N557WN

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,789 hrs · 34,214 cycles

EMERGENCY LIGHT OUT 11FED / [01] RELAMPED EMERGENCY LT AT ROW 11DEF REF AMM 33-51-03

Part: PANEL — ELONGATED · airframe 68,363 hrs · 33,386 cycles

PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES AND OVERSIZED COUNTERSINKS. / [01] REPLACED PANEL 193B PER SRM 51-40-02

Part: BUSTLE — LOOSE (L1 DOOR) · airframe 67,363 hrs · 32,824 cycles

FWD ENTRY DOOR SLIDE BUSTLE NOT SECURE / [01] SECURED PER MT 725-61-06-FE

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

AFT CARGO BAY FLOOR PNL 140DF HAS CORROSION ALONG AFT EDGE BS 947 RBL 22 - LBL 22 WL 157 ; / [01] FABRICATED NEW ACB FLOOR PNL 140DF FROM 2024T3#0.071X48SH-C; LOT# 1461004-1 IAW BOING DWG 435A2610 AND BOEING DWG 435A2600; [02] PRIOR TO MAINTENANCE; BLENDED DAMAGE IN AREA OF L=12'X W=4' X D=.012'. FOUND TO BE OUT OF LIMITS WITH REMAINING THICKNESS OF .059' OF ORIGINAL THICKNESS OF .071' IAW SRM 53-00-53-1A-1; [03] VERIFIED FLOOR PANEL DAMAGE OUT OF LIMITS. VERIFIED FABRICATION OF NEW FLOOR PANEL PER BOEING DWG 435A2610 AND BOEING DWG 435A2600

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACK ON FRAME BS 500C STR 8L AIR CONDITIONING RAIL BRACKET OUTBD ATTACH HOLE. CRACK EXTENDS UP .300' AND DOWN .300' FROM INBD EDGE OF HOLE. NOT IN FRAME RADIUS. ; / [01] REPAIRED ON CARD TTG8Q006QK4S; [02] VERIFIED BS500C STR8L REWORK PERFORMED ON CC# TTG8Q006QK4S.

Part: SUPPORT ANGLE — CRACKED (R2 DOOR) · airframe 66,485 hrs · 32,340 cycles

AFT SERVICE DOOR LOWER HINGE PANEL # 844DZ HAS CRACKED FWD SUPPORT ANGLE CRACKED. ; / [01] REMOVED AND REPLACED AFT SERVICE DOOR LOWER HINGE PANEL #844DZ FWD SUPPORT ANGLE IAW SRM 51-40-02; [02] VERIFIED REPLACEMENT OF THE AFT SERVICE DOOR LOWER HINGE PANEL SUPPORT BRACKET PER SRM 51-40-02

Part: SKIN — CRACKED (R/H HORIZ. STAB.) · airframe 66,485 hrs · 32,340 cycles

WHILE ACCOMPLISHING HFEC INSPECTION ON CCN: 5510-I-15029-NG #2; FOUND 1 INCH CRACK ON R/H HORIZONTAL STABILIZER LOWER SKIN AT RIB STATION 193.90; 18 INCHES AFT OF THE THE FWD EDGE. ; / [01] REQUEST HFEC FOR CRACK VERIFICATION ON R/H HORIZONTAL STAB ON LOWER SKIN AT RIB STA. 193.9 18 INCHES AFT OF LEADING EDGE; [02] FOUND CRACK ON R/H HORZ. STAB RIB STA. 193.9 18 INCHES FROM LEADING EDGE TO BE OUT OF LIMITS PER SRM 55-10-01-1A-2 STEP 4-A; [03] VERIFIED EXISTING CRACK IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; MARKED ENDS OF CRACK. EQUIP ID#: IS000450 S/N: N500D000M120071; [04] CUT OUT DAMAGE ON R/H HORZ. STAB AT RIB STA. 193.90 18 INCHES FROM LEADING EDGE IN A LENGTH 1.8 'X WIDTH 1' PER SRM 55-10-01-2R-11 STEP 4-2 FIG 204; [05] VERIFIED CRACK DAMAGE TRIM OUT PER SRM 55-10-01-2R-11 STEP 4-2 FIG 204; [06] HFEC INSPECTED CUT OUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. <BR><BR>EQUIP ID#: IS000450 S/N: N500D000M120071; [07] FABRICATED; LOCATED AND DRILLED REPAIR PARTS; DOUBLER MA[11] VERIFIED DOUBLER AND FILLER FABRICATION PER SRM 55-10-01-2R-11 FIG 204 SHT 2. VERIFIED CHEMICAL TREATMENT AND PRIMER- OK TO INSTALL SKIN REPAIR.; [12] REPAIRED DAMAGED AREA AT R/H RIB STA 193.90; 18 INCHES AFT OF FWD EDGE IAW SRM 53-10-01-2R-11; [20] R/H HORIZONTAL STAB LOWER SKIN REPAIR IS COMPLETE PER SRM 55-10-01-11; STEP 4) R. CATEGORY B REPAIR REQUIRES REINSPECTION. WORKSCOPE COMPLETE

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

FWD CARGO BAY BAFFLE CRACKED AT FASTENER HOLE BS 500B - BS 500C RBL 23 WL 156 ; / [01] EVALUATED CRACK AT FWD CARGO BAFFLE BS 500B-500C. BAFFLE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [02] REMOVED FWD CARGO BAY BAFFLE CRACKED BS 500B-500C RBL 23 WL 156 IAW SRM 51-40-02.; [03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.; [04] LOCATED AND DRILLED FWD CARGO BAY NEW BAFFLE BS 500B - 500C RBL 23 WL 156 IAW SRM 51-40-05.; [05] VERIFIED CORRECTIVE ACTION ITEM 4.; [06] OK TO INSTALL; [07] VERIFIED IT IS OK TO INSTALL NEW FCB BAFFLE AT BS 500B - BS 500C RBL 23 WL 156.; [08] INSTALLED FWD CARGO BAY NEW BAFFLE BS 500B -500C RBL 23 WL 156 P/N 143A7510-12 PO#827526/4 IAW SRM 51-40-02 AND DWG143A7505 REV:D.; [09] VERIFIED INSTALLATION OF BS500B- 500C RBL23 WL156 PER SRM 51-40-02 AND DWG143A7505 REV:D.; [10] WORKSCOPE COMPLETE

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 500C LBL 23 WL 154 FWD SIDE OF FRAME ; / [01] REMOVED FWD CARGO BAY BAFFLE ATTACH CLIP BS 500C LBL 23 WL 154 FWD SIDE OF FRAME P/N 143A7502-13 IAW SRM 51-40-02; [02] LOCATED AND DRILLED BAFFLE ATTACH CLIP BS 500C LBL 23 IAW SRM 51-40-05; DWG# 143A7505. REQUEST OK TO INSTALL.; [03] VERIFIED CORRECTIVE ACTION 2. OK TO INSTALL; [04] INSTALLED BAFFLE ATTACH CLIP BS 500C LBL 23 FWD SIDE OF FRAME IAW SRM 51-40-02; DWG# 143A7505.; [05] VERIFIED CORRECTIVE ACTION 4; [06] VERIFIED JOB COMPLETE

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 400 LBL 23 WL 154 AFT SIDE OF FRAME ; / [01] REMOVED AT FWD CARGO BAY BAFFLE ATTACH CLIP B/S 400 LBL 23 WL 154 AFT SIDE OF FRAME P/N 143A7502-5 IAW SRM 51-40-02; [02] LOCATED AND DRILLED BAFFLE ATTACH CLIP BS 400 LBL 23 IAW SRM 51-40-05; DWG# 143A7505. REQUEST OK TO INSTALL.; [03] VERIFIED CORRECTIVE ACTION 2; OK TO INSTALL; [04] INSTALLED BAFFLE ATTACH CLIP BS 400 LBL 23 IAW SRM 51-40-02; DWG# 143A7505.; [05] VERIFIED CORRECTIVE ACTION 4; [06] VERIFIED JOB COMPLETE

Part: WEB — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

FWD CARGO WEB CRACKED AT FASTENER HOLE BS 500 - BS 500A RBL 22 WL 154 ; / [01] REMOED WEB AT FWD CARGO BS 500 - BS 500A RBL 22 WL 154 IAW SRM 51-40-02-0G-0; [02] WEB FORMING AND HEAT TREATMENT ACCOMPLISHED ON PO#839725/1.; [03] LOCATED AND DRILLED REPLACEMENT WEB; APPLIED CHEMICAL CONV. COATING PER DWG# 143A0080 REV:-; SRM 51-40-05-0G-0 AND SOPM 20-43-03. OK TO PRIME.; [04] VERIFIED CORRECTIVE ACTION 3.; [05] APPLIED PRIMER TO FWD CARGO WEB BS 500-500A RBL 22 WL 154 PER AMM 51-21-72-370-804. OK TO INSTALL WEB ASSY.; [06] VERIFIED STEP 5.; [07] INSTALLED FCB WEB BS 500-500A; RBL 22 WL 154 PER SRM 51-40-02; DWG#143A0080.; [08] VERIFIED INSTALLED FCB WEB BS 500-500A; RBL 22 WL 154 PER SRM 51-40-02; DWG#143A0080.; [09] WORKSCOPE COMPLETE

Part: NONE — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 500C LBL 23 WL 154 AFT SIDE OF FRAME ; / [01] REMOVED FWD CARGO BAY BAFFLE ATTACH CLIP BS 500C LBL 23 WL 154 AFT SIDE OF FRAME P/N 143A7502-5 IAW SRM 51-40-02; [02] LOCATED AND DRILLED BAFFLE ATTACH CLIP BS 500C LBL 23 IAW SRM 51-40-05; DWG# 143A7505. REQUEST OK TO INSTALL.; [03] VERIFIED CORRECTIVE ACTION 2. OK TO INSTALL; [04] INSTALLED BAFFLE ATTACH CLIP BS 500C LBL 23 AFT SIDE OF FRAME IAW SRM 51-40-02; DWG# 143A7505.; [05] VERIFIED CORRECTIVE ACTION 4; [06] VERIFIED JOB COMPLETE

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 440 LBL 23 WL 154 AFT SIDE OF FRAME ; / [01] REMOVED FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 440 LBL 23 WL 154 AFT SIDE OF FRAME P/N 143A7502-5 IAW SRM 51-40-02; [02] LOCATED AND DRILLED BAFFLE ATTACH CLIP BS 440 LBL 23 IAW SRM 51-40-05; DWG# 143A7505. REQUEST OK TO INSTALL.; [03] VERIFIED CORRECTIVE ACTION 2. OK TO INSTALL; [04] INSTALLED BAFFLE ATTACH CLIP BS 440 LBL 23 IAW SRM 51-40-02; DWG# 143A7505.; [05] VERIFIED CORRECTIVE ACTION 4; [06] VERIFIED JOB COMPLETE

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 500B LBL23 WL 154 FWD SIDE OF FRAME ; / [01] REMOVED AT FWD CARGO BAY BAFFLE ATTACH CLIP B/S 500B LBL 23 WL 154 FWD SIDE OF FRAME P/N 143A7502-13 IAW SRM 51-40-02; [02] LOCATED AND DRILLED BAFFLE ATTACH CLIP BS 500B LBL 23 IAW SRM 51-40-05; DWG# 143A7505. REQUEST OK TO INSTALL.; [03] VERIFIED CORRECTIVE ACTION 2. OK TO INSTALL; [04] INSTALLED BAFFLE ATTACH CLIP BS 500B LBL 23 IAW SRM 51-40-02; DWG# 143A7505.; [05] VERIFIED CORRECTIVE ACTION 4; [06] VERIFIED JOB COMPLETE

Part: NONE — CRACKED (R/H WING) · airframe 66,485 hrs · 32,340 cycles

RIGHT WING T/E WIGGLE PLATE IS CRACKED AT ORSS 261 ; / [01] REMOVED R/W T/E WIGGLE PLATE IAW AMM 51-40-02-0G-0 STEP 4. FIG 8; [02] VERIFIED; [03] INSTALLED NEW WIGGLE PLATE O/ R/W T/E ORSS 261 IAW SRM 51-40-02-0G-0 STEP 4; [04] INSTALLED NEW WIGGLE PLATE ON R/W T/E ORSS 261 IAW SRM 51-40-02-0G-0 STEP 4; [05] VERIFIED; [06] VERIFIED CORRECTIVE ACTION STEPS 3 AND 4

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

FWD CARGO BAY BAFFLE CRACKED AT FASTENER HOLE BS 500C - BS 500D RBL 23 WL 156 ; / [01] REMOVED FWD CARGO BAY BAFFLE CRACKED BS 500C - 500D RBL23 WL 156 IAW SRM 51-40-02.; [02] LOCATED AND DRILLED NEW FCB BAFFLE BS 500C-500D RBL23 WL156 AS PER DWG 143A7505 AND SRM 51-40-05-0G-0. REQUESTING OK TO TREAT AND PRIME.; [03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2. VERIFIED OK TO TREAT AND PRIME.; [04] 0K TO INSTALL.; [05] OK TO INSTALL BAFFLE; [06] INSTALLED FWD CARGO NEW BAFFLE BS 500C-500D RBL 23 WL 156 ;143A7503-9;PO#839727;IAW SRM 51-40-02 AND DWG 143A7505 REV:A.; [07] VERIFIED INSTALLATION OF THE BS500C-500D RBL 23 WL156 PER SRM 51-40-02 AND DWG 143A7505 REV:A

Part: NONE — CRACKED (L/H WING) · airframe 66,485 hrs · 32,340 cycles

LEFT WING T/E WIGGLE PLATE AT ORSS 261 IS CRACKED ; / [01] REMOVED AND REPLACED L/W T/E WIGGLE PLATE AT ORSS 261 IAW SRM 51-40-02-0G-0 STEP 4; [02] VERIFIED CORRECTIVE ACTION STEP 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACK IN FRAME BS 747 STR 8R OUTBD ATTACH HOLE FOR AIR CONDITIONING RAIL BRACKET. CRACKS PROPAGATE FROM INBD EDGE OF HOLE UP .300 IN AND DOWN .300 IN. MARKED ENDS FO CRACKS IN RED ; / [01] FAULT TO BE REPAIRED ON TTG8Q006QAGC; [02] VERIFIED CORRECTIVE ACTION 1.

Part: FRAME — CRACKED · airframe 66,485 hrs · 32,340 cycles

CRACK IN FRAME BS 747 STR 8L OUTBD ATTACH HOLE FOR AIR CONDITIONING RAIL BRACKET. CRACKS PROPAGATE FROM INBD EDGE OF HOLE UP .300 IN AND DOWN .300 IN. MARKED ENDS OF CRACKS IN RED. ; / [01] REPAIRED ON TTG8Q006Q5KY; [02] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

INTERIOR; BS 867 FRAME; IN-BETWEEN STR 9L AND STR8L; WL 273; IS CRACKED AT I/B FASTENER HOLE. (AREA WHERE THE SUPPORT BRACKET IS REMOVED). ; / [01] CRACK AT BS 867 BETWEEN 8-9 L/H TO BE REPAIRED ON TTG8Q006Q5L5; [02] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE

Part: FRAME — CRACKED · airframe 66,485 hrs · 32,340 cycles

CRACK IN FRAME BS 747 STR 8L OUTBD ATTACH HOLE FOR AIR CONDITIONING RAIL BRACKET. CRACKS PROPAGATE FROM INBD EDGE OF HOLE UP .400 IN AND DOWN .250 IN. MARKED ENDS OF CRACKS IN RED. ; / [01] CORRECTION TO FAULT - DISCREPANCY SHOULD BE BS 867 NOT 747.; [02] REPAIRED ON TTG8Q006Q5L5; [03] VERIFIED CORRECTIVE ACTION ENTRY 2. CARD COMPLETE

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CORROSION ON DOUBLER BS 1016-1040 LBL 6- LBL 9 W/L 306.5 ; / [01] REMOVED CORROSION AT DOUBLER BS.1016+20 TO BS.1040 LBL.5 TO LBL.9 REWORK DIMENSION L:7' X W:3' IAW SRM 51-10--02; [02] REMOVER 5EA RIVETS AT DUOBLER IAW SRM 51-40-02; [03] REMOVED CORROSION AT DOUBLER BS.1016+20 TO BS.1016+23 LBL.5 TO LBL.9 REWORK DIMENSION L:4' X W:33' IAW SRM 51-10--02; [04] CERTIFIED; [05] REMOVED CORROSION AT DOUBLER BS.1016+20 TO BS.1016+23 LBL.5 TO LBL.9 REWORK DIMENSION L:4' X W:3' IAW SRM 51-10--02; [06] CERTIFIED; [07] VERIFIED CORRECTIVE ACTION STEP 5; [08] REQUIRED NDT INSPECTION AT AREA FOR FREE CRACK CONDITION; OPEN HOLE AND UT REMNANT THICKNESS; [09] HFEC INSPECTED DOUBLER BLENDOUT AREA; IAW B737 NDTM P6; 51-00-00 PROC 23. NO CRACKS NOTED. TOOL ID ATS1465; N600; [10] HFEC INSPECTED OPEN HOLES IAW B737 NDTM P6; 51-00-00 PROC 16. NO CRACKS NOTED. TOOL ID ATS1465; N600; TOOL ID ATS1411; MINIMITE; [11] HFEC INSPECTED COUNTERSINKS IAW B737 NDTM P6; 53-30-00 PROC 3. NO CRACKS NOTED. TOOL ID ATS1465; N600; TOOL ID ATS1411; MINIMITE; [12] UT INSPECTED DOUBLER BLENDOUT AREA IAW B737 NDTM P4; 51-00-00 PROC 2. REMAINING MAT. 0.036 TOOL ID ATS2342; E650; [13] VERIFIED DAMAGED REPAIRED PER EA 21-153-02996 REV: A.; [14] VERIFIED DAMAGE REPAIRED PER EA 21-153-02996; REV A

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CORROSION ON SUPPORT ANGLE BS 1016+23' RBL 6 - RBL 12 W/L 306.5<REMOVED 3EA FASTENERS AT SUPPORT ANGLE BS.1016+23 RBL.9 TO RBL.12 IAW SRM 51-40-02 REMOVED CORROSION AT SUPPORT ANGLE BS.1016+23 RBL.9 TO RBL.12 REWORKED DIMENSION L:3' X W:0.750' IAW SRM 51-10-02. HFEC INSPECTED ANGLE BLENDOUT AREA IAW B737 NDTM P6 51-00-00 PROC 23. NO CRACKS NOTED. HFEC INSPECTED OPEN HOLES IAW B737 NDTM P6 51-00-00 PROC 16. LOCATED AND DRILLED ANGLE BS 1016+23 LBL 12 - RBL 12 IAW SRM 51-40-05 DWG# 148A3110. APPLIED CHEMICAL CONVERSION COATING ON ANGLE PER SRM 51-20-01

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-23R WL164. MARKED ; / [21] INSTALLED REPLACEMENT STRINGER SECTION BS 500D+12 TO 540 AND HAT SECTION REPAIR BS 500D+4 TO 500D+16 STR 23R/H WL 164 IAW SRM 53-00-03-2R-1 AND SRM 51-40-02 AND EA NO: 21-153-02931 REV A; [22] REPAIR COMPLETE; [23] VERIFIED INSTALLED REPLACEMENT STRINGER SECTION BS 500D+12 TO 540 AND HAT SECTION REPAIR BS 500D+4 TO 500D+16 STR 23R/,NG,NRC,2021-10-25 16:05:41,22Y,Y,MX,0,0,,CRACKED STRINGER AT AREA AFT OF FCB BS540 S-23R WL164. MARKED ;"

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-25R WL156. MARKED ; / [01] EVALUATED CRACK AT STRINGER 25RH; BS 540 WL 156- STRINGER FOUND OUT OF LIMIT PER SRM 53-00-03-1A-1 PARAGRAPH 4 A(2)(A)1; [02] REMOVED FASTENERS FROM STRINGER 26R BS 500D+6'- 540; IAW SRM 51-40-02-0G-0.; [03] REMOVED DAMAGED BY TRIMMING OUT STRINGER SECTION BETWEEN BS 500D-520; STR- 25RH. PER SRM 51-10-02.; [04] HFEC INSPECTED STRINGER CUTOUT 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 IAW B737 NDTM P6; 51-00-00 PROC 16. NO CRACKS NOTED. TOOL ID ATS1465; N600; TOOL ID ATS1411; MINIMITE; [06] HFEC INSPECTED COUNTERSINK HOLES COMMON TO REPAIR AREA; IAW B737 NDTM P6; 51-30-00 PROC 3. NO CRACKS NOTED. TOOL ID ATS1465; N600; TOOL ID ATS1411; MINIMITE; [07] VERIFIED CORRECTIVE ACTION STEP 3; [08] CORRECTION FOR ITEM 2- FASTENERS REMOVE FROM STRINGER 25R BS 500D+6'- 540; IAW SRM 51-40-02-0G-0.(NOT STRINGER 26R AS STATED ON ITEM 2); [09] INSTALLED ALL FASTENERS COMMON TO REPAIRED STRINGER. BETWEEN BS 500D-540; STR 25. REPAIR ACCOMPLISH PER EA#21-153-02934 REV:A.; [10] CORRECTION FOR ITEM 9- INSTALLED ALL FASTENERS COMMON TO REPAIRED STRINGER. BETWEEN BS 500D-540; STR 25R. REPAIR ACCOMPLISHED PER EA#21-153-02934 REV:A.; [11] VERIFIED STRINGER REPAIR BS 500D-540; STR 25R ACCOMPLISHED PER EA 21-153-02934 REV: A.; [12] VERIFIED STR 25R AT BS500D-540 WAS REPAIRED ON EA 21-153-02934 REV: A. AND CORRECTIVE ACTION STEPS 9-11.

Part: STIFFENER — CRACKED (R/H HORIZ. STAB.) · airframe 66,485 hrs · 32,340 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; 129.50; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] REQUEST NDI TO VERIFY RH RIB AT STAB STA 129.50;3RD VERTICAL STIFFENER CRACKED.;[11] FABRICATED REPAIR PARTS -1 T SECTION FROM 7075-T76511 0.063 INCH LOT#1463116-1;-2 ANGLE BAC1490 7075T6 0.063 INCH LOT#1464923-1;-3 FILLER 7075T6 0.050 INCH LOT# 5087747-1;-4 SHIM 7075T6 0.016 INCH LOT# 1439717-1 PER SRM 55-10-09-2R-5.; [12] REQUEST Q.C DO A GENERAL VISUAL INSPECTION OF ALL AREAS WITHIN THE REPAIR AREA PER SRM 55-10-09-2R-5.STEP 4F.; [13] VERIFIED CORRECITIVE ACTION 11 AND 12.; [14] APPLIED A CHEMICAL CONVERSION COATING TO THE REPAIR PARTS AND THE BARE SURFACES AND EDGES OF THE RIB. APPLIED ONE LAYER OF BMS 10-11; TYPE I PRIMER TO THE REPAIR PARTS AND THE BARE SURFACES AND EDGES OF THE RIB. PER SRM 55-10-09-2R-5. O.K TO INSTALL REPAIR PARTS.; [15] INSTALLED THE REPAIR PARTS WITH FASTENERS PER SRM 55-10-09-2R-5.; [16] VERIFIED CORRECTIVE ACTION 14.; [17] VERIFIED CORRECTIVE ACTION 15.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACK INDICATION ON FRAME DURING MFEC INSPECTION BS 500C STR 8R AT AIR CONDITIONING BRACKET INBD FASTENER HOLE ; / [01] CORRECTION TO ORIGINAL DISCREPANCY SHOULD BE STRINGER 8 LEFT.; [02] DISPLACED INSULATION BLANKETS FOR ACCESS AT BS 500B - 500D; STR 7 - 10 LH PER AMM 25-80-00-000-801.; [03] INSULATION BLANKETS TO BE INSTALLED ON CUSTOMER CARD TTG8Q006V3MH; [04] REPAIR COMPLETED ON CARD TTG8Q006QK4S; [05] VERIFIED BS500C STR8L FRAME REPAIRED ON CC# TTG8Q006QK4S AND BLANKETS RESTORED ON CC# TTG8Q006V3MH

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-26R WL153. MARKED ; / [09] FABRICATED AND LOCATED AND DRILLED NEW STRINGER REPAIR SECTION BS 500D+12' TO 540 ; APPLIED CHEMICAL CONVERSION ON STR REPAIR 26 R/H. ITEM: HFAB53-STR-011; LOT: 1470602-1; P.O.# 839549/1. IAW SRM 53-00-03-2R-1 FIGURE 205/REPAIR 1. REQUEST OK TO PRIMER; [10] VERIFIED CORRECTIVE ACTION ITEMS 7-9.; [11] OK TO PRIME STRINGER SECTION.; [12] PREVIOUS FABRICATED PART FORMED INCORRECTLY. RECEIVED NEW PART FROM O.S.S PER PO# 841052-SWA.<BR>FABRICATED; LOCATED AND DRILLED HAT/SPLICE SECTION AND STRINGER SECTION PER SRM 53-00-03-2R-1 FIGURE 205/REPAIR 1. <BR><BR>APPLIED CHEMICAL CONVERISON COATING ON REPAIR PARTS PER SRM 53-00-03-2R-1 FIGURE 205/REPAIR 1; 4.I REQUEST OK TO PRIME.; [13] VERIFIED CORRECTIVE ACTION ENTRY 12. OK TO PRIME GIVEN; [14] APPLIED PRIMER PER SRM 53-00-03-2R-1 FIGURE 205/REPAIR 1; 4.J. REQUEST OK TO INSTALL.; [15] VERIFIED CORRECTIVE ACTION ENTRY 1. OK TO INSTALL GIVEN.; [16] INSTALLED REPAIR PARTS PER SRM 53-00-03-2R-1 FIGURE 205/REPAIR 1.; [17] VERIFIED CORRECTIVE ACTION STEP 16.; [18] TASK CARD COMPLETE; [19] ALL WORK HAS BEEN ACCOMPLISHED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACK INDICATION ON FRAME FOUND ON MFEC INSPECTION. BS 747 STR 8R AT AIR CONDITIONING BRACKET INBD ATTACH FASTENER ; / [01] REPAIRED ON TTG8Q006QGJW; [02] VERIFIED CORRECTIVE ACTION 1

Part: SHIELD — CORRODED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

AFT CARGO BAY; R/H FLOOR TO SIDE WALL SHIELD HAS SEVERAL AREAS OF CORROSION AND HAS BEEN PREVIOUSLY BLENDED; BS 767 TO 787; RBL 21; WL 156; ; / [01] NOT FOUND ALLOWABLE DAMAGE ON THE SRM;REPAIR BY REPLACEMENTE PART IAW SRM 51-10-02-0G- 0 STEP 9.REMOVED SHIELD IAW SRM 51-40-02-0G-0; [02] UP DATE MEASUREMENTS; [03] RECEIVED NEW SHIELD ITEM 7530271 ; LOCATED AND DRILLED NEW ACB; R/H FLOOR TO SIDE WALL SHIELD BS 767 TO 787; RBL 21 WL 156 IAW SRM 51-47-05 AND DWG 146A8127 ID:0001 REV:C. OK TO APPLY WHITE PAINT; [04] RECEIVED NEW SHIELD ITEM 7530271 ; LOCATED AND DRILLED NEW ACB; R/H FLOOR TO SIDE WALL SHIELD BS 767 TO 787; RBL 21 WL 156 IAW SRM 51-47-05 AND DWG 146A8127 ID:0001 REV:C; [05] VERIFIED CORRECTIVE ACTION ENTRY 3; OK TO PAINT GIVEN; [06] OK TO INSTALL; [07] OK TO INSTALL; [08] REQUEST OK TO INSTALL SHIELD. PAINT APPLIED ON CUST CARD TTG8Q0048CWL; [09] UPDATED OK TO INSTALL; [10] OKAY TO INSTALL AFT CARGO BAY FWD SHIELD; [11] OK TO INSTALL GIVEN.; [12] INSTALLED ACB R/H FLOOR TO SIDE WALL SHIELD BS 767 - 787 RBL 21 WL 156 IAW SRM 51-40-02 AND DWG 146A0081 ID:0010 REV:A; [13] INSTALLED ACB R/H FLOOR TO SIDE WALL SHIELD BS 767 - 787 RBL 21 WL 156 IAW SRM 51-40-02 AND DWG 146A0081 ID:0010 REV:A; [14] FINAL INSPECTION. JOB COMPLETE PER SRM 51-40-02 AND DWG 146A0081 ID:0010 REV:A; [15] UPDATED MEASUREMENTS; [16] UPDATED MEASUREMENTS; [17] VERIFIED JOB COMPLETE

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED FRAME AT STRINGER 8 LEFT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 747. ; / [01] REPAIRED ON TTG8Q006Q8BH; [02] VERIFIED CORRECTIVE ACTION 1

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 500A. ; / [01] REPAIR ACCOMPLISHED ON TTG8Q006Q92Z; [02] REPAIR FRAME AT B.S 500A R/H STRINGER 8 AIR CONDITIONING BRACKET ACCOMPLISHED ON CUST SYSTEM ID: TTG8Q006Q92Z; [03] VERIFIED CORRECTIVE ACTION 2

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED FRAME AT STRINGER 8 LEFT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 400. ; / [01] TO BE REPAIRED ON TTG8Q006Q91V; [02] VERIFIED FAULT REPAIRED ON CC# TTG8Q006Q91V

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 727D. ; / [01] REPAIRED ON TTG8Q006Q934; [02] VERIFIED BS727D STR8L REWORK PERFORMED ON CC# TTG8Q006Q934

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 480. ; / [01] REFER TO FAULT TTG8Q006QSFD WHERE EA 21-153-02907 WAS ADDED AS A SUBTASK; [02] VERIFIED CORRECTIVE ACTION 1

Part: FORMER — NONE (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

FAIRING FORMER FOR FWD EDGE OF PANEL 192BR AT BS 540 HAS BARE METAL AND HAS FRETTING WEAR.REMOVED TAPERED SHIM AT FAIRING FORMER FWD EDGE OF PANEL 192BR IAW SRM 51-40-02-0G-0. CHEMICAL CONVERSION AT NEW SHIM IAW BAC5719 TYPE II CLASS A AND PRIME. INSTALLED TAPERED SHIM IAW SRM 51-40-02-0G-0 AS SHOWN IN NON-CONFORMANCE RECORD N1440006068. REMOVED CLAMPS APPLIED TEFLON URETHANE COATING AT NEW SHIM IAW BAC5715.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 400. ; / [01] TO BE REPAIRED ON TTG8Q006Q8C6; [02] VERIFIED CRACKED FRAME AT BS 400 STR8R WAS REPAIRED ON CC# TTG8Q006Q8C6

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED FRAME AT STRINGER 8 LEFT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 480. ; / [01] TO BE REPAIRED ON TTG8Q006Q8B7; [02] VERIFIED BS480 STR8L FRAME WAS REPAIRED ON CC# TTG8Q006Q8B7

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 727B. ; / [01] INSTALLED EWIS PROTECTION IN WORK AREA IAW AMM 20-60-07; [02] VERIFIED INSTALLATION OF EWIS PROTECTION PER AMM 20-60-07; [03] CERTIFY; [04] REMOVED EWIS PER AMM 20-60-07 REPAIRED ON TTG8Q006Q8CB; [05] VERIFIED CORRECTIVE ACTION 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED FRAME AT STRINGER 8 LEFT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 727D. ; / [01] REPAIR COMPLETED ON CUSTOMER CARD NO. TTG8Q006Q91P.; [02] VERIFIED CORRECTIVE ACTION 1

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 827. ; / [01] TO BE REPAIRED ON TTG8Q006Q93G; [02] VERIFIED CORRECTIVE ACTION 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 787. ; / [01] REPAIR COMPLETED ON CUSTOMER CARD NO TTG8Q006Q8CK; [02] CERTIFY; [03] VERIFIED CORRECTIVE ACTION 1

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

CRACKED FRAME AT STRINGER 8 LEFT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 867. ; / [01] REPAIRED ON TTG8Q006Q924; [02] VERIFIED CORRECTIVE ACTION 1

Part: BATTERY — FAILED (CABIN) · airframe 66,485 hrs · 32,340 cycles

M1675 EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST ; / [01] REMOVED M1675 EMERGENCY BATTERY AND REPLACED WITH SERVICEABLE BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(1)-(5); [02] VERIFIED CORRECTIVE ACTIONS STEP 1.; [03] PERFORMED GOOD INSTALLATION TEST OF M1675 EMERGENCY LIGHT BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(6); [04] VERIFIED CORRECTIVE ACTION #3

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 66,485 hrs · 32,340 cycles

AFT CARGO FWD SCUFF PLATE IS CRACKED ; / [01] WELDED CRACK 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 E10583 S/N:KJ256554 12/2021; [02] VERIFIED CORRECTIVE ACTION 1.; [03] FLUORESCENT DYE PENETRANT INSPECTED REPAIR AREA IN ACCORDANCE WITH SOPM 20-20-02 METHOD C. NO DEFECTS NOTED<BR><BR>TOOL I.D. ATS2504 RADIOMETER; [04] SANDED REPAIR WELD AREA PER SRM 53-60-15-2R-1 PARA 4.B.(5); [05] VERIFIED WELD REWORK AREA SANDED PER SRM 53-60-15-2R-1 PARA 4.B.(5); [06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01; [07] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01; [08] COMPLETION OF THIS CARD AND INSTALLATION OF AFT CARGO FWD SCUFF PLATE WILL BE DONE ON CARD:<BR><BR>TTG8Q006PKNV<BR><BR>727142 FUSELAGE 5088; [09] COMPLETION OF THIS CARD AND INSTALLATION OF AFT CARGO FWD SCUFF PLATE WILL BE DONE ON CARD:<BR><BR>TTG8Q006PJFK; [10] COMPLETION OF THIS CARD AND INSTALLATION OF AFT CARGO FWD SCUFF PLATE WILL BE DONE ON CARD:TTG8Q006PJFK; [11] VERIFIED CORRECTIVE ACTION 10.; [12] VERIFIED ALL STEPS COMPLETE.

Part: BATTERY — FAILED (CABIN) · airframe 66,485 hrs · 32,340 cycles

M1668 EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST ; / [01] REMOVED AIR RETURN GRILL AT STA 603 LBL 67 PER CMM 25-23-01 PARA. 1.2 AND REMOVED M1668 EMERGENCY BATTERY AND REPLACED WITH SERVICEABLE BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(1)-(5); [02] VERIFIED CORRECTIVE ACTION STEP 1.; [03] OK TO CLOSE GIVEN.; [04] REINSTALLED AIR RETURN GRILL AT STA 603 LBL 67 PER CMM 25-23-01 PARA. 1.3 AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805 STEP 4.D.(6); [05] CORRECTION FOR ITEM 4; REINSTALLED AIR RETURN GRILL AT STA 603 LBL 67 PER CMM 25-23-01 PARA. 1.3 AND PERFORMED GOOD INSTALLATION TEST OF M1668 EMERGENCY LIGHT BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(6); [06] VERIFIED CORRECTIVE ACTION #5

Part: BATTERY — FAILED (CABIN) · airframe 66,485 hrs · 32,340 cycles

M1670 EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST ; / [01] REMOVED AIR RETURN GRILL AT STA 727C+13 LBL 68 PER CMM 25-23-01 PARA. 1.2 AND REMOVED M1670 EMERGENCY BATTERY AND REPLACED WITH SERVICEABLE BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(1)-(5); [02] VERIFIED CORRECTIVE ACTIONS STEP 1.; [03] OK TO CLOSE GIVEN.; [04] REINSTALLED AIR RETURN GRILL AT STA 727C+13 LBL 68 PER CMM 25-23-01 PARA. 1.3 AND PERFORMED GOOD INSTALLATION TEST OF M1670 EMERGENCY BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(6); [05] VERIFIED CORRECTIVE ACTION STATEMENT 4

Part: BATTERY — FAILED (CABIN) · airframe 66,485 hrs · 32,340 cycles

M1669 EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST ; / [01] REMOVED AIR RETURN GRILL AT STA 603 RBL 67 PER CMM 25-23-01 PARA. 1.2 AND REMOVED M1669 EMERGENCY BATTERY AND REPLACED WITH SERVICEABLE BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(1)-(5); [02] VERIFIED CORRECTIVE ACTIONS STEP 1.; [03] OK TO CLOSE GIVEN.; [04] REINSTALLED AIR RETURN GRILL AT STA 603 RBL 67 PER CMM 25-23-01 PARA. 1.3 AND PERFORMED GOOD INSTALLATION TEST OF M1669 EMERGENCY BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(6); [05] VERIFIED CORRECTIVE ACTION #4

Part: BATTERY — FAILED (CABIN) · airframe 66,485 hrs · 32,340 cycles

M1674 EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST ; / [01] REMOVED M1674 EMERGENCY BATTERY AND REPLACED WITH SERVICEABLE BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(1)-(5); [02] VERIFIED CORRECTIVE ACTIONS STEP 1.; [03] PERFORMED GOOD INSTALLATION TEST OF M1674 EMERGENCY BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(6); [04] VERIFIED CORRECTIVE ACTION #3

Part: LAMP — INOPERATIVE (EXERIOR LIGHT) · airframe 65,397 hrs · 31,757 cycles

RIGHT OVERWING EXIT EXTERIOR EMERGENCY EXIT LIGHT INOP / REPLACED RIGHT OVER WING EXTERIOR EMERGENCY EXIT LIGHT LAMP; OPS CHECK GOOD IAW AMM 33-51-04-960-801.; COMPLETED FINAL INSPECTION CARD STEP 1.<BR>AUDIT C/W

Part: LIGHT — UNSECURE (CABIN) · airframe 63,935 hrs · 30,904 cycles

EMERGENCY EXIT FLOOR TRACK LIGHT STRIP NEAR ROW 8, LEFT SIDE IS NOT SECURED, POPS OUT OF CHANNEL. SECURED EMERGENCY FLOOR TRACK LIGHT STRIP, IAW SIP.

Part: FILTER — FAULTY (NR 2 ENGINE) · airframe 63,150 hrs · 30,446 cycles

IMMEDIATELY AFTER TAKE OFF F/A'S REPORTED FUMES/ SMOKE IN CABIN. FOLLOWED QRH PROCEDURES FOR RETURN TO LAX. SOURCE OF FUMES/SMOKE COULD NOT DETERMINED BY CABIN CREW. NOTE: NR 2 ENG OIL QTY DURING START WAS 70%. AT STRTR CUTOUT OIL QTY WAS 98% / REPLACED NR 2 ENG SUPPLY FILTER PER AMM 79-21-03 & SCAVENGE FILTER PER AMM 79-21-06. DRAINED EXCESS OIL FROM RESERVOIR & SERVICED TO PROPER LEVEL PER AMM 12-13-11. ENG IDLE RUNS GOOD, NO OTHER FAULTS NOTED AT THIS TIME. PERFORMED NR 2 ENG INTERNAL OIL SYSTEM INSPECTION BORESCOPE PER POWER PLANT ENGINEERING REF NRC D350652 FOR COMPLETION. REF LOGPAGE FOR RESOLUTION OF SMOKE/FUMES IN CABIN.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 61,799 hrs · 29,631 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672 IN THE CABIN. / R&R BATTERY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,774 hrs · 29,614 cycles

RH OVERWING EMERGENCY LIGHTS INOP. / REPLACED AND OPS CHECKED THE SLIDE/OVERWING LIGHT LAMP IAW AMM 33-51-04. OPS CHECK GOOD.

Part: LIGHT — DAMAGED (LT OVERWING) · airframe 61,774 hrs · 29,614 cycles

LH OVERWING EMERGENCY LIGHT ASSEMBLY IS DAMAGED. / REMOVED AND REPLACED L/H OVERWING EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-04-960-802 OPS CHECK GOOD.

Part: FRAME — DAMAGED (BS 787) · airframe 61,774 hrs · 29,614 cycles

FOUND DAMAGE AT THE UNDERSIDE OF THE AFT CARGO FRAME NEXT TO ATTACHING FASTENER HOLE FOR THE ZEE CHANNEL AT STA 787 LBL 24 TO LBL 25 WL 153. / REPAIRED DAMAGE TO UNDERSIDE OF FRAME BS 787 LBL 24-25 WL 153, PER SWA EA 1-753-35931 REV IR (ATS ER 19-05439 REV IR).

Part: PANEL — CRACKED (CABIN) · airframe 61,774 hrs · 29,614 cycles

PANEL BREAK FOUND CRACKED AT STA 540 BL 0 TO RBL 24 WL 208 / CRACK ON PANEL BREAK AT 540 BLO TO RBL 24 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM PER SRM 51-10-02 9C REPAIRABLE BY REPLACEMENT REMOVED AND REPLACED PANEL BREAK PER SRM 51-40-02-0G-0 AND BOEING DWG 143A0060 REB B SRM 51-40-05-0G-0 ITEM 7530909 PO 766806 57773 10/17/19

Part: PANEL — CRACKED (CABIN) · airframe 61,774 hrs · 29,614 cycles

PANEL BREAK FOUND CRACKED AT STA 540 BL 0 TO LBL 24 WL 208 / REMOVED AND REPLACED PANEL BREAK AT STA 540 BL 0 TO LBL 24 WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; BOEING DWG 143A5240 REV B; AND BOEING DWG 143A0060 REV B PO# 487849 57335U 10/16/19 PN# 143A5240-3

Part: INTERCOSTAL — CORRODED (BS 847-855) · airframe 61,774 hrs · 29,614 cycles

AFT CARGO INTERCOSTAL AFT OF DOOR CORRODED AROUND SEVERAL HOLES BETWEEN BS. 847 TO BS. 855, STR. 25R. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,774 hrs · 29,614 cycles

FORWARD EMERGENCY LIGHT POWER UNIT BATTERY DEAD. / R&R BATTERY PACK M1675 PER AMM.

Part: STIFFENER — BROKEN · airframe 61,774 hrs · 29,614 cycles

STIFFENER BROKEN AT STA 663 RBL 6 TO RBL 30 WL 153 / REMOVED AND REPLACED WITH NEW STIFFNER AT STA 663 RBL 6 TO RBL 30 WL 153 PO# 746581 IAW SRM 51-40-05 AND DWG 111A1001. STIFFENER IS BEING TRANSFERRED TO TASK CARD NUMBER N226420; OF ALL WORK AND DOCUMENTATION PERFORMED.

Part: SUPPORT CHANNEL — CORRODED (FWD CARGO) · airframe 61,774 hrs · 29,614 cycles

***CORROSION*** FWD. CARGO COMPARTMENT; STA 510 BL 0 WL 148 UPPER SIDE OF SUPPORT ANTENNA HAS CORROSION. / CORROSION AT FWD CARGO COMPARTMENT STA 510 BL 0 WL 148 ON UPPER SIDE OF SUPPORT ANTENNA WAS FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS SHOWN IN THE SRM. REMOVED AND REPLACED ANTENNA SUPPORT CHANNEL IAW SRM 51-40-02 AND BOEING DRAWING 143A3230 REV A

Part: BEAM — CRACKED (GALLEY DOOR) · airframe 61,774 hrs · 29,614 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 AND #5 BEAM TO BE CRACKED. / REPLACED FORWARD SERVICE DOOR. COMPLETED DOOR ADJUSTMENTS. PERFORMED SYSTEM TEST AND CABIN PRESSURE LEAK CHECK IAW AMM 52-41-00, 52-71-11, 05-51-91 LEAK AND OPS CHECK GOOD.

Part: LUG — CORRODED (VERT. STAB.) · airframe 61,774 hrs · 29,614 cycles

* CORROSION * VERTICAL STABILIZER FWD ATTACH LUGS AT UPPER FUSELAGE STA 1016 RBL 8 WL 300.8 / REMOVED CORROSION IAW ATS ER 19-05192 REV IR & SWA EA 1-753-35935 REV IR.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,774 hrs · 29,614 cycles

FORWARD CARGO SUB THRESHOLD WEB CORRODED BETWEEN BS. 440 TO BS. 494, STR. 24R TO STR. 25R. / R&R WEB IAW SRM & DWG.

Part: STIFFENER — CORRODED (BS 1128) · airframe 61,774 hrs · 29,614 cycles

STIFFENER CORRODED AT THE APU TAIL CONE COMPARTMENT BS. 1128, RBL 23. / R&R STIFFENER IAW SRM AND DWG.

Part: LUG — CORRODED (VERT. STAB.) · airframe 61,774 hrs · 29,614 cycles

*CORROSION* VERTICAL STABILIZER LEFT FWD ATTACH LUGS AT UPPER FUSELAGE STA 1016 LBL 8 WL 300.8 / REMOVED CORROSION IAW ATS ER 19-05192 REV IR AND SWA EA 1-753-35935 REV IR.

Part: FLAP — DEBONDED (L/H WING) · airframe 61,774 hrs · 29,614 cycles

LEFT HAND INBOARD AFT FLAP LOWER SURFACE DISBOND AT 29' FROM O/B AND 4' FROM T/E / DISBOND ON LEFT HAND I/B AFT FLAP WAS TO PROTECTIVE PLIES ONLY AT 4' FROM T/E AND 29' FROM O/B EDGE. REPAIR DISBOND PER SRM 57-53-01-2R-4 PARA 3D AND SRM 51-70-05-2R-0.

Part: BRACKET — BROKEN (L/H WING) · airframe 61,774 hrs · 29,614 cycles

LEFT WING PANEL 551FB; HAS A BROKEN CLIP UPPER FWD EDGE / REMOVED & REPLACED BROKEN CLIP/BRACKET ON FWD EDGE OF LH WING LOWER TRAILING EDGE PANEL 551FB; IAW B737 SRM 51-40-02-0G-0 & BOEING ENGINEERING DRAWING 115A2710

Part: BRACKET — CORRODED (FUSELAGE) · airframe 61,774 hrs · 29,614 cycles

***CORROSION*** VERTICAL ANTENNA SUPPORT BRACKET AT BS 360 BL0 WL 146 CORRODED ON RH FLANGE / REMOVED AND REPLACED NEW VERTICAL ANTENNA SUPPORT BS 360 BL 0 WL 146; PER SRM 51-40-02-0G-0; DWG. 141A1160 REV C; AND DWG 141A1153 REV. A

Part: SKIN — CORRODED (LOWER INT FUSELA) · airframe 61,774 hrs · 29,614 cycles

***CORROSION*** POSSIBLE CORROSION AROUND FASTENERS BS 358 TO 362 BETWEEN STR 27L TO 28L ON FUSELAGE INNER SKIN AND ATTACHING HARDWARE / REMOVED CORROSION ON UPPER SURFACE OF THE BS 360 SPLICE P/N 141A3523-14 BETWEEN BS 358 TO 362 AND STR 27L TO STR 28L (ON FUSELAGE INNER SKIN AND ATTACHING HARDWARE) PER ER 19-05079 AND S.R.M 51-10-02. CORROSION REMOVAL EVALUATION WITHIN ALLOWABLE LIMITS IAW SWA EA 1-753-35818 REV. IR AND ER 19-05079 REV. IR

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 61,774 hrs · 29,614 cycles

SEAT TRACK CORRODED BETWEEN BS. 540 TO BS. 727B, LBL 24. / R&R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 380-446) · airframe 61,774 hrs · 29,614 cycles

SEAT TRACK HAS CORRODED BETWEEN BS. 380 TO BS. 446, RBL 24. / R&R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 61,774 hrs · 29,614 cycles

SEAT TRACK CORRODED BETWEEN BS. 540 TO BS. 727B, RBL 24. / R&R SEAT TRACK IAW SRM, AMM & DWG.

Part: SEAT TRACK — CORRODED (BS 380-446) · airframe 61,774 hrs · 29,614 cycles

SEAT TRACK HAS CORRODED BETWEEN BS. 380 TO BS. 446, RBL 45. / R&R SEAT TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 727B-887) · airframe 61,774 hrs · 29,614 cycles

SEAT TRACK HAS CORRODED BETWEEN BS. 727B TO BS 887, LBL 24. R&R SEAT TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 61,774 hrs · 29,614 cycles

SEAT TRACK CORRODED BETWEEN BS. 540 TO BS. 727B, LBL 45. / R&R SEAT TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,774 hrs · 29,614 cycles

SEAT TRACK CORRODED BETWEEN BS. 727B TO BS. 887, RBL 24. R&R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 480-540) · airframe 61,774 hrs · 29,614 cycles

SEAT TRACK CORRODED BETWEEN BS. 480 TO BS. 540, LBL 24. / R&R SEAT TRACK PER SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 61,774 hrs · 29,614 cycles

SEAT TRACK CORRODED BETWEEN BS. 540 TO BS. 727B, RBL 45. / R&R SEAT TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 480-540) · airframe 61,774 hrs · 29,614 cycles

SEAT TRACK CORRODED BETWEEN BS. 480 TO BS. 540, LBL 45. / R&R SEAT TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 727B-887) · airframe 61,774 hrs · 29,614 cycles

SEAT TRACK CORRODED BETWEEN BS. 727B TO BS. 887, RBL 45. / R&R SEAT TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 480-540) · airframe 61,774 hrs · 29,614 cycles

SEAT TRACK CORRODED BETWEEN BS. 480 TO BS. 540, RBL 24. R&R SEAT TRACK PER SRM & DWG.

Part: SKIN — DENTED (BS 219) · airframe 61,774 hrs · 29,614 cycles

FOUND DENT ON EXTERIOR FUSELAGE SKIN @STA. 219+3, 16.5" ABOVE STR. 24R. / SKIN DENT DAMAGE BS 219+3, 16.5" ABOVE 24R STR IS REPAIRED PER SWA EA 1-753-35906 REV IR (ATS ER 19-05208 REV IR).

Part: SKIN — DENTED (RT NR 7 SPOILER) · airframe 61,774 hrs · 29,614 cycles

R/H WING #7 SPOILER LOWER SURFACE HAS A DENT 42" FROM I/B END 12" FROM T/E. / REPLACED #7 SPOILER WITH SERVICEABLE UNIT DUE TO DENTS OUT OF LIMITS IAW B737 AMM 27-62-12-400-801.

Part: GUSSET — CRACKED (BS 500D) · airframe 61,774 hrs · 29,614 cycles

FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET PER SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 61,774 hrs · 29,614 cycles

FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET PER SRM AND DWG.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 61,774 hrs · 29,614 cycles

VAPOR BARRIER CRACKED AT BS. 663.75, BETWEEN RBL 4.00 TO RBL 25.4. / REPAIRED VAPOR BARRIER PER SRM.

Part: CHANNEL — CORRODED (BS 867-885) · airframe 61,774 hrs · 29,614 cycles

AFT CARGO BAY R/H AFT Z-CHANNEL CORRODED BETWEEN BS. 867 TO BS. 885, RBL 21. / R&R Z-CHANNEL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 61,774 hrs · 29,614 cycles

***CORROSION*** AFT CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT STA 947 RBL 21-LBL 10 WL 177 HAS CORROSION / REMOVED AND REPLACED AFT CARGO AFT BULKHEAD FLOOR SUPPORT STA 947 RBL 21- LBL 10 WL 177 IAW SRM 51-40-02-0G-0 AND DWG 149A8110 DUE TO OUT OF LIMITS CORRISION IAW SRM 51-10-02-0G-0 STEP 9(C)

Part: SKIN — DENTED (BS 312) · airframe 61,774 hrs · 29,614 cycles

FOUND DENT ON EXTERIOR FUSELAGE SKIN @STA. 312+4.8, .5" ABOVE STR. 22R. / REMOVED DAMAGE & REPAIRED EXTERIOR FUSELAGE SKIN @ STA 312+4.8, 5" ABOVE STR 22R IAW EA 1-753-35902 REV IR & ATS ER 19-05221.

Part: SKIN — DENTED (BS 792) · airframe 61,774 hrs · 29,614 cycles

FOUND DENT ON EXTERIOR FUSELAGE SKIN @STA. 792+9, 4.0" ABOVE STR. 27R. / REMOVED DENT DAMAGE ON THE EXTERIOR FUSELAGE SKIN @ STA 792+9, 4.0" ABOVE STR. 27R AND INSTALLED REPAIR PARTS IAW SWA EA 1-753-35955 REV. IR AND ER 19-05191 REV. IR.

Part: SHIELD — CORRODED (BS 492-500A) · airframe 61,774 hrs · 29,614 cycles

FORWARD CARGO DOOR SHIELD AFT OF DOOR CORRODED AROUND SEVERAL FASTENER HOLES BETWEEN BS. 492 TO BS. 500A, STR. 25R. / R&R SHIELD PER SRM AND DWG.

Part: SKIN — DENTED (BS 787) · airframe 61,774 hrs · 29,614 cycles

FOUND DENT ON EXTERIOR FUSELAGE SKIN @ STA. 787+13.8, 1.6" BELOW STR. 27L. / THE DAMAGE IS REPAIRED UNDER ATS ER 19-05191 REV IR AND EA 1-753-35955 REV IR.

Part: SKIN — CORRODED (FWD FUSELAGE) · airframe 61,774 hrs · 29,614 cycles

***CORROSION*** ON EXTERNAL FUSELAGE SKIN BETWEEN STA 500D - 520; STR 28R - 28L; WL 150 / EXTERNAL FUSELAGE SKIN BS 500D-520 STR 28R-28L WL 150 REPAIRED PER ATS ER 19-05155 REV IR AND SWA EA 1-753-35948 REV IR.

Part: SHIELD — CORRODED (BS 787-798) · airframe 61,774 hrs · 29,614 cycles

AFT CARGO SHIELD FORWARD OF DOOR CORRODED AROUND SEVERAL FASTENER HOLES FROM BETWEEN BS. 787 TO BS 798, STR. 25R. / R&R SHIELD IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 420-440) · airframe 61,774 hrs · 29,614 cycles

FORWARD CARGO SHIELD FORWARD OF DOOR CORRODED AROUND SEVERAL FASTENER HOLES BETWEEN BS. 420 TO BS. 440, STR. 25R. / R&R SHIELD PER SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,774 hrs · 29,614 cycles

AFT CARGO BAY L/H Z CHANNEL CORRODED AROUND SEVERAL FASTENER HOLES BETWEEN BS. 727D TO BS. 787, STR. 25L. / R&R ZEE CHANNEL IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 847-867) · airframe 61,774 hrs · 29,614 cycles

AFT CARGO SHIELD AFT OF DOOR CORRODED AROUND SEVERAL FASTENER HOLES BETWEEN BS. 847 TO BS. 867, STR. 25R.. / R&R SHIELD IAW DWG & SRM.

Part: CHANNEL — CORRODED (FWD CARGO RH) · airframe 61,774 hrs · 29,614 cycles

***CORROSION*** FWD CARGO R/H Z CHANNEL HAS CORROSION AROUND SEVERAL FASTENER HOLES FROM BS 500A TO BS 500D; STR 25R; RBL 18; WL 157. / CORROSION OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED 'Z' CHANNEL I-A-W SRM 51-40-02-0G-0 AND BDWG# 143A7501; LOCATED AND DRILLED FASTENER HOLES PER SRM 51-40-05-0G-0. TREATED AND PRIMED PER AMM 51-21-41-370; AMM 51-21-72-370; MATERIAL USED BAC 1496-444; 707576 0.040 PO# 745571 PER SRM 53-30-53-01-2 AT FWD CARGO R/H STA 500A & 500D; C.I.C APPLIED PER SOPM 20-41-05

Part: SKIN — DENTED (BS 787) · airframe 61,774 hrs · 29,614 cycles

FOUND DENT ON EXTERIOR FUSELAGE SKIN @STA. 787+14.6, 1.5" BELOW STR. 27R. / THE DAMAGE IS REPAIRED UNDER ATS ER 19-05191 REV IR AND EA 1-753-35955 REV IR.

Part: SKIN — DENTED (BS 807) · airframe 61,774 hrs · 29,614 cycles

FOUND DENT ON EXTERIOR FUSELAGE SKIN @STA. 807, STR. 27R TO 27L. / THE DAMAGE IS REPAIRED UNDER ATS ER 19-05191 REV IR AND EA 1-753-35955 REV IR.

Part: CHANNEL — CORRODED (AFT CARGO COMPT) · airframe 61,774 hrs · 29,614 cycles

***CORROSION*** AFT CARGO BAY R/H Z CHANNEL HAS CORROSION AROUND SEVERAL FASTENER HOLES FROM BS 727 TO BS 787; STR 25R; RBL 18; WL 157. / REMOVED & REPLACED AFT CARGO BAY R/H Z CHANNEL FROM BS 727 TO BS 787 STR 25R RBL 18 WL 157 IAW EA 1-753-35928 REV IR / ATS ER 19-05229; REV IR DATED 04-NOV-2019 PAGES 1-8

Part: SKIN — DENTED (BS 792) · airframe 61,774 hrs · 29,614 cycles

FOUND DENT ON EXTERIOR FUSELAGE SKIN @ STA. 792+10.3, 3.0" ABOVE STR. 26R. / THE DAMAGE IS REPAIRED UNDER ER 19-05191 REV IR AND EA 1-753-35955 REV IR.

Part: LENS — MISSING (CABIN) · airframe 61,030 hrs · 29,134 cycles

LOWER FWD EMERGENCY EXIT LIGHT MISSING DIRECTIONAL ARROW. R&R COVER PER AMM.

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 61,030 hrs · 29,134 cycles

OVERWING EMERGENCY EXIT DOOR HANDLE MOLDING IS NOT SECURED. SECURED IAW AMM.

Part: STRAP — BROKEN (FWD FLASHLIGHT) · airframe 60,827 hrs · 29,019 cycles

TOP FORWARD CABIN EMERGENCY FLASHLIGHT HOLDER PLASTIC RETAINING STRAP BROKEN. / R&R STRAP PER AMM.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 60,319 hrs · 28,702 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING P/N 115A5211-2 LOWER O/B LUG FACE CORRODED REPAIRED PER EA NO: 1-A57-3246 REV 10

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 60,319 hrs · 28,702 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING P/N 115A5211-2 UPPER I/B LUG FACE CORRODED REPAIRED PER EA NO: 1-A57-3246 REV 10.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 60,319 hrs · 28,702 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING P/N 115A5211-1 UPPER I/B LUG FACE CORRODED REPAIRED PER EA 1-A57-3246 REV 10

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 60,319 hrs · 28,702 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING P/N 115A5211-1 LOWER O/B LUG FACE CORRODED REPAIRED PER EA 1-A57-3246 REV 10

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 60,319 hrs · 28,702 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING P/N 115A5211-2 LOWER I/B LUG FACE CORRODED REPAIRED PER EA NO: 1-A57-3246 REV 10

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 60,319 hrs · 28,702 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING P/N 115A5211-1 UPPER O/B LUG FACE CORRODED REPAIRED PER EA 1-A57-3246 REV 10

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 60,319 hrs · 28,702 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING P/N 115A5211-1 LOWER I/B LUG FACE CORRODED REPAIRED PER EA 1-A57-3246 REV 10

Part: STRUT — DAMAGED (RT MLG) · airframe 60,147 hrs · 28,602 cycles

R/H MLG LOWER SIDE STRUT HAS A 1" X 3.5" AREA OF LOOSE AND MISSING PAINT AND EVIDENCE OF LIGHT CORROSION IN CENTER LOWER RADIUS OF H BEAM AREA UPPER SIDE MOD REPAIRED PER EA 1-732-1383. THIS IS A TIME LIMITED REPAIR/ACTION REMOVE AND REPLACE THE R/H MAIN LANDING GEAR FOR OVERHAUL. (REMOVABLE COMPONENT: P N 161A1100-32 SN MAL01346Y0661) PERMANENT ACTON REQUI

Part: LINK — CORRODED (LT MAIN GEAR) · airframe 60,147 hrs · 28,602 cycles

L/H MLG REACTON LINK HAS CORROSION @ UPPER SIDE STRUT ATTACH POINT MOD SEE DISC#/JO J10229137 FOR CORRECTIVE ACTION.

Part: STRUT — CORRODED (RT MLG) · airframe 60,147 hrs · 28,602 cycles

R/H MAIN LANDING GEAR SHOCK STRUT OUTER CYLINDER CORRODED AT AFT SIDE OF UPPER TORSION LINK OUTBOARD ATTACH LUG. / REPAIRED GEAR PER EA.

Part: STRUT — CORRODED (LT MAIN GEAR) · airframe 60,147 hrs · 28,602 cycles

L/H MLG LOWER SIDE STRUT HAS CORROSION IN RADIUS OF LOWER CENTER H BEAM UPPER SIDE MOD REPAIRED PER EA 1-732-1382. THIS IS A TIME LIMITED REPAIR ACTION. REMOVE AND REPLACE THE L/H MAIN LANDING GEAR FOR OVERHAUL IN 30 DAYS. (REMOVABLE COMPONENT: P N 161A1100-31 SN MAL01345Y0661) PERMANENT ACTION REQU

Part: STRUT — CORRODED (RT MLG) · airframe 60,147 hrs · 28,602 cycles

R/H MAIN LANDING GEAR SHOCK STRUT OUTER CYLINDER CORRODED AT R/H AFT TRUNNION WEB. / REPAIRED GEAR PER EA.

Part: STRUT — CORRODED (RT MLG) · airframe 60,147 hrs · 28,602 cycles

R/H MAIN LANDING GEAR SHOCK STRUT OUTER CYLINDER CORRODED AT FORWARD SIDE STRUT PIN LUG, AFT SIDE. / REPAIRED GEAR PER EA.

Part: SUPPORT BRACKET — CRACKED (LWR FUSELAGE) · airframe 59,856 hrs · 28,424 cycles

DIAGONAL SUPPORT BRACKET ABOVE FUSELAGE PANEL 192JR BROKEN. / REMOVED AND REPLACED DIAGONAL SUPPORT BRACKET ABOVE FUSELAGE PANEL 192JR PER SRM 51-40-02.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 59,856 hrs · 28,424 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STA 193.90, 18" FORWARD OF THE AFT SPAR. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 59,856 hrs · 28,424 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STA 193.90, 10" FORWARD OF THE AFT SPAR. REPAIRED SKIN PER EA.

Part: SLIDER — CRACKED (HORIZONTAL STAB) · airframe 59,856 hrs · 28,424 cycles

RH HORIZONTAL STABILIZER UPPER FWD SLIDER IS CRACKED / R/R R/H UPPER FWD SLIDER REF AMM 53-31-31.

Part: SLIDER — CRACKED (HORIZONTAL STAB) · airframe 59,856 hrs · 28,424 cycles

LH HORIZONTAL STABILIZER UPPER FWD SLIDER IS CRACKED / R/R L/H UPPER FWD SLIDER REF AMM 53-31-31.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 59,159 hrs · 28,006 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 58,963 hrs · 27,889 cycles

REAR GALLEY PHOTOLUMINESCENT FLOOR LIGHT INOP. R&R STRIP PER AMM.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 58,963 hrs · 27,889 cycles

FORWARD GALLEY PHOTOLUMINESCENT FLOOR LIGHT INOP. R&R STRIP PER AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 58,915 hrs · 27,863 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 58,460 hrs · 27,582 cycles

FORWARD GALLEY FLASHLIGHT STRAP BROKEN. R&R STRAP IAW SIP.

Part: VAPOR BARRIER — CRACKED (WHEEL WELL RH) · airframe 57,911 hrs · 27,248 cycles

RIGHT WHEEL WELL VAPOR BARRIER HAS SINGLE CRACK 10.5 INCH LONG. / ACCOMPLISHED INTERIM REPAIR IAW SRM 57-10-10.-2R-2.

Part: SLIDE — WORN (L2 DOOR) · airframe 57,764 hrs · 27,153 cycles

L2 DOOR SLIDE GIRT ASSEMBLY WORN. R&R SLIDE PER MT.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,586 hrs · 27,045 cycles

RT WING INBOARD AFT FLAP DELAMINATED ON LOWER SURFACE. R&R AFT FLAP PER AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 55,689 hrs · 25,901 cycles

RT OVERWING EMERGENCY EXIT SIGN COVER LENS MISSING. INSTALLED LENS IAW AMM.

Part: FITTING — UNSECURE (L2 DOOR) · airframe 55,624 hrs · 25,864 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR CLASP MISALIGNED. SECURED FITTING PER MT AND SIP.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,588 hrs · 25,843 cycles

EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY CHECK AT LOCATION M01673. R & R THE BATTERY PACK IAW MM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO BAY FORWARD BULKHEAD BRACKET CRACKED AT BS 727+4, BETWEEN BL 0 TO RBL 10. R&R BRACKET PER SRM AND DWG.

Part: LIGHT — DAMAGED (CABIN) · airframe 55,212 hrs · 25,579 cycles

G1 GALLEY EMERGENCY EXIT LIGHT DAMAGED. R&R LIGHT IAW MM.

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

***CORROSION*** ACB; BS 727+4; BL0; WEB; CORRODED. / OUT OF LIMITS DUE TO CORROSION OVER MORE THAN 3 IN 10 FASTENERS PER SRM 53-00-53-1A-2 STEP 4C(B) FIG 103(E). FORMED; ALODINED; DRILLED AND PRIMED PER DWG. 146A3426-7 & SRM 51-40-05-0G-0. MADE OUT OF 7075-0- .032 CLAD LOT # 1285531 HEAT TREATED TO T62 ON P.O.# 64969T. PART TO BE INSTALLED ON SWA CARD NO. T704486.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 55,212 hrs · 25,579 cycles

LT HORIZONTAL STABILIZER RIB ASSEMBLY CRACKED AT STAB STA 120.30, BETWEEN 2ND AND 4TH VERTICAL STIFFENERS. REPAIRED RIB ASSEMBLY PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 55,212 hrs · 25,579 cycles

LT HORIZONTAL STABILIZER RIB ASSEMBLY CRACKED AT STAB STA. 92.70, 2ND VERTICAL STIFFENER. REPAIRED RIB ASSEMBLY PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

MOPSILL STRAP CORRODED AT BS 294.5, RBL 52. R&R STRAP IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

SKIN CORRODED AT BS 1016, BETWEEN RBL 12 TO LBL 12. REPAIRED SKIN PER SRM AND EA.

Part: TIE DOWN — CORRODED (AFT CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

DUE TO THE EXTENT OF DAMAGE; ACB; LH; BS 731 TO BS 867; LBL 17.2; TIE DOWN TRACK REQUIRES REPLACEMENT. / REMOVED AND INSTALLED NEW ACB; LH; B.S. 707+4 TO 867; LBL & 7.2 TIE-DN TRACK PER SRM 51-40-02-0G-0 AND DWG. # 146A T500

Part: WEB — ELONGATED (FWD CARGO RH) · airframe 55,212 hrs · 25,579 cycles

FWD CARGO BAY VERTICAL WEB HAS OBLONG HOLES BS500-500A; STR26R. / REMOVED AND REPLACED DAMAGED VERTICAL WEB BS 500-500A STR 26R PER DWG 143A0080 AND DWG 143A8122 AND SRM 51-40-02

Part: WEB — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO BAY, VERTICAL WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 21. R&R WEB PER SRM & DWG.

Part: CARGO TRACK — DAMAGED (CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

DUE TO EXTENT OF DAMAGE, CARGO TIE DOWN TRACK BS 727+4 TO BS 887, RBL 13.84 REQUIRES TO BE REPLACE. REMOVED DAMAGED CARGO TIE DOWN TRACK B.S. 727+4 - B.S. 887 RBL 13.84 AND REPLACED WITH NEW CARGO TIE DOWN TRACK PER SRM 51-40-02-0G-0, SRM 53-00-53-2R-3 AND DWG # 146A7500. 41473U 24SEP17 (PER SA-M735 R ARCENEAUX 3/7/20)

Part: FLOOR PANEL — DENTED (COCKPIT) · airframe 55,212 hrs · 25,579 cycles

DENTS ON FLIGHT DECK FLOOR FROM B.S. 255-257, LBL 14 - RBL 4. W.L. 208. INSTALLED REPAIR AT STA 255-257 LBL 14 TO RBL 4 IAW SRM 53-10-51-2R-2 REPAIR 2 STEP 4.B.C.D.E.F.G.H.I.J. K.& M (SAM-735/R. ARCENEAUX)

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 55,212 hrs · 25,579 cycles

MOISTURE BARRIER WEB CRACKED AT BS 663, LBL 13. REPAIRED BARRIER PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

BULKHEAD STIFFENER CRACKED AT BS 663, LBL 27. R&R STIFFENER PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 20. REPAIRED SUPPORT PER ER & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 727E+10, LBL 20. REPAIRED SUPPORT PER ER & EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO LAV TANK DRAIN PAN SUPPORT ANGLE CORRODED AT BS 849, BETWEEN STR 24L TO STR 25L. R&R ANGLE PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO RT FLOOR SUPPORT CORRODED AT BS 727D+5, RBL 3. R&R SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO LAV TANK DRAIN PAN AT WATER SERVICING TUBE UNION NUTPLATES AREA CORRODED. R&R INTERCOSTAL ASSEMBLY PER SRM & DWG.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

***CORROSION*** AFT CARGO FLOOR SUPPORT AT 727A+4; RBL 3 CORRODED / ACB; CARGO FLOOR SUPPORT AT BS 727A+4; RBL 3 CORRODED; REMOVED CORROSION. 1.0' X 2.0' X 0.020' ORGINAL MATERIAL 0.063' REMAINING THICKNESS 0.043' DAMAGE OUT OF REPAIR LIMITS PER SRM 53-00-53-1A-2 AND SRM 51-10-02-0G-0; DAMAGE WILL BE REPAIRED ON CUSTOMER CARD T704367

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO LT FLOOR SUPPORT CORRODED AT BS 727D+5, LBL 8. R&R FLOOR BEAM PER SRM & DWG.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

***CORROSION*** AFT CARGO FLOOR SUPPORT AT 727-727A LBL 3 HAS CORROSION / ACB; FLOOR SUPPORT AT BS 727-727A LBL 3 CORROSION REMOVED 1.0' X 2.0' AND 1.0' X 1.0'; LOST MATERIAL 0.020' ORIGINAL MATERIAL 0.063' REMAINING THICKNESS 0.043' FOUND TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2 AND SRM 51-10-02-0G-0; DAMAGE WILL BE REPAIRED ON CUSTOMER CARD T704364

Part: NONE — CORRODED · airframe 55,212 hrs · 25,579 cycles

CORROSION ON MOPSILL INBD CHORD BS 960-980 RBL 60 WL 208 ON THRESHOLD SUPPORT FLANGE. / REMOVED CORRODED ASD MOPSILL INNERER CHORD BS 897 - 1006 RBL 60 WL 208. INSTALLED NEW CHORD IAW SRM 51-40-02; DWG 147A8501 DWG 147A0000.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

STUB FRAME CRACKED AT BS 294.5, RBL 57. REPAIRED STUB FRAME PER ER AND EA.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO DOORWAY LOWER THRESHOLD WEB CORRODED BETWEEN BS 795 TO BS 847. R&R WEB IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO LT FLOOR SUPPORT CORRODED UPPER SURFACE AT BS 727 TO BS 727E+10, LBL 3. R&R FLOOR SUPPORT PER DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 794, RBL 21. R&R SUPPORT PER SRM & DWG.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO RT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 887 TO BS 947, RBL 21. R&R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO LT FLOOR SUPPORT CORRODED AT BS 727D+5, LBL 12. REPAIRED SUPPORT BEAM PER SRM & EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 727 TO BS 727A, LBL 17.24. REPAIRED SUPPORT PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO RT FLOOR SUPPORT CORRODED AT BS 727D+5, RBL 8. R&R SUPPORT PER SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS 727A+10, LBL 17.24. REPAIRED SUPPORT PER SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

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

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

AFT CARGO LAV TANK DRAIN PAN SUPPORT ANGLE CORRODED AT BS 859, STR 25L. R&R ANGLE PER SRM.

Part: SCUFF PLATE — CORRODED (AFT CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

***CORROSION*** AFT CARGO BAY SCUFF PLATE BS 847 HAS CORROSION / REPLACED THE SCUFF PLATE BS 847 WITHE 453A2611-2 NEW PER SRM 51-10-02-0G-0. 9.2 TO BE INSTALLED ON CUSTOMER CARD JPANEL-141-CLOSE 56708U 27SEP17

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

***CORROSION*** AT FCB SHIELD BS 500 TO 500A RBL 25 / REMOVED AND REPLACED DAMAGED SHIELD BS 495-500A RBL PER DWG 143A0080 AND SRM 51-40-02

Part: TIE DOWN — CRACKED (AFT CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

ACB; BS 727E; RBL 13; CARGO TIE DOWN TRACK CRACKED. / ACB BS 727E; RBL 13 CARGO TIE DOWN TRACK WILL BE REPAIRED ON CUSTOMER CARD T704437 LEAD 45 19SEP17

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

***CORROSION*** AFT CARGO BAY CAP STRIP BS 727-787 R/H HAS CORROSION / REPLACED THE ACB CAPSTRIP BS 727-787 R/H WITH 453A2611-9 NEW & 453A2611 NEW PER SRM 51-10-02-0G-0 9.2 TO BE INSTALLED ON CUSTOMER CARD JPANEL-141-CLOSE 56708U 27SEP17

Part: WEB — CRACKED (RT WING) · airframe 55,212 hrs · 25,579 cycles

RT WING UPPER T/E PANEL WEB IS CRACKED AT O/B FASTENER FOR PROGRAM FITTING. / REMOVED AND REPLACED RT WING UPPER T/E PANEL WEB THAT WAS CRACKED AT O/B FASTENER FOR PROGRAM FITTING IAW SRM 51-40-02 AND AMM 20-50-11-910-801 FASTENER CALL OUT IAW BOEING DRAWING 115A2512 89813U 09-22-17

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 440 TO BS 500D, LBL 24. R&R SUPPORT PER SRM.

Part: SERVICE DOOR — CORRODED (LWR FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

LAVATORY SERVICE DOOR IS CORRODED AT BONDING JUMPER AND AFT LATCH / REMOVED LAVATORY SERVICE DOOR PER SRM 51-40-02 LEAD45 18SEP17 56708U INSTALLED A 7523161 NEW DOOR REPLACED AFT LATCH & BONDING JUMPER PER SRM 51-40-02 AMM 52-49-07-400-801 OHMS CHECK IS GOOD 56708U 28SPE17 AS WELL AS IPC 52-48-07-01 & AMM 52-49-07-000-802 56708U 28SEP17

Part: PLATE — CORRODED (FWD CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

***CORROSION*** FCB FLOOR TO CARGO NET ANCHOR PLATE HAS CORROSION / RECIEVED REPLACEMENT PART NO. 458A1611-25 FCB FLOOR TO CARGO NET ANCHOR PLATE. TO BE INSTALLED ON SWA CARD NO. JPANEL-121-CLOSE.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

***CORROSION*** AFT CARGO BAY CAP STRIP BS 847-947 R/H HAS CORROSION / RECEVED AFT CARGO BAY CAP STRIP BS 847-947 R/H WITH NEW STRIP TO BE INSTALLED ON CUSTOMER CARD JPANEL-141-CLOSE 56708U 28SEP17 FOR TRAKING PERPUSES ONLY 56708U 28SEP17

Part: SCUFF PLATE — CORRODED (AFT CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

***CORROSION*** AFT CARGO BAY SCUFF PLATE BS 795 HAS CORROSION / REPLACED THE ACB SCUFF PLATE BS 795 WITH NEW 453A2611-1 NEW PER SRM 51-10-02-0G-0 9-2 TO BE INSTALLED ON CUSTOMER CARD JPANEL-141-CLOSE 56708U 27SEP17

Part: BRACKET — CRACKED (RT WING) · airframe 55,212 hrs · 25,579 cycles

RT WING PANEL 657BT BRACKET ASSEMBLY CRACKED AT FASTENER HOLE. R&R BRACKET ASSEMBLY IAW AMM AND DWG.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 55,212 hrs · 25,579 cycles

***CORROSION*** AFT CARGO BAY CAP STRIP BS 727-847 L/H HAS CORROSION / REPLACED THE ACB CAPSTRIPS BS 727-847 L/H WITH 453A2611-4 NEW & 453A2611-10 & 7253311 NEW PER SRM 51-40-02-0G-0 9;2 TO BE INSTALLED ON CUSTOMER CARD JPANEL-141-CLOSE 56708U 27SEP17

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 55,212 hrs · 25,579 cycles

LT MAIN WHEEL WELL VAPOR BARRIER WEB CRACKED AT BS 663, BETWEEN LBL 28.5 TO LBL 31. REPAIRED WEB PER SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 55,212 hrs · 25,579 cycles

***CORROSION*** FLOOR PANEL 120AF HAS CORROSION / EVALUATION FOUND FLOOR PNL # 120AF OUT OF LIMITS PER SRM 53-00-53-1A-1; ITEM 5.A.(1)(B). FABRICATED NEW PANEL #120AF MATERIAL I.D. 0.71 2024T-3 LOT# 1283496; DRILLED; COUNTERSINK & ALODINE PER DRWING 453A1610. DRILL / HOLES PER SRM 51-40-05-0G-0; COUNT / SINK PER SRM 51-40-08-0G-0; ALODINED PER BAC5619 CLASS B; AMM 51-21-41-37-801; APPLICATION. 1035C 19SEP17. 385INSP 09/19/17 PRIMED FLOOR PANEL # 120AF PER AMM 51-21-72-370-804. 88641U 19SEP17 1035C 19SEP17

Part: SKIN — CRACKED (LE SLAT) · airframe 55,212 hrs · 25,579 cycles

RT WING NR 6 SLAT LOWER SURFACE NOSE SKIN CRACKED AT ACTUATOR RIB ATTACH POINT. REPAIRED SKIN PER SRM.

Part: SHIELD — BROKEN (FLASHLIGHT) · airframe 53,268 hrs · 24,480 cycles

AFT EMERGENCY FLASH LIGHT SHIELD BROKEN. R&R SHIELD IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 52,609 hrs · 24,113 cycles

L1 DOOR EMERGENCY EXIT SLIDE LOOSE. SECURED SLIDE PER MT.

Part: FASTENER — LOOSE (GIRT BAR) · airframe 51,554 hrs · 23,523 cycles

R1 DOOR ESCAPE SLIDE AFT GIRT BAR RETAINER CLIP FASTENERS LOOSE. R & R FASTENERS IAW SRM.

Part: BULKHEAD — CRACKED (BS 663) · airframe 51,554 hrs · 23,523 cycles

BULKHEAD FIBERGLASS PANEL CRACKED BS 663, LBL 14.5. REPAIRED THE BULKHEAD PANEL IAW EA.

Part: BULKHEAD — CRACKED (BS 663) · airframe 51,554 hrs · 23,523 cycles

BULKHEAD FIBERGLASS PANEL CRACKED AT BS 663, LBL 27. REPAIRED THE BULKHEAD PANEL IAW EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 51,554 hrs · 23,523 cycles

R1 DOOR EMERGENCY SLIDE OUT OF POSITION. R & R THE SLIDE IAW MT.

Part: BRACKET — CRACKED (BS 867) · airframe 51,554 hrs · 23,523 cycles

BRACKET CRACKED AT BS 867, STRINGER 2R. R & R BRACKET IAW SRM.

Part: FRAME — CRACKED (BS 727) · airframe 51,554 hrs · 23,523 cycles

LOWER FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED FRAME WEB IAW EA.

Part: SIGN — MISSING (CABIN) · airframe 51,202 hrs · 23,328 cycles

R2 DOOR EXIT SIGN MISSING. INSTALLED SIGN PER SIP.

Part: SIGN — MISSING (CABIN) · airframe 51,202 hrs · 23,328 cycles

MID CABIN EXIT SIGN MISSING. INSTALLED SIGN PER SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,398 hrs · 22,336 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 4 ABC. RELAMPED IAW MM.

Part: MOUNT — MISALIGNED (L2 DOOR) · airframe 49,245 hrs · 22,257 cycles

L2 DOOR EMER EVAC SLIDE FWD & AFT MOUNTS MISALIGNED. REALIGNED MOUNT IAW EA.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 48,970 hrs · 22,091 cycles

FORWARD EMER FLASHLIGHT SAFETY STRAPS BROKEN. R & R STRAPS IAW AMM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 46,981 hrs · 20,944 cycles

R1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. R & R SLIDE IAW MT.

Part: LENS — MISSING (CABIN) · airframe 46,386 hrs · 20,594 cycles

CABIN AISLE EMER LIGHT LENS MISSING. INSTALLED LENS IAW SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,982 hrs · 20,363 cycles

R2 DOOR SLIDE ILLUMINATION LIGHT WEAK. R & R BATTERY PACK IAW MM.

Part: FUSE — BLOWN (CABIN) · airframe 45,094 hrs · 19,858 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 8. R & R FUSE IAW AMM.

Part: COVER — OUT OF ADJUST (CABIN) · airframe 45,094 hrs · 19,858 cycles

AFT EMER LIGHT SWITCH COVER OUT OF ADJUSTMENT. ADJUSTED COVER IAW SWPM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,094 hrs · 19,858 cycles

LEFT EMER LIGHT INOPERATIVE AT ROW 14. R & R LIGHT IAW AMM.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 45,094 hrs · 19,858 cycles

RIGHT DOOR OVERWING EMER EXIT LIGHT OUT OF POSITION. REPOSITIONED LIGHT IAW AMM.

Part: LENS — DIRTY (CARGO DOOR) · airframe 45,094 hrs · 19,858 cycles

AFT CARGO DOOR EMER LIGHT FWD LENS DIRTY. CLEANED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,094 hrs · 19,858 cycles

EEPLS INOPERATIVE AT BS 880 LBL 30. REPAIRED EEPLS IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

AFT SEAT TRACK OTBD FLANGE HOLE CRACKED AT BS 727B LBL 45.5. R & R SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

SEAT TRACK CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW ATS ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

SEAT TRACK CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW ATS ER & EA.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 45,094 hrs · 19,858 cycles

FORWARD RT SERVICE DOOR EXIT LIGHT PLUG CONNECTOR DAMAGED. R & R CONNECTOR IAW WDM & AMM.

Part: SIGN — BROKEN (CABIN) · airframe 45,094 hrs · 19,858 cycles

AFT LOWER CEILING EXIT SIGN HOUSING BROKEN. R & R SIGN IAW AMM.

Part: PLATE — CRACKED (LT WING) · airframe 45,094 hrs · 19,858 cycles

LEFT WING WIGGLE PLATE CRACKED AT REAR SPAR BS 261. R & R WIGGLE PLATE IAW SRM & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

INTERCOSTAL CRACKED BETWEEN BS 927 TO 947, RBL 22. R & R INTERCOSTAL IAW DWG & SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

INTERCOSTAL CORRODED BETWEEN BS 747 TO BS 767, RBL 22. R & R INTERCOSTAL IAW DWG & SRM.

Part: SUPPORT — CORRODED (GIRT BAR) · airframe 45,094 hrs · 19,858 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR MOUNT SUPPORT CORRODED AT BS 312, LBL 55. R & R SUPPORT IAW DWG & SRM.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

PANEL 221BF DAMAGED TO OTBD AFT CORNER. REPAIRED PANEL IAW SRM.

Part: SUPPORT — CORRODED (GIRT BAR) · airframe 45,094 hrs · 19,858 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR MOUNT SUPPORT CORRODED AT BS 344, LBL 55. R & R SUPPORT IAW DWG & SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

RIGHT NR 3 WINDOW FRAME E - F POST CRACKED AT SECOND LOWEST HOLE. REPAIRED FRAME IAW ER & EA.

Part: POST — CRACKED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

LEFT NR 1 WINDOW FRAME C - D POST CRACKED AFT LT UPPER CORNER. REPAIRED POST IAW ACO.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

AFT PRESS BULKHEAD WEB DOME OIL CANNED AT STRINGER 12R. REPAIRED WEB DOME IAW DWG & SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

AFT CARGO BAY FLOOR SUPPORT STRAP CORRODED AT BS 767+4. R & R STRAP IAW DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

AFT CARGO BAY AFT BULKHEAD LOWER SUPPORT CORRODED AT BS 947, BETWEEN LBL 7 TO RBL 24. R & R SUPPORT IAW DWG & SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

BULKHEAD CRACKED AT BS 663, RBL 41. REPAIRED BULKHEAD IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 45,094 hrs · 19,858 cycles

RIGHT WING AFT & INBD OF NACELLE CTR LINE, FIXED TE INBD SUPPORT BRACKET CRACKED AT AFT FASTENER HOLE. R & R BRACKET IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 767+4, LBL 8. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 767+4, LBL 12. REPAIRED SUPPORT IAW EA.

Part: STRIP — CRACKED (RT WING) · airframe 45,094 hrs · 19,858 cycles

RIGHT WING INBD END OF AFT NUTPLATE STRIP BENEATH PANEL 661AB CRACKED. REPAIRED STRIP IAW SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

AFT CARGO BAY DOUBLER CORRODED AT BS 727D RBL 7. REPAIRED DOUBLER IAW ER & EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 767+4, RBL 3. REPAIRED SUPPORT IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

LEFT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 747+6 TO BS 827, LBL 22. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 767+4, LBL 3. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 767+4, RBL 8. REPAIRED SUPPORT IAW EA.

Part: PLATE — CRACKED (RT WING) · airframe 45,094 hrs · 19,858 cycles

RIGHT WING INBD FWD WIGGLE NUTPLATE STRIP BENEATH PANEL 651GB CRACKED. R & R WIGGLE PLATE IAW SRM & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

FORWARD BULKHEAD SUPPORT CORRODED AT BS 847-1, LBL 23. REPAIRED SUPPORT IAW ER & EA.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 45,094 hrs · 19,858 cycles

BULKHEAD CRACKED AT BS 663, LBL 35. REPAIRED BULKHEAD IAW TC.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,094 hrs · 19,858 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727C TO BS 767, RBL 22. REPAIRED SUPPORT IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 45,094 hrs · 19,858 cycles

RIGHT HORIZONTAL STABILIZER LE 9 RIB AT STAB STATION 138.7 CRACKED. REPAIRED RIB IAW SRM.

Part: GROUNDING STRAP — CORRODED (NR 2 NACELLE) · airframe 45,094 hrs · 19,858 cycles

NR 2 ENG STRUT FWD GND STRAP CORRODED. R &R STRAP IAW DWG & SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 45,094 hrs · 19,858 cycles

RIGHT HORIZONTAL STABILIZER LE NR 5 RIB AT STAB STATION 101.9 CRACKED. R & R RIB ASSEMBLY IAW SRM & DWG.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 45,094 hrs · 19,858 cycles

BULKHEAD CRACKED AT BS 663, LBL 40. REPAIRED BULKHEAD IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 45,094 hrs · 19,858 cycles

LEFT WING UPPER TE SUPPORT ANGLE CRACKED AT LOWER FASTENER, RSS 274. R & R ANGLE IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 45,094 hrs · 19,858 cycles

LEFT WING BULB SEAL ATTACH ANGLE CRACKED AT RSS 274. R & R ANGLE IAW SRM.

Part: SIGN — FADED (CABIN) · airframe 45,094 hrs · 19,858 cycles

FORWARD RT EXIT SIGN LETTERING FADED. R & R SIGN IAW AMM.