACKED BETWEEN STR 6 & STR 5. INBOARD CHORD REPLACED AS PER SRM 51-40-03 FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, U/D - BS 420 - 440 LBL 43 SEAT TRACK CROWN AND LIP FOUND CORROSION. SEAT TRACK REPLACED AS PER SRM 51-10-01 PAGE 8.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, COCKPIT - BS 360 LT FRAME ATTACH SUPPORT ANGLE FOUND CRACKED AT STR 2. COCKPIT BS 360 LT FRAME STR 2 SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, U/D - BS 560 LBL 80 LONGITUDINAL FLOOR SUPPORT FOUND CORROSION. FLOOR SUPPORT REPAIRED PER SRM 51-40-04 FIG 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, BS 460 RT FRAME WEB FOUND CRACKED AT STR -R14. BS 460 RIGHT FRAME WEB DOUBLER AT STR 14R CRACKED AREA REPAIRED AS PER RS R53-12-35179 AND EO B747-5310-20787-A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C U/D - BS 420 - 440 BL 0 LONGITUDINAL FLOOR SUPPORT LWR FACE FOUND CORRODED AROUND SCREW. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PAGE 8.

Part: RIB — CRACKED (APU BAY) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, APU COMPT FUSELAGE RIB CRACKED AT LEFT STA 2669.52 AS MARK. APU COMPT FUSELAGE RIB AT STA 2669.52 CRACK REPAIRED AS PER SRM 51-40-03 FIG 1.

Part: RIB — CRACKED (NR 4 PYLON) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, NR 4 PYLON NAC STA 232 APPROX I/B RIB CRACKED AS MARK (JUST FWD OF PYLON VALVE PANEL CUTOUT). NR 4 PYLON RIB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 8 AND SRM 51-30-02.

Part: FITTING — CORRODED (LT WING) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, LEFT WING - BS 1241 LONGERON FITTING ATTACH BOLT HOLE NR 6 FOUND CORRODED. FX - LEFT BS 1241 AREA BETWEEN EXTERNAL & INTERNAL LONGERON FITTING ATTACH NR 6 BOLT HOLE CORROSION CLEANED BY OVERSIZE .0156 INCH AND NR 6 ATTACH BOLT. ALSO REPLACED AS PER MM 20-51-01 AND SRM 51-30-05 PG 13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, U/D- BS 540-580 RBL 27 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.060 X 1 X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AT BS 540 - BS 620 RBL 27 PER SRM 53-10-05 FIG 6. CIC APPLIED IAW EO M5100-2780E.

Part: FLOORBEAM — CORRODED (COCKPIT) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, COCKPIT - BS 340 LBL 7-45 FLOORBEAM FOUND CORRODED AS MARKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.060 INCH X 2 INCH X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, FLOORBEAM REPAIRED PER SRM 53-10-07 FIG 10 & CIC APPLIED IAW EO M5100-2780E.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, M/D- BS 460 LT FRAME WEB & WEB STIFFENER FOUND CRACKED AS MARKED BETWEEN STR 13A & STR 14. FRAME REPAIRED AS PER SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, BS 510-520 RBL 45 SEAT TRACK I/B FLANGE CHIPPED AND CORRODED. *S/D* CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 8 INCHES EXCEED SRM 51-10-01 FIG 1 LIMITS. SEAT TRACK REPLACED PER SRM 51-10-01 PG 8, CIC APPLIED IAW EO M-5100-2780E.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, BS 990 S7L STRINGER END FOUND CRACKED. STR REPAIRED AS PER 53-10-03 FIG 4 AT BS 990 STR 7L.

Part: FITTING — CRACKED (STRINGER) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, M/D- STRINGER END FITTING (TRIANGULAR SHAPE) FOUND CRACK AT BS 854 STR 25R. STRINGER END FITTING REPLACED AS PER SRM 51-10-01 PG 8.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C M/D- BS 1140 - 1144 LBL 8-11, WING CENTER SECTION UPPER FACE FOUND CORROSION AS MARKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.094 X 4 X 4 INCH EXCEED SRM 57-30-01 LIMITS, WING CENTER SECTION SKIN BLENDING REPAIRED PER HXRS R57-14-35180 & UPS ENGINEERING FILE 747-57-20055. CIC APPLIED IAW EO M5100-2780-E.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, BS 200 LT FRAME WEB FOUND CRACKED BETWEEN 13A & STR 14A. BS 200 LT FRAME WEB CRACKED AREA REPAIRED AS PER RS R53-12-35175 FIG 3 AND EO B747-5310-20791-A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, BS 200 RIGHT FRAME WEB FOUND SEVERAL CRACK BETWEEN STR 13A & STR 14A. BS 200 RIGHT FRAME WEB CRACKED AREA REPAIRED AS PER RS R53-12-35175 FIG 4 AND EO B747-5310-20791-A.

Part: STRINGER — CRACKED (FUSLEAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C M/D - STA 2183 TO 2184 RIGHT NR 11 STRINGER END FOUND CRACKED. M/D STA 2183 TO STA 2184 RIGHT NR 11 CRACKED STRINGER REPAIRED AS PER SRM 53-10-03 FIGURE 4.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, LT BS 340 WL 300 UPPER DECK FLOORBEAM FOUND 1 FASTENER HOLE CRACKED AT FRAME WEB. LT BS 340 UPPER DECK FLOORBEAM AREA FRAME WEB CRACK REPAIRED AS PER RS R53-12-35177 AND EO B747-5310-20786-A.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, RIGHT BS 340 WL 300 UPPER DECK FLOORBEAM FOUND 1 EACH FASTENER HOLE CRACKED AT FRAME WEB. RIGHT BS 340 UPPER DECK FLOORBEAM AREA FRAME WEB CRACK REPAIRED AS PER RS R53-12-35177 AND EO B747-5310-20786-A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C M/D - STA 1959 TO STA 1960 RIGHT NR 1 STRINGER END FOUND CRACK. M/D - STA 1959 TO STA 1960 RIGHT NR 1 STRINGER CRACK REPAIRED AS PER SRM 53-10-03 FIGURE 4.

Part: BOLT — CORRODED (LT WING) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, LT WING CENTER SECTION REAR SPAR WEB AT BS 1241 BULKHEAD FITTING CORROSION REVEALED BETWEEN BOLT NR 7, 8 AND 9. THICKNESS CHECK PER NTM PART 4,57-10-19 RESULT: NR 7 HOLE 0.335 INCH, NR 8 HOLE 0.350 INCH, NR 9 HOLE 0.370 INCH. NR 7, 8 & 9 FASTENER HOLES REAMED TO 0.375 INCH DIA PER UPS EO B747-5710-11129 FIG 6. FASTENER HOLES AREA CORROSION REMOVED AS PER SRM 21-10-01 & REPROTECTED AS PER SRM 51-12-02.

Part: ANGLE — CRACKED (NLG WW) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE: C, NLG W/W LT UPPER CORNER AREA SUSPECT CRACKED AS MARKED AT STA 280. LT UPPER CORNER ANGLE REPLACED AS PER SB 747-53-2293.

Part: ANGLE — CRACKED (NLG WW) · airframe 68,765 hrs · 16,239 cycles

INSPECTION TYPE:C, NLG W/W RIGHT UPPER CORNER AREA SUSPECT CRACKED MARKED AT STA 314. RIGHT UPPER CORNER ANGLE REPLACED AS PER SB 747-53-2293.

Part: LINE — CHAFED (NR 3 HYD SYSTEM)

NR 3 HYD SYS LOST FLUID TO 0.5 GAL EDP ZERO WITH LOW PRESSURE LIGHT. ADP PRESSURE NORMAL. CHECKLIST COMPLETE FOR SYSTEM LEAK. FOUND PRESSURE LINE CHAFED ON PNEU DUCT IN UPPER SECTION OF NR 3 PYLON (MARKED WITH RED TAPE) BB 09326 INSTALLED NEW LINE, LEAK CHECK OK.

Part: PANEL — DELAMINATED (RT WING)

REF D277226 RT WING FIXED UPPER LEADING EDGE PANEL HAS DELAMINATION. ACCOMPLISH TEMP REPAIR. REMOVED PANEL FROM A/C. REPLACED RT WING UPPER LEADING EDGE PANEL AS PER SRM 51-30-02. THIS CLEARS D277226.

Part: SKIN — CRACKED (BS 1935-1945) · airframe 65,143 hrs · 15,580 cycles

INSPECTION TYPE:C DURING PATCH N522UP-46-08 BTN BS 1935-1945 STR 43L-45L REMOVED SHORT EDGE MARGIN FOUND BTN FASTENER & CUT OUT ABOUT 0.280" REPAIR AGAIN REQUIRED. FX - BS 1935-1945 STR 43L-45L SKIN REPAIRED AS PER SRM 53-30-03 FIG.1.

Part: ANGLE — CRACKED (DOOR #5R) · airframe 65,143 hrs · 15,580 cycles

INSPECTION TYPE:C CRACK REVEALED AT PASSENGER DOOR #5R AT THE DOOR FRAMES FWD BOTTOM CORNER VERTICAL RADIUS, THE CRACK RUNNING UPWARD WITH LENGTH 2.5" LONG APPROX. DOOR FWD ANGLE INSTALLED AS PER SRM 52-10-02 FIG.10

Part: FRAME — CRACKED (DOOR #1R) · airframe 65,143 hrs · 15,580 cycles

INSPECTION TYPE:C CRACK REVEALED AT PASSENGER DOOR #1R AT THE DOOR FRAMES FWD BOTTOM CORNER VERTICAL RADIUS. THE CRACK RUNNING UPWARD WITH LENGTH 3" LONG APPROX. AND A STOP HOLE DRILLED AT UPPER CRACK END. #1R DOOR FWD VERTICAL FRAME CRACKED AT RADIUS PREVIOUS STOP DRILLED C/OUT. HFEC C/OUT NIL CRACK BEYOND STOP DRILLED AND CRACKED FRAME PREVIOUS REPAIRED PER SRM 52-10-02 FIGURE 10.

Part: FITTING — CRACKED (WING REAR SPAR) · airframe 65,143 hrs · 15,580 cycles

INSPECTION TYPE: C, RIGHT BS 1241 WING REAR SPAR KICK FITTING, HOLE D-CORROSION CRACK FOUND APPROX 0.040 INCH RUNNING I/B FWD SURFACE. D-HOLE REWORKED AS PER EO B747-5710-12138 AND EO B747-5710-18343A RS 57-12-34973.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,143 hrs · 15,580 cycles

INSPECTION TYPE:C FX - LOWER FUSELAGE INTERIOR STRUCTURE ATT STRINGER FOUND HEAVY CORROSION AT STA 2340 TO STA 2360 STR 50R. STRINGER CUT OFF AND REPROTECTED AS PER SRM 51-10-01 AND SRM 51-10-0 2. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. TIE CLIP REPLACED AS PER SRM 51-10-01 PAGE 8. CORROSION BLEND OUT 0.060 X 1 X 2 INCH.

Part: FITTING — CORRODED (WING REAR SPAR) · airframe 65,143 hrs · 15,580 cycles

INSPECTION TYPE: C, LT WING REAR SPAR KICK FITTING AREA, CORROSION FOUND ON HOLE-D AT TERMINAL FITTING. D-HOLE REWORK AS PER EO B747-5710-18343A AND RS 57-12-34973.

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

INSPECTION TYPE: C M/D, R4 DOOR AFT UPPER CORNER FOUND CRACKED (AS MARKED). M/D - R4 DOOR AFT UPPER CORNER REPAIRED AS PER SRM 51-10-02 FIG 10.

Part: FLAP TRACK — CORRODED (NR 3 FLAP) · airframe 65,143 hrs · 15,580 cycles

INSPECTION TYPE: C, LEFT WING - NR 3 FLAP TRACK AFTER END INNER SURFACE I/B WALL AREA FOUND CORROSION (FINDING AFTER PIVOT FITTING REMOVAL). LEFT WING NR 3 FLAP TRACK AFT END INNER SURFACE INBD WALL AREA CORROSION REMOVED AND REPROTECTED REFER CWS SERIAL NR 016250, 016850 TO 16854 FOR WORK DETAILS. REF HX RS 57-53-34971 AND EO B747-5740-18331 -A. BLEND AREA 1.5 X 1.5 INCH, THICKNESS REMAIN 0.124 INCH AND ORIGINAL THICKNESS 0.207 INCH.

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

INSPECTION TYPE: C M/D, R2 DOOR FUSELAGE CUTOUT REVEAL FOUND CRACKED AT BS 805 BELOW STR 24. M/D - R2 DOOR FUSELAGE CUTOUT REVEALED PANEL REPLACED AS PER SRM 51-10-01, JUST AT BS 805 BELOW STR 24.

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

INSPECTION TYPE: C M/D, R4 DOOR FUSELAGE CUTOUT REVEAL FOUND CRACKED BELOW STR 24. M/D - R4 DOOR FUSELAGE CUTOUT REVEAL PANEL REPLACED AS PER SRM 51-10-01, JUST AT BS 1664 BELOW STR 24.

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

INSPECTION TYPE: C M/D, L4 DOOR FUSELAGE CUTOUT REVEAL FOUND CRACKED AT BS 1664 BELOW STR 24. M/D- L4 DOOR FUSELAGE CUTOUT REVEAL PANEL REPLACED AS PER SRM 51-10-01, JUST AT BS 1664 BELOW STR-24.

Part: SKIN — BULGED (FUSELAGE) · airframe 65,143 hrs · 15,580 cycles

INSPECTION TYPE: C M/D, BS 2360 BULKHEAD SKIN TO Y-RING FOUND BULGED UP AT STR 51L. BULKHEAD SKIN REPAIRED AS PER RS NR R53-83-34972 AND FX SKIN REPAIRED AT BS 2360 - 2370 BETWEEN S46L TO S46R AS PER SRM 53-10-04 FIG 5 DETAIL V, REF EO B747-5310-18355-A. TRIMMED AREA 1.5 X 10 INCH AT STR 50L AREA.

Part: ANGLE — CORRODED (RT KEELBEAM BOX) · airframe 65,143 hrs · 15,580 cycles

INSPECTION TYPE: C FX, KEEL BEAM BOX INTERIOR LOWER FRAME RT SIDE FOUND HEAVY CORROSION AT STA 1460 TO STA 1470 RBL 6 TO RBL 9. REPAIRED ANGLE FABRICATED AS PER HX RS R53-49-34970 AND EA 747-53-20123. BLEND OUT 0.146 X 2.4 X 3 INCH.

Part: ANGLE — CORRODED (LT KEELBEAM BOX) · airframe 65,143 hrs · 15,580 cycles

INSPECTION TYPE: C FX, KEELBEAM BOX INTERIOR LONGER FRAME FOUND HEAVY CORROSION AT LT SIDE STA 1465 TO STA 1475 LBL 6 TO LBL 8. REPAIRED ANGLE FABRICATED AS PER HX RS R53-49-34970 AND EA 747-53-20123. BLEND OUT 0.079 X 2.4 X 4 INCH.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY SIGN)

INSPECTION TYPE: PFLT, EMERGENCY EXIT SIGN ABOVE ESCAPE SLIDE DOOR INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE: ASE UPPER DECK EMERGENCY EXIT DOOR SILL WOULD NOT ILLUMINATE DURING ASE CHECK REPLACED EMERGENCY LIGHT BATTERY PACK REF MM 33-51-04. LIGHT OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN)

INSPECTION TYPE:W/E UPPER DECK CREW DOOR EMERGENCY EXIT SIGN INTERMITTENT, FAILED TO COME ON DURING MAINTENANCE TEST RETORQUED LOOSE CONNECTIONS ON LIGHT ASSY.

Part: TRU — BURNED (E/E BAY)

MOMENTARY HEAVY SMOKE FROM BEHIND S/O PANEL. T/R-2 C/B POPPED, SMOKE RAPIDLY DISSIPATED. SMOKE WAS NOT OBSERVED COMING FROM TRU. REMOVED AND REPLACED NR 2 TRU IAW MM 24-32-01. ALL INDICATIONS NORMAL. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY EXIT DOOR LIGHT OVER CREW SERVICE INOP. REMOVED AND REPLACED CREW SERVICE DOOR BATTERY PER 33-51-05. OPS CHECKED GOOD.

Part: WEB — CRACKED (#3 PYLON) · airframe 63,514 hrs · 15,263 cycles

INSPECTION TYPE:C #3 PYLON REAR ENGINE MOUNT B/H FOUND CRACKED AT AFT WEB FROM EDGE TO 3RD FASTENER HOLE. REFER ATTACH SKETCH FOR DETAILS. B/HEAD WEB CRACKED AREA REPAIRED AS PER RS 54-53-34781 AND UPS EO B747-5410-16695-A.

Part: POWER SUPPLY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A 2 EMERGENCY LIGHTS ABOVE CREW SERVICE DOOR INOP. REMOVED AND REPLACED CREW SERVICE DOOR POWER SUPPLY MODULE IAW B747 MM 33-51-04, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: CONNECTOR — DIRTY (COCKPIT)

INSPECTION TYPE:N/A CREW SERVICE DOOR EMERGENCY EXIT SIGN INOP. OPS CHECK AFTER CLEANING CANNON PLUG NO DEFECTS NOTED PER MM 33-51-04.

Part: CIRCUIT CARD — LOOSE (FIRE DETECTION)

INSPECTION TYPE:N/A DURING CLIMB NR 3 ENG FIRE DETECT FAULT LIGHT ILLUMINATED CHANNEL A NEEDLE WAVERED IN RED/ORANGE BAND. STABLE IN GREEN BAND ONCE POWER REDUCED. SELECTED CHANNEL B ONLY. NR 3 ENG FIRE DETECTOR -A- INOP. REF M23 4208. RESEATED THE A-3/A-7 WARNING AND CONTROL CARDS IAW MM 26-10-0 0, CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A CREW ENTRY EMERG EXIT LIGHT INOP. INSTALLED LIGHT ASSY TESTED EMERGENCY LIGHT SYSTEM OPS.

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

INSPECTION TYPE:C FX - NLG AFT CUTOUT SKIN FOUND CRACKED AT SCREW HOLE AREA LT BS 400 S45L LBL 24 AREA. NLG W/W AFT CUTOUT LT BS 400 S45L LBL 24 SKIN CRACKED AREA REPAIRED AS PER EO B747-5330-3520-E WORK DETAIL REFER ATTACH CWS.

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

INSPECTION TYPE:C EMP - TAIL COMPT SKIN CRACKED AT FASTENER HOLE, BS 2658 BETWEEN STR 11R AND STR 12R. CRACKED EXTERNAL SKIN AT BS 2658 BETWEEN STR R11 & R12 AREA REPAIRED AS PER SRM 53-30-03 FIG 1A.

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

INSPECTION TYPE:C EMP - TAIL COMPT LT SKIN CRACKED AT FASTENER HOLE, BS 2658 BETWEEN STR 11L AND STR 12L. CRACKED EXTERNAL SKIN AT BS 2658 BETWEEN STR L11 & L12 AREA REPAIRED AS PER SRM 53-30-03 FIG 1A.

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

INSPECTION TYPE:C U/D - BS 360 LT STR 4 & 3A FRAME CRACKED. REPAIRED FRAME AS PER SRM 53-10-04 FIG 18.

Part: SPAR — CORRODED (ELEVATOR) · airframe 61,383 hrs · 14,839 cycles

INSPECTION TYPE:C EMP - RT OUT/B ELEVATOR INTERIOR FRONT SPAR UPPER CHORD FOUND SURFACE CORROSION AT ELEV STA 310 TO STA 390 AS MARK. THE RT O/B ELEVATOR FRONT SPAR UPPER CHORD BETWEEN ELEV STA 310 AND 390 AREA CORROSION CLEANED UP. BLEND OUT AREA OUT OF ALLOWABLE LIMIT AS PER SRM 55-20-01 FIG 1.4. REPAIR WAS CARRIED OUT IAW SRM 51- 40-04. ELEVATOR BALANCE ALSO C/OUT AS PER SRM 51-80-02 AFTER REPAIR.

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

INSPECTION TYPE:C, RT BS 300 FRAME BETWEEN STR 39R AND 40R FOUND 2 FASTENER HOLE CRACKED AT FRAME WEB. PLS REFER ATTACHED SKETCH. RT BS 300 STR 39R TO 40R AREA FRAME WEB REPAIRED AS PER SRM 51-40-03.

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

INSPECTION TYPE:C, LT BS 300 NOSE WHEEL WELL VERTICAL BEAM WEB FOUND CRACK AT NR 3 INSULATION BLANKET STAND-OFF HOLE (COUNT FROM TOP) APPROX .375 INCH AND .5 INCH RUNNING UPWARD AND DOWNWARD RESPECTIVELY. LT BS 300 NOSE WHEEL WELL VERTICAL WEB REPLACED AS PER SRM 51-10-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,383 hrs · 14,839 cycles

INSPECTION TYPE:C FX - BODY FAIRING SUPPORT FRAME STA 880 LBL 50 - RBL 50 FOUND CORROSION. FX - BODY FAIRING SUPPORT REPAIR AT BS 880 FROM LBL 50 - RBL 50.

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

INSPECTION TYPE:C LT BS 320 NOSE WHEEL WELL VERTICAL BEAM WEB FOUND 1 FASTENER HOLE COMMON TO THE FRAME CRACKED, PLS REFER THE ATTACH SKETCH. VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 & REFER NRC 5251 FOR DETAIL.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,383 hrs · 14,839 cycles

INSPECTION TYPE:C FX - BODY FAIRING SUPPORT FRAME STA 960 LBL 110 - RBL 60 FOUND CORROSION. BS 960 BODY FAIRING SUPPORT FROM RBL 19 - RBL 21 REPAIR.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,383 hrs · 14,839 cycles

INSPECTION TYPE:C FX - BODY FAIRING SUPPORT FRAME STA 840 LBL 50 - RBL 50 FOUND CORROSION. FX - BODY FAIRING SUPPORT REPAIR AT BS 840 FROM RBL 9 - RBL 25.

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

INSPECTION TYPE:C U/D - BS 460 S-11L TO S-12L FRAME FOUND CRACKED. REPAIRED FRAME AS PER SRM 53-10-04 FIG 11.

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

INSPECTION TYPE:C, RT BS 320 FRAME BETWEEN STR 39R AND 41R FOUND 4 FASTENER HOLE CRACKED AT FRAME WEB AND FRAME INNER CHORD, PLS REFER ATTACHED SKETCH. RT BS 320 FRAME REPAIRED AT STR 39R - 41R AS PER SRM 51-40-03 AND FRAME INNER CHORD REPLACED AS PER SRM 51-10-01.

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

INSPECTION TYPE:C, LT BS 320 NOSE WHEEL WELL VERTICAL BEAM WEB FOUND CRACK AT NR 3 INSULATION BLANKET STAND - OFF HOLE (COUNT FROM TOP) APPROX .3125 INCH RUNNING UPWARD. VERTICAL BEAM WEB REPAIRED AND REPLACED AS PER SRM 51-10-01.

Part: TEE CHORD — BULGED (LT WING) · airframe 61,383 hrs · 14,839 cycles

INSPECTION TYPE:C LHW - UPPER SURFACE L/E FIXED PANEL BUTT JOINT AREA FOUND BULGE AT ILES 997 AFT OF NR 7 V.C. FLAP AS MARKED. L/E FIXED PANEL SUPPORT T-CHORD REPLACED AND RIB REINSTALLED AS PER SRM 51-30-02, 51-10-01 L/E PNEUMATIC DUCT TRUSS ROD AND TORQUE SHAFT REMOVED AND RECONNECTED AS PER MM 36-11-00, 20-51-01, 27-81-05.

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

INSPECTION TYPE:C LT SIDE BS 1241 BULKHEAD FORWARD HOLE FOUND CRACKED AT BULKHEAD FRAME FORGING O/B EDGE APPROX 0.040 INCH RUNNING UP. PLS REFER TO ATTACH SKETCH FOR DETAILS. LT SIDE BS 1241 BULKHEAD FRAME FORGING FWD HOLE REWORKED AS PER EO B747-5310-0323-L APPENDIX H AND HAECO REPAIR SCHEME R-53-41-346 69.

Part: ANGLE — CORRODED (L5 DOOR) · airframe 61,383 hrs · 20,928 cycles

INSPECTION TYPE:C M/D - L5 DOOR BS 2238 BETWEEN 1 X 2 FRAME WL 230 NR 4 WEB (COUNT FROM LOWER) ATT INTERIOR ANGLE HEAVY CORROSION. REPLACED L5 DOOR INNER ANGLE PER SRM 51-10-01.

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

INSPECTION TYPE:C U/D - BS 480 S-10AR FRAME FOUND CRACKED. REPAIRED FRAME AS PER SRM 53-10-04 FIG 11.

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

INSPECTION TYPE:C, RT BS 320 FRAME AT SKIN ATTACH FLANGE BETWEEN STR 39R AND 40R FOUND CRACKED APPROX .25 INCH AS MARKED. RT BS 320 FRAME ATT SHEAR TIE BETWEEN S39R - S40R REPAIRED AS PER SRM 51-40-03.

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

INSPECTION TYPE:C U/D - BS 500 S-10AR TO S-11R FRAME FOUND CRACKED. REPAIRED FRAME AS PER SRM 53-10-04 FIG 11.

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

INSPECTION TYPE:C U/D - BS 460 S-11R FRAME FOUND CRACKED. REPAIRED FRAME PER SRM 53-10-04 FIG 11.

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

INSPECTION TYPE:C U/D - BS 480 S-11L TO S-12L FRAME FOUND CRACKED. REPAIRED FRAME PER SRM 53-10-04 FIG 11.

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

INSPECTION TYPE:C, RT BS 320 NOSE WHEEL WELL VERTICAL BEAM WEB FOUND CRACK AT NR 3 INSULATION BLANKET STAND - OFF HOLE (COUNT FROM TOP) APPROX .1875 INCH RUNNING UPWARD AS MARKED. RT BS 320 NOSE WHEEL WELL VERTICAL BEAM WEB REPLACED AS PER SRM 51-10 -01.

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

INSPECTION TYPE:C RT BS 300 NOSE WHEEL WELL VERTICAL BEAM WEB FOUND CRACK AT NR 3 INSULATION BLANKET STAND - OFF HOLE (COUNT FROM TOP) APPROX .25 INCH AND .375 INCH RUNNING UPWARD AND DOWNWARD RESPECTIVELY. VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 AT RT BS 300 NOSE WHEEL WELL AREA.

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

INSPECTION TYPE:C M/D - BS 400, S-15L TO S-16L FRAME FOUND CRACKED. REPAIRED FRAME PER HXRS R53-12-34671, BETWEEN S-15L TO S-16L BS 400 LT.

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

INSPECTION TYPE:C M/D - BS 500 S-16L WEB FOUND CRACKED. REPLACED BRACKET AS PER SRM 51-10-01.

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

INSPECTION TYPE:C M/D - BS 400 S-14R FRAME FLANGE FOUND CRACKED. INSTALLED REINFORCED DOUBLER PER SRM 51-30-02.

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

INSPECTION TYPE:C M/D - BS 220, S14CR - S14DR FRAME FOUND CRACKED. REPAIRED FRAME PER SRM 53-10-04 FIG 4.

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

INSPECTION TYPE:C M/D - BS 380-400, S-14R WEB FOUND CRACKED. REPAIRED SUPPORT WEB PER SRM 51-40-03 FIG 1.

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

INSPECTION TYPE:C CRACK REVEALED ON LT BS 1241 BULKHEAD CANTED PRESSURE DECK FITTING AT THE AFT HOLE AREA BY APPROX 0.080 INCH LONG RUNNING FWD DOWN DIRECTION AS PER ATTACH SKETCH. LH BS 1241 BULKHEAD CANTED PRESSURE DECK FITTING AFT BOLT HOLE CRACKED AREA REWORKED AS PER HAECO REPAIR SCHEME R-53-41-34669 WORK DETAIL REFER ATT CWS.

Part: BRAKE ASSY — INOPERATIVE (MLG)

WHILE EXITING RAMP NO NORMAL BRAKES AVAILABLE MOMENTARILY. INSPECTED ALL SYSTEM FOR LEAKS, NONE FOUND. PERFORMED OPERATION OF BRAKE SYSTEM ON NR 4, NR 1 AND RESERVE SYSTEM. FOUND NORMAL IAW MM 32-40-00. OK FOR SERVICE.

Part: FIRE DETECTOR — MALFUNCTIONED (NR 4 ENGINE)

INSPECTION TYPE:N/A NR 4 ENGINE FIRE DETECTION LIGHT ILLUMINATED REMOVED AND REPLACED NR 4 ENGINE UPPER AFT TEST DECTECTOR ASSY. I.A.W. MMNL 26-11-00. OPERATIONAL CHK SYSTEM NORMAL.

Part: FCU — LEAKING (NR 4 ENGINE)

INSPECTION TYPE:N/A, NR 4 ENG FUEL LEAK. *S/D* FOUND FUEL LEAKING BETWEEN FCU AND FUEL PUMP. REMOVED FCU, REPLACED O-RINGS AND RE-INSTALLED FCU IAW 73-21-01.

Part: DOOR FRAME — CORRODED (L5 DOOR) · airframe 61,383 hrs · 14,839 cycles

INSPECTION TYPE:C M/D L5 DOOR BS 2238 BETWEEN 1 AND 2 FRAME WL 235 NR 5 WEB, COUNT FROM LWR, CORRODED. REPLACED FRAME PER SRM 51-10-01 (ATT CHANNEL / BRACKET REPLACED AS WELL) DOOR L5 OPERATIONAL TEST DONE SATISFACTORY.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE:C 44.EVIDENCE OF CORROSION ON STINGER 50L/H AND 51L/H TO TIE FITTING A T BS2360.FWD OF REAR PRESSURE BULK HEAD.PLEASE EVALUATE. ***CPCP*** FUSELAGE SKIN OPENED AT BS2360 FOR ACCESS FOR REMOVEL OF STRINGERS.C ORRODED SECTIONS OF STRINGERS 51L,50L,AND 51R WHERE REMOVED AND NEW SECTIONS SPLICED IN I.A.W SRM 53-10-03.AREA CLOSED I.A.W SRM 51-30-0 2.

Part: CHANNEL — CORRODED (NR 4 ENGINE) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C, RT WING LEADING EDGE. CORROSION ON SUPPORT CHANNEL FOR LE LOWER. FALSE WORK PANEL I/B OF NR 4 ENGINE.

Part: CHANNEL — CORRODED (LT WING) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C, LT WING LEADING EDGE. CORRODED ON SUPPORT CHANNEL FOR LE LOWER. FALSEWORK PANEL INBOARD OF NR 1 ENGINE. CHANNEL REPAIRED I.A.W QUERY NOTE 36/2000.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C, CRACK FOUND REPAIRED I.A.W QUERY NOTE N522UP/11/2000.NOTE THIS REPAIR IS SUBJECT TO A REPEAT INSPECTION.

Part: SPAR — CORRODED (RT WING) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C, RT WING FRONT SPAR. CORROSION ON FRONT SPAR AT ILES 427. REPAIRED ACCOMPLISHED I.A.W QUERY NOTE N522UP/15/2000,AND APPROVED 8 110-3.

Part: RIB — CORRODED (RT WING) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C, RT WING LEADING EDGE, CORROSION ON LE RIB AT OLES 1543 RT O/B SIDE. NEW RIB FABRICATED AND INSTALLED I.A.W SRM 51-30-02.REF WORK SHOP OR DER E0098342.

Part: SPAR — CORRODED (RT WING) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C, RT WING LEADING EDGE. CORROSION ON FRONT SPAR OF LT WING AT ILES 621. REPAIRED IAW QUERY NOTE N522UP/08/2000, AND APPROVED 8110-3

Part: SPAR — CORRODED (LT WING) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C, LT WING LEADING EDGE. CORROSION ON FRONT SPAR OF LT WING WEB BETWEEN OLES 1543 AND OLES 1562.

Part: SPAR — CORRODED (RT WING) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C, RT WING LEADING EDGE. CORROSION ON RT FRONT SPAR WEB AT OLES 1418-1446. REPAIRED I.A.W QUERY NOTE N522UP/10/2000,AND APPROVED 8110-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C 44. AFT CARGO HOLD.EXTENSIVE SURFACE CORROSION ON BULK CARGO HOLD FLOOR SUPPORTS AT HOLES AND AT ATTACHMENT TO INNER CHORD OF FLOORBEAMS. (1) REMOVE CORROSION (2) EVALUATE (3) REPROTECT. CORROSION REMOVED AND REPROTECTED I.A.W SRM 51-10-02.NEW TIE DOWN RAIL FABRICATED I.A.W E0097612 AND INSTALLED I.A.W SRM 51-40-03.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C, REAR CARGO HOLD. LIGHT CORROSION AT BS 2160 BETWEEN STRINGERS 43 AND 51 RT. (1) REMOVE CORROSION (2) EVALUATE (3) REPROTECT SHEAR TIE SECTION FROM STRS 43 LT TO 51 RT REPLACED I.A.W 51-30-02 AND 53-10-04.

Part: SPAR — CORRODED (RT WING) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C, RT WING FRONT SPAR. CORROSION ON RT UPPER SPAR SKIN EXTENSION, AT OLES 1395. CORROSION REMOVED I.A.W SRM 51-10-01 AND REPROTECTED I.A.W SRM51-10- 02.REF NRC 44255054 FOR NDT INSPECTION.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C, AFT UNDER FLOOR LIGHT CORRODED ON FUSELAGE INNER SKIN AT BS.2180 - 2200 BETWEEN STRINGERS 48 -49 LT AND 49-50 LT. (1) REMOVE CORROSION (2) EVALUATE (3)REPROTECT REF.NON ROUTINE CARD 44256 585 FOR ACCESS UNDER TANK.REPAIRED I.A.W Q UERY NOTE N522UP/6/2000.STRINGER REPAIR CARRIED OUT I.A.W SRM 53-10-0 3 FIG1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE: C, IN REAR CARGO HOLD CORRODED AND SHEARED FASTENER ON SHEAR TIE AT BS .2160 BETWEEN STRINGERS 47 - 48 RT. CARRY OUT REPAIR. SHERE TIES FABRICATED I.A.W WORK ORDERS E0097634 & E0097646 INSTALLED I.A.W SRM 53-10-04.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE:C, AFT CARGO HOLD BULK CARGO HOLD FLOOR SUPPORT IS CRACKED AT BS 1975, 2060 AND 2080 RBL 9. CARRY OUT REPAIR. SUPPORT REPLACED IAW SRM 51-30-02 AND 51-40-03. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-10-01. FASTENERS REMOVED AND REPLACED IAW SRM 51-30-02.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE:C 44. AFT CARGO HOLD BULK CARGO HOLD FLOOR SUPPORT IS CRACKED AT BS 202 0, 2024 AND 2026 RBL 9. CARRY OUT REPAIR/REPLACEMENT. SUPPORT REPLACED IAW SRM 51-40-03. CORROSION REMOVED IAW SRM 51-10-02, REPROTECTED TREATED IAW SRM 51-30-01. FASTENERS REMOVED AND INSTALLED IAW SRM 51-40-03.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE:C 44 AFT CARGO HOLD BULK CARGO HOLD FLOOR SUPPORT IS CRACKED AT BS 202 0 RBL 39. CARRY OUT REPAIR. SUPPORT REPLACED IAW SRM 51-40-03. CORROSION REMOVED AND REPROTECTED IAW 51-10-01, 51-10-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE:C 44. AFT CARGO HOLD SHEAR TIE IS BADLY CORRODED AT BS 2160 BETWEEN STR.45-46 LT. CARRY OUT REPAIR. SHEAR TIE FABRICATED AND REPLACED IAW SRM 53-10-04. REF WORK ORDER E0097646.

Part: CARGO TRACK — DAMAGED (FUSELAGE) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE:C 44 AFT CARGO HOLD BULK CARGO HOLD SUPPORT IS DAMAGED AT BS 1980 RBL 9. CARRY OUT REPAIR. SUPPORT REPLACED IAW SRM 51-40-03, CORROSION REMOVED IAW 51-10-0 2, REPROTECTED IAW SRM 51-10-01.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE:C 44. LOWER SECTION 41 STR 39 RIGHT HAND IS DAMAGED AT BS 280, CARRY OUT REPAIR. STRINGER REPLACED IAW SRM 51-30-02.

Part: SKIN — DAMAGED (RUDDER) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE:C 44. DAMAGE TO L/E OF UPPER RUDDER JUST BELOW PCU (LHS), PLEASE INVESTIGATE. NEW SKIN PANEL FABRICATED IAW E0097709 AND INSTALLED IAW SRM 51-30-02.

Part: WEB — CORRODED (RT WING) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE:C 44. RT WING L/E CORROSION ON FRONT SPAR WEB AT SEVERAL LOCATIONS BETWEEN OLES 1200 AND OLES 1300 RT. PLEASE INVESTIGATE / RECTIFY. REPAIRED IAW QUERY NOTE N522UP/9/2000 AND APPROVED 8110-3.

Part: SKIN — CORRODED (LT WING) · airframe 58,016 hrs · 14,146 cycles

INSPECTION TYPE:C 44. LEFT HAND WING LEADING EDGE CORROSION ON LT LWR INSPAR SKIN EXTENSION AT OLES 1328. REMOVED CORROSION AND REPROTECT AREA. REPAIRED IAW QUERY NOTE N522UP/7/2000 AND APPROVED 8110-3 DATED 29TH OF MARCH 2000.

Part: BATTERY PACK — DISCHARGED (GALLEY)

UPPER DECK EMERGENCY LIGHT (2) IN CEILING AFT OF CREW GALLEY ARE INOP. THE LIGHTS COME ON AND THEN GO OUT IMMEDIATLY. FOUND CEILING BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, CREW SERVICE DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED CREW SERVICE DOOR EMERGENCY LIGHT BATTERY POWER PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

CREW SERVICE DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED CREW SERVICE DOOR EMERGENCY LIGHT BATTERY POWER PACK. OPS CHECK NORMAL.

Part: BLEED VALVE — FAILED (NR 4 ENGINE)

INSPECTION TYPE:N/A, AT 1000 FEET ENGINE NR 4 SHOWED ENGINE FIRE. SHUT ENGINE DOWN PER UPS OPERATING PROCEDURES. REMOVED AND REPLACED NR 4 ENGINE HIGH STAGE BLEED VALVE AND CONTROLLER PER MM 36-11-17 AND 36-11-06, OPS CHECKS NORMAL PER MM 71-00-00. INSPECTED TIRES AND BRAKES AFTER COOL DOWN, CKS NORMAL.

Part: PANEL — CRACKED (RT WING)

INSPECTION TYPE:N/A, CRACK IN UPPER L/E WING PANEL I/B NR 2 ENGINE. *S/D* INSTALLED NEW PANEL AS REQUIRED.

Part: SKIN — CRACKED (LT TE MIDFLAP)

INSPECTION TYPE:A/CK, LT MID FLAP CRACKED.

Part: CONNECTOR — DIRTY (COCKPIT)

SDF - EEL ABOVE ESCAPE DOOR IN COCKPIT INOPERABLE, NR 325 326. CLEANED CONNECTION, OPS CHECK NORMAL. (X)

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:W, END EEL ABOVE ESCAPE HATCH DOOR IN COCKPIT INOP, NR X325-X326. CLEANED CONECTOR, OP'S CHECK NORMAL.

Part: SKIN — CRACKED (NR 1 PYLON)

INSPECTION TYPE N/A, CRACK FOUND ON PYLON NR 1 RT SIDE WHICH EXTENDS THE TRIMMING AREA REQUIRED BY SB 54-2034 IN FRONT OF STATION 180. REMOVED PREVIOUS REPAIR, TRIMMED EFFECTED CRACK, INSTALLED REPAIR PER SB 54-2034.

Part: DOUBLER — MISREPAIRED (NR 3 PYLON)

INSPECTION TYPE-N/A, PREVIOUS DOUBLER REPAIR ON PYLON NR 3 LT SIDE FOUND INSTALLED ON THE AREA WHERE IT WILL INTERFERE WITH THE INSTALLATION OF NEW DOULBLER PER SB-54-2034. REMOVED PREVIOUS REPAIR, INSTALLED NEW REPAIR PER SB 54-2034.

Part: SKIN — CRACKED (NR 2 PYLON)

INSPECTION TYPE-N/A, RT SIDE OF PYLON NR 2 IS CRACKED ON EXTERIOR SKIN IN FRONT OF STA 180 WHICH EXTENDS THE TRIMMING AREA, REPAIRED PER SB-54-2034. REMOVED PREVIOUS REPAIR, TREATED AND INSTALLED NEW REPAIR UP TO TRIMMING AREA PER SB-54-2034.