N755SA

Part: NONE — CRACKED (LH HOR STAB) · airframe 77,677 hrs · 45,975 cycles

LEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED. / [01] R&R LEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDER PER AMM 53-31-31-401 CONFIG 2-NG.

Part: BATTERY PACK — INOPERATIVE (L1 DOOR) · airframe 77,647 hrs · 45,956 cycles

CUSTOMER REQUEST: L-1 DOOR UPPER EMERGENCY EXIT SIGN INOPERATIVE / [01] REMOVED AND REPLACED M1674 EMERGENCY BATTERY PACK ON TTG8Q 00F9CTY. L-1 DOOR EMERGENCY EXIT SIGN TEST NORMAL PER AMM33-51-00-710-801.;[02] VERIFIED STEP 1

Part: BATTERY PACK — INOPERATIVE (R/H CABIN) · airframe 77,647 hrs · 45,956 cycles

CUSTOMER REQUEST: RT STOW BIN ROW 3/ROW 6 EMERGENCY LIGHT INOP / [01] REMOVED AND REPLACED M1674 EMERGENCY BATTERY PACK PER AMM 35-51-06-960-805. TEST NORMAL.;[02] VERIFIED STEP 1

Part: SIGN — INOPERATIVE (L1 DOOR) · airframe 77,647 hrs · 45,956 cycles

CUSTOMER REQUEST: ONE BULB INOP EMERGENCY LOWER AT L-1 DOOR / [01] RELAMPED EMERGENCY LOWER EXIT SIGN AT L-1 DOOR PER REF. AMM 33-51-01-960-801. PERFORMED OPS CHECK AND FOUND NORMAL.;[02] VERIFIED STEP 1

Part: BATTERY PACK — INOPERATIVE (FUSELAGE) · airframe 77,647 hrs · 45,956 cycles

CUSTOMER REQUEST: EXTERIOR EMERGENCY LIGHT AFT OF R-1 DOOR INOP / [01] REMOVED AND REPLACED BATTERY PACK M1674 ON TTG8Q00F9CTY. R-1 DOOR EXTERIOR EMERGENCY LIGHT TEST NORMAL PER AMM 33-51-00-710-801.;[02] VERIFIED STEP 1

Part: BATTERY PACK — INOPERATIVE (AFT CABIN) · airframe 77,647 hrs · 45,956 cycles

EMERGENCY LIGHTS INOP AT AFT CABIN AREA LEFT AND RIGHT SIDE / [01] REMOVED AND REPLACED BATTERY PACK M1673 PER AMM 33-51-06-960-805. TEST NORMAL.;[02] VERIFIED STEP 1

Part: BULKHEAD — CANNING (AFT FUSELAGE) · airframe 77,647 hrs · 45,956 cycles

OIL CANNING FOUND ON BS AFT PRESSURE BULKHEAD 5 IN. BELOW STRINGER 11R - 60 IN. FROM APEX. / [01] CUT OUT DAMAGE AREA AT AFT PRESSURE BULKHEAD 5 IN. BELOW STRINGER 11R - 60 INCHES FROM APEX AS PER B737-700 SRM 53-80-08-2R-1 AND SRM 51-10-02-0G-0.;[12] INSTALLED REPAIR PLATE AT AFT PRESSURE BULKHEAD; 5 INCHES BELOW STRINGER 11R ; 60 INCHES FROM APEX AS SRM 53-80-08-2R-1 AND SRM 51-40-02-0G-0.;[13] (CORRECTING STEP 12) INSTALLED REPAIR PLATE AT AFT PRESSURE BULKHEAD; 5 INCHES BELOW STRINGER 11R ; 60 INCHES FROM APEX AS PER SRM 53-80-08-2R-1 AND SRM 51-40-02-0G-0.;[14] APPLIED CIC ON ALL REPAIR AREA IN IAW AMM 51-21-91-620-802;[15] VERIFIED 11; 13; 14.;[16] FABRICATED AND INSTALLED REPAIR PLATE AT AFT PRESSURE BULKHEAD; 5 INCHES BELOW STRINGER 11R; 60 INCHES FROM APEX; MATERIAL USED P/N 148A2281 IN IAW SRM 53-80-08-2R-1; 51-40-02-0G-0; 51-40-05-0G-0; FIG 205 SHEET 1;[17] FINAL WORK COMPLETE. VERIFIED 16.

Part: BULKHEAD — CANNING (AFT FUSELAGE) · airframe 77,647 hrs · 45,956 cycles

OIL CANNING FOUND ON BS1016 AFT PRESSURE BULKHEAD AT STRINGER 2L - 60 IN. FROM APEX. / [01] CUT OUT DAMAGE AREA AT BS1016 AFT PRESSURE BULKHEAD AT STRINGER 2L - 60 IN. FROM APEX. CUT OUT DIMENSION ( 2.0' X 1.5' ); ASPER B737-700 SRM 51-10-02-0G-0.[16] DRILLED HOLE FROM LAYOUT ON AREAS ; START FABRICATE DOUBLER AS PER REF B737-700 AND EA 22-153-02894-WIP2 FIG 2-1;SHEET 4;[17] FABRICATED TAPERED FILLER FROM 2024-T3 0.032' MATERIAL AS PER EA 22-153-02894-WIP2.;[18] ADDING INFORMATION TO STEP 10. FINAL TRIM OUT AREA LOCATED 3.20' AND 4.70' FROM EDGE OF DAMAGE TO EXISTING PRESSURE CHORD DOUBLER FASTENER HOLES; AS SHOWN ON ATTACHED SKETCH.;[19] VERIFIED 16-18. SEE WIPI 2 AND 3.<BR>OK TO INSTALL REPAIR.;[20] ACCOMPLISHED ALL REPAIR AND PROCEDURES AS PER EA 22-153-02894.;[21] SUMMARY EA 22-153-02894 WAS ISSUED

Part: NONE — WARPED · airframe 77,643 hrs · 45,955 cycles

OIL CANNING FOUND ON BS AFT PRESSURE BULKHEAD 5 IN. BELOW STRINGER 11R - 60 IN. FROM APEX. / [01] TRANSFERRED TO N/R FAULT TTG8Q00EXJBY

Part: NONE — WARPED · airframe 77,643 hrs · 45,955 cycles

OIL CANNING FOUND ON BS1016 AFT PRESSURE BULKHEAD AT STRINGER 2L - 60 IN. FROM APEX. / [01] N/A'D REMAINING MEASUREMENTS; MEASUREMENTS TRANSFERRED TO FAULT TTG8Q00EXJCA;[02] TRANSFERRED TO N/R FAULT TTG8Q00EXJCA

Part: DOUBLER — CRACKED (FWD FUSELAGE) · airframe 77,298 hrs · 45,723 cycles

EXTERNAL GROUND POWER DOOR CUTOUT INTERNAL SKIN DOUBLER IS CRACKED ON LOWER SIDE OF DOOR. REMOVED DAMAGE SECTION IAW SRM 53-10-15-2R-4.FIG 204. HFEC IAW NDT PART 6; 51-00-00 P23. NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION WITH 10X GLASS OF TRIM OUT AREA IAW SRM 53-10-15-2R-4. DAMAGE DOES NOT EXTEND UNDER SKIN. NO DISBOND OF EGPR SURROUND DOUBLER AND SKIN. FABRICATED, LOCATED AND DRILLED REPAIR PARTS -2 DOUBLER & -3 FILLER IAW SRM 53-10-15-2R-4 STEP 4.E; 4.F; 4.G; 4.H; 4.I & 4.J. TREATED AND PRIMED REPAIR PARTS AND TRIM OUT IAW SRM 53-10-15-2R-4. INSTALLED REPAIR PARTS IAW SRM 53-10-15-2R-4 & DWG 141A8701 REV -. APPLIED CIC AS REQUIRED IAW AMM 51-21-91-620-802.

Part: TIRE — FAILED (LT MLG) · airframe 75,364 hrs · 44,479 cycles

#3 MAIN TIRE BLOWN ON TAKEOFF. DAMAGE TO WING & FLAPS NOTED AFTER LANDING. ; / [01] C/W TIRE THREADLOSS OR TIRE BURST CONDITIONAL INSPECTION PER AMM 05-51-54.REF LOGBOOK# 1831150 FOR #3&#4 MLG WHEEL ASSY R&R; REF LOGBOOK# 1787451 & LOGBOOK# 1787452 FOR RIGHT IN DIAMETER FLAP DAMAGE; REF LOGBOOK# 1787453 FOR RH MLG AFT W/W FAIRING DAMAGE.

Part: TIRE — FAILED (LT MLG) · airframe 75,364 hrs · 44,479 cycles

#3 MAIN TIRE BLOWN ON TAKEOFF. DAMAGE TO WING & FLAPS NOTED AFTER LANDING. ; / [01] C/W TIRE THREADLOSS OR TIRE BURST CONDITIONAL INSPECTION PER AMM 05-51-54.REF LOGBOOK# 1831150 FOR #3&#4 MLG WHEEL ASSY R&R; REF LOGBOOK# 1787451 & LOGBOOK# 1787452 FOR RIGHT IN DIAMETER FLAP DAMAGE; REF LOGBOOK# 1787453 FOR RH MLG AFT W/W FAIRING DAMAGE.

Part: FAIRING — DELAMINATED (R/H MLG) · airframe 75,364 hrs · 44,479 cycles

RH MLG AFT W/W FAIRING DENTED & DELAMINATED. PANEL 194GR MEASURES 1.75'H X 4.25'W X 2/32'DREF LOGBOOK#1831149 ; / [01] REF LOG# 178451. COMPLY WITH MPM 3 DAYS METALLIC TAPE REINSPECT WITHIN 3 DAYS. PERMANENT REPAIR REQUIRED WITHIN 20 DAYS. OK TO CONTINUE PER MXNOTE. REMOVED AND REPLACED PANEL 194GR PER AMM 53-51-21 SRM 51-20-07 AND 51-20-01.

Part: NONE — BROKEN (CABIN) · airframe 75,147 hrs · 44,350 cycles

AFT GALLEY ENTRY DOOR EXIT SIGN MID DOOR BROKEN ; / [01] REPLACED AFT GALLEY SVC DOOR EXIT SIGN LENS RH SIDE REF AMM 33-51-01

Part: MOUNT — BROKEN (EMERGENCY LIGHT) · airframe 74,726 hrs · 44,101 cycles

MID CABIN EMERGENCY EXIT LIGHT HANGING FROM CEILING HAS BROKEN MOUNT. ; / [01] ACCOMPLISH EA 21-133-02605 ASSIGNED AS A SUBTASK.; [02] L/P 1686559 INSTALLED INTERIM REPAIR PER EA 21-133-02605. PERMANENT REPAIR REQUIRED WITHIN 2 DAYS

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,723 hrs · 44,099 cycles

FWD GALLEY EXIT SIGN HAS A BULB OUT / [01] RELAMPED AND PERFORMED GOOD TEST OF FWD GALLEY EXIT SIGN PER AMM 33-25-00-960-801.; [02] CORRECTION FOR REF. S/B 33-51-01-960-801; [03] REF. CORRECTION; [04] VERIFIED CORRECTIVE ACTION 1 AND 2 PER AMM 33-51-01-960-801

Part: LAMP — MISSING (EMERGENCY LIGHT) · airframe 74,723 hrs · 44,099 cycles

R/H OVERWING EMERGENCY LIGHT MISSING BULBS. ; / [01] RE-LAMPED R/H OVERWING EMERGENCY LIGHT AND PERFORMED A GOOD OP CHECK ALL AS PER AMM 33-51-03-960-801.; [02] VERIFIED CORRECTIVE ACTION 1

Part: INTERCOSTAL — CORRODED (BS 807) · airframe 74,723 hrs · 44,099 cycles

CORROSION; AFT CARGO; BS 807 + 2; RBL 19; WL 156; SUBTHRESHOLD INTERCOSTAL UPPER FLANGE; LWR SURFACE AT NUTPLATE HOLE; MARKED. ; / [01] REMOVED DAMAGE IN ACB BS 807+2 RBL19 WL156 IN AN AREA 1'X1' IAW SRM 53-60-15-1A-1.; [02] VERIFIED CORROSION REMOVED PER SRM 53-60-15-1A-1.; [03] HFEC INSPECTED BLEND IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071<BR><BR>UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.064'. EQUIP ID#: ATS2031 S/N: 170515011; [05] DAMAGE REMOVAL EVAL ORIGINAL THICKNESS OF .060'; REMAINING THICKNESS OF .049'; FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1.; [06] VERIFIED CORRECTIVE ACTION 5; [07] REMOVED SUBTHRESHOLD INTERCOSTAL BS 792 TO BS 847 RBL 19 WL 156 IAW SRM 51-40-02.; [08] UPDATED PART USE; [09] LOCATED; DRILLED AND DEBURRED NEW SUBTHRESHOLD INTERCOSTAL BS792 TO 847 RBL19 WL156 IAW SRM 51-40-05 AND DWG 146A0081. [12] INSTALLED SUBTHRESHOLD INTERCOSTAL WEB BS 792-847 RBL 19; WL 156 PER SRM 51-40-02-0G-0; DWG 146A0081; DWG 146A8120.

Part: WEB — CORRODED (BS 789) · airframe 74,723 hrs · 44,099 cycles

CORROSION; AFT CARGO BS 789; RBL 20; WL 155; INTERCOSTAL WEB UPPER END; OB SURFACE; MARKED ; / [01] REMOVED CORROSION IN ACB BS789 RBL20 WL 155 IN A 1'X1' AREA IAW SRM 53-60-15-1A-1.; [02] VERIFIED CORROSION REMOVED PER SRM 53-60-15-1A-1.; [03] HFEC INSPECTED BLEND IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071<BR><BR>UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.040'. EQUIP ID#: ATS2031 S/N: 170515011; [04] DAMAGE REMOVAL EVAL ORIGINAL THICKNESS OF .050'; REMAINING THICKNESS OF .040'; FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1.; [05] VERIFIED CORRECTIVE ACTION 4 OUT OF LIMITS; [06] REMOVED INTERCOSTAL WEB BS 787 TO BS 792 RBL 20 WL 155 IAW SRM 51-40-02.; [07] RECEIVED NEW INTERCOSTAL WEB FROM OSS CUSTOMER RO #834705-SWA.; [08] VERIFIED ACTION 6;7; [09] LOCATED;DRILLED AND DEBURRED NEW INTERCOSTAL @ BS 787 TO 792 RBL20 WL 155 IAW SRM 51-40-05 AND DWG #146A0081. OK TO INSTALL.; [10] INSPECTED ACTION 9; OK TO INSTALL; [11] INSTALLED ACB NEW INTERCOSTAL WEB AT BS787 - BS794; RBL20; WL155 PER SRM 51-40-02-0G-0 AND DWG 146A8120; DWG 146A0081; [12] CORRECTED MEASUREMENT; [13] VERIFIED CORRECTIVE ACTION 11 PER SRM 51-40-02-0G-0 AND DWG 146A8120; DWG 146A0081; [14] VERIFIED ALL CORRECTIVE ACTIONS HAVE BEEN ACCOMPLISHED AND VERIFIED

Part: SUPPORT — DAMAGED (BS 500D BLKHD) · airframe 74,723 hrs · 44,099 cycles

FCB AFT R/H BS500D BULKHEAD SUPPORT HAS OVERSIZE ON LOWER END RBL21 WL 156 ; / [01] EVALUATED OVERSIZE HOLE ON R/H BS 500D BULKHEAD SUPPORT RBL 21 WL 156 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] REMOVED FCB AFT R/H BS 500D BULKHEAD SUPPORT ANGLE PER SRM 51-40-02-0G-0; [03] LOCATED AND DRILLED NEW BULKHEAD ANGLE PO# 831153/1 PER SRM 51-40-05-0G-0 AND DWG 143A7902. UPDATED PART TABLE; [04] VERIFIED STEPS 2 AND 3.; [05] VERIFIED LOCATE AND DRILL UP OF NEW ANGLE PER SRM 51-40-05 AND DWG 143A7902.; [06] OK TO INSTALL AFT R/H BS 500D BULKHEAD SUPPORT.; [07] OK TO INSTALL; [08] INSTALLED FCB AFT R/H BS 500D BULKHEAD SUPPORT ANGLE PER SRM 51-40-02-0G-0 AND DWG 143A7902; [09] VERIFIED STEP 8; [10] RII INSPECTED ACTION 8; [11] INSPECTION COMPLETE

Part: SPLICE — DAMAGED (FLOOR PANEL) · airframe 74,723 hrs · 44,099 cycles

AFT CARGO BAY FLOOR PANEL SPLICE STRAP AT BS 767+4 HAS OVERSIZE HOLES RBL 10 TO LBL10 WL 156 ; / [01] UPDATED MEASUREMENT TABLE; [02] EVALUATED OVERSIZE HOLES ON SPLICE STRAP; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] RECEIVED NEW STRAP ON PO# 829373 NEW PART WILL BE INSTALLED ON FAULT # TTG8Q0060TDE; [04] VERIFIED NEW STRAP RECEIVED; INSTALLATION ON TTG8Q0060TDE; JOB COMPLETE.

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 74,723 hrs · 44,099 cycles

FCB GUSSET BS 500D STRINGER 19 L/H IS CRACKED ; / [01] EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED GUSSET BS 500D STR 19L PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW GUSSET BS 500D STR 19L PER SRM 51-40-05-0G-0 AND DWG 143A7902. OK TO INSTALL; [05] VERIFIED ITEMS 3 AND 4; [06] VERIFIED LOCATED AND DRILLED NEW GUSSET BS 500D STR 19L PER SRM 51-40-05-0G-0 AND DWG 143A7902. OK TO INSTALL; [07] INSTALLED GUSSET BS 500D STR 19L PER SRM 51-40-02-0G-0 AND DWG 143A7902; [08] VERIFIED STEP 7; [09] VERIFIED CORRECTIVE ACTION STEP 7.; [10] APPLIED CIC ON GUSSET BS 500D STR 19L PER AMM 51-21-91-620-802; [11] VERIFIED STEP 10; [12] VERIFIED CORRECTIVE ACTIONS 7 TO 11. <BR><BR>GUSSET AT BS500D; S-19L REPLACED.; [13] FCB GUSSET AT BS500D; S-19L REPLACED. ALL WORK ACCOMPLISHED

Part: FRAME — DAMAGED (BS 727A RBL21.5) · airframe 74,723 hrs · 44,099 cycles

OVERSIZE HOLE IN FRAME AT BS727A RBL21.5 WL156 COMMON TO UPPER FLOOR TO SIDEWALL SUPPORT FASTENER HOLE ; / [01] REMOVED DAMAGE ON FRAME BS727A RBL21.5 WL156 IAW SRM 53-60-072R-2.; [02] REQUEST DVI OF THE UNDERLYING STRUCTURE AND FUSELAGE SKIN IN REPAIR AREA.; [03] ACCOMPLISHED DVI OF THE UNDERLYING STRUCTURE AND FUSELAGE SKIN IN REPAIR AREA NO DEFECTS NOTED IAW SRM 53-60-07-2R-2 STEP 4D (6); [04] REFERENCE CORRECTION. REMOVED DAMAGE IAW SRM 53-60-07-2R-2.; [05] VALIDATE APPLICABILITY OF SRM 53-60-07-2R-2.; [06] VERIFIED VALIDATION OF APPLICABILITY OF SRM 53-60-07-2R-2.; [07] REMOVED EXISTING SPLICE @ BS727A BETWEEN STR25R AND STR24R IAW SRM 51-40-02.; [08] REQUEST HFEC OF THE CUT EDGES IAW SRM 53-60-07-2R-2.; [09] REQUEST HFEC INSPECTION OF ALL OPEN HOLES COMMON TO REPAIR IAW SRM 53-60-07-2R-2.; [10] REQUEST HFEC INSPECTION OF COUNTERSINKS COMMON TO REPAIR IAW SRM 53-60-07-2R-2.;[19] INSTALLED FRAME REPAIR AT BS727A RBL 21.5; WL 156 PER SRM 53-60-07-2R-2; [20] VERIFIED CORRECTIVE ACTION #19; [21] VERIFIED ALL STEPS COMPLETE

Part: ANGLE — CRACKED (BS 400 LBL 23) · airframe 74,723 hrs · 44,099 cycles

FORWARD CARGO BAY L/H BAFFLE CLIP BS 400 LBL 23 WL 155 IS CRACKED ; / [01] EVALUATED DAMAGE ON BAFFLE CLIP AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0. REMOVED OLD BAFFLE CLIP PER SRM 51-40-02-0G-0; [02] VERIFIED EVALUATED DAMAGE ON BAFFLE CLIP AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0. REMOVED OLD BAFFLE CLIP PER SRM 51-40-02-0G-0; [03] LOCATED AND DRILLED NEW BAFFLE CLIP AT BS400 LBL23 WL155 PER SRM 51-40-05-0G-0 AND DWG 143A7505.<BR>OK TO INSTALL.; [04] VERIFIED CORRECTIVE ACTION #3; OK TO INSTALL GIVEN.; [05] INSTALLED NEW BAFFLE CLIP AT FCB BS400 LBL23 WL155 PER SRM 51-40-02-0G-0 AND DWG 143A7505.; [06] VERIFIED JOB COMPLETE; [07] VERIFIED CORRECTIVE ACTION 5 AND 6.<BR><BR>NEW BAFFLE CLIP INSTALLED.; [08] BAFFLE CLIP AT BS400; LBL23; WL155 REPLACED. ALL WORK ACCOMPLISHED.

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 74,723 hrs · 44,099 cycles

FCB GUSSET BS 500D STRINGER 19 R/H IS CRACKED ; / [01] EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED GUSSET BS 500D STR 19R PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW GUSSET BS 500D STR 19R PER SRM 51-40-05-0G-0 AND DWG 143A7902. OK TO INSTALL; [05] VERIFIED ITEMS 3 AND 4; [06] VERIFIED LOCATED AND DRILLED NEW GUSSET BS 500D STR 19R PER SRM 51-40-05-0G-0 AND DWG 143A7902. OK TO INSTALL; [07] INSTALLED GUSSET BS 500D STR 19R PER SRM 51-40-02-0G-0 AND DWG143A7902; [08] VERIFIED STEP 7; [09] VERIFIED CORRECTIVE ACTION STEP 7.; [10] APPLIED CIC ON GUSSET BS 500D STR 19R PER AMM 51-21-91-620-802; [11] VERIFIED STEP 10; [12] VERIFIED CORRECTIVE ACTIONS 7 TO 11.<BR><BR>FCB GUSSET AT BS500D; S-19R REPLACED.; [13] FCB GUSSET AT BS500D; S-19R HAS BEEN REPLACED. ALL WORK ACCOMPLISHED.

Part: GUSSET — CRACKED (BS 500D S21L) · airframe 74,723 hrs · 44,099 cycles

FCB GUSSET BS 500D STRINGER 21 L/H IS CRACKED ; / [01] EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CRACK; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED GUSSET BS 500D STR 21L PER SRM 51-40-05-0G-0; [04] LOCATED AND DRILLED NEW GUSSET AT BS 500D STR 21L PER SRM 51-40-05-0G-0 AND DWG 143A7902. OK TO INSTALL; [05] REMOVED GUSSET BS 500D STR 21L PER SRM 51-40-02-0G-0; [06] VERIFIED ITEMS 3;4 AND 5; [07] VERIFIED LOCATED AND DRILLED NEW GUSSET AT BS 500D STR 21L PER SRM 51-40-05-0G-0 AND DWG 143A7902. OK TO INSTALL; [08] INSTALLED GUSSET AT BS 500D STR 21L PER SRM 51-40-02-0G-0 AND DWG 143A7902; [09] VERIFIED STEP 8; [10] VERIFIED CORRECTIVE ACTION STEP 8.; [11] APPLIED CIC ON GUSSET BS 500D STR 21L PER AMM 51-21-91-620-802; [12] VERIFIED STEP 11; [13] VERIFIED CORRECTIVE ACTIONS 8 TO 12. <BR><BR>GUSSET AT BS500D; S-21L REPLACED; [14] FCB GUSSET AT BS500D; S-21L HAS BEEN REPLACED. ALL WORK ACCOMPLISHED.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 74,723 hrs · 44,099 cycles

LT HORIZ. STAB RIB ASSY. 4 (STAB STA 120.30) 2ND VERT STIFFENER IS CRACKED. ; / [01] REMOVED CRACK DAMAGE LOWER RADIUS OF VERTICAL STIFFENER AND WEB L=0.45' X W=0.35' IAW SRM 55-10-09-2R-4 ITEM 4 STEP B.; [02] VERIFIED REMOVAL OF CRACK DAMAGE AND PERFORMED GVI PER SRM 55-10-09-2R-4 STEP 4.B AND E; HOLES ON EITHER SIDE OF THE VERTICAL STIFFENER FOUND CRACKED BY HFEC INSPECTION LAST STEP; IAW SRM 55-10-09-2R-5 ITEM 4 STEPS B & C. NEW DIMENSION FOR CUTOUT L=1.65' X W=0.65'.[07] VERIFIED REMOVAL OF ADDITIONAL DAMAGE PER SRM 55-10-09-2R-5; [08] REQUEST HFEC INSPECTION FOR CUT EDGES OF THE RIB CHORD.; [09] HFEC INSPECTED CUT OUT PER NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS NOTED IAW SRM 55-10-09-2R-5 REPAIR 5. ITEM 4 STEP G-K. FIGURE 204 REPAIR 5 DETAIL A.; [11] APPLIED CHEMICAL CONVERSION COATING TO REPAIR PARTS; BARE SURFACES AND EDGES OF THE RIB IAW SRM 55-10-09-2R-5 REPAIR 5 ITEM 4 STEP L.; [12] VERIFIED CORRECTIVE ACTION 10 AND 11; OK TO PRIME; [13] APPLIED PRIMER TO REPAIR PARTS; BARE SURFACES AND EDGES OF THE RIB IAW SRM 55-10-09-2R-5 REPAIR 5 ITEM 4 STEP M. OK TO INSTALL REPAIR PARTS.; [14] VERIFIED CORRECTIVE ACTION 13; OK TO INSTALL REPAIR PARTS; [15] INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-5 REPAIR 5 ITEM 4 STEPS N-Q.;

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 74,723 hrs · 44,099 cycles

LT HORIZ. STAB RIB ASSY. 4 (STAB STA 120.30) LOWER CHORD AT THE 4TH VERT STIFFENER IS CRACKED. ; / [01] REMOVED CRACK DAMAGE LOWER CHORD AT 4TH VERTICAL STIFFENER L=0.85'X W=0.65' IAW SRM 55-10-09-2R-5 ITEM 4 STEP B.[04] CUT AND REMOVED 1.E.A CRACKED HOLE AFT OF THE VERTICAL STIFFENER FOUND CRACKED BY HFEC INSPECTION LAST STEP; IAW SRM 55-10-09-2R-5 ITEM 4 STEPS B & C. NEW CUTOUT DIMENSIONS L=1.70' X W=0.65'.; [05] VERIFIED REMOVAL OF ADDITIONAL NOTED DAMAGE PER STRM 55-10-09-2R-5; [06] REQUEST HFEC INSPECTION FOR CUT EDGES OF THE RIB CHORD.; [07] HFEC INSPECTED CUT OUT PER NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS NOTED.<BR>CAL ID: IS000450 S/N : N500D000M120071; [08] FABRICATED REPAIR PARTS. T-SECTION 60-5872#7075T76511 0.063' THICK LOT # 1430775-2; ANGLE BAC1490-2793#7075T62 0.063' THICK LOT # 1435997-1; FILLER 7075T6# 0.050' THICK LOT # 1376846-2; IAW SRM 55-10-09-2R-5 REPAIR 5. ITEM 4 STEP G-K. FIGURE 203 REPAIR 5 DETAIL A.[13] INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-5 REPAIR 5 ITEM 4 STEPS N-Q.; [14] VERIFIED CORRECTIVE ACTION 13; [15] APPLIED FILLET SEAL AND FINISH TO REPAIR PARTS IAW SRM 55-10-09-2R-5 REPAIR 5 ITEM 4 STEPS R & S.; [16] VERIFIED CORRECTIVE ACTION 15; [17] REMOVED CRACK DAMAGE LEFT HORIZONTAL STABILIZER RIB ASSY AT STA 120.30 AT THE 4TH VERTICAL STIFFENER LOWER CHORD AND INSTALLED REPAIR IAW SRM 55-10-09-2R-5 REPAIR 5.

Part: PANEL — CHAFED · airframe 74,723 hrs · 44,099 cycles

PANEL 192F HAS CHAFING DAMAGE TO FWD AND AFT INNER MATING SURFACES ; / [01] IDENTIFIED PANEL 192F IAW SRM 53-40-70-0I-1 FIGURE 2. TABLE 2. ITEM 15.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.B.2.(A).<BR><BR>DAMAGE IS TO BE REPAIRED IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 PARA 4.B.(2). AND D.<BR><BR>REMOVED CHAFING DAMAGE FROM FWD AND AFT EDGE 2.5']X 15.75' WITH NO CONTAMINATION NOTED AND CLEANED IAW SRM 51-70-05-2R-6 PARA 4.A.-D.; [02] CORRECTION TO CORRECTIVE ACTION 1<BR><BR>REMOVED CHAFING DAMAGE FROM FWD AND AFT EDGE 2.5IN X 15.75IN WITH NO CONTAMINATION NOTED AND CLEANED IAW SRM 51-70-05-2R-6 PARA 4.A.-D.; [03] VALIDATED APPLICABILITY OF REPAIR TO PANEL 192F INNER SURFACES TO BE COMPLETED IAW SRM 51-70-05-2R-6.; [04] VERIFIED CORRECTIVE ACTIONS 1-3 PER SRM 53-40-70-0I-1; SRM 53-40-70-1A-1; AND SRM 51-70-05-2R-6.<BR>VALIDATED REPAIR PER SRM 51-70-05-2R-6; [05] FABRICATED REPAIR PLIES USING BMS 8-79CL3ST120 LOT # 1464911-2 AND INSTALLED USING BMS 5-129TY2GR05 LOT # 1461506-1; VACUUM BAGGED; 5X5 CHECKED OK USING GAUGE ID: ATS2438 S/N: UNKNOWN IAW SRM 51-70-05-2R-6 PARA 4.E.-F.S IAW SRM 51-70-05-2R-6 PARA 4.G

Part: SHIELD — CORRODED (BS 767-775 RBL21) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767 - BS775 RBL21 WL157. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED SHIELD BS 767-794 RBL 21; WL 157 PER SRM 51-40-02-0G-0.; [04] RECEIVED NEW SHIELD P/N: 146A8127U1 AT AFT CARGO BAY BS 767 TO BS 775 RBL 21 WL 157.<BR>LOCATED AND DRILLED NEW SHIELD . IAW. SRM 51-40-05 AND DGW: 146A0081.; [05] VERIFIED LOCATE AND DRILL; [06] VERIFIED CORRECTIVE ACTIONS 3-5.<BR><BR>NEW SHIELD LOCATED AND DRILLED.; [07] OK TO INSTALL.; [08] OK TO INSTALL SHIELD STA 767-775; [09] INSTALLED ACB NEW FWD SHIELD AT BS767 - BS787; RBL21; WL157 PER SRM 51-40-02-0G-0 AND DWG 146A0081; [10] VERIFIED CORRECTIVE ACTION 9; [11] VERIFIED JOB COMPLETE

Part: TRACK — CORRODED (BS 727A) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727A+17 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; ALL WORK TO BE ACCOMPLISHED ON CUST CARD# TT8Q0064GV4; [02] VERIFIED EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; ALL WORK TO BE ACCOMPLISHED ON CUST CARD# TT8Q0064GV4

Part: ANGLE — CORRODED (BS 727D) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON CLIP AT AFT CARGO BAY BS727D+9 RBL7 WL151. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED ACB CLIP AT BS727+9; RBL7; WL151 PER SRM 51-40-02-0G-0; [04] FABRICATED NEW CLIP AT AFT CARGO BAY727D+9; RBL7; WL151; LOCATED AND DRILLED IAW DWG 146A7730 SH1 REV B AND SRM 51-40-05; [05] APPLIED CHEMICAL CONVERSION IAW AMM 51-21--41-370-801 AND APPLIED PRIMER IAW AMM 51-21-72-370-804; [06] OK TO INSTALL; [07] VERIFIED STEPS 4; 5 AND STEP 6; [08] VERIFIED CORRECTIVE ACTION STEPS 3-6 OK TO INSTALL; [09] INSTALLED CLIP AT AFT CARGO BAY BS 727D+9; RBL 7; WL151 PER DWG 146A7734 SH 1 REV A AND SRM 51-40-02; [10] VERIFIED STEP 9; [11] VERIFIED CORRECTIVE ACTIONS 9 AND 10.<BR><BR>CLIP INSTALLED; [12] VERIFIED ALL WORK ACCOMPLISHED. CLIP REPLACED.

Part: ANGLE — CORRODED (BS 727D) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON CLIP AT AFT CARGO BAY BS727D+4 LBL7 WL151. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED ACB CLIP AT BS727+4; LBL7; WL151 PER SRM 51-40-02-0G-0; [04] FABRICATED NEW CLIP AT AFT CARGO BAY727D+4; LBL7; WL151; LOCATED AND DRILLED IAW DWG 146A7730 SH1 REV B AND SRM 51-40-05; [05] APPLIED CHEMICAL CONVERSION IAW AMM 51-21--41-370-801 AND APPLIED PRIMER IAW AMM 51-21-72-370-804; [06] OK TO INSTALL; [07] VERIFIED STEPS 4; 5 AND 6; [08] VERIFIED CORRECTIVE ACTION STEPS 4-6 OK TO INSTALL; [09] INSTALLED CLIP AT AFT CARGO BAY BS 727D+4 LBL 7 WL 151 IAW SR. 51-40-02 AND DWG 146A7730 AND 146A7734; [10] VERIFIED CORRECTIVE ACTION 9.<BR><BR>CLIP INSTALLED.; [11] CLIP AT ACB BS727D+4; LBL7; WL151 REPLACED. <BR><BR>NO FURTHER ACTIONS REQUIRED.

Part: TRACK — CORRODED (BS 727A) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727A+19 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; [02] EDITED MEASUREMENT FIELD; [03] VERIFIED EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; [04] REMOVED ACB CARGO TRACK TIE DOWN AT BS727 -BS867; LBL17; WL156 PER SRM 51-40-02-0G-0; [05] LOCATED AND DRILLED NEW ACB CARGO TIE DOWN TRACK BS727+4 - BS867 LBL17 WL156 IAW SRM 51-40-05-0G-0 AND DWG 146A7500; OK TO INSTALL; [06] VERIFIED LOCATE AND DRILL UP OF NEW TRACK PER SRM 51-40-05 AND DWG 146A7500; OK TO INSTALL.; [07] INSTALLED NEW ACB CARGO TIE DOWN TRACK BS727+4 - BS867 LBL17 WL156 IAW SRM 51-40-05-0G-0; DWG 146A7500 AND DWG 146A0061; [08] RII INSPECTED GOOD INSTALLATION OF TRACK PER SRM 51-40-02 AND DWG 146A7500 AND DWG 146A0061.; [09] VERIFIED GOOD INSTALLATION OF TRACK PER SRM 51-40-02 AND DWG 146A7500 AND DWG 146A0061. JOB COMPLETE.

Part: WEB — CORRODED (BS 773) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON WEB AT AFT CARGO BAY BS773 RBL20 WL157 ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED WEB BS 767-787 RBL20; WL 157 PER SRM 51-40-02-0G-0.; [04] RECEIVED NEW WEB P/N: 146A8123U19 AT AFT CARGO BAY BS 773 RBL 20 WL 157. <BR>LOCATED AND DRILLED NEW WEB IAW. SRM 51-40-05 AND DWG:146A0081. <BR>REQUEST OK TO INSTALL NEW WEB.; [05] VERIFIED CORRECTIVE ACTION 4. <BR><BR>OK TO INSTALL NEW WEB.; [06] INSTALLED NEW WEB P/N: 146A8123U19 AT AFT CARGO BAY BS 773 RBL 20 WL 157. IAW. SRM 51-40-02 AND DWG:146A0081; [07] INSTALLED NEW WEB P/N: 146A8123U19 AT AFT CARGO BAY BS 767-787; RBL 20 WL 157. IAW. SRM 51-40-02 AND DWG:146A0081; [08] VERIFIED CORRECTIVE ACTIONS 6-7<BR><BR>WEB INSTALLED; [09] WEB AT ACB BS773; RBL20; WL157 REPLACED. <BR><BR>NO FURTHER ACTIONS REQUIRED.

Part: INTERCOSTAL — CORRODED (BS 928) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS928 LBL3 WL168. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED ACB INTERCOSTAL AT BS927 - BS947; LBL3; WL168 PER SRM 51-40-02-0G-0; [04] RECEIVED INTERCOSTAL FROM HEAT TREAT/FORM PO#833546; [05] VERIFIED CORRECTIVE ACTION ITEMS 3 AND 4; [06] LOCATED AND DRILLED ACB INTERCOSTAL AT BS927 - BS947; LBL3; WL168 PER SRM 51-40-05-0G-0 AND DWG 147A7500; [07] APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO INTERCOSTAL PER AMM 51-21-41-370-802; AMM 51-21-72-370-804. OK TO INSTALL; [08] VERIFIED CORRECTIVE ACTION ITEMS 6 AND 7; OK TO INSTALL; [09] INSTALLED INTERCOSTAL PER SRM 51-40-02-0G-0; AND DWG 147A7500; [10] VERIFIED INSTALLED INTERCOSTAL PER SRM 51-40-02-0G-0; AND DWG 147A7500; [11] RII; VERIFIED GOOD INSTALLTION OF INTERCOSTAL PER SRM 51-40-02-0G-0; AND DWG 147A7500.; [12] COMPLETED JOB PER SRM 51-40-02-0G AND DWG 147A7500; [13] VERIFIED COMPLETED

Part: INTERCOSTAL — CORRODED (BS 928) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS928 RBL3 WL168. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED ACB INTERCOSTAL AT BS927 - BS947; RBL3; WL168 PER SRM 51-40-02-0G-0; [04] RECEIVED INTERCOSTAL FROM HEAT TREAT/FORM PO#833545; [05] VERIFIED CORRECTIVE ACTION ITEMS 3 AND 4; [06] LOCATED AND DRILLED ACB INTERCOSTAL AT BS927 - BS947; RBL3; WL168 PER SRM 51-40-05-0G-0 AND DWG 147A7500; [07] APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO INTERCOSTAL PER AMM 51-21-41-370-802; AMM 51-21-72-370-804. OK TO INSTALL; [08] VERIFIED CORRECTIVE ACTION ITEMS 6 AND 7; OK TO INSTALL; [09] INSTALLED INTERCOSTAL PER SRM 51-40-02-0G-0; AND DWG 147A7500; [10] VERIFIED INSTALLED INTERCOSTAL PER SRM 51-40-02-0G-0; AND DWG 147A7500; [11] RII; VERIFIED GOOD INSTALLTION OF INTERCOSTAL PER SRM 51-40-02-0G-0; AND DWG 147A7500.; [12] COMPLETED JOB PER SRM 51-40-02-0G AND DWG 147A7500; [13] VERIFIED COMPLETED

Part: SUPPORT — CORRODED (BS 727A-807) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727A- BS807 LBL21 WL157. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.040 IN A 1'X160' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [02] VERIFIED EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.040 IN A 1'X160' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [03] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS847; LBL21; WL157 PER SRM 51-40-02-0G-0.; [04] FABRICATED; LOCATED AND APPLIED CHEMICAL CONVERSION COATING TO ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS847 AND SPLICE REPAIR AT BS767+8 - BS 767+18 USING BAC1496-377#7075T62 PER SRM 51-40-05-0G AND DWG 146A7500; SRM 53-00-53-2R-5; AMM 51-21-41-370-802; [05] FABRICATED;08] VERIFIED CORRECTIVE ACTION ITEM 7; [09] OK TO INSTALL FLOOR TO SIDEWALL SUPPORT; [10] VERIFIED CORRECTIVE ACTION 9 OK TO INSTALL; [11] INSTALLED FLOOR TO SIDE WALL SUPPORT L/H IAW SRM 51-40-02-0G-0 AND DWG 146A7500.

Part: WEB — CORRODED (THRESHOLD) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS807- BS827 RBL26 WL159. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X20' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [02] VERIFIED EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X20' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [03] REMOVED SUBTHRESHOLD WEB BS 749-847 RBL27; WL159 PER SRM 51-40-02-0G-0.; [04] LOCATED AND DRILLED NEW SUBTHRESHOLD WEB PER SRM 51-40-05-0G-0; DWG 146A8120; AND DWG 143A8340; [05] LOCATED; DRILLED NEW SUBTHRESHOLD WEB PER SRM 51-40-05-0G-0; DWG 146A8120; AND DWG 143A8340. INSTALLED NUTPLATES PER DWG 143A8340; [06] CERTIFIED STEPS 4 AND 5; [07] UPDATED PARTS TABLE; [08] VERIFIED LOCATE AND DRILL UP OF NEW WEB; AND INSTALLATION OF NUT PLATES PER SRM 51-40-05 AND DWG 146A8120; 143A8340.; [09] OK TO INSTALL SUBTHRESHOLD WEB; BS794-847 RBL26;WL 159.; [10] VERIFIED OK TO INSTALL SUBTHRESHOLD WEB; BS794-847 RBL26;WL 159.; [11] INSTALLED SUBTHRESHOLD WEB BS 794-847 RBL 26; WL 159 PER SRM 51-40-02-0G-0; DWG 146A8340.; [12] VERIFIED INSTALLED SUBTHRESHOLD WEB BS 794-847 RBL 26; WL 159 PER SRM 51-40-02-0G-0; DWG 146A8340.; [13] VERIFIED ALL STEPS COMPLETE.

Part: SUPPORT — CORRODED (BS 727C) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS767- BS727C RBL21 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X20' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [02] VERIFIED EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X20' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [03] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS767; RBL21; WL156 PER SRM 51-40-02-0G-0; [04] UPDATED PARTS TABLE; [05] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-05-0G-0; AND DWG 146A7500. OK TO INSTALL; [06] VERIFIED STEP 5; [07] VERIFIED CORRECTIVE ACTION #5; [08] INSTALLED FLOOR TO SIDEWALL SUPPORT BS 727- 767 RBL 21; WL 156 PER SRM 51-40-02-0G-0; DWG 146A7500.; [09] VERIFIED INSTALLED FLOOR TO SIDEWALL SUPPORT BS 727- 767 RBL 21; WL 156 PER SRM 51-40-02-0G-0; DWG 146A7500.; [10] VERIFIED ALL STEPS COMPLETE.

Part: TRACK — CORRODED (BS 727A) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727A+10 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; ALL WORK TO BE ACCOMPLISHED ON CUST CARD# TT8Q0064GV4; [02] VERIFIED EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; ALL WORK TO BE ACCOMPLISHED ON CUST CARD# TT8Q0064GV4

Part: SHIELD — CORRODED (BS 500) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON SHIELD IN FWD CARGO BAY AFT OF DOOR BS500 RBL 21 WL 156 ; / [01] UPDATED MEASUREMENTS TABLE; [02] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] VERIFIED CORROSION OUT OF LIMITS AND PART TO BE REPLACED PER SRM 51-10-02; [04] REMOVED SHIELD BS 492-500A RBL 21; WL 156; PER SRM 51-40-02-0G-0.; [05] LOCATED AND DRILLED NEW SHIELD AT FCB BS492 TO BS500A RBL21 WL156 PER SRM 51-40-05-0G AND DWG 143A0080.; [06] VERIFIED LOCATE AND DRILL UP OF NEW SHIELD PER SRM 51-40-05 AND DWG 143A7902.; [07] EDIT TO DWG #; VERIFIED LOCATE AND DRILL UP OF NEW SHIELD PER SRM 51-40-05 AND DWG 143A0080.; [08] CERTIFIED EDIT TO DWG #.; [09] UPDATED PARTS TABLE; [10] OK TO INSTALL SHIELD; [11] OK TO INSTALL; [12] INSTALLED FWD CARGO BAY AFT OF DOOR SHIELD IAW SRM 51-40-02-0G-0;DWG # 143A0080; [13] VERIFIED INSTALLED FWD CARGO BAY AFT OF DOOR SHIELD IAW SRM 51-40-02-0G-0;DWG # 143A0080; [14] CORRECTED MEASUREMENT TABLE ORDER#20 SHOULD BE N/A NOT MAJOR; [15] CERTIFIED STEP 1 AND 14

Part: STRINGER CLIP — CORRODED (BS 867) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS867 LBL6 WL162. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED ACB STRINGER CLIP AT BS867; LBL6; WL162 PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW STRINGER CLIP AT AFT CARGO BAY BS 867 LBL6; WL162; IAW DWG 146A1282 SH 88;89 RV A AND SRM 51-40-05; [05] VERIFIED STEP 4; [06] VERIFIED LOCATED AND DRILLED NEW STRINGER CLIP AT AFT CARGO BAY BS 867 LBL6; WL162; IAW DWG 146A1282 SH 88;89 RV A AND SRM 51-40-05 OK TO INSTALL; [07] INSTALLED STRINGER CLIP AT AFT CARGO BAY BS 867 LBL 6 WL 162 IAW SRM 51-40-02 AND DWG 146A1282 AND 146A1010; [08] VERIFIED CORRECTIVE ACTION 7.<BR><BR>STRINGER CLIP INSTALLED.; [09] STRINGER CLIP AT BS867; LBL6; WL162 REPLACED.<BR><BR>NO FURTHER ACTIONS REQUIRED.

Part: STRINGER CLIP — CRACKED (BS 827) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS827 LBL6 WL156. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED STR.CLIP BS827; LBL 6 WL 156 PER SRM51-40-02-0G-0.; [04] RECEIVED NEW STRINGER CLIP P/N:146A1010 LOT:146303; LOCATED AND DRILLED NEW STRINGER CLIP AT AFT CARGO BAY BS827 LBL6 WL156 IAW SRM 51-40-05. OK TO INSTALL; [05] VERIFIED CORRECTIVE ACTION 4. <BR><BR>OK TO INSTALL NEW STRINGER CLIP.; [06] INSTALLED STRINGER CLIP AT AFT CARGO BAY BS 827 LBL 6 WL 156 IAW SRM 51-40-02 AND DWG 146A1280 AND 146A1010; [07] VERIFIED INSTALLATION.; [08] VERIFIED CORRECTIVE ACTIONS 6; 7. <BR><BR>STRINGER CLIP INSTALLED.; [09] STRINGER CLIP AT ACB BS827; LBL6; WL156 REPLACED.<BR><BR>NO FURTHER ACTIONS REQUIRED.

Part: TRACK — CORRODED (BS 727B) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS727B+3 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; ALL WORK TO BE ACCOMPLISHED ON CUST CARD# TT8Q0064GV4; [02] VERIFIED EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; ALL WORK TO BE ACCOMPLISHED ON CUST CARD# TT8Q0064GV4

Part: TRACK — CORRODED (BS 727A) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON TRACK AROUND FASTENER HOLE BS727A+3 LBL17 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; ALL WORK TO BE ACCOMPLISHED ON CUST CARD# TT8Q0064GV4; [02] VERIFIED EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.070 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID# 4566A S/N UNKNOWN; ALL WORK TO BE ACCOMPLISHED ON CUST CARD# TT8Q0064GV4

Part: SHIELD — CORRODED (BS 430 RBL 21) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON SHIELD IN FWD CARGO BAY FORWARD OF DOOR BS430 RBL 21 WL 156 ; / [01] UPDATED MEASUREMENT TABLE; [02] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] VERIFIED CORROSION OUT OF LIMITS AND PART TO BE REPLACED PER SRM 51-10-02; [04] REMOVED SHIELD; BS 420-440; RBL 21; WL 156 PER SRM 51-40-02-0G-0.; [05] LOCATED AND DRILLED NEW SHIELD AT FCB BS430 RBL21 WL156 PER SRM 51-40-05-0G AND DWG 143A0080.; [06] VERIFIED LOCATE AND DRILL UP OF NEW SHIELD PER SRM 51-40-05 AND DWG 143A0080.; [07] UPDATED PARTS TABLE; [08] OK TO INSTALL SHIELD; [09] OK TO INSTALL; [10] INSTALLED FWD CARGO BAY FORWARD OF DOOR SHIELD IAW SRM 51-40-02-0G-0; DWG # 143A0080; [11] VERIFIED INSTALLED FWD CARGO BAY FORWARD OF DOOR SHIELD IAW SRM 51-40-02-0G-0; DWG # 143A0080; [12] CORRECTED MEASUREMENT TABLE; [13] CERTIFIED STEP 1

Part: SUPPORT — CORRODED (BS 500B) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500B+11 RBL24 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIGINAL 0.040 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [02] FLOOR TO SIDEWALL SUPPORT TO BE REPLACED ON CUST CARD# TTG8Q0063ZEV; [03] VERIFIED SUPPORT TO BE REPLACED ON FAULT # TTG8Q0063ZEV

Part: STRINGER CLIP — CORRODED (BS 500A) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON STRINGER CLIP AT FWD CARGO BAY BS500A+15 RBL6 WL152. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED STR. CLIP AT BS 500A + 15; RBL6 WL 152 PER SRM 51-40-02-0G-0.; [04] FABRICATED STRINGER CLIP BS 500A+15; RBL 6; WL 152 PER SRM51-40-05-0G-0; DWG 143A3233; DWG 143A3230 USING BAC1493-856; 7075 T62; LOT #1459381-1. APPLIED A CHEMICAL CONVERSION COATING PER AMM 51-21-41-370-802.; [05] VERIFIED CORRECTIVE ACTION 4. <BR><BR>FABRICATION OF STRINGER CLIP.; [06] PRIMED STR. CLIP PER AMM 51-21-72-370-804; OK TO INSTALL.; [07] VERIFIED CORRECTIVE ACTION 6. <BR><BR>OK TO INSTALL STRINGER CLIP.; [08] INSTALLED STR. CLIP BS 500A +15; RBL 6; WL 152 PER SRM 51-40-02-0G-0; DWG 143A3230.; [09] VERIFIED CORRECTIVE ACTION 1. <BR><BR>STRINGER CLIP INSTALLED; [10] STRINGER CLIP AT BS500A+15'; RBL6; WL152 HAS BEEN REPLACED.<BR><BR>NO FURTHER ACTIONS REQUIRED.

Part: WEB — CORRODED (BS 470 THRESHOLD) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS470 RBL28 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN. SUB THRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q0063WWM; [02] VERIFIED EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN. SUB THRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q0063WWM

Part: WEB — CORRODED (BS 467 THRESHOLD) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS467 RBL28 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN. SUB THRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q0063WWM; [02] VERIFIED EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN. SUB THRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q0063WWM

Part: WEB — CORRODED (BS 462 THRESHOLD) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS462 RBL28 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN. SUB THRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q0063WWM; [02] VERIFIED EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN. SUB THRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q0063WWM

Part: SUPPORT — CORRODED (BS 450-475) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS450 - 475 LBL24 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIGINAL 0.040 IN 1'X25' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [02] FLOOR TO SIDEWALL SUPPORT TO BE REPLACED ON CUST CARD# TTG8Q0063ZEY; [03] VERIFIED SUPPORT TO BE REPLACED ON FAULT # TTG8Q0063ZEY

Part: DOUBLER — CORRODED (BS 500) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON DOUBLER AT FWD CARGO BAY BS500+8 BL0 WL148. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED DOUBLER; FWD CARGO BAY; BS 500+8; BL0; WL 148 PER SRM 51-40-02-0G-0.; [04] LOCATED; DRILLED; DEBURRED NEW DOUBLER AND INSTALLED NUTPLATES PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 143A3230; DWG 143A3233. OK TO INSTALL.; [05] VERIFIED CORRECTIVE ACTION STEP 4; OK TO INSTALL GIVEN.; [06] INSTALLED DOUBLER PER SRM 51-40-02-0G-0; DWG 143A3230; DWG 143A3233 FASTENERS THROUGH SKIN AND CLIPS.; [07] VERIFIED CORRECTIVE ACTION 6.; [08] INSTALLED ANTENNA BLANK OUT PLATE PER SRM 51-40-02-0G-0; USING SCREW GUN ID: NCX001167; SN: UNKNOWN. APPLIED FILLET SEAL PER AMM 51-31-00-390-804; BELLY SKIN PAINT TOUCH UP TO BE ACCOMPLISHED ON CUSTOMER CARD #TTG8Q0067YJQ.; [09] RII INSPECTED REPAIR COMPLETION PER SRM 51-40-02 AND DWG 143A3230 AND DWG 143A3233.; [10] VERIFIED REPAIR COMPLETION PER SRM 51-40-02 AND DWG 143A3230 AND DWG 143A3233; REFINISH ON TTG8Q0067YJQ; JOB COMPLETE.

Part: ANGLE — CORRODED (BS 500D) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL22 TO RBL20 WL156. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] VERIFIED CORRECTIVE ACTION 1 AND 2; [04] REMOVED BS 500D LOWER CENTER BULKHEAD SUPPORT PER SRM 51-40-02-0G-0; [05] LOCATED AND DRILLED NEW FLOOR SUPPORT ANGLE AT FCB BS500D LBL24.75 TO RBL24.75 WL156 PER SRM 51-40-05-0G AND DWG 143A7902.; [06] VERIFIED LOCATE AND DRILL UP OF NEW ANGLE PER SRM 51-40-05 AND DWG 143A7902.; [07] UPDATED PARTS TABLE; [08] OK TO INSTALL; [09] VERIFIED STEP 8; [10] OK TO INSTALL; [11] INSTALLED AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS 500D PER SRM 51-40-02-0G-0; DWG 143A7902 AND DWG 143A9481; [12] VERIFIED STEP 11; [13] RII INSPECTED ACTION 11; [14] INSPECTION COMPLETE

Part: DOUBLER — CORRODED (BS 500A) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON DOUBLER AT FWD CARGO BAY BS500A+12 BL0 WL148. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED DOUBLER AT FWD CARGO BAY; BS 500A +12; BL0; WL 148 PER SRM 51-40-02-0G-0.; [04] LOCATED; DRILLED; DEBURRED NEW DOUBLER; INSTALLED NUTPLATES PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 143A3230; DWG 143A3233. OK TO INSTALL.; [05] VERIFIED CORRECTIVE ACTION 3 AND 4.<BR><BR>OK TO INSTALL NEW DOUBLER.; [06] INSTALLED DOUBLER PER SRM 51-40-02-0G-0 ; DWG 143A3230; DWG 143A3233; FASTENERS THROUGH SKIN AND CLIPS.; [07] VERIFIED CORRECTIVE ACTION 6. <BR><BR>DOUBLER INSTALLED.; [08] INSTALLED ANTENNA BLANK OUT PLATE PER SRM 51-40-02-0G-0 USING SCREW GUN ID:NCX001167 SN: UNKNOWN. APPLIED FILLET SEAL PER AMM 51-31-00-390-804. BELLY SKIN PAINT TOUCH UP TO BE ACCOMPLISHED ON CUSTOMER CARD # TTG8Q0067YJQ.; [09] RII INSPECTED REPAIR COMPLETION PER SRM 51-40-02 AND DWG 143A3230 AND DWG 143A3233.; [10] VERIFIED REPAIR COMPLETION PER SRM 51-40-02 AND DWG 143A3230 AND DWG 143A3233; REFINISH ON TTG8Q0067YJQ; JOB COMPLETE.

Part: FLOORBEAM — CRACKED (BS 540 BL0-RBL25) · airframe 74,723 hrs · 44,099 cycles

CRACKED FLOOR SUPPORT AT B.S 540; B.L. 0 - R.B.L. 24.5; W.L. 208.1. ; / [01] REMOVED FLOOR SUPPORT AT BS540 RBL24.5 PER SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS540 RBL24.5 PER SRM 51-40-05-0G-0; OK TO INSTALL; [03] VERIFIED CORRECTIVE ACTION #2. OK TO INSTALL GIVEN.; [04] INSTALLED FLOOR SUPPORT AT BS 540 BLO-RBL24.5 WL 208 PER SRM 51-40-02-0G-0 AND DWG #143A0060; [05] VERIFIED CORRECTIVE ACTION 4.<BR><BR>FLOOR SUPPORT REPLACED.; [06] FLOOR SUPPORT AT BS540; BL0 - RBL24.5; WL208.1 REPLACED. ALL WORK ACCOMPLISHED.

Part: WEB — CORRODED (F CRGO THRESHOLD) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS455 RBL28 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIGINAL 0.045 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [02] VERIFIED EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIGINAL 0.045 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [03] REMOVED FORWARD CARGO BAY SUB THRESHOLD WEB PER SRM 51-40-02-0G-0; [04] LOCATED; DRILLED; DEBURRED NEW SUBTHRESHOLD WEB; INSTALLED NUTPLATES; PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 143A8330.; [05] VERIFIED CORRECTIVE ACTION 4.; [06] OK TO INSTALL; [07] INSTALLED FWD CARGO BAY SUBTHRESHOLD WEB IAW SRM 51-40-02-0G-0 ;DWG #143A8330; [08] VERIFIED INSTALLED FWD CARGO BAY SUBTHRESHOLD WEB IAW SRM 51-40-02-0G-0 ;DWG #143A8330

Part: SUPPORT — CORRODED (BS 500B RBL 24) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500B+19 RBL24 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIGINAL 0.040 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [02] VERIFIED EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIGINAL 0.040 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [03] REMOVED FLOOR TO SIDEWALL SUPPORT BS 500A-500D; RBL24; WL 156 PER SRM 51-40-02-0G-0.; [04] LOCATED; DRILLED AND APPLIED CHEMICAL CONVERSION COATING TO FLOOR TO SIDEWALL SUPPORT AT FCB BS500B TO BS500D RBL24 WL156 PER SRM 51-40-05-0G-0; DWG 143A7500 AND AMM 51-21-41-370-802; [05] LOCATED; DRILLED AND APPLIED CHEMICAL CONVERSION COATING TO FLOOR TO SIDEWALL SUPPORT AT FCB BS500A TO BS500D RBL24 WL156 PER SRM 51-40-05-0G-0; DWG 143A7500 AND AMM 51-21-41-370-802; [12] OK TO INSTALL FLOOR TO SIDEWALL SUPPORT; [13] INSTALLED FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-02-0G-0; DWG 143A7500; AND DWG143A7505; [14] VERIFIED STEP 13; [15] RII INSPECTED ACTION 13; [16] INSTALLED FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-02-0G-0; DWG 143A7500; AND DWG 143A7505

Part: SUPPORT — CORRODED (BS 500-500C) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500 - BS500C LBL24 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIGINAL 0.040 IN 1'X60' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [02] VERIFIED EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIGINAL 0.040 IN 1'X60' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN; [03] REMOVED FLOOR TO SIDEWALL SUPPORT BS 396-500D RBL 24; WL 156 PER SRM 51-40-02-0G-0.; [04] SHOULD READ LBL 24; NOT RBL.; [05] FABRICATED NEW L/H FLOOR TO SIDEWALL SUPPORT BS 396 TO 500D AND SPLICE DOUBLER FROM EXTRUSION BAC1496-444#7075 T62 CLAD LOT# 1466234-1 PER SRM 51-40-05-0G-0; SRM 53-00-53-2R-5; DWG 143A7501; DWG 143A7500; [06] VERIFIED STEP 5; [07] VERIFIED CORRECTIVE ACTION STEP 5<BR>OK TO APPLY CHEMICAL CONVERSION AND PRIMER; [11] INSTALLED SPLICE DOUBLER PER SRM 53-00-53-2R-5 AND DWG 143A7501; [12] CERTIFIED STEP 11; [13] RII INSPECTED GOOD INSTALLATION OF SPLICE DOUBLER PER SRM 53-00-53-2R-5 AND DWG 143A7501.; [14] SRM SPLICE REPAIR LOCATION IS AT BS 480+8'; [15] VERIFIED LOCATION OF SRM SPLICE REPAIR; [16] VERIFIED CORRECTIVE ACTION ITEMS 14 AND 15; [17] OK TO INSTALL L/H FLOOR TO SIDEWALL SUPPORT; [18] OK TO INSTALL; [19] INSTALLED FCB NEW FLOOR TO SIDEWALL SUPPORT AT BS396 - BS500D; LBL24; WL156 PER SRM 51-40-020G-0 AND DWG 143A7500

Part: FLOORBEAM — CRACKED (BS 540 BL0-LBL25) · airframe 74,723 hrs · 44,099 cycles

CRACKED FLOOR SUPPORT AT B.S 540; B.L. 0 - L.B.L. 24.5; W.L. 208.1. ; / [01] REMOVED FLOOR SUPPORT AT BS540 LBL24.5 PER SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 540;BL0-LBL24.5 PER SRM 51-40-05-0G-0 ; OK TO INSTALL; [03] VERIFIED CORRECTIVE ACTION #2. OK TO INSTALL GIVEN.; [04] INSTALLED FLOOR SUPPORT AT BS 540 BL0-LBL24.5 WL 208 PER SRM 51-40-02-0G-0 AND DWG#143A0060; [05] VERIFIED CORRECTIVE ACTION 4.<BR><BR>FLOOR SUPPORT REPLACED.; [06] FLOOR SUPPORT AT BS540; BL0 - LBL24.5; WL208.1 REPLACED. ALL WORK ACCOMPLISHED

Part: WEB — CORRODED (BS 452 THRESHOLD) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS452 RBL28 WL156. ; / [01] EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN. SUB THRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q0063WWM; [02] CARD COMPLETE; [03] VERIFIED EVALUATED CORROSION; FOUND 0.015 REMOVED FROM ORIG 0.045 IN A 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING DIAL DEPTH GAUGE ATS 2472 S/N UNKNOWN. SUB THRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q0063WWM

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 74,723 hrs · 44,099 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED (MARKED) ; / [01] UPDATED MEASUREMENTS; [02] WELDED CRACK ON ACB; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT#1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(2) AND (4)<BR>CALIBRATION I.D. E10583; S/N KJ256554; [03] VERIFIED CORRECTIVE ACTION 1 AND 2; [04] DYE PENETRANT INSPECTED WELDED AREA PER SOPM 20-20-02. NO DEFECTS NOTED. RADIOMETER ID ATS2504; S/N 191348; [05] SANDED WELD REPAIR AREA IAW SRM 53-60-15-2R-1 PARA 4.B.(5); [06] VERIFIED CORRECTIVE ACTION 5; [07] APPLIED CHEMICAL CONVERSION COATING AND PRIMED REPAIR AREA PER SRM 53-60-15-2R-1; [08] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIMED REPAIR AREA PER SRM 53-60-15-2R-1

Part: STRINGER — CORRODED (BS 520 S26L) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON END OF STRINGER 26 LEFT AT B.S. 520+15; W.L. 152.. ; / [01] UPDATED MEASURING TABLE; [02] REMOVED DAMAGED SECTION OF S-26L BS 500D+10'- 540 AND PERFORMED GVI NO ADDITIONAL DAMAGED FOUND ON REPAIR AREA IAW SRM 53-00-03-2R-1 REP.1;07] UPDATED MEASUREMENT TABLE; [08] CERTIFIED STEPS 1 AND STEP 7; [09] RECEIVED REPAIR STRINGER AND HAT SECTION FABRICATED AT OSS ON SWA PO# 834064 FOR STR AND 834071 FOR HAT SECTION DATED 19 AUG 21 AND 20 AUG 21; [10] VERIFIED CORRECTIVE ACTIONS 6 TO 9; [11] LOCATED DRILLED AND TRIMMED NEW STRINGER REPAIR SECTION FABRICATED FROM 7075-T0 .045 LOT # 1439668-1 HEAT TREATED TO T6 CONDITION ALL ON SWA PO# 834064 HAT REPAIR SECTION FABRICATED FROM 7075-T0 .050 LOT #1442011-1 HEAT TREATED TO T6 CONDITION ALL ON SWA PO# 834071 APPLIED CHEMICAL CONVERSION TO REPAIR PARTS AND REPAIR AREA ALL IAW SRM 51-40-05-0G-0 AND SRM 53-00-03-2R-1 STEPS 4 E F G H AND I OK TO PRIME; [12] VERIFIED CORRECTIVE ACTION ITEM 11 OK TO PRIME; [15] INSTALLED REPAIR PARTS BS 500D+6'-540 S-26L IAW SRM 51-40-02-0G-0 AND DWG 143A3230;143A1215.

Part: STRINGER — CRACKED (BS 520 S25L) · airframe 74,723 hrs · 44,099 cycles

CRACKED STRINGER END ON STRINGER 25 LEFT AT B.S. 520+15. ; / [01] REMOVED DAMAGED SECTION OF S-25L BS 500D+10'- 540 AND PERFORMED GVI NO ADDITIONAL DAMAGED FOUND ON REPAIR AREA IAW SRM 53-00-03-2R-1 REP.1; [02] VERIFIED CORRECTIVE ACTION 1; [03] REQUIRED NDI FOR CRACK FREE VERIFICATION AFTER DAMAGED REMOVAL S-25L BS500D+10' IAW SRM 53-00-03-2R-1-REP.1; [04] HFEC INSPECTED CUTOUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [05] UPDATED MEASUREMENT TABLE; [06] VERIFIED; [07] RECEIVED REPAIR STRINGER SECTION AND HAT SECTION FROM OSS FABRICATED ON SWA PO#834067 FOR STR AND 834072 FOR HAT SECTION DATED 20 AUG 21 AND 19 AUG 21; [08] VERIFIED CORRECTIVE ACTION 7.; [09] LOCATED DRILLED AND TRIMMED NEW STRINGER REPAIR SECTION FABRICATED FROM 7075-T0 .045 LOT # 1439668-1 HEAT TREATED TO T6 CONDITION ALL ON SWA PO# 834067 HAT SECTION FABRICATED FROM 7075-T0 .050 LOT # 1457313-101 AND HEAT TREATED TO T6 CONDITION ON SWA PO# 834072 APPLIED CHEMICAL CONVERSION TO REPAIR PARTS AND REPAIR AREA ALL IAW SRM 51-40-05-0G-0 AND SRM 53-00-03-2R-1 STEPS 4 E F G H AND I OK TO PRIME; [10] VERIFIED CORRECTIVE ACTION ITEM 9 OK TO PRIME; [11] PRIMED REPAIR PARTS AND REPAIR AREA AT BS 500D+10 TO 540 STR 25L WL 152 IAW SRM 53-00-03-2R-1 STEP 4 J OK TO INSTALL; [13] INSTALLED REPAIR PARTS BS 500D+6'-540 S-25L IAW SRM 51-40-02-0G-0 AND DWG 143A3230;143A1215.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 74,723 hrs · 44,099 cycles

PANEL 193AR HAS (8EA) ELONGATED ATTACH HOLES (MARKED) ; / [01] PART/MATERIAL IDENTIFIED PER SRM 53-40-70-0I-1 FIG 2 TABLE 2 ITEM 18 . <BR>PREVIOUS EDGE BAND REPAIRS FAILED ; DAMAGE EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-40-70-1A-1 PARA 4 B. <BR>REPAIR TO BE PERFORMED IAW SRM 51-70-05-2R-6 AS GIVEN IN SRM 53-40-70-2R-1 PARA 4 D REF TABLE 202; [02] VALIDATED APPLICABILITY OF REPAIR TO PANEL 193AR EDGEBAND TO BE COMPLETED IAW SRM 51-70-05-2R-6.; [03] VERIFIED CORRECTIVE ACTION 1 PER SRM 53-40-70-0I-1; SRM 53-40-70-1A-1; AND SRM 51-70-05-2R-6 <BR>VALIDATED REPAIR PER SRM 51-70-05-2R-6; [04] PERFORMED DAMAGE REMOVAL & SURFACE PREPARATION STEPS IAW SRM 51-70-05-2R-6 PARA 4 STEPS A-D; [05] INSPECTED ACTION 4; FABRICATED REPAIR PLIES THEN STARTED LAY UP & PLY COMPACTION IAW SRM 51-70-05-2R-0 PARA 4 K 1; [07] COMPLETED THE PLY COMPACTION AS GIVEN IN SRM 51-70-05-2R-0 PARA 4 K 1.<BR>COMPLETED THE REPAIR LAYUP VACUUM BAGGED LEAK CHECKED & SET FOR CURE IAW SRM 51-70-05-2R-6 PARA 4 STEPS E & F; [08] CURED THE REPAIR IAW SRM 51-70-05-2R-6 PARA 4 STEP G<BR>REF CAL TOOL HOT BONDER ID ATS532 SN 15092117; [09] VERIFIED CORRECTIVE ACTION ITEMS 6; 7; AND 8.; [10] UT INSPECTED REPAIR PER NDTM PART 4; 51-00-02. NO DISBONDS NOTED.<BR>CAL ID: ATS2341 S/N: 190848104; [11] REFINISHED INNER SURFACE IAW SRM 51-70-05-2R-6 PARA 4I.<BR>APPLIED CONDUCTIVE COATING TO OUTER SURFACE; <BR>RESISTIVITY TESTED GOOD WITH MULTIMETER ID:ATS1658 S/N:34000350<BR>IAW AMM 51-21-71-370-801 PARA 3D(1-4)(7).; [

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 74,723 hrs · 44,099 cycles

PANEL 193AR DELAMINATED ON OUTER SURFACE; 7' FROM FWD EDGE; 31.25' FROM I/B EDGE. ; / [01] PART/MATERIAL IDENTIFIED PER SRM 53-40-70-0I-1 FIG 2 TABLE 2 ITEM 18 . <BR>PREVIOUS REPAIR FAILED ; DAMAGE EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-40-70-1A-1 PARA 4 A. <BR>REPAIR TO BE PERFORMED IAW SRM 51-70-05-2R-3 AS GIVEN IN SRM 53-40-70-2R-1 PARA 4 D REF TABLE 201; [02] CORRECTION FOR CORRECTIVE ACTION LINE 1; CHANGING 'SRM 51-70-05-2R-3' TO 'SRM 51-70-05-2R-2'. [19] VERIFIED CORRECTIVE ACTION ITEMS 13 - 18.; [20] UT INSPECTED REPAIR PER NDTM PART 4; 51-00-02. NO DISBONDS NOTED.<BR>CAL ID: ATS2341 S/N: 190848104; [21] APPLIED CONDUCTIVE COATING TO OUTER SURFACE; <BR>RESISTIVITY TESTED GOOD WITH MULTIMETER ID:ATS1658 S/N:34000350<BR>IAW AMM 51-21-71-370-801 PARA 3D(1-4)(7).; [22] BEGAN REFINISHING BY APPLYING PRIMER TO EXTERIOR SURFACE IAW AMM 51-21-99-300-801.; [23] ADDITIONAL REFINISHING REFERENCE USED: SRM 51-70-05-2R-2 PARA 4K.; [24] CERTIFIED CORRECTIVE ACTIONS 22+23.; [25] COMPLETED FINAL REFINISH OF PANEL IAW SRM 51-70-05-2R

Part: CROSSBEAM — CORRODED (BS 295 R-LBL 9) · airframe 74,723 hrs · 44,099 cycles

CORROSION ON AFT EDGE OF LATERAL BEAM 259.5; WL208.1; LBL 9 TO RBL 9. ; / [01] UPDATED MEASUREMENT TABLE; [02] REMOVED CORROSION ON AFT EDGE OF LATERAL BEAM BS259.5 WL208.1 LBL9 TO RBL9 IN A 1.2'X 15' AREA IAW SRM 51-10-02-0G-0; [17] REPAIRED DAMAGE ON AFT EDGE OF LATERAL BEAM BS 259.5; WL 208.1; LBL 9 TO RBL 9 PER EA 21-153-02384 (N755SA - ATS (PAE) - REPAIR - BS 259.5 BULKHEAD AFT CHORD REPAIR BETWEEN LBL 20 AND RBL 20; WL 208) [TTG8Q006CRDD].; [18] VERIFIED REPAIR OF DAMAGE ON AFT EDGE OF LATERAL BEAM BS 259.5; WL 208.1; LBL 9 TO RBL 9 PER EA 21-153-02384 (N755SA - ATS (PAE) - REPAIR - BS 259.5 BULKHEAD AFT CHORD REPAIR BETWEEN LBL 20 AND RBL 20; WL 208) [TTG8Q006CRDD].; [19] VERIFIED REPAIR OF DAMAGE ON AFT EDGE OF LATERAL BEAM BS 259.5; WL 208.1; LBL 9 TO RBL 9 PER EA 21-153-02384 (N755SA - ATS (PAE) - REPAIR - BS 259.5 BULKHEAD AFT CHORD REPAIR BETWEEN LBL 20 AND RBL 20; WL 208) [TTG8Q006CRDD].

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 74,723 hrs · 44,099 cycles

LT HORIZ. STAB RIB ASSY. 4 (STAB STA 120.30) 3RD VERT STIFFENER IS CRACKED. ; / [01] REMOVED CRACK DAMAGE LOWER RADIUS OF 3RD VERTICAL STIFFENER AND WEB L=0.85' X W=0.35' IAW SRM 55-10-09-2R-4 ITEM 4 STEP B.; [02] VERIFIED REMOVAL OF CRACK DAMAGE AND PERFORMED GVI PER SRM 55-10-09-2R-4 STEP 4.B AND E; [05] FABRICATED REPAIR PARTS.T-SECTION 60-5872#7075T76511 0.063' THICK LOT # 1430775-2; ANGLE BAC1490-2793#7075T62 0.063' LOT # 1435997-1; SHIM 2.E.A 7075T6 0.016' THICK LOT # 1439717-1 IAW SRM 55-10-09-2R-4 REPAIR 4. ITEM 4 STEP F-J. FIGURE 202 REPAIR 4 DETAIL A.[11] INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4 REPAIR 4 ITEM 4 STEPS M-P.; [12] VERIFIED CORRECTIVE ACTION 11; [13] APPLIED FILLET SEAL AND FINISH TO REPAIR PARTS IAW SRM 55-10-09-2R REPAIR 4 ITEM 4 STEPS Q & R.; [14] VERIFIED CORRECTIVE ACTION 13; [15] REMOVED LEFT HORIZONTAL STABILIZER RIB ASSY AT STAB STA 120.30 PRIOR TO PERFORMING REPAIR IAW SRM 51-40-02-OG-0.; [18] INSTALLED LEFT HORIZONTAL STABILIZER RIB ASSY AT STAB STA 120.30 IAW SRM 51-40-02-OG-0; BOEING DRAWINGS #182A1500; 182A3001 AND 002A0001.;[20] REMOVED CRACK DAMAGE ON LEFT HORIZONTAL STABILIZER RIB ASSY AT STAB STA 120.30 3RD VERTICAL STIFFENER LOWER RADIUS AND WEB AND INSTALLED REPAIR IAW SRM 55-10-09-2R 4 FIGURE 202 REPAIR 4 DETAIL A.; [21] VERIFIED REMOVED CRACK DAMAGE ON LEFT HORIZONTAL STABILIZER RIB ASSY AT STAB STA 120.30 3RD VERTICAL STIFFENER LOWER RADIUS AND WEB AND INSTALLED REPAIR IAW SRM 55-10-09-2R 4 FIGURE 202 REPAIR 4 DETAIL A.

Part: BEAM — CRACKED (R1 DOOR) · airframe 74,723 hrs · 44,099 cycles

UPON COMPLETION OF HFEC INSPECTION; FOUND #4 BEAM TO BE CRACKED COMMON TO THE FORWARD SERVICE DOOR ; / [01] FWD SERVICE DOOR #4 BEAM REPAIRED ON CUSTOMER RO NO: P0670359-1; JOB NUMBER: 541772 SENT OUT ON CCN: TTG8Q0061FYA.; [02] VERIFIED FWD SERVICE DOOR #4 BEAM REPAIRED ON CUSTOMER RO NO: P0670359-1; JOB NUMBER: 541772 SENT OUT ON CCN: TTG8Q0061FYA.

Part: PANEL — CRACKED (RT WING TE) · airframe 74,723 hrs · 44,099 cycles

RT WING UPPER T/E PANEL JUST AFT OF #2 PYLON HORIZ. SEAL RETAINER IS CRACKED. ; / [01] UPDATED MEASUREMENT SECTION; [02] REMOVED AND REPLACED SEAL RETAINER ON RT WING UPPER T/E PANEL JUST AFT OF #2 PYLON IAW SRM 51-40-02-0G-0 STEP 4; IPC 57-50-00-25; AND MM 20-50-11-910-801.<BR>CAL TOOL: ID# 7957G S/N A96F11016; [03] VERIFIED REPLACED SEAL RETAINER ON RT WING UPPER T/E PANEL JUST AFT OF #2 PYLON IAW SRM 51-40-02-0G-0 STEP 4; IPC 57-50-00-25; AND MM 20-50-11-910-801.<BR>CAL TOOL: ID# 7957G S/N A96F11016

Part: PANEL — CHAFED (FAIRING 193CR) · airframe 74,723 hrs · 44,099 cycles

FAIRING PANEL # 193CR HAS CHAFFING ALONG THE EDGES OF THE INTERNAL SIDE OF PANEL AND 2 OVERSIZED HOLES ON INBOARD EDGE OF PANEL ; / [01] IDENTIFIED MATERIAL OF PANEL 193CR IAW SRM 53-40-70-0I-1 FIGURE 1-2; ITEM #9; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 TABLE 101; PARA 4.B(2)<BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05 PER SRM 53-40-70-2R-1 PARA 4.B(2); [08] INNER SURFACE: REFINISHED REPAIR AREA IAW AMM 51-21-99-300-802 PARA 3.C(1) <BR><BR>OUTER SURFACE: APPLIED AND CURED CONDUCTIVE COATING; RESISTANCE CHECK 'GOOD' IAW AMM 51-21-71-370-801 PARA 3.D(2-4) AND 3.D(7)(A)<BR><BR>FLUKE 62 IR THERMOMETER ID ATS2209 SN 43300739WS<BR>FLUKE 77 MULTIMETER ID ATS1658 SN 34000350<BR><BR>REFINISHED REPAIR AREAS IAW AMM 51-21-99-300-802 PARA 3.C(1)<BR><BR>REPAIRED CHAFING DAMAGE ALONG INNER MATING SURFACE AND 2EA OVERSIZED OF PANEL 193CR IAW SRM 51-70-05-2R-6; [09] REPAIRED CHAFING DAMAGE ALONG INNER MATING SURFACE AND 2EA OVERSIZED OF PANEL 193CR IAW SRM 51-70-05-2R-6; [10] VERIFIED CORRECTIVE ACTIONS 8 AND 9 PER AMM 51-21-99-300-802; AMM 51-21-71-370-801; AND SRM 51-70-05-2R-6<BR><BR>VERIFIED COMPLETION OF PANEL 193CR REPAIR PER SRM 51-70-05-2R-6

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 74,723 hrs · 44,099 cycles

B.S 663 LOWER COMPOSITE BULKHEAD VERTICAL SUPPORT STIFFENER IS CRACKED ON AFT SIDE OF BULKHEAD; AT L.B.L. 26; W.L. 150. ; / [01] REMOVED VERTICAL SUPPORT STIFFENER BS 663 LBL 26 WL 150 IAW SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW VERTICAL SUPPORT STIFFENER P/N 111A1308U15ATSMRO AT BS 663 LBL26 WL 150 IAW SRM 51-40-05-0G-0 AND DWG 111A1000. OK TO INSTALL.; [03] OKAY TO INSTALL SUPPORT STIFFENER P/N 111A1308U15ATSMRO AT BS 663 LBL 26 WL150.; [04] INSTALLED NEW VERTICAL SUPPORT STIFFENER P/N 111A1308U15ATSMRO AT BS 663 LBL26 WL 150 IAW SRM 51-40-02-0G-0 AND DWG 111A1000.; [05] RII INSPECTED STIFFENER INSTALLATION PER SRM 51-40-02 AND DWG 111A1000.; [06] VERIFIED STEPS 1-5.; [07] VERIFIED ALL CORRECTIVE ACTION ITEMS COMPLETE; JOB COMPLETE.

Part: GUIDE ARM — INOPERATIVE (L1 DOOR) · airframe 73,980 hrs · 43,665 cycles

MAIN FWD ENTRY DOOR DID NOT SEAL PROPERLY UPON TAKEOFF+ DEPARTURE OVERHEAD LIGHT DID NOT ILLUMINATE. AIR RETURNED TO MDW NO; REMOVED AND REPLACED L1 DOOR GUIDE ARM IAW AMM 521121; REPLACED DOOR WARNING SWITCH S1147 IAW 527111 OPS CK GOOD

Part: SENSOR — STUCK (FLAP SKEW) · airframe 73,211 hrs · 43,216 cycles

FLAPS 2 SELECTED INDICATED BETWEEN UP AND 1. LEADING EDGE FLAP TRANSIT LIGHT REMAINED ON. ASYMMETRY NOTED-STUCK BETWEEN FLAPS UP AND 1. BRAKE COOLING PROCEDURES COMPLETED. PERFORMED FIM 27-51 TASK 836 FOUND NO CURRENT FAULTS BUT FLT LEG O SHOWS 27-53252. R & R NR 3 FLAP SKEW SENSOR, PER M/M 27-59-00 PN OFF ON 9000421-2 SN OFF 17609 SN ON 13225.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 72,336 hrs · 42,647 cycles

PASSENGER FLOOR TRACK IS CRACKED AT PASSENGER SEAT ROW 15ABC, REPLACED FLOOR TRACK AT 15 ABC PER SIP

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,011 hrs · 42,440 cycles

AFT RT EMERGENCY LIGHT INOP. REMOVE AND REPLACE AFT RT EMERGENCY LIGHT PER AMM 33-51-04.

Part: ARM — LACK OF LUBE (COCKPIT) · airframe 71,518 hrs · 42,138 cycles

TAKEOFF WARNING ORN SOUNDED ON TAKEOFF TRIM 5.3; FLAPS 1; SPEEDBRAKE LEVER DOWN. / FOUND S132 TAKEOFF WARNING SWITCH ROLLER ARM REQUIRING LUBRICATION. PERFORMED TAKEOFF WARNING TEST IAW 31-51-00. OK FOR CONTINUED SERVICE

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 71,482 hrs · 42,112 cycles

R1 DOORSLIDE MAY NEED ADJUSTMENT REPOSITIONED R1 DOORSLIDE PER MT 725-61-06

Part: LENS — MISSING (EXIT SIGN) · airframe 70,831 hrs · 41,695 cycles

MID CABIN EXIT SIGN AFT COVER MISSING. / R&R LENS PER AMM.

Part: SNUBBER — OUT OF POSITION (R1 DOOR) · airframe 70,034 hrs · 41,182 cycles

R1 DOOR AFT PORITON OF GIRT BAR CONTACTED DOOR FRAME WHEN OPENED. R&R SNUBBER ON R1 DOOR.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 69,992 hrs · 41,157 cycles

L1 DOOR SLIDE GIRT FLAP CAME OUT OF THE SLIDE COMPARTMENT. / REPOSITIONED SLIDE IAW AMM.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 69,725 hrs · 40,986 cycles

R1 DOOR SLIDE NOT STOWED PROPERLY. REPOSITIONED GIRT BAR MATERIAL PER AMM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,689 hrs · 40,968 cycles

R/H OVERWING DOOR EMERGENCY EXIT SIGNS INOP. / R&R FUSES AT POWER SUPPLY FOR EMERGENCY BATTERY M1669 PER AMM.

Part: LIGHT — INOPERATIVE (SEAT 8) · airframe 69,689 hrs · 40,968 cycles

R/H OVERHEAD BIN EMERGENCY LIGHT INOP AT SEAT 8. REPAIRED LIGHT PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 69,689 hrs · 40,968 cycles

EMERGENCY LIGHT BATTERY PACK FAILED AT M1669. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 69,689 hrs · 40,968 cycles

EMERGENCY LIGHT BATTERY PACK FAILED AT M1674. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 69,689 hrs · 40,968 cycles

EMERGENCY LIGHT BATTERY PACK FAILED AT M1670. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 69,689 hrs · 40,968 cycles

EMERGENCY LIGHT BATTERY PACK FAILED AT M1668. R&R BATTERY PACK PER AMM.

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 69,689 hrs · 40,968 cycles

LOWER CHORD FASTENER HOLE CRACKED AT R/H HORIZONTAL STABILIZER RIB NR 5 ,15" FROM FORWARD END. REPAIRED THE STABILIZER STRUCTURE PER EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,689 hrs · 40,968 cycles

R/H HORIZONTAL STABILIZER LOWER INBOARD CHORD FASTENER HOLE CRACKED AT NR 5 RIB NEXT TO STIFFENER NR 2. REPAIRED THE RIB IAW SRM.

Part: STRINGER FITTING — CRACKED (FUSELAGE) · airframe 69,689 hrs · 40,968 cycles

ELONGATED BOLT HOLD NOTED ON FWD AND AFT STRINGER END FITTING AT STA 1016 S-2L-HOLE 5L / REMOVED FWD AND AFT STRINGER END FITTING; REAMED HOLE SL AT FWD STRINGER END FITTING TO 0.484 AND REAMED HOLE 5L AT AFT STRINGER END FITTING TO 0.469 AT STA 1016 S-2L. REINSTALLED FWD AND AFT STRINGER END FITTING AT STA 1016 S-2L PER REF SI 12107-53 AND SRM 51-40-02-0G-0

Part: FITTING — CRACKED (R1 DOOR SLIDE) · airframe 69,689 hrs · 40,968 cycles

R1 DOOR ADJUSTMENT, ESCAPE SLIDE, AFT SUPPORT FITTING CRACKED ON DOOR. R&R FITTING PER SRM.

Part: WEB — CORRODED (BS 344-360) · airframe 69,689 hrs · 40,968 cycles

INTERCOSTAL CORRODED BETWEEN BS. 344+12 TO BS. 360, STR. 28L. / R&R WEB PER DWG AND SRM.

Part: RETAINER — CRACKED (WHEEL WELL RH) · airframe 69,689 hrs · 40,968 cycles

RT WHEEL WELL VAPOR SEAL DUCT RETAINER CRACKED AROUND THE NUT PLATE / REMOVED AND REPLACED CRACKED DUCT RETAINER AT RT WHEEL WELL VAPOUR SEAL AS PER BOEING 737 SRM 51-40-02-0G-9 737 AND SRM 51-40-05-0G-0.

Part: STRINGER — OUT OF TOLERANCE (AFT FUSELAGE) · airframe 69,689 hrs · 40,968 cycles

MEASURED THE INNER HOLE DIAMETER FOR HOLE 5L AT STR-2L; STA 1016; MEASURE 0.380 INCHES ;FOUND OUT OF TOLERANCE. / REAMED HOLE #5L AT STR 2L STA 1016 TO .3906' IAW CUSTOMER CARD 11407 AND SB 737-53-1249 HOLE #5L IS TRUE AND ROUND STEP 5A

Part: WEB — CRACKED (BS 663-675) · airframe 69,689 hrs · 40,968 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN LBL 30 TO LBL 60, AT THE EDGE OF STIFFENING BEAD. REPAIRED WEB IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 69,689 hrs · 40,968 cycles

R/H HORIZONTAL STABILIZER RIB 5 CRACKED AT STIFFENER 3 LOWER CORNER. REPAIRED STIFFENER #3 IAW SRM.

Part: FAIRING — ELONGATED (LWR FUSELAGE) · airframe 68,754 hrs · 40,379 cycles

FASTENER HOLE ENLARGED AT POSITION 17 ON PANEL 193B / REMOVED AND REPLACED PANEL PER SRM 51-20-07 AND SRM 51-40-02

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 68,311 hrs · 40,109 cycles

R1 DOOR SLIDE OUT OF ADJUST. R&R SLIDE PER MT.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 66,640 hrs · 39,022 cycles

R2 DOOR SLIDE GIRT FLAP "Z" FOLD LOOSE. SECURED Z FOLD IAW AMM.

Part: CONTROL MODULE — FAULTY (COCKPIT) · airframe 66,615 hrs · 39,007 cycles

DIVERSION, ON TAKEOFF, GEAR HANDLE DIFFICULT TO BRING TO UP POSITION. R&R LANDING GEAR CONTROL LEVER MODULE PER AMM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 65,925 hrs · 38,572 cycles

R1 DOOR SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE ASSEMBLY PER MT.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 65,888 hrs · 38,547 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL PARTIALLY OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,557 hrs · 38,304 cycles

FORWARD ENTRY EMERGENCY EXIT LIGHT ON HEADER PANEL INOP AT LOCATION M1674. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,557 hrs · 38,304 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 65,557 hrs · 38,304 cycles

RIGHT MAIN WHEEL WELL BULKHEAD WEB CRACKED AT BS 663, RBL 40. REPAIRED THE BULKHEAD WEB IAW EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,557 hrs · 38,304 cycles

LEFT FORWARD EMERGENCY LIGHT BATTERY INOPERATIVE. R & R THE BATTERY IAW AMM.

Part: LENS — MISSING (SIGN) · airframe 65,015 hrs · 37,968 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED THE LENS IAW SIP.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 64,186 hrs · 37,437 cycles

FORWARD ENTRY EMERGENCY FLASHLIGHT SECURITY STRAP BROKEN. INSTALLED A STRAP IAW SIP.

Part: COVER — MISSING (EXIT SIGN) · airframe 63,956 hrs · 37,297 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER AFT MISSING. INSTALLED SIGN PER SIP.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO R/H FWD AND AFT CAPS STRIP IS CORRODED / REMOVED AND REPLACED FWD AND AFT RH CAPSTRIPS IAWSRM51-40-02-0G-0STEP 9BL AND DWG#453A2600 REV D.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,236 hrs · 36,810 cycles

AFT OVERWING EXTERIOR EMERGENCY EGRESS LIGHT INOP. R&R LIGHT IAW AMM.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO COMP. FLOOR PANEL SPLICE STRAP CORRODED AT STA. 767+4 BETWEEN PANEL 140CF AND 140BF / REMOVED AND REPLACED AFT CARGO COMP. FLOOR PANEL SPLICE STRAP AT STA. 767+4' BETWEEN PANEL 140CF AND 140BF I/A/W 737 AMM 25-52-10-400-801 TAG WN 1627

Part: TRUNNION — CORRODED (LT MLG) · airframe 63,236 hrs · 36,810 cycles

LEFT FORWARD TRUNNION FITTING LUG CORRODED. REPAIRED THE TRUNNION FITTING IAW EA.

Part: FITTING — CORRODED (RT MLG) · airframe 63,236 hrs · 36,810 cycles

RIGHT FORWARD TRUNNION FITTING LUG CORRODED. REPAIRED THE TRUNNION FITTING IAW EA.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,236 hrs · 36,810 cycles

INTERCOASTAL CRACKED AT STA. 380 TO STA. 400 BL.0 / INTERCOSTAL ANGLE IS CRACKED AT FLOOR LEVEL STA 380 TO STA 400 BL-O-. REMOVED AND REPLACED ANGLE P/N 143A5410-170 IAW B737-700 SRM 51-40-02-0G-0;51-40-05-0G-0 AND DWG 143A5400 REV A. APPLIED CIC TO ANGLE AND ADJACENT INTERCOSTAL IAW B737-700 AMM 51-21-91-620-802 TAG A85059

Part: ANGLE — CRACKED (BS 500B) · airframe 63,236 hrs · 36,810 cycles

FORWARD CARGO BAY VERTICAL WEB ATTACH ANGLE FOUND CRACKED AT BS 500B, BETWEEN STRINGERS 25L TO 26L. R & R THE ANGLE IAW DWG & SRM.

Part: FLAP — DELAMINATED (LH OUTBD AFT FLA) · airframe 63,236 hrs · 36,810 cycles

L/H OUTBD FLAP; INBD CORNER OF AFT FLAP DELAMED. / REPAIRED L/H OUTBD FLAP INBD CORNER OF AFT FLAP IAW 737-700 SRM 51-70-10-2R-1 PAR 3 D-F REV 62

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO PIT BAFFLE CRACKED BETWEEN STA 500 AND 500A LBL 21 / REMOVED AND REPLACED CRACKED BAFFLE BETWEEN BS 500 AND 500A LBL 21 IAW SRM 51-40-02-0G-0 AND BOEING DWG # 143A7505 APPLIED CIC IAW AMM 51-21-91-620 ATG # A79030

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

AFT WASTE WATER SERVICE PAN CHANNEL IS CRACKED / REMOVED AND REPLACED CHANNEL AT AFT WASTE WATER SERV ICE PAN IAW SRM 51-40-02-0GO; 51-40-05-0G-0; SOPM 20 -41-05; BOEING DWG# 146A7402 REV B. AND DWG# 146A740 1 REV-

Part: RETAINER — BENT (GIRT BAR) · airframe 63,236 hrs · 36,810 cycles

R1 DOOR EMERGENCY EVAC SLIDE FORWARD GIRT BAR RETAINER BENT. R&R RETAINER IAW SRM.

Part: FRAME — ELONGATED (LWR FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

ELONGATED HOLE ON FRAME AT STA 500 ABOVE STR 25L AT Z ANGLE ATTACH POINT / CUT OUT AND REMOVED DAMAGED HOLE ON FRAME AT STA 500 ABOVE STR 25L AT Z ATTACH POINT. ACCOMPLISHED HFEC INSPECTION OF CUT OUT AND ALL OPEN HOLES NO DEFECTS NOTED. FABRICATED REPAIR PARTS AND INSTALLED I/A/W EA 170278 REV IR AND S/W EA 1-753-31453 REV IR

Part: SPLICE STRAP — CORRODED (AFT CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO FLOOR PANEL SPLICE AT STA 727D + 3 IS CORRODED / REMOVED AND REPLACED AFT CARGO FLOOR PANEL SPLICE AT STA 727D + 3 I/A/W 737 AMM 25-52-10-400-801

Part: STIFFENER — CRACKED (LT WHEEL WELL) · airframe 63,236 hrs · 36,810 cycles

LEFT WHEEL WELL; STATION 663; U-SHAPED STIFFNER ABOVE THE AIR CONDITIONER PACK EXHAUST; IS CRACKED AS MARKED. / REMOVED AND REPLACED U-SHAPED STIFFNER AT STATION 663 ABOVE THE AIRCONDITIONER PACK EXHAUST I.A.W SRM 51-40-2-0G-0 AND BOEING DWG 111A1000 AND APPLIED CIC IA.W AMM 51-21-91

Part: STIFFENER — CRACKED (LWR FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

RIGHT AIR CONDITIONING BAY; STATION 663.2' OUTBOARD OF THE RIGHT KEEL BEEM WEB; MID SPAN ANGLE STIFFNER IS CRACKED AS MARKED / REMOVED CRACKED ANGLE STIFFNER AT RT AIR COND. BAY STA 663.2 OUTBD OF RT KEEL BEAM WEB. INSTALLED NEW ANGLE STIFFNER I.A.W. B737 SRM 51-40-02-0G-0; DWG. NO. 111A1001 REV.F. RE APPLIED C.I.C. ON STIFFNER ANGLE I.A.W. B737 AMM 57-00-59.

Part: STIFFENER — CRACKED (RT WHEEL WELL) · airframe 63,236 hrs · 36,810 cycles

RIGHT WHEEL WELL; STATION 663; U-SHAPPED STIFFNER ABOVE THE AIR CONDITIONER PACK EXHAUST; IS CRACKED AS MARKED. / REMOVED AND REPLACED USHAPE STIFFNER AT STATION 663 ABOVE THE AIR CONDITIONER PACK EXHAUST I.A.W SRM 51- 40-02-0G-0 AND BOEING 111A1000 AND APPLIED CIC I.A:W AMM 51-21-91

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO COMPARTMENT FWD FLOOR TRANSITION PIECE WITH TIE DOWN HAS CORROSION / REPLACED CORRODED FWD FLOOR TRANSITION TIE DOWN I.A.W AMM 25-52-10-400 FIG 401 SHT3 NO SRM LIMITS FOUND INSTALLED ON JPANEL CARD-121-CLOSE- ATG # A87769

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO COMPARTMENT L/H SIDE MIDDLE FLOOR TO SIDEWALL TRANSITION STRIP IS CORRODED / REPLACED LEFT SIDE MIDDLE TRANSITION STRIP DUE TO CORROSION IAW AMM 25-52-10-400 FIJ 401 SHT 3 NO SRM LIMITS FOUND TO BE INSTALLED ON JPANEL CARD 121-CLOSE- ATAG #CW2698

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO COMPARTMENT L/H SIDE AFT FLOOR TO SIDEWALL TRANSITION STRIP IS CORRODED / REPLACED CORRODED LEFT SIDE AFT TRANSITION STRIP IAW AMM 25-52-10-400 FIJ 401 SHT 3 NO SRM LIMITS FOUND TO BE INSTALLED ON JPANEL CARD 121-CLOSE- ATAG #CW2697

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO COMPARTMENT R/H SIDE AFT FLOOR TO SIDEWALL TRANSITION STRIP IS CORRODED ON FULL LENGTH OF PART / REPLACED CORRODED TRANSITION STRIP RIGHT AFT SIDE IAW AMM 25-52-10-400 FIJ 401 SHT 3 NO SRM LIMITS FOUND TO BE INSTALLED ON JPANEL CARD 121-CLOSE- ATAG #WN2488

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO COMPARTMENT FLOOR PANEL TRASNITION STRIP AT STA 500D COMMON TO FLOOR PANEL 120CF IS CORRODED / REMOVED AND REPLACED FWD CARGO FLOOR PANEL TRANSITION AT STA 500D COMMON TO FLOOR PANEL 120CF PN 453A1611.9 IAW DWG 453A1600 REV-

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO COMPARTMENT L/H SIDE FWD FLOOR TO SIDEWALL TRANSITION STRIP IS CORRODED / REPLACED LEFT SIDE TRANSITION STRIP TO CORROSION IAW AMM 25-52-10-400 FIJ 401 SHT 3 NO SRM LIMITS FOUND TO BE INSTALLED ON JPANEL CARD 121-CLOSE ATG #WN3456

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO COMPARTMENT R/H SIDE FWD FLOOR TO SIDEWALL TRANSITION STRIP HAS CORROSION IN SEVERAL PLACES / REPLACED RIGHT FWD SIDE CORRODED TRANSITION STRIP IAW AMM 25-52-10-400 FIJ 401 SHT 3 NO SRM LIMITS FOUND TO BE INSTALLED ON JPANEL CARD 121-CLOSE- ATAG #A73780

Part: BRACKET — CORRODED (AFT CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO BAY STA 863 WASTE WATER PAN ASSY; AFT LOWER ANGLE BRACKET BELOW WATER FILL TEMP SENSOR IS CORRODED AS MARKED / REMOVED AND REPLACED CLIP (ANGLE BRACKET) PN146A7406 -2 AT AFT CARGO BAY STA 863 WASTE WATER PAN ASSY; AFT LOWER BRACKET BELOW WATER FILL TEMP SENSOR IAW B737-700 SRM 51-40-02-0G-0AND DWG146A7401 REV.-

Part: ANGLE — CORRODED (BS 727A-727C) · airframe 63,236 hrs · 36,810 cycles

RIGHT ZEE ANGLE CORRODED BETWEEN BS 727C TO 727A. R & R THE ZEE ANGLE IAW SRM.

Part: PAN — CORRODED (AFT CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO BAY STA 861 WASTE WATER PAN ASSY; WATER FI LL FLANG ASSY IS CORRODED ON PAN AS MARKED / REMOVED AND REPLACED CHANNEL (PAN) AT AFT CARGO BAY STA 861 WASTE WATER PAN ASSY. IAW B737-700 SRM 51-40-02-0G-0; 51-40-05-0G-0 SOPM 20-41-05; DWG# 146A7402 REVB; DWG# 417A850 REV D. EXISTING CHANNEL HAD 100% MATERIAL LOSS WITH NO ALLOWABLE DAMAGE LIMITS. REPLACED WASTE TANK HEATER IAW AMM 30-71-04-400-801. ATAG:A73568 ATAG:72927 A83241 AD2349 A69887 A10146 CW2757 POS: AFT CARGO P/N OFF:CH0175D S/N OFF:0084 P/N ON:CH017SD S/N ON:0113

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO COMPARTMENT LEFT SIDE Z ANGLE STA 727C+10 TO 787+10 LBL 22 HAS CORROSION ON UPPER AND LOWER SURFACE / AFT CARGO PIT L/H 'Z' ANGLE CORRODED STA 727C+10' TO STA 787+10'. BLENDED CORROSION IAW B737-700 SRM 53-00-53-1A-2. 2 STEP 2.D. ORIGINAL 0.040'; MAX LOSS 0.025' WITH 0.015' REMAINING. FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2 PARA 4.A. AND FIG103;DETAIL D. REMOVED AND REPLACED L/H 'Z' ANGEL STA 727C + 10' TO STA 847 IAW B737-700 SRM 53-00-53-2R-6 AND DWG 146A7502 REV-. APPLIED CIC TO NEW 'Z' IAW B737-700 AMM 51-21-91-620-802. BLENDING VERIFIED 10X MAGNIFER. TAG A64691

Part: SPLICE STRAP — CORRODED (AFT CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO COMPARTMENT FLOOR PANEL SPLICE STRAP AT STA 887 HAS CORROSION LBL 6 - RBL 21 / REMOVED CORRODED FLOOR PANEL SPLICE STRAP AT STA 887. RECIVED NEW SPLICE STRAP PIN 146A9401-39. LOCATED AND DRILLED NEW FLOOR PANEL SPLICE STRAP. INSTALLED NEW SPLICE STRAP AT STA 887 IAW SRM 51-40-02-06-0; SRM 51-40-05-06-01. DWG 146A7500 TAG WN 3238

Part: FAIRING — ELONGATED (LWR FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

LWR BODY FRG 193CL MOST INBD FASTENER HOLES ELONGATED. / PREPPED CLEANED BONDED AND RESTORED FINISH TO LWR BODY PNL # 193 CL IAW 737 SRM 51-70-04-2R-9 REV 62 AMM 51-21-99-300-801 REV 62

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO COMPARTMENT LOWER LOBE FRAME SHEAR TIE CORRODED AT BS 847, BETWEEN STR 26L TO STR 27L. R&R SHEAR TIE IAW SRM.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO COMPARTMENT FLOOR LOWER BULKHEA ANGLE AT STA 947 HAS CORROSION RBL 6 TO RBL 21 / REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR LOWER BULKHEAD ANGLE @ STA 947 IAW B737 SRM 51-40-02-0G-0 AND DWG # 149A8117 NO LIMITS FOUND IAW SRM

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO BAY BETWEEN STA 847 AND 867 AFT FLOOR SHIELD IS CORRODED AS MARKED TOP SURFACE / REMOVED CORROSION AT AFT CARGO FLOOR SHIELD STA 847 TO 867 RH IAW SRM 53-00-52-1A-2 ORIG T .050 REM T .040 LOSS OF .010 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED AFT CARGO SHIELD PN 146A8127Y5 IAW DWG 146A0081 REV A AND SRM 51-40-02-0G-0 ATAG OP0508

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS 827, STR 26L. R&R STRINGER CLIP IAW SRM & DWG.

Part: CARGO TRACK — CRACKED (BS 727E-747) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO BAY TRACK CRACKED AT BS 727E TO 747, RBL 13.8. R & R THE CARGO TRACK IAW SRM AND DWG.

Part: PAN — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

AFT FUSELAGE WATER SERVICE PANEL PAN CORRODED AROUND FASTENERS. R&R PAN IAW DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS 847, STR 27L. R&R STRINGER CLIP IAW SRM & DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

L1 DOOR LOWER INBOARD SCUFF PLATE ATTACH ANGLE ATTACHED TO CREASE BEAM CORRODED. R&R ANGLE IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED BETWEEN BS 927 TO BS 947, LBL 3. R&R FLOOR TRACK IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS 767, STR 26L. R&R STRINGER CLIP IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (BS 907) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO BAY BILGE AREA LOWER STRUCTURE CORRODED AT BS 907+3, RBL 8. R & R THE STRUCTURE IAW DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO COMPARTMENT BILGE AREA VERTICAL INTERCOSTAL CORRODED BETWEEN BS 847 TO BS 867, RBL 6. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

INTERCOSTAL CORRODED BETWEEN BS 807 TO BS 827, STR 27R. R&R INTERCOSTAL IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO BAY LOWER DOOR CUTOUT THRESHOLD WEB CORRODED BETWEEN BS 794 TO BS 847. R&R WEB IAW SRM.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO BAY BETWEEN STA 794 AND 767 FWD FLOOR SHIELD IS CORRODED SEVERAL AREAS TOP AND BOTTOM SURFACE AS MARKED / REMOVED CORROSION AT AFT CARGO BAY BETWEEN STA 794AND 767 FWD FLOOR SHIELD (ZANGLE CLOSEOUT SHIELD).VERIFIED MATERIAL LOSS ORIG'T'0.030'; REMAIN 0.000' LOSS 100%; FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS. REMOVED AND REPLACED SHIELD; APPLIED CIC IAW B737-700 SRM 51-40-02-00-0 51-40-05-0G-0; 53-00-53-1A-2 AND BOEING DWG#146A8127 REV.C; SOPM 51-41-05

Part: BRACKET — CRACKED (RIGHT WING) · airframe 63,236 hrs · 36,810 cycles

RIGHT RING ROOT AT UPPER SUPPORT BRACKET CRACKED AT REAR SPAR ATTACH POINT. / REMOVED + REPLACED SUPPORT BRACKET AT REAR SPUR ATTACH POINT IAW SRM 51-40-02 + DWG#115A2000 REV B

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,236 hrs · 36,810 cycles

PASS CABIN FLOOR; UPR FLANGE OF INTERCOSTAL IS CRACKED AT LBL 46; BETWEEN BS 328 AND BS 344. / REMOVED AND REPLACED INTERCOSTAL AT LBL 46 BETWEEN BS 328 AND 344 PN141A5410VI6 IAW SRM 51-40-02-0G-0 AND DWG 141A5400 REV-

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO TRACK CORRODED BETWEEN BS 777 TO BS 887, RBL 13. R&R CARGO TRACK IAW DWG & SRM.

Part: CHANNEL — CORRODED (FWD CARGO RH) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO Z-CHANNEL CORRODED FROM STA 500A TO 500D RBL 26. / EVALUATED CORROSION AT FWD CARGO Z-CHANNEL STA 500A TO 500D RBL 2G FOUND TO BE 100% OUT OF LIMITS IAW SRM 53-00-53-1A-1 REMOVED AND REPLACED Z-CHANNEL AT STA 980 TO 500D RBL 26 IAW SRM 53-00-53-2R-5 REPAIR 5

Part: SHIELD — CORRODED (BS 480-500A) · airframe 63,236 hrs · 36,810 cycles

FORWARD CARGO SHIELD CORRODED BETWEEN BS 480 - 500A, RBL 25. R & R THE SHIELD IAW AMM AND DWG.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 63,236 hrs · 36,810 cycles

CABIN FLOOR PANEL 221GF; FWD OTBD CORNER IS BROKEN. / PREPPED CLEANED AND REPAIRED BROKEN CORNER AT FWD O/B EDGE ON FLOOR BOARD 221 GF IAW B737 SRM 53-00-50-2R-4 PAR 3 (A-K1 L1 M1) REV 62

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

R1 CREASE BEAM ATTACH CHORD CORRODED. R&R CHORD IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

UPPER FLANGE OF INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R&R INTERCOSTAL PER DWG AND SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

FORWARD GALLEY FLOORBEAM CRACKED AT BS 328, BETWEEN RBL 20 TO RBL 56. R&R T CHORD IAW SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

RT SIDE SHEAR WEB CORRODED BETWEEN BS 1004 TO BS 1016, RBL 38. R&R SHEAR WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

L1 DOOR CREASE BEAM INBOARD CHORD CORRODED BETWEEN BS 312 TO BS 348. R&R L1 CREASE BEAM IAW SRM AND DWG.

Part: SUPPORT BRACKET — CORRODED (L1 DOOR) · airframe 63,236 hrs · 36,810 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING SUPPORT BRACKET CORRODED AT BS 344. R&R BRACKET IAW SRM.

Part: CHANNEL — CORRODED (BS 400-500D) · airframe 63,236 hrs · 36,810 cycles

FORWARD CARGO ZEE CHANNEL CORRODED BETWEEN BS 400 TO 500D, LBL 26. R & R THE ZEE CHANNEL IAW SRM.

Part: SUPPORT BRACKET — CORRODED (GIRT BAR) · airframe 63,236 hrs · 36,810 cycles

L1 DOOR FORWARD GIRT BAR FITTING SUPPORT BRACKET CORRODED AT BS 312. R&R BRACKET IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

INTERCOSTAL CRACKED BETWEEN BS 348 AND BS 360 BL 0. R&R INTERCOSTAL PER DWG AND SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

R2 CREASE BEAM CORRODED. R&R CREASE BEAM IAW SRM AND DWG.

Part: ANGLE — CRACKED (FWD CARGO LH) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO. ANGLE CRACKED @ STA 500C LBL ''26. / REMOVED AND REPLACED FWD CARGO ANGLE CLIP AT STA 500 C LBL26 FWD OF FRAMW I/A/W 737-700 SRM 51-40-02-0G-0 AND BOEING DWG 143A7505 REV. B

Part: PAN — CORRODED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

PASSENGER CABIN AFT WET AREA FLOOR PAN CORRODED AT BS 1016+7, RBL 18. R&R FLOOR PAN IAW SRM AND DWG.

Part: ANGLE — BROKEN (LEFT WING) · airframe 63,236 hrs · 36,810 cycles

LEFT WING PANEL 551GB OUTBOARD ATTACH ANGLE BROKEN AT FORWARD ATTACH POINT. / REMOVED AND REPLACED LEFT WING PANEL 551GB OUTBOARD ATTACH CNGLE IAW SRM 51-40-02 AND DWG 115A2001 REV -

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,236 hrs · 36,810 cycles

INTERCOSTAL UPPER FLANGE CRACKED BETWEEN BS 270 TO BS 294, RBL 1. R&R INTERCOSTAL IAW DWG AND SRM.

Part: CHANNEL — CORRODED (FWD CARGO COMPT) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO L-CHANNEL CORRODED LOCATED @ STA 500D. / REMOVED CORROSION IAW SRM51-10-02-0G-0 STEP 15/NO LIMITS WAS FOUND IN THE MANUALS; REPLACED WITH NEW PART. REMOVED/REPLACED FWD CARGO L-CHANNEL AT STA 500D LOWER IAW SRM51-40-02-0G-0 STEP4AND BOEING DWG# 143A9481

Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 63,236 hrs · 36,810 cycles

R/H HORIZONTAL STAB UPPER SLIDER SEAL CRACKED / REMOVED CORNER PLATES AND TIE BAR FROM CRACKED SLIDER SEAL PLATE AT R/H HORIZ STAB UPPER SEAL IAW MM 53-31-31-000-801 DRILLED NEW SEAL PLATE IAW MM 53-31-31-400-801 INSTALLED CORNER PLATES AND TIE BAR TO NEW SEAL

Part: SHIELD — CORRODED (FWD CARGO RH) · airframe 63,236 hrs · 36,810 cycles

FORWARD CARGO PIT FORWARD SHEILD STA 420 TO 440 RBL 24 HAS CORROSION ON UPPER SURFACE / EVALUATED CORROSION AT FWD CARGO PIT FWD SHIELD STA 420 TO 440 RBL 24 AND FOUND TO BE 100% OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED SHIELD IAW SRM 51-40-02-0G-0 AND DWG 143A0080 PN 143A8126-21

Part: ANGLE — CRACKED (LEFT WING) · airframe 63,236 hrs · 36,810 cycles

LEFT WING MIDSPAN FIXED UPPER TRAILING EDGE PANEL BULB SEAL ATTACH ANGLE AFT OF LATERAL WEB IS CRACKED / REMOVED AND REPLACED CRACKED UPPER TRAILING EDGE PANEL BULB SEAL ATTACH ANGLE IAW SRM 51-40-02-0G-0 AND BOEING DWG 115A2930 AND APPLIED CIC IAW AMM 51-21-91-620 ATG # A76684

Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 63,236 hrs · 36,810 cycles

L/H HORIZONTAL STAB UPPER SLIDER SEAL CRACKED / REMOVED CORNER PLATES AND TIE BAN FROM SLIDING SEAL PLATE AT L/H HORIZ STAB UPPER SLIDER SEAL IAW MM 53-31-31-000-801 DRILLED NEW SEAL PLATE IAW MM 53-31-31-400-801 INSTALLED CORNER PLATES AND TIE BAR TO NEW SEAL PLATE IAW MM 53-31-31-400-801

Part: SKIN — CRACKED (LE SLAT) · airframe 63,236 hrs · 36,810 cycles

LT WING NR 1 LEADING EDGE SLAT LOWER SURFACE ACTUATOR RIBS CRACKED ON THE SKIN AROUND FASTENER HOLE. REPAIRED SKIN IAW SRM.

Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO LOWER SILL WEB IS CORRODED / REMOVED CORROSION FROM FWD CARGO LOWER SILLWEB. ORG'T' .045'; LOSS .006' REMAINING .039'; OUT OF LIMITS IAW SRM 53-30-15-1A-1 FIG 103 REMOVED OLD AND INSTALLED NEW LOWER SILL WEB 51-40-02 AND DWG 143A8330 REV B

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 63,236 hrs · 36,810 cycles

RT OVERHEAD EMERGENCY EXIT SIGN LIGHT INOP AT ROW 2R. R&R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 63,236 hrs · 36,810 cycles

RT STOWBIN EMERGENCY EXIT LIGHT INOP AT ROW 22. R&R POWER SUPPLY PER MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 63,236 hrs · 36,810 cycles

LT STOWBIN EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 14 TO ROW 24. R&R POWER SUPPLY PER AMM.

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 63,236 hrs · 36,810 cycles

AFT CARGO PIT AFT TIE DOWN PLATE HAS 2 AREAS OF CORROSION / REPLACE WITH NEW PIT TIE DOWN COENER PLATE PER DWG#453A2600 REFERANCE INSTALL ON JPANEL-141 PART#45 3A2611-2 A-TAG#A70846

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 63,236 hrs · 36,810 cycles

L2 CABIN DOOR AFT EMERGENCY EXIT LIGHT INOP. R&R POWER SUPPLY IAW AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 63,236 hrs · 36,810 cycles

FWD CARGO PIT FWD CORNER SCUFF PLATE CRACKED / FWD CARGO PIT FWD CORNER SCUFF PLATE REPAIRON W/O# 36054 1400 0001 IAW EA. 1-A53-2076

Part: ANGLE — CRACKED (RT WING) · airframe 61,940 hrs · 36,016 cycles

RT WING ANGLE BRACKET THAT ATTACHES TO INBOARD SIDE OF FLAP DEFLECTION ROLLER CRACKED. R&R ANGLE PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,940 hrs · 36,016 cycles

FORWARD CARGO BIN AIR CONDITIONING DISTRIBUTION BAY UPPER CENTER FLOOR BOARD INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520. R&R INTERCOSTAL PER SRM.

Part: WEB — CRACKED (RT WING) · airframe 61,940 hrs · 36,016 cycles

RT WING UPPER TRAILING EDGE SHELF PANEL OUTBOARD NR 7 SPOILER LOWER VERTICAL WEB CRACKED UPPER OUTBOARD CORNER. R&R WEB PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 59,832 hrs · 34,733 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1669. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,832 hrs · 34,733 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1672. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,832 hrs · 34,733 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1673. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,832 hrs · 34,733 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1675. R & R BATTERY IAW AMM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 59,832 hrs · 34,733 cycles

RIGHT FWD PHOTO LUMINESCENT STRIP LENS COVER CRACKED. R & R STRIP IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,832 hrs · 34,733 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1670. R & R BATTERY IAW AMM.

Part: CAP — BROKEN (R1 DOOR) · airframe 58,822 hrs · 34,159 cycles

R1 DOOR EMER EVAC SLIDE BUMPER END CAP BROKEN ON FWD SIDE. R & R END CAP IAW AMM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 58,292 hrs · 33,848 cycles

AFT PRESSURE BULKHEAD BS 1016, CRACKED AT STRINGER 23L. REPAIRED BULKHEAD IAW EA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 57,649 hrs · 33,489 cycles

FORWARD GALLEY SERVICE DOOR, CRACKED AT RADIUS AT BOTTOM LT SIDE OF DOOR SKIN. R & R FWD SERVICE DOOR IAW MM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 57,557 hrs · 33,432 cycles

RIGHT OVERWING EXIT FWD LOWER EMER EXIT LIGHT INOPERATIVE. CONNECTED LIGHT IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,557 hrs · 33,432 cycles

RIGHT WING, OTBD AFT FLAP DELAMINATED ON INBD UPPER SURFACE. REPAIRED AFT FLAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,557 hrs · 33,432 cycles

FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,557 hrs · 33,432 cycles

FRAME WEB CRACKED AT BS 520, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,557 hrs · 33,432 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,557 hrs · 33,432 cycles

FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,557 hrs · 33,432 cycles

FRAME WEB CRACKED AT BS 787, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,557 hrs · 33,432 cycles

FUSELAGE FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,557 hrs · 33,432 cycles

FRAME WEB CRACKED AT BS 400, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,557 hrs · 33,432 cycles

FRAME WEB CRACKED AT BS 400, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,557 hrs · 33,432 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,557 hrs · 33,432 cycles

FRAME WEB CRACKED AT BS 727D, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,557 hrs · 33,432 cycles

FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 57,557 hrs · 33,432 cycles

FLIGHT DECK RT NR 3 E - F WINDOW POST, CRACKED IN SECOND LOWER CORNER FASTENER HOLE. REPAIRED POST IAW EA.

Part: LENS — FAULTY (EXIT SIGN) · airframe 56,562 hrs · 32,880 cycles

FORWARD ENTRY DOOR EMER EXIT SIGN COVER MISSING ARROW. R & R LENS IAW MM.

Part: LENS — MISSING (CABIN) · airframe 56,562 hrs · 32,880 cycles

EMERGENCY LIGHT LENS ABOVE 14 ABC MISSING. INSTALLED LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,558 hrs · 32,877 cycles

LEFT EMER LIGHT BULB INOPERATIVE AT ROW 14. RELAMPED BULB IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 55,753 hrs · 32,404 cycles

RIGHT OVERWING OUTSIDE EMER ESCAPE LIGHT INOPERATIVE. R & R BATTERY POWER SUPPLY IAW AMM.

Part: WINDOW — ARCED (COCKPIT) · airframe 55,596 hrs · 32,317 cycles

R1 WINDOW OUTER PANE ARCED. R & R R1 WINDOW IAW MM & MT.

Part: SUPPORT FRAME — CRACKED (LT WING) · airframe 53,153 hrs · 30,930 cycles

LEFT FWD UPPER WING TO BODY FAIRING SUPPORT FRAME CRACKED. REPAIRED FRAME IAW EA.

Part: SKIN SPLICE — CRACKED (FUSELAGE) · airframe 51,849 hrs · 30,162 cycles

SKIN CHORD SPLICE CRACKED AT BS 540, BETWEEN STRINGER 22L TO STRINGER 23L. REPAIRED SPLICE IAW EA.

Part: SKIN SPLICE — CRACKED (FUSELAGE) · airframe 51,849 hrs · 30,162 cycles

SKIN CHORD SPLICE CRACKED AT BS 540, BETWEEN STRINGER 22R TO STRINGER 23R. REPAIRED SPLICE IAW EA.

Part: LIGHT — MISSING (CABIN) · airframe 51,104 hrs · 29,732 cycles

RT OVERWING DOOR BOTTOM LT EMERGENCY EXIT COVER PLATE MISSING. INSTALLED LIGHT ASSEMBLY IAW MM.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 50,732 hrs · 29,519 cycles

WW PANEL 193AR DELAMINATED 36" FROM UPPER EDGE & 7" FROM FWD EDGE. REPAIRED PANEL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,732 hrs · 29,519 cycles

SEAT TRACK CRACKED AT STATION 727B LBL 24.75. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,732 hrs · 29,519 cycles

SEAT TRACK CRACKED AT STATION 727B RBL 24.75. REPAIRED TRACK IAW EA.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 50,732 hrs · 29,519 cycles

RT SIDE FLIGHT DECK NR 3 E-F WINDOW POST SECOND LOWER CORNER FASTENER HOLE CRACKED. REPAIRED POST IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,732 hrs · 29,519 cycles

MAIN WW LT VERTICAL PRESSURE WEB CRACKED AT STATION 663, LBL 34. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,732 hrs · 29,519 cycles

MAIN WW LT VERTICAL PRESSURE WEB CRACKED AT STATION 663, LBL 40. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,732 hrs · 29,519 cycles

SEAT TRACK CRACKED AT STATION 727B LBL 45.5. REPAIRED TRACK IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,732 hrs · 29,519 cycles

LT SIDE FLIGHT DECK NR 1 E-F WINDOW FRAME UPPER OTBD CORNER CRACKED. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,732 hrs · 29,519 cycles

LT WING NR 3 SLAT LE SKIN CRACKED AT ACTUATOR RIB FITTING. REPAIRED SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,732 hrs · 29,519 cycles

LT WING NR 4 SLAT LE SKIN CRACKED AT ACTUATOR RIB FITTING. REPAIRED SLAT IAW SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,732 hrs · 29,519 cycles

MLG WW RT VERTICAL PRESSURE WEB CRACKED AT STATION 663, RBL 40. REPAIRED WEB IAW SRM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 50,732 hrs · 29,519 cycles

LT SIDE FLIGHT DECK NR 3 E-F WINDOW POST SECOND LOWER CORNER FASTENER HOLE CRACKED. REPAIRED POST IAW EA.

Part: SELECTOR VALVE — LEAKING (HYDRAULIC SYS) · airframe 50,175 hrs · 29,180 cycles

DECLARED EMERGENCY, "B" SYSTEM HYDRAULIC FAILURE. R&R BRAKE ACCUMULATOR SELECTOR VALVE IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 49,414 hrs · 28,726 cycles

R2 DOOR EGRESS LIGHT COVER BROKEN. REMOVED AND REPLACED AFT GALLEY EGRESS LIGHT ASSY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 48,714 hrs · 28,295 cycles

RIGHT AFT CABIN EMERGENCY LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACS M1672 AND M1673 PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 48,714 hrs · 28,295 cycles

LEFT AFT CABIN EMERGENCY LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACKS M1672 AND M1673 PER AMM.

Part: ENGINE — FAILED (LEFT) · airframe 44,809 hrs · 26,043 cycles

INFLIGHT SHUTDOWN/DIVERSION. NR 1 OIL QUANTITY STARTED TO DECREASE AND EVENTUALLY WENT TO 0 THEN BACK TO 100 PERCENT THEN OIL PRESSURE / SLOWLY WENT AMBER THEN RED. SHUT IT DOWN. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,263 hrs · 26,794 cycles

LEFT EEPLS INOP AT ROW 9. RELAMPED EEPLS PER M/M.

Part: SIGN — LOOSE (CABIN) · airframe 45,743 hrs · 26,495 cycles

R1 DOOR EMERGENCY EXIT SIGN AT LOWER CORNER LOOSE. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 45,444 hrs · 26,323 cycles

R2 DOOR EMERGENCY EXIT SIGN MISSING COVER. REMOVED AND REPLACED EMERGENCY EXIT SIGN ASSY PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 44,017 hrs · 25,522 cycles

DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM O/B FLANGE CRACKED AT BS 727A+18, RBL 46. REPAIRED CHORD PER ER.

Part: RIB — CRACKED (HORIZ STAB) · airframe 44,017 hrs · 25,522 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT HORIZONTAL STABILIZER VERTICAL RIB CRACKED AT STA 92.7. REPAIRED RIB IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 44,017 hrs · 25,522 cycles

DURING SCHEDULED 12Y CHECK, FOUND WEB CRACKED BETWEEN BS 719 TO BS 728, BETWEEN RBL 50 TO RBL 64. REMOVED AND REPLACED WEB PER ER AND EA.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 44,024 hrs · 25,528 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. CONNECTED CONNECTOR PER MM.

Part: CONNECTOR — BROKEN (FUSELAGE) · airframe 44,017 hrs · 25,522 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT CONNECTOR BROKEN. REMOVED AND REPLACED CONNECTOR PER SWPM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 44,017 hrs · 25,522 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR CUTOUT FRAME CRACKED AT BS 295.5, STR 17R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,017 hrs · 25,522 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,017 hrs · 25,522 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,017 hrs · 25,522 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: SLIDE — UNWANTED DEPLOY (R2 DOOR) · airframe 43,718 hrs · 25,346 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE IAW MT.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 43,254 hrs · 25,049 cycles

NR 1 FUEL TANK SHOWS APPROX 400 LBS LOW EVERY 30-45 MIN OF FLIGHT. REMOVED AND REPLACED FUEL TANK CROSS FEED VALVE PER MM AND MT.

Part: NUT PLATE — CRACKED (R1 DOOR) · airframe 39,741 hrs · 22,968 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC AFT SLIDE MOUNT, UPPER NUT PLATE CRACKED. REMOVED AND REPLACED NUT PLATE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,700 hrs · 21,899 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 19. REMOVED AND REPLACED LIGHT PER MM.

Part: INDICATOR — CRACKED (EVAC SLIDE) · airframe 37,547 hrs · 21,674 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR CRACKED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 36,074 hrs · 20,788 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 36,074 hrs · 20,788 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 35,402 hrs · 20,375 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 33,236 hrs · 19,080 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,983 hrs · 18,920 cycles

DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,983 hrs · 18,920 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,983 hrs · 18,920 cycles

DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 30,528 hrs · 17,475 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: FLOOR SUPPORT — CORRODED (BS 995-1007) · airframe 30,028 hrs · 17,161 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CORRODED BETWEEN BS 995 AND BS 1007, RBL 39. REMOVED AND REPLACED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,016 hrs · 17,152 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER TEE CAP CORRODED AT BS 986, LBL 34 TO LBL 44. REMOVED AND REPLACED TEE CAP PER SWA EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 30,016 hrs · 17,152 cycles

DURING SCHEDULED 8Y CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REPAIRED FLAP PER SRM.

Part: CONTROLLER — SHORTED (COCKPIT) · airframe 27,532 hrs · 15,712 cycles

R1 WINDOW HEAT TURNED ON, WINDOW HEAT CONNECTOR SHORTED, AND WINDOW CRACKED. REMOVED AND REPLACED WINDOW HEAT CONTROLLER AND AND WINDOW PER MM.

Part: FITTING — LOOSE (L1 DOOR GIRT BAR) · airframe 26,122 hrs · 14,914 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED GIRT BAR FITTING PER MM.

Part: TOILET — LEAKING (LAVATORY) · airframe 25,911 hrs · 14,795 cycles

DECLARED EMERGENCY, BURNING SMELL REPORTED IN AFT GALLEY, TURNED POWER OFF, SMELL DISSIPATED. PRIOR TO LANDING, THE FRONT LAV WAS LEAKING AROUND THE BASE, ALL WATER VALVES TURNED OFF. DURING DESCENT L/E TRANSIT LIGHT ILLUMINATED, THE MACH TRIM FAIL LIGHT ALSO ILLUMINATED. BURNING SMELL PRESENT IN COCKPIT AT THIS TIME. REMOVED AND REPLACED FSEU, FLIGHT ACC UNIT, AND TOILET PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,380 hrs · 14,502 cycles

DURING SCHEDULED HC2 CHECK, RT FWD EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 22,297 hrs · 12,734 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BULB — INOPERATIVE (FUSELAGE) · airframe 21,778 hrs · 12,438 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 21,461 hrs · 12,250 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 21,091 hrs · 12,030 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BULKHEAD — CANNING (AFT) · airframe 20,494 hrs · 11,691 cycles

DURING SCHEDULED HC2 CHECK, FOUND BS 1016 AFT PRESSURE BULKHEAD OIL CANNED AT STR 3L. REPAIRED AFT PRESSURE BULKHEAD PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,708 hrs · 11,233 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,537 hrs · 9,474 cycles

DURING SCHEDULED C3 CHECK, FOUND RED EMERGENCY EXIT LIGHT AT MID CABIN INOP. RELAMPED LIGHT PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 16,537 hrs · 9,474 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED THROUGHOUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 11,761 hrs · 6,892 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 11,698 hrs · 6,853 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 1, NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 11,698 hrs · 6,853 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, FOUND RT ELEVATOR TAB HINGE ATTACH POINTS NR 2 AND NR 4 WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 2 AND NR 4 HINGE ATTACH POINTS PER MM.

Part: HINGE — WORN (LT ELEVATOR) · airframe 11,609 hrs · 6,805 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11038-55, LT ELEVATOR TAB NR 4 HINGE WORN. REMOVED AND REPLACED LT ELEVATOR TAB NR 4 HINGE PER MM.

Part: FUSE — MALFUNCTIONED (HYD SYSTEM) · airframe 10,084 hrs · 5,950 cycles

AIR TURNBACK, AFTER TAKEOFF L/E FLAPS WOULD NOT RETRACT. RESET HYD FUSES PER MM.

Part: TAB — DELAMINATED (ELEVATOR) · airframe 6,649 hrs · 4,068 cycles

DURING SCHEDULED A2 CHECK, FOUND LH ELEVATOR TAB DELAMINATED AT STA 74-94, TRAILING EDGE UPPER SKIN. REPAIRED TAB PER SWA RA.

Part: SENSOR — INOPERATIVE (RT WING TE FLAP) · airframe 3,729 hrs · 2,275 cycles

DECLARED EMERGENCY, DURING APPROACH FLAPS WOULD NOT EXTEND. T/E FLAPS SPLIT INDICATION WHEN FLAP HANDLE PLACED TO 5 DEG POS, FLAPS STOPPED BETWEEN UP POS AND 1 DEG POS. L/E DEVICES EXTENDED THROUGH MANUAL MEANS. REMOVED AND REPLACED NR 7 FLAP SKEW SENSOR PER MM.

Part: SENSOR — MALFUNCTIONED (COCKPIT)

DURING APPROACH, CYCLED THE GEARS TWICE TO GET A GREEN LIGHT NOSE GEAR INDICATION, PSEU LIGHT ILLUMINATED AFTER. C/W PSEU BITE CHECK, RESET MSG D9082 AT PIN NR 9, SENSOR S0846. OPS CK GOOD PER MM.