N788SA

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 73,744 hrs · 43,838 cycles

EMERG LIGHT BATTERY PACK M1672 INOP<[01] R/R EMERG LIGHTS BATTERY PACK M1672 PER AMM 33-51-06. OPS CHECKS GOOD.

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 73,742 hrs · 43,837 cycles

FORWARD LEFT DOOR GIRTBAR NOT SEATED CORRECTLY<[01] REPOSITIONED L1 DOOR SLIDE. IAW MT 725-61-06

Part: LIGHT — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 73,538 hrs · 43,699 cycles

AFT ENTRY PLASTIC COVER FOR EXIT LIGHT FELL OFF<[01] REMOVED AND REPLACED PER AMM 33-51-01

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 73,348 hrs · 43,560 cycles

EMERGENCY LIGHT INOP AT 14ABC<[01] RELAMPED EMERGENCY AREA LIGHT AT 14ABC PER AMM 33-51-03. OPS CHECK GOOD.

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 73,028 hrs · 43,366 cycles

LEFT SIDE AFT SLIDE IS PULLED OUT FARTHER THAN NORMAL<[01] STOWED LEFT SIDE AFT SLIDE GIRT BAR SLIDE MATERIAL OUT OF THE WAY. REF. SIP. -END-

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 73,020 hrs · 43,360 cycles

FORWARD GIRT BAR MISSALIGNED (R1)<[01] REPOSITIONED R1 SLIDE GIRT BAR. AMM 25-66-01

Part: CHARGER — INOPERATIVE (ZN 200 FUS TOP) · airframe 72,761 hrs · 43,196 cycles

R1 EXTERIOR EMER LIGHT INOP<[01] REPLACED FWD RH BATTERY PACK / PACK CHARGER ASSY REF AMM 33-51-06. OPS CHECKS GOOD

Part: PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 72,438 hrs · 42,990 cycles

RIGHT WING I/B TRAILING EDGE PANEL 551AT CRACKED AND DENTED ON LOWER SURFACE.<[01] REMOVED AND REPLACED PANEL PER AMM 20-50-11.

Part: SLIDER — CRACKED (ZN 300 STABILIZE) · airframe 71,979 hrs · 42,693 cycles

R/H HORIZONTAL STABILIZER FRONT SPAR LOWER SLIDER IS CRACKED<[01] REMOVED AND REPLACED SLIDER SEAL IAW AMM 53-31-31

Part: BRACKET — BROKEN (ZN 100) · airframe 71,979 hrs · 42,693 cycles

KEEL BEAM FWD PANEL; AFT LEFT MOUNT BRACKET IS BROKEN KEEL BEAM FWD PANEL AFT LEFT MOUNT BRACKET IS BROKEN<[01] REPLACED FWD KEEL BEAM PANEL; AFT LEFT MOUNT BRACKER PER SRM 51-40-02 AND REFERENCE EA 23-153-00387; TSR 202300859; TTG8Q00HM8FD; DWG 149A7701; DWG 149A7712-45.

Part: BRACKET — BROKEN (ZN 100) · airframe 71,979 hrs · 42,693 cycles

KEEL BEAM FWD PANEL; FWD LEFT MOUNT BRACKET IS BROKEN KEEL BEAM FWD PANEL FWD LEFT MOUNT BRACKET IS BROKEN<[01] REMOVED AND REPLACED KEEL BEAM FWD PANEL; FWD LEFT MOUNT BRACKET PER SRM 51-40-02

Part: SLIDER — CRACKED (ZN 300 STABILIZE) · airframe 71,979 hrs · 42,693 cycles

R/H HORIZONTAL STABILIZER FRONT SPAR UPPER SLIDER IS CRACKED<[01] REMOVED AND REPLACED UPPER SLIDER IAW AMM 53-31-31

Part: SLIDE — OUT OF ADJUST (ZN 900 LAV/GALLE) · airframe 71,941 hrs · 42,664 cycles

FWD RT SLIDE OUT OF RIG IN COMPARTMENT. CAN BARLEY SEE PRESS GAUGE.<[01] REMOVED AND REINSTALLED FWD RT ESCAPE SLIDE PER AMM 25-66-01.

Part: SLIDE — UNSECURE (FWD SERVICE DOOR) · airframe 71,930 hrs · 42,654 cycles

FORWARD SERVICE DOOR; EMERGENCY SLIDE; PROTRUDING FROM CONTAINER<[01] RE-SECURED FWD SERVICE DOOR SLIDE PER AMM 25-66-01.

Part: FAIRING — ERODED (NOT REPORTED) · airframe 71,669 hrs · 42,492 cycles

FAIRING PANEL 193B HAS ELONGATED HOLES AND DRAIN HOLE ERODED. REMOVED AND REPLACED 193B PANEL IAW SOPM 20-50-01. INSPECTION C/W REMOVAL AND REPLACEMENT OF 193B PANEL IAW SOPM 20-50-01.

Part: BEAM — OUT OF LIMITS (RT WING FLAP) · airframe 71,552 hrs · 42,413 cycles

#2 FLAP FAIRING HANGING DOWN WITH FLAPS UP / [01] R & R NR 2 FLAP BEAM ASSY, OPS CHECKED GOOD IAW AMM 27-51-28.

Part: NONE — DETERIORATED (PAX CABIN) · airframe 70,868 hrs · 41,951 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2022-493650 / [01] FAUL RESOLVED ON OTHER FAULT; SEE TTG8Q00EMH5D.;[02] FAUL RESOLVED ON OTHER FAULT; SEE TTG8Q00EMH5D

Part: ANGLE — CRACKED (FWD CARGO BAY) · airframe 70,868 hrs · 41,951 cycles

CRACK ANGLE LOCATED STA 500D AND STR 28L FWD CARGO COMPARTMENT 2022-493563 / [01] TOOL USED POWER PACK P/N:FMK0003223;S/N:PE0412/63335;DUE DATE:26-JAN-23.MULTIMETER P/N:FLUKE-37;S/N:5335022;DUE DATE:04-DEC-22;THERMOMETER P/N:FLUKE 566;S/N:AE-405697;DUE DATE:30-MAR-23.;[02] REPLACED ANGLE AND FASTENERS LOCATED STA 500D AND STR 28L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DWG#143A7902 REV:A.SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] REPLACED ANGLE AND FASTENERS LOCATED STA 500D AND STR 28L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DWG#143A7902 REV:A. RII ;SEE INDIVIDUAL STEP SIGN OFF BELOW.

Part: WEB — CRACKED (FWD CARGO BAY) · airframe 70,868 hrs · 41,951 cycles

CRACK WEB LOCATED BTW STA 500D TO STA 520 AT STR 28R AT FWD CARGO COMPARTMENT 2022-493562 / [01] REPLACED WEB AND FASTENERS LOCATED BTW STA 500D TO STA 520 AT STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9. AND DWG#143A7902 REV:A SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — CRACKED (FWD CARGO) · airframe 70,868 hrs · 41,951 cycles

CRACK ANGLE LOCATED STA 500D AND STR 28L FWD CARGO COMPARTMENT 2022-493563 / [01] TOOL USED POWER PACK P/N:FMK0003223;S/N:PE0412/63335;DUE DATE:26-JAN-23.MULTIMETER P/N:FLUKE-37;S/N:5335022;DUE DATE:04-DEC-22;THERMOMETER P/N:FLUKE 566;S/N:AE-405697;DUE DATE:30-MAR-23.;[02] REPLACED ANGLE AND FASTENERS LOCATED STA 500D AND STR 28L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DWG#143A7902 REV:A.SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] REPLACED ANGLE AND FASTENERS LOCATED STA 500D AND STR 28L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DWG#143A7902 REV:A. RII ;SEE INDIVIDUAL STEP SIGN OFF BELOW.

Part: WEB — CRACKED (FWD CARGO) · airframe 70,868 hrs · 41,951 cycles

CRACK WEB LOCATED BTW STA 500D TO STA 520 AT STR 28R AT FWD CARGO COMPARTMENT 2022-493562 / [01] REPLACED WEB AND FASTENERS LOCATED BTW STA 500D TO STA 520 AT STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9. AND DWG#143A7902 REV:A SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — CRACKED (VERTICAL STAB) · airframe 70,868 hrs · 41,951 cycles

CRACK ON RIB 8 OF DORSAL FIN 321A 2022-493542 / [01] REPLACED RIB 8 LOCATED ON DORSAL FIN 321A. IAW B737-700 SRM 51-10-02 PARAGRAPH 9. AND DWG 174A0101 REV. ?D?. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETE <BR>IAW B737-700 SRM 51-10-02 PARAGRAPH 9. AND DWG 174A0101 REV. ?D?

Part: BRACKET — CRACKED (RH WING) · airframe 70,868 hrs · 41,951 cycles

CRACK TRAILING EDGE BRACKET LOCATED ON ORSS 274 AT RT WING 2022-493538 / [01] REPLACED BRACKET AND FASTENERS LOCATED ON TRAILING EDGE AT ORSS 274 RT WING. IAW B737-700 SRM 51-40-02 AND DWG 115A2930. REV. ?-?;[02] CERTIFIED WORK PERFORMED.

Part: BRACKET — CRACKED (LH WING) · airframe 70,868 hrs · 41,951 cycles

CRACK TRAILING EDGE BRACKET LOCATED ON ORSS 274 AT LT WING 2022-493539 / [01] REPLACED BRACKET AND FASTENERS LOCATED ON TRAILING EDGE AT ORSS 274 LT WING. IAW B737-700 SRM 51-40-02 AND DWG 115A2930. REV. ?-?;[02] CERTIFIED WORK PERFORMED.

Part: NONE — DETERIORATED (PAX CABIN) · airframe 70,868 hrs · 41,951 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2022-493519. / [01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W DWG 33500007 REV: 2 AND SOPM 20-50-12;[02] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W DWG 33500007 REV: 2 AND SOPM 20-50-12

Part: STRUT — CRACKED (#2 ENGINE) · airframe 70,576 hrs · 41,772 cycles

#2 ENGINE RTF STRUT #1 HAS .500 CRACK AT LOCATION C2 FWD SIDE OF WELD AT CENTER OF CUTOUT / [01] ENGINEERING ADDED EA# M-21-172-00811; REFERENCE BARCODE# TTG8Q00E05YP.

Part: COVER — OUT OF POSITION (L2 DOOR) · airframe 70,343 hrs · 41,604 cycles

CREW REPORTS AFT ENTRY DOOR SLIDE MANUAL DEPLOY HANDLE COVER OUT OF POSITION / [01] REPOSITIONED COVER PER SIP

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 68,363 hrs · 40,408 cycles

LH HORIZONTAL STABILIZER LOWER SLIDE SEAL CRACKED ; / [01] R&R LH HORIZONTAL STABILIZER LOWER SLIDE SEAL PER MM REF 53-31-31; [02] R&R LH HORIZONTAL STABILIZER LOWER SLIDE SEAL PER MM REF 53-31-31; [03] R&R LH HORIZONTAL STABILIZER LOWER SLIDE SEAL PER MM REF 53-31-31

Part: LIGHT — INOPERATIVE (CABIN)

LH OWE CUTOUT FWD SIDE; AND RH OWE CUTOUT AFT SIDE; EMERGENCY ESCAPE LIGHTS ON SIDEWALL PANELS HAVE INOP BULBS ; / [01] REPLAMPED LH OWE CUTOUT FWD SIDE; AND RH OWE AFT SIDE; EMERGENCY ESCAPE LIGHTS ON SIDEWALL PANELS PER AMM 33-51-14-960-801. OPS CHECK GOOD.; [02] VERIFIED CORRECTIVE ACTION 1

Part: BATTERY — INOPERATIVE (CABIN) · airframe 68,361 hrs · 40,407 cycles

EMERGENCY EXIT LIGHTS ON BULLNOSE ON LEFT SIDE OF AIRCRAFT AT ROW 9 AND 12 INOP ; CHANGED BULBS STILL NO WORK / [01] TROUBLESHOT TO BAD BATTERY CHARGER AT M1670. CHARGER WILL NOT CHARGE BATTERY VERIFIED THERE IS VOLTAGE AT PIN 2 AND 22 FOR CHARGING. CHARGER IN WAREHOUSE WILL BE ON 1600 TRUCK.; [02] VERIFIED TROUBLESHOOTING TO BAD BATTERY CHARGER AT M1670; WORK TO CONTINUE UPON RECEIPT OF NEW CHARGER; [03] REMOVED AND REPLACED M1670 BATTERY CHARGER PER AMM 33-51-06-960-806. REMOVED AND REPLACED BATTERY M1670 PER AMM 33-51-06-960-805. PERFORMED GOOD OPS TEST OF BULL NOSE LIGHTS AT L/H ROWS 9 AND 12 PER AMM 33-51-06-960-805.; [04] VERIFIED REMOVED AND REPLACED M1670 BATTERY CHARGER PER AMM 33-51-06-960-806. REMOVED AND REPLACED BATTERY M1670 PER AMM 33-51-06-960-805. PERFORMED GOOD OPS TEST OF BULL NOSE LIGHTS AT L/H ROWS 9 AND 12 PER AMM 33-51-06-960-805.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 68,361 hrs · 40,407 cycles

EMERGENCY EXIT LIGHTS ON BULLNOSE ON LEFT SIDE OF AIRCRAFT AT ROW 9 AND 12 INOP ; CHANGED BULBS STILL NO WORK / [01] TROUBLESHOT TO BAD BATTERY CHARGER AT M1670. CHARGER WILL NOT CHARGE BATTERY VERIFIED THERE IS VOLTAGE AT PIN 2 AND 22 FOR CHARGING. CHARGER IN WAREHOUSE WILL BE ON 1600 TRUCK.; [02] VERIFIED TROUBLESHOOTING TO BAD BATTERY CHARGER AT M1670; WORK TO CONTINUE UPON RECEIPT OF NEW CHARGER; [03] REMOVED AND REPLACED M1670 BATTERY CHARGER PER AMM 33-51-06-960-806. REMOVED AND REPLACED BATTERY M1670 PER AMM 33-51-06-960-805. PERFORMED GOOD OPS TEST OF BULL NOSE LIGHTS AT L/H ROWS 9 AND 12 PER AMM 33-51-06-960-805.; [04] VERIFIED REMOVED AND REPLACED M1670 BATTERY CHARGER PER AMM 33-51-06-960-806. REMOVED AND REPLACED BATTERY M1670 PER AMM 33-51-06-960-805. PERFORMED GOOD OPS TEST OF BULL NOSE LIGHTS AT L/H ROWS 9 AND 12 PER AMM 33-51-06-960-805.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 68,361 hrs · 40,407 cycles

EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1669 ARE INOP ; / [01] REMOVED AND REPLACED AND PERFORMED GOO OPS TEST OF M1669 BATTERY PACK PER AMM 33-51-06-960-805.; [02] VERIFIED REMOVED AND REPLACED AND PERFORMED GOOD OPS TEST OF M1669 BATTERY PACK PER AMM 33-51-06-960-805.

Part: NONE — DELAMINATED (R/H WING) · airframe 68,361 hrs · 40,407 cycles

R/H O/B AFT FLAP HAS MINOR DELAM ON O/B AFT EDGE. ; / [01] IDENTIFIED PART AND MATERIAL IAW SRM 57-53-01-0I-4 FIGURES 1-2; TABLE 2; ITEMS [2] AND [5].<BR>DAMAGE WAS FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-53-01-1A-4 PAR 4.A(6).<BR>REPAIR WILL BE ACCOMPLISHED IAW SRM 57-53-01-2R-14.<BR><BR>REMOVED .8'X.8' OF DAMAGED SKIN FROM UPPER SURFACE AND .8'X.8' OF DAMAGED SKIN FROM LOWER SURFACE AND CLEANED REPAIR AREA IAW SRM 57-53-01-2R-14 PAR 4.B; [02] VALIDATED REPAIR TO BE COMPLETED IAW SRM 57-53-01-2R-14 TO UPPER AND LOWER SKINS.; [03] VERIFIED CORRECTIVE ACTION ITEMS 1 & 2.; [04] FABRICATED REPAIR SKIN AND REPAIR DOUBLER FOR UPPER SKIN USING PRE PRIMED ALUMINUM 7075-T6 .016' LOT#1351319-2.<BR>FABRICATED REPAIR SKIN AND REPAIR DOUBLER FOR LOWER SKIN USING PRE PRIMED ALUMINUM 7075-T6 .020' LOT#J000054940.<BR>PREPARED SURFACE FOR REPAIR USING BOEGEL(AC-130) LOT#1074P<BR>APPLIED ADHESIVE PRIMER BMS 5-89TY2 LOT#1470544-1 TO BONDING SURFACE<BR>IAW SRM 57-53-01-2R-14 PARA 4C(1-2);D AND SRM 51-70-10-2R-0 PARA 8; 14 AND 15A-E.;

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 68,361 hrs · 40,407 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED ; / [01] WELDED CRACKS 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>WELDING MACHINE CALIBRATION I.D. E10583; S/N; KJ256554. 12/2021; [02] VERIFIED CORRECTIVE ACTION 1; [03] FLUORESCENT DYE PENETRANT INSPECTED REPAIRED AREA IN ACCORDANCE WITH SOPM 20-20-02 METHOD C. NO CRACKS FOUND.<BR><BR>TOOL I.D. ATS2504 (DLM-1000) RADIOMETER<BR>S.N. 191348; [04] SANDED REPAIR WELD AREA PER SRM 53-60-15-2R-1 PARA 4.B.(5); [05] INSPECTED ACTION 4; [06] CARD COMPLETE.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 68,361 hrs · 40,407 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED ; / [01] WELDED CRACKS ON ACB; FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(2) AND (4)<BR>WELDING MACHINE CALIBRATION I.D. E10583; S/N; KJ256554.; [02] VERIFIED CORRECTIVE ACTION 1; [03] FLUORESCENT DYE PENETRANT INSPECTED REPAIRED AREA IN ACCORDANCE WITH SOPM 20-20-02 METHOD C. NO CRACKS FOUND.<BR><BR>TOOL I.D. ATS2504 (DLM-1000) RADIOMETER<BR>S.N. 191348; [04] SANDED REPAIR WELD AREA PER SRM 53-60-15-2R-1 PARA 4.B.(5); [05] INSPECTED ACTION 4; [06] CARD COMPLETE.

Part: INTERCOSTAL — CRACKED · airframe 68,361 hrs · 40,407 cycles

FOUND INTERCOSTAL CRACKED AT BS947 RBL21 WL155 ; / [01] THIS PART NO FOUND ALLOWABLE DAMAGE ON SRM; REPAIR BY REMPLACEMENT PER SRM 51-10-02 PARA 9; [02] REMOVED INTERCOSTAL FROM AFT CARGO BETWEEN BS 927 TO BS 947 RBL 21 WL 155 PER SRM 51-40-02; [03] LOCATED AND DRILLED NEW INTERCOSTAL AT AFT CARGO BAY BETWEEN BS 927 TO BS 947 RBL 21 WL 155 P/N 147A7580-83 LOT#1472422-7 PO#826957/7 IAW SRM 51-40-05 ;DWG147A7500 REV:C AND DWG 147A7500REV:-.; [04] VERIFIED ITEM 3 CORRECTIVE ACTIONS.; [05] OK TO INSTALL.; [06] OK TO INSTALL; [07] INSTALLED NEW INTERCOSTAL AT BS 927 TO BS 947 RBL 21 WL 155;P/N 147A7580-83; LOT#1472422-7; PO#826957/7 IAW SRM 51-40-02; DWG 147A7500 REV:C ; AND DWG 147A7500 REV:-.; [08] RII INSPECTED ACTION 7; [09] INSPECTION COMPLETE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CAPTAINS OUTBOARD FWD SEAT TRACK IS CORRODED ; / [01] RECEIVED AND INSTALLED NEW CAPTAINS OUTBOARD FWD SEAT TRACK IAW AMM 25-11-11-400-801.; [02] VERIFIED CORRECTIVE ACTION 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

FIRST OFFICERS INBOARD FWD SEAT TRACK IS CORRODED ; / [01] RECEIVED AND INSTALLED NEW F/O'S INBOARD FWD SEAT TRACK IAW AMM 25-11-11-400-801.; [02] VERIFIED CORRECTIVE ACTION 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CAPTAINS INBOARD FWD SEAT TRACK IS CORRODED ; / [01] RECEIVED AND INSTALLED NEW CAPTAINS INBOARD FWD SEAT TRACK IAW AMM 25-11-11-400-801.; [02] VERIFIED CORRECTIVE ACTION 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

FIRST OFFICERS OUTBOARD FWD SEAT TRACK IS CORRODED ; / [01] RECEIVED AND INSTALLED NEW F/O'S OUTBOARD FWD SEAT TRACK IAW AMM 25-11-11-400-801.; [02] UPDATED MEASUREMENT FIELDS.; [03] VERIFIED CORRECTIVE ACTION 1.

Part: ANGLE — CRACKED · airframe 68,361 hrs · 40,407 cycles

WATER TANK SUPPORT ANGLE P/N 149A8113-6 IS CRACKED BS 948 LBL 10 WL 178 ; / [01] REMOVED TANK SUPPORT ANGLE P/N 149A8113U6 IS CRACKED BS 948 LBL 10 WL 178 IAW SRM 51-40-02.; [02] THERE IS NO ALLOWABLE DAMAGE FOR WATER TANK SUPPORT ANGLE CRACK. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARA#9.; [03] LOCATED AND DRILLED NEW TANK SUPPORT ANGLE P/N 149A8113-6 PO#825068/4 BS 948 LBL 10 WL 178 IAW 51-40-05.; [04] CORRECTIVE ACTION STEP #3 LOCATED AND DRILLED NEW TANK SUPPORT ANGLE P/N 149A8113-6 LOT# 1459439-4 PO#825068/4 AT BS 948 LBL 10 WL 178 IAW SRM 51-40-05. AND DWG 149A8103 REV:-.; [05] VERIFIED CORRECTIVE ACTIONS 1-4.; [06] OK TO INSTALL; [07] VERIFIED CORRECTIVE ACTION 6; OK TO INSTALL; [08] INSTALLED NEW WATER TANK SUPPORT ANGLE P/N 149A8113-6; LOT#1459439-4; PO#825068-4; AT BS 948 LBL 10 WL 178; IAW SRM 51-40-02 AND DWG 149A8103 REV:-.; [09] VERIFIED CORRECTIVE ACTION 8.

Part: SHIELD — ELONGATED (AFT CARGO BAY) · airframe 68,361 hrs · 40,407 cycles

AFT CARGO BAY AFT SHIELD HAS ELONGATED HOLES ; / [01] ENLOGATED HOLES ACB AFT SHIELD AT BS847 - BS867 ; RBL21 WL164 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PARA 9C.; [02] VERIFIED ENLOGATED HOLES ACB AFT SHIELD AT BS847 - BS867 ; RBL21 WL164 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PARA 9C.; [03] REMOVED AT AFT CARGO BAY AFT SHIELD BS 867-887 RBL 21 WL 170 IAW SRM 51-40-02; [04] LOCATED DRILLED AFT CARGO BAY AFT NEW SHIELD BS 867-887 RBL 21 WL 170 ;P/N 146A8127-6 PO#780795/1 IAW SRM 51-40-05 AND DWG 146A0081 REV:A.; [05] VERIFIED CORRECTIVE ACTIONS 3-4; [06] OK TO INTALL; [07] OK TO INSTALL; [08] INSTALLED AFT CARGO BAY AFT SHIELD AT BS 846 TO 867 RBL 21 WL 164 IAW B737 SRM 51-40-02 AND DWG 146A0081.; [09] UPDATED PARTS REMOVED / INSTALLED.; [10] RII INSPECTED ACTION 8; [11] INSPECTION COMPLETE

Part: PANEL — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON FILLER PANEL JUST BELOW TOILET SERVICE DOOR CUT OUT AT B.S. 847+6 - 867; STRINGER 25 LEFT. ; / [01] REMOVED 4 EACH FASTNERS AT FILLER PANEL JUST BELOW TOILET SERVICE DOOR CUT OUT AT B.S. 847+6-867; STRINGER 25 LEFT PER SRM#51-40-02-0G-0; [02] REMOVED CORROSION BY BLEND OUT AREA L=3.3' W=2.0' PER SRM#51-10-02-0G-0 STEPS 15.A.(6)(A); [03] UPON FURTHER INVESTIGATION; NO ALLOWABLE LIMITS FOUND IN SRM; PART WILL BE REMOVED AND REPLACED.; [04] REMOVED FILLER PANEL JUST BELOW TOILET SERVICE DOOR CUT OUT AT B.S. 847+6-867; STRINGER 25LH PER REF SRM 51-40-02-0G <BR><BR>FABRICATED NEW FILLER FROM MATERIAL .100'' 2024T3 CLAD LOT NBR 1443470-1 PER REF DWG NBR 146A7401 AND SRM 51-40-05; [05] VERIFIED CORRECTIVE ACTION 4.; [06] APPLIED CHEMICAL CONVERSION COATING AND PRIME AT NEW FILLER PANEL PER SRM 51-20-01; [07] VERIFIED CORRECTIVE ACTION 6; OK TO INSTALL GIVEN.; [08] INSTALLED FILLER PANEL BELOW TOILET SERVICE DOOR CUT OUT AT BS 847+6 - 867 STRINGER 25LH PER REF SRM 51-40-02 AND DWG NBR 146A7401; [09] VERIFIED CORRECTIVE ACTION 8.; [10] INSPECTION COMPLETE

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON B.S. 1088; R.B.L. 27; W.L. 252. APU INLET CUT OUT UPPER FLANGE. ; / [01] REMOVED CORROSION ON APU INLET CUT UPPER STIFFENER P/N 148A2488-5 AT BS 1088; RBL 27; WL 252 : AREA 2' X 1' X .020' IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT'LL BE REAPIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9.C.; [02] REMOVED APU INLET CUT OUT UPPER STIFFENER P/N 148A2488-5 AT BS 1088; RBL 27; WL 252 IAW SRM 51-40-02.; [03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.; [04] LOCATED AND DRILLED NEW APU INLET CUT OUT UPPER STIFFENER P/N 148A2488-5 AT BS 1088; RBL 27; WL 252 IAW SRM 51-40-05 ; OK TO INSTALL; [05] VERIFIED CORRECTIVE ACTION 4; [06] INSTALLED NEW APU INLET CUT OUT UPPER STIFFENER P/N 148A2488-5 AT BS 1088; RBL 27; WL 252 IAW SRM 51-40-02 AND DWG # 148A0924; [07] PART USAGE INFO; [08] VERIFIED INSTALLED NEW APU INLET CUT OUT UPPER STIFFENER P/N 148A2488-5 AT BS 1088; RBL 27; WL 252 IAW SRM 51-40-02 AND DWG # 148A0924

Part: BRACKET — CRACKED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

FWD CARGO BAY BAFFLE ATTACH BRACKET IS CRACKED; FWD SIDE OF BS 420 FRAME RBL 21; WL 154 ; / [01] REMOVED FCB BAFFLE ATTACH BRACKET AT FWD SIDE OF BS 420 RBL21 IAW SRM 51-40-02; [02] FORMED ATTACH BRACKET ( CLIP) FROM MATERIAL 7075T0# 0.020' CLAD LOT. 1472547-1 IAW SRM 51-30-01-0G-0; DWG#143A7502.; [03] VERIFIED FORMED ATTACH BRACKET ( CLIP) FROM MATERIAL 7075T0# 0.020' CLAD LOT. 1472547-1 IAW SRM 51-30-01-0G-0; DWG#143A7502.; [04] HEAT TREATED CLIP RECEIVED (1EA.) ITEM HFAB53-CL-011; LOT.1472861-1; IN T62 CONDITION. LOCATED AND DRILLED CLIP IAW SRM 51-40-05-0G-0; DWG # 143A7505. OK TO TREAT AND PRIME..; [05] VERIFIED ACTION 4;OK TO TREAT AND PRIME; [06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON NEW CLIP IAW SRM 51-20-01; SOPM 20-41-02. OK TO INSTALL.; [07] INSPECTED ACTION 6; OK TO INSTALL; [08] INSTALLED AT FCB BAFFLE ATTACH BRACKET AT FWD SIDE OF BS 420 RBL21 IAW SRM 51-40-02; DWG# 143A7505.; [09] RII INSPECTED ACTION 8; [10] INSPECTION COMPLETE

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT IS CRACKED; BS 400-420 RBL 21; WL 156 ; / [01] REMOVED BAFFLE BS400-BS420 RBL21 WL156 IAW SRM 51-40-02; [02] DAMAGE FOUND ON FCB BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT BS 400- BS420 RBL 21 WL 156 P/N143A7510-34 L=0.500; OT=0.032 WITH DIGITAL CALIPER<BR>ID:ATS1317<BR>S/N:UNKNOWN<BR>DATE:06/2021<BR>DUE:06/2022<BR>FOUND TO BE OUT LIMITS IAW SRM 53-00-53-1A-2 AND IT WILL REPAIRABLE BY REPLACEMENT IAW 51-10-02-0G PAR 9C.; [03] RECEIVED AND DRILLED NEW BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT BS 400- BS420 RBL 21 WL 156 P/N 143A7510-34 IAW SRM 51-40-05-0G-0 AND DWG 143A7510.; [04] VERIFIED CORRECTIVE ACTION ITEMS 2 & 3.; [05] OK TO INSTALL.; [06] VERIFIED CORECTIVE ACTION 5; OK TO INSTALL GIVEN.; [07] INSTALLED BAFFLE LOCATED AT BTW. BS400-BS420 RBL21 WL156 IAW SRM 51-40-02; DWG# 143A7505.; [08] RII INSPECTED ACTION 7; [09] INSPECTION COMPLETE

Part: SUPPORT — CRACKED (FLIGHT DECK) · airframe 68,361 hrs · 40,407 cycles

FLIGHT DECK P18 CIRCUIT BREAKER PANEL ATTACH GUSSET CRACKED BS261 S-10L WL254. MARKED ; / [01] REMOVED SUPPORT CLIP WITH P/N 141A9502-10; LOCATED BTW BS. 261; STR10L; WL 254; IAW SRM 51-40-02; NO ALLOWABLE DAMAGE ENTRIES IN SRM PART WILL BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 PARAG.9.C; [02] VERIFIED CORRECTIVE ACTION STEP 1.; [03] FORMED NEW SUPPORT CLIP 6013T4#0.050'' LOT#1451927-1 IAW DRAWING#141A9502; HEAT TREATMENT REQUIRED TO T6; [04] VERIFIED FORMED NEW SUPPORT CLIP 6013T4#0.050'' LOT#1451927-1 IAW DRAWING#141A9502; HEAT TREATMENT REQUIRED TO T6.; [05] RECIVED ATTACH GUSSET FROM OSS PO NUMBER 841036-SWA; LOCATED AND DRILLED ATTACH GUSSET AT BS 261 STR 10L WL 254 PER SRM 51-40-05 AND DWG 141A9502; [06] OK TO TREAT AND PRIME PART; [07] VERIFIED CORRECTIVE ACTION 5 AND 6.; [08] APPLIED CHEMICAL CONVERTION COATING AND PRIMED ATTACH GUSSET PER AMM 51-21-41-370-802 AND AMM 51-21-72-370-804; OK TO INSTALL PART; [09] VERIFIED CORRECTIVE ACTION 8.; [10] INSTALLED AT FLIGHT DECK P18 CIRCUIT BREAKER PANEL ATTCH GUSSET (SUPPORT CLIP) LOCATED BS 261 STR10L WL 274 IAW SRM 51-40-02. DWG# 141A0720. ALL MAINTENANCE ACTIONS ARE COMPLETE REQUEST FINAL BUYOFF.; [11] VERIFIED CORRECTIVE ACTION 10; ALL WORK COMPLETE

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON FCB RH FLOOR TO SIDEWALL SUPPORT BS 400-420 RBL 21 WL 156 ; / [01] REMOVED CORROSION FLOOR TO SIDEWALL SUPPORT FWD CARGO BAY AT DISCREPANCY AREA BS400-420 RBL21 WL156; IN AREA L=3''; W=2''; D=0.012''; ORIGINAL THICKNESS 0.040''; REMAINING THICKNESS 0.030'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; TOOL USED: DEPTH GAGE ID:ATS1672; DUE DATE: 03/2022; [02] CORRECTION=REMOVED CORROSION FLOOR TO SIDEWALL SUPPORT FWD CARGO BAY AT DISCREPANCY AREA BS400-420 RBL21 WL156; IN AREA L=3''; W=2''; D=0.012''; ORIGINAL THICKNESS 0.040''; REMAINING THICKNESS 0.028'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; TOOL USED: DEPTH GAGE ID:ATS1672; DUE DATE: 03/2022; [03] VERIFIED CORRECTIVE ACTION 1 AND 2; [04] FABRICATED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT FCB FROM BS400 TO BS420 RBL21 WL156; MAT. ITEM #BAC1496-444#7075T6; LOT#5098100-1 IAW SRM 51-40-05-0G-0; DWG#143A7500;OK TO TREAT.; [05] VERIFIED CORRECTIVE ACTION STEP 4.; [06] APPLIED CHEMICAL CONVERCION COATING AND PRIMER IAW SRM 51-20-01-OG-0 AND SOPM 20-41-02 AT FLOOR TO SIDEWALL SUPPORT; [07] VERIFIED CORRECTIVE ACTION STEP 6.; [08] OK TO INSTALL .; [09] VERIFIED CORRECTIVE ACTION 8; OK TO INSTALL GIVEN.; [10] INSTALLED ON FCB RH FLOOR TO SIDEWALL SUPPORT BTW BS400 -420 RBL 21 WL 156 IAW SRM 51-40-02; DWG# 143A7500; [11] RII INSPECTED ACTION 10; [12] INSPECTION COMPLETE

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON R/H FCB SHIELD BS 420-440 WL 156 RBL 21 ; / [01] CORROSION ON THE R/H FCB SHIELD FROM BS 420-BS440 WL 156 RBL 21 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PARA 9C; [02] VERIFIED CORRECTIVE ACTION STEP 1.; [03] REMOVED R/H FCB SHIELD FROM BS 420-BS440 WL 156 RBL 21 IAW SRM 51-40-02; [04] LOCATED AND DRILLED NEW SHIELD P/N 143A8126U21; LOT# 1466561-1 IAW SRM 51-40-05 AND DWG 143A8126; [05] CORRECTED MEASUREMENTS SECTION; [06] VERIFIED STEPS 3; 4; AND 5 COMPLETE; [07] OK TO INSTALL; [08] VERIFIED OK TO INSTALL SHIELD; [09] INSTALLED NEW SHIELD-21 AT DISCREPANCY AREA PER SRM 51-40-02 AND DWG 143A0080 SHEET 27; [10] VERIFIED CORRECTIVE ACTION ITEM 9.; [11] ALL WORK STEPS COMPLETE; REQUESTING FINAL BUYOFF; [12] UPDATED PARTS USAGE; [13] VERIFIED ALL ITEMS COMPLETED AND VERIFIED. NO FURTHER ACTION REQUIRED.

Part: SUPPORT — CRACKED (FLIGHT DECK) · airframe 68,361 hrs · 40,407 cycles

FLIGHT DECK P18 CIRCUIT BREAKER PANEL ATTACH GUSSET CRACKED BS261 S-8L WL265. MARKED ; / [01] REMOVED SUPPORT CLIP WITH P/N 141A9502-5; LOCATED BTW BS. 261; STR8L; WL 265; IAW SRM 51-40-02; [02] REMOVED SUPPORT CLIP WITH P/N 141A9502-5; LOCATED BTW BS. 261; STR8L; WL 265; IAW SRM 51-40-02; NO ALLOWABLE DAMAGE ENTRIES IN SRM PART WILL BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 PARAG.9.C; [03] VERIFIED CORRECTIVE ACTION STEP 2.; [04] FORMED NEW SUPPORT CLIP 6013T4#0.050'' LOT#1451927-1 IAW DRAWING#141A9502; HEAT TREATMENT REQUIRED TO T6; [05] VERIFIED FORMED NEW SUPPORT CLIP 6013T4#0.050'' LOT#1451927-1 IAW DRAWING#141A9502; HEAT TREATMENT REQUIRED TO T6.; [06] RECIVED ATTACH GUSSET FROM OSS PO NUMBER 841036-SWA; LOCATED AND DRILLED ATTACH GUSSET AT BS 261 STR 8L WL 265 PER SRM 51-40-05 AND DWG 141A9502. OK TO TREAT AND PRIME PART; [07] VERIFIED CORRECTIVE ACTION 6.; [08] APPLIED CHEMICAL CONVERTION COATING AND PRIMED ATTACH GUSSET PER AMM 51-21-41-370-802 AND AMM 51-21-72-370-804; OK TO INSTALL PART; [09] VERIFIED CORRECTIVE ACTION 8.; [10] INSTALLED AT FLIGHT DECK P18 CIRCUIT BREAKER PANEL ATTCH GUSSET (SUPPORT CLIP) LOCATED BS 261 STR8L WL 274 IAW SRM 51-40-02. DWG# 141A0720. ALL MAINTENANCE ACTIONS ARE COMPLETE REQUEST FINAL BUYOFF.; [11] VERIFIED CORRECTIVE ACTION 10. ALL WORK COMPLETE.

Part: WEB — CORRODED (THRESHOLD) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON FCB SUBTHRESHOLD WEB ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-15-0I-1 FOR IDENTIFICATION AND SRM 53-30-15-1A-1 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROCION ON FCB SUBTHRESHOLD WEB IAW SRM 51-10-02-0G-0 MAXIMUM BLENDED AREA 10''X1''X0.010''DEEP; FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1; PAR.4.G.(2) FIG. 103 DETAIL G.; TOOL USED: DIAL DEEPTH GAGE; ID:ATS1225; S/N: N/A; DUE DATE: 07/2022.; [03] VERIFIED REMOVED CORROSION ON FCB SUBTHRESHOLD WEB IAW SRM 51-10-02-0G-0 MAXIMUM BLENDED AREA 10''X1''X0.010''DEEP; FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1; PAR.4.G.(2) FIG. 103 DETAIL G.; [04] LOCATED AND DRILLED ON FCB SUBTHRESHOLD WED BS. 440 TO 490 IAW SRM 51-40-05; [05] VERIFIED LOCATED AND DRILLED REPLACEMENT FCB SUBTHRESHOLD WEB AT FCB BS. 440 TO 490 IAW SRM 51-40-05; [06] REQUEST OK TO INSTALL THRESHOLD; [07] VERIFIED OK TO INSTALL FCB SUBTHRESHOLD WEB.; [08] INSTALLED NEW THRESHOLD WEB IN FCB IAW SRM 51-40-02 AND DWG 143A8330; [09] VERIFIED CORRECTIVE ACTION 8.; [10] VERIFIED ALL INSPECTION STEPS ARE COMPLETE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON FUSELAGE SKIN AT B.S. 1016 - 1088; L.B.L. 14 - R.B.L. 14; W.L. 306.5. ; / [01] REMOVED CORROSION ON FUSELAGE SKIN AT BS 1016 - 1088 LBL 14 - RBL 14 WL 306.5 ; ON MULTIPLE AREAS OF 20'X5' ; 10'X5' ; 33'X11' IAW SRM 53-00-01-1A-1; [02] VERIFIED CORRECTIVE ACTION STEP 1.; [03] REMOVED 55 FASTENERS IN THE DAMAGED AREA FOR ACCESS IAW SRM 51-40-02; [04] UT THICKNESS TESTED ALL BLENDED AREAS PER 737NDT PART 4 51-00-00 PROCEDURE 2. LOWEST REMAINING THICKNESS IN .063 POCKETS IS .059' AND LOWEST REMAINING IN .080 AREAS IS .076'. CAL ID E650; ATS2342.; [05] CORROSION ON FUSELAGE SKIN AT BS 1016 - 1088 LBL 14 - RBL 14 WL 306.5 FOUND TO BE OUT OF LIMITS DUE TO THE REMOVAL OF MATERIAL AROUND MORE THAN 3 FASTENERS IAW SRM 53-00-01-1A-1; [06] VERIFIED CORRECTIVE ACTION STEP 5.; [07] CORRECTION TO ITEM 4: LOWEST REMAINING THICKNESS IN ORIGINAL .080' AREA IS .067' PER ORIGINAL GRID MAP.; [08] CERTIFIED CORRECTION TO ITEM 4.; [09] INSTALLED 55 FASTENERS PER SRM 51-40-02 AND EA 21-153-03115; [10] VERIFIED FASTENERS REINSTALLED ON EA 21-153-03115-WIP 2 REF FAULT #TT8Q00705Z7; [11] VERIFIED TASK CARD IS COMPLETE.

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

FLOORBOARD 242VF HAS A PULLED THROUGH INSERT ON THE O/B EDGE ; / [01] DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 242VF; REPLACED PANEL IAW SRM 51-10-02-0G-0 PARA 9A(1) AND AIPC 53-21-00-26 ITEM 225.; [02] FLOORBOARD REPLACED. JOB COMPLETE.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

FLOORBOARD 242WF HAS PLY DAMAGE AND DELAMINATION ; / [01] IDENTIFIED PANEL 242WF IAW SRM 53-00-50-0I-1 FIGURE 6 AND TABLE 6. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F. AND WILL BE REPAIRED IAW SRM 53-00-50-2R-1. REMOVED 6 EA. INSERTS IAW SRM 53-00-50-2R-1 PARA 3.B. REMOVED TOOLSIDE PLY DAMAGE FROM THREE AREAS; THE LARGEST OF WHICH MEASURED APPROXIMATELY 9'X4.25'; AND CLEANED THE REPAIR AREAS. WORK ACCOMPLISHED IAW SRM 53-00-50-2R-1 PARA 4.A AND C-F. [13] FLOOR BOARD PANEL 242WF WAS REPAIRED IAW SRM 53-00-50-2R-1. REPAIR COMPLETE.; [14] VERIFIED CORRECTIVE ACTION 12 AND 13

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS947 RBL12 WL177. ; / [01] REMOVED CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE P/N 149A8118-29 AT BS 947; RBL 12; WL 177; AREA 2.5' X 1' X .020' IAW SRM51-10-02-0G-0. FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM; IT'LL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9.C.<BR><BR>TOOL USED ID: IS000686 ; 67171914; [02] REMOVED AND REPLACED AFT BULKHEAD TO FLOOR SUPPORT ANGLE P/N 149A8118-29 AT BS 947; RBL 12; WL 177 WILL BE ACCOMPLISHED ON C.C. TTG8Q006SXB5.; [03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2; [04] ALL WORK COMPLETED; REMOVAL AND INSTALLATION OF NEW BULKHEAD TO FLOOR SUPPORT ANGLE ACCOMPLISHED ON CUSTOMER CARD TTG8Q006SXB5; [05] VERIFIED CORRECTIVE ACTION ENTRY 4.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON STRINGER CLIP AT AREA AFT OF ACB BS986 RBL10 WL185. ; / [01] EVALUATED CORROSION DAMAGE ON STR CLIP AT ACB BS 986.5 STR 26R RBL10 WL185 FOUND TO BE OUT OF LIMIT DUE NO LIMITS IN SRM PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; [02] VERIFIED CORROSION OUT OF LIMITS DUE TO NO LIMIT STATED IN SRM; [03] REMOVED STR CLIP AT AREA AFT OFACB BS.986 RBL10 WL 185 IAW SRM 51-40-02; [04] LOCATED AND DRILLED NEW STR CLIP AT ACB BS 986 STR 26R RBL10 WL185 IAW SRM 51-40-05-0G-0; OK TO INSTALL; [05] VERIFIED CORRECTIVE ACTIONS 3-4; [06] INSTALLED NEW STR CLIP AT ACB BS 986 STR 26R RBL10 WL185 IAW SRM 51-40-02-0G-0 DWG 147A0040 - 147A0002; [07] VERIFIED CORRECTIVE ACTIONS 6

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 68,361 hrs · 40,407 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO BAY; FLOOR TO SIDE WALL SUPPORT CORRODED; BS500+4; 10; 14; 18;19;22; 30; 34; 42; 46; LBL24; WL156 / REMOVED CORROSION ON FLOOR TO SIDEWALL SUPP0RT AT DISCREPANCY AREA .FOUND TO BE OUT OF LIMITS AT BS 500 +4 L=1.6' W=0.6' D=0.14' ORIGINAL THICKNEES 0.040' REMAINING MAT=0.026' PER IAW 53-00-53-1A-2 FIG 103 CORECTION :USED TOOL ID ATS1672 DATE DUE 03/2022 VERIFIED CORRECTIVE ACTION 1 AND 2. CORRECTION:INFORMATION MEASUREMENTS VERIFIED CORRECTIVE ACTION 4 FABRICATED FLOOR TO SIDEWALL SUPPOR ZEE FROM BAC1496-444 7075T62 LOT#1467644-1 FROM BS400 TO 500D LBL24 IAW SRM 53-00-53-2R-6 REPAIR 6. OK TO TREAT AND PRIME REPAIR PARTS VERIFIED FABRICATED FLOOR TO SIDEWALL SUPPOR ZEE FROM BAC1496-444 7075T62 LOT#1467644-1 FROM BS400 TO 500D LBL24 IAW SRM 53-00-53-2R-6 REPAIR 6. FABRICATED (1EA) SPLICE SIDEPLATE FROM BAC1496-444 7075T62 LOT#1467644-1 LOCATED AT BS480+10LBL24WL.156 IAW SRM 53-00-53-2R-6 REPAIR 6 TABLE 201 [2]. VERIFIED CORRECTIVE ACTION STEP 8. APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON ALL REPAIR PARTS IAW SRM 53-00-53-2R-6PARAG.4.I.J. & SRM 51-20-01-0G-0 AND SOPM 20-41-02. OK TO INSTALL. VERIFIED CORRECTIVE ACTION STEP 10. VERIFIED OK TO INSTALL. INSTALLED AT FWD. CARGO BAY FLOOR TO SIDEWALL SUPPORT LOCATED BTW BS 400 - BS. 500D LBL 24 WL 156. IAW SRM 51-40-02 DWG# 143A7500 AND DWG#143A7505. VERIFIED CORRECTIVE ACTIONS 12

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-26L WL153. MARKED ; / [01] EVALUATED DAMAGE AREA ON STRINGER 26L FCB BS 540 WL 153 AND FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS OF SRM 53-00-03-1A-1; PART REPAIRABLE IAW SRM 53-00-03-2R-1-A01573 (REPAIR 1) FIGURE 205; CRACK L=2.0'' TOOL USED CALIPER ID:ATS2318 S/N:B19006095; [10] INSTALLED REPAIR PARTS REPLACEMENT STRINGER SECTION AND HAT SECTION SPLICE AT FCB FROM BS 500D+10 TO BS 540 S-26L WL153 AND APPLIED FILLET SEAL AND CIC AROUND REPAIR AREA IAW SRM 53-00-03-2R-1 REPAIR 1; [11] VERIFIED INSTALLED REPAIR PARTS REPLACEMENT STRINGER SECTION AND HAT SECTION SPLICE AT FCB FROM BS 500D+10 TO BS 540 S-26L WL153 AND APPLIED FILLET SEAL AND CIC AROUND REPAIR AREA IAW SRM 53-00-03-2R-1 REPAIR 1.; [12] N/A STEP 2 - SHEAR TIE REMOVED AND REPLACED ON FAULT TTG8Q006SS4Z; [13] COMPLETED/VERIFIED STEP 1 AND 2; [14] UPDATE TO STEP 12: COMPLETED STEP 2.; [15] VERIFIED CORRECTIVE ACTION 14- CORRECTIVE ACTION 12 FOR WORK IN STEP 2 WAS NOT N/A- VERIFIED SHEAR TIE INSTALLED ON FAULT TTG8Q006SS4Z

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-26R WL153. MARKED ; / [01] PERFORMED CUT OUT STRINGER 26R FCB AT BS 500D+ 10 TO BS 540 WL 153 IAW SRM 53-00-03-2R-1; [02] VERIFIED PERFORMED CUT OUT STRINGER 26R FCB AT BS 500D+ 10 TO BS 540 WL 153 IAW SRM 53-00-03-2R-1; [03] REQ HFEC CUT OUT FOR FREE CRACK CONDITION STR 26R FCB AT BS 500D+10 IAW SRM 53-00-03-2R-1; [04] HFEC INSPECTED IAW B737 NDTM P6; 51-00-00 PROC 23. NO CRACKS FOUND. TOOL ID IS000450; N500; [05] RECEIVED REPLACEMENT STRINGER SECTION FROM OSS TO HT T62 AND PENETRANT INSPECTED ON CUSTOMER # 840677-SWA IAW SRM 53-00-03-2R-1 REPAIR 1; [06] FABRICATED REPLACEMENT STRINGER SECTION FROM ITEM 5 ABOVE AND HAT SECTION SPLICE FROM PN# BAC1498-132#7075T62 CLAD LOT# 1454946-1. TREATED REAIR PARTS IAW SRM 53-00-03-2R-1 REPAIR 1... OK TO PRIME REPAIR PARTS AND REWORKED AREA; [07] VERIFIED CORRECTIVE ACTIONS 5 AND 6.; [08] PRIMED REPAIR PARTS AND REWORKED AREA IAW SRM 53-00-03-2R-1 REPAIR 1.... OK TO INSTALL; [09] VERIFIED ITEM 8 CORRECTIVE ACTIONS. OK TO INSTALL.; [10] INSTALLED REPAIR PARTS IAW SRM 53-00-03-2R-1 REPAIR 1; [11] REMOVED STRINGER CLIP AT BS 520 STR 26R IAW SRM 51-40-02; [12] INSTALLED STRINGER CLIP AT BS 520 STR26R IAW SRM 51-40-02; [13] VERIFIED CORRECTIVE ACTIONS 10-12

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

FWD CARGO BAY; FLOOR TO SIDE WALL SUPPORT CORRODED; BS500A+2; 6; 10; 18; 22; 26; RBL24; WL156 ; / [01] REMOVED CORROSION FLOOR TO SIDEWALL SUPPORT FWD CARGO BAY AT DISCREPANCY AREA BS500A+22 RBL24 WL156; IN AREA L=4''; W=2''; D=0.010; ORIGINAL THICKNESS 0.040''; REMAINING THICKNESS 0.030'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; TOOL USED: DEPTH GAGE ID:ATS1672; DUE DATE: 03/2022; [02] CORRECTION; INFORMATION MEASUREMENTS.; [03] VERIFIED CORRECTIVE ACTION 1; [04] FABRICATED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT FCB FROM BS 500A TO BS 500D RBL24 WL156; MAT. ITEM #BAC1496-444#7075T6; LOT#5098100-1 IAW SRM 51-40-05-0G-0; DWG#143A7501;OK TO TREAT.; [05] VERIFIED CORRECTIVE ACTION STEP 4. VERIFIED OK TO TREAT.; [06] APPLIED CHEMICAL CONVERCION COATING AND PRIMER IAW SRM 51-20-01-OG-0 AND SOPM 20-41-02 AT FLOOR TO SIDEWALL SUPPORT; [07] VERIFIED CORRECTIVE ACTION STEP 6.; [08] OK TO INSTALL; [09] OK TO INSTALL; [10] OKAY TO INSTALL FLOOR TO SIDEWALL SUPPORT IN FWD CARGO BAY AT BS 500A TO 500D; RBL 24.; [11] INSTALLED SIDE WALL SUPPORT IN FWD BAY AT BS 500A TO 500D; RBL 24 IAW SRM 51-40-02 DWG 143A7501; [12] VERIFIED INSTALLED FLOOR TO SIDE WALL SUPPORT IN FWD BAY AT BS 500A TO 500D; RBL 24 IAW SRM 51-40-02 DWG 143A7501; [13] VERIFIED ALL STEPS COMPLETE.; [14] UPDATED MEASURES TABLE

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

FWD CARGO BAY; FLOOR TO SIDE WALL SHIELD CORRODED; BS 492 TO 500A; RBL24; WL156 ; / [01] CORROSION FOUND ON SHIELD FWD CARGO BAY BS492 TO BS500A RBL24 WL156; P/N 143A8126U31; FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PARA 9C; [02] VERIFIED CORRECTIVE ACTION STEP 1.; [03] RECEIVED AND DRILLED NEW SHIELD P/N 143A8126U31 LOCATED ON FWD CARGO BAY BS492 TO BS500A RBL24 WL156 IAW SRM 51-40-05-0G-0 AND DWG 143A8126; [04] VERIFIED CORRECTIVE ACTION ITEM 3.; [05] OK TO INSTALL; [06] VERIFIED CORRCTIVE ACTION 5; OK TO INSTALL; [07] INSTALLED NEW FLOOR TO SIDE WALL SHIELD; BS. 492 T0 500A; WL 156 IAW SRM 51-40-02 DWG 143A8126; [08] INSTALLED NEW FLOOR TO SIDE WALL SHIELD; BS. 492 T0 500A; WL 156 IAW SRM 51-40-02 DWG 143A0080. ALL MAINTENANCE ACTION ARE COMPLETED REQUEST FINAL BUYOFF.; [09] VERIFIED CORRECTIVE ACTION 7 AND 8.; [10] VERIFIED ALL STEPS COMPLTETE.; [11] UPDATED PART INFORMATION.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-25R WL155. MARKED ; / [01] PERFORMED CUT OUT STRINGER 25R FCB AT BS 500D+ 10 TO BS 540 WL 155 IAW SRM 53-00-03-2R-1; [02] VERIFIED PERFORMED CUT OUT STRINGER 25R FCB AT BS 500D+ 10 TO BS 540 WL 155 IAW SRM 53-00-03-2R-1; [03] REQ HFEC CUT OUT FOR FREE CRACK CONDITION STR 25R FCB AT BS 500D+10 IAW SRM 53-00-03-2R-1; [04] HFEC INSPECTED IAW B737 NDTM P6; 51-00-00 PROC 23. NO CRACKS FOUND. TOOL ID IS000450; N500; [05] FORMED -2 CHANNEL (1EA) AND -3 ANGLE (2EA) FROM MATERIAL 7075TO - 0.040' CLAD LOT# 1468510-2 IAW SRM 53-00-03-2R-1 REPAIR 1 AND WIP1 21-153-03049; [06] VERIFIED CORRECTIVE ACTION 5.; [07] REPAIRED STR 25R PER EA 21-153-03049 AND SRM 53-00-03-2R-1; [08] VERIFIED REPAIRED STR 25R PER EA 21-153-03049 AND SRM 53-00-03-2R-1

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-23R WL164. MARKED ; / [01] PERFORMED CUT OUT STRINGER 23R FCB AT BS 500D+ 10 TO BS 540 WL 164 IAW SRM 53-00-03-2R-1; [02] REQ HFEC CUTOUT FOR FREE CRACK CONDITION STR 23R FCB AT BS 500D+10 IAW SRM 53-00-03-2R-1; [03] VERIFIED PERFORMED CUT OUT STRINGER 23R FCB AT BS 500D+ 10 TO BS 540 WL 164 IAW SRM 53-00-03-2R-1; [04] HFEC INSPECTED IAW B737 NDTM P6; 51-00-00 PROC 23. NO CRACKS FOUND. TOOL ID IS000450; N500; [05] RECEIVED REPLACEMENT STRINGER SECTION FROM OSS TO HT T62 AND PENETRANT INSPECTED PO#840653 IAW SRM 53-00-03-2R-1 REPAIR 1; [06] FABRICATED -1 HAT SECTION SPLICE FROM PN#69-78188-1 AND -7 REPLACEMENT STRINGER SECTION FROM ITEM 5 ABOVE. TREATED ALL REPAIR PARTS IAW SRM 53-00-03-2R-1 REPAIR 1 AND IAW ER#21-153-03064-WIP1. OK TO PRIME REPAIR PARTS AND REWORKED AREA...; [07] VERIFIED CORRECTIVE ACTION 5 AND 6.; [08] PRIMED REPAIR PARTS AND REWORKED AREA IAW SRM 53-00-03-2R-1 REPAIR 1 STEP 4J.... OK TO INSALL; [09] VERIFIED APPLICATION OF PRIMER ON REPAIR PARTS AND REWORKED AREA IAW SRM 53-00-03-2R-1 REPAIR 1 STEP 4J.... OK TO INSALL; [10] INSTALLED REPAIR PARTS IAW SRM 51-40-02 AND IAW SRM 53-00-03-2R-1 REPAIR 1 AND IAW EA#21-153-03064-WIP1; [11] VERIFIED INSTALLED REPAIR PARTS IAW SRM 51-40-02 AND IAW SRM 53-00-03-2R-1 REPAIR 1 AND IAW EA#21-153-03064-WIP1 .; [12] 'THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 21-153-03064'; [13] VERIFIED TASK IS COMPLETE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-27L WL150. MARKED ; / [01] EVALUATED DAMAGE AREA ON STRINGER 27L FCB BS 540 WL 153 AND FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS OF SRM 53-00-03-1A-1; PART REPAIRABLE IAW SRM 53-00-03-2R-1-A01573 (REPAIR 1) FIGURE 205; CRACK L=2.5'' TOOL USED CALIPER ID:ATS2318 S/N:B19006095; [10] INSTALLED REPAIR PARTS; REPLACEMENT STRINGER SECTION AND HAT SECTION SPLICE AT FCB BS 500D+10 TO BS 540 S-27L WL150 IAW SRM 53-00-03-2R-1 REPAIR 1; VERIFY STEP 1 AND STEP 2 FOR STRINGER CLIP AND SHEAR TIE INSTALLATION; [11] APPLIED FILLET SEAL AND CIC PROTECTION AROUND REPAIR AREA S-27L AT BS500D TO BS 540 FCB IAW SRM 53-00-03-2R-1; [12] VERIFIED CORRECTIVE ACTION 10<BR><BR>VERIFIED STEPS 1 AND 2 (STR CLIP AND SHEAR TIE INSTALL); [13] VERIFIED CORRECTIVE ACTION 11.; [14] UPDATED MEASUREMENTS; [15] ALL WORK STEPS COMPLETE; [16] VERIFIED ALL WORK COMPLETE AND ALL STEPS COMPLETE

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CRACKED INTERCOSTAL AT B.S. 312-328; L.B.L. 47; W.L. 208.1. ; / [01] REMOVED CRACKED INTERCOSTAL AT BS 312-328 ; LBL 47 WL 208.1 DUE TO NO ALLOWABLE LIMITS FOR CRACKS FOR THIS PART IAW SRM 51-10-02; [02] LOCATED AND DRILLED NEW INTERCOSTAL AT BS 312-328 LBL 47 WL 208.1 IAW SRM 51-40-05 OK TO INSTALL; [03] VERIFIED CORRECTIVE ACTIONS 1 AND 2; [04] INSTALLED NEW INTERCOSTAL AT BS 312-328 LBL 47 WL 208.1 IAW SRM 51-40-02AND DWG #141A5400; [05] VERIFIED INSTALLED NEW INTERCOSTAL AT BS 312-328 LBL 47 WL 208.1 IAW SRM 51-40-02AND DWG #141A5400

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CRACKED INTERCOSTAL AT B.S. 312-328; R.B.L. 31; W.L. 208.1. ; / [01] REMOVED CRACKED INTERCOSTAL AT BS 312-328 ; RBL 31 WL 208.1 DUE TO NO ALLOWABLE LIMITS FOR CRACKS FOR THIS PART IAW SRM 51-10-02; [02] LOCATED AND DRILLED NEW INTERCOSTAL AT BS 312-328 RBL 31 ; WL 208.1 IAW SRM 51-40-05 OK TO INSTALL; [03] VERIFIED CORRECTIVE ACTIONS 1 AND 2.; [04] INSTALLED NEW INTERCOSTAL AT BS 312-328 RBL31 WL 208.1 IAW SRM 51-40-02AND DWG #141A5400; [05] VERIFIED INSTALLED NEW INTERCOSTAL AT BS 312-328 RBL31 WL 208.1 IAW SRM 51-40-02AND DWG #141A5400

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767 - BS787 RBL21 WL157. ; / [01] REMOVED AT AFT CARGO BAY AFT SHIELD BTW BS 767 - BS 787; RBL21; WL 157; P/N 146A8127U1; PER SRM51-40-02; PART NO HAVE ENTRIES IN SRM BY ALLOWABLE DAMAGE MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 PARAG 9.C; [02] RECIVED NEW SHIELD ITEM 146A8127U1 LOT 1471800-1 LOCATED AND DRILLED NEW SHIELD AT BS 767-787 RBL21 WL 157; SRM 51-40-05-OG-0 DWG 146A0081.-; [03] VERIFIED CORRECTIVE ACTION STEP 1 AND 2; [04] OK TO INSTALL; [05] OK TO INSTALL; [06] INSTALLED NEW SHIELD ITEM 146A8127U1 LOT 1471800-1 AT AFT CARGO BAY BS 767-787 RBL21 WL 157 PER SRM 51-40-02-OG-0 DWG 146A0081.-; [07] REJECT: 21 EACH INCORRECT FASTENERS INSTALLED ON ACB FORWARD SHIELD BS 767 +1 - 787; RBL 20.5 - RBL 22.4; WL 157. RAISED FAULT TTG8Q0070TVC.; [08] REMOVED AND REPLACED FASTENERS INSTALLED ON ACB FORWARD SHIELD BS 767 +1 - 787; RBL 20.5 - RBL 22.4; WL 157 PER SRM 51-40-02-OG-0 DWG 146A0081.<BR> ALL REQUIRED MAINTENANCE ACTIONS ARE COMPLETE=REQUEST FINAL BUYOFF; [09] RII INSPECTED ACTION 8; [10] INSPECTION COMPLETE; [11] ALL REQUIRED MAINTENANCE ACTIONS ARE COMPLETE=REQUEST FINAL BUYOFF; [12] UPDATED PN IS MEASUREMENT FIELD.

Part: NONE — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON CHORD AT AREA AFT OF ACB BS1016 LBL5 WL188. ; / [01] REMOVED CORROSION FROM ACB BS 1016 LOWER CHORD SPLICE LBL 5; WL 188 IN AREA OF 3.5' X 1.5' ORIGINAL MATERIAL THICKNESS 0.080' FOUND TO BE OUT OF LIMIT DUE TO DAMAGE FOUND UNDER 8 EA FASTENERS IAW SRM 53-80-08-1A-1 PAR.4C (2A) FIG.103 E [12] VERIFIED 'REFER TO FAULT TTG8Q006SWEF WHERE EA 21-153-03031 WAS ADDED AS A SUBTASK'.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS727D S-26R WL151. ; / [01] EVALUATED CORROSION DAMAGE ON STR CLIP AT ACB BS.727D. S-26R WL151 FOUND TO BE OUT OF LIMITS DUE NO LIMIT IN RSM PART WILL BE REPAIRBLE BY REPLACEMENT IAW SRM 51-10-0-0G-0; [02] REMOVED STR CLIP AT AREA AFT OF ACB BS.727D STR 26R WL 151. IAW SRM 51-40-02; [03] LOCATED AND DRILL STR CLIP AT BS.727D STR 26R WL 151 IAW SRM 51-40-02 DWG 146A1220; OK TO INSTALL; [04] VERIFIED CORRECTIVE ACTIONS 1-3.; [05] ISNTALLED STR CLIP AT AFT CARGO BAY BS.727D STR 26R WL 151 IAW SRM 51-40-02 DWG 146A1260; [06] VERIFIED CORRECTIVE ACTIONS 5

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON STRINGER CLIP AT AREA AFT OF ACB BS986 RBL16 WL185. ; / [01] EVALUATED CORROSION DAMAGE ON STR CLIP AT ACB BS 986.5 STR 25R RBL16 WL185 FOUND TO BE OUT OF LIMIT DUE NO LIMITS IN SRM PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; [02] VERIFIED CORROSION REMOVAL FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS STATED IN SRM; [03] REMOVED STR CLIP AT AREA AFT OF ACB BS.986 RBL16 WL 185 IAW SRM 51-40-02; [04] LOCATED AND DRILLED NEW STR CLIP AT ACB BS 986.5 STR 25R RBL16 WL185 IAW SRM 51-40-05-0G-0; OK TO INSTALL; [05] VERIFIED CORRECTIVE ACTIONS 3-4; [06] INSTALLED NEW STR CLIP AT ACB BS 986 RBL16 WL185 IAW SRM 51-40-02-0G-0 DWG 147A0040 - 147A0002 CARD IS COMPLETED; [07] VERIFIED CORRECTIVE ACTIONS 6

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727B - BS767 RBL21 WL156. ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB P/N 146A7502-2 AREA 100' X 1' X .008' IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS DUE TO ORIGINAL MAT. THICKNESS .040' AND REMAINNING THICKNESS .032' IAW SRM 53-00-53-1A-2 STEP 4.A.(2).<BR><BR>IT WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP. 9.C.<BR><BR>TOOL USED ID: IS000686 ; S/N: 67171914<BR> DATE: 03/2021 ; DUE:03/2022; [02] REMOVED FLOOR TO SIDEWALL SUPPORT AT ACB P/N 146A7502-2 FROM BS 727 + 4' TO BS 787; RBL 21; WL 156 IAW SRM 51-10-02-0G-0; [03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2; [04] RECIVED NEW FLOOR TO SIDEWALL SUPPORT ITEM 146A8127U1 LOT 1471800-1 LOCATED AND DRILLED NEW FLOOR TO SIDEWALL AT BS 727-767 RBL21 WL 156; SRM 51-40-05-OG-0 DWG 146A7500.-; [11] VERIFIED INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727-767 RBL 21 WL 156;IAW SRM 51-40-02;DWG 146A7500 REV:C AND DWG 146A7502 REV:A.; [12] VERIFIED ALL STEPS COMPLETE.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS767 S-26L WL151. ; / [01] EVALUATED CORROSION DAMAGE ON STR CLIP AT ACB BS.767. S-26L WL151 FOUND TO BE OUT OF LIMITS DUE NO LIMIT IN RSM PART WILL BE REPAIRBLE BY REPLACEMENT IAW SRM 51-10-0-0G-0; [02] REMOVED STRINGER CLIP AT AFT CARGO BAY BS767; STR26L; WL151 IAW SRM 51-40-02.<BR><BR>TRIMMED; LOCATED AND DRILLED STRINGER CLIP WITH EXTRUSION BAC1493-856#7075T62-C; LOT 5062963-1; IAW SRM 51-40-05; [03] INSPECTED ACTION 2; [04] APPLIED A CHEMICAL CONVERSION COATING AND PRIMER ON NEW CLIP IAW SRM 51-20-01 AND SOPM 20-41-02; [05] VERIFIED ITEM 4 CORRECTIVE ACTIONS.; [06] OK TO INSTALL NEW CLIP; [07] OK TO INSTALL GIVEN.; [08] INSTALLED NEW STRINGER CLIP AT ACB BS767; STR26L; WL151 IAW SRM 51-40-02-0G-0 AND DRAWING#146A1261<BR>TASK COMPLETE; [09] VERIFIED CORRECTIVE ACTION ITEM 8.; [10] VERIFIED TASK IS COMPLETE.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON ATTACH ANGLE AT AFT CARGO BAY BS727D+4 RBL7 WL151. ; / [01] EVALUATED DAMAGE IN ATTACH ANGLE ACB AT BS 727D+4 RBL7 WL151 FOUND TO BE OUT LIMIT DUE NOT LIMITS IN SRM; PART WILL BE REPARAIBLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; [02] REMOVED ATTACH ANGLE ACB AT BS 727D+4 RBL 7 WL151 IAW SRM 51-40-02-0G-0; [03] VERIFIED CORRECTIVE ACTION STEPS1 AND 2.; [04] FABRICATED AND DRILLED NEW ANGLE FROM EXTRUSION BAC1493-672#7075-T62 LOT#1458580-1 TO BS 727D+4 RBL7 WL151 WL; 151 IAW SRM 51-40-05-0G-0 AND DWG 146A7730 .OK TO PRIME .; [05] VERIFIED FABRICATED AND DRILLED NEW ANGLE FROM EXTRUSION BAC1493-672#7075-T62 LOT#1458580-1 TO BS 727D+4 RBL7 WL151 IAW SRM 51-40-05-0G-0 AND DWG 146A7730.<BR>VERIFIED OK TO TREAT AND PRIME.; [06] APPLIED ONE LAYER OF BMS 10-11; TYPE I PRIMER ON ANGLE TO BS 727D+4 RBL 7 WL; 151 IAW SOPM SOPM 20-41-02.; [07] VERIFIED TREATED AND APPLIED ONE LAYER OF BMS 10-11; TYPE I PRIMER ON ANGLE TO BS 727D+4 RBL 7 WL 151 IAW SOPM 20-41-02.; [08] OK TO INSTALL ANGLE; [09] OK TO INSTALL.; [10] INSTALLED NEW ATTACH ANGLE AT ACB BS727D+4 RBL7 WL151 IAW SRM 51-40-02-0G-0 AND DRAWING#146A7730.<BR>TASK COMPLETE; [11] VERIFIED CORRECTIVE ACTION ITEM 10.; [12] CORRECTED REPAIR TYPE (N/A); [13] VERIFIED TASK IS COMPLETE.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON ATTACH ANGLE AT AFT CARGO BAY BS727D+5 RBL7 WL151. ; / [01] EVALUATED DAMAGE IN ATTACH ANGLE ACB AT BS 727D+5 RBL7 WL151 FOUND TO BE OUT LIMIT DUE NOT LIMITS IN SRM; PART WILL BE REPARAIBLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; [02] REMOVED ATTACH ANGLE ACB AT BS 727D+5 RBL7 WL151 IAW SRM 51-40-02-0G-0; [03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.; [04] FABRICATED AND DRILLED NEW ANGLE FROM EXTRUSION BAC1493-672#7075-T62 LOT#1458580-1 TO BS 727D+5 RBL 7 WL; 151 IAW SRM 51-40-05-0G-0 AND DWG 146A7730 .OK TO PRIME .; [05] VERIFIED FABRICATED AND DRILLED NEW ANGLE FROM EXTRUSION BAC1493-672#7075-T62 LOT#1458580-1 TO BS 727D+5 RBL 7 WL 151 IAW SRM 51-40-05-0G-0 AND DWG 146A7730.<BR>VERIFIED OK TO TREAT AND PRIME.; [06] APPLIED ONE LAYER OF BMS 10-11; TYPE I PRIMER ON ANGLE TO BS 727D+5 RBL 7 WL; 151 IAW SOPM SOPM 20-41-02.; [07] VERIFIED TREATED AND APPLIED ONE LAYER OF BMS 10-11; TYPE I PRIMER ON ANGLE TO BS 727D+5 RBL 7 WL 151 IAW SOPM 20-41-02.; [08] OK TO INSTALL ANGLE; [09] OK TO INSTALL.; [10] INSTALLED NEW ATTACH ANGLE AT ACB BS727D+5 RBL7 WL151 IAW SRM 51-40-02-0G-0 AND DRAWING#146A7730.<BR>TASK COMPLETE; [11] CORRECTED REPAIR TYPE (N/A); [12] VERIFIED CORRECTIVE ACTION ITEM 10.; [13] VERIFIED TASK IS COMPLETE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727 - BS807 LBL21 WL156. ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB P/N 146A7502-2 FROM BS 727 TO BS 807 LBL 21 WL 156; AREA 100' X 1' X .010' IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS DUE TO ORIGINAL MAT. THICKNESS .040' AND REMAINNING THICKNESS .030' IAW SRM 53-00-53-1A-2 STEP 4.A.(2). <BR><BR>IT WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP. 9.C. AND SRM 53-00-53-2R-5 REPAIR 5<BR><BR>TOOL USED ID: IS000686 ; S/N: 67171914 <BR> DATE: 03/2021 ; DUE:03/2022; [11] INSTALLED NEW SIDEWALL SUPPORT AT AFT CARGO BAY BTW BS727 THRU BS847; LBL21; WL156. IAW. SRM 51-40-02 AND DWG. 146A7500; [12] VERIFIED INSTALLATION OF NEW ACB FLOOR-TO-SIDEWALL SUPPORT; BS 727 - 847; LBL 21; WL 156; PER SRM 51-40-02 AND DWG 146A7500; [13] INSPECTION COMPLETE

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS895 RBL21 WL170. ; / [01] DAMAGE FOUND ON ACB AFT SIDEWALL SUPPORT BS895 RBL21 WL 170 P/N 147A7501-17;AREA OT=0.040 RT=0.035 X=0.005 L=0.600 W=0.300; <BR>WITH MICROMETER ID IS000686 <BR>SN:67171914 <BR>DATE:03/2021 <BR>DUE:03/2022 <BR> FOUND TO BE OUT LIMITS IAW SRM 53-00-53-1A-2 PAR 4.A(2) AND IT WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G PAR 9C.; [02] VERIFIED CORRECTIVE ACTION 1; [03] REMOVED FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 867-947 ;RBL 21 WL 170 IAW SRM 51-40-02.; [04] FABRICATED LOCATED AND DRILLED ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 867 TO BS 947 RBL 21 SPLICED ANGLE AT BS 887 MADE FROM BAC1496-377 LOT#5095753-1 EXTRUSION IAW SRM 51-40-05-0G-0 AND DWG#147A7500 OK TO TREAT AND PRIME; [05] VERIFIED CORRECTIVE ACTION ITEM 4.; [06] OK TO APPLY CHEMICAL CONVERSION COATING & PRIMER.; [07] APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 867 TO BS 947 RBL 21 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02; [08] VERIFIED CORRECTIVE ACTION ITEM 7.; [09] OK TO INSTALL.; [10] OK TO INSTALL; [11] INSTALLED NEW SIDEWALL SUPPORT AT AFT CARGO BAY BS 867 TO BS 947 RBL 21` WL 170 ;MADE FROM BAC 1496-377 LOT# 5095753-1 EXTRUSION IAW SRM 51-40-02; DWG 147A7500 REV:- AND DWG 146A7502 REV:A.; [12] VERIFIED INSTALLATION OF ACB FLOOR-TO-SIDEWALL SUPPORT; BS 867-947; RBL 21; WL 170; PER SRM 51-40-02; DWG 147A7500 AND DWG 146A7502; [13] INSPECTION COMPLETE

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS913 RBL21 WL173. ; / [01] DAMAGE FOUND ON ACB AFT SIDEWALL SUPPORT BS913 RBL21 WL 173 P/N 146A7502 FOUND TO BE OUT LIMITS ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G; [02] DAMAGE FOUND ON ACB AFT SIDEWALL SUPPORT BS913 RBL21 WL 173 P/N 147A7501-17;AREA OT=0.040 RT=0.035 X=0.005 L=0.600 W=0.300;<BR>WITH MICROMETER ID IS000686<BR>SN:67171914<BR>DATE:03/2021<BR>DUE:03/2022<BR> FOUND TO BE OUT LIMITS IAW SRM 53-00-53-1A-2 PAR 4.A(2) AND IT WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G PAR 9G.; [03] DAMAGE FOUND ON ACB AFT SIDEWALL SUPPORT BS913 RBL21 WL 173 P/N 147A7501-17;AREA OT=0.040 RT=0.035 X=0.005 L=0.600 W=0.300;<BR>WITH MICROMETER ID IS000686<BR>SN:67171914<BR>DATE:03/2021<BR>DUE:03/2022<BR> FOUND TO BE OUT LIMITS IAW SRM 53-00-53-1A-2 PAR 4.A(2) AND IT WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G PAR 9C.; [04] FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS913 RBL21 WL 173 WILL BE ACCOMPLISHED ON COSTUMER CARD[TTG8Q006SWH1].; [05] VERIFIED CORRECTIVE ACTION 3 AND 4; [06] FLOOR TO SIDEWALL SUPPORT INSTALLED ON FAULT TTG8Q006SWH1 STEP 11; [07] VERIFIED WORK TO BE ACCOMPLISHED ON TTG8Q006SWH1

Part: INTERCOSTAL — CORRODED (AFT CARGO BAY) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS946 LBL3 WL172. ; / [01] REMOVED CORROSION ON INTERCOSTAL AND ONE FASTENER AT ACB BS946; LBL3; WL172 IAW SRM 51-10-02 AND 51-40-02; [02] VERIFIED CORRECTIVE ACTION 1.; [03] UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.038' ADJACENT TO 0.045'. <BR>EQUIP ID#: ATS2031 S/N: 170515011; [04] ORIGINAL MATERIAL THICKNESS 0.045' REMAINING MATERIAL THICKNESS 0.038' FOUND TO BE OUT OFF LIMIT IAW SRM 53-70-51-1A-1 PAR.4B(2A) FIG 103 E; [05] VERIFIED ORIGINAL MATERIAL THICKNESS 0.045' REMAINING MATERIAL THICKNESS 0.038' FOUND TO BE OUT OFF LIMIT IAW SRM 53-70-51-1A-1 PAR.4B(2A) FIG 103 E.; [06] REMOVED INTERCOSTAL FROM ACB BS927 TO BS 947 LBL3 IAW SRM51-40-02-0G-0; [07] RECEIVED INTERCOSTAL FROM OSS TO HT T62 ON CUSTOMER RO# 843225-SWA (JOB# 544119); [08] FABRICATED; LOCATED AND DRILLED INTERCOSTAL FROM BS927-BS947 LBL3 AND APPLIED A CHEMICAL CONVERSION COATING TO THE REPARI PART IAW SRM 51-40-05 AND IAW SRM 51-20-01 AND IAW DWG#147A7580... OK TO PRIME REPAIR PART AND REWORKED AREA; [09] VERIFIED CORRECTIVE ACTION STEPS 7 AND 8. VERIFIED OK TO PRIME.; [10] PRIMED REPAIR PART AND REWORKED AREA IAW AMM 51-21-72-370-804... OK TO INSTALL; [11] VERIFIED CORRECTIVE ACTION STEP 10. VERIFIED OK TO INSTALL.; [12] INSTALLED NEW INTERCOSTAL AT BS 927 TO BS 947 LBL3 WL 172 ITEM#HFAB53-IN-011 ; PO#843225 IAW SRM 51-4-02-0G-0;DWG#147A7500; [13] VERIFIED CORRECTIVE ACTION ENTRY 12.; [14] VERIFIED COMPLETE

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 68,361 hrs · 40,407 cycles

FWD CARGO BAY; FLOOR TO SIDE WALL SUPPORT CORRODED;BS460+10; 14. LBL24; WL156 ; / [01] REMOVED CORROSION ON SIDEWALL SUPPORT AT DISCREPANCY AREA FOUND TO BE OUT OF LIMITS AT BS.460+14 . L=1.5' W=0.5' D=0.015' ORIGINAL THICKNEES 0.040' IAW SRM 53-00-53-1A-2 . FIG 103 USED TOOL ID ATS 1672 DATE DUE 03/2022; [02] THIS TASK CARD WILL BE ACCOMPLISHED WITH CUSTOMER CARD # TTG8Q006SQQM.; [03] VERIFIED CORRECTIVE ACTION 1.; [04] VERIFIED CORRECTIVE ACTION 2; THIS FAULT WILL BE ACCOMPLISHED ON CUSTOMER CARD #TTG8Q006SQQM; [05] UPDATED MEASUREMENT TABLE.

Part: RAIL — CORRODED (AFT CARGO BAY) · airframe 68,361 hrs · 40,407 cycles

CORROSION AT ACB ON RAIL AROUND FASTENER HOLE BS727+10 RBL3 WL156. ; / [01] REMOVED CORROSION ON RAILAROUND FASTENER HOLE CARGO BAY BS727+10 RBL3 WL156. MEASURES:L=1.2'; W=0.900'; D=0.008'. ORIGINAL THICKNESS: 0.063'; MATERIAL LOSS:0.008'; REMAINING THICKNESS OF MATERIAL:0.055'. THE RAIL IS OUT OF LIMITS. I.A.W. SRM 53-00-53-1A-2; ALLOWABLE DAMAGE 2; STEP 4(2). TOOL USED:ID ATS601 CAL DUE 05/2022.; [02] THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q006SWFB; [03] VERIFIED CORRECTIVE ACTIONS 1 AND 2.; [04] UPDATED PN IN MEASUREMENT TABLE.

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 68,361 hrs · 40,407 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS918 RBL10 WL171. ; / [01] DAMAGE ON SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS 918 WITH CRACK L=0.900 FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM AND IT WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G PAR 9C.; [02] REMOVED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS 918 RBL 10 WL 171 P/N 147A7221-32 IAW SRM 51-40-02.; [03] LOCATED AND DRILLED NEW SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGOBAY BS 918 RBL 10 WL 171;P/N 147A7221-32;LOT #1466021 PO#833561/1 IAW SRM 51-40-05 AND DWG 147A7221 REV:D.; [04] VERIFIED CORRECTIVE ACTIONS 1-3; [05] OK TO INSTALL.; [06] VERIFIED CORRECTIVE ACTIONS 5; [07] INSTALLED NEW SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS 918 RBL 10 WL 171 ;P/N 147A7221-32 LOT # 1466021 PO#833561/1 IAW SRM 51-40-02 AND DWG 147A7221 REV:D.; [08] UPDATED PARTS INFO; [09] VERIFIED CORRECTIVE ACTION 7-8

Part: RAIL — CORRODED (AFT CARGO BAY) · airframe 68,361 hrs · 40,407 cycles

CORROSION AT ACB ON RAIL AROUND FASTENER HOLE BS727+13 RBL3 WL156. ; / [01] REMOVED CORROSION ON RAILAROUND FASTENER HOLE CARGO BAY BS727+10 RBL3 WL156. MEASURES:L=1.2'; W=0.900'; D=0.007'. ORIGINAL THICKNESS: 0.063'; MATERIAL LOSS:0.007'; REMAINING THICKNESS OF MATERIAL:0.056'. THE RAIL IS OUT OF LIMITS. I.A.W. SRM 53-00-53-1A-2; ALLOWABLE DAMAGE 2; STEP 4(2). TOOL USED:ID ATS601 CAL DUE 05/2022.; [02] THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q006SWFB; [03] VERIFIED CORRECTIVE ACTIONS 1 AND 2.; [04] UPDATED PN IN MEASUREMENT TABLE.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS747 S-26R WL151. ; / [01] EVALUATED CORROSION DAMAGE ON STR CLIP AT ACB BS.747. S-26R WL151 FOUND TO BE OUT OF LIMITS DUE NO LIMIT IN SRM PART WILL BE REPAIRBLE BY REPLACEMENT IAW SRM 51-10-0-0G-0; [02] REMOVED STR CLIP AT AREA AFT OF ACB BS.747 STR 26R WL 151. IAW SRM 51-40-02; [03] LOCATED AND DRILL STR CLIP AT BS.747 STR 26R WL 151 IAW SRM 51-40-02 DWG 146A1220; OK TO INSTALL; [04] VERIFIED CORRECTIVE ACTIONS 1-3.; [05] ISNTALLED STR CLIP AT AFT CARGO BAY BS.747 STR 26R WL 151 IAW SRM 51-40-02 DWG 146A1260; [06] VERIFIED CORRECTIVE ACTION 5

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 68,361 hrs · 40,407 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS914 RBL10 WL171. ; / [01] DAMAGE ON SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS 914 WITH CRACK L=0.900 FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM AND IT WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G PAR 9C.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] REMOVED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS 914 RBL 10 WL 171; P/N 147A7221-32 IAW SRM 51-40-02.; [04] LOCATED AND DRILLED NEW SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS 914 RBL 10 WL 171; P/N 147A7221-32 ;LOT#1466021; PO#833561/1 IAW SRM 51-40-05 AND DWG 147A7221 REV:D.; [05] VERIFIED CORRECTIVE ACTIONS 1-4; [06] OK TO INSTALL.; [07] VERIFIED CORRECTIVE ACTIONS 6; [08] INSTALLED NEW SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS 914 RBL 10 WL 171 P/N 147A7221-32; LOT # 1466021 PO #833561/1 IAW SRM 51-40-02 AND 147A7221 REV:D.; [09] UPDATED PARTS INFO; [10] VERIFIED CORRECTIVE ACTION 8-9

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS933 RBL21 WL177. ; / [01] DAMAGE FOUND ON ACB AFT SIDEWALL SUPPORT BS933 RBL21 WL 177 P/N 147A7501-17;AREA OT=0.040 RT=0.035 X=0.005 L=0.600 W=0.300;<BR>WITH MICROMETER ID IS000686<BR>SN:67171914<BR>DATE:03/2021<BR>DUE:03/2022<BR> FOUND TO BE OUT LIMITS IAW SRM 53-00-53-1A-2 PAR 4.A(2) AND IT WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G PAR 9C.; [02] FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS933 RBL21 WL 177 WILL BE ACCOMPLISHED ON COSTUMER CARD[TTG8Q006SWH1].; [03] VERIFIED CORRECTIVE ACTION 1 AND 2; [04] FLOOR TO SIDEWALL SUPPORT INSTALLED ON FAULT TTG8Q006SWH1 STEP 11; [05] VERIFIED CORRECTIVE ACTION ENTRY 4.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CRACKED INTERCOSTAL AT B.S. 277-294.5; B.L. 0; W.L. 298.1. ; W.L. 208.1 / [01] REMOVED CRACKED INTERCOSTAL AT BS 277-294.5 ; BL 0 WL 208.1 DUE TO NO ALLOWABLE LIMITS FOR CRACKS FOR THIS PART IAW SRM 51-10-02; [02] LOCATED AND DRILLED NEW INTERCOSTAL AT BS 277-294.5 BL 0 WL 298.1 IAW SRM 51-40-05 OK TO INSTALL; [03] VERIFIED CORRECTIVE ACTIONS 1 AND 2.; [04] INSTALLED NEW INTERCOSTAL AT BS 277-294.5 BL 0 WL 208.1 IAW SRM 51-40-02AND DWG #141A5400; [05] VERIFIED INSTALLED NEW INTERCOSTAL AT BS 277-294.5 BL 0 WL 208.1 IAW SRM 51-40-02AND DWG #141A5400

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON STRINGER CLIP AT AREA AFT OF ACB BS986 RBL4 WL185. ; / [01] EVALUATED CORROSION DAMAGE ON STR CLIP AT ACB BS 986 STR 27R WL185 FOUND TO BE OUT OF LIMIT DUE NO LIMITS IN SRM PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 OG-0; [02] VERIFIED CORRECTIVE ACTION 1; [03] REMOVED STR CLIP AT AREA AFT OF ACB BS. 986 RBL 4 WL 185 IAW SRM 51-40-02; [04] LOCATED AND DRILLED NEW STR CLIP AT ACB BS 986 STR 27R RBL4 WL185 IAW SRM 51-40-05-0G-0; OK TO INSTALL; [05] VERIFIED CORRECTIVE ACTIONS 3-4; [06] INSTALLED NEW STR CLIP AT ACB BS 986 RBL4 WL185 IAW SRM 51-40-02-0G-0 DWG 147A0040 - 147A0002 CARD IS COMPLETED; [07] VERIFIED CORRECTIVE ACTIONS 6

Part: RAIL — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION AT ACB ON RAIL AROUND FASTENER HOLE BS727A+5 RBL3 WL156. ; / [01] REMOVED CORROSION ON RAILAROUND FASTENER HOLE CARGO BAY BS727A+5 RBL3 WL156. MEASURES:L=1.2'; W=0.900'; D=0.010'. ORIGINAL THICKNESS: 0.063'; MATERIAL LOSS:0.0010'; REMAINING THICKNESS OF MATERIAL:0.053'. THE RAIL IS OUT OF LIMITS. I.A.W. SRM 53-00-53-1A-2; ALLOWABLE DAMAGE 2; STEP 4(2). TOOL USED:ID ATS601 CAL DUE 05/2022.; [14] INSTALLED NEW RAIL SECTION(CHANNEL FILLER ) FROM B/S 727 TO B/S 727B+10' AND CHANNEL SPLICE LOCATED BTW B/S 727B TO B/S 727C RBL 3 WL 156 IAW SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 1 AND DWG 146AOO61 REV:A; [15] VERIFIED CORRECTIVE ACTIONS 14.; [16] UPDATED PN IN MEASUREMENT TABLE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

FWD CARGO BAY; FLOOR TO SIDE WALL SUPPORT CORRODED; BS500B+10; 14; 30; 34; LBL24; WL156 ; / [01] REMOVED CORROSION ON SIDEWALL SUPPORT AT DISCREPANCY AREA FOUND TO BE OUT OF LIMITS AT BS.500B+10 L=1.8' W=0.6' D=0.013 ORIGINAL THICKNEES 0.040' IAW SRM 53-00-53-1A-2 . FIG 103 USED TOOL ID ATS 1672 DATE DUE 03/2022; [02] THIS TASK CARD WILL BE ACCOMPLISHED WITH CUSTOMER CARD # TTG8Q006SQQM.; [03] VERIFIED CORRECTIVE ACTIONS 1 AND 2<BR>WILL BE ACCOMPLISHED ON TTG8Q006SQQM.; [04] UPDATED MEASURES TABLES.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS747 S-26L WL151. ; / [01] EVALUATED CORROSION DAMAGE ON STR CLIP AT ACB BS.747. S-26L WL151 FOUND TO BE OUT OF LIMITS DUE NO LIMIT IN SRM PART WILL BE REPAIRBLE BY REPLACEMENT IAW SRM 51-10-0-0G-0; [02] VERIFIED CORRECTIVE ACTION 1 (OUT OF LIMITS).; [03] REMOVED STR CLIP AT AREA AFT OF ACB BS.747 STR 26L WL 151. IAW SRM 51-40-02; [04] LOCATED AND DRILLED NEW STRINGER CLIP P/N 146A1010-14; LOT 1472287-1; IAW SRM 51-40-05<BR><BR>OK TO INSTALL; [05] INSPECTED ACTION 4; OK TO INSTALL; [06] INSTALLED NEW STRINGER CLIP AT ACB BS747; STR26L; WL151 IAW SRM 51-40-02-0G-0 AND DRAWING#146A1220<BR>TASK COMPLETE; [07] CORRECTED REPAIR TYPE (N/A); [08] VERIFIED CORRECTIVE ACTION ITEM 6.; [09] VERIFIED TASK IS COMPLETE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS947 RBL17 WL177. ; / [01] REMOVED CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE P/N 149A8118-29 AT BS 947; RBL 17; WL 177; AREA 2.5' X 1' X .020' IAW SRM 51-10-02 -0G-0; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM. IT'LL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9.C.<BR><BR>TOOL USED ID: IS000686 ; S/N: 67171914; [[10] INSTALLED AFT BULKHEAD TO FLOOR SUPPORT ANGLE P/N 149A8118-29 AT BS 947; RBL 21 FROM LBL 10; WL 177 IAW SRM 51-40-02-0G-0 AND DWG149A8117 ID:004; REV:C; [11] VERIFIED INSTALLATION OF AFT BULKHEAD-TO-FLOOR-SUPPORT ANGLE; BS 947; RBL 17; WL 177 PER SRM 51-40-02 AND DWG 149A8117; [12] VERIFIED ALL WORK STEPS COMPLETE THIS TASK

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON ATTACH ANGLE AT AFT CARGO BAY BS727D+5 LBL5 WL151. ; CORROSION ON ATTACH ANGLES AT AFT CARGO BAY BS 727D+5 LBL5 AND 727D+5 LBL4 WL151 / [01] EVALUATED DAMAGE IN ATTACH ANGLE ACB AT BS 727D+5 LBL5 WL151 FOUND TO BE OUT LIMIT DUE NOT LIMITS IN SRM; PART WILL BE REPARAIBLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; [02] REMOVED ANGLE ACB AT BS 727D+5 LBL5 WL151 IAW SRM 51-40-02-0G-0; [03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.; [04] FABRICATED AND DRILLED NEW ANGLE FROM EXTRUSION BAC1493-672#7075-T62 LOT#1458580-1 TO BS 727D+5 LBL5 WL151 WL; 151 IAW SRM 51-40-05-0G-0 AND DWG 146A7730 .OK TO PRIME .; [14] INSTALLED NEW ATTACH ANGLE AT ACB BS727D+5 LBL5 WL151 IAW SRM 51-40-02-0G-0 AND DRAWING#146A7730.<BR>TASK COMPLETE; [15] VERIFIED CORRECTIVE ACTION ITEM 14.; [16] CORRECTED REPAIR TYPE (N/A); [17] VERIFIED TASK IS COMPLETE.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CRACKED BULKHEAD PANEL SUPPORT ATTACH ANGLE AT AFT CARGO BAY BS866 LBL10 WL166. ; / [01] REMOVED SUPPORT ATTACH ANGLE AT AFT CARGO BAY BS866; LBL10; WL166. IAW. SRM 51-10-02-0G-0.; [02] RECEIVED BRACKET P/N 149A8109U114; LOT 1467715-3; LOCATED AND DRILLED NEW BRACKET OF PANEL SUPPORT ATTACH <BR>AT AFT CARGO BAY BS866; LBL10; WL166. IAW.SRM 51-40-05. OK TO INSTALL.; [03] INSPECTED ACTION 2; OK TO INSTALL; [04] INSTALLED NEW BRACKETON SUPPORT ATTACH ANGLE AT AFT CARGO BAY BS866; LBL10; WL166. IAW. SRM 51-40-02-0G-0 AND DWG#149A8102.; [05] RII INSPECTED ACTION 4; [06] INSPECTION COMPLETE

Part: NONE — CORRODED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

CORROSION ON CHORD AT AREA AFT OF ACB BS1016 RBL5 WL188. ; / [01] REMOVED CORROSION FROM ACB BS 1016 LOWER CHORD SPLICE RBL 5; WL 188 IN AREA OF 3.5' X 1.5' ORIGINAL MATERIAL THICKNESS 0.080' FOUND TO BE OUT OF LIMIT DUE TO DAMAGE FOUND UNDER 8 EA FASTENERS IAW SRM 53-80-08-1A-1 PAR.4C (2A) FIG.103 E; [15] REPAIRED PER EA 21-153-03031 ALL COMPLETED; [16] VERIFIED CORRECTIVE ACTIONS 14-15

Part: GUSSET — CRACKED (L/H WING) · airframe 68,361 hrs · 40,407 cycles

LEFT WING; UPPER T/E PANEL BETWEEN #5 AND 6 SPOILERS; LOWER SURFACE CENTER SUPPORT GUSSET IS CRACKED AT TRANSVERSE WEB ATTACH POINT ; / [01] REMOVED CRACKED L/W T/E UPPER PANEL CENTER SUPPORT GUSSET PER AMM 20-00-00 AND SRM 51-10-02-0G-0 STEP 9. LOCATED AND DRILLED NEW GUSSET PER SRM 51-40-05-0G-0 TABLE 3. REMOVED AND INSTALLED SEAL RETAINER ONTO NEW GUSSET PER SRM 51-40-02-0G-0 STEP 4. B.; C.; & E. AND VERIFIED FASTENER CALLOUT PER AIPC 57-50-00-25 ITEM 35. PAINTED NEW GUSSET PER AMM 51-21-99-300-801 STEP 2. E. (6). INSTALLED NEW GUSSET ON TRAILING EDGE PER AMM 20-50-11. CALIBRATED TOOL USED:<BR>CALID: PER1189 SN: 04155309 DUE: 07/2022; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] UPDATED MEASUREMENTS.; [04] VERIFIED ALL STEPS COMPLETE.

Part: GUSSET — CRACKED (R/H WING) · airframe 68,361 hrs · 40,407 cycles

RIGHT WING; UPPER T/E PANEL BETWEEN #7 AND 8 SPOILERS; LOWER SURFACE CENTER GUSSET IS CRACKED AT TRANSVERSE WEB ATTACH POINT ; / [01] REMOVED CRACKED R/W T/E UPPER PANEL CENTER SUPPORT GUSSET PER AMM 20-00-00 AND SRM 51-10-02-0G-0 STEP 9. LOCATED AND DRILLED NEW GUSSET PER SRM 51-40-05-0G-0 TABLE 3. REMOVED AND INSTALLED SEAL RETAINER ONTO NEW GUSSET PER SRM 51-40-02-0G-0 STEP 4. B.; C.; & E. AND VERIFIED FASTENER CALLOUT PER AIPC 57-50-00-25 ITEM 35. PAINTED NEW GUSSET PER AMM 51-21-99-300-801 STEP 2. E. (6). INSTALLED NEW GUSSET ON TRAILING EDGE PER AMM 20-50-11. CALIBRATED TOOL USED:<BR>CALID: PER1189 SN: 04155309 DUE: 07/2022; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] UPDATED MEASUREMENTS.; [04] VERIFIED ALL STEPS COMPLETE.

Part: DOOR — OUT OF ADJUST (L1 DOOR) · airframe 68,361 hrs · 40,407 cycles

FWD ENTRY DOOR IS SAGGING ; / [01] REMOVED PANEL 831AZ FOR ACCESS PER AMM 52-11-00-820-801 STEPS 2. I. (1) (E) 1).; [02] REMOVED FORWARD ENTRY DOOR PER AMM 52-11-00-000-802; [03] REMOVED UPPER LWR GUIDE PLATE AND INSTALLED NEW (141A6285-1) PER SOPM 20-50-01 AND IPC: 52-11-51-09.; [04] REMOVED LWR UPPER GUIDE PLATE FOR REPLACEMENT PER SOPM 20-50-01 AND IPC: 52-11-51-09; [05] INSPECTED ACTION 3; [06] INSTALLED NEW FED LOWR UPPER GUIDE PLATE PER SOPM 20-50-01 AND IPC: 52-11-51-09.; [07] UPDATE TO PARTS LIST.; [08] INSPECTED ACTION 6;7; [09] REINSTALLED FWD ENTRY DOOR PER AMM 52-11-00-400-802. STEPS 3. G. 1-12 H. 2; 3; 4.; [11] VERIFIED FWD ENTRY DOOR REINSTALLED AND SAFETY DEVICES PER AMM 52-11-00-400-802. STEPS 3. G. 1-12 H. 2; 3; 4. VERIFIED FWD ENTRY DOOR ADJUSTED PER AMM 52-11-00-820-801 STEPS (2) I. (1) A-J; AND STEP U. (1) A-D. DOOR IS NO LONGER SAGGING OR RIDING LATCH FITTING.; [12] OK TO CLOSE PANEL 831AZ; [13] CLOSED PANEL 831AZ PER AMM 52-11-00-820-801 STEP 2. R. (1) (F) AND SOPM 20-50-01.;

Part: STIFFENER — CRACKED (R/H HORIZ. STAB.) · airframe 68,361 hrs · 40,407 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; 129.50; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 129.50 RIB 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4; [15] INSTALLED REPAIR PARTS AT RH HORIZONTAL STABILIZER INSPAR RIB STAB STA 129.50 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-5; [16] VERIFIED CORRECTIVE ACTION 15.

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 68,361 hrs · 40,407 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; 92.7; 2ND VERTICAL STIFFENER IS CRACKED. ; / [01] REMOVED THE DAMAGED PART OF THE RIB AT R/H HORIZ. STAB. 92.7 2ND VERTICAL IAW SRM 55-10-09-2R-4; [02] VERIFIED DAMAGE REMOVAL: REMOVED THE DAMAGED PART OF THE RIB AT R/H HORIZ. STAB. 92.7 2ND VERTICAL IAW SRM 55-10-09-2R-4; [03] HFEC REQUEST ON THE CUT OUT EDGES; WEB AND EXISTING FASTENERS HOLES WITHIN THE REPAIR AREA TO ENSURE NO CRACKS EXIST.; [04] HFEC INSPECTED CUTOUT RIB AREA; IAW B737 NDTM P6; 51-00-00 PROC 23. NO CRACKS NOTED. TOOL ID ATS1465; N600; [05] HFEC INSPECTED OPEN HOLES COMMON TO REPAIR AREA IAW B737 NDTM P6; 51-00-00 PROC 16. NO CRACKS NOTED. TOOL ID ATS1465; N600; TOOL ID ATS1411; MINIMITE; [06] FABRICATED REPAIR PARTS (1) T-SECTION FROM 60-5872 7075 T76511 LOT# 1449876-1 (2) ANGLE FROM BAC 1490-2793 7075 T62 CLAD LOT# 1442205-1 (3) SHIM FROM 7075 T6 0.020' CLAD LOT# 1381332-1; APPLIED CHEMICAL CONVERSION COATING IAW SRM 55-10-09-2R-4 OK TO PRIME.; [07] VERIFIED CORRECTIVE ACTION STEP 6. VERIFIED OK TO PRIME.; [08] PRIMED REPAIR PARTS AND COMMON AREA IAW SRM 55-10-09-2R-4 OK TO INSTALL.; [09] VERIFIED CORRECTIVE ACTION 8; OK TO INSTALL; [10] INSTALLED REPAIR PARTS AT RH HORIZONTAL STABILIZER INSPAR RIB STAB STA 92.7 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4; [11] VERIFIED CORRECTIVE ACTION 10

Part: RIB — CRACKED (RL/H HORIZ. STAB) · airframe 68,361 hrs · 40,407 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; 92.7; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] REMOVED THE DAMAGED PART OF THE RIB AT R/H HORIZ. STAB. 92.7 3RD VERTICAL IAW SRM 55-10-09-2R-4; [02] VERIFIED DAMAGE REMOVAL: REMOVED THE DAMAGED PART OF THE RIB AT R/H HORIZ. STAB. 92.7 3RD VERTICAL IAW SRM 55-10-09-2R-4; [03] HFEC REQUEST ON THE CUT OUT EDGES; WEB AND EXISTING FASTENERS HOLES WITHIN THE REPAIR AREA TO ENSURE NO CRACKS EXIST.; [04] HFEC INSPECTED CUTOUT AREA OF RIB IAW B737 NDTM P6; 51-00-00 PROC 23. NO CRACKS NOTED. TOOL ID ATS1465; N600; [05] HFEC INSPECTED OPEN HOLES COMMON TO REPAIR AREA IAW B737 NDTM P6; 51-00-00 PROC 16. NO CRACKS NOTED. TOOL ID ATS1465; N600; TOOL ID ATS1411; MINIMITE; [06] FABRICATED REPAIR PARTS (1) T-SECTION FROM 60-5872 7075 T76511 LOT# 1449876-1 (2) ANGLE FROM BAC 1490-2793 7075 T62 CLAD LOT# 1442205-1 (3) SHIM FROM 7075 T6 0.020' CLAD LOT# 1381332-1; APPLIED CHEMICAL CONVERSION COATING IAW SRM 55-10-09-2R-4 OK TO PRIME.; [07] VERIFIED CORRECTIVE ACTION STEP 6.VERIFIED OK TO TREAT AND PRIME.; [08] PRIMED REPAIR PARTS AND COMMON AREA IAW SRM 55-10-09-2R-4 OK TO INSTALL.; [09] VERIFIED CORRECTIVE ACTION 8; OK TO INSTALL; [10] INSTALLED REPAIR PARTS AT RH HORIZONTAL STABILIZER INSPAR RIB STAB STA 92.7 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4; [11] VERIFIED CORRECTIVE ACTION 10.

Part: NONE — CRACKED (FUSELAGE) · airframe 68,361 hrs · 40,407 cycles

MAIN CABIN; HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 664.5; RBL 40.5 ; / [01] CRACK FOUND ON HORIZONTAL PRESSURE DECK WEB AT BS 664.5; RBL40.5 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM PART WILL BE REPAIRED IAW SRM 53-40-51-2R-2 REPAIR 2; FIG. 202.; ANT MIXED UP ON O8-OCT-2021 AT 18:00 UTC ; 100% TEMPORARY AND PERMANENT FASTENERS INSTALLED WITHIN SEALANT SQUEEZE OUT PRIOR TO 09-OCT- 2021 AT 18:00 TIME REF. SOPM 20-56-19 AND SRM 53-40-51-2R-2; REPAIR 2 AND SRM 51-40-02-0G-0.; [15] INSTALLED REAPIR PARTS AT BS 663.75 FROM RBL 38 TO RBL 60 HORIZONTAL PRESSURE DECK WEB IAW SRM 53-40-51-2R-2 REPAIR 2; SRM -51-40-02-0G-0 AND DWG#144A7710; [16] VERIFIED INSTALLED REAPIR PARTS AT BS 663.75 FROM RBL 38 TO RBL 60 HORIZONTAL PRESSURE DECK WEB IAW SRM 53-40-51-2R-2 REPAIR 2; SRM -51-40-02-0G-0 AND DWG#144A7710.; [17] APPLIED FILLET SEAL AND CIC TO THE REPAIR AREA AT BS 663.75 FROM RBL 38 TO RBL 60 HORIZONTAL PRESSURE DECK WEB IAW SRM 53-40-51-2R-2 REPAIR 2; [18] REMOVED EWIS PROTECTION FROM THE REPAIR AREA IAW AMM 20-60-07-913-801; [19] VERIFIED REMOVAL OF EWIS PROTECTION FROM REPAIR AREA PER AMM 20-60-07; [20] VERIFIED FILLET SEAL AND CIC TO THE REPAIR AREA AT BS 663.75; FROM RBL 38 TO RBL 60; IAW SRM 53-40-51-2R-2 REPAIR 2; [21] VERIFIED COMPLETION OF REPAIR ON RH HORIZONTAL PRESSURE DECK WEB; BS 664.5; RBL 38-60; IAW SRM 53-40-51-2R-2; REPAIR 2

Part: NONE — CRACKED (L/H WING) · airframe 68,361 hrs · 40,407 cycles

CRACK AROUND THE FASTENER AT NO.2 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. MARKED ; / [01] NDI VERIFY CRACK AT #2 SLAT LOWER SKIN AT ACTUATOR RIB PER SRM 51-10-02-0G-0 STEP 5.C.; [ [22] INSTALLED REPAIR PARTS IAW SRM 57-42-01-2R-8; STEP L.<BR>OK TO CLOSE.; [23] VERIFIED CORRECTIVE ACTION STEP 22. VERIFIED OK TO CLOSE.; [24] INSTALLED PANELS 524CB; 524DB; 524EB AND FLEX SKIN SLAT #2 IAW SRM 51-40-02.; [25] VERIFIED CORRECTIVE ACTION STEP 24.; [26] COMPLETED REPAIR AT SLAT # 2 IAW SRM 57-42-01-2R-8; STEPS M; O; P AND R.; [27] COMPLETE; [28] VERIFIED ALL NDT REQUIREMENTS ARE COMPLETE; JOB COMPLETE.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 65,277 hrs · 38,479 cycles

R2 DOOR SLIDE PRESSURE IN THE RED. R&R SLIDE PER MT.

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 63,650 hrs · 37,431 cycles

FAIRING PANEL 193B-FASTENER HOLE #33; #38 AND #28 DAMAGE AND DELAMINATION / PERMANENT REPAIR PERFORMED PER SRM 51-70-05-2R-10; REPAIR 10.

Part: FITTING — LOOSE (R2 DOOR) · airframe 63,225 hrs · 37,171 cycles

R2 DOOR FORWARD GIRT BAR FITTING LOOSE. SECURED FITTING IAW AMM.

Part: GIRT BAR — LOOSE (L2 DOOR) · airframe 63,225 hrs · 37,171 cycles

L2 DOOR AFT GIRT BAR FITTING LOOSE. SECURED GIRT BAR ASSEMBLY IAW AMM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 63,225 hrs · 37,171 cycles

LT CENTER CEILING EMERGENCY EXIT LIGHT CONNECTOR DAMAGED AT BS 640. R&R CONNECTOR PER AMM.

Part: STRINGER CLIP — ELONGATED (AFT CARGO BAY) · airframe 63,225 hrs · 37,171 cycles

STRINGER CLIP AT BS 807 STRINGER 27 R/H HAS ELONGATED HOLE COMMON TO BS 807 FRAME / REMOVED DAMAGED STRINGER CLIP; FABRICATED AND INSTALLED NEW STRINGER CLIP FROM AFT CARGO BAY AT BS 807 STR 27R IAW SRM 51-40-02-0G-0 SRM 51-30-01; DWG# 146A8133; PO# 705171; SRM 51-40-05-0G-0 AND DWG# 146A8130

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 63,225 hrs · 37,171 cycles

VAPOR BARRIER STIFFENER CRACKED AT BS 663, LBL 31. R&R STIFFENER IAW DWG AND SRM.

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 63,225 hrs · 37,171 cycles

VERTICAL STIFFENER IS CRACKED AT BS663 RBL 27 WL145 / REPLACED AND REINSTALLED VERTICAL STIFFENER AT BS 663 RBL 27 WL 145 P/N 7530305 PO # 703100 REMOVED ON CUSTOMER CARD T896911 IAW SRM 51-40-02 AND DWG # 111A1000 REV B 80641U 30AUG18

Part: ANGLE — CRACKED (RT MLG WW) · airframe 63,225 hrs · 37,171 cycles

REAR SPAR VAPOR BARRIER ATTACHED ANGLE CRACKED AT BS 663, RBL 8. REPAIRED ANGLE IAW EA.

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 63,225 hrs · 37,171 cycles

PANEL 193CR HAS A CRACK ON THE INNER SKIN / REPAIRED CRACK ON THE INNER SKIN PANEL 193CR IAW SRM 51-70-05-2R-1. 56749U 27AUG18

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT SIDE UNDER CARGO BAY FLOOR TO SIDEWALL SUPPORT ATTACH CLIP CRACKED AT BS 500C, LBL 24. R&R CLIP IAW DWG & SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

RT FLOOR TO SIDEWALL SUPPORT INTERCOSTAL ATTACH CLIP CRACKED AT BS 500C. R&R CLIP IAW DWG & SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD CARGO BAY INTERCOSTAL ATTACH ANGLE CRACKED AT BS 500C, LBL 24. R&R ANGLE IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500B TO BS 500C, LBL 24. R&R INTERCOSTAL IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500A TO BS 500B, LBL 24. R&R INTERCOSTAL IAW SRM & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500 TO BS 500A, LBL 24. R&R INTERCOSTAL IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FWD CARGO LH) · airframe 63,225 hrs · 37,171 cycles

FWD CARGO BAY INTERCOSTAL IS CRACKED AT BS 400 TO 420 LBL 24 / REMOVED AND REPLACED FCB INTERCOSTAL BS400 TO BS420 LBL24 P/N 143A7510-33 P/O# 703416 AND ATTACH CLIP BS 400 FWD SIDE P/N 143A7502U155 PO# 703366 IAW SRM 51-40-02 AND DWG 143A7505 REV B 89004U 25AUG18

Part: WEB — CORRODED (FSD THRESHOLD) · airframe 63,225 hrs · 37,171 cycles

***CORROSION*** FSD MOP SILL WEB LOWER SURFACE FWD OF STA 312 / REMOVED CORROSION ON FSD MOP SILL WEB LOWER SURFACE FWD OF BS312 MAT. LOSS IS MORE THAN 25% THEREFORE FOUND TO BE OUT OF LIMITS PER REF BS737 SRM 53-10-15-1A-2 ALLOWABLE DAMAGE 2. 4678C 25AUG18 W=2'; L=1'; D=.030' ORIGINAL THICKNESS IS .063' 92462U 25AUG18 LEAD 98 25AUG18 INSP 24 25AUG18. REMOVED AND REPLACED FSD MOPSILL WEB IAW SRM 51-40-02-0G-0; FSD MOPSILL WEB WAS REPLACED ON CARD #T827305

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

R1 DOOR MOP SILL WEB LOWER SURFACE CORRODED AT BS 300. R&R WEB IAW SRM.

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 63,225 hrs · 37,171 cycles

***CORROSION*** AFT CARGO BAY FLOOR PANEL SPLICE AT B.S. 767. / REPLACED AFT CARGO BAY FLOOR PANEL SPLICE AT BS 767 IAW DWG #146A9401. SPLICE WILL BE REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARA 9.C PO# 701616/12

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 63,225 hrs · 37,171 cycles

***CORROSION*** AFT CARGO BAY FLOOR PANEL SPLICE AT B.S. 727D+10. / AFT CARGO BAY FLOOR PANEL SPLICE AT BS 727D+10 WILL BE REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0. REPLACED SPLICE PO # 697620/8 IAW DWG 146A9401 AND DWG 146A7500

Part: ANGLE — CRACKED (LT MLG WW) · airframe 63,225 hrs · 37,171 cycles

REAR SPAR VAPOR BARRIER ATTACHED ANGLE CRACKED AT BS 663, LBL 8. REPAIRED ANGLE PER ER AND EA.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 63,225 hrs · 37,171 cycles

***CORROSION*** ON AFT CARGO BAY PANEL; 140CF; ON UPPER SURFACE ALONG OUTBOARD EDGE. / CORROSION ON AFT CARGO BAY FLOOR PANEL 140CF UPPER SURFACE EXCEEDS SRM 53-00-53-1A-1 ALLOWABLE LIMITS PANEL 140CF IS REPAIRABLE BY REPLACEMENT. CARGO PANEL 140CF TO BE REPLACED ON CARD T827238

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 63,225 hrs · 37,171 cycles

R2 DOOR SLIDE OUT OF POSITION. R&R SLIDE IAW MT.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,225 hrs · 37,171 cycles

AFT CABIN FLOOR PANEL 241ABF LOWER SKIN OF AFT O/B CORNER IS DISBONDED. / REPAIRED DAMAGE TO AFT O/B CORNER ON FLOOR PANEL 241ABF IAW SRM 53-00-50-2R-4. 56749U 19AUG18

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO TRACK TIE DOWN CORRODED AT BS 849, RBL 13.8. R&R TRACK IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD SERVICE DOOR STUB FRAME CRACKED AT BS 294, STR 17R. R&R STUB FRAME IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO TRACK TIE DOWN CORRODED AT BS 787, LBL 18. R&R TRACK IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 TO BS 867, RBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 24. R&R SUPPORT PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 24. R&R SUPPORT PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN LBL 60 TO RBL 60. R&R UPPER CHORD PER SRM & EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO FLOOR SUPPORT TRACK CORRODED BETWEEN BS 771 TO BS 773, LBL 12.5. REPAIRED TRACK IAW SRM AND EA

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO FLOOR INTERCOSTAL WEB CORRODED BETWEEN BS 773 TO BS 777, RBL 7. R&R WEB IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 47. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SPLICE — CORRODED (AFT CARGO) · airframe 63,225 hrs · 37,171 cycles

***CORROSION*** AFT CARGO FLOOR PANEL SPLICE; BS 727D + 10 (ATTACHED TO PANEL 140AF) RBL 18 TO LBL 18 / AFT CARGO FLOOR PANEL SPLICE AT BS 727D+10 RBL 18 TO LBL 18 REPLACED ON CARD DEFECT NO T827286

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD CARGO BAY AFT BULKHEAD RT PANEL LOWER SUPPORT, AROUND STIFFENER HOLES. R&R SUPPORT PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO RT FLOOR INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, RBL 20. R&R INTERCOSTAL PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

R1 DOOR SURROUND STRUCTURE LOWER SILL, INBOARD ANGLE CORRODED BETWEEN BS 310 TO BS 340, RBL 61. R&R ANGLE IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD CARGO BAY SUB WEB THRESHOLD CORRODED BETWEEN BS 440 TO BS 492.4. R&R THRESHOLD IAW DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 21. R&R SUPPORT PER SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO DOORWAY THRESHOLD SUB WEB CORRODED BETWEEN BS 795 TO BS 847, BETWEEN RBL 21 TO RBL 28. R&R WEB IAW DWG & SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO RT FLOOR INTERCOSTAL CORRODED BETWEEN BS 787 TO BS 795, RBL 20. R&R INTERCOSTAL IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 21. R&R SUPPORT PER DWG AND SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO DOORWAY LOWER THRESHOLD INBOARD STRAP CORRODED BETWEEN BS 767 TO BS 857, RBL 20. R&R STRAP IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 12. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO FLOOR SUPPORT STRINGER CORRODED BETWEEN BS 771 TO BS 773, RBL 7.5. REPAIR STRINGER PER EA.

Part: FITTING — CORRODED (MAIN CABIN) · airframe 63,225 hrs · 37,171 cycles

***CORROSION*** NOTED ON FLOOR STRUCTURE HARDPOINT FITTING (BS 312 / LBL 54 / WL 208). / REMOVED AND INSTALLED NEW FLOOR STRUCTURE HARDPOINT FITTING ON (BS 312/LBL 54/ WL208) PN# 141A5220-02 IAW SRM 51-40-02-0G-0 AND AIPC 53-42-00-29

Part: SPLICE — CORRODED (AFT CARGO) · airframe 63,225 hrs · 37,171 cycles

***CORROSION*** AFT CARGO FLOOR PANEL SPLICE; BS 887; RBL 18 TO LBL 18 / REMOVED AND REPLACED ACB FLOOR PANEL SPLICE; BS 887 RBL 18 TO LBL 18 TEE ASSY IAW AMM 25-52-10-000-801; AMM 25-52-10-400-801; AND DWG 146A7500 93140U 13SEP18

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO FLOOR INTERCOSTAL WEB CORRODED BETWEEN BS 788 TO BS 790, RBL 7. R&R WEB IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO DOORWAY LOWER THRESHOLD INBOARD INTERCOSTAL CORRODED BETWEEN BS 780 TO BS 835, RBL 20. R&R INTERCOSTAL PER SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD SERVICE DOOR MOP SILL CORRODED AT RBL 60. R&R MOPSILL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT ENTRY DOOR MOP SILL CORRODED BETWEEN BS 947 TO BS 995. R&R MOPSILL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD ENTRY DOOR MOP SILL CORRODED AT LBL 60. R&R MOPSILL IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO FLOOR SUPPORT STRINGER CORRODED BETWEEN BS 771 TO BS 773, RBL 2.5. REPAIRED STRINGER PER EA.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 63,225 hrs · 37,171 cycles

LT MAIN WHEEL WELL VERTICAL PRESSURE BULKHEAD WEB CRACKED AT BS 663, BETWEEN LBL 32 TO LBL 45. REPAIRED WEB PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO FLOOR SUPPORT STRINGER CORRODED BETWEEN BS 771 TO BS 773, LBL 7.5. REPAIRED STRINGER PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FLOORBEAM UPPER FLANGE CORRODED AT BS 328, BETWEEN RBL 32 TO RBL 57. REPAIRED FLANGE PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED BETWEEN LBL 24 TO RBL 24. R&R SUPPORT PER SRM AND DWG.

Part: PANEL SUPPORT — CORRODED (FWD CARGO BAY) · airframe 63,225 hrs · 37,171 cycles

***CORROSION*** ON FORWARD CARGO BAY AFT BULKHEAD LEFT PANEL LOWER SUPPORT; AROUND FASTENER HOLES. / REMOVED AND REPLACED FCB AFT BULKHEAD L/H PANEL LOWER SUPPORT PER B737 SRM 51-40-02-0G-0 AND DRAWING # 143A9481.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO SIDEWALL TO AFT BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, BETWEEN RBL 21 TO RBL 26. R&R SUPPORT ASSEMBLY IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO RTFLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 767 TO BS 795, RBL 21. R&R SHIELD PER SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT SERVICE DOOR MOP SILL CORRODED BETWEEN BS 947 TO BS 990. R&R MOPSILL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 494 TO BS 500A, RBL 24. R&R SUPPORT PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, RBL 1. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SPLICE — CORRODED (AFT CARGO) · airframe 63,225 hrs · 37,171 cycles

***CORROSION*** AFT CARGO FLOOR PANEL SPLICE; BS 774 (ATTACHED TO PANEL 140BF) RBL 18 TO LBL 18 / AFT CARGO FLOOR PANEL SPLICE AT BS 774 RBL 18 TO LBL 18 REPLACED ON CARD DEFECT NO T827287

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO RH FLOOR INTERCOSTAL CORRODED BETWEEN BS 787 TO BS 795, RBL 20. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

AFT CARGO FLOOR SUPPORT STRINGER CORRODED BETWEEN BS 771 TO BS 773, LBL 2.5. REPAIRED STRINGER PER EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 TO BS 440 RBL 24. R&R SUPPORT PER SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FLOORBEAM UPPER FLANGE CRACKED AT BS 328, RBL 20. REPAIRED FLANGE PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 47. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FASTENER — CRACKED (RT WING) · airframe 63,225 hrs · 37,171 cycles

RT WING TRAILING EDGE SUPPORT ANGLE FASTENERS CRACKED. R&R FASTENERS IAW SRM AND DWG.

Part: PLATE — CRACKED (RT WING) · airframe 63,225 hrs · 37,171 cycles

RT WING LOWER TRAILING EDGE WIGGLE PLATE AT ORSS 261 CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: SUPPORT BEAM — CRACKED (RT WING) · airframe 63,225 hrs · 37,171 cycles

RT WING T/E LOWER PANEL SUPPORT BEAM FOR PANEL 661AB IS CRACKED ON I/B END / REMOVED AND REPLACED RT WING T/W LOWER SUPPORT PANEL BEA IAW SRM 51-40-02 AND AIPC 57-50-00-18. FOR PANEL 661AB 7381C 21AUG18

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 63,225 hrs · 37,171 cycles

LT WING TRAILING EDGE SUPPORT ANGLE ATTACHED TO DEFLECTION CONTROL RIB CRACKED. R&R ANGLE PER SRM AND DWG.

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FWD FLOOR PANEL 221EF UPPER SKIN HAS SMALL AREA OF PULLED STRANDS AT FWD R/H CORNER. (MARKED) / FWD FLOOR PANEL 221EF UPPER SKIN WITH SMALL AREA OF PULLED STRANDS AT FWD R/H CORNER. (MARKED) WAS REPAIRED IAW SRM 53-00-50-2R-1 57545U 8-17-18

Part: SEAL — CRACKED (LT WING) · airframe 63,225 hrs · 37,171 cycles

LT WING T/E BULB SEAL RETAINER ABOVE #1 PYLON AFT TIP IS CRACKED / REMOVED AND REPLACED LEFT WING TRAILING EDGE SEAL RETAINER IAW SRM 51-40-02-0G-0 STEP 4 AND SRM 51-40-02-0G-0.

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 63,225 hrs · 37,171 cycles

FWD FLOOR PANEL 221FF UPPER SKIN HAS SMALL AREA OF PULLED STRANDS AT FWD SECTION. (MARKED) / REPAIRED DAMAGE TO UPPER SKIN ON FWD FLOOR PANEL 221FF IAW SRM 53-00-50-2R-1. 56749U 19AUG18

Part: FORMER — CRACKED (RT WING) · airframe 63,225 hrs · 37,171 cycles

RT WING FIXED LEADING EDGE INBOARD FAIRING SUPPORT FORMER CRACKED ON UPPER END. R&R FORMER IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 63,225 hrs · 37,171 cycles

LOWER COMPOSITE BULKHEAD CRACKED AT BS 663, LBL 12. REPAIRED BULKHEAD IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 63,225 hrs · 37,171 cycles

LOWER COMPOSITE BULKHEAD CRACKED AT BS 663, LBL 48. REPAIRED BULKHEAD IAW SRM.

Part: BULKHEAD — CRACKED (RT MLG) · airframe 63,225 hrs · 37,171 cycles

LOWER COMPOSITE BULKHEAD CRACKED AT BS 663, RBL 12. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — INFLT SEPARATION (EXIT SIGN) · airframe 63,225 hrs · 37,171 cycles

L1 DOORWAY LOWER FORWARD EMERGENCY EXIT SIGN BULB INOP. R&R SIGN PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,225 hrs · 37,171 cycles

LT LOWER FORWARD OVERWING EMERGENCY EXIT SIGN BULB INOP. R&R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,225 hrs · 37,171 cycles

L1 DOORWAY UPPER EDGE EMERGENCY EXIT LIGHT BULB INOP. R&R BULB IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,075 hrs · 36,450 cycles

EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST AT M01674. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,075 hrs · 36,450 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,075 hrs · 36,450 cycles

EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST AT M10746. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,075 hrs · 36,450 cycles

EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST AT M01675. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,075 hrs · 36,450 cycles

EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST AT M10744. R&R BATTERY PACK PER AMM.

Part: FUSE — BLOWN (CABIN) · airframe 60,639 hrs · 35,562 cycles

RT AFT ENTRY EMERGENCY LIGHT INOP. R&R FUSE PER AMM.

Part: LENS — MISSING (CABIN) · airframe 60,382 hrs · 35,409 cycles

L2 DOOR "EXIT" LIGHT LENS COVER MISSING. INSTALLED LENS PER AMM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 60,187 hrs · 35,271 cycles

LT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT STA 95.96. R&R RIB PER SRM & AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 60,187 hrs · 35,271 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT STA 105.26. R&R LEADING EDGE ASSEMBLY PER AMM & EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 60,187 hrs · 35,271 cycles

LT HORIZONTAL STABILIZER LEADING EDGE CRACKED AT STA 105.26. R&R RIB ASSEMBLY PER DWG & SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 60,187 hrs · 35,271 cycles

R/H HORIZ. L/E RIB @ STA. 95.96 IS CRACKED MARKED. / R/R R/H LEADING EDGE OF STAB. AS PER AMM 27-41-21 AND EA 1-755-3847 PN OFF/ON 186A1001-16 SN OFF 1771662 SN ON WN0038 A1060106

Part: HANDLE — BROKEN (EMERGENCY EXIT) · airframe 60,064 hrs · 35,189 cycles

RIGHT OVERWING EMERGENCY EXIT HATCH LINER PULL HANDLE BROKEN. R & R THE HANDLE IAW AMM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 58,832 hrs · 34,412 cycles

R1 DOOR EMERGENCY EXIT SIGN COVER BROKEN. R & R THE COVER IAW MM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 56,891 hrs · 33,275 cycles

WEB FLOOR SUPPORT CRACKED BETWEEN BS. 312 TO BS. 328, LBL 45. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (BS 663) · airframe 56,891 hrs · 33,275 cycles

FORWARD BULKHEAD CRACKED AT BS 663.75, BETWEEN RBL 6.15 TO RBL 15.54. REPAIRED THE BULKHEAD IAW EA.

Part: STRAP — MISSING (FLASHLIGHT ASSY) · airframe 56,891 hrs · 33,275 cycles

AFT GALLEY AREA EMERGENCY FLASHLIGHT WINDSCREEN STRAP MISSING. INSTALLED A NEW STRAP IAW CMM.

Part: SKIN — CRACKED (LT WING) · airframe 56,891 hrs · 33,275 cycles

LEFT WING NR 1 FLAP TRACK SKIN CRACKED ON EDGE FORWARD POSITION. REPAIRED SKIN IAW EA.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 56,891 hrs · 33,275 cycles

FORWARD GALLEY LAVATORY A WALL HAS A BROKEN EMERGENCY EXIT LIGHT LENS. R & R THE LENS IAW AMM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 56,891 hrs · 33,275 cycles

LEFT WING NR 1 SLAT SKIN CRACKED ON LOWER SURFACE, APPROXIMATELY WS 667.50. REPAIRED THE SLAT SKIN IAW SRM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 56,891 hrs · 33,275 cycles

AFT CABIN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING DELAMINATED. R & R LIGHT IAW AMM AND DWG.

Part: BULKHEAD WEB — CRACKED (RT MLG WW) · airframe 56,891 hrs · 33,275 cycles

RIGHT MAIN WHEEL WELL SPAR VERTICAL PRESSURE BULKHEAD WEB CRACKED AT BS 663.75, BETWEEN RBL 25 TO RBL 42.5 REPAIRED BULKHEAD WEB IAW SRM.

Part: FRAME — CRACKED (BS 727) · airframe 56,891 hrs · 33,275 cycles

AFT CARGO COMPARTMENT FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED WEB IAW EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 56,726 hrs · 33,176 cycles

L1 DOOR EMERGENCY EVACUATION SLIDE FOUND OUT OF POSITION. REPOSITIONED SLIDE PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,829 hrs · 32,638 cycles

R2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 55,808 hrs · 32,627 cycles

R1 DOOR LOWER EMER EXIT LIGHT COVER MISSING. R & R LIGHT ASSEMBLY IAW SIP.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 53,713 hrs · 31,409 cycles

LEFT HORIZONTAL STABILIZER RIB STATION 92.70 VERTICAL STIFFENER, AT SECOND FROM FWD SPAR CRACKED. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT WING) · airframe 53,713 hrs · 31,409 cycles

LEFT WING VERTICAL RIB COMMON TO UPPER. R & R RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 53,713 hrs · 31,409 cycles

LEFT HORIZONTAL STABILIZER RIB STATION 92.70 LOWER CHORD, AT SECOND FROM FWD SPAR VERTICAL STIFFENER CRACKED ON INBD EDGE. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 53,713 hrs · 31,409 cycles

LEFT HORIZONTAL STABILIZER RIB STATION 92.70, LOWER CHORD AT FWD VERTICAL STIFFENER, CRACKED ON INBD EDGE. REPAIRED RIB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,713 hrs · 31,409 cycles

LONGITUDINAL FLOORBEAM FLANGE, CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,713 hrs · 31,409 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME E-F POST, 3RD FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED FRAME IAW ACO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,713 hrs · 31,409 cycles

LONGITUDINAL FLOORBEAM FLANGE, CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,713 hrs · 31,409 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME E-F POST, 2ND FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,713 hrs · 31,409 cycles

RIGHT FLIGHT DECK NR 1 WINDOW FRAME, CRACKED IN UPPER OTBD CORNER. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,713 hrs · 31,409 cycles

LEFT NR 3 FLIGHT DECK WINDOW FRAME E-F POST, 2ND FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED FRAME IAW ACO.

Part: LIGHT — BROKEN (CABIN) · airframe 53,320 hrs · 31,186 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 52,650 hrs · 30,820 cycles

R1 DOOR EMER EVAC SLIDE COVER AFT GIRT BAR HOOK FASTENER LOOSE. R & R HOOK ASSEMBLY IAW SRM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 51,962 hrs · 30,422 cycles

RIGHT OVERWING EXIT SIGN LENS BROKEN. R & R LENS IAW SIP.

Part: HOOK AND LOOP — WORN (EMERGENCY EXIT) · airframe 51,658 hrs · 30,250 cycles

EMERGENCY EXIT COVER VELCRO WORN. R & R COVER ASSEMBLY IAW SIP.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 51,476 hrs · 30,134 cycles

KEEL BEAM PANEL 192E, FWD LT MOUNT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: STRINGER — CRACKED (LT WING) · airframe 50,661 hrs · 29,650 cycles

STRINGER CRACKED JUST INBD OF THE LT PYLON IN THE LE. R & R STRINGER IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,661 hrs · 29,650 cycles

LEFT WING NR 3 SLAT LOWER SKIN CRACKED. R & R NR 3 SLAT IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 49,219 hrs · 28,824 cycles

LEFT WING OTBD AFT FLAP INBD END UPPER SIDE DELAMINATED. R & R AFT FLAP IAW AMM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 49,219 hrs · 28,824 cycles

LEFT WING UPPER FIXED TE AFT OF PYLON AFT CURVED BULB SEAL SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: ACTUATOR — FAULTY (NLG UPLOCK) · airframe 49,190 hrs · 28,805 cycles

DIVERSION, RED & GREEN NOSE GEAR LIGHT ILLUMINATED WITH GEAR HANDLE IN UP POSITION. R & R NLG LOCK ACTUATOR IAW MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 48,248 hrs · 28,269 cycles

L1 WINDOW ARCED. R & R WINDOW IAW AMM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 48,038 hrs · 28,138 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 129.5, 9 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 45,806 hrs · 26,783 cycles

L2 DOOR EMERGENCY EVAC SLIDE BOTTLE PRESSURE LOW. R & R SLIDE IAW MT.

Part: LIGHT — BROKEN (R1 DOOR) · airframe 45,591 hrs · 26,655 cycles

FWD SERVICE DOOR EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT ASSY IAW M/M.

Part: COVER — BROKEN (LT AILERON TAB) · airframe 44,680 hrs · 26,116 cycles

LEFT AILERON TAB INBOARD HINGE COVER BROKEN. REMOVED AND REPLACED LEFT I/B AILERON TAB COVER PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 44,680 hrs · 26,116 cycles

ALL BATTERIES FAILED EMERGENCY LIGHT CAPACITY TEST. REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERIES LOCATED AT M1668, M1669, M1670, M1672, M1673, M1674 AND M1675 PER AMM AND SSM.

Part: LIGHT — LOOSE (CABIN) · airframe 44,680 hrs · 26,116 cycles

PASSENGER COMPARTMENT AISLE OVERHEAD CEILING EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 44,680 hrs · 26,116 cycles

LEFT WING NR 2 SLAT SKIN IS CRACKED AT THREE ACTUATOR ATTACH FITTING FASTENERS. REPLACED NR 2 SLAT PER M/M 27-81-21-400-801 AND MT.

Part: BEARING — LOOSE (TE FLAP) · airframe 44,680 hrs · 26,116 cycles

LEFT WING OUTBOARD AFT FLAP OUTBOARD ATTACH BEARING IS LOOSE. REMOVED AND REPLACED FLAP TRACK PER M/M.

Part: BEARING — LOOSE (TE FLAP) · airframe 44,680 hrs · 26,116 cycles

LEFT WING OUTBOARD AFT FLAP INBOARD ATTACH BEARING IS LOOSE. REMOVED AND REPLACED LEFT WING OUTBOARD AFT FLAP INBOARD TRACK PER MM.

Part: BUSHING — LOOSE (LT AILERON TAB) · airframe 44,680 hrs · 26,116 cycles

LEFT WING AILERON TAB IS LOOSE AT INBOARD HINGE. REMOVED AND REPLACED LEFT WING AILERON TAB INBOARD HINGE BUSHINGS, RIG CHECK GOOD REF M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,681 hrs · 25,493 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED LIGHT IAW WDM AND AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 43,681 hrs · 25,493 cycles

AFT LAV FORWARD SIDE EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,681 hrs · 25,493 cycles

STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,681 hrs · 25,493 cycles

FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,681 hrs · 25,493 cycles

LEFT PASSENGER COMPARTMENT FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,681 hrs · 25,493 cycles

FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,681 hrs · 25,493 cycles

FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,681 hrs · 25,493 cycles

FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,681 hrs · 25,493 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,681 hrs · 25,493 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,681 hrs · 25,493 cycles

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

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,681 hrs · 25,493 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,681 hrs · 25,493 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 43,443 hrs · 25,329 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 43,015 hrs · 25,049 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — CRACKED (LT HORIZ STAB) · airframe 42,690 hrs · 24,867 cycles

LEFT HORIZONTAL STABILIZER FWD LOWER SLIDE CRACKED. REMOVED AND REPLACED STABILIZER PER AMM.

Part: SLIDE — CRACKED (RT HORIZ STAB) · airframe 42,690 hrs · 24,867 cycles

RIGHT HORIZONTAL STABILIZER FWD LOWER SLIDE CRACKED. REMOVED AND REPLACED PER AMM.

Part: SENSOR — FAULTY (TE FLAP) · airframe 40,112 hrs · 23,350 cycles

DIVERSION -- ON TAKEOFF FLAP RETRACTION WENT TO ZERO THEN LEFT INDICATOR SNAPPED TO 1/2 ASYMMETRICAL USED LED'S ON LANDING PSEU LIGHT ILLUMINATED UPON LANDING. REMOVED AND REPLACED NR 3 & NR 6 SKEN SENSORS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,980 hrs · 22,108 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 5. RELAMPED PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,884 hrs · 22,061 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,884 hrs · 22,061 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: GASPER FAN — FAULTY (CARGO BAY) · airframe 37,689 hrs · 21,929 cycles

FLIGHT ATTENDANTS REPORTED UNUSUAL ODOR COMING FROM CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,723 hrs · 21,380 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOOR DECK ANGLE CORRODED AT BS 270, BETWEEN LBL 10 TO RBL 10. REPAIRED ANGLE PER EA.

Part: STRAP — FRAYED (EMERGENCY EXIT) · airframe 36,707 hrs · 21,367 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT EMERGENCY EXIT HATCH SCAPE STRAP FRAYED. REMOVED AND REPLACED STRAP PER MM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,707 hrs · 21,367 cycles

DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 540, LBL 14.5. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,707 hrs · 21,367 cycles

DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 540, LBL 7. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,707 hrs · 21,367 cycles

DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 540, LBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,707 hrs · 21,367 cycles

DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 540, RBL 14.5. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,193 hrs · 20,484 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,193 hrs · 20,484 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,129 hrs · 20,448 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 34,508 hrs · 20,096 cycles

R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: COVER — CRACKED (CABIN) · airframe 34,455 hrs · 20,062 cycles

DURING SCHEDULED CV CHECK, FOUND FWD EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,711 hrs · 18,360 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 13. RELAMPED LIGHT PER MM.

Part: GLOWSTRIP — DETERIORATED (CABIN) · airframe 30,263 hrs · 17,482 cycles

DURING SCHEDULED 8Y CHECK, FOUND CABIN FLOOR PHOTOLUMINESCENT LIGHT STRIP IN POOR CONDITION. REMOVED AND REPLACED STRIP PER SWA DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,254 hrs · 17,475 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 38 TO RBL 40. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,254 hrs · 17,475 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED BEAM PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,711 hrs · 17,149 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHT AT SEAT 3D INOP. RELAMPED LIGHT PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 28,955 hrs · 16,665 cycles

DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 27,223 hrs · 15,616 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,443 hrs · 15,121 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 21,288 hrs · 12,154 cycles

DURING SCHEDULED HC2 CHECK, ALL EMERGENCY EXIT LIGHT BATTERIES FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,396 hrs · 11,616 cycles

DURING SCHEDULED MV2 CHECK, FOUND CABIN EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 1 ABC. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 20,166 hrs · 11,495 cycles

DURING SCHEDULED RON CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 18,481 hrs · 10,512 cycles

DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 775, LBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 18,481 hrs · 10,512 cycles

DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 775, LBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: WEDGE — DELAMINATED (LT WING TE FLAPS) · airframe 16,613 hrs · 9,458 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD MAIN FLAP OUTBOARD T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 14,325 hrs · 8,152 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 13,874 hrs · 7,896 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS AT ROW 2 DEF, ROW 14 DEF, ROW 16 ABC, DAMAGED. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 13,874 hrs · 7,896 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: COVER — MISSING (ROW 7) · airframe 12,616 hrs · 7,167 cycles

EEPLS TRACK COVER MISSING AT ROW 7. INSTALLED COVER PER MM.

Part: BATTERY PACK — DISCHARGED (CARGO BAY) · airframe 10,393 hrs · 5,924 cycles

DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (FWD ENTRY DOOR) · airframe 10,354 hrs · 5,892 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 6,080 hrs · 3,590 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER IN JETWAY. REINSTALLED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,589 hrs · 2,723 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP IN AFT CABIN AND SEVERAL COVERS CRACKED. RELAMPED EEPLS AND REMOVED AND REPLACED COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 1,879 hrs · 1,124 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 7. RELAMPED EEPLS PER MM.