N7723E

BOEING 737 Part 121 — SOUTHWEST AIRLINES, CO.

Cessna 150 None injury — operator not yet resolved

ATA 3350

EMERGENCY LIGHT BATTERY PACK M01672 FAILED A CAPACITANCE CHECK. REMOVED AND REPLACED EMX BATTERY BACK M01672 IAW AMM 33-51-06-960-805-NG.

ATA 7200

NR 2 ENG FAIL ON T/O ROLL. NR 2 ENGINE FAILURE AND RTO AT 100KTS METAL IN THE TAILPIPE. REPLACED NR 2 ENGINE IAW MT 771-00-01 REF TTG8Q00YY43D.

ATA 3350

12 DEF EXIT/SALIDA COVER MISSING. INSTALLED NEW EMERG EXIT LENS PER AMM 33-51-01.

ATA 5730

L/H O/B UPPER SURFACE DISBOND ON EXISITING REPAIR DOUBLER. REMOVED DAMAGE PER SRM 57-53-01-2R14; PERFORMED TAP TEST PER 737 NET MANUEL PART 1 51-05-01 . PREPED AREA ;FABRICATED REPAIR PARTS INSTALLED REPAIR PARTS PER SRM 57-53-01-2R-14. AND SRM 51-70-05-2R-0 GEN. REPAIR. PREPED AREA AND AND APPLIED PRIMER AND TOP COAT PER AMM 1-21-72 AND 51-21-99.

ATA 2560

R1 GIRT BAR LOOSE<[01] INSTALLED NEW RIVET ON R1 DOOR GIRT BAR BRACKET PER SRM 51-40-02.

ATA 7200

HIGH SPEED REJECTED TAKEOFF DUE TO LARGE BIRD STRIKE ON #2 ENGINE. NO ABNORMAL INDICATIONS; HOWEVER PAX AND FLIGHT ATTENDANTS COMPLAINED OF AN ODOR. <[01] C/W BIRD STRIKE INSPECTION ON ACFT PER 05-51-18 BIRD REMAINS FOUND IN NUMBER TWO ENGINE EVIDENCE OF BIRD REMAINS IN CORE OF ENGINE NUMBER TWO; [02] COMPLETED BIRD STRIKE INSPECTION REF AMM 05-51-18. NO DAMAGE NOTED. COMPLETED E3 BORESCOPE REF TASK 772-00-02. NO DAMAGE NOTED. A/C OK FOR SERVICE.

ATA 5210

FWD ENTRY DOOR AFT DOOR ASSIST HANDLE IS BROKEN<[01] REMOVED AND INSTALLED IAW AMM 25-21-31-420-802<BR><BR>WN49860<BR>WN49856;[02] VERIFIED ITEM 1<BR>AUDIT C/W

ATA 3350

EMERGENCY EXIT BATTERY PACK M1670 WILL NOT CHARGE<[01] REMOVED AND REPLACED M1670 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR>WN49839;[02] VERIFIED ITEM 1<BR>C/W

ATA 3350

EMERGENCY EXIT BATTERY PACK M2335 WILL NOT CHARGE<[01] REMOVED AND REPLACED M2335 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD<BR>WN49840;[02] VERIFIED ITEM 1<BR>C/W

ATA 3350

EMERGENCY EXIT BATTERY PACK M1674 WILL NOT CHARGE<[01] REMOVED AND REPLACED M1674 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD<BR>WN49843;[02] VERIFIED ITEM 1<BR>C/W

ATA 3350

EMERGENCY EXIT BATTERY PACK M1668 WILL NOT CHARGE<[01] REMOVED AND REPLACED M1668 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD<BR>01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] WN49841;[03] VERIFIED ITEM 1;2<BR>C/W

ATA 3350

EMERGENCY EXIT BATTERY PACK M1675 WILL NOT CHARGE<[01] OPS CHECKED M1675 BATTERY IAW AMM 33-51-06-960-805; NO FAULT FOUND; OPS CHECK GOOD;[02] VERIFIED ITEM 1<BR>C/W

ATA 5320

(152-02) PASSENGER CABIN STA 867 STR 1R; FEEDER CABLE SUPPORT BRACKET IS CRACKED.<[01] REMOVED BRACKET AT BS867; BETWEEN S-1 AND S-2R; IAW SRM 51-40-02-0G-0. FABRICATED NEW BRACKET IAW BOEING DWG 287A4015 REV. -; BOEING PL 287A4015 REV. K; AND EA 25-153-00335. BRACKET WAS FORMED AND HEAT TREATED ON BACK SHOP W/O# 46301-2400-0002. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G-0 AND BOEING DWG. 146A7901 REV. -.;[02] AUDIT C/W

ATA 5320

DOT A24-77 FORWARD PIT. VERTICAL INTERCOSTAL AT STATION 480+15 BETWEEN STRINGERS 23L AND 25L CRACKED AT UPPER EDGE. BLENDED DAMAGE IAW SRM 51-10-02-0G-0. FOUND ADJACENT TO BLEND .040'; LOSS .007'; REMAINING .033' USING NDT TO VERIFY IN STEP 5. UPON FURTHER INVESTIGATION FOUND INTERCOSTAL TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1<BR>UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ADJACENT TO BLEND .040'; LOSS .007'; REMAINING .033'. REMOVED; LOCATED & DRILL HOLES NEW FORMED ANGLE IAW SRM 51-40-05-0G-0 AND SRM SRM 51-40-02-0G-0<BR><BR>PERFORMED COMFORMITY INSPECTION OF NEW PART AND VERIFIED INTERCOSTAL P/N 143A9403-14 COMFORME TO SPECIFICATIONS FOUND IN BOEINGDWG 143A9403 REV:-. MIX SEALANT 870 B 1/2 APPLIED FAY SEAL TO INTERCOSTAL AT 2.00 PM SQUEEZE -OUT 1/2 HRS CURE TIME 20 HRS AND INSTALLED INTERCOSTAL ALL FASTENERS BEFORE SQUEEZE OUT TIME IAW SRM 51-40-02-0G-0 AND DWG 143A7550 REV: A.

ATA 5321

DOT#54 A-043 CABIN FLOOR PANEL 242GF HAS PULLED FIBERS ON TOP SIDE OF PANEL<[01] AUDITED;[02] REFER TO FAULT TTG8Q00YBAGR WHERE EA 25-153-00203 WAS ADDED AS A SUBTASK.

ATA 5321

DOT#53 A-043 CABIN FLOOR PANEL 231WF HAS PULLED FIBERS ON TOP SIDE OF PANEL<[01] REPAIRED PER EA 25-153-00203.

ATA 5321

DOT#55 A-043 CABIN FLOOR PANEL 241KF HAS PULLED FIBERS ON TOP SIDE OF PANEL<[01] AUDIT C/W;[02] REFER TO FAULT TTG8Q00YBAGR WHERE EA 25-153-00203 WAS ADDED AS A SUBTASK..

ATA 5713

FASTENER TAB FOR LEFT WING INBOARD UPPER FIXED LEADING-EDGE STRINGER P/N 116A4531-5 IS BROKED OFF. REMOVED AND REPLACED -5 STRINGER ON LEFT WING INBOARD UPPER FIXED LEADING-EDGE P/N 116A4531-5 ATAG WN49678 IAW BOEING DWG 116A4008 REV - SRM 51-40-02. VERIFIED ITEM 1.

ATA 5321

FLOOR PANEL 222DF HAS PULLED FIBERS ON TOP SURFACE<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/W

ATA 5311

FWD GALLEY DOOR CUTOUT; UPPER FWD STUB FRAME HFEC SURFACE INSPECTION; FOUND 1' CRACK IN STUB FRAME AT JOGGLE; .70' ABOVE SEAL DEPRESSOR. MARKED IN BLACK. REF. CARD TTG8Q00TSZ8V INSP - FORWARD GALLEY DOOR (R1) BEAR STRAP BS 290-296 BETWEEN S-8R AND S-9R - GROUP 2. UPPER FWD STUB FRAME WAS REMOVED I.A.W. SRM 51-40-02-0G-0 INSTALLED NEW UPPER FWD STUB FRAME I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 141A8370; REV D.

ATA 5321

FLOOR PANEL 221BF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] REPLACED FLOOR PANEL 221BF WITH SERVICEABLE FLOOR PANEL ON SHELF I.A.W REFERENCE TO AIPC 53-21-51-75 PG 14 SHEET 01 ITEM A;[02] INFO ONLY: PANEL 221BF WAS REPLACED ON #TTG8Q00Y4M8W & INSTALLED ON #TTG8Q00YHR2;[03] INFO ONLY: PANEL 221BF WAS REPLACED ON #TTG8Q00Y4M8W & INSTALLED ON #TTG8Q00Y1HR2.

ATA 5321

(A204 DOT 98) FLOOR PANEL 231KF; AFT LH CORNER OF FLOOR PANEL IS DISBONDED.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/W

ATA 5321

FLOOR PANEL 221BF HAS 5EA PLACES OF PANEL BEING CRACKED/BROKEN ON LOWER SURFACE.<[01] REPLACED FLOOR PANEL 221BF WITH SERVICEABLE FLOOR PANEL ON SHELF I.A.W REFERENCE TO AIPC 53-21-51-75 PG 14 SHEET 01 ITEM A;[02] INFO ONLY: PANEL 221BF WAS REPLACED ON #TTG8Q00Y4M8W & INSTALLED ON #TTG8Q00YHR2

ATA 5321

(A204 DOT 101) FLOOR PANEL 231DF; UPPER SURFACE FACE SHEET MISSING FIBERS.<[01] C/W EA 25-153-00105. VERIFIED ALL STEPS COMPLETE.;[02] VERIFIED C/W;[03] C/W

ATA 5321

FLOOR PANEL 231UF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.

ATA 5321

(A204 DOT 93) FLOOR PANEL 221BF HAS 8EA FASTNER INSERTS WITH CORROSION; MARKED IN RED.<[01] REPLACED FLOOR PANEL 221BF WITH SERVICEABLE FLOOR PANEL ON SHELF I.A.W REFERENCE TO AIPC 53-21-51-75 PG 14 SHEET 01 ITEM A;[02] INFO ONLY: PANEL 221BF WAS REPLACED ON #TTG8Q00Y4M8W & INSTALLED ON #TTG8Q00YHR2;[03] INFO ONLY: PANEL 221BF WAS REPLACED ON #TTG8Q00Y4M8W & INSTALLED ON #TTG8Q00Y1HR2.

ATA 5321

(A204 DOT 99) FLOOR PANEL 231GF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/W

ATA 5220

(A204 DOT 86) RH EMERGENCY EXIT DOOR 843 PULL CLOSE HANDLE RECESS HAS 2EA MISSING QUARTER TURN STUDS.<[01] REPLACED MISSING QUARTER TURN STUDS IN HANDLE RECESS ON DOOR 843 I/A/W 52-22-51-400-801 .;[02] VERIFIED STEP 1<BR>AUDIT C/W

ATA 5321

(A204 DOT 97) FLOOR PANEL 231KF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/W

ATA 5310

DOT#38 A-043 FWD CARGO COMPARTMENT AFT BKHD UPPER STAINTION RAIL CAMLOCK RECIVER CRACKED STA 500D LBL 39 WL 193<[01] REMOVED AND REPLACED CAMLOCK AT AFT BULKHEAD UPPER RAIL IAW SRM 51-40-02-0G-0;[02] VERIFIED ITEM 1<BR>AUDIT C/W

ATA 5710

DOT#43 A-043 RH WINGLET HAS CORROSION ON UPPER INBD T/E 42' FROM BOTTOM EDGE<[01] 04 - REPAIRED PER [SRM 51-10-02-0G-0-A00248 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)] AND IAW APB 57-30-01 FIGURE 102 (D);[02] 04 - REPAIRED PER [SRM 51-10-02-0G-0-A01522 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - TRACKED COMPONENT - PERMANENT)] AND IAW APB 57-30-01 FIGURE 102 (D);[03] VERIFIED STEP 2<BR>AUDIT CW

ATA 5710

DOT#42 A-043 RH WINGLET HAS CORROSION ON LOWER OTBD T/E 18' FROM BOTTOM EDGE<[01] 04 - REPAIRED PER [SRM 57-30-01-1A-2-APB-AP37.1-0632-A01611 (PERMANENT (NON-DENT DAMAGE TYPES)-WINGLETS)];[02] VERIFIED STEP 1<BR>AUDIT CW

ATA 5320

154-86 AFT CARGO COMPARTMENT STA 907 STR 24R+4 SIDEWALL PANEL SUPPORT CORRODED NEAR THE FASTENER HOLE<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR> BOEING DWG 147A9409 ID:0015 REV:-;[02] VERIFIED STEP 1<BR>AUDIT CW

ATA 5514

(DOT 152-2) LEFT HORIZONTAL STABILIZER PANEL 333AB; SLIDING SEAL SUPPORT BRACKET IS CRACKED.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER PANEL 333AB; SLIDING SEAL I.A.W SRM 51-40-02-0G<BR>ISSUE TAG WN49657;[02] VERIFIED TASK COMPLETE<BR><BR>AUDIT C/W

ATA 5514

(DOT 152-1) LEFT HORIZONTAL STABILIZER GAP COVER 333AB; SLIDING SEAL IS CRACKED.<[01] REMOVE AND REPLACED LEFT HORIZONTAL STABILIZER GAP COVER 333AB; SLIDING SEAL I.A.W SRM STEP 4.<BR>ISSUE TAG WN49657;[02] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER GAP COVER 333AB; SLIDING SEAL I.A.W SRM STEP 4.<BR>ISSUE TAG WN49657;[03] VERIFIED TASK COMPLETE;[04] REMOVE AND REPLACED LEFT HORIZONTAL STABILIZER GAP COVER 333AB; SLIDING SEAL I.A.W SRM STEP 4.<BR>ISSUE TAG WN49657;[05] VERIFIED TASK COMPLETE<BR><BR>AUDIT C/W

ATA 5321

DOT#27 A-043 FLIGHT COMPARTMENT FLOOR PANEL 211AF HAS CORROSION ON BOTTOM FWD EDGE STA 259.5 BL 0 WL 208<[01] REPLACED IAW SRM 51-40-02-0G-0 & BOEING DWG: 141A631 REV: B<BR>ATAG: WN 49596<BR>P/N: 141A5133U15ATSMR0;[02] FAULT RESOLVED ON OTHER FAULT. SEE FAULT TTG8Q00Y4M96 WHERE PANEL WAS REMOVED AND REPLACED.;[03] VERIFIED STEP 2<BR>AUDIT CW

ATA 5311

MAIN CABIN STA 440 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H. REMOVED DAMAGE AND REPAIRED FRAME AT STA 440 S-8L IAW EA 25-153-00218.

ATA 5311

MAIN CABIN STA 380 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H. REPAIRED PER EA 25-153-00153 TTG8Q00YDMJL;[02] REPAIRED FRAME AT BS380; BETWEEN S-7L AND S-8L; IAW EA 25-153-00153.

ATA 5311

(DOT#147-48) MAIN CABIN STA 400 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H<[01] REPAIRED FRAME AT BS400; BETWEEN S-7L AND S-8L; IAW EA 25-153-00154.;[02] VERIFIED ITEM 1<BR>C/W;[03] C/W

ATA 5310

CABIN FWD WET AREA R1 CREASE BEAM CRRODED AT STA 312+15' LBL 60 WL 208<[01] REMOVED DAMAGE FROM CABIN FWD WET AREA R1 CREASE BEAM CORRODED AT STA 312+15' LBL 60 WL 208; FOUND IT OUT OF LIMITS ; ORIG T . ADJACENT TO BLEND .085'; LOSS .017'; REMOVED DAMAGED PART ;LOCATED; DRILLED;INSTALLED NEW R1 DOOR CREASE BEAM P/ N 6540004-134;A TAG# WN11061;APPLIED CIC ON NEW PART. IAW SRM 51-10-02; SRM 51-40-05; DWG # 141A8310; REV B; DWG # 141A8310; REV:-A; AMM 51-21-91.

ATA 5321

DOT L7-012: AFT CARGO COMPARTMENT FLOOR PANEL 140CF IS CORRODED AT FASTENER HOLES<[01] VERIFIED LIMITS ON AFT CARGO COMPARTMENT FLOOR PANEL 140CF; DISTANCE BETWEEN DAMAGE IS 2' (MINIMUM ALLOWABLE DISTANCE BETWEEN DAMAGE IS 5') THEREFORE IS FOUND OUT OF THE LIMITS; I.A.W. SRM 53-00-53-1A-1 VERIFIED MATERIAL WITH P/N: 2024-T3-071 AND AAR TAG# A274684 I.A.W. SRM 53-60-53-0I-1 FABRICATED NEW PANEL 140CF I/A/W AMM 25-52-01-201-801;[02] AUDIT C/W

ATA 5321

DOT L7-010: AFT CARGO COMPARTMENT FLOOR PANEL 140AF IS CORRODED AT FASTENER HOLES<[01] EVALUATED CORROSION ON AFT CARGO COMPARTMENT FLOOR PANEL 140AF; FOUND TOTAL ACCUMULATED CORROSION DAMAGE TO BE MORE THAN THE 20IN ALLOWED; OUT OF LIMITS IAW SRM 53-00-53-1A-1<BR>FABRICATION OF NEW PNL IAW AMM 25-52-01-201-801; TREATED IAW AMM 51-21-41-370-801 AND PRIMED IAW AMM 51-21-72-370-804<BR>(WORK ACCOMPLISHED BY SETH BYAS EMPLOYEE NUMBER 38482);[02] VERIFIED ITEM 1<BR><BR>AUDIT C/W

ATA 5321

FWD CARGO FLOOR PANEL 120CF HAS CORROSION AT FASTENER HOLES<[01] UPON FURTHER INVESTIGATION FOUND THAT CORROSION WAS 30 INCHES IN LENGTH WITH A MAX ALLOWED LENGTH OF 3 INCHES FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1; RECEIVED REPLACEMENT MATERIAL PN 2024-T3-.071 A TAG A276640 AND VERIFIED TO BE CORRECT REPLACEMENT MATERIAL IAW SRM 53-60-53-0I-1; FABRICATED NEW PANEL FOR 120CF IAW AMM 25-52-01-201-801; TREATED NEW PANEL IAW AMM 51-21-41-701 AND PRIMED NEW PANEL IAW AMM 51-21-72-370-804;[02] C/W<BR>AUDIT C/W

ATA 5320

(A204 DOT 78) FWD CARGO STA 492; RBL 21; WL 155; SPLASH SHIELD HAS CORROSION ON UPPER SURFACE<[01] REMOVED CORROSION AND VERIFIED WITH A 10-POWER MAGNIFYING GLASS ON FWD CARGO STA 492; RBL 21; WL 155; SPLASH SHIELD UPPER SURFACE I.A.W SRM 51-10-02-0G-0 VERIFIED LIMITS WITH ORIGINAL THICKNESS IS 0.032'; LOSS 0.006'; REMAINING 0.026' WERE THE MAXIMUM ALLOWED IS 0.10T ON ALLOWABLE DAMAGE; THEREFORE IS OUT OF LIMITS I.A.W SRM 53-30-15-1A-1 REMOVED DAMAGED SHIELD IAW SRM 51-40-02-0G-0 RECEIVED REPLACEMENT PART 143A8126-31 A TAG WN49564 AND VERIFIED TO BE CORRECT REPLACEMENT PART IAW BOEING DWG 143A0080 REV - LOCATED AND DRILLED SHIELD IAW BOEING DWG NUMBER 143A0080 REV - AND IAW SRM 51-40-05-0G-0 INSTALLED SHIELD IAW SRM 51-40-02-0G-0 AND IAW BOEING DWG 143A0080 REV-;[02] VERIFIED ITEM 1<BR>C/W;[03] C/W

ATA 5320

(A204 DOT 73) FORWARD CARGO STA 500 TO 500A; STR 26L; BAFFLE PLATE UNDER Z-ANGLE IS BUCKLED ON FORWARD SIDE.<[01] REMOVED AND INSTALLED NEW RIVETS AT FORWARD CARGO STA 500 TO 500A STR 26L BAFFLE PLATE UNDER Z ANGLE I/A/W SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] AUDIT C/W

ATA 5320

DOT#03 A-043 AFT CARGO COMPARTMENT DOOR SILL WEB CORRODED STA 807+3' TO 827+4' RBL 27 WL 156<[01] VERIFIED ALL NDT TASK COMPLETE;[02] 01 - REMOVED AND REPLACED AFT CARGO PIT LOWER DOOR SILL WEB PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)] AND BOEING DWG 146A8340 REV. -.;[03] VERIFIED TASK COMPLETE<BR><BR>AUDIT C/W

ATA 5320

DOT#14 A-043 AFT CARGO COMPARTMENT RH Z ANGLE CORRODED STA 727+4 TO 767 RBL 24 WL 156<[01] REMOVED CORRSION IAW SRM 51-10-02-0G-0; UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .032'; LOSS .009'; REMAINING .023'. TOOL#40084; DUE 06AUG25; EVALUATED AREA. ORGININAL THICKNESS 0.032'. LOSS 0.009'. REMAINING THICKNESS 0.023'. MAX. OF 10T ON ALLOWABLE DAMAGE. OUT OF LIMITS IAW SRM 53-00-53-1A-2; REMOVED RH Z ANGLE IAW 51-40-02-0G-0; VERIFIED MATERIAL WITH PN BAC1496-377 7075T6 A TAG A265296 IAW 53-60-53-0I-2; FABRICATED NEW PART IAW SRM 53-00-53-2R-5; TREATED IAW AMM 51-21-41-701 AND PRIMED IAW AMM 51-21-72-370-804NEW PART; FINISHED APPLYING PAINT IAW M-22-125-02598 STEP 1; APPLIED CIC UNDERNEATH RH Z ANGLE; APPLIED CIC ON TOP RH Z ANGLE IAW AMM 51-21-91-620-802; INSTALLED RH Z ANGLE IAW SRM 53-00-53-2R-5;[02] C/W<BR>AUDIT C/W

ATA 5320

FWD CARGO DOOR CUTOUT LOWER SILL WEB HAS EVIDENCE OF CORRION IN SEVERAL AREAS OF WEB<[01] 01 - REMOVED AND REPLACED PER SRM 53-30-15-1A-1-A00071.

ATA 5320

DOT#05 A-043 AFT CARGO COMPARTMENT FWD BKHD LOWER CENTER FAIRING ATTACH ANGLE TOP STRAP CORRODED STA 727+4' RBL 20 WL 156<[01] REPLACED (PLATE) AFT CARGO COMPARTMENT P/N453A2611-12 TAG#A289211 IAW IPC 25-52-10-02 INSTALLED ON W/O TTG8Q00WXN8W;[02] REPLACED (PLATE) AFT CARGO COMPARTMENT P/N453A2611-12 TAG#A289211 IAW IPC 25-52-10-02 INSTALLED ON W/O TTG8Q00WXN8W;[03] VERIFIED C/W

ATA 5320

DOT#07 A-043 AFT CARGO COMPARTMENT RH 'Z' ANGLE CORRODED STA 887+8 RBL 24 WL 156<[01] EVALUATED AREA. ORGININAL THICKNESS 0.032'. LOSS 0.012'. REMAINING THICKNESS 0.020'. MAX. OF 10T ON ALLOWABLE DAMAGE. OUT OF LIMITS IAW SRM 53-00-53-1A-2<BR>FABRICATED NEW Z ANGLE STA 887 TO STA 947 I.A.W. SRM 51-40-05-0G-0 AND I.A.W DWG 147A7501 REV A<BR>INSTALLED NEW RH Z ANGLE STA 887+8 RBL 24 WL 156 I.A.W. SRM 51-40-02-0G-0;[02] VERIFIED STEP 1<BR>AUDIT CW

ATA 5320

DOT#08 A-043 AFT CARGO COMPARTMENT FLOORBOARD 'T' STRAP CORRODED STA 727D RBL 2 WL 156<[01] REPLACED AFT CARGO COMPARTMENT FLOORBOARD 'T' STRAP P/N 146A9401-8 TAG#49635 IAW IPC 53-42-11-30 INSTALLED ON W/O TTG8Q00WXN8W;[02] VERIFIED ITEM 1<BR>C/W

ATA 5511

LH HORIZONTAL STAB LEADING EDGE 331B; LE STA 198.25; RIB IS BUCKLED AT AFT RADIUS.<[01] REMOVED L/H HORZ STAB L/E 331B RIB IAW SRM 51-40-02-0G-0 AND DWG 186A1001 REV A VERIFIED PART USING P/N 654A0004-685 ATAG A285988 AND DWG 186A1001 REV A INSTALLED RIB IAW SRM 51-40-02-0G-0 AND IAW BOEING DWG 186A1001 REV A.

ATA 5320

DOT#11 A-043 AFT CARGO COMPARTMENT LH Z ANGLE CORRODED STA 727E+14' TO 787+5' LBL 24 WL 156<[01] REMOVED CORRSION IAW SRM 51-10-02-0G-0<BR>UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .032'; LOSS .010'; REMAINING .022'. TOOL#40084; DUE 06AUG25<BR>EVALUATED AREA. ORGININAL THICKNESS 0.032'. LOSS 0.010'. REMAINING THICKNESS 0.022'. MAX. OF 10T ON ALLOWABLE DAMAGE. OUT OF LIMITS IAW SRM53-00-53-1A-2<BR>REMOVED; FABRICATED AND INSTALLED NEW AFT CARGO L/H Z ANGLE AT STA 727 TO 847 LBL 24 AND FABRICATED ONE SPLICE SIDEPLATE LOCATED ON 727E +9.5' I.A.W. SRM 53-00-53-2R-6 DWG 146A7500 REV A<BR><BR>PERFORMED BY JOSE TORRES #38397;[02] AUDIT C/W

ATA 5320

DOT#10 A-043 AFT CARGO COMPARTMENT LH Z ANGLE CORRODED STA 727E+6' TO 727D+3' LBL 24 WL 156<[01] REMOVED CORRSION IAW SRM 51-10-02-0G-0<BR>UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .032'; LOSS .013'; REMAINING .019'. TOOL#40084; DUE 06AUG25<BR>EVALUATED AREA. ORGININAL THICKNESS 0.032'. LOSS 0.013'. REMAINING THICKNESS 0.019'. MAX. OF 10T ON ALLOWABLE DAMAGE. OUT OF LIMITS IAW SRM 53-00-53-1A-2<BR><BR>ACCOMPLISHED LH Z ANGLE REPAIR ON TASK CARD TTG8Q00Y0N4K<BR><BR><BR>PERFORMED BY JOSE TORRES#38397;[02] VERIFIED ITEM 1<BR>AUDIT C/W

ATA 5320

DOT#13 A-043 AFT CARGO COMPARTMENT RH FWD SHIELD CORRODED STA 767 TO 787 RBL 24 WL 156<[01] REMOVED CORRSION ON TOP SIDE OF SHIELD IAW SRM 51-10-02-0G-0 EVALUATED AREA. ORGININAL THICKNESS 0.050'. LOSS 0.010'. REMAINING THICKNESS 0.040'. MAX. OF 10T ON ALLOWABLE DAMAGE. OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVED RH FWD SHIELD IAW SRM 51-40-02-0G RECEIVED REPLACEMENT PART PN 146A8127-12 A TAG WN49588 AND VERIFIED IT TO BE CORRECT PART IAW BOEING DWG 146A0081 REV- LOCATED AND DRILLED SHIELD IAW SRM 51-40-05-0G-0 AND IAW BOEING DWG 146A0081 REV- INSTALLED SHIELD IAW SRM 51-40-02-0G-0 AND IAW BOEING DWG 146A0081 REV-;[02] VERIFIED ITEM 1;[03] AUDIT C/W

ATA 5511

(A204 DOT 64) LH HORIZONTAL STAB LEADING EDGE 331B; LE STA 114.5; RIB IS CRACKED NEXT TO BEND RADIUS AT LOWER AFT HOLE.<[01] REMOVED L/H L/E HORZ STAB RIB AT STA114.5 IAW SRM 51-40-02-0G-0 AND DWG 186A1305 REV - VERIFIED PART USING P/N 186A1352-9 AND ATAG WN49531 AND DWG 186A1305 REV - LOCATED AND DRILLED L/H L/E HORZ STAB IAW SRM 51-40-02-0G-0 AND DWG 186A1305 REV - INSTALLED RIB IAW SRM 51-40-02-0G-0 AND IAW BOEING DWG 186A1305 REV -;[02] VERIFIED ITEM 1<BR>C/W;[03] C/W

ATA 5220

(A204 DOT 60) LEFT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK HAS MINOR CORROSION<[01] LEFT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK WAS REMOVED AND REPLACED I.A.W. AMM 25-61-10-400-802-NG<BR><BR>TOOL USED: STAAR 39119; DUE 03/03/25;[02] VERIFIED STEP 1<BR>AUDIT CW

ATA 2560

(A204 DOT 59) RIGHT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK HAS MINOR CORROSION<[01] 01 - REMOVED AND REPLACED R/H EMERGENCY EXIT DOOR LIFE LINE PER [AMM 25-61-10-400-802-NG (EMERGENCY EXIT DOOR LIFE LINE INSTALLATION - PERMANENT)]<BR><BR>STRAP P/N: 416A1531-17<BR>TAG: WN 49634<BR><BR>USED TOOL: ST AAR 39119<BR>DUE DATE: 03/03/25;[02] VERIFIED STEP 1<BR>COMPLETE <BR>AUDIT C/W

ATA 3350

EMERGENCY EXIT LIGHT ON FWD LAVATORY IS CRACKED<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT ON FWD LAVATORY IAW AMM 33-51-01-960-802 STEP 3A-3C(1-4)(5)(D) (6)(7)(10)(12).<BR>SIGNING FOR JOSEPH KREBS EMP#38394;[02] REMOVED AND REPLACED EMERGENCY EXIT LIGHT ON FWD LAVATORY IAW AMM 33-51-01-960-802 STEP 3A-3C(1-4)(5)(D) (6)(7)(10)(12). OPS CHECK GOOD<BR>SIGNING FOR JOSEPH KREBS EMP#38394;[03] VERIFIED STEPS 1 AND 2<BR>COMPLETE<BR>AUDIT C/W

ATA 5321

154-06 PASSENGER CABIN FLOOR BOARD 241AF HAS MULTIPLE AREAS OF PULLED FIBERGLASS ON SURFACE<[01] 'REFER TO FAULT TTG8Q00XXV53 WHERE EA 25-153-00035 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/W

ATA 5321

154-05 PASSENGER CABIN FLOOR BOARD 231XF HAS MULTIPLE AREAS OF PULLED FIBERGLASS FROM TAPE REMOVAL. REFER TO FAULT TTG8Q00XXV53 WHERE EA 25-153-00035 WAS ADDED AS A SUBTASK.

ATA 5321

154-10 PASSENGER CABIN FLOOR BOARD 232SF HAS MULTIPLE DENTS AND PULLED FIBERGLASS ON UPPER SURFACE<[01] 'REFER TO FAULT TTG8Q00XXV53 WHERE EA 25-153-00035 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/W

ATA 5320

FWD CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED<[01] CRACK ON FWD CARGO DOOR FWD CORNER SCUFF PLATE WAS REPIARED ON BACK SHOP WORK ORDER 46301/1400/0001 SERIAL NO: 9519433 IAW SRM 53-30-15-2R-1 (WELD REPAIR);[02] VERIFIED ITEM 1<BR><BR>AUDIT C/W

ATA 5321

154-15 PASSENGER CABIN FLOOR BOARD 242DF HAS MULTIPLE DENTS AND PULLED FIBERGLASS ON SURFACE<[01] 'REFER TO FAULT TTG8Q00XXV53 WHERE EA 25-153-00035 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/W

ATA 5350

R/H WING TO BODY FAIRING PANEL 191AR AFT EDGE; CENTER ATTACH BEAM IS CRACKED AT UPPER END.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] VERIFIED STEP 1<BR>AUDIT CW

ATA 5754

R/H WING # 5 SLAT LOWER CENTER WEDGE HAS CRACK ON EDGE OF WEDGE. REMOVED R/H WING # 5 SLAT LOWER CENTER WEDGE IAW SRM 51-40-02-0G-0. UT IAW B737 NDT PART 4; 51-00-01. NO ADDITIONAL DEFECTS NOTED. TOOL#31896; DUE 29APR25. EVALUATED AND FOUND SMALL CRACK AT CENTER OF FLEX SKIN AS MARKED. FOUND TO BE REPAIRABLE FOR 250 DEGREE PRE-PREG LAY UP IAW SRM 57-42-01-2R-13 AND SRM 51-70-05-2R-0 REPAIR GENERAL.REMOVED DAMAGE & TAPER SANDED IAW SRM 57-42-01-2R-13 STEP 4 E-H. VERIFIED MATERIAL IAW SRM 57-42-01-2R-13 STEP 4 I-J. BONDED REPAIR IAW SRM 57-42-01-2R-13 STEP 4 J-U AND SRM 51-70-05-2R-0 REPAIR GENERAL LWR AND UPPER SURFACE AT 250 DEGREES FOR 90 MINUTES EACH SIDE (OVEN B0-06 EXP 4-25-25). UT IAW B737 NDT PART 4; 51-00-01. NO DEFECTS NOTED. SEALED TOOL SIDE AROUND REPAIR IAW SRM 57-42-01-2R-13 STEP 4 (X)(1-2). EC3501 (B108904). APPLIED ANTI-STATIC IAW SRM 57-42-01-2R-13 STEP 4(X)(3) AND SOPM 20-10-06. APPLIED PRIMER BMS 10-103 (A275086) IAW SRM 57-42-01-2R-13 STEP 4 (X)(4). APPLIED DECORATIVE FINISH IAW SRM 57-42-01-2R-13 STEP 4 (X)(5). PAINT. APPLIED TOPCOAT PAINT IAW SRM 57-42-01-2R-13 AND AMM 51-21-99-701.

ATA 5754

(A-204 DOT 29) LH WING FIXED LEADING EDGE CAVITY. FORWARD EDGE OF KRUEGER FLAP CUTOUT. NOSE BEAM HAS CORROSION IN RADIUS FROM #1 KRUEGER FLAP 2ND FROM I/B HINGE TO #2 KRUEGER FLAP 2ND FROM I/B HINGE<[01] REMOVED DAMAGE AND REPAIRED PER EA 25-157-00351;[02] COMPLETE<BR>AUDIT C/W

ATA 5710

(A204 DOT 3) #1 FLAP TRACK FORWARD FAIRING. INNTER FORWARD MOUNT PLATE HAS EVIDENCE OF CORROSION<[01] 04 - REPAIRED PER [SRM 57-53-71-1A-1-A00978 (PERMANENT (NON-DENT DAMAGE TYPES))];[02] COMPLETE<BR>AUDIT C/W

ATA 3350

L1 DOOR AND R/H MID EMERGENCY EXIT SIGN SEVERAL LAMPS INOP<[01] R&R SEVERAL LAMPS ON L1 DOOR AND R/H EMERGENCY DOOR EXIT SIGNS PER AMM 33-51-01. OPS CHECK GOOD.

ATA 3350

L1 DOOR AND R/H MID EMERGENCY EXIT SIGN SEVERAL LAMPS INOP<[01] R&R SEVERAL LAMPS ON L1 DOOR AND R/H EMERGENCY DOOR EXIT SIGNS PER AMM 33-51-01. OPS CHECK GOOD.

ATA 3350

L2 EMERGENCY LIGHT INOP.<[01] RELAMPED; REF. AMM 33-51-04. NO FIX. SWAPPED POWER SUPPLIES M1672 AND M1673; REF. AMM 33-51-06. NO FIX. SWAPPED BACK TO ORIGINAL. CHECK CONTINUITY FROM D10746 TO GND; REF. WDM 33-51-14-6. GOOD CONTINUITY. REQUIRES MORE T/S; SHORT-TO-GROUND MOST LIKELY.;[02] RE-INSTALLED L2 EMERGENCY LIGHT REF AMM 33-51-04. OPS CHECKS GOOD.

ATA 3350

L2 EMERGENCY LIGHT LENS ASSEMBLY MISSING 1 SCREW.<[01] REPLACED MISSING SCREW IAW SIP.

ATA 5320

LH UPPER CENTER INTERCOSTAL FLOOR SUPPORT CRACKED ABOVE AIR CONDITIONING DISTRIBUTION BAY STA. 540<[01] REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02.

ATA 2565

L1 DOOR SLIDE HAS SLIDE LATCHING MECHANISM TO BEZEL DAMAGED.<[01] REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE IAW MT 725-61-06-FE.

ATA 2560

FWD SERVICE GIRT BAR BRACKET BROKEN<[01] R&R GIRT BAR RETAINING BRACKET FASTENER PER SRM 51-40-02. SLIDE REMOVAL NOT REQUIRED.

ATA 2560

FWD SERVICE DOOR GIRT BAR BRACKET BROKEN.<[01] MADE TEMPORARY REPAIR PER EA M-23-125-01839. PERMANENT REPAIR DUE BY 11/30/23. OK TO CONTINUE PER M-23-125-01839TLD. A/C OK FOR SERVICE.

ATA 3350

INOP EMERGENCY LIGHT FWD ENTRY DOOR; FWD GALLEY; STOWAGE BIN 3 RH; EME RGENCY DOOR LH(2EA) AT PASSENGER CABIN 2023-238132<[01] PERFORMRD FIM 33-50 TASK 801 AND FOUND BURNED FUSE (3 3/A) ON POWER SUPPLY ;WERE REPLACED IAW B737-700 AMM 33-51-06-960-804 AND PERFORMED OPERATIONAL TEST EMERGENCY LIGHT IAW B737-700 AMM 33-51-00-710-801 AND TEST IS OK.;[02] PERFORMRD FIM 33-50 TASK 801 AND FOUND BURNED FUSE (3 3/A) ON POWER SUPPLY ;WERE REPLACED IAW B737-700 AMM 33-51-06-960-804 AND PERFORMED OPERATIONAL TEST EMERGENCY LIGHT IAW B737-700 AMM 33-51-00-710-801 AND TEST IS OK.

ATA 2560

PASSENGER CABIN R1 DOOR SLIDE BAR HARD TO EXTEND AND CONNECT TO THE FLOOR 2023-238139<[01] INSTALLED CORRECTLY ESCAPE SLIDE FWD SERVICE DOOR IAW SWA TASK MT 725-61-06; STEP 3K(2)(3);[02] TASK CARD COMPLETE.

ATA 5714

CRACK BODY STA 663.75 ANGLE UPPER POSITION LBL 43 AT AIR CONDITIONING BAY 2023-238062<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23.;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220272712; DUE DATE: 17-DEC-23;[03] REPAIRED ANGLE UPPER POSITION STA 663.75 BTW LBL 25 TO LBL 65. IAW B737-700 SRM 57-10-10-2R-5 REPAIR 5 AND SRM 51-40-02; AND DWG 111A1000 REV.-. SEE INDIVIDUAL SIGN OFF BELOW.;[04] RII ITEM <BR>REPAIRED ANGLE UPPER POSITION STA 663.75 BTW LBL 25 TO LBL 65. IAW B737-700 SRM 57-10-10-2R-5 REPAIR 5 AND SRM 51-40-02; AND DWG 111A1000 REV.-. SEE INDIVIDUAL SIGN OFF BELOW.

ATA 5710

CORROSION WEB LOC ON FUELING STATION INTERNAL AREA OF PANEL 621GB AT RT WING 2023-238059<[01] REPLACED REFUEL STATION PANEL AND PERFORMED OPERATIONAL TEST IAW B737-700 AMM 28-41-61-400-801 TEST IS OK<BR>SEE INDIVIDUAL SIGN OFF STEP BELOW;[02] CORRECTED STEP 1<BR>REPLACED REFUEL STATION PANEL AND PERFORMED OPERATIONAL TEST IAW B737-700 AMM 28-41-61-000-801 AND AMM 28-41-61-400-801 TEST IS OK<BR>SEE INDIVIDUAL SIGN OFF STEP BELOW;[03] REPLACED REFUEL STATION PANEL AND PERFORMED OPERATIONAL TEST IAW B737-700 AMM 28-41-61-000-801 AND AMM 28-41-61-400-801 TEST IS OK <BR>SEE INDIVIDUAL SIGN OFF STEP BELOW<BR>TASKCARD COMPLETED

ATA 5753

BROKEN ACCESS PANEL 651GB SUPPORT ANGLE AT RT WING 2023-238052<[01] REPLACED SUPPORT ANGLE AT RT WING LOC. ON ACCESS PANEL 651GB IAW B737-700 SRM 51-10-02 ITEM 9;[02] CORRECTED STEP 1 <BR>REPLACED SUPPORT ANGLE AT RT WING LOC. ON ACCESS PANEL 651GB IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[03] REPLACED SUPPORT ANGLE AT RT WING LOC. ON ACCESS PANEL 651GB IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02

ATA 5720

CRACK INBOARD TRAILING EDGE CORRUGATED PLATE IRSS 215 AT RT WING 2023-237955<[01] REPLACED CORRUGATED PLATE LOC. IRSS 215 AT RT WING AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 . SEE INDIVIDUAL SIGN OFF BELOW.;[02] COMPLETE TASK CERTIFIED

ATA 5310

CRACK ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 LBL47 AT FWD GALLEY AREA 2023-237856<[01] REPLACED INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 LBL47 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET 26; REV:- SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] REPLACED INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 LBL47 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET 26; REV:- SEE INDIVIDUAL SIGN-OFFS BELOW. RII Ï¿½TEM

ATA 5512

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.500 INCH 2023-237925<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X1210V022240; DUE DATE: 12 MAR 24.;[02] PERFORMED REPAIR LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. I.A.W B737-700 55-10-01-2R-11 REPAIR 11; SEE INDIVIDUALS SIGN-OFF BELOW;[03] RII ITEM <BR>PERFORMED REPAIR LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. I.A.W B737-700 55-10-01-2R-11 REPAIR 11; SEE INDIVIDUALS SIGN-OFF BELOW

ATA 5320

CRACK ANGLE LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT 2023-237904<[01] REPLACED ANGLE LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT IAW B737 -700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 143A7505 SHEET 2 REV: B SEE INDIVIDUAL SIGNOFFS BELOW.;[02] RII ITEM <BR>REPLACED ANGLE LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT IAW B737 -700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 143A7505 SHEET 2 REV: B SEE INDIVIDUAL SIGNOFFS BELOW.

ATA 5310

CRACK ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 328 TO BS 344 LBL47 AT FWD GALLEY AREA 2023-237863<[01] REPLACED INTERCOSTAL WEB AND FASTENERS LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL47 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET 44; REV:- SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] REPLACED INTERCOSTAL WEB AND FASTENERS LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL47 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET 44; REV:- SEE INDIVIDUAL SIGN-OFFS BELOW.RII Ï¿½TEM

ATA 5315

CORROSION ON FLOOR BEAM 986.5 RBL 44 WL 208.1 AT AFT GALLEY AREA 2023-237792<[01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN 220272712; DUE DATE 17-DEC-23;[02] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 RBL44 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4 FIGURE 205; SHEET 1;2 AND 3. SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

ATA 5315

CORROSION ON FLOOR BEAM 986.5 LBL 44 WL 208.1 AT AFT GALLEY AREA 2023-237791<[01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN 220272712; DUE DATE 17-DEC-23;[02] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 LBL44 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4 FIGURE 205; SHEET 1;2 AND 3. SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

ATA 5320

CRACK ON INTERCOSTAL LOCATED FWD ENTRY DOOR CUTOUT BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2023-237784<[01] REPLACED INTERCOSTAL LOCATED FWD ENTRY DOOR CUTOUT BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9 DWG 141A8180 SHEET 27 REV C. AND DWG 141A8180 SHEET 28 REV C. <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] JOB COMPLETED AND CERTIFIED RII.

ATA 5315

CRACK ON FLOOR BEAM LOCATED BS 294.5 AT LEVEL STR 17R RBL 53 AT FWD GALLEY AREA 2023-237816<[01] TOOL USED: EDDY CURRENT EQUIPMENT ; P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 27-MAR-24;[02] TOOL USED: RADIOMETER/PHOTOMETER P/N: XRP-3000; S/N:1859843; CAL DUE DATE: 04-MAY-23;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[04] RADIOMETER PHOTOMETER P/N XRP-3000 S/N 1859843 DUE DATE 04-MAY-23;[05] REPAIRED FLOOR BEAM BS 294.5 AT LEVEL STR 17R BTW RBL 14 TO RBL 60 IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16. SEE INDIVIDUAL SIGNOFFS BELOW;[06] REPAIRED FLOOR BEAM BS 294.5 AT LEVEL STR 17R BTW RBL 14 TO RBL 60 IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16. SEE INDIVIDUAL SIGNOFFS BELOW COMPLETE TASK CERTIFIED RII

ATA 5310

CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-237783<[01] REPLACED TIE CLIP AND FASTENERS LOC. ON BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; DWG 141A1110 SHEET 18; REV - AND DWG 143A8380 SHEET 21; REV -. SEE INDIVIDUAL SIGN-OFF BELOW;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

ATA 5311

CRACK ON STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R RBL 53 AT FWD GALLEY AREA 2023-237787<[01] TOOL USED EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220273012; DUE DATE: 17-DEC-23.;[02] REMOVED DAMAGE ON STUB FRAME LOC. BTW BS291.5 TO BS 294.5 AT LEVEL STR 17R RBL 53 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND B737-700 SRM 53-10-15-2R-7 REPAIR 7.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[03] REMOVED DAMAGE ON STUB FRAME LOC. BTW BS291.5 TO BS 294.5 AT LEVEL STR 17R RBL 53 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND B737-700 SRM 53-10-15-2R-7 REPAIR 7. <BR>SEE INDIVIDUAL SIGN-OFF BELOW.AS RII. JOB COMPLETED.

ATA 2560

DETERIORATED GIRT BAR FITTING SLEEVE (4 E/A) ON FLOOR PANEL 242UF AT AFT GALLEY AREA 2023-237740<[01] REPLACED GIRT BAR FITTING SLEEVE (4 E/A) ON FLOOR PANEL 242UF AT AFT GALLEY AREA AND CURED EPOXY ADHESIVE ON SLEEVES OF FLOOR PANEL IAW B737-700 SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 5.S (1). APPLIED EPOXY ADHESIVE LOCAL TIME 20:00. TOOL USED: BÏ¿½SCULA; P/N: 91847; S/N: AE-409320; DUE DATE: 09/JUN/23.;[02] REPLACED GIRT BAR FITTING SLEEVE (4 E/A) ON FLOOR PANEL 242UF AT AFT GALLEY AREA AND CURED EPOXY ADHESIVE ON SLEEVES OF FLOOR PANEL IAW B737-700 SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 5.S (1). APPLIED EPOXY ADHESIVE LOCAL TIME 20:00. TOOL USED: BÏ¿½SCULA; P/N: 91847; S/N: AE-409320; DUE DATE: 09/JUN/23.

ATA 5720

CRACK TRAILING EDGE DEFLECTION SUPPORT ANGLE LOCATED ORSS 261 PLUS 9 INCHES APROX AT RT WING 2023-237732<[01] REPLACED DEFLECTION SUPPORT ANGLE LOCATED ORSS 261 PLUS 9 INCHES APROX AT RT WING I.A.W B737-700 SRM 51-10-02 ITEM 9.;[02] TASK CARD COMPLETED

ATA 5720

CRACK TRAILING EDGE DEFLECTION CONTROL SUPPORT ANGLE LOCATED ORSS 261 PLUS 18 INCHES APROX. AT RT WING. REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE DEFLECTION CONTROL; ORSS 261 PLUS 18 INCHES APROX. AT RT WING IAW SRM 51-10-02 ITEM 9 AND DRAWING 115A6200 SHEET 10 REV -.

ATA 5730

DELAMINATED ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2023-237730<[01] TOOL USED: CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27-DEC-23.;[02] TOOL USED SCALE P/N SPX601 S/N 8340225441 DUE DATE 20 JUL 23;[03] TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18196127 DUE DATE: 22-JAN-24;[04] TOOL USED: SCALE PN: SPX621 SN: 8340225441 DUE DATE:20-JUL-23;[05] TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18175478 DUE DATE: 24-SEP-23;[06] TOOL USED; MULTIMETER P/N: FLUKE 1587 ; S/N: 18820026 ; DUE DATE: 28-MAR-24.;[07] REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.SEE INDIVIDUAL SIGNOFF BELOW.;[08] TASK COMPLETED

ATA 2560

DETERIORATED GIRT BAR FITTING HARDWARE LT AND RT AT FWD GALLEY AREA 2023-237710<[01] REPLACED GIRT BAR FITTING HARDWARE LT AND RT AT FWD GALLEY AREA IAW SOPM 20-50-01 REV 38;[02] REPLACED GIRT BAR FITTING HARDWARE LT AND RT AT FWD GALLEY AREA IAW SOPM 20-50-01 REV 38; INSTALLATION IS DOCUMENTED ON TASK CARD 725-025-00-01Y; TTG8Q002DY7N STEP 33.;[03] TASK COMPLETED

ATA 5320

CRACK ON SUPPORT ANGLE LOCATED CEILING AREA OF BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2023-237749<[01] REPLACED SUPPORT ANGLE LOCATED CEILING AREA OF BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A7901 SHEET 18; REV:-.;[02] CORRECTED STEP 1<BR>REPLACED SUPPORT ANGLE LOCATED CEILING AREA OF BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A7901 REV. -;[03] REPLACED SUPPORT ANGLE LOCATED CEILING AREA OF BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A7901 REV. -

ATA 5511

CRACK INSPAR RIB 129.50 AT 19 INCHES FRONT SPAR LT HORIZONTAL STAB 2023-237689<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC500D; S/N: N500X12101V022235; CAL DUE DATE: 03-AUG-23;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[03] PEFORMED PERMANENT REPAIR ON INSPAR RIB 129.50 AT 19 INCHES FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. SEE INDIVIDUAL SIGNOFFS BELOW;[04] PEFORMED PERMANENT REPAIR ON INSPAR RIB 129.50 AT 19 INCHES FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. SEE INDIVIDUAL SIGNOFFS BELOW CERTIFIED RII

ATA 5511

CRACK INSPAR RIB 111.10 AT 28 INCHES FRONT SPAR LT HORIZONTAL STAB 2023-237687<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022237; DUE DATE: 26-JAN-24.;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N:220272712; CAL DUE DATE: 17-DEC-23;[03] REPAIRED INSPAR RIB 111.10 AT 28 INCHES FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4; FIGURE 202; SHEET 1. SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED INSPAR RIB 111.10 AT 28 INCHES FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4; FIGURE 202; SHEET 1. <BR><BR>RII ACCOMPLISHED <BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.

ATA 5753

CRACK ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 272 LT WING 2023-237685<[01] REPLACED ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 272 LT WING AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 115A2930 REV. ?-?. MEASURE OF CRACK IS: L=.0.254?. TOOL USED: DIGITAL CALIPER. P/N: 500-752-20. S/N: B21014945. DUE DATE: 08/NOV/23.;[02] CERTIFIED WORK PERFORMED.

ATA 5753

CRACK CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 231 AT LT WING 2023-237690<[01] REPLACED CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 231 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SING-OFF BELOW.;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

ATA 5753

CRACK CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 215 LT WING 2023-237688<[01] REPLACED CORRUGATED PLATE AND FASTENERS INBOARD TRAILING EDGE IRSS 215 LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG #115A2001 SHETT:34 REV: -.;[02] REPLACED CORRUGATED PLATE AND FASTENERS INBOARD TRAILING EDGE IRSS 215 LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG #115A2001 SHEET:34 REV: -.

ATA 5753

CRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 LT WING 2023-237691<[01] REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE ORSS 261 LT WING. IAW B737 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 115A2001 SHEET 32 REV: -;[02] REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE ORSS 261 LT WING. IAW B737 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 115A2001 SHEET 32 REV: -

ATA 5753

CRACK TRAILING EDGE BRACKET DEFLECTION CONTROL RIB ORSS 272 AT LT WING 2023-237686<[01] REPLACED BRACKET DEFLECTION CONTROL RIB ORSS 272 AT LT WING IAW B737-700 SRM: 51-10-02 ITEM 9.;[02] TASK CARD COMPLETED

ATA 3350

INOP BATTERY PACK ON POWER SUPPLY M1669 2023-237680<[01] REMOVED AND INSTALLED BATTERY PACK ON POWER SUPPLY M1669 IAW B737-700 AMM 33-51-06-960-805. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REMOVED AND INSTALLED BATTERY PACK ON POWER SUPPLY M1669 IAW B737-700 AMM 33-51-06-960-805. SEE INDIVIDUAL SIGN OFF BELOW.

ATA 5320

CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2023-237601<[01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N B20189510; DUE DATE 26-DEC-23;[02] TOOL USED RADIOMETER P/N: XRP-3000; S/N: 1858843; DUE DATE: 04-MAY-23.;[03] REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-30-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] TASK COMPLETED.

ATA 2565

DETERIORATED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE AT AFT GALLEY AREA 2023-237613<[01] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE AT AFT GALLEY AREA IAW SOPM 20-50-01 REV 38;[02] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE AT AFT GALLEY AREA IAW SOPM 20-50-01 REV 38; INSTALLATION IS DOCUMENTED ON TASK CARD 725-025-00-02Y TTG8Q002DY4W STEP 33;[03] TASK COMPLETED

ATA 5320

CRACK SCUFF PLATE ON AFT CORNER AT AFT CARGO COMPARTMENT 2023-237595<[01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N B20189510; DUE DATE 26-DEC-23;[02] TOOL USED RADIOMETER P/N: XRP-3000; S/N: 1858843; DUE DATE: 04-MAY-23.;[03] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] TASK COMPLETED.

ATA 5320

CRACK GUSSET LOCATED BS 500D AT LEVEL STR 19L FWD CARGO COMPARTMENT 2023-237582<[01] REPLACED GUSSET AND FASTENER ON STRINGER 19L BS500D IAW B737-700 SRM 51-10-02 ITEM 9;[02] CORRECTED ITEM 1.<BR>REPLACED GUSSET AND FASTENER ON STRINGER 19L BS500D IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7902 SHEET 174 REV.?. SEE INDIVIDUAL SIGNOFFS BELOW;[03] CORRECTIVE ACTION STEP 2 CERTIFIED RII

ATA 5320

CRACK SUPPORT ANGLE LOCATED BS 695 LBL 24.75 AT CENTER SECTION 2023-237536<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] REPLACED SUPPORT ANGLE LOCATED BS 695 LBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9; AND B737-700 DWG 273A9110 SHEET: 6 REV: A.SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] REPLACED SUPPORT ANGLE LOCATED BS 695 LBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9; AND B737-700 DWG 273A9110 SHEET: 6 REV: A.SEE INDIVIDUAL SIGN-OFFS BELOW.

ATA 5320

CRACK SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT CENTER SECTION 2023-237537<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] REPLACED SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-10-02; ITEM 9 AND B737-700 DWG 273A9110 SHEET: 6; REV: A. SEE INDIVIDUAL SIGN-OFF BELOW BELOW.;[03] REPLACED SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-10-02; ITEM 9 AND B737-700 DWG 273A9110 SHEET: 6; REV: A. SEE INDIVIDUAL SIGN-OFF BELOW BELOW.

ATA 3350

INOP EMERGENCY EXIT LIGHT 231YJW BALLAST LT SIDE AT PASSENGER CABIN (1 EA) 2023-237524<[01] REPLACED EMERGENCY EXIT LIGHT 231YJW BALLAST LT SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-21-00-960-802 STEP 7. C. (4) TO 7. C. (6) PERFORMED OPERATIONAL TEST; IS OK <BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] COMPLETE TASK CERTIFIED

ATA 5320

CRACK WEB - INTERCOSTAL LOCATED BTW BS 500A TO BS 500B AT LEVEL STR 26R FWD CARGO COMPARTMENT 2023-237540<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS 500A TO BS 500B AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 53-30-53-2R-1 REAPIR 1. SEE INDIVIDUAL SING-OFF BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS 500A TO BS 500B AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SING-OFF BELOW.;[03] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS 500A TO BS 500B AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SING-OFF BELOW. AS RII

ATA 5320

CRACK ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26R FWD CARGO COMPARTMENT 2023-237539<[01] REPLACED ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737 -700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 143A7505 SHEET 6 REV ?D SEE INDIVIDUAL SIGNOFFS BELOW.;[02] RII ITEM <BR>REPLACED ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737 -700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 143A7505 SHEET 6 REV ?D SEE INDIVIDUAL SIGNOFFS BELOW.

ATA 3350

INOP EMERGENCY EXIT LIGHT 232YJW BALLAST RT SIDE AT PASSENGER CABIN (1 EA) 2023-237523<[01] REPLACED EMERGENCY EXIT LIGHT 232YJW BALLAST RT SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-21-00-960-802 STEP 7. C. (4) TO 3. C. (6) PERFORMED OPERATIONAL TEST; IS OK <BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] COMPLETE TASK CERTIFIED

ATA 5312

CUSTOMER REQUEST CRACK ON RH SIDE VAPOR BARRIER LOCATED AT MAIN WHEEL WELL COMPARTMENT 2023-237509<[01] TOOL USED CALIPER P/N:8647A42 S/N:B22058354 DUE DATE:27-AUG-23.;[02] TOOL USED:HOT BONDER P/N:HCS9200B S/N:15102320 DUE DATE:22-JAN-24.;[03] TOOL USED SCALE P/N 91847; S/N AE-409320; DUE DATE: 06-JUN-23.;[04] REPAIRED VAPOR BARRIER OF RH SIDE AT MAIN WHEEL WELL COMPARTMENT ON RBL 31.83 LOWER POSITION IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW;[05] REPAIRED VAPOR BARRIER OF RH SIDE AT MAIN WHEEL WELL COMPARTMENT ON RBL 31.83 LOWER POSITION IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.AS RII. JOB COMPLETED.

ATA 3350

FWD EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED FWD EMERGENCY LIGHT M1675 BATTERY PACK REF B737 AMM 33-51-06 OP/C GOOD

ATA 3350

OVERHEADBIN EMERGENCY LIGHT AT 4ABC ONE LIGHT INOP; RELAMP NO HELP. OK TO CONTINUE PER MEL 33-15-02; SP1B<BR>NIS FOR PARTS;[02] MX REMOVED AND REPLACED OVERHEAD BIN EMERGENCY LIGHT ASSEMBLY AT 4 ABC PER AMM 33-51-03

ATA 3350

EMERGENCY LIGHT INOP ROWS 1-8 LH SIDE. REMOVED AND REPLACED EMERGENCY LIGHT POWER PACK AND BATTERY M1668 REF B737 AMM 33-51-06 OP/C IS GOOD

ATA 3350

EMERGENCY LIGHT INOP ROWS 1-8 LH SIDE. REMOVED AND REPLACED EMERGENCY LIGHT POWER PACK AND BATTERY M1668 REF B737 AMM 33-51-06 OP/C IS GOOD

ATA 5510

RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED / [01] REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL PER AMM 53-31-31

ATA 5314

KEEL BEAM PANEL #192E L/H FWD ATTACH BRACKET CRACKED / [01] REMOVED AND REPLACED ATTACH BRACKET PER SRM 51-40-02

ATA 5510

LEFT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED / [01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL PER AMM 53-31-31.

ATA 3350

6ABC EMERGENCY LIGHT LENS IS NOT SECURE; FALLING FROM THE LIGHT ASSY. 6ABC EMERGENCY LIGHT LENS IS NOT SECURE FALLING FROM THE LIGHT ASSY. / [01] RESECURED LENS REF AMM 33-51-03

ATA 5210

ASSIST HANDLE NEAR L2 DOOR BROKEN. / [01] R&R L2 DOOR ASSIST HANDLE PER A.M.M. 52-13-31.

ATA 3410

AIRSPEED UNRELIABLE ABOUT 1000 AGL; CAPR SIDE 5 KNTS SLOW DETERMINED STBY AIRSPEED AND F.O. AIRSPEED WAS RELIABLE. LANDED OVERWEIGHT AT 135.O / [01] ACCOMPLISHED VISUAL INSP OF CAPTAIN?S PITOT PROBE FOUND WHAT APPEARED TO BE INSECT REMAINS STUCK IN PROBE; ACCOMPLISHED SATISFACTORY PITOT SYSTEM FLUSH AND LEAK TEST PER AMM 34-11-00. OPS AND LEAK CHECKED GOOD. ALSO ACCOMPLISHED OVERWEIGHT LANDING INSP PER AMM 05-51-35. NO DAMAGE FOUND.

ATA 3350

3 EMERGENCY LIGHTS ARE INOP. ROW 20CBA OVERHEAD BIN; AFT ENTRY SIDE WALL LIGHT; AND AFT ENTRY EXTERIOR LIGHT. / [01] REMOVED AND REPLACED LT AFT BATTERY PACK. OPS CHECKS GOOD. IN REF TO AMM 33-51-06.

ATA 5750

LH WING TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB CRACKED. / [01] ACCOMPLISHED STEP 4A THRU 4R AND STARTED TO INSTALL REPAIR PER SRM REPAIR 57-51-02-2R-3.;[02] ACCOMPLISHED PERMANENT REPAIR REF SRM 57-51-02-2R-3

ATA 5753

SEAL RIB UNDER RIGHT WING INBOARD TRAILING EDGE CRACKED / [01] REMOVED AND INSTALLED SEAL RIB UNDER RIGHT WING INBOARD TRAILING EDGE. REF SRM 51-40-02

ATA 5321

193D PNL HAS FIBERGLASS DELAMINATION ON INSIDE TRAILING EDGE ; / [01] INSTALLED NEW PANEL (193D) PER AMM 53-21-21

ATA 5350

194E PNL HAS 2 FASTENER HOLES ELONGATED AND 2 DIMPLED AND CRACKED FASTENER HOLES. ; / [01] INSTALLED NEW PANEL (194E) PER AMM 53-51-21

ATA 5350

193D PNL HAS 8 ELONGATED; DIMPLED AND CRACKED FASTENER HOLES ON THE TRAILING EDGE. ; / [01] INSTALLED NEW PANEL (193D) PER AMM 53-51-21

ATA 2560

AFT ENTRY DOOR ESCAPE SLIDE CATCHES ON SCUFF PLATE ; / [01] READJUSTED GIRT BAR Z-FOLD SEAL USING LITE HAND PRESSURE PER AMM INTRODUCTION - STEP 2 - USE OF STANDARD INDUSTRY PRACTICE. ACCOMPLISHED OP CHECK OF AFT ENTRY DOOR PER AMM 52-13-00-860-803 AND AMM 52-13-00-860-804. OPS CHECK GOOD.; [02] VERIFIED READJUSTED GIRT BAR Z-FOLD SEAL USING LITE HAND PRESSURE PER AMM INTRODUCTION - STEP 2 - USE OF STANDARD INDUSTRY PRACTICE. ACCOMPLISHED OP CHECK OF AFT ENTRY DOOR PER AMM 52-13-00-860-803 AND AMM 52-13-00-860-804. OPS CHECK GOOD.

ATA 3350

EMERGENCY LIGHTS AT BOTH OVERWING EXITS ARE INOP / [01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY LIGHTS AT BOTH L/H AND R/H OVERWING EXITS PER AMM 33-51-01-960-801; [02] VERIFIED RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY LIGHTS AT BOTH L/H AND R/H OVERWING EXITS PER AMM 33-51-01-960-801

ATA 5320

AFT CARGO COMP. DOOR CUTOUT SURROUND; MISSING NUTPLATE BELOW STR-21R; WL-170; BS 794.3; MARKED ; / [01] UPON INVESTIGATION FOUND NUT ELEMENT MISSING FROM THE NUTPLATE AT FAULT LOCATION; INSTALLED NEW NUT ELEMENT INTO NUTPLATE IAW BAC SPEC FOR BACN10KE NUTPLATE PAGE 11 AND 12; [02] VERIFIED COMPLETE

ATA 5320

ACB DOOR CUTOUT; AFT CORNER SCUFF PLATE IS CRACKED. ; / [01] WELDED 2EA 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>CAL INFO E10583; S/N KJ256554; [02] VERIFIED WELDING OF 2EA CRACKS ON ACB; AFT CORNER SCUFF PLATE PER SRM 53-60-15-2R-1; NO OBVIOUS DEFECTS NOTED; [03] ACCOMPLISHED FPI INSPECTION TO AFT CORNER SCUFF PLATE IAW BOEING SOPM 20-20-02. NO CRACKS NOTED. TOOL ID D3045995330; UV LAMP: ATS2504; RADIOMETER; [04] SANDED WELD REPAIR AREA PER SRM 53-60-15-2R-1 PARA 4.B.(5); [05] VERIFIED SANDING OF WELD REPAIR PER SRM 53-60-15; [06] APPLIED CHEMICAL CONV COAT AND TWO LAYERS OF BMS10-11; TYPE 1 PRIMER PER SRM 53-60-15-2R-1 PARA 4.B.(6) & (7); [07] VERIFIED; REFINISHED PER SRM 53-60-15-2R-1.; [08] CORRECTED MEASUREMENTS; [09] AFT CORNER SCUFF PLATE WILL BE INSTALLED ON FAULT TTG8Q002DSUG.; [10] CORRECTED MEASUREMENTS; [11] VERIFIED INSTALLED ON CARD TTG8Q002DSUG

ATA 5313

CORROSION STILL PRESENT (AFT OF REMOVED FASTENER) ON STRINGER 23L AT BS 311; WL 167. ; REJECT - CORROSION STILL PRESENT (AFT OF REMOVED FASTENER) ON STRINGER 23L AT BS 311; WL 167. / [01] REMOVED CORROSION ON STRIGER 23 LEFT AT BS 311; WL 167; AREA 1' X 2' IAW SRM 53-10-15-1A-1 ALLOWABLE DAMAGE 1.; [02] VERIFIED REMOVAL OF CORROSION ON STRIGER 23 LEFT AT BS 311; WL 167; AREA 1' X 2' IAW SRM 53-10-15-1A-1 ALLOWABLE DAMAGE 1.

ATA 5510

LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.50 LOWER CORD AT 3RD VERTICAL STIFFENER HAS CRACK INDICATIONS ON I/B FLANGE. ; / [01] PERFORMED CUT OUT LOWER CORD AT 3RD VERTICAL STIFFENER ON I/B FLANGE HORIZONTAL STAB INSPAR RIB STA 129.50 L: 1.7' W: .300' IAW SRM 55-10-09-2R REPAIR 5; [02] REQ NDI CUT OUT FOR FREE CRACK CONDITION AND ALL HOLE AROUND REPAIR AREA IAW SRM 55-10-09-2R REPAIR 5; [03] VERIFIED PERFORMED CUT OUT LOWER CORD AT 3RD VERTICAL STIFFENER ON I/B FLANGE HORIZONTAL STAB INSPAR RIB STA 129.50 L: 1.7' W: .300' IAW SRM 55-10-09-2R REPAIR 5; [04] HFEC INSPECTED CUT OUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR>CAL ID IS000450 N500D; [05] REPAIR ACCOMPLISHED ON N/C TTG8005TE54; [06] VERIFIED STEP 5.; [07] VERIFIED JOB COMPLETE; [08] COMPLETE; [09] VERIFIED COMPLETE; [10] SRM REFERENCE SHOULD BE 55-10-09-2R-5; [11] STEP 5: REPAIR ACCOMPLISHED ON FAULT TTG8Q005TE54

ATA 5321

PANEL 140CF IS CORRODED AT FASTNER ATTACH HOLES ; / [01] FABRICATED NEW ACB FLOOR PANEL 140CF FROM 071 2024T-3 LOT# 1461004-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] CORROSION ON ACB FLOOR PANEL 140CF DETERMINED TO BE OUT OF LIMIT DUE TO LENGTH OF DAMAGE EXCEEDS 20' IAW SRM 53-00-53-1A-1 FIG 102; [03] VERIFIED FABRICATION OF NEW ACB FLOOR PANEL 140CF PER AMM 25-52-01

ATA 5321

CORROSION ON PANEL 140BF ; / [01] FABRICATED NEW ACB FLOOR PANEL 140BF FROM 071 2024T-3; LOT# 1461004-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] UPDATEDMEASUREMENTS AND ADDED OUT OF LIMITS STATEMENT=CORROSION ON ACB FLOOR PANEL 140DF DETERMINED TO BE OUT OF LIMIT DUE TO LENGTH OF DAMAGE EXCEEDS 20' IAW SRM 53-00-53-1A-1 FIG 102; [03] CORRECTION TO ITEM 2= PANEL NUMBER IS 140BF; [04] UPDATED MEASUREMENT; [05] VERIFIED FABRICATION OF NEW ACB FLOOR PANEL 140BF PER AMM 25-52-01

ATA 5510

LEFT HAND HORIONTAL STABILIER INSPAR RIB AT STABILIER STATION 129.50 4TH VERTICAL STIFFENER IS CRACKED. ; / [01] PERFORMED CUT OUT IN 4TH VERTICAL STIFFENER STAB INSPAR RIB AT STA 129.50; IAW SRM 55-10-09-2R-4; [02] REQ NDI FOR FREE CRACK CONDITION; AND ALL HOLE AROUND REPAIR AREA IAW SRM 55-10-09-2R-4 REPAIR 4; [03] VERIFIED DAMAGE REMOVAL STEP 1; [04] HFEC INSPECTED BLENDED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; 1 (EA) CRACK NOTED AT CUT OUT AREA; MARKED END OF CRACK . EQUIP ID#: IS000450 S/N: N500D000M120071; [05] HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071 EQUIP ID#: ATS2407 S/N: MM1591DD064104;10] FABRICATED REPAIR PARTS -1 T SECTION FROM MAT 60-5872-7075-T6511 LOT# 1463618-1 -2 REPAIR ANGLE FROM MAT BAC 1490-2793 7075-T62 LOT# 1449279-1 -3 SHIMS 2EA FROM MAT .020' 7075-T6 LOT# J000046012 IAW SRM 55-10-09-2R-4 REPAIR 4 OK TREAT AND PRIMER; [11] VERIFIED FABRICATION OF REPAIR PARTS IN STEP 10 PER SRM. VERIFIED OK TO APPLY CONVERSION COATING AND PRIMER.; [12] APPLIED CHEMICAL CONVERSION COATING AND PRIMED REPAIR PARTS AND REWORKED AREA AT L/H HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50 4TH VERTICAL STIFFENER PER SRM 55-10-09-2R-4 STEP 4 K;L. OK TO INSTALL REPAIR PARTS;

ATA 5313

CORROSION ON STRINGER 23 LEFT AT B.S. 311; W.L. 167. ; / [02] REMOVED DAMAGE ON STRIGER 23 LEFT AT BS 311; WL 167; AREA 1' X 1' IAW SRM 53-10-15-1A-1 ALLOWABLE DAMAGE 1.[04] REJECTED ITEM 2: 2 EA FASTENERS REQUIRE REPLACEMENT FOR HEAD DAMAGE. (FORWARD OF REMOVED FASTENER AND INBOARD OF REMOVED FASTENER). NEW FAULT RAISED.; [05] REMOVED CORROSION ON STRIGER 23 LEFT AT BS 311; WL 167; AREA 1' X 2' IAW SRM 53-10-15-1A-1 ALLOWABLE DAMAGE 1.<BR><BR>REMOVED 2 EA FASTENERS ; FORWARD OF REMOVED FASTENER AND INBOARD OF REMOVED FASTENER IAW SRM 51-40-02-0G-0; [06] VERIFIED REMOVAL OF CORROSION ON STRIGER 23 LEFT AT BS 311; WL 167; AREA 1' X 2' IAW SRM 53-10-15-1A-1 ALLOWABLE DAMAGE 1. REJECTION ITEM 1 CORRECTED ON TTG8Q005VSF2.<BR><BR>VERIFIED REMOVED 2 EA FASTENERS ; FORWARD OF REMOVED FASTENER AND INBOARD OF REMOVED FASTENER IAW SRM 51-40-02-0G-0 FOR REJECTED ITEM 2; [07] ACCOMPLISHED 10X VISUAL INSPECTION NO DEFECTS NOTED; FOUND TO BE OUT OF LIMITS PER SRM 53-10 15-1A-1 FIGURE 108 DETAIL E; FOUND TO BE OUT OF LIMITS PER SRM 53-10 15-1A-1 FIGURE 108 DETAIL E RRECTION STEP 10; [14] VERIFIED STEP 13; [15] ALL STEPS COMPLETED FOR EA 21-153-02064 IS COMPLETE; [16] VERIFIED ALL STEPS COMPLETED FOR EA 21-153-02064 IS COMPLETE;

ATA 5321

CORROSION ON PANEL 140DF ; / [01] CORROSION ON ACB FLOOR PANEL 140DF DETERMINED TO BE OUT OF LIMIT DUE TO LENGTH OF DAMAGE EXCEEDS 20' IAW SRM 53-00-53-1A-1 FIG 102; PANEL TO BE REPLACED ON FAULT TTG8Q005V6S1; [02] VERIFIED REPLACEMENT TO BE ACCOMPLISHED ON FAULT TTG8Q005V6S1

ATA 5321

PANEL 140AF IS CORRODED AT ATTACH FASTNER HOLES ; / [01] FABRICATED NEW ACB FLOOR PANEL 140AF FROM 071 2024T-3 LOT# 1461004-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] CORROSION ON ACB FLOOR PANEL 140AF DETERMINED TO BE OUT OF LIMIT DUE TO LENGTH OF DAMAGE EXCEEDS 20' IAW SRM 53-00-53-1A-1 FIG 102; PANEL TO BE REPLACED ON FAULT TTG8Q005V76V; [03] CORRECTION TO ITEM 2=PANEL WILL BE REPLACED ON THIS FAULT; [04] VERIFIED FABRICATION OF NEW ACB FLOOR PANEL 140AF PER AMM 25-52-01 AND DWG 453A2610

ATA 5321

PANEL 140BF IS CORRODED AT ATTACH FASTNER HOLES ; / [01] CORROSION ON ACB FLOOR PANEL 140BF DETERMINED TO BE OUT OF LIMIT DUE TO LENGTH OF DAMAGE EXCEEDS 20' IAW SRM 53-00-53-1A-1 FIG 102; PANEL TO BE REPLACED ON FAULT TTG8Q005V49D; [02] VERIFIED OUT OF LIMITS STATEMENT AND VERIFIED FAULT TO BE ADDRESSED ON TTG8Q005V49D

ATA 5321

PANEL 140DF IS CORRODED AT ATTACH FASTNER HOLES ; / [01] FABRICATED NEW ACB FLOOR PANEL 140DF FROM 071 2024T-3; LOT# 1461004-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] CORROSION ON ACB FLOOR PANEL 140DF DETERMINED TO BE OUT OF LIMIT DUE TO LENGTH OF DAMAGE EXCEEDS 20' IAW SRM 53-00-53-1A-1 FIG 102; [03] VERIFIED OUT OF LIMITS STATEMENT PER SRM 53-00-53 AND VERIFIED FABRICATION OF NEW ACB FLOOR PANEL 140DF PER AMM 25-52-01

ATA 5241

AFT SERVICE DOOR VIEW PORT FAIRING IS CRACKED AT SEVERAL FASTENERS / [01] REMOVED AND REPLACED AFT SERVICE DOOR VIEW PORT FAIRING PER AIPC 52-13-21-04 AND SOPM 20-50-01<BR>USED SCREW GUN <BR>ID: PER1854<BR>SN: UNKNOWN<BR>DATE:09/2020<BR>DUE:09/2021; [02] ADDED PART INFORMATION.; [03] INSPECTION COMPLETE

ATA 5321

PANEL 194BL HAS A DAMAGED FASTENER HOLE (MARKED) ; / [01] IDENTIFIED PANEL 194BL MATERIAL IAW SRM 53-60-70-0I-1 TABLE 2 FIGURE 2 ITEM 10. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-70-1A-1 PARAGRAPH 4.C(6). DAMAGE WILL BE REPAIRED IAW SRM 51-70-05-2R-10 AS DIRECTED PER SRM 53-60-70-2R-1. <BR><BR>REMOVED DAMAGED PLIES AND TAPER SANDED ON TOOL SIDE AND BAG SIDE. NO CONTAMINANTS NOTED IAW SRM 51-70-05-2R-10 PARAGRAPH 4.A-C; [02] VALIDATED REPAIR PER SRM 51-70-05-2R-10; [03] VALIDATED OUT OF LIMITS; DAMAGE REMOVAL; SRM 51-70-05-2R-10 IS VALID; [04] FABRICATED REPAIR PLIES FROM BMS8-79ST120 LOT#1457859-1; BMS5-129GR05 LOT#1457270-4 AND BMS8-79ST1581 LOT#1462650-1; INSTALLED PLIES; VACUUM BAGGED PLIES; VERIFIED 5X5 AND SET PLIES TO CURE USING HOTBONDER ID: ATS532 S/N: 5092117 IAW SRM 51-70-05-2R-10 PARA 4.D-F.; [05] CORRECTED 'USING HOTBONDER ID: ATS532 S/N: 15092117'; [06] CURED PLIES; REMOVED VACUUM BAGGING MATERIAL AND LIGHTLY SANDED IAW SRM 51-70-05-2R-10 PARA 4. F.-H.; [07] CERTIFIED WORK ACCOMPLISHED IN LINE ITEM 6.; [08] VERIFIED CORRECTIVE ACTIONS 4-7 PER SRM 51-70-05-2R-10; [09] UT INSPECTED POST CURE IAW 737 NDTM PART 4 51-00-02; NO DISBONDS NOTED. EQUIP ID#: ATS2341 S/N: 190848104;

ATA 5320

RIGHT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE (SKATE ANGLE) CHAFED AT BS 1104 - BS 1129. ; / [01] RIGHT FUSELAGE FIN TOBODY INTERFACE CLOSURE ANGLE (SKATE ANGLE) AT BS 1104 TO BS 1129 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-OG-0 STEP 9.C.; [02] REMOVED RIGHT FUSELAGE FIN TOBODY INTERFACE CLOSURE ANGLE P/N 148A8310U4 (SKATE ANGLE) FROM BS 1016 TO BS 1137 ; S-2R IAW SRM 51-40-02-0G-0.; [03] VERIFIED RIGHT FUSELAGE FIN TOBODY INTERFACE CLOSURE ANGLE (SKATE ANGLE) AT BS 1104 TO BS 1129 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-OG-0 STEP 9.C.; [04] LOCATED AND DRILLED R/H SKATE ANGLE PN# 148A8310U4 IAW SRM 51-40-05 AND IAW DWG# 148A8300...OK TO INSTALL; [05] INSPECTED LOCATED AND DRILLED R/H SKATE ANGLE PN# 148A8310U4 IAW SRM 51-40-05 AND IAW DWG# 148A8300...OK TO INSTALL; [06] INSTALLED R/H SKATE ANGLE PN# 148A8310U4 IAW SRM 51-40-02 AND IAW DWG#148A8300; [07] VERIFIED INSTALLATION OF R/H SKATE ANGLE PN# 148A8310U4 IAW SRM 51-40-02 AND IAW DWG#148A8300; [08] VERIFIED CARD COMPLETE; [09] VERIFIED CARD COMPLETE

ATA 5320

CORROSION ON UNDERSIDE OF FWD SHIELD AT AFT CARGO BAY BS767 - BS787 RBL21 WL157 ; / [01] EVALUATED ACB SHIELD BS767-787 RBL21 WL157 AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM 53-60-15-1A-1; PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9C<BR>THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q005TL8J; [02] VERIFIED OUT OF LIMITS AND WILL BE REWORKED ON TTG8Q005TL8J

ATA 5320

CORROSION ON UNDERSIDE OF AFT SHIELD AT AFT CARGO BAY BS856 RBL21 WL164 ; / [01] EVALUATED ACB SHIELD BS856 RBL21 WL164 AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM 53-60-15-1A-1; PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9C<BR>THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q005THQT; [02] VERIFIED OUT OF LIMITS- TO BE REWORKED ON TTG8Q005THQT

ATA 5320

CORROSION ON UNDERSIDE OF FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727C+11 LBL21 WL156 ; / [01] REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727C+11 LBL21 WL 156 MAX MATERIAL LOSS L=2'; W=1'; D=0.006'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 146A7502 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022 <BR>THIS JOB CARD WILL BE ACCOMPLISHED ON CARD ID: TTG8Q005TWAV; [02] INSPECTED AND VERIFIED REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727C+11 LBL21 WL 156 MAX MATERIAL LOSS L=2'; W=1'; D=0.006'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 146A7502 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022 <BR>THIS JOB CARD WILL BE ACCOMPLISHED ON CARD ID: TTG8Q005TWAV

ATA 5313

FWD CARGO COMPARTMENT HAS CRACKED STRINGER 22L AT STA 540 ; / [01] CUT AND REMOVED THE DAMAGED PART OF THE STRINGER 22L FROM BS 500D+12 - BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1 STEP 4B; [02] VERIFIED REMOVED DAMAGE PART OF THE STRINGER 22L FROM BS 500D+12 - BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1 STEP 4B; [03] VERIFIED REMOVED DAMAGE PART OF THE STRINGER 22L FROM BS 500D+12 - BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1 STEP 4B; [04] SRM 53-30-03-0I-01 IDENTIFICATION 1 AND SRM 53-00-03-2R-1 REPAIR 1 ARE APPLICABLE TO THIS A/C; [05] VERIFIED APPLICABILITY STATEMENT.; [06] REQUESTED HFEC INSPECTION OF THE REPAIR AREA IAW SRM 53-00-03-2R-1 REPAIR 1 STEP 4C; [07] HFEC INSPECTED CUT OUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [08] RECEIVED STRINGER SECTION FROM OSS FORMED AND HEAT TREATED TO 7075T6#0.036' CONDITION PER CUSTOMER RO NO 831342-SWA AND STINGER SPLICE FORMED AND HEAT TREATED IN THE FORM OF 7075T6#0.045' CUSTOMER RO NO 831355-SWA; LOCATED AND DRILLED ALL REPAIR PARTS AT BS510 TO BS540 STR 22L IAW EA#21-153-02109 REV-A AND SRM 53-00-03-2R-1 REPAIR-1 FIG-205 OK TO TREAT AND PRIME; [09] RECEIVED STRINGER SECTION FROM OSS FORMED AND HEAT TREATED TO 7075T6#0.036' CONDITION PER CUSTOMER RO NO 831342-SWA AND STINGER SPLICE FORMED AND HEAT TREATED IN THE FORM OF 7075T6#0.045'

ATA 5313

FWD CARGO COMPARTMENT HAS CRACKED STRINGER 23R AT STA 540 ; / [01] CU AND REMOVED THE DAMAGED PART OF STRINGER 23R FROM BS 50D+12 - BS540 IAW SRM 53-00-03-2R-1 REPAIR 1 STEP 4B; [02] CUT AND REMOVED THE DAMAGED PART OF STRINGER 23R FROM BS 500D+12 - BS540 IAW SRM 53-00-03-2R-1 REPAIR 1 STEP 4B; [03] VERIFIED DAMAGE REMOVAL PER SRM 53-00-03-2R-1 REPAIR 1 STEP 4.B; [04] SRM 53-30-03-0I-01 IDENTIFICATION 1 AND SRM 53-00-03-2R-1 REPAIR 1 ARE APPLICABLE TO THIS A/C; [05] VERIFIED APPLICABILITY STATEMENT SRM 53-00-03-2R-1 REPAIR 1; [06] REQUESTED HFEC INSPECTION OF THE REPAIR AREA IAW SRM 53-00-03-2R-1 REPAIR 1 STEP 4C; [07] HFEC INSPECTED CUTOUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [08] -RECEIVED REPLACEMENT STRINGER SECTION (1E/A) HFAB53-STR-011 (7075T0#0.036 LOT#145783; HEAT TREAT TO T6 CONDITION PER BAC5602; DYE PENETRANT INSPECT PER SOPM 20-20-02. IAW CUSTOMER RO NO. 831348-SWA JOB#541338<BR>-RECEIVED HAT SECTION (1E/A) HFAB53-HS-011 (7075T0#0.040) ; HEAT TREAT TO T6 CONDITION PER BAC5602 LOT#1464420-1 IAW CUSTOMER RO NO. 831351-SWA JOB#541339; [09] FABRICATED; LOCATED AND DRILLED NEW STRINGER SECTION AND HAT STRINGER SECTION IAW EA#21-153-02051 AND SRM 53-00-03-2R-1.

ATA 5320

CORROSION ON UNDERSIDE OF FLOOR TO SIDEWALL SUPPORT AT BS727C+18 RBL20 WL 156 ; / [01] EVALUATED CORROSION ON ACB SIDEWALL SUPPORT BS 727C+18'' RBL 20 WL 156 AND FOUND TO BE OUT OF LIMITS DUE TO EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 PART 4A(2); MEASURES OF CORROSION L=2.0'' X W= 1.5'' X D=0.015'' FROM ORIGINAL THICKNESS OF TH=0.040''; TOOL USED CALIPER ID:ATS2318 S/N:B19006095; DEPTH GAUGE ID: ATS2472 S/N: UNKNOWN<BR>THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q005THRJ; [02] VERIFIED OUT OF LIMITS AND TO BE REPAIRED ON TTG8Q005THRJ (FLOOR TO SIDEWALL REPLACEMENT); [03] REFERENCE NOT SELECTED FROM DROP DOWN; CORRECT REFERENCE IS SRM 53-00-53-1A-2-A00028 (PERMANENT (NON-DENT DAMAGE TYPES))

ATA 5320

CORROSION ON UNDERSIDE OF FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS761-BS787 LBL 21 WL156 ; / [01] REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 761-BS 787 LBL21 WL 156 MAX MATERIAL LOSS L=2.5';W=0.9';D=0.018' FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 146A7502 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022; [02] CORRECTION: FOUND TO BE OUT OF LIMITS; [03] VERIFIED EVALUATION AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [04] LOCATED AND DRILLED NEW EXTRUSION FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY FROM BS727 THRU BS847 LBL21 WL156 IAW SRM 51-40-05 AND DWG 146A7502<BR>OK TO PROTECTIVE TREATMENT; [05] AND SPLICE FABRICATION IAW SRM 53-00-53-2R-6; [06] VERIFIED LOCATE AND DRILL UP OF NEW SUPPORT AND SPICE MATERIAL; OK TO PROCEED AFTER LOT # ID IS UPDATED BY AMT FOR MATERIAL; [07] UPDATED; EXTRUSION BAC1496-377 LOT# 1462654-1; [08] APPLIED CONVERSION COATING AND PRIMER ON NEW PARTS IAW SRM 51-20-01 AND SOPM 20-41-04.; [09] VERIFIED STEP 7 AND 8; [10] OK TO INSTALL FLOR TO SIDEWALL SUPPORT BS727 TO BS 847 LBL 21 WL 156; [11] VERIFIED OK TO INSTALL STEP 10.; [12] INSTALLED FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727 TO BS 847 LBL 21 WL 156 IAW SRM 51-40-02 AND DWG 146A7500; [13] VERIFIED FLOOR TO SIDEWALL SUPPORT INSTALL PER SRM AND DWG.; [14] COMPLETE

ATA 5320

CORROSION ON UNDERSIDE OF FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS902-BS907 RBL21 WL 170 ; / [01] REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 902-BS 907 RBL 21 WL 170 MAX MATERIAL LOSS L=2.5';W=1.2';D=0.007' FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 147A7501-18 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022; [02] CORRECTION: FOUND TO BE OUT OF LIMITS; [03] VERIFIED CORROSION REMOVAL; EVALUATED; AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [04] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL AT BS 887-947; RBL 21; WL 170; IAW 737-700 SRM 51-40-05-OG-0 DWG 146A7501; [05] INSPECTED ACTION 4 LOCATED AND DRILLED NEW FLOOR TO SIDEWALL AT BS 887-947; RBL 21; WL 170; IAW 737-700 SRM 51-40-05-OG-0 DWG 146A7501; [06] APPLIED CHEMICAL CONVERCION COATING AND PRIMER ON FLOOR TO SIDEWALL BS 887-947; RBL 21; WL 169; IAW 737-700; AMM 51-21-72-370-804; AMM 51-21-41-370-802 OK TO INSTALL; [07] VERIFIED STEP 6; [08] OK TO INSTALL; [09] INSTALLED FLOOR TO SIDEWALL SUPPORT AT BS 887-947; RBL 21; WL 170; IAW 737-700 SRM 51-40-02 AND DWG 146A7500; [10] VERIFIED INSTALL OF FLOOR TO SIDEWALL SUPPORT PER SRM AND DWG.

ATA 5320

CORROSION ON UNDERSIDE OF FLOOR TO SIDE WALL SUPPORT AT AFT CARGO BAY BS873 - BS887 RBL21; WL 169 ; / [01] REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 873 BS 887 RBL 21 WL 169 MAX MATERIAL LOSS L=5';W=2.5';D=0.006' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 146A7502-50 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022; [02] VERIFIED CORROSION REMOVAL; EVALUATED; AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL AT BS 867-887; RBL 21; WL 169; IAW 737-700 SRM 51-40-05-OG-0 DWG 146A7502; [04] INSPECTED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL AT BS 867-887; RBL 21; WL 169; IAW 737-700 SRM 51-40-05-OG-0 DWG 146A7502; [05] APPLIED CHEMICAL CONVERCION COATING AND PRIMER ON FLOOR TO SIDEWALL BS 847-887; RBL 21; WL 169; IAW 737-700; AMM 51-21-72-370-804; AMM 51-21-41-370-802 OK TO INSTALL; [06] CORRECTION: BS 867-887; [07] VERIFIED STEPS 5 AND 6; [08] OK TO INSTALL; [09] INSTALLED FLOOR TO SIDEWALL AT BS 867-887; RBL 21; WL 169; IAW 737-700 SRM 51-40-02 AND DWG 146A7500; [10] VERIFIED INSTALLATION OF FLOOR TO SIDEWALL AT BS 867-887; RBL 21; WL 169; IAW 737-700 SRM 51-40-02 AND DWG 146A7500; [11] VERIFIED INSTALLATION OF FLOOR TO SIDEWALL AT BS 867-887; RBL 21; WL 169; IAW 737-700 SRM 51-40-02 AND DWG 146A7500

ATA 5315

CORROSION ON UNDERSIDE OF FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS887 LBL3 TO LBL8 WL 169 ; / [01] VERIFIED APPLICABILITY NOT ALLOWABLE DAMAGE PARTS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-OG-0 STEP 9C. LOCATED AND DRILLED FLOOR SPLICE AT AFT CARGO BAY BS 887 LBL 3 TO LBL 8 WL 169 IAW SRM 51-40-05 AND DWG 146A9401 INSTALLATION WILL BE ACCOMPLISHED ON CARD # TTG8Q004AMCD VERIFIED ACTION 5

ATA 5320

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 500B+1 TO 500B+13 LBL 24 WL 156 ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 500+6'; LBL24; WL 156 PER SRM51-10-02-0G-0 MEASURE L=1.5'X W=1'X D=0.008' MAX. MAT LOSS IS 0.008'; REMAINING THICKNESS IS 0.008'; ORIGINAL THICKNESS IS 0.040' (BAC1496-444) FOUND TO BE OUT OF LIMITS; REWORKED AREA PER B737-700 SRM53-00-53-1A-2; ALLOWABLE DAMAGE PARAG. 4.A (2) DETAIL (E) FIG 103.- MICROMETER;S/N 65092939 DUE 03/2022. THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q005TGWB; [02] THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q005TGWB; [03] CORRECTING CORROSION REMOVAL LOCATION AND DIMENSIONS: REMOVED CORROSION BS 500B+1- 500B+13 L=12'; W=1' D=.008' MAX; OUT OF LIMITS PER SRM 53-00-53-1A-2.; [04] VERIFIED THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q005TGWB

ATA 5320

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 500A+2 TO 500C+15 RBL 25 WL 156 ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 500A+2 - BS500C+15'; RBL25; WL 156 PER SRM51-10-02-0G-0 MEASURE L=59'X W=1'X D=0.006' MAX. MAT LOSS IS 0.006'; REMAINING THICKNESS IS 0.0034'; ORIGINAL THICKNESS IS 0.040' (BAC1496-444) FOUND TO BE OUT OF LIMITS; REWORKED AREA PER B737-700 SRM53-00-53-1A-2; ALLOWABLE DAMAGE PARAG. 4.A (2) DETAIL (E) FIG 103.- MICROMETER;S/N 65092939 DUE 03/2022.; [02] VERIFIED REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 500A+2 - BS500C+15'; RBL25; WL 156 PER SRM51-10-02-0G-0 MEASURE L=59'X W=1'X D=0.006' MAX. MAT LOSS IS 0.006'; REMAINING THICKNESS IS 0.0034'; ORIGINAL THICKNESS IS 0.040' (BAC1496-444) FOUND TO BE OUT OF LIMITS; REWORKED AREA PER B737-700 SRM53-00-53-1A-2; ALLOWABLE DAMAGE PARAG. 4.A (2) DETAIL (E) FIG 103.; [03] REMOVED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT FORM BS 500A TO BS500D RBL25 WL156; IAW SRM 51-40-02-0G-0.; [04] FABRICATED LOCATED AND DRILLED NEW FCB FLOOR TO SIDEWALL SUPPORT BS500A BS500D RBL25 WL156; FROM EXTRUSION BAC1496-444#7075T62 LOT#1453146-2 IAW SRM 53-30-53-0I-2 AND 51-40-05-0G-0 AND DWG #143A7500;

ATA 5320

CORROSION ON STRAP AT AFT CARGO BAY BS809 RBL19 WL159. ; / [01] REMOVED CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1 W=1; [02] VERIFIED REMOVAL OF CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1'; W=1'; [03] UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.082'<BR>CAL ID ATS2031 E650; [04] VERIFIED LIMITS ON BLENDED AREA L=1 W=1 ORIGINAL MATERIAL THICKNESS IS .100 REMAINING THICKNESS .082 THEREFORE FOUND TO BE OUT OF LIMITS PER REF SRM 53-60-15-1A-1; [05] VERIFIED OUT OF LIMITS PER REF SRM 53-60-15-1A-1; [06] REPLACEMENT OF PART WILL BE ACCOMPLISHED ON CARD ID: TTG8Q005TJ0X; [07] VERIFIED ACTION 6; [08] VERIFIED ACTION 6

ATA 5320

CORROSION ON STRAP AT AFT CARGO BAY BS820 RBL19 WL159. ; / [01] REMOVED CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1 W=1; [02] VERIFIED REMOVAL OF CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1'; W=1'; [03] UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.079'<BR>CAL ID ATS2031 E650; [04] VERIFIED LIMITS ON BLENDED AREA L=1 W=1 ORIGINAL MATERIAL THICKNESS IS .100 REMAINING THICKNESS .079 THEREFORE FOUND TO BE OUT OF LIMITS PER REF SRM 53-60-15-1A-1; [05] VERIFIED OUT OF LIMITS; [06] REPLACEMENT OF PART WILL BE ACCOMPLISHED ON CARD ID: TTG8Q005TJ0X; [07] VERIFIED ACTION 6; [08] VERIFIED ACTION 6

ATA 5320

CORROSION ON STRAP AT AFT CARGO BAY BS824 RBL19 WL159. ; / [01] REMOVED CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1 W=1; [02] VERIFIED REMOVAL OF CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1'; W=1'; [03] UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.075'<BR>CAL ID ATS2031 E650; [04] VERIFIED LIMITS ON BLENDED AREA L=1 W=1 ORIGINAL MATERIAL THICKNESS IS .100 REMAINING THICKNESS .075 THEREFORE FOUND TO BE OUT OF LIMITS PER REF SRM 53-60-15-1A-1; [05] VERIFIED OUT OF LIMITS PER REF SRM 53-60-15-1A-1; [06] REPLACEMENT OF PART WILL BE ACCOMPLISHED ON CARD ID: TTG8Q005TJ0X; [07] VERIFIED ACTION 6; [08] VERIFIED ACTION 6

ATA 5320

CORROSION ON STRAP AT AFT CARGO BAY BS816.5 RBL19 WL159. ; / [01] REMOVED CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1 W=1; [02] VERIFIED REMOVAL OF CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1'; W=1'; [03] UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.081'<BR>CAL ID ATS2031 E650; [04] VERIFIED LIMITS ON BLENDED AREA L=1 W=1 ORIGINAL MATERIAL THICKNESS IS .100 REMAINING THICKNESS .081 THEREFORE FOUND TO BE OUT OF LIMITS PER REF SRM 53-60-15-1A-1; [05] VERIFIED OUT OF LIMITS PER REF SRM 53-60-15-1A-1; [06] REPLACEMENT OF PART WILL BE ACCOMPLISHED ON CARD ID: TTG8Q005TJ0X; [07] VERIFIED ACTION 6; [08] VERIFIED ACTION 6

ATA 5320

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 500C+1 TO 500C+4 LBL 24 WL 156 ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 500C+1'; LBL24; WL 156 PER SRM51-10-02-0G-0 MEASURE L=1.5'X W=1'X D=0.007' MAX. MAT LOSS IS 0.007'; REMAINING THICKNESS IS 0.033'; ORIGINAL THICKNESS IS 0.040' (BAC1496-444) FOUND TO BE OUT OF LIMITS; REWORKED AREA PER B737-700 SRM53-00-53-1A-2; ALLOWABLE DAMAGE PARAG. 4.A (2) DETAIL (E) FIG 103.- MICROMETER;S/N 65092939 DUE 03/2022. THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q005TGWB; [02] VERIFIED THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q005TGWB

ATA 5320

FLOOR TO SIDEWALL SUPPORT HAS DAMAGE AT AFT CARGO BAY BS727E+7 RBL21 WL156. MARKED ; / [01] EVALUATED CORROSION ON ACB SIDEWALL SUPPORT BS 727E+7'' RBL 21 WL 156 AND FOUND TO BE OUT OF LIMITS DUE TO EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 PART 4A(2); MEASURES OF CORROSION L=3.0'' X W= 1.0'' X D=0.015'' FROM ORIGINAL THICKNESS OF TH=0.040''; TOOL USED CALIPER ID:ATS2318 S/N:B19006095; DEPTH GAUGE ID: ATS2472 S/N: UNKNOWN; [02] REMOVED ACB SIDEWALL SUPPORT BS727-767 RBL 21 WL 156 IAW SRM 51-40-02-0G-0; [03] VERIFIED EVALUATED CORROSION ON ACB SIDEWALL SUPPORT BS 727E+7'' RBL 21 WL 156 AND FOUND TO BE OUT OF LIMITS DUE TO EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 PART 4A(2); MEASURES OF CORROSION L=3.0'' X W= 1.0'' X D=0.015'' FROM ORIGINAL THICKNESS OF TH=0.040''; TOOL USED CALIPER ID:ATS2318 S/N:B19006095; DEPTH GAUGE ID: ATS2472 S/N: UNKNOWN; [04] REPLACEMENT OF ACB SIDEWALL SUPPORT BS 727-767 RBL 21 WL156 IS DOCUMENTED ON TASK CARD TTG8Q005THRJ; [05] VERIFIED REPLACEMENT OF ACB SIDEWALL SUPPORT BS 727-767 RBL 21 WL156 IS DOCUMENTED ON TASK CARD TTG8Q005THRJ

ATA 5320

CORROSION ON FWD CARGO BAY FWD SHIELD AT BS 436 RBL 24 WL 156 ; / [01] NO ENTRIES ALLOWABLE DAMAGE IN SRM PART MUST BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 STEP 9.C; [02] VERIFIED ITEM 1 CORRECTIVE ACTION; REPAIRED BY REPLACEMENT IAW SRM 51-10-02 STEP 9.C; [03] LOCATED AND DRILLED SHIELD LOCATED BTW BS 420-440 P/N 143A8126-21 ; ITEM 7530143; PER SRM 51-40-05; DWG# 143A0080; [04] SHIED WILL BE INSTALLED WITH CUSTOMER CARD # TTG8Q004CVKKC; [05] EDIT STEP 4: SHIELD WILL BE INSTALL ON CUSTOMER CARD # TTG8Q004CVKC; [06] VERIFIED STEP 3 AND 5 JOB COMPLETE; [07] UPDATED MEASUREMENT

ATA 5320

CORROSION ON FWD CARGO BAY SUB THRESHOLD WEB BS 464 RBL 28 WL 156 ; / [01] REMOVAL CORROSION ON FWD CARGO BAY SUB THRESHOLD WEB BS 464 RBL 28 WL 156 ; MEASURES L=2.5' X W= 1.8' X D=0.018' MAX MAT LOSS IS 0.018' REMAINING THICKNESS 0.027' FOUND OUT OF LIMITS REWORKED AREA IAW. SRM 53-00-53-1A-2;ALLOWABLE DAMAGE 2 PARAGRAPH 4.A.(2)(A) DETAIL D FIG.103; AND SRM 53-30-15-0I-1 IDENTIFICATION 1 TABLE 4 ITEM 3 FIG.5 . ORIG. THICKNESS 0.045' . USED TOOL DEPTH GAUGE ID:ATS400; DUE DATE:04/2022; [02] VERIFIED CORROSION REMOVAL; EVALUATED; AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] LOCATED AND DRILLED NEW FWD CARGO BAY SUB THRESHOLD WEB ITEM: 54003-58 LOT #1463905-1; BS 440 TO BS 490 RBL28 WL156 IAW SRM 51-40-05-0G-0 AND DWG #143A8122.<BR>THE ENAMEL PAINT IS DOCUMENTED ON TASK CARD TTG8Q004CVKC; DRILLED NEW FWD CARGO BAY SUB THRESHOLD WEB ITEM: 654A0003-58 LOT #1463905-1; BS 440 TO BS 490 RBL28 WL156 IAW SRM 51-40-05-0G-0 AND DWG #143A8122.

ATA 5320

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS847 RBL23 WL163. ; / REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9; [02] REMOVED INTERCOSTAL AT AFT CARGO BAY BS847 RBL23 WL163. THIS PART DOES NOT HAVE ENTRY ON THE LOWER DAMAGED THERE FOR IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9; [03] REMOVED INTERCOSTAL AT AFT CARGO BAY BS847 RBL23 WL163.THIS PART DOES NOT HAVE ENTRY ON THE LOWER ALLOWABLE DAMAGE LIMITS THERE FOR IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9; [04] REMOVED INTERCOSTAL AT AFT CARGO BAY BS847 RBL23 WL163. REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9; [05] REMOVED INTERCOSTAL AT AFT CARGO BAY BS847 RBL23 WL163.REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9; [06] REMOVED CORROSION ON INTERCOSTAL AT BS 847; RBL23; WL 163 PER SRM51-10-02-0G-0 REMAINING THICKNESS IS 0.048'; ORIGINAL THICKNESS IS 0.063' FOUND TO BE OUT OF LIMITS; REWORKED AREA PER B737-700 SRM53-60-15-1A-1; ALLOWABLE DAMAGE PARAG. 4.C (2 [07] FABRICATED NEW INTERCOSTAL P/N 146A8322-12 FROM SHEET 7075-0 CLAD 0.063' LOT # 1407552-1; AT BS 847; RBL23; WL 163 IAW BOEING DWG 146A8322 ID:- REV:R AND SRM 51-30-01-0G-0[14] INSTALLED NEW INTERCOSTAL AT AFT CARGO BAY BBS 847 TO BS 855 RBL 23 WL 163 IAW SRM 51-40-02 AND DWG 146A8321;

ATA 5311

CORROSION ON FRAME SPLICE AT AFT CARGO BAY BS767 RBL25 WL157. ; / [01] DAMAGE FOUND AT ACB FRAME SPLICE BS-767 RBL-25 WL-157 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-O PAR.9C; [02] VERIFIED DAMAGE FOUND AT ACB FRAME SPLICE BS-767 RBL-25 WL-157 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-O PAR.9C; [03] REMOVED ACB FRAME SPLICE ANGLE P/N 146A1300-2 FROM BS-767 RBL-25 WL-157 IAW SRM 51-40-02-0G-0; [04] FORMED I EA FRAME SPLICE ANGLE FROM 7075T0#0.063' CLAD LOT# 1407552-1 IAW DWG#146A1300; 07] RECEIVED SPLICE ANGLE ITEM 146A1300-2 LOT.#1464382-1. LOCATED AND DRILLED ON FRAME SPLICE AT AFT CARGO BAY BS767 RBL 25 WL157 IAW SRM 41-40-05. DWG#146A1261;146A1260. OK TO TREAT AND PRIMER.; [08] RECEIVED SPLICE ANGLE ITEM 146A1300-2 LOT.#1464382-1. LOCATED AND DRILLED ON FRAME SPLICE AT AFT CARGO BAY BS767 RBL 25 WL157 IAW SRM 51-40-05. [12] INSTALLED NEW FRAME SPLICE AT AFT CARGO BAY BS 767 RBL 25 WL157 IAW SRM 51-40-02-0G-0 AND DWG #146A1300; [13] VERIFIED INSTALLED NEW FRAME SPLICE AT AFT CARGO BAY BS 767 RBL 25 WL157 IAW SRM 51-40-02-0G-0 AND DWG #146A1300.; [14] VERIFIED INSTALLED NEW FRAME SPLICE AT AFT CARGO BAY BS 767 RBL 25 WL157 IAW SRM 51-40-02-0G-0 AND DWG #146A1300.

ATA 5320

CORROSION ON WEB AT AFT CARGO BAY BS773 RBL20 WL157. ; / [01] REMOVED CORROSION ON ACB WEB BS 773 RBL 20 WL 157 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1; PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9; [02] REMOVED CORROSION ON ACB WEB BS 773 RBL 20 WL 157 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1; MEASURES OF MATERIAL REMOVED L=3.0'' X W=1.0'' X D=0.010'' ORIGINAL THICKNESS TH=0.050'' TOOL USED CALIPER ID:ATS1317 S/N: UNKNOWN. MICROMETER ID:ATS1672 S/N 65092939; PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9; [03] VERIFIED CLOSED WING TO BODY PANEL 324AL PER AMM 20-00-00 SCREW GUN I/D PER1463 S/N A638018 CAL DUE04/2022; [04] REMOVED INTERCOSTAL ON ACB FROM BS 767 TO BS 787 RBL 20 WL 157 IAW SRM 51-40-02-0G-0.; [05] FABRICATED NEW INTERCOSTAL P/N 146A8123-20 FROM SHEET 7075-0 0.050' CLAD LOT # 1457313-101 AT ACB FROM BS 767 TO BS 787 RBL 20 WL 157 IAW BOEING DWG 146A8123 ID: 16 ; REV: - AND SRM 51-30-01-0G-0;

ATA 5311

CORROSION ON FRAME SPLICE AT AFT CARGO BAY BS787 RBL25 WL158. ; / REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-O PAR.9C; [02] VERIFIED DAMAGE FOUND AT ACB FRAME SPLICE BS-787 RBL-25 WL-158 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-O PAR.9C; [03] REMOVED ACB FRAME SPLICE ANGLE P/N 146A1300-3 FROM BS-787 RBL-25 WL-158 IAW SRM 51-40-02-0G-0; [04] FORMED 1 EA FRAME SPLICE ANGLE FROM 7075T0#0.063' CLAD LOT# 1407552-1 IAW DWG#146A1300; 07] RECEIVED SPLICE ITEM146A1300-3 LOT. 1464383-1. LOCATED AND DRILLED ON FRAME AT AFT CARGO BAY BS787; RBL 25; WL 158 IAW SRM 51-40-05; DWG#146A1262. OK TO TREAT AND PRIMER;[11] INSTALLED NEW FRAME SPLICE AT AFT CARGO BAY BS787 RBL 25 WL 158 IAW SRM 51-40-02-0G-0 AND DWG#146A1300;

ATA 5320

CORROSION ON STRAP AT AFT CARGO BAY BS787+17 RBL19 WL159. ; / [01] REMOVED CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1 W=1; [02] VERIFIED REMOVAL OF CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1' W=1'; [03] UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.081'<BR>CAL ID ATS2031 E650; [04] VERIFIED LIMITS ON BLENDED AREA L=1 W=1 ORIGINAL MATERIAL THICKNESS IS .100 REMAINING THICKNESS .081 THEREFORE FOUND TO BE OUT OF LIMITS PER REF SRM 53-60-15-1A-1; [05] REMOVED STRAP PER REF SRM 51-40-02; [06] VERIFIED OUT OF LIMITS PER SRM 53-60-15-1A-1; STRAP REMOVAL; [07] LOCATED AND DRILLED NEW STRAP AT AFT CARGO BAY BS 767+10 TO BS 857+5 RBL 19 WL 159 ITEM 146A8128U14 PO# 828684 IAW SRM 51-40-05 ; DWG 146A8120; DWG 146A8340 AND DWG 146A0081; [14] INSTALLED NEW STRAP AT AFT CARGO BAY BS 767+10 TO BS 857+5 RBL 19 WL 159 ITEM 146A8128U14 PO# 828684 IAW SRM 51-40-02 AND DWG 146A8120; [15] PART USAGE INFO;

ATA 5320

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS500C+12 TO 500C+14 LBL 24 WL 156 ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 500C+12'; LBL24; WL 156 PER SRM51-10-02-0G-0 MEASURE L=1.5'X W=1'X D=0.010' MAX. MAT LOSS IS 0.010'; REMAINING THICKNESS IS 0.030'; ORIGINAL THICKNESS IS 0.040' (BAC1496-444) FOUND TO BE OUT OF LIMITS; REWORKED AREA PER B737-700 SRM53-00-53-1A-2; ALLOWABLE DAMAGE PARAG. 4.A (2) DETAIL (E) FIG 103.- MICROMETER;S/N 65092939 DUE 03/2022. THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q005TGWB; [02] VERIFIED THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q005TGWB

ATA 5320

CORROSION ON WEB AT AFT CARGO BAY BS792 RBL19 WL157. ; / [01] REMOVED CORROSION ON WEB AT AFT CARGO BAY BS 792 RBL 19 WL 157 MAX MATERIAL LOSS L=4';W=1';D=0.020 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 STEP 4G (2)(B) FIG 103 TOOL USED ID ATS1672 S/N 65092939 DUE 03/2022; [02] VERIFIED CORROSION REMOVALVON WEB AT AFT CARGO BAY BS 792 RBL 19 WL 157 MAX MATERIAL LOSS L=4';W=1';D=0.020 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 STEP 4G (2)(B) FIG 103 TOOL USED ID ATS1672 S/N 65092939 DUE 03/2022; [03] REMOVED WEB AT AFT CARGO BAY BS 787 - BS 793 RBL 19 WL 157 IAW SRM 51-40-02 AND FORMED WEB AT AFT CARGO BAY BS 787 - BS 793 FROM 7075T0#0.045'SH C LOT #1460866-1 IAW DWG 146A8123-22 REV A; [10] INSTALLED NEW WEB AT AFT CARGO BAY BS 787 - BS 793 RBL 19 WL 157 IAW SRM 51-40-02 DWG # 146A8120;

ATA 5320

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS873 - BS887 RBL21 WL169. ; / [01] REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 873 BS 887 RBL 21 WL 169 MAX MATERIAL LOSS L=5';W=2.5';D=0.006' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 146A7502-50 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022 <BR>THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q005TVEW; [02] VERIFIED REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 873 BS 887 RBL 21 WL 169 MAX MATERIAL LOSS L=5';W=2.5';D=0.006' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 146A7502-50 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022 <BR>THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q005TVEW

ATA 5320

CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS802 - BS827 RBL26 WL159. ; / [01] REMOVED CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS802-BS827 RBL26 WL159 DIMENSIONS: L=25' W=2' D=0.007' WAS FOUND OUT OF LIMIT DUE MATERIAL LOSS IS MORE THAN 10% OF THICKNESS IAW SRM 53-60-15-1A-1 ITEM 4.G(2) FIG. 103 <BR>TOOL USED: ID E9655; S/N:UNKNOWN; DUE DATE: 03/2022; [02] VERIFIED EVALUATION AND FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1; [03] REMOVED SUBTHRESHOLD WEB AT AFT CARGO BAY BS790 BS847 RBL 26 WL 159 IAW SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW SUBTHRESHOLD WEB AT AFT CARGO BAY BS 790- BS 847 RBL26 WL159 ITEM #146A8123U25; LOT #1462694 IAW SRM 51-40-05-0G-0 AND DWG #146A8123; [05] VERIFIED LOCATE AND DRILL OF NEW SUBTHRESHOLD WEB AT ACB BS 790-BS 847 RBL 26 WL 159 ITEM #146A8123U25; LOT # 1462694 IAW SRM 51-40-05-0G-0 AND DWG #146A8123.; [06] OK TO INSTALL; [07] VERIFIED ACTION 5; 6; [08] INSTALLED NEW SUBTHRESHOLD WEB AT AFT CARGO BAY BS802-BS827 RBL26 WL159 ITEM# 146A8123U25 LOT# 1462694; PO#829359; IAW SRM 51-40-02; DWG 146A8340; [09] VERIFIED; ACTION 8; [10] VERIFIED ACTION 8

ATA 5510

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] CUT 0UT AND REMOVED DAMAGED SECTION AT VERTICAL STIFFENER OF THE RIB L= .80; W=.312 STATION 129.50 3RD VERTICAL STIFFENER PER SRM 55-10-09-2R; [02] DO A HFEC INSPECTION OF THE CUT EDGES OF THE STIFFENER AND WEB AND ALL EXISTING FASTENER HOLES PER SRM 55-10-09-2R-4 STEP 4 C; D; [03] VERIFIED CUT 0UT AND REMOVED DAMAGED SECTION AT VERTICAL STIFFENER OF THE RIB L= .80; W=.312 STATION 129.50 3RD VERTICAL STIFFENER PER SRM 55-10-09-2R; [04] ET INSPECTED CUT EDGE/HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23 AND PROCEDURE 16; NO CRACKS NOTED.<BR>CAL ID IS000450 N500D; [05] DO A GENERAL VISUAL INSPECTION OF ALL AREAS WITHIN THE REPAIR AREA PER SRM 55-10-09-2R-4 STEP 4 E; [06] ACCOMPLISHED A GENERAL VISUAL INSPECTION OF ALL AREAS WITHIN THE REPAIR AREA PER SRM 55-10-09-2R-4 STEP 4 E NO FAULTS FOUND; [07] FABRICATED -1 T SECTION FROM 60-5872 7075T76511 LOT #1463618-1 ; -2 REPIR ANGLE FROM BAC1490-2793 7075T62 LOT # 1449279-1 AND -3 SHIMS 2 EA FROM 7075T6 .020' LOT # J000046012 AT <BR>RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER PER SRM 55-10-09-2R-4 OK TO TREAT AND PRIME PARTS; [11] INSTALLED REPAIR PARTS AT R/H HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50 3RD VERTICAL STIFFENER PER SRM 55-10-09-2R-4 STEP 4 M;N;O;P;

ATA 5510

LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] PERFORMED CUT OUT 3RD VERTICAL STIFFENER STAB INSPAR RIB AT STA 129.50 L: .900' W: .312' IAW SRM 55-10-09-2R-4 REPAIR 4; [02] REQ NDI CUT OUT FOR FREE CRACK CONDITION; AND ALL HOLE AROUND REPAIR AREA IAW SRM 55-10-09-2R-4 REPAIR 4; [03] TTG8Q004CVKC; [04] HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16. FOUND 2 (EA) FASTENERS TO BE CRACKED; AREA MARKED. EQUIP ID#: IS000450 S/N: N500D000M120071 EQUIP ID#: ATS2407 S/N: MM1591DD064104; [05] HFEC INSPECTED CUT OUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.REPAIR ANGLE FROM MAT BAC 1490-2793 7075-T62 LOT# 1449279-1 -3 FILLER FROM MAT .040' 7075-T6 LOT# 1463598-1 -4 SHIMS 2EA FROM MAT .020' 7075-T6 LOT# J000046012 IAW SRM 55-10-09-2R-5 REPAIR 5 OK TREAT AND PRIMER; [09] VERIFIED FABRICATION OF REPAIR PARTS IN STEP 8 PER SRM. VERIFIED OK TO APPLY CONVERSION COATING AND PRIMER. [12] INSTALLED REPAIR PARTS AT L/H HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50 3RD VERTICAL STIFFENER AND LOWER CORD PER SRM 55-10-09-2R-5 REPAIR 5

ATA 5320

CRACKED SUPPORT ANGLE AT AFT CARGO BAY BS866 LBL11 WL166. ; / [01] REMOVED SUPPORT ANGLE AT AFT CARGO BAY BS866 LBL11 WL166 IAW SRM 51-10-02 ITEM 9.C; [02] LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05 <BR>OK TO INSTALL; [03] VERIFIED LOCATE AND DRILL PER 51-40-5. PRIMED AND ENAMELED ON TTG8Q004AMCD. OK TO INSTALL.; [04] INSTALLED NEW SUPPORT ANGLE AT AFT CARGO BAY BS866 LBL11 WL166 IAW SRM 51-40-02 AND DWG 149A8104; [05] VERIFIED INSTALLATION OF NEW SUPPORT ANGLE AT AFT CARGO BAY BS866 LBL11 WL166 IAW SRM 51-40-02 AND DWG 149A8104; [06] VERIFIED INSTALLATION OF NEW SUPPORT ANGLE AT AFT CARGO BAY BS866 LBL11 WL166 IAW SRM 51-40-02 AND DWG 149A8104

ATA 5320

AFT CARGO BAY SUPPORT ANGLE BEHIND WATER SERVICE PANEL CRACKED BS918 RBL12 WL170. ; / [01] REMOVED IN AFT CARGO BAY SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT BS918 RBL12 WL170 IAW SRM 51-10-02 ITEM 9.C; [02] VERIFIED APPLICABILITY NOT ALLOWABLE DAMAGE PARTS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARAGRAPH 9C.; [03] VERIFIED NO ALLOWABLE DAMAGE; REPAIRABLE BY REPLACEMENT.; [04] LOCATED AND DRILLED NEW AFT CARGO BAY SUPPORT ANGLE BEHIND WATER SERVICE PANEL BS 918 RBL12 WL170 IAW SRM 51-40-05-0G-0 AND DWG 147A7221 AND OK TO INSTALL.; [05] VERIFIED LOCATED AND DRILLED NEW AFT CARGO BAY SUPPORT ANGLE BEHIND WATER SERVICE PANEL BS 918 RBL12 WL170 IAW SRM 51-40-05-0G-0 AND DWG 147A7221. <BR>VERIFIED OK TO INSTALL.; [06] INSTALLED NEW AFT CARGO BAY SUPPORT ANGLE BEHIND WATER SERVICE PANEL BS 918 RBL12 WL170 IAW SRM 51-40-02-0G-0 AND DWG 147A7221.; [07] CORRECTED MEASUREMENTS; [08] ADDED PART REQUIEMENT; [09] VERIFIED INSTALLATION OF NEW ACB SUPPORT ANGLE ABOVE WATER SERVICE PANEL AT BS 918 RBL 12 WL 170 IAW SRM 51-40-02-0G-0 AND DWG 147A7221.; [10] VERIFIED INSTALLATION OF NEW ACB SUPPORT ANGLE ABOVE WATER SERVICE PANEL AT BS 918 RBL 12 WL 170 IAW SRM 51-40-02-0G-0 AND DWG 147A7221.; [11] CORRECTION: RETRACTING PREVIOUS STATEMENT IN CORRECTIVE ACTION #10. CORRECT STATEMENT: VERIFIED COMPLETION OF TASK CARD TTG8Q005THNH.

ATA 5320

CORROSION ON FWD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT AT BS 500D RBL 13 WL 156 ; / [01] CORROSIONON FWD CARGO BAY AFT BULKHEAD TO FLOOR AT BS 500D RBL13 WL156 MEASURES ; L=3'. X W=1.5' THE AREA SHOWS THE 100% OF MATERIAL THICKNESS LOSS; [02] CORROSIONON FWD CARGO BAY AFT BULKHEAD TO FLOOR AT BS 500D RBL13 WL156 MEASURES ; L=3'. X W=1.5' THE AREA SHOWS THE 100% OF MATERIAL THICKNESS LOSS; [03] CORROSIONON FWD CARGO BAY AFT BULKHEAD TO FLOOR AT BS 500D RBL13 WL156 MEASURES ; L=3'. X W=1.5' THE AREA SHOWS THE 100% OF MATERIAL THICKNESS LOSS MUST BE REPLACED IAW SRM 51-10-02 STEP 9.C; [04] VERIFIED CORROSIONON FWD CARGO BAY AFT BULKHEAD TO FLOOR AT BS 500D RBL13 WL156 MEASURES ; L=3'. X W=1.5' THE AREA SHOWS THE 100% OF MATERIAL THICKNESS LOSS MUST BE REPLACED IAW SRM 51-10-02 STEP 9.C; [05] LOCATED AND DRILLED AFT BULKHEAD TO FLOOR SUPPORT P/N 143A9485-35; ITEM 7530142; IAW. SRM 51-40-05; DWG# 143A9481.; [06] INSPECTED ACTION 5; [07] OK TO INSTALL .; [08] OK TO INSTALL.; [09] INSTALLED FCB AFT BULKHEAD TO FLOOR SUPPORT BS 500D RBL-24 TO LBL-24 WL-156 IAW SRM 51-40-02-0G-0 AND DWG#143A7902; [10] VERIFIED INSTALLATION OF FCB AFT BULKHEAD TO FLOOR SUPPORT BS 500D RBL-24 TO LBL-24 WL-156 IAW SRM 51-40-02-0G-0 AND DWG#143A7902; [11] ADDED PART REMOVAL IN PART REQUIREMENTS; [12] VERIFIED CARD COMPLETE; [13] UPDATED MEASUREMENTS

ATA 5315

CORROSION ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS727D+6 LBL18 TO RBL17 WL156. ; / [01] CORROSION FOUND ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS727D+6'' LBL18 TO RBL17;FOUND TO BE OUT OF LIMIT DUE TO NO LIMITS ON SRM PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9.C.; [02] CORRECTED MEASUREMENTS; [03] VERIFIED FLOOR SUPPORT SPLICE IN ACB BS 727D+6; LBL 18 TO RBL 17; WL 156 IS OUT OF LIMITS DUE TO NO LIMITS ON SRM; PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9. C.; [04] LOCATED AND DRILLED ON FLOOR SUPPORT AT SPLICE AT AFT CARGO BS 727D+6 LBL18 TO RBL 17 WL 156 IAW SRM 51-40-05 AND DWG 146A9401; [05] THE INSTALLATION WILL BE ACCOMPLISHED ON CARD# TTG8Q004AMCD; [06] VERIFIED LOCATE AND DRILL UP OF NEW SPLICE; OK TO INSTALL ON THIS CARD. VERIFIED INSTALLATION WILL NOT BE ACCOMPLISHED ON CARD# TTG8Q004AMCD; SPLICE INSTALLATION MUST BE ADDRESSED ON THIS CARD.; [07] INSTALLED NEW FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS727D+6 LBL18 TO RBL17 WL156 PER BOEING DRAWING#146A7500 REV DATE 7-31-00 REV.LTR T; [08] VERIFIED INSTALL OF NEW FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS727D+6 LBL18 TO RBL17 WL156 PER BOEING DRAWING#146A7500 REV DATE 7-31-00 REV.LTR; [09] VERIFIED ACCOMPLISHMENT OF RII INSTALL STEPS IN STEP 7 PER DWG.; [10] COMPLETE

ATA 5340

BENT STRINGER CLIP AT AFT CARGO BAY BS887 LBL5 WL165. ; / [01] REMOVED STRINGER CLIP AT AFT CARGO BAY BS887 LBL5 WL165 IAW SRM 51-10-02 ITEM 9.C; [02] LOCATED AND DRILL NEW STRINGER CLIP LOT# 1464337 AT AFT CARGO BAY BS887 LBL5 WL165 IAW SRM 51-40-05<BR>REQUEST OK TO INSTALL; [03] VERIFIED LOCATING AND DRILLING OF CLIP PER SRM AND VERIFIED OK TO INSTALL.; [04] INSTALLED STRINGER CLIP AT AFT CARGO BAY BS 887 LBL5 WL165 IN ACCORDANCE WITH SRM 51-40-02-0G-0 AND DWG 147A0060.; [05] VERIFIED INSTALLED STRINGER CLIP AT AFT CARGO BAY BS 887 LBL5 WL165.; [06] VERIFIED INSTALLED STRINGER CLIP AT AFT CARGO BAY BS 887 LBL5 WL165.

ATA 5320

CORROSION ON FWD CARGO BAY AFT BULKHEAD TO SIDEWALL SUPPORT AT BS 500D RBL 25 WL 156 ; / [01] REMOVED CORROSION ON FWD CARGO BAY AFT BULKHEAD TO SIDEWALL SUPPORT AT BS 500D RBL25 WL156 MEASURES ; L=2.5' X W=1.5' X D=0.026' MAX. MAT. LOSS IS 0.026' REMAINING THICKNESS 0.045' FOUND TO BE OUT OF LIMITS REWORKED AREA IAW SRM 53-30-08-1A-1; PARAG 4.A (2) DETAIL D USED TOOL ID:ATS1671; S/N:65093024. DUE DATE:01/2022.; [02] REMOVED CORROSION ON FWD CARGO BAY AFT BULKHEAD TO SIDEWALL SUPPORT AT BS 500D RBL25 WL156 MEASURES ; L=2.5' X W=1.5' X D=0.026' MAX. MAT. LOSS IS 0.026' REMAINING THICKNESS 0.045' FOUND TO BE OUT OF LIMITS REWORKED AREA IAW SRM 53-30-08-1A-1; PARAG 4.A (2) DETAIL D USED TOOL ID:ATS1671; S/N:65093024. DUE DATE:01/2022.; [03] INSPECTED AND VERIFIED REMOVED CORROSION ON FWD CARGO BAY AFT BULKHEAD TO SIDEWALL SUPPORT AT BS 500D RBL25 WL156 MEASURES ; L=2.5' X W=1.5' X D=0.026' MAX. MAT. LOSS IS 0.026' REMAINING THICKNESS 0.045' FOUND TO BE OUT OF LIMITS REWORKED AREA IAW SRM 53-30-08-1A-1; PARAG 4.A (2) DETAIL D; [04] LOCATED AND DRILLED AFT BULKHEAD TO SIDEWALL SUPPORT P/N 143A9485-34 IAW SRM 51-40-05 AND DWG#143A9481.; [05] AFT BULKHEAD SUPPORT WILL BE INSTALLED WITH THE CUSTOMER CARD TTG8Q004CVKC STEP#46; [06] VERIFIED STEPS 4 AND 5; [09] INSTALLED ON FWD CARGO BAY AFT BULKHEAD TO SIDEWALL SUPPORT P/N 143A9485-34; BTW BS 500D RBL 25 WL;156-WL 195.95 IAW SRM 51-40-02;DWG#143A7902;

ATA 5320

CORROSION ON SUPPORT ANGLE AT AFT CARGO BAY BS852 RBL23 WL164. ; / [01] REMOVED ANGLE AT AFT CARGO BAY BS852 RBL23 WL164.THIS PART DOES NOT HAVE ENTRY ON THE ALLOWABLE DAMAGE LIMITS THERE FOR IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9; [02] REMOVED ANGLE AT AFT CARGO BAY BS852 RBL23 WL164.THIS PART DOES NOT HAVE ENTRY ON THE ALLOWABLE DAMAGE LIMITS THERE FOR IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9; [03] REMOVED CORROSION ON INTERCOSTAL AT BS 852; RBL23; WL 164 PER SRM51-10-02-0G-0 MEASURE L=1'X W=0.75'X D=0.020' MAX. MAT LOSS IS 0.0020'; REMAINING THICKNESS IS 0.043'; ORIGINAL THICKNESS IS 0.063' FOUND TO BE OUT OF LIMITS;[05] FABRICATED SUPPORT ANGLE AT AFT CARGO BAY BS 848 TO BS 852 RBL 23 WL 164 FROM ITEM AND10134-1005#7075T73511 LOT #1464595-1 IAW SRM 51-40-05 AND DWG 146A8323 OK TO TREAT AND PRIMER; [06] VERIFIED FABRICATED SUPPORT ANGLE AT AFT CARGO BAY BS 848 TO BS 852 RBL 23 WL 164 FROM ITEM AND10134-1005#7075T73511 LOT #1464595-1 IAW SRM 51-40-05 AND DWG 146A8323 OK TO TREAT AND PRIMER; [09] INSTALLED NEW SUPPORT ANGLE AT AFT CARGO BAY BS 848 TO BS 852 RBL 23 WL 164 IAW SRM 51-40-02 AND DWG 146A83321;

ATA 5320

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727C+18 RBL20 WL156. ; / [01] EVALUATED CORROSION ON ACB SIDEWALL SUPPORT BS 727C+18'' RBL 20 WL 156 AND FOUND TO BE OUT OF LIMITS DUE TO EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 PART 4A(2); MEASURES OF CORROSION L=2.0'' X W= 1.5'' X D=0.015'' FROM ORIGINAL THICKNESS OF TH=0.040''; TOOL USED CALIPER ID:ATS2318 S/N:B19006095; DEPTH GAUGE ID: ATS2472 S/N: UNKNOWN; [02] REMOVED ACB SIDEWALL SUPPORT BS727-767 RBL 20 WL 156 IAW SRM 51-40-02-0G-0; [03] VERIFIED EVALUATED CORROSION ON ACB SIDEWALL SUPPORT BS 727C+18'' RBL 20 WL 156 AND FOUND TO BE OUT OF LIMITS DUE TO EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 PART 4A(2); MEASURES OF CORROSION L=2.0'' X W= 1.5'' X D=0.015'' FROM ORIGINAL THICKNESS OF TH=0.040''; TOOL USED CALIPER ID:ATS2318 S/N:B19006095; DEPTH GAUGE ID: ATS2472 S/N: UNKNOWN; [04] FABRICATED; LOCATED AND DRILLED ACB SIDEWALL SUPPORT BS727-767 RBL 20 WL 156 IAW SRM 51-40-05-0G-0 AND DRAWING# 146A7502;

ATA 5320

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727C+11 LBL21 WL156. ; / [01] REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727C+11 LBL21 WL 156 MAX MATERIAL LOSS L=2'; W=0.9'; D=0.006'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 146A7502 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022<BR>THIS JOB CARD WILL BE ACCOMPLISHED ON CARD ID: TTG8Q005TWAV; [02] INSPECTED AND VERIFIED REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727C+11 LBL21 WL 156 MAX MATERIAL LOSS L=2'; W=0.9'; D=0.006'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 146A7502 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022 <BR>THIS JOB CARD WILL BE ACCOMPLISHED ON CARD ID: TTG8Q005TWAV

ATA 5320

CORROSION ON SUPPORT AT AFT CARGO BAY BS767 RBL23 WL157. ; / [01] EVALUATED CORRODED AREA ON ACB SUPPORT BS767 RBL23 WL157 AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM 53-00-53-1A-2; PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9C; [02] REMOVED ACB SUPPORT BS747-767 RBL23 WL157 IAW SRM 51-40-02-0G-0; [03] VERIFIED EVALUATED CORRODED AREA ON ACB SUPPORT BS767 RBL23 WL157 AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM 53-00-53-1A-2; PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9C; [04] LOCATED AN DRILLED NEW SUPPORT AT AFT CARGO BAY BS 747 TO BS 767 RBL 23 WL 157 ITEM 7531031 PO #688683 IAW SRM 51-40-05 AND DWG 146A7500 REV A OK TO INSTALL; [05] VERIFIED LOCATED AN DRILLED NEW SUPPORT AT AFT CARGO BAY BS 747 TO BS 767 RBL 23 WL 157 ITEM 7531031 PO #688683 IAW SRM 51-40-05 AND DWG 146A7500 REV A OK TO INSTALL; [06] INSTALLED NEW SUPPORT AT AFT CARGO BAY BS 747 TO BS 767 RBL 23 WL 157 IAW SRM 51-40-02 AND DWG 146A7500 REV A; [07] VERIFIED INSTALLATION OF NEW SUPPORT AT AFT CARGO BAY BS 747 TO BS 767 RBL 23 WL 157 IAW SRM 51-40-02 AND DWG 146A7500 REV A; [08] VERIFIED INSTALLATION OF NEW SUPPORT AT AFT CARGO BAY BS 747 TO BS 767 RBL 23 WL 157 IAW SRM 51-40-02 AND DWG 146A7500 REV A

ATA 5320

CORROSION ON WEB AT AFT CARGO BAY BS809 RBL19 WL159. ; / [01] REMOVED CORROSION ON ACB WEB BS809 RBL 19 WL 159 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PART 4G(2); MEASURES OF MATERIAL REMOVED L=1.0'' X W=1.0'' X D=0.016'' ORIGINAL THICKNESS TH=0.056'' TOOL USED CALIPER ID:ATS1317 S/N:UNKNOWN; MICROMETER ID:ATS1672 S/N:65092939. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9; [02] VERIFIED REMOVED CORROSION ON ACB WEB BS809 RBL 19 WL 159 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PART 4G(2); MEASURES OF MATERIAL REMOVED L=1.0'' X W=1.0'' X D=0.016'' ORIGINAL THICKNESS TH=0.056'' TOOL USED CALIPER ID:ATS1317 S/N:UNKNOWN; MICROMETER ID:ATS1672 S/N:65092939. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9; [03] THE REPLACEMENT OF ACB WEB BS787-847 RBL19 WL159 IS DOCUMENTED ON TASK CARD TTG8Q005TL9W; [04] VERIFIED REPLACEMENT OF ACB WEB AT BS 809; RBL 19; WL 159 WILL BE ACCOMPLISHED ON TTG8Q005TL9W.

ATA 5320

CORROSION ON WEB AT AFT CARGO BAY BS824 RBL19 WL159. ; / [01] REMOVED CORROSION ON ACB WEB BS824 RBL 19 WL 159 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PART 4G(2); MEASURES OF MATERIAL REMOVED L=1.0'' X W=1.0'' X D=0.014'' ORIGINAL THICKNESS TH=0.056'' TOOL USED CALIPER ID:ATS1317 S/N:UNKNOWN; MICROMETER ID:ATS1672 S/N:65092939. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9; [02] VERIFIED REMOVED CORROSION ON ACB WEB BS824 RBL 19 WL 159 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PART 4G(2); MEASURES OF MATERIAL REMOVED L=1.0'' X W=1.0'' X D=0.014'' ORIGINAL THICKNESS TH=0.056'' TOOL USED CALIPER ID:ATS1317 S/N:UNKNOWN; MICROMETER ID:ATS1672 S/N:65092939. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9; [03] THE REPLACEMENT OF ACB WEB BS787-847 RBL19 WL159 IS DOCUMENTED ON TASK CARD TTG8Q005TL9W; [04] VERIFIED REPLACEMENT OF ACB WEB AT BS 824; RBL 19; WL 159 WILL BE ACCOMPLISHED ON TTG8Q005TL9W.

ATA 5320

CORROSION ON WEB AT AFT CARGO BAY BS839 RBL19 WL159. ; / [01] REMOVED CORROSION ON ACB WEB BS839 RBL 19 WL 159 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PART 4G(2); MEASURES OF MATERIAL REMOVED L=5.0'' X W=1.0'' X D=0.018'' ORIGINAL THICKNESS TH=0.056'' TOOL USED CALIPER ID:ATS1317 S/N:UNKNOWN; MICROMETER ID:ATS1672 S/N:65092939. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9; [02] VERIFIED REMOVED CORROSION ON ACB WEB BS839 RBL 19 WL 159 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PART 4G(2); MEASURES OF MATERIAL REMOVED L=5.0'' X W=1.0'' X D=0.018'' ORIGINAL THICKNESS TH=0.056'' TOOL USED CALIPER ID:ATS1317 S/N:UNKNOWN; MICROMETER ID:ATS1672 S/N:65092939. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9; [03] THE REPLACEMENT OF ACB WEB BS787-847 RBL19 WL159 IS DOCUMENTED ON TASK CARD TTG8Q005TL9W; [04] VERIFIED REPLACEMENT OF ACB WEB AT BS 839; RBL 19; WL 159 WILL BE ACCOMPLISHED ON TTG8Q005TL9W.

ATA 5320

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS761 - BS787 LBL21 WL156. ; / [01] REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS761 - BS787 LBL21 WL 156 MAX MATERIAL LOSS L=3'; W=2'; D=0.009'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 146A7502 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022 <BR>THIS JOB CARD WILL BE ACCOMPLISHED ON CARD ID: TTG8Q005TWAV; [02] INSPECTED AND VERIFIED REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS761 - BS787 LBL21 WL 156 MAX MATERIAL LOSS L=3'; W=2'; D=0.009'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 146A7502 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022 <BR>THIS JOB CARD WILL BE ACCOMPLISHED ON CARD ID: TTG8Q005TWAV

ATA 5320

CORROSION ON WEB AT AFT CARGO BAY BS797 RBL19 WL159. ; / [01] REMOVED CORROSION ON ACB WEB BS797 RBL 19 WL 159 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PART 4G(2); MEASURES OF MATERIAL REMOVED L=3.0'' X W=1.0'' X D=0.015'' ORIGINAL THICKNESS TH=0.056'' TOOL USED CALIPER ID:ATS1317 S/N:UNKNOWN; MICROMETER ID:ATS1672 S/N:65092939. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9; [02] VERIFIED REMOVED CORROSION ON ACB WEB BS797 RBL 19 WL 159 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PART 4G(2); MEASURES OF MATERIAL REMOVED L=3.0'' X W=1.0'' X D=0.015'' ORIGINAL THICKNESS TH=0.056'' TOOL USED CALIPER ID:ATS1317 S/N:UNKNOWN; MICROMETER ID:ATS1672 S/N:65092939. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9; [03] REMOVED ACB WEB FROM BS794 - BS847 RBL 21 IAW SRM 51-40-02; [04] LOCATED AND DRILLED ACB WEB BS794 - BS847 RBL19 IAW SRM 51-40-05-0G-0 AND DRAWING#146A8123.<BR>OK TO INSTALL; [05] VERIFIED LOCATE & DRILL OF ACB WEB AT BS 794 - BS 847 RBL 19 IAW SRM 51-40-05-0G-0 AND DRAWING# 146A8123.<BR>OK TO INSTALL GIVEN.; [06] INSTALLED ACB WEB FROM BS 794 - BS847 RBL 19 IAW SRM 51-40-02 AND IAW DWG# 146A8121; [07] VERIFIED INSTALLATION OF ACB WEB FROM BS 794 - BS847 RBL 19 IAW SRM 51-40-02 AND IAW DWG# 146A8121

ATA 5320

CORROSION ON WEB AT AFT CARGO BAY BS831 RBL19 WL159. ; / [01] REMOVED CORROSION ON ACB WEB BS831 RBL 19 WL 159 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PART 4G(2); MEASURES OF MATERIAL REMOVED L=2.0'' X W=1.0'' X D=0.017'' ORIGINAL THICKNESS TH=0.056'' TOOL USED CALIPER ID:ATS1317 S/N:UNKNOWN; MICROMETER ID:ATS1672 S/N:65092939. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9; [02] VERIFIED REMOVED CORROSION ON ACB WEB BS831 RBL 19 WL 159 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PART 4G(2); MEASURES OF MATERIAL REMOVED L=2.0'' X W=1.0'' X D=0.017'' ORIGINAL THICKNESS TH=0.056'' TOOL USED CALIPER ID:ATS1317 S/N:UNKNOWN; MICROMETER ID:ATS1672 S/N:65092939. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9; [03] THE REPLACEMENT OF ACB WEB BS787-847 RBL19 WL159 IS DOCUMENTED ON TASK CARD TTG8Q005TL9W; [04] VERIFIED REPLACEMENT OF ACB WEB AT BS 831; RBL 19; WL 159 WILL BE ACCOMPLISHED ON TTG8Q005TL9W.

ATA 5320

CORROSION ON FWD CARGO BAY AFT SHIELD AT BS 497-519 RBL 24 WL 156 ; / [01] NO ENTRIES ALLOWABLE DAMAGE IN SRM PART MUST BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 STEP 9.C; [02] VERIFIED ITEM 1 CORRECTIVE ACTION.; [03] LOCATED AND DRILLED SHIELD WITH P/N 143A8126-31; LOT.1461424 IAW SRM 51-40-05; DWG#143A8126; [04] THE SHIELD WILL BE INSTALLED ON THE CUSTOMER CARD # TTG8Q004CVKC STEP # 44; [05] INSPECTED AND VERIFIED LOCATED AND DRILLED SHIELD WITH P/N 143A8126-31; LOT.1461424 IAW SRM 51-40-05; DWG#143A8126. THE SHIELD WILL BE INSTALLED ON THE CUSTOMER CARD # TTG8Q004CVKC STEP # 44; [06] OK TO INSTALL.; [07] OK TO INSTALL.; [08] INSTALLED ON FWD CARGO BAY AFT SHIELD P/N 143A8126-31;LOT.1461424 BTW. BS 500-500A;RBL 24; WL 156; IAW SRM 51-40-02; DWG#143A0080; [09] VERIFIED INSTALLATION OF FWD CARGO BAY AFT SHIELD P/N 143A8126-31;LOT.1461424 BTW. BS 500-500A;RBL 24; WL 156; IAW SRM 51-40-02; DWG#143A0080; [10] CORRECTED MEASUREMENTS; [11] ADDED PART REQUIREMENT; [12] VERIFIED; CONFIRMED JOB COMPLETE; [13] NO REFERENCE SELECTED; CORRECT REFERENCE IS SRM 53-30-15-1A-1-A00071 (PERMANENT (NON-DENT DAMAGE TYPES))

ATA 5315

CORROSION ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS887 LBL3 TO RBL8 WL169. ; / [01] CORROSION FOUND ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS887 LBL3 TO RBL8 WL169;FOUND TO BE OUT OF LIMIT DUE TO NO LIMITS ON SRM PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9.C.; [02] CORRECTED MEASUREMENTS; [03] VERIFIED FLOOR SUPPORT SPLICE IN ACB BS 887; LBL 3 TO RBL 8; WL 169 IS OUT OF LIMITS DUE TO NO LIMITS ON SRM; PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9. C.; [04] THIS DISCREPANCY WILL ACCOMPLISHED ON CARD #TTG8Q005TWAE; [05] UPDATED PARTS INFO.; [06] VERIFIED CORRECTIVE ACTION 4 & 5 REPLACEMENT OF PART TO BE ON ACCOMPLISHED ON TTG8Q005TWAE.<BR><BR>NO FURTHER ACTIONS REQUIRED.

ATA 5320

CORROSION ON AFT SHIELD AT AFT CARGO BAY BS856 RBL21 WL164. ; / [01] EVALUATED ACB SHIELD BS856 RBL21 WL164 AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM 53-60-15-1A-1; PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9C; [02] REMOVED ACB SHIELD BS847-867 RBL21 WL164 IAW SRM 51-40-02-0G-0; [03] VERIFIED EVALUATED ACB SHIELD BS856 RBL21 WL164 AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM 53-60-15-1A-1; PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9C; [04] RECIVED NEW SHIELD ITEM 146A8127Y10 LOT 1463083-1 LOCATED AND DRILLED NEW SHIELD AT BS 856; RBL 21; WL164; IAW 737-700 SRM 51-40-05-OG-0 DWG146A0081; [05] VERIFIED; CONFIRMED LOCATE AND DRILL UP OF NEW SHIELD; OK TO PROCEED; [06] APPLIED ONE COAT OF BMS10-11 TYPE II ENAMEL ON NEW SHIELD PER SOPM 20-41-02 ; OK TO INSTALL; [07] VERIFIED APPLICATION OF ONE COAT OF BMS10-11 TYPE II ENAMEL ON NEW SHIELD PER SOPM 20-41-02 ; OK TO INSTALL; [08] INTALED NEW SHIELD AT AFT BS 856 RBL 21 WL64 IWA 737-700 SRM 51-40-02-GO-0 DWG 146A081.ALL REQUIRED MAINTENANC ACTION ARE COMPLETE = REQUEST FINAL BUYOFF.-; [09] CORRECTION WL164; [10] PART USAGE INFO; [11] VERIFIED ACTION 8; 9; [12] VERIFIED ACTION 8; 9

ATA 5320

CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767 - BS787 RBL21 WL157. ; / [01] EVALUATED ACB SHIELD BS767-787 RBL21 WL157 AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM 53-60-15-1A-1; PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9C; [02] REMOVED ACB SHIELD BS767-787 RBL21 WL157 IAW SRM 51-40-02-0G-0; [03] VERIFIED EVALUATED ACB SHIELD BS767-787 RBL21 WL157 AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM 53-60-15-1A-1; PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9C; [04] RECIVED NEW SHIELD ITEM 7531132 P/N 146A8127-12 LOCATED AND DRILLED NEW SHIELD AT BS 767 - BS 787; RBL21; WL 157 ; IAW B 737-700 SRM 51-40-05-OG-0 DWG 146A0081.-; [05] UPDATED PARTS USAGE; [06] INSPECTED RECIVED NEW SHIELD ITEM 7531132 P/N 146A8127-12 LOCATED AND DRILLED NEW SHIELD AT BS 767 - BS 787; RBL21; WL 157 ; IAW B 737-700 SRM 51-40-05-OG-0 DWG 146A0081.-; [07] APPLIED ONE COAT OF BMS10-11 TYPE II ENAMEL ON NEW SHIELD PER SOPM 20-41-02 ; OK TO INSTALL; [08] VERIFIED APPLICATION OF ONE COAT OF BMS10-11 TYPE II ENAMEL ON NEW SHIELD PER SOPM 20-41-02 ; OK TO INSTALL; [09] INTALED NEW SHIELD AT AFT BS 7767 RBL 21 WL157 IWA 737-700 SRM 51-40-02-GO-0 DWG 146A081.ALL REQUIRED MAINTENANC ACTION ARE COMPLETE = REQUEST FINAL BUYOFF.-; [10] VERIFIED ACTION 9; [11] VERIFIED ACTION 9; [12] CORRECTION FOR CORRECTIVE ACTION 9: INSTALLED NEW SHIELD AT BS 767-787 RBL 21; WL 157 PER AMM 51-40-02-0G-0 AND DWG 146A0081

ATA 5320

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 441 TO 458 LBL 24 WL 156 ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 400+6'; LBL24; WL 156 PER SRM51-10-02-0G-0 MEASURE L=1'X W=0.75'X D=0.006' MAX. MAT LOSS IS 0.006'; REMAINING THICKNESS IS 0.006'; ORIGINAL THICKNESS IS 0.040' (BAC1496-444) FOUND TO BE OUT OF LIMITS; REWORKED AREA PER B737-700 SRM53-00-53-1A-2; ALLOWABLE DAMAGE PARAG. 4.A [07] FABRICATED; LOCATED AND DRILLED NEW FCB SIDEWALL SUPPORT BS396-500D LBL24 WL156 IAW SRM 51-40-05-0G-0 AND DRAWING# 143A7501; MATERIAL USED BAC1496-444 7075-T6 LOT#1453146-2.<BR>FABRICATED; LOCATED AND DRILLED SPLICE REPAIR AT SIDEWALL SUPPORT BS490 LBL24 WL156 IAW SRM 53-00-53-2R-6 REPAIR#6 MATERIAL USED BAC1496-444 7075-T6 LOT#1453146-2.<BR>OK TO TREAT AND PRIME; [08] CORRECTED REPAIR TYPE TO MAJOR REPAIR.12] OK TO INSTALL NEW FLOOR TO SIDEWALL SUPPORT FROM BS400 TO BS500D LBL24 WL156; [13] VERIFIED CORRECTIVE ACTION ITEM 12. OK TO INSTALL; [14] INSTALLED NEW FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS400 TO BS500D LBL24 WL156 IAW SRM 51-40-02-0G-0 AND DWG #143A7500;

ATA 5320

FLOOR TO SIDEWALL SUPPORT HAS DAMAGE AT AFT CARGO BAY BS727E LBL21 WL156. MARKED ; / [01] REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727C+11 LBL21 WL 156 MAX MATERIAL LOSS L=2'; W=1'; D=0.007'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 146A7502 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022 <BR>THIS JOB CARD WILL BE ACCOMPLISHED ON CARD ID: TTG8Q005TWAV; [02] CORRECTION; BS727E; [03] INSPECTED AND VERIFIED REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727C+11 LBL21 WL 156 MAX MATERIAL LOSS L=2'; W=1'; D=0.007'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4A(2)(A) FIG 103 AND DWG 146A7502 TOOL USED ID:ATS1672 S/N:65092939 DUE 03/2022 <BR>THIS JOB CARD WILL BE ACCOMPLISHED ON CARD ID: TTG8Q005TWAV

ATA 5310

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. ; / [01] DAMAGED AT EXISTING REPAIR FOUND TO BE OUT OF LIMITS NO ALLOWABLE DAMAGE FOUND AT SRM; [02] ADDING SRM REFERENCE USED: SRM 53-10-51-1A-1; [03] CORRECTING MEASUREMENT FOR SHORTEST/DEPTH (RATIO); [04] REMOVED EXISTING REPAIR FROM FLIGHT DECK FLOOR BETWEEN BS 250 TO BS 270 LBL 20 TO LBL 10 WL 207.54 PER SRM 51-40-02; [05] FABRICATED -1 REPLACEMENT WEB FROM 2024T3 .040 LOT # 1463135-1 ; FABRICATED DOUBLER -2 AND -3 FROM 2024T3 .050 LOT # 1459974-1 AT FLIGHT DECK FLOOR BETWEEN LBL 20 TO RBL 10 WL207.54 BS 250 TO BS 270; FABRICATED DOUBLER -2 AND -3 FROM 2024T3 .050 LOT # 1459974-1 AT FLIGHT DECK FLOOR BETWEEN LBL 20 TO RBL 10 WL207.54 BS 250 TO BS 270; APPLIED CHEMICAL CONVERSION COATING AT REPAIR PARTS REFERENCE SWA EA 1-753-34875 REV. IR. OK TO APPLY PRIMER ON PARTS;[12] INSTALLED NEW REPAIR PARTS ON FLIGHT DECK FLOOR BETWEEN BS 250 TO BS 270 LBL 20 TO RBL 10 WL 207.54 IAW SRM 51-40-02-OG-0; EA NO: 1-753-34875 REV IR AND APPLIED FILLET SEAL OF BMS 5-95 SEALANT AROUND THE EDGES OF THE REPAIR PER 737-700 SRM 51-20-05 AND EA NO:1-753-34875 REV IR. OK TO APPLY CIC AND PAINT; [13] INSTALLED NEW REPAIR PARTS ON FLIGHT DECK FLOOR BETWEEN BS 250 TO BS 270 LBL 20 TO RBL 10 WL 207.54 IAW SRM 51-40-02-OG-0;ESR:21-02218; EA NO: 1-753-34875

ATA 5330

FUSELAGE AFT SKIN PANEL AT BUTT JOINT BS 1016 HAS CORROSION BETWEEN STR 21L - 22L ; / [01] REMOVED PAINT AT DISCREPANCY AREA PER REF AMM 51-21-11; [02] REMOVED FASTENERS AT DISCREPANCY AREA PER REF SRM 51-40-02; [03] REMOVED CORROSION AT DISCREPANCY AREA PER SRM 53-00-01-1A-1; [04] (10EA) FASTENERS WERE REMOVED FROM BLENDED OUT AREA PER REF SRM 51-40-02; [05] PERFORMED VISUAL INSPECTION WITH A 10X MAGNIFYING GLASS AT DISCREPANCY AREA PER REF SRM 51-10-02-0G-0. NO ADDITIONAL DAMAGE NOTICE.; [06] PERFORMED VISUAL INSPECTION WITH A 10X MAGNIFYING GLASS AT DISCREPANCY AREA PER REF SRM 51-10-02-0G-0. NO ADDITIONAL DAMAGE NOTED.; [07] ET INSPECTED BLEND/HOLES/COUNTERSINKS IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; PROCEDURE 16 AND 737 NDTM PART 6 53-30-00 PROCEDURE 3; NO CRACKS NOTED.<BR>CAL ID IS000450 N500D<BR>UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.075'<BR>CAL ID ATS2031 E650; [08] VERIFIED CORROSION RMOVAL; [09] VERIFIED DIMENSIONS L=7 W=1.5 ORIGINAL MATERIAL THICKNESS IS

ATA 5330

FUSELAGE EXTERNAL SKIN HAS A DENT AT BS 500C+9'; 2.3' ABOVE STR 5R. ; / [01] REMOVED DECORATIVE EXTERIOR PAINT AT DISCREPANCY AREA TO FOM PER AMM 51-21-11; [02] EVALUATED DENT AT DISCREPANCY AREA L= 1.5' W=1.3' FOUND TO BE OUT OF LIMITS DUE TO BLEND OUT (AREA L=1.2 W=0.9') AT DENT AREA PER SRM 53-00-01-1A-1 FIG 103 DETAIL G.; [03] PERFORMED EXTERNAL GVI AT DISCREPANCY AREA PER SRM 51-00-06. NO ADDITIONAL DAMAGE NOTED; [04] PERFORMED EXTERNAL GVI AT DISCREPANCY AREA PER SRM 51-00-06. NO ADDITIONAL DAMAGE NOTED; [05] VERIFIED OUT OF LIMITS; [06] ET INSPECTED BLEND IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. <BR>CAL ID IS000450 <BR>UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.036' <BR>CAL ID ATS2031 E650; [07] VERIFY DAMAGE DIMENSION AT DENT L=1.5' W=1.3' Y=0.025' W/Y=52 AT BLEND OUT ORIGINAL THICKNESS 0.040' REMAINING 0.036' MAX LOSS 0.004' PER SRM 53-00-01-1A-1. PIT AND DENT GAUGE ID ATS2607 S/N F00387 DUE 04/2022; [08] VERIFIED VERIFY DAMAGE DIMENSION AT DENT L=1.5' W=1.3' Y=0.025' W/Y=52 AT BLEND OUT ORIGINAL THICKNESS 0.040' REMAINING 0.036' MAX LOSS 0.004' PER SRM 53-00-01-1A-1.; [09] APPLIED DECORATIVE EXTERIOR PAINT AT DISCREPANCY AREA PER SRM 51-21-99.; [10] VERIFIED DECORATIVE EXTERIOR PAINT AT DISCREPANCY AREA PER SRM 51-21-99.;; [12] AS PER EA 21-153-02055; THE DAMAGE IS ALLOWABLE FOR CONTINUED SERVICE WITH AN INSPECTION THRESHOLD DEFINED ON 21-153-02055-DTI.

ATA 5330

FUSELAGE EXTERNAL SKIN HAS A CORROSION AT 1089 BETWEEN STR 18LH- STR 21LH ; / [01] REMOVED PAINT AT DISCREPANCY AREA PER REF AMM 51-21-11; [02] REMOVED CORROSION AT DISCREPANCY AREA PER REF SRM 51-10-02-0G-004] ET INSPECTED BLEND/HOLES/COUNTERSINKS IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; PROCEDURE 16 AND PART 6 53-30-00 PROCEDURE 3; NO CRACKS NOTED.<BR>CAL ID IS000450 N500D<BR>UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.075'<BR>CAL ID ATS2031 E650; [05] VERIFIED BLEND OUT L=2.5'' W=1.5'' ORIGINAL MATERIAL THICKNESS IS .080'' AND REMAINING THICKNESS IS .075''. THE MATERIAL REMOVAL IS LOCATED IN A 2ND ROW OF A 2-ROW BUTT. THEREFORE FOUND TO BE OUT LIMITS PER REF SRM 53-00-01-1A-1 FIG.103 DETAIL E.; [06] VERIFIED DIMENSIONS FOUND TO OUT OF LIMITS PER SRM 53-00-01-1A-1 FIG.103 DETAIL E.; [07] REMOVED 2EA EXTRA FASTENERS (TOTAL 4EA FASTENERS REMOVED) AT BLEND AREA BELOW STR 17L COMMON TO SHEAR TIE PER SRM 51-40-02; [08] INSTALLED 4 EA FASTENERS AT DISCREPANCY AREA PER EA 21-153-02081-WIP1 AND SRM 51-40-02;

ATA 5330

FUSELAGE EXTERNAL SKIN HAS CORROSION AT BS 1089 AROUND PRIMARY JACK POINT 'C' ; / [01] REMOVED PAINT AT DISCREPANCY AREA PER REF AMM 51-21-11; [02] REMOVED CORROSION AT DISCREPANCY AREA L=3.7' W=2.7' PER SRM 51-40-02; [03] STEP 2 REFERENCE ENTRY AND ERROR. REMOVED CORROSION AT DISCREPANCY AREA L=3.7' W=2.7' PER SRM 51-10-02; [04] REMOVED 4 EA FASTENERS AT REWORKED AREA PER SRM 51-40-02; [05] PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS TO MAKE SURE ALL OF THE CORROSION WAS REMOVED PER SRM 51-10-02 PARAGRAPH 15.A.6.A; [06] VERIFIED CORROSION REMOVAL PER SRM 51-10-02 PARAGRAPH 15.A.6.A; [07] ET INSPECTED BLEND/HOLES/COUNTERSINKS IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; PROCEDURE 16 AND 737 NDTM PART 6 53-30-00 PROCEDURE 3; NO CRACKS NOTED. <BR>CAL ID IS000450 N500D <BR>UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.075' <BR>CAL ID ATS2031 E650; [08] EVALUATED CORROSION REMOVAL AT DISCREPANCY AREA L=3.7' W=2.7' ORIGINAL MATERIAL THICKNESS 0.080' REMAINING 0.075' MAX LOSS 0.005' FOUND TO BE OUT OF LIMITS DUE TO REMOVAL OF MATERIAL AROUND MORE THAN 3 FASTENERS IN ALL GROUPS OF TEN PER SRM 53-00-01-1A-1 FIG 103 DETAIL D.; [09] VERIFIED CORROSION REMOVAL AT DISCREPANCY AREA L=3.7' W=2.7' ORIGINAL MATERIAL THICKNESS 0.080' REMAINING 0.075' MAX LOSS 0.005' FOUND TO BE OUT OF LIMITS DUE TO REMOVAL OF MATERIAL AROUND MORE THAN 3 FASTENERS IN ALL GROUPS OF TEN PER SRM 53-00-01-1A-1 FIG 103 DETAIL D.;

ATA 5330

FUSELAGE AFT SKIN PANEL AT BUTT JOINT BS 1016 HAS CORROSION BETWEEN STR 24L - 24R ; / [01] REMOVED PAINT AT DISCREPANCY AREA PER REF AMM 51-21-11; [02] REMOVED CORROSION AT DISCREPANCY AREA PER REF SRM 53-00-01-1A-1; [03] REMOVED 11EA FASTENERS AT BLENDED AREA PER REF SRM 51-40-02; [04] CORROSION REMOVAL SRM REFERENCE 51-10-02; [05] PERFORMED VISUAL INSPECTION WITH A 10X MAGNIFYING GLASS AT DISCREPANCY AREA PER REF SRM 51-10-02-0G-0. NO ADDITIONAL DAMAGE NOTICE.; [06] VERIFIED ACTION 5 NO ADDITIONAL DAMAGE FOUND; [07] ET INSPECTED BLEND/HOLES/COUNTERSINKS IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; PROCEDURE 16 AND PART 6 53-30-00 PROCEDURE 3; NO CRACKS NOTED. <BR>CAL ID IS000450 <BR>UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.076'<BR>CAL ID ATS2031 E650; [08] VERIFIED BLEND OUT L=11 W=2 ORIGINAL MATERIAL THICKNESS IS .080'' AND LOWEST THICKNESS IS .076''. MATERIAL REMOVAL IS LOCATED IN THE 2ND ROW OF A 2-ROW BUTT; THEREFORE FOUND TO BE OUT OF LIMITS PER REF SRM 53-00-01-1A-1 FIG. 103 DETAIL E; [09] RE-VERIFIED BLEND OUT AREA L= 27'' AND W=2'';

ATA 5754

CRACK IN #5 SLAT LOWER SKIN NEAR ACTUATOR FITTING ATTACH FASTENER ; / [01] HFEC INSPECTED CRACK ON #5 SLAT LOWER SKIN IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; AREA MARKED. EQUIP ID#: IS000450 S/N: N500D000M120071; [02] REMOVED HI LOCK AT #5 SLAT LOWER SKIN NEAR ACTUATOR FITTING ATTACH AND OVERSIZE HOLE TO 0.215 IAW SRM 51-40-02.; [03] HFEC REQUEST ON OPEN HOLE; SLAT LOWER SKIN AND ACTUATOR FITTING FOR FREE CRACK CONDITION.; [04] ET INSPECTED HOLE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; CRACK STILL NOTED IN SKIN.18] FABRICATED REPAIR PARTS: DOUBLER; MADE FROM CLAD 7075-T6 #0.071' LOT#1459410-1 AND FILLER MADE FROM CLAD 7075-T6 0.063'; LOT#1418646-2. APPLIED CHEMICAL CONVERSION COATING. IAW SRM 51-20-01-0G-0 AND SRM 57-42-01-2R-8 STEP 4E THRU 4J. OK TO PRIMER.; [19] VERIFIED FABRICATION OF REPAIR PARTS: DOUBLER & FILLER FROM CLAD 7075-T6 0.071' LOT# 1459410-1 AND FROM CLAD 7075-T6 0.063' LOT# 1418646-2. VERIFIED APPLICATION OF CHEMICAL CONVERSION COATING. ALL IAW SRM 51-20-01-0G-0 & SRM 57-42-01-2R-8 STEP 4. E.-4. J.<BR>OK TO APPLY PRIMER GIVEN.;

ATA 5321

AFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS. /

ATA 5321

FWD FLOOR PANEL 222DF HAS 2 AREAS OF EDGE DAMAGE. (MARKED) /

ATA 5321

FWD FLOOR PANEL 222DF HAS DAMAGED INSERTS. /

ATA 5321

FWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS. /

ATA 5321

FWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS. /

ATA 5321

FWD FLOOR PANEL 221CF HAS DAMAGED INSERTS. /

ATA 5321

FWD FLOOR PANEL 221AF UPPER SKIN HAS AREAS OF PULLED STRANDS. /

ATA 5321

FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS. /

ATA 3350

RT SIDE EMERGENCY OVERWING EXIT SIGN ARROW WAS POINTING WRONG. / INSTALLED CORRECT EXIT SIGN PER MM.

ATA 2565

R1 DOOR SLIDE GIRT FLAP HUNG UP ON THRESHOLD DUE TO FASTENER MISSING. REPOSITIONED SLIDE PER MT.

ATA 2565

R1 DOOR ESCAPE SLIDE WAS NOT PACKED CORRECTLY. GIRT BAR WAS HANGING DOWN TO FAR. SECURED SLIDE PER MT.

ATA 2560

L2 DOOR SLIDE GIRT NEEDS REINSTALLED, TOO LONG. REATTACHED GIRT PER MT.

ATA 3350

EMERGENCY EXIT LIGHT AFT OF L1 DOOR INOP. REPAIRED EXIT LIGHT ELEC WIRING PER AMM.

ATA 5320

ATS RESPONSIBILITY WHILE WORKING SEAT TRACK FOUND STRAP AT BS 867-887 RBL 45 WL 207 TO HAVE 4 EA ELONGATED FASTENER HOLES / ACCOMPLISHED HIDDEN DAMAGE INSP.; REF. SRM 51-10-02-0G-0; NO ADDTIONAL DEFECTS NOTED. INSP 107 05-06-19 LOCATED AND DRILLED REPLACMENT STRAP AT BS867-887 RBL 45 IAW SRM 51-40-05-0G-0 AND PRIMED IAW 51-21-72 56173U 10MAY19 OK TO INSTALL. 56173U 10MAY19 INSP 34 10MAY19 INSTALLED NEW STRAP AT BS 867-887 RBL 45 IAW SRM 51-40-02-0G-0 STEP 7 AND REFERENCING BOEING DWG #146A5300 57264U 05/10/2019

ATA 5730

PANEL 521KB HAS DELAMINATION AT FORWARD CORNERS OF CUTOUT / PANEL 521KB WITH DELAMINATION AT FORWARD CORNERS OF CUTOUT WAS REPAIRED IAW SRM 51-70-05-2R-6. 59702U 05/09/19

ATA 5750

R/W T/E WIGGLE STRIP AT ORSS 261 HAS SHEARED RIVETS AND IS CRACKED.. / REMOVED & REPLACED R/W T/E WIGGLE STRIP PER SRM 51-40-02-0G-0 STEPS 4.A.& B.

ATA 5720

L/W T/E UPPER SEAL RETAINER IS CRACKED ON THE NO STEP PANEL ORSS 271. / REMOVED AND REPLACED SEAL RETAINER BRACKET ON LH T/E UPR NO STEP PANEL AT STA 271 PER SRM 51-40-02-0G-0; STEP 4;9.

ATA 3397

MID CABIN OVERHEAD EMERGENCY EXIT LOCATOR SIGN CONNECTOR D12030 DAMAGED. R&R CONNECTOR PER SWPM AND WDM.

ATA 5320

AFT CARGO BAY FORWARD CORNER THRESHOLD CRACKED. R&R THRESHOLD IAW AMM & EA.

ATA 5320

FORWARD CARGO DOOR FORWARD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

ATA 5320

FORWARD CARGO DOOR AFT CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

ATA 5347

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

ATA 3350

R1 DOOR LOWER FORWARD EMERGENCY EXIT LIGHT HOUSING BROKEN. R&R LIGHT HOUSING IAW AMM.

ATA 2565

L1 DOOR SLIDE OUT OF POSITION IN SLIDE COMPARTMENT. REPOSITIONED SLIDE PER MT.

ATA 2560

FORWARD L1 DOOR GIRT BAR RETAINER CLIP RIVET SHEARED. R&R FASTENER IAW EA AND DWG.

ATA 3350

LT OVER WING EMERGENCY LIGHTS INOP. R&R LIGHTS IAW AMM.

ATA 3350

LT EMERGENCY LIGHTS INOP BETWEEN ROW 13 TO ROW 17 (M1670). R&R LIGHTS IAW AMM.

ATA 2910

DIVERSION, NR 1 ENGINE "LOW PRESSURE" A HYDRAULIC PUMP ILLUMINATED. R&R NR 1 ENGINE HYDRAULIC PRESSURE LINE PER AMM.

ATA 5720

UPPER FIXED T/E PNL AT RT WS 278.50 HAS CRACKED SUPPORT BRACKET AT DEFLECTION ROLLER SUPPORT FITTING / REMOVED AND REPLACED CRACKED SUPPORT BRACKET AT RIGHT WING STATION 278.5 PER SRM 51-40-02.

ATA 5720

RT WING UPPER FIXED TRAILING EDGE PANEL SUPPORT BRACKET CRACKED AT WING STA 278.50. R&R BRACKET PER SRM.

ATA 3350

L2 DOOR EXIT LIGHT LENS MISSING. REPLACED THE LENS IAW MM.

ATA 3350

FORWARD BULKHEAD EMERGENCY EXIT LIGHT INOP. INSTALLED BATTERY PACK PER MM.

ATA 3350

FORWARD BULKHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

ATA 3350

AFT BULKHEAD EMERGENCY EXIT LIGHT INOP. INSTALLED BATTERY PACK PER MM.

ATA 3350

AFT BULKHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

ATA 2560

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET OUT OF ADJUST. ADJUSTED BRACKET PER SIP.

ATA 5310

UPPER SURFACE OF CREASE BEAM WEB CORRODED AT BS 705. R & R CREASE BEAM WEB IAW SRM AND DWG.

ATA 5320

FORWARD GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R GUSSET IAW SRM & DWG.

ATA 5320

FORWARD GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R THE GUSSET IAW SRM.

ATA 5320

FLOOR SUPPORT CRACKED AT BS 344 TO 360, LBL 11, WL 207. R & R THE FLOOR SUPPORT IAW SRM.

ATA 5320

FLOOR SUPPORT CRACKED AT BS 344 TO 360, BL 0, WL 207. R & R THE FLOOR SUPPORT IAW SRM.

ATA 5320

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, LBL 46. R & R THE FLOOR SUPPORT IAW SRM.

ATA 5320

AFT CARGO BAY SUB THRESHOLD WEB CORRODED. R & R THE WEB IAW SRM & DWG.

ATA 3350

LEFT EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED THE LENS IAW MM.

ATA 2560

R1 DOOR SLIDE GIRT BAR LOOSE. SECURED THE GIRT BAR HOLDING BRACKET IAW SIP.

ATA 3350

L2 DOOR OVERHEAD EMERGENCY EXIT SIGN BULB INOPERATIVE. R & R BULB IAW AMM.

ATA 3350

AFT CABIN OVERHEAD EMER EXIT SIGN LOOSE. R & R SIGN IAW MM.

ATA 5320

FLOORBOARD SUPPORT CRACKED AT BS 540, BL 0. R & R SUPPORT IAW SRM.

ATA 5312

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN RBL 34 - RBL 35. REPAIRED WEB IAW SRM.

ATA 5312

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN RBL 42 - RBL 43. REPAIRED WEB IAW SRM.

ATA 3350

LEFT AFT OF WING TO BODY EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

ATA 2565

L2 DOOR EMER DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW SIP.

ATA 5320

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, RBL 45. REPAIRED IAW EA.

ATA 5320

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 25. REPAIRED IAW EA.

ATA 5320

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 45. REPAIRED IAW EA.

ATA 5320

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, RBL 45. REPAIRED IAW EA.

ATA 5514

LEFT HORIZONTAL STAB RIB STIFFENER CRACKED AT STATION 101.39. REPAIRED STIFFENER IAW SRM.