N667US

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 112,687 hrs · 13,736 cycles

UPPER DECK CEILING EMERGENCY LIGHTS BETWEEN SEAT 73 WILL NOT TURN-OFF AFTER 20 SEC. REPLACED BATTERY-POWER SUPPLY AT M335. FUNCTIONAL CHECK OK AS PER B747-400 AMM 33-51. AFFECTED LTS STAY ON AFTER 20 SEC. (7856385)

Part: DOOR FRAME — CRACKED (L5) · airframe 109,569 hrs · 13,384 cycles

AFT UPPER CORNER OF CUTOUT FOR LT MAIN ENTRY DOOR NR 5 FOUND 1 CRACK APPROXIMATELY 1.2" LENGTH. PLEASE REFER TO 5330-01212-03A FOR WORK DETAILS FOR AFT CORNER OF CUTOUT FOR LT MAIN DOOR NR 5 FOUND CRACK, JOB COMPLETED.

Part: DOOR FRAME — CRACKED (RK) · airframe 109,569 hrs · 13,384 cycles

AFT UPPER CORNER OF CUTOUT FOR RT MAIN ENTRY DOOR NR 5 FOUND 1 CRACK APPROXIMATELY 2" IN LENGTH. PLEASE REFER TO 5330-01212-03B FOR WORK DETAILS FOR AFT UPPER CORNER OF CUTOUT FOR RT MAIN DOOR NR 5 FOUND CRACK, JOB COMPLETE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 109,471 hrs · 13,373 cycles

SEAT 63 JK AND SEAT 65 JK EMERGENCY LIGHTS INOPERATIVE. FOUND UNDER SEAT CONNECTOR DISCONNECTED, RECONNECTED SAME, OPS CKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 109,441 hrs · 13,369 cycles

ROWS 35-43 CEILING EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK M7927 IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 109,441 hrs · 13,369 cycles

ROWS 22-32 SEAT MOUNTED EMERGENCY LIGHTS AND DOOR 2R EXIT SIGNS INOPERATIVE. R & R E-LIGHT BATTERY PACK M7918 IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 109,441 hrs · 13,369 cycles

ROWS 51-66 SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE AND DOOR 4R EXIT SIGNS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK M7924 IAW AMM.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 108,810 hrs · 13,284 cycles

EMERGENCY LIGHTS INOPERATIVE ROW 52 TO 60 LT SIDE. RECONNECTED CONNECTOR AT SEAT 52.

Part: FUSE — OPEN (EMERGENCY LIGHTS) · airframe 106,216 hrs · 12,979 cycles

FOUND EXTERIOR EMERGENCY LIGHTS OUT. FOUND OPEN POWER SUPPLY FUSE, REPLACED FUSE.

Part: FUSE — OPEN (EMERGENCY LIGHTS) · airframe 106,216 hrs · 12,979 cycles

L3 DOOR EXIT LIGHT WOULD NOT ILLUMINATE. POWER SUPPLY FUSE OPEN. REPLACED FUSE.

Part: SKIN — CRACKED (WING) · airframe 105,556 hrs · 12,911 cycles

FOUND A FOURTY ONE INCH CRACK ON RT OVERWING L/E FIXED SKIN PANEL AT APPROXIMATELY ILES 430. R & R PANEL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 104,977 hrs · 12,838 cycles

DURING SERVICE CHECK, FOUND OVERWING EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 104,787 hrs · 12,817 cycles

LEFT OVERWING EMERGENCY LIGHT WOULD ILLUMINATE POSITION MOST FWD AND SECOND FROM FWD. REPLACED FUSE ON POWER SUPPLY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 104,188 hrs · 12,746 cycles

RT OVERWING EMERGENCY LIGHT IS OUT. REPLACED CHARGER ASSY.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 104,137 hrs · 12,739 cycles

EMERGENCY LIGHTS SEATS 51C THRU 60C INOPERATIVE. RECONNECTED EMERGENCY LIGHT CONNECTOR.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 102,676 hrs · 12,560 cycles

SEAT 1K EMERGENCY LIGHTS INOPERATIVE. FOUND WIRING BURIED IN LAYFLAT SEATS. FURTHER TROUBLESHOOTING FOUND CONNECTOR DETACHED. SECURED CONNECTOR AND CHECKED OK. EMERGENCY LIGHT OPS OK IAW 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 102,035 hrs · 12,486 cycles

FOUND BOTH UPPER DECK SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AND CHECKED OK IAW AMM 33-51.

Part: BRACKET — DAMAGED (BS 2698.85) · airframe 101,356 hrs · 12,408 cycles

LEFT APU DOOR FRAME BRACKET DAMAGED BS 2698.85. HFEC INSPECTED THE TRIMMED EDGE FOUND NO CRACK IAW NDTM MANUAL, PART 6, 51-00-00, PROCEDURE 16. REPAIRED IAW ERA 520405-14, REV ORIGINAL.

Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 101,356 hrs · 12,408 cycles

AFT CARGO DOOR INTERNAL STRUCTURE FWD LOWER CORNER FOUND CORRODED BS 1813. HFEC INSPECED AND CORROSION BLENDED OUT, FOUND NO CRACKS FOUND IAW NDT MANUAL PART6 51-00-00, PROCEDURE 16 AND PROCEDURE 23. REPAIRED IAW ERA 520406-14, REV.

Part: STANCHION — CRACKED (BS 460) · airframe 101,356 hrs · 12,408 cycles

CRACK ON STANCHION BS 460 LBL 98.5. STANCHION REPAIRED IAW ERA 520400-14, REV ORIGINAL.

Part: STANCHION — CRACKED (BS 460) · airframe 101,356 hrs · 12,408 cycles

CRACKED STANCHION BS 460 RBL 98.5. STANCHION REPAIRED IAW ERA 520401-14, REV ORIGINAL. HFEC INSPECTED, CUTOUT EDGE FOUND CRACK FREE IAW NDTM PART 6 53-30-00, PROCEDURE 23.

Part: SKIN — DENTED (CARGO DOOR) · airframe 101,356 hrs · 12,408 cycles

BULK CARGO DOOR ABOVE DOOR OPEN/CLOSE HANDLE FOUND SIX DENTS. DENTS REMOVED AND SKIN RESTORED TO ORIGINAL COUNTOUR IAW SRM 51-70-01. HFEC INSPECTION CARRIED OUT IAW NDTM PART 6 51-00-00, PROCEDURE 23. ONE CRACK FOUND. REPAIRED IAW SRM 52-00-01, REPAIR 8. FABRICATED REPAIR IAW SRM 52-00-01, REPAIR 8. HFEC INSPECTION CARRIED OUT ON THE REWORKED AREA IAW NDTM PART 6 51-00-00, PROCEDURE 23 . NO CRACKS FOUND.

Part: SEAT TRACK — CORRODED (BS 1660) · airframe 101,356 hrs · 12,408 cycles

BS 1660, RBL 98, WL 199.8 SEAT TRACK FOUND CORRODED. CORROSION REPAIR PERFORMED IAW SRM 53-00-52. REPAIR 1, NEW REPAIR PART FABRICATED IAW SRM 53-00-52, REPAIR 1.

Part: STRINGER — CORRODED (BS 1930) · airframe 101,356 hrs · 12,408 cycles

BULK CARGO BS 1930 STRINGER 51R, FOUND CORRODED. CORROSION REMOVED IAW SRM 53-00-03, REPAIR 6 . FABRICATED REPAIR PARTS IAW SRM 53-00-53, REPAIR 6. HFEC INSPECTION WAS CARRIED OUT ON REWORK AREA IAW NDTM PART 6 51-00-00, PROCEDURE 23 AND NO CRACKS FOUND.

Part: STRINGER — CORRODED (BS 1910) · airframe 101,356 hrs · 12,408 cycles

AFT CARGO BAY, STRINGER 51R BS 1910, FOUND CORRODED . CORROSION REMOVED IAW SRM 53-00-53, REPAIR 6. REPAIR PARTS FABRICATED IAW SRM 53-00-03, REPAIR 6. HFEC INSPECTION ON REWORK AREA CARRIED OUT IAW NDTM PART 651-00-00 PROCEDURE 23 AND NO CRACK FOUND.

Part: STOP FITTING — CRACKED (R3 DOOR FRAME) · airframe 101,356 hrs · 12,408 cycles

R3 DOOR FWD CUT-OUT NR 4 STOP SUPPORT FITTING FOUND CRACKED. FITTING REPLACED.

Part: SEAT TRACK — DAMAGED (BS 2270-2250) · airframe 101,356 hrs · 12,408 cycles

BS 2270-2250 RBL 33 WL 199.8 SEAT TRACK DAMAGED. SEAT TRACK REPLACED IAW SRM 53-00-52, REPAIR 9.

Part: SKIN — DEFORMED (PAX DOOR) · airframe 101,356 hrs · 12,408 cycles

NR 5 MAIN DOOR EXTERIOR SKIN FWD AND AFT LOWER CORNER FOUND DEFORMED. REPAIRED IAW SRM 52-00-01, REPAIR 9, TABLE 1.

Part: FRAME — CRACKED (BS 1220) · airframe 101,356 hrs · 12,408 cycles

FRAME BS 1220 S8L FOUND CRACKED. REPAIRED IAW SRM 53-40-07, REPAIR 6 .

Part: STRAP — CRACKED (BS 2231 FRAME) · airframe 101,356 hrs · 12,408 cycles

TWO CRACKS FOUND ON FRAME STRAP AT BS 2231,S25- 26L. REPAIRED FRAME STRAP IAW SRM 53-60-15. REPAIR 2.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 101,276 hrs · 12,399 cycles

EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED FUSE IN POWER SUPPLY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 99,616 hrs · 12,197 cycles

LT OVER WING PATH EXTERIOR EMERGENCY LIGHT INOPERATIVE (4 POSITION). FOUND FUSE DEFECTIVE ON CHARGER AT 3L DOOR OVERHEAD PANEL BUT NO HELP. REPLACED BATTERY AND POWER SUPPLY UNIT ABOVE DOOR 3L. EMERGENCY LIGHT OPS TESTED NORMAL IAW AMM 33-51.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 97,617 hrs · 11,960 cycles

DOOR 3R AND RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY AND BATTERY PACK (M7920). OPS CHECKED GOOD.

Part: CHANNEL — CRACKED (BS 1180) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1180 TENSION TIE, FOUND ONE CRACK AT AFT CHANNEL, LWR ROW 5TH FASTENER HOLE FROM OTBD AFTER FRAME. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00, PROC 16 AND FOUND, NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1180 TENSION TIE, FOUND ONE CRACK AT FWD CHANNEL, LOWER ROW 5TH FASTENER HOLE FROM OTBD AFTER FRAME. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507 REV 1.

Part: PLATE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 1ST FASTENER HOLE FROM OTBD AFTER FRAME. REAMED OVERSIZE FROM 0.187" TO 0.216" DIA IAW SB747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00, PROC 16 AND FOUND NO CRACK EVIDENT.

Part: PLATE — CRACKED (BS 1180) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1180 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 7TH FASTENER HOLE FROM OTBD. STEEL PLATE REMOVED IAW SRM 51-40-02. FABRICATED IAW DWG 65B09631 REV AG AND INSTALLED SRM 51-40-02.

Part: FAILSAFE — CRACKED (BS 1120 FRAME) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1120 TENSION TIE, FOUND ONE CRACK AT FAILSAFE, UPPER ROW 1ST FASTENER HOLE FROM OTBD. FRAME SEGMENT REPAIR CARRIED OUT IAW SRM 53-40- 07, FIG 201, REPAIR 4. FAILSAFE REPAIR CARRIED OUT IAW SRM 51-70-11, FIG 1.

Part: SKIN — CRACKED (BS 980) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC OPEN HOLE ON BS 1000, BULKHEAD FUSELAGE SKIN ON REMOVE FASTENER HOLE AND FOUND CRACK TWO. FUSELAGE BS 980 RT SIDE SKIN REPAIR CARRIED OUT IAW PRI 510085-14, AD REV 0 AND REV 1, DATED 16 JAN 2013. PRI 510085-14AD, REV 0 AND REV 1 COMPARED AND COMPLIED WITH ER/A 510085-14AD. REV ORIGINAL.

Part: PLATE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 2ND FASTENER HOLE FROM OTBD. STEEL PLATE REMOVED IAW SRM 51-40-02. FABRICATED IAW DWG 65B09631, REV: AG AND INSTALLED IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,543 hrs · 11,950 cycles

DURING ULTRASOUND INSP, CARRIED OUT AND FOUND CRACK INDICATION ON FUSELAGE SKIN AT 01 EA FASTENER BETWEEN BS 980 AND BS 990 AT RH S-38. ACFT JACKED IAW 65B16707 DWG XXX. Q METHOD. DRAG SPLICE FITTINGS REMOVED IAW SRM 51-40-02. STRINGER FITTING REMOVED IAW SRM 51-40-02. REFER TO WC NRC 10 0-128 FOR FUSELAGE SKIN REPAIR WORK DETAILS (REF: LOG 0712137, ER/A 510085-14AD REV ORIGINAL DATED 16 JAN 2013). STRINGER FITTING INSTALLED IAW SRM 51-40-02. DRAG SPLICE FITTINGS INSTALLED IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE, FOUND ONE CRACK AT FRAME, LOWER ROW 2ND FASTENER HOLE FROM OTBD. FRAME R & R IAW SRM 51-40-02 BETWEEN S-4 AND S11R AND FAILSAFE REPAIR CARRIED OUT SRM 51-70-11, FIG 1.

Part: FITTING — CRACKED (BS 1000 BULKHEAD) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC OPEN HOLE ON BS 1000 BULKHEAD LOWER DRAG SPLICE FITTING ANGLES. REMOVED FASTENER HOLE AND FOUND CRACK 01EA AS MARK. BS 1000 BULKHEAD LOWER DRAG SPLICE FITTING REMOVED IAW SRM 51-40-02. NEW DRAG SPLICE FITTING HOLES PICKED UP IAW SRM 51-40-05. NEW DRAG SPLICE FITTING INSTALLED IAW SRM 51-40-02.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 8TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1220 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, MID ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE, FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187 TO 0.199" DIA IAW SB747-53A2507, REV 1.

Part: PLATE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB 747-53A2507, REV 1.

Part: PLATE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1220, TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, LOWER ROW 6TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507 REV1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142 PART 6 51-00-00 PROC16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.216" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FRAME, UPPER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 12TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW NDTM D6-7170, REV142, PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FRAME, UPPER ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB74 7-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.216" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FRAME, LOWER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" IAW SB747-53 A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1220 TENSION TIE FOUND ONE CRACK AT WEB, MID ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FRAME, LOWER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00, PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1200 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, LOWER ROW 2ND FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB747-5 3A2507 REV 1.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1180 TENSION TIE FOUND ONE CRACK AT WEB, UPPER ROW 1ST FASTENER HOLE FROM OTBD. REAMED FROM 0.278" TO 0.309" DIA IAW REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE FOUND 01 EA CRACK AT STEEL PLATE, LOWER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV1.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1220 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 9TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB747-53A2507, REV1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSP ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, LWR ROW 12TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.216" IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.247" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FRAME, UPPER ROW 3RD FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507 REV 1.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1220 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, MID ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1200 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FRAME, UPPER ROW 2ND FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB74 7-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 3RD FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.216" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 3RD FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FRAME, LOWER ROW 3RD FASTENER HOLE FROM OTBD. REAMED OVERSIZE FORM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, LOWER ROW 9TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.216" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 3RD FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, LOWER ROW 7TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.247" DIA IAW SB747-53A2507 REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 2ND FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT FRAME, LOWER ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FRAME, LWR ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSP ON RT SIDE BS 1120 TENSION TIE, FOUND ONE CRACK AT FRAME, UPPER ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 7TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.247" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LWR ROW 6TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 7TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.262" DIA IAW SB747-53A2507 REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.247" DIA SB747-53A2507, REV1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FRAME, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1180 TENSION TIE, FOUND ONE CRACK AT FWD CHANNEL, LOWER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.216" DIA IAW SB747-53A2507, REV 1.

Part: PLATE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE FOUND 01EA CRACK AT STEEL PLATE, UPPER ROW 2ND FASTENER HOLE FROM OTBD. REAMED FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV 1.

Part: STRINGER — CRACKED (BS 480 S10L) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC INSPECTION ON BS 480 S10L FOUND CRACK APPROX 0.7 IAW SB 747-53A2482, REV 1, FIG 18, STEP 2. STRINGER CUT IAW SB 747-53A2484, REV 1, FIG 18, STEP 4. TRIMMED STRINGER FOUND NO CRACK EVIDENT IAW SB 747-53A2484, REV 1, FIG 18, STEP 4. REPAIR INSTALLED IAW SB 747-53A2484, REV 1, FIG 18, STEP 5-21.

Part: CHANNEL — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT AFT CHANNEL, LOWER ROW 6TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB747-53A2507 REV 1.

Part: STRINGER — CRACKED (BS 500 S10R) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC INSPECTION ON BS 500, S10R FOUND CRACK APPROX 0.5. AS PER SB 747-5 3A2484, REV 1, FIG 26, STEP 2. STRINGER CUT IAW SB 747-53A 2484, REV 1, FIG 26, STEP 4. TRIMMED STRINGER FOUND NO CRACK EVIDENT IAW SB 747-53A2484, REV 1, FIG 26, STEP 4. REPAIR INSTALLED IAW SB 747-53A2484, REV 1, FIG 26, STE P 6-21.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE INSPECTION ON LT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, MID ROW 2ND FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170 REV 142 PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FRAME, LWR ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.278" DIA IAW SB747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: CHANNEL — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE, BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, LOWER ROW, 9TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 7TH FASTENER HOLE FROM O/B. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA AS PER B747-400 SB747-53A2507 REV 1.

Part: CHANNEL — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.247" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE INSPECTION ON LT SIDE BS 1140, TENSION TIE FOUND ONECRACK AT STEEL PLATE, UPPER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB747-53A2507 REV 1.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.262" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT LOWER FILLER, 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.262" DIA IAW SB 747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00, PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 8TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SV747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW DELTA NDTM D6-7170, REV 142, PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB747-53A2507 REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00, PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT FRAME, LWR ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.262" DIA IAW SB747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.247" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, LWR ROW 2ND FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB747-53A2507 REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.262" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, LWR ROW 6TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB747-53A2507, REV 1.

Part: STRINGER — CRACKED (BS 480 S8R) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC INSPECTION ON BS 480 S8R FOUND CRACK APPROX 0.5 IAW SB 747-53A2484, REV 1, FIG 12, STEP 2. STRINGER CUT IAW SB 747-53 A2484, REV 1, FIG 12, STEP 4. TRIMMED STRINGER FOUND NO CRACK EVIDENT IAW SB 747-53A2484, REV 1, FIG 12, STEP 4. REPAIR INSTALLED SB 747-53A2484, REV 1, FIG 12, STEP 5-21.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE INSPECTION ON LT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB747-53A2507 REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170 REV 142 PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

SHIP 6307 DURING OPEN HOLE INSPECTION ON LT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 10TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.278" DIA IAW SB747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00, PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE INSPECTION ON LT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.247" DIA IAW SB747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00, PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE INSPECTION ON LT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, LOWER ROW 3RD FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA SB747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 2ND FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.267" DIA IAW SB747-53A2507 REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142, PART 6 51-00-00, PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1160 TENSION TIE. FOUND ONE CRACK AT FRAME, LOWER ROW 3RD FASTENER HOLE FROM OTBD. REAMED & OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB747-53A2507, REV 1.

Part: PLATE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.262" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT AFT CHANNEL, UPPER ROW 12TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.278" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSP ON LT SIDE BS 1160 TENSION TIE, FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 9TH FASTENER HOLE FROM OTBD. REAMED & OVERSIZED FROM 0.216" TO 0.278" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1160 TENSION TIE, FOUND ONE CRACK AT FWD CHANNEL, LOWER ROW 11TH FASTENER HOLE FORM OTBD AS MARKED. REPAIRED, REAMED OVERSIZE FROM 0.216" TO 0.278" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 2ND FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1160 TENSION TIE. FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 12TH FASTENER HOLE FROM OTBD. REPAIRED, REAMED, & OVERSIZED FROM 0.216" TO 0.278" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FRAME, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB74 7-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT UPPER FILLER, 6TH FASTENER HOLE FROM OTBD, REPAIRED, OVERSIZED FROM 0.187" TO 0.199" DIA IAW SB747-53A 2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT FRAME, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REPAIRED, REAMED OVERSIZED FROM 0.216" TO 0.262" IAW SB747- 53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSP ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 9TH FASTENER HOLE FROM OTBD. REAMED, & OVERSIZED FROM 0.199" TO 0.216" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1120 TENSION TIE. FOUND ONE CRACK AT STEEL PLATE, LWR ROW 7TH FASTENER HOLE FROM OTBD. REPAIR, REAMED OVERSIZE FROM 0.187" TO 0.216" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSP ON RT SIDE BS 1140 TENSION TIE FOUND 01 EA CRACK AT FWD CHANNEL, LWR ROW 5TH FASTENER HOLE FORM OTBD. REPAIRED, REAMED, & OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSP ON LT SIDE BS 1140 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, LWR ROW 10TH FASTENER HOLE FROM OTBD. REPAIRED, REAMED, & OVERSIZED FROM 0.187" TO 0.199" DIA IAW B747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSP ON LT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, MID ROW 1ST FASTENER HOLE FROM OTBD. REPAIRED, REAMED, & OVERSIZED FROM 0.199" TO 0.216" DIA IAW SB747-53A2507, REV 1.

Part: STRINGER — CRACKED (BS 500 S10R) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC INSPECTION ON BS 500 S10R FOUND CRACK APPROX 0.5".

Part: STRINGER — CRACKED (BS 480 S10L) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC INSPECTION ON BS 480, S10L FOUND CRACK APPROX 0.7".

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW 8TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB 747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142. PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION FOUND ONE CRACK AT FWD CHANNEL , UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.247" DIA IAW SB 747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142. PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 3RD FASTTENER HOLE FROM OTBD. REAMED, & OVERSIZED FROM 0.199" TO 0.216" DIA IAW0 SB 747-53A2507 REV 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC INSPECTION, FOUND CRACK ON TENSION TIE. RT SIDE BS 1120, AFT CHANNEL UPPER RADIUS, FASTENER 13 AND 14. REPLACED FWD AND AFT TENSION TIE IAW SRM 53-40-30, REPAIR 1.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT FRAME UPPER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.247" DIA IAW SB 747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142. PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION TIE FOUND ONE CRACK AT FRAME, UPPER ROW 2ND FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB 747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142. PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC INSPECTION, FOUND CRACK ON TENSION TIE. LT SIDE BS 1120 FWD CHANNEL MID ROW, 2ND FASTENER. REPLACED FWD TENSION TIE IAW SRM 53-40-30, REPAIR 2.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION FOUND ONE CRACK AT FWD CHANNEL, LWR ROW 6TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB 747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142. PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1120 TENSION FOUND ONE CRACK AT FRAME, UPPER ROW 3RD FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA SB 747-53 A2507 REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170 REV 142. PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE, FOUND ONE CRACK AT FWD CHANNEL, LOWER ROW 13TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA SB 747-53A2507, REV 1.

Part: CHANNEL — CRACKED (BS 1160) · airframe 97,560 hrs · 11,953 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE, FOUND ONE CRACK AT FWD CHANNEL ,UPPER ROW SIXTH FASTENER HOLE FROM OTBD. TENSION TIE FWD & AFT CHANNEL R & R AND ESTABLISHED MONITORING IAW SRM 53-40-30 REPAIR 1 PAGE 214.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LWR ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, LOWER ROW 4TH FASTENER HOLE FROM OTBD. REPAIRED IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSP ON LT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL,UPPER ROW 7TH FASTENER HOLE FROM O/B. REPAIR, REAMED OVERSIZE FROM 0.199" TO 0.247" DIA AS PER SB747-53A2507 REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE, FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW, 9TH FASTENER HOLE FROM OTBD, REAM OVERSIZE FROM 0.187" TO 0.216" DIA IAW B747-53A25 07, REV 1.

Part: CHANNEL — CRACKED (BS 1160) · airframe 97,560 hrs · 11,953 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, LOWER ROW FIFTH FASTENER HOLE FROM OTBD. TENSION TIE FWD CHANNEL R & R AND ESTABLISHED MONITORING IAW SRM 53-40-30. REPAIR 2 PAGE 214.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 97,543 hrs · 11,950 cycles

PERFORMED OPEN HOLE HFEC INSPECTION ON NR 3 RT MAIN ENTRY DOORWAY UPPER AFT CORNER FASTENER HOLES, FOUND ONE CRACK ON BEARSTRAP AT 2ND HOLE OF 2ND ROW FROM BELOW DOUBLER AREA CLASSIFIED AS 'LARGE'. REPAIRED IAW PRI 509724-14AD REV 0,1,3,5 DATED 09 JAN 20 13 19:14. PRI 509724-14AD, REV 0,1,3,5 COMPARED WITH ERA 509724-14, REV O FOUND IN COMPLIANCE.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE, BS 1160 TENSION TIE FOUND ONE CRACK AT FWD CHANNEL, LWR ROW 10TH FASTENER HOLE FROM OTBD AS MARKED. REPAIR, REAMED OVERSIZE IAW SB747-53A2507, REV 1.

Part: SKIN — CRACKED (FUSLAGE) · airframe 97,543 hrs · 11,950 cycles

PERFORMED OPEN HOLE HFEC INSPECTION ON NR 3, RT MAIN ENTRY DOORWAY UPPER AFT CORNER REP & MOD: SECTION 02D FASTENER HOLES FOUND ONE CRACK ON BEARSTRAP AND 01EA CRACK ON SKIN AT 4TH HOLE FROM FWD OF 3RD ROW FROM BELOW DOUBLER AREA CLASSIFIED AS 'LARGE'. NR 3, RT MAIN ENTRY DOORWAY UPPER AFT CORNER FASTENER HOLES ONE CRACK ON BEARSTRAP AND ONE CRACK ON SKIN AT 4TH HOLE FROM FWD OF 3RD ROW FROM BELOW DOUBLER ARE REPAIRED IAW PRI509725-14AD, REV 0,1,3.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.216" DIA SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1160) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1160 TENSION TIE, FOUND ONE CRACK AT FWD CHANNEL, LWR ROW 7TH FASTENER HOLE FROM OTBD REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB 747-53A2507, REV 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,543 hrs · 11,950 cycles

PERFORMED SURFACE HFEC ON NR 3 LT MAIN ENTRY DOORWAY UPPER AFT CORNER REP & MOD: SECTION 02B, IDENTIFIED SIX CRACKS ON SKIN EDGE. NR 3 LT MAIN ENTRY DOORWAY UPPER AFT CORNER 06 EA CRACKS ON SKIN EDGE CLASSIFIED AS "SMALL" TRIMMED OFF AND AN INSURANCE CUT ON REWORK AREA CARRIED OUT IAW SB 747-53A2512, REV 1, FIG 22, SA 533-01209-20.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,543 hrs · 11,950 cycles

PERFORMED OPEN HOLE HFEC ON NR 3 LT MAIN ENTRY DOORWAY UPPER AFT CORNER, FOUND ONE CRACK ON SKIN 9TH HOLE OF 1ST ROW FROM BELOW DOUBLER AREA CLASSIFIED AS "MEDIUM". NR 3 LT MAIN ENTRY DOORWAY UPPER AFT CORNER ONE CRACK ON SKIN 9TH HOLE OF 1ST ROW FROM BELOW DOUBLER AREA REPAIRED IAW PRI 509 723-14AD, REV 0,1,2,3.

Part: FAILSAFE — CRACKED (BS 1180) · airframe 97,560 hrs · 11,953 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1180 TENSION TIE, FOUND ONE CRACK AT FAIL SAFE CHORD, UPPER ROW 1ST FASTENER HOLE FROM OTBD. REPAIR CARRIED OUT IAW SRM 53-40-07, FIG 201, REPAIR 4. FAILSAFE REPAIR CARRIED OUT IAW SRM 51-70-11, FIG 1, STEEL PLATE R & R IAW SRM 51-40-02 AND 'C' CHANNEL FWD AND AFT SEGMENT. R & R AND ESTABLISHED MONITORING ON 'C'CHANNEL SECTION SRM 53-40-30 REPAIR 1, PAGE 214.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 2ND FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199' TO 0.216" DIA IAW SB 747-53A2507, REV 1.

Part: PLATE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 5TH FASTENER, HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA AS IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 9TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA SB 747-53A2507, REV 1.

Part: PLATE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 3RD FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB 747-53A2507, REV 1.

Part: SHEAR WEB — CRACKED (BS 1140) · airframe 97,560 hrs · 11,953 cycles

DURING HFEC SURFACE INSPECTION ON TENSION TIE, RT SIDE, BS 1140 FWD CHANNEL TO WEB , 3RD FASTENER FROM INBD FOUND CRACK AS MARKED. RT SIDE, BS 1140 TENSION TIE SHEAR WEB REPAIR CARRIED OUT IAW SRM 53-40-30, FIG 201, REPAIR 4, AND ESTABLISHED MONITORING IAW SRM 53-40-30. REPAIR 4, PAGE 207.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT FWD CHANNEL , LOWER ROW 6TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB 747-53A2507, REV 1.

Part: PLATE — CRACKED (BS 1180) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSP ON RT SIDE BS 1180 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LWR ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.247" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 10TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB 747-53A2507, REV 1 .

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 97,543 hrs · 11,950 cycles

PERFORMED OPEN HOLE HFEC ON NR 3 LT MAIN ENTRY DOORWAY UPPER AFT CORNER REP & MOD: SECTION 02B FASTENER HOLES FOUND 01EA CRACK ON BEAR STRAP 1ST HOLE OF 2ND ROW FROM BELOW DOUBLER AREA CLASSIFIED AS "LARGE" AS MARKED. NR 3 LT MAIN ENTRY DOORWAY UPPER AFT CORNER FASTENER HOLE 01EA CRACK ON BEARSTRAP 1ST HOLE OF 2ND ROW FROM BELOW DOUBLER AREA REPAIRED IAW PRI509723-14AD, REV 0,1,2,3,5 DATED 11 JAN 2013 21:39 . PRI 509723-14AD REV 0,1,2,3,5 COMPARED WITH ERA 509723-14AD REV O, FOUND IN COMPLIANCE.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 9TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507, REV 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,543 hrs · 11,950 cycles

PERFORMED OPEN HOLE HFEC ON NR 3 LT MAIN ENTRY DOORWAY UPPER AFT CORNER REP & MOD : SECTION 02B FASTENER HOLES FOUND 01EA CRACK ON SKIN 7TH HOLE OF 1ST ROW FROM BELOW DOUBLER AREA CLASSIFIED AS "MEDIUM" AS MARKED. NR 3 LT MAIN ENTRY DOORWAY UPPER AFT CORNER FASTENER HOLES 01EA CRACK ON SKIN 7TH HOLE OF 1ST ROW FROM BELOW DOUBLER AREA REPAIRED IAW PRI 509723-14AD, REV 0,1,3,5 DATED 11 JAN 2013 21:37. PRI 509723-14AD REV 0,1,3,5 COMPARED WITH ERA 509723-14AD, REV O FOUND IN COMPLIANCE.

Part: CHANNEL — CRACKED (BS 1200) · airframe 97,560 hrs · 11,953 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW FIFTH FASTENER HOLE FROM OTBD. TENSION TIE FWD CHANNEL R & R AND ESTABLISHED MONITORING IAW SRM 53-40-30, REPAIR 2 PAGE 214.

Part: CHANNEL — CRACKED (BS 1140) · airframe 97,560 hrs · 11,953 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1140 TENSION TIE, FOUND ONE CRACK AT FWD CHANNEL, UPPER ROW FIRST FASTENER HOLE FROM OTBD. TENSION TIE FWD CHANNEL R & R AND ESTABLISHED MONITORING IAW SRM 53-40-30 REPAIR 2 PAGE 214 .

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 6TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB 747-53A2507, REV 1.

Part: PLATE — CRACKED (BS 1180) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1180 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 8TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA SB 747-53A2507 REV 1.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 7TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB 747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142. PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE,UPPER ROW 6TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB747-53A2507 REV 1.NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142. PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 8TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA SB 747-53A2507, REV 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,543 hrs · 11,950 cycles

PERFORMED OPEN HOLE HFEC ON NR 3 LT MAIN ENTRY DOORWAY, UPPER AFT CORNER, FASTENER HOLES FOUND ONE CRACK ON SKIN 17TH HOLE OF 1ST ROW FROM BELOW DOUBLER AREA CLASSIFIED AS "MEDIUM" AS MARKED. NR 3 LT MAIN ENTRY DOORWAY UPPER AFT CORNER FASTENER HOLES 01EA CRACK ON SKIN 17TH HOLE OF 1ST ROW FROM BELOW DOUBLER AREA REPAIRED IAW PRI 509723-14 REV 0,1,3,5 DATED 11 JAN 2013 21:37. PRI 509723-14 REV 0,1,3,5 COMPARED WITH ERA 509723-14AD REV O, FOUND IN COMPLIANCE.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB 747-53A2507, REV 1.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 97,543 hrs · 11,950 cycles

PERFORMED OPEN HOLE HFEC ON NR 3 RT MAIN ENTRY DOORWAY UPPER AFT CORNER REP & MOD: SECTION 02D FASTENER HOLES FOUND 01EA CRACK ON BEAR STRAP 9TH HOLE OF 1ST ROW FROM BELOW DOUBLER AREA CLASSIFIED AS "MEDIUM" AS MARKED. NR 3 RT MAIN ENTRY DOORWAY UPPER AFT CORNER FASTENER HOLES 01EA CRACK ON BEAR STRAP 9TH HOLE OF 1ST ROW FROM BELOW DOUBLER AREA REPAIRED IAW PRI509724-14AD REV 0,1,3,5 DATED 09 JAN 2013 19:11.P RI 509724-14AD REV 0,1,3,5 COMPARED WITH ERA509724-14AD REV O FOUND IN COMPLIANCE.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 4TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSP ON LT SIDE BS 1200 TENSION TIE FOUND 01EA CRACK AT STEEL PLATE, MID ROW 2ND FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB 747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142. PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, LWR ROW 7TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB 747-53A2507 REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142. PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1180 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 7TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB 747-53A2507 REV 1.NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170, REV 142. PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1200 TENSION TIE FOUND ONE CRACK AT STEEL PLATE, MID ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB 747-53A2507 REV 1. NDT OPEN HOLE INSPECTION CARRIED OUT IAW NDTM D6-7170 REV 142. PART 6 51-00-00 PROC 16 AND FOUND NO CRACK EVIDENT.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1180 TENSION TIE FOUND ONE CRACK AT AFT CHANNEL, LOWER ROW 8TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA IAW SB 747-53A2507, REV 1. NDT OPEN HOLE INSPECTION CARRIED IAW NDTM D6-7170, REV 142. PART 6 51-00-00, PROC 16 AND FOUND NO CRACK EVIDENT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 97,543 hrs · 11,950 cycles

PERFORMED SURFACE HFEC ON NR 3 RT MAIN ENTRY DOORWAY UPPER AFT CORNER SECTION, IDENTIFIED ONE CRACK ON SKIN EDGE CLASSIFIED AS 'SMALL'. REPAIRED IAW PRI 509724-14AD, REV 2, 3.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1220 TENSION TIE, FOUND ONE CRACK AT AFT CHANNEL, UPPER ROW 6TH FASTENER HOLE FROM OTBD AFTER FRAME. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB 74 7-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON LT SIDE BS 1220 TENSION TIE, FOUND ONE CRACK AT WEB, UPPER ROW 5TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.199" DIA SB 747- 53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC INSPECTION, FOUND CRACK ON TENSION TIE. LT SIDE BS 1220 FWD CHANNEL LOWER ROW, 1ST FASTENER. REPLACED FWD TENSION TIE, IAW SRM 53-40-30, REPAIR 2.

Part: PLATE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1220 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 3RD FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1220 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 6TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1220 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 6TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.187" TO 0.216" DIA IAW SB747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1220 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 7TH FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.199" TO 0.216" DIA IAW SB 747-53A2507, REV 1.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1220 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, LOWER ROW 1ST FASTENER HOLE FROM OTBD. REAMED OVERSIZE FROM 0.216" TO 0.247 " DIA SB 747-53A2507, REV 1.

Part: PLATE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION ON RT SIDE BS 1220 TENSION TIE, FOUND ONE CRACK AT STEEL PLATE, UPPER ROW 5TH FASTENER HOLE FROM OTBD. STEEL PLATE REMOVED IAW SRM 51-40-02 AND FABRICATED IAW DWG 65B09631, REV AG AND INSTALLED SRM 51-40-02.

Part: TENSION TIE — CRACKED (BS 1220) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC INSPECTION ON RT SIDE BS 1220 TENSION TIE FOUND CRACK IN FASTENER HOLE. LOWER ROW 6TH HOLE FROM OTBD. TENSION TIE FWD AND AFT R & R IAW SRM 53-40-30, REPAIR 1.

Part: SKIN — CRACKED (BS 2521) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK AT ON FUSELAGE SKIN TO VERTICAL STAB UPPER LOBE DOUBLER RT AT BS 2521. CRACK LENGTH OF APPROX. 1 INCH. REPAIRED IAW PRI 509709-14AD REV 0, 1, 2, 3. PRI 5090709-14AD REV 0, 1, 2, 3 COMPARED WITH ERA 509709-14AD, REV 0 AND REFER SB 747-53A2651, REV 1, FOUND IN COMPLIANCE.

Part: SKIN — CRACKED (BS 2521) · airframe 97,543 hrs · 11,950 cycles

DURING HFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK AT SKIN TO VERTICAL STAB UPPER LOBE DOUBLER LT SIDE AT BS 2521 WITH CRACK LENGTH OF APPROX 0.5". REPAIRED IAW PR I509709-14AD REV 0, 1, 2, 3. PRI 509709-14AD REV 0, 1, 2, 3, COMPARED WITH ERA 509709-14AD REV 0 AND REFER SB 747-53A2651, REV 1 FOUND IN COMPLIANCE.

Part: FRAME — CRACKED (BS 1265) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE INSPECTION AT BS 1265 LT FRAME INNER CHORD AND WEB FOUND CRACK INDICATION AT THE FASTENER HOLE 4TH LAYER , 3 O`CLOCK DIRECTION VIEW FROM AFT AS MARKED. BS 1265 LT FRAME INNER CHORD AND WEB FOUND CRACK AT 4TH LAYER ,3 O'CLOCK DIRECTION REPAIRED IAW PRI 509705-14AD, REV 0, 1, 2 DATED 27, DEC 2012 11:48. PRI 509705-14AD REV 0,1,2 COMPARED WITH ER/A 509705-14AD REV 0, FOUND IN COMPLIANCE.

Part: FRAME — CRACKED (BS 1265) · airframe 97,543 hrs · 11,950 cycles

DURING OPEN HOLE HFEC INSPECTION AT BS 1265 RT FRAME INNER CHORD AND WEB FOUND CRACK INDICATION AT THE FASTENER HOLE 4TH LAYE R 9 O'CLOCK DIRECTION VIEW FROM AFT. BS 1265 RT FRAME INNER CHORD AND WEB FOUND CRACK AT 4TH LAYER 9 O`CLOCK DIRECTION REPAIRED IAW PRI 509705-14AD, REV 0,1,2,3 DATED 14 JAN 2013 20:04. PRI 509705-14 AD, REV 0, 1, 2, 3 COMPARED WITH ERA 509705-14AD, REV 0 FOUND IN COMPLIANCE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 96,562 hrs · 11,831 cycles

LEFT OUTSIDE EMERGENCY LIGHTS 1ST AND 2ND FROM FWD INOPERATIVE. REPLACED POWER SUPPLY AT DOOR 3L. OPS CHECKED GOOD IAW AMM 33-51

Part: LIGHT — INOPERATIVE (CABIN) · airframe 96,394 hrs · 11,811 cycles

DURING INSPECTION, FOUND L2 DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED DOOR SLIDE LIGHT AT 2L PER AMM 33-51.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 96,305 hrs · 11,801 cycles

DURING INSPECTION FOUND RIGHT OVERWING ESCAPE SLIDE LIGHT ASSEMBLY AT 1ST AND 2ND FROM BOTTOM INOPERATIVE. MAINTENANCE REPLACED FUSE AT POWER SUPPLY. OPERATIONAL CHECKED NORMAL PER AMM 33-52.

Part: ANGLE — CRACKED (BS 505) · airframe 95,992 hrs · 11,758 cycles

DURING INSPECTION, FOUND MAIN DECK CABIN ZONE B, RIGHT FLOOR AREA AT STATION 505 RIGHT, RBL 66.00 INTERCOSTAL ATTACHED UPPER ANGLE CRACKED. MAINTENANCE FABRICATED AND REPLACED UPPER ANGLE AS PER B747-400 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (BS 580) · airframe 95,992 hrs · 11,758 cycles

DURING INSPECTION, FOUND MAIN DECK CABIN ZONE B LEFT SIDE FLOOR AREA, AT BS 580 LT ALONG LBL 91.67 INTERCOSTAL FLANGE CORRODED. MAINTENANCE REMOVED DAMAGED INTERCOSTAL, FABRICATED AND REPLACED NEW INTERCOSTAL AS PER ERA 503518-14.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 95,985 hrs · 11,756 cycles

DURING INSPECTION FOUND LEFT OVERWING FORWARD PAIR OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED FUSE OF POWER SUPPLY AT DOOR 3L. OPERATIONAL CHECK OK PER AMM 747-400-33-51-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,780 hrs · 11,731 cycles

DURING INSPECTION FOUND FLOOR EMERGENCY PATH LIGHTS OUT. MAINTENANCE REPLACED LIGHT ASSEMBLY, OPS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 95,780 hrs · 11,731 cycles

DURING INSPECTION FOUND 2 LEFT FORWARD OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY (M7919) AND TESTED OK PER B747 AMM 33-51-04/201. AIRCRAFT OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 95,331 hrs · 11,674 cycles

DURING INSPECTION FOUR LEFT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY PER AMM 33-51. OPERATIONAL CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 93,101 hrs · 11,414 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY FLOOR PROXIMITY LIGHT AT 43ABC WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE POWER SUPPLY AT FAULT AND REPLACED IT. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 5,605 hrs · 683 cycles

DURING A LINE CHECK, MAINTENANCE FOUND THE LEFT 1ST AND 2ND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD.

Part: FUSE — OPEN (POWER SUPPLY) · airframe 90,735 hrs · 11,132 cycles

DURING A MAINTENANCE VISIT, 2 OF 4 RIGHT OVERWING ESCAPE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE POWER SUPPLY F3 FUSE OPEN AND REPLACED IT. SYSTEM OPERATION WAS NORMAL AFTER THE FUSE WAS REPLACED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,631 hrs · 11,120 cycles

DURING A LINE CHECK, MX FOUND THE EMERGENCY EXIT SIGN AT DOOR 3L INOPERATIVE. MX REPLACED THE POWER SUPPLY. OPS CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,631 hrs · 11,120 cycles

DURING A LINE CHECK, MX FOUND THE LT FWD 2 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MX REPLACED THE POWER SUPPLY. OPS CHECK WAS GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 90,503 hrs · 11,106 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY FLOOR LIGHTS AT ROW 51 THROUGH 58 WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTOR AND SECURED IT. SYSTEM OPERATION WAS NORMAL. THE CONNECTOR WAS SECURED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 90,243 hrs · 11,073 cycles

MAINTENANCE VISIT THE OVERWING RIGHT EMERGENCY LIGHTS L1870 AND L1165 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY M7920. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.

Part: STRUCTURE — CORRODED (BS 1000 S46-47L) · corrosion level 2 · airframe 89,404 hrs · 10,968 cycles

DURING L-CHECK FOUND FWD CARGO COMPARTMENT BS 1000 LOWER CHORD S46L-S47L FOUND CORROSION. REPLACED IAW EM 5312-01106-02.

Part: SKIN — DELAMINATED (NR2 SPOILER) · airframe 89,404 hrs · 10,968 cycles

DURING L-CHECK, FOUND LT WING - NR2 SPOILER TOP SKIN DELAMINATED IN T/E OTBD SECTION AS MARKED. SPOILER SKIN WAS REPAIRED IAW SRM 51-07-10, REPAIR 4, FIG 202, DETAIL REFER HX PROCESS CARD FDG503802-1. NR2 SPOILER WAS R & R FOR ACCESS IAW AMM 27-81-02. SPOILER RIGGING AND OPS CHECK CARRIED OUT IAW AMM 27-61-00.

Part: ATTACH ANGLE — CRACKED (BS 460) · airframe 89,404 hrs · 10,968 cycles

DURING L-CHECK, FOUND BS460 STR 16R FRAME ATTACH ANGLE FOUND CRACKED, SECTION 01B & DWG 141U1005 AND SRM 51-40-02.

Part: SILL — CRACKED (BS 460 S16R) · airframe 89,404 hrs · 10,968 cycles

BS 460, STR 16R DOOR CUTOUT UPPER SILL WEB LOWER FACE FOUND CRACKED. REPAIRED IAW ERA 461688-14 AD SECTION I. SECTION II REQUIRES REPEAT INSP IAW SB 747-53A2785, REV 01/ EO5316-01039 AT 12000 ACFT CYCLES AND 6000 CYCLE INTERVALS SECTION III REQUIRES REPEAT INSP IAW SB 747-53A2500, REV 01/ EM 5300-01049 AT 22,000 ACFT CYCLES, THEN AT 3000 CYCLES INTERVALS.

Part: SILL — CORRODED (BS 560) · corrosion level 2 · airframe 89,404 hrs · 10,968 cycles

DURING L-CHECK FOUND FWD CARGO DOOR SILL STA 560 CORNER AREA FOUND CORROSION. FWD CARGO DOOR SILL STA 560 CLIP REPLACED IAW SRM 51-10-02 & DWG 65B07170 AND INSTALLED IAW SRM51-40-02.

Part: WEDGE — DELAMINATED (RT WING TE FLAP) · airframe 89,404 hrs · 10,968 cycles

DURING L-CHECK, FOUND RT INBD T/E MID FLAP AFT WEDGE UPPER SURFACE DELAMINATED JUST OTBD OF NR 5 FLAP TRACK AREA AS MARKED. REPAIRED IAW SRM 51-70-07 PARA 5A, FIG 5.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 88,566 hrs · 10,864 cycles

DURING A LINE CHECK, MX FOUND THE EMERGENCY PATH LIGHTS AT DOOR 3R AND SEAT 43KJH INOPERATIVE. MX REPAIRED THE PATH LIGHT WIRING AT SEAT 43KJH. LIGHTS OPERATIONALLY CHECK GOOD.

Part: INTERFACE UNIT — MALFUNCTIONED (EFIS/EICAS) · airframe 87,227 hrs · 10,700 cycles

AFTER TAKEOFF, FLIGHT CREW RECEIVED MUTABLE MESSAGES ON UPPER EICAS: CABIN ALT AUTO, HYD CONTROL 4, PACK 1, PACK 2, PACK 3, FUEL TEMP, FUEL JETT B, WINDSHEAR, GRD PROX SYS, ALT CALLOUTS APPEARED. EICAS CROSSFEED VALVE INDICATIONS AND FUEL FLOW PICTORIALS ALSO ABSENT. DIVERTED FOR MX. MX REPLACED THE EFIS/EICAS INTERFACE UNIT. ALL MESSAGES CLEARED. RAN ENGINES AND ALL OPERATIONS/INDICATIONS WERE NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 86,801 hrs · 10,647 cycles

DURING LAYOVER CHECK, MX FOUND EMERGENCY PATH LIGHTS BY DOOR 2L INOPERATIVE. MX REPLACED A RECEPTACLE AND REPAIRED WIRING. OPS CHECK WAS GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 86,660 hrs · 10,631 cycles

DURING LAYOVER CHECK, MX FOUND THE EMERGENCY PATH LIGHTS AT LAV DR2L INOPERATIVE. MX SECURED LOOSE CONNECTION. OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,276 hrs · 10,587 cycles

DURING LAYOVER CHECK, MX FOUND UPPER DECK RT EMERGENCY EXIT DOOR SIGN INOPERATIVE. MX REPLACED THE POWER SUPPLY BATTERY. OPS CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,253 hrs · 10,585 cycles

DURING LAYOVER CHECK, MX FOUND 2 RT OVERWING EMERGENCY LIGHTS INOPERATIVE. MX REPLACED THE POWER SUPPLY. OPS CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,780 hrs · 10,157 cycles

DURING OVERNIGHT CHECK FOUND EMERGENCY LIGHT INOP AT INSIDE OF RIGHT UPPER DECK DOOR. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,048 hrs · 9,531 cycles

DURING OVERNIGHT CHECK, FOUND UPPER DECK FORWARD EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY M335 AND BATTERY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — MISINSTALLED (BS 2040-2060) · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK, DURING ACCOMPLISHMENT OF DOOR 5 CREW REST MODIFICATION PER SB 747-53-2481 FOUND NEW FITTING AT BS 2040-2060 S11R-S12R WITH INSUFFICIENT EDGE MARGIN. REPAIRED PER EA 63-211300.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK, FOUND CRACK IN SKIN FASTENER HOLES AND SHORT EDGE MARGIN ON FRAME AT BS 460 BETWEEN S14 AND S16. REPAIRED PER EA 63-211348.

Part: SHEAR WEB — CRACKED (BS 1120) · airframe 75,742 hrs · 9,239 cycles

DURING "M" CHECK, FOUND CRACK IN TENSION TIE AREA GUSSET AND SHEAR WEB AT BS 1120. REPAIRED PER EA 63-211013.

Part: FRAME — CRACKED (BS 1180) · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK, FOUND 3 HOLES WITH CRACKS AT BS 1180 FRAME TENSION TIE AREA. REPAIRED PER EA 63-211310.

Part: SILL — CORRODED (BS 1990) · corrosion level 2 · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK, FOUND CORROSION THE UNDERSIDE OF OUTBOARD FLANGE OF BULK CARGO LOWER MAIN SILL CHORD AT BS 1990. REPAIRED PER EA 63-211345.

Part: INTERCOSTAL — CORRODED (BS 1940) · corrosion level 2 · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK, FOUND CORROSION IN BULK CARGO SIDEWALL PANEL INTERCOSTAL AT BS 1940. REPAIRED PER EA 63-211343.

Part: STRINGER — CRACKED (BS 500 S10L) · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK WHILE ACCOMPLISHING BS 747-53A2484, FOUND CRACK IN STRINGER 10L AT BS 500. REPAIRED PER EA 63-211355.

Part: ANGLE — CRACKED (BS 480 S10R) · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK WHILE ACCOMPLISHING SB 747-53A2484, FOUND CRACK IN ANGLE AT BS 480 S10R. REPAIRED PER EA 63-211354.

Part: SKIN — CRACKED (BS 1480) · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK WHILE ACCOMPLISHING SB 747-53A2390, FOUND CRACK IN LEFT SKIN PANEL LAYER AT BS 1480 HOLE NR 11. REPAIRED PER EA 63-211311.

Part: FRAME — CRACKED (BS 1140 S10R) · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK, FOUND 3 HOLES WITH CRACK INDICATIONS ON FRAME AND CRACKED FRAME WEB DOUBLER AT BS 1140 S10R TENSION TIE AREA. REPAIRED PER EA 63-211005.

Part: FRAME — CRACKED (BS 1160) · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK, FOUND 5 HOLES WITH CRACKS AT BS 1160 FRAME TENSION TIE AREA. REPAIRED PER EA 63-211309.

Part: SKIN — CRACKED (BS 1816 S26R) · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK, FOUND CRACK IN FUSELAGE SKIN AND FASTENER HOLE LOCATIONS WITH SHORT EDGE MARGIN AT UPPER FORWARD CORNER OF AFT CARGO DOOR CUTOUT AT BS 1816 S26R. REPAIRED PER EA 63-211303.

Part: FLOORBEAM — WORN (BS 940) · airframe 76,610 hrs · 9,342 cycles

DURING "M" CHECK, FOUND UPPER DECK FLOORBEAM WEB EDGE WORN AT BS 940 RBL 30. REPAIRED PER EA 63-211312.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY EXIT) · airframe 76,211 hrs · 9,289 cycles

DURING LINE CHECK, FOUND UPPER DECK RT EMERGENCY DOOR BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK PER AMM 52-23-14. OPS CHECKS GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 75,968 hrs · 9,256 cycles

DURING OVERNIGHT CHECK, FLOOR PROXIMITY EMERGENCY LIGHTS WILL NOT TURN ON. MAINTENANCE SECURED CONNECTORS. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — NO TEST (EMERGENCY LIGHT)

DURING LINE CHECK UPPER DECK LT EMERGENCY DOOR BATTERY TEST FAILED. REPLACED BATTERY PACK PER AMM 52-23-14 AND TESTED OK. Â

Part: SKIN — CORRODED (BS 2090) · corrosion level 2 · airframe 68,951 hrs · 8,339 cycles

DURING L-CHECK FOUND CORROSION ON RT FUSELAGE SKIN AT BS 2090 AT LAV VACUUM VENT HOSE OUTLET. REPAIRED PER EA 63-206472 SECTION I. PERMANENT REPAIR WILL BE ACCOMPLISHED DURING NEXT L-CHECK PER EA 63-206472 SECTION II.

Part: BLADES — BIRD STRIKE (COMPRESSOR) · airframe 64,662 hrs · 7,770 cycles

DURING CLIMB, THE NR 2 ENGINE INGESTED A BIRD. AFTER THE BIRDSTRIKE, THE ENGINE HAD NOTICEABLE VIBRATION. THE ENGINE WAS SHUT DOWN, FUEL WAS DUMPED, AND THE AIRCRAFT RETURNED TO JFK. THE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED EIGHT PAIRS OF FAN BLADES AND REPAIRED DAMAGE TO THE FAN ACOUSTIC LINER AND A FAN EXIT GUIDE VANE. AN ENGINE RUN WAS THEN ACCOMPLISHED WITH NORMAL INDICATIONS.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 59,886 hrs · 7,184 cycles

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51AB-62AB. RECONNECTED WIRE AT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: OVEN — ODOR (1B GALLEY) · airframe 59,559 hrs · 7,144 cycles

DURING FLIGHT, A SMOKE ODOR EMITTED FROM THE RIGHT OVEN IN GALLEY 1B. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN AND THE OVEN CONTROL CIRCUIT BREAKER. OPERATIONAL CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 57,900 hrs · 6,941 cycles

DURING LINE CHECK, FOUND LT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROW 1-14. REPAIRED WIRING. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,304 hrs · 6,483 cycles

DURING LINE CHECK FOUND LEFT (C) ZONE FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,426 hrs · 5,875 cycles

DURING "H" CHECK FOUND CORROSION ON FLOOR SUPPORT BETWEEN BS 510-520 LBL 41.5. REPAIRED PER EA 63-186876.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,426 hrs · 5,875 cycles

DURING "H" CHECK FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 920 RBL 51. REPAIRED PER EA 63-186690.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,295 hrs · 5,734 cycles

DURING LINE CHECK (PEK), FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN SEAT ROWS 16L-18L. REPAIRED LIGHTING. OPERATIONAL CHECK NORMAL.

Part: WIRE — DISCONNECTED (CABIN) · airframe 48,127 hrs · 5,717 cycles

DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT LAV DOOR 4L, LAV DOOR 2L, AND ROW 10AB. RECONNECTED WIRING AT SEAT 10AB LIGHT ASSEMBLY AND LAV DOOR 4L. OPERATIONAL CHECK NORMAL.

Part: SKIN — CRACKED · airframe 47,338 hrs · 5,621 cycles

During line check found crack in skin on the lower aft corner of cutout for number one pylon access panel 452ER . Repaired per EA 63-184047.

Part: WIRE — LOOSE (CABIN) · airframe 45,985 hrs · 5,452 cycles

DURING OVERNIGHT LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN ROWS 31-43. MAINTENANCE RECONNECTED LOOSE WIRE. OPERATIONAL CHECK NORMAL.

Part: WIRE — DISCONNECTED (CABIN) · airframe 45,827 hrs · 5,432 cycles

DURING LINE CHECK, MAINTENANCE FOUND NUMEROUS FLOOR MOUNTED EMERGENCY LIGHTS INOPERATIVE. RECONNECTED WIRING. OPERATIONAL TEST NORMAL.

Part: LIGHT — INOPERATIVE (ROW 22-43)

DURING LINE CHECK (PEK), FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 22-43. RECONNECTED LIGHTS, OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (CABIN)

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 40 TO 43. REPAIRED WIRING, OPERATIONAL CHECK GOOD.

Part: WIRE — FAILED (CABIN)

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 2AB TO 4AB. REPAIRED WIRING, OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (CABIN)

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 31ABC TO 43ABC. REPAIRED BROKEN WIRE, OPERATIONAL CHECK GOOD.

Part: PSEU — LOOSE (LANDING GEAR)

DURING APPROACH, EICAS MESSAGE GEAR DISAGREE APPEARED. RECYCLED THE LANDING GEAR AND THE MESSAGE DID NOT REAPPEAR. AIRCRAFT LANDED WITHOUT INCIDENT. RESEATED THE PROXIMITY SWITCH ELECTRONIC UNIT. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK, FOUND LEFT FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROWS 35 TO 43. RECONNECTED LIGHT ASSEMBLY AT ROW 43, OPERATIONAL CHECK GOOD.

Part: PANEL — SEPARATED (LT WING)

JUST AFTER TAKEOFF, THE UPPER OUTBOARD NACELLE ACCESS PANEL ABOVE THE NR 1 ENGINE SEPARATED 521 FT. NO CONTROL PROBLEMS WERE NOTED. DUMPED 213,000 LBS OF FUEL AND DIVERTED TO MSP WITHOUT FURTHER INCIDENT. REPLACED PANEL (P/N 65814964-39).

Part: WIRE — LOOSE (CABIN)

DURING LINE CHECK, FOUND FIRST CLASS LEFT EMERGENCY FLOOR LIGHTS INOPERATIVE. RECONNECTED WIRES, OPERATIONAL CHECK OK.

Part: FLOOR BEAM — CORRODED (FS 980)

DURING P-CHECK, FOUND CORROSION ON THE UPPER DECK FLOOR BEAM UPPER CHORD AT BS 980, RBL 20 TO RBL 30. REPAIRED BEAM (P/N 65B25643-4) PER EA 63-101956.

Part: WIRE — LOOSE (CABIN)

DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHTS INOPERATIVE ON THE LEFT SIDE FROM ROWS 51 TO 55. RECONNECTED WIRE AND OPERATIONAL CHECK GOOD.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING LINE CHECK, THE FLOOR MOUNTED EMERGENCY PATH LIGHTS AT DOOR 2L AND SEAT ROW 21L WERE FOUND INOPERATIVE. REPLACED THE FLOOR MOUNTED EMERGENCY LIGHT ASSEMBLY AT ROW 21L AND OPERATIONAL CHECK OK.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK, THE FLOOR MOUNTED EMERGENCY PATH LIGHTS BETWEEN SEAT ROWS 52L TO 58L WERE FOUND INOPERATIVE. RECONNECTED LIGHT PIN IN FLOOR TRACK. OPERATIONAL CHECK OK.

Part: PINS — LOOSE (CABIN)

DURING LINE CHECK, THE FLOOR PATH EMERGENCY LIGHT BETWEEN SEAT ROWS 26L AND 31L AND 53L TO 58L WERE FOUND INOPERATIVE. RECONNECTED SEAT PINS IN FLOOR TRACK AT ROWS 26L AND 58L, OPERATIONAL CHECK OK.