N551WN

BOEING 737 Part 121 — SOUTHWEST AIRLINES, CO.

Boeing 737-700 Serious injury Part 121 — SOUTHWEST AIRLINES, CO.

ATA 2560

FWD EMERGENCY FLASH LIGHT INOP<[01] R&R FWD EMERGENCY FLASHLIGHT BATTERY PER AMM 25-64-00; OPS CHECK GOOD.

ATA 3350

EMERGENCY EXIT ROW PLACARD CAPT. SIDE MISSING.<[01] INSTALLED MISSING LENS COVER COVER ON CAPT.'S SIDE EMERGENCY EXIT ROW SIGN. PER AMM 33-51-01.

ATA 7200

FLAMES OBSERVED FROM #1 ENGINE DURING ENGINE START . NO COCKPIT FIRE INDICATIONS. FLAMES EXTINGUISHED AFTER SHUTDOWN<[01] PERFORMED ENG RUN ON #1 ENG NO DEFECTS NOTED GOOD START PER AMM 71-00-00-800-803 FOO

ATA 3350

FWD SERVICE DOOR EMERGENCY LIGHT INOP<[01] RE-LAMPED FWD SERVICE DOOR EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK NORMAL.

ATA 2560

CREW REPORTED FWD SERVICE DOOR SLIDE GIRT BAR STUCK BETWEEN A/C AND TRUCK.<[01] DISLODGED GIRT BAR. INSTALLED GIRT BAR IN FLOOR BRACKETS. INSPECTED GIRT BAR. NO DAMAGE NOTED REF AMM 25-66-01.

ATA 5241

R2 AFT SERVICE DOORLOWER PAN AFT BRACKET CRACKED<[01] R&R R2 AFT SERVICE DOORLOWER PAN AFT BRACKET PER AMM 52-41-31

ATA 2565

FWD SERVICE DOOR RAFT GAUGE IS RED<[01] REMOVED SLIDE PER THE TASK 725-61-06;[02] INSTALLED SLIDE PER TASK 725-61-06

ATA 3350

PASSENGER CABIN ISLE WAY EMERGENCY EXIT LIGHT FOR OVER-WING DOORS IS INOP.<[01] REMOVED AND REPLACED PAX CABIN ISLE WAY EMERGENCY EXIT LIGHT FOR OVER-WING DOORS IAW AMM 33-51-01-960-802 OPS CHECK GOOD;[02] INSPECTED AND VERIFIED CORRECTIVE ACTION. JOB COMPLETE.

ATA 3350

BATTERY PACK M2335 AND RELATED EMERGENCY LIGHTS FAIL TEST<[01] REPLACED BATTERY PACK M2335 PER AMM 33-51-06-960-805; PERFORMED GOOD TEST;[02] VERIFIED CORRECTIVE ACTION #1.

ATA 5320

AFT CARGO BAY INTERCOSTAL AT BS 927-947 RBL 20 IS CRACKED<[01] REMOVED INTERCOSTAL AT AFT CARGO BAY BETWEEN BS 927 - BS 947 RBL 20 IAW SRM 51-40-02.<BR>MEASURED CRACK ON WEB: L=.6' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 PARAGRAFH 4.C;[02] RECEIVED INTERCOSTAL P/N 147A7500-22; LOT:1492095-10.<BR>LOCATED AND DRILLED INTERCOSTAL AT AFT CARGO BAY AT BS 927-947 RBL 20 IAW SRM 51-40-05 DWG# 147A7500.<BR>OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2. TASK CARD COMPLETE.;[04] INSTALLED INTERCOSTAL AT AFT CARGO BAY INTERCOSTAL AT BS 927-947 RBL 20 IAW SRM 51-40-02 & DWG# 147A7500.;[05] VERIFIED CORRECTIVE ACTION STEP 4.;[06] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

ATA 5320

FWD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACKED RADIUS ON FWD CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARA 4.B. (2) AND (4)<BR>EQUIP USED: WELDING MACHINE E10583. CAL DUE 01/2024;[02] VERIFIED CORRECTION ACTION ITEM 1. AND STEP 1.;[03] ITEM 1 IS REJECTED DUE TO WRONG REFERENCE USED;[04] UPON FURTHER INVESTIGATION FOUND ACTION ITEM TO HAVE THE CORRECT REFERENCE. STEPS 1 AND 2 WERE GENERATED IN ERROR;[05] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2504-A; B; C CAL DUE: 05/23;[06] SANDED WELD REPAIR AREA PER SRM 53-30-15-2R-1 PARA.4.B. (5);[07] VERIFIED CORRECTION ACTION 6.;[08] OK TO APPLY CHEMICAL CONVERSION COATING AND PRIMER;[09] OK TO APPLY CHEMICAL CONVERSION COATING AND PRIMER GIVEN.;[10] APPLIED CHMICAL CONVERSION COATING AND PRIMER PER AMM#51-21-41 AND AMM#51-21-72-370-804;[11] VERIFIED CORRECTIVE ACTION 10.;[12] OK TO INSTALL FWD CARGO BAY AFT CORNER SCUFF PLATE;[13] VERIFIED CORRECTION ACTION ITEM 12; OK TO INSTALL.;[14] INSTALLED FWD CARGO BAY AFT CORNER SCUFF PLATE PER AMM#53-11-02-420-801 STEPS 3.F.(2) USING TOOLING TORQUE WRENCH ID:ATS2035 S/N:UKNOWN DUE:01/31/24;[15] VERIFIED CORRECTION ACTION 14 CARD COMPLETE.

ATA 5753

L/W WING STA 220; CLIP ON LOWER REAR SPAR FOR PANEL SUPPORT 551FB IS BROKEN.<[01] REMOVED AND REPLACED L/W WING STA 220; CLIP P/N 115A5552-1 ON LOWER REAR SPAR FOR PANEL SUPPORT 551FB IAW SRM 51-40-02 AND AIPC 57-50-00-23;[02] VERIFIED CORRECTIVE ACTION 1.

ATA 5330

CORROSION ON DOUBLER UNDER VERTICAL FIN AT WL 308 BS 1016+23 RBL 8.<EVALUATED DAMAGE ON DOUBLER UNDER VERTICAL FIN AT WL 308; BS 1016+23; RBL 8. MAXIMUM MATERIAL LOSS 0.8' X 0.8' X 0.004' ORIGINAL THICKNESS 0.040' REMAINING THICKNESS 0.036' FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM FOR THIS PART.;[09] VERIFIED CORRECTION ACTION ITEM 8.;[10] INSTALLED FASTENER DOCUMENTED IN STEP 1;[11] VERIFIED CORRECTIVE ACTION 10 AND THE MEASUREMENT TABLE.;[12] STEP 2<BR>OK TO INSTALL ACCESS PANEL 323AR & PANEL 323BR;[13] UPDATED MESURMENT TABLE;[14] VERIFIED MEASUREMENT TABLE COMPLETED.<BR>PROVIDED PARTIAL UPDATE FOR STEP 2.;[15] COMPLETED STEP 2 INSTALLED PANELS 323AR AND 323BR PER AMM#20-50-11 USING TOOLING SCREWGUN ID:ATS1310 S/N:1310158 DUE:10/2023;[16] VERIFIED CORRECTIVE ACTION ITEM 15.;[17] 'AS PER EA 23-153-01355; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.';[18] JOB COMPLETE.;[19] JOB COMPLETE.

ATA 5510

L/H HORIZONTAL STAB INSPAR RIB 4 (STAB STA 120.30) HAS A CRACKED 4TH STIFFENER.<[01] SRM 55-10-09-2R-4 IS APPLICABLE TO THIS REPAIR.;[02] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 120.30 RIB 4RT VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[03] HFEC REQUEST ON THE CUT OUT EDGES; WEB AND EXISTING FASTENERS HOLES WITHIN THE REPAIR AREA TO ENSURE NO CRACKS EXIST.;[04] PERFORMED GVI OF ALL AREAS WITHIN THE REPAIR AREA; NO DEFECTS NOTED IAW SRM 55-10-09-2R-4 STEP E.;[05] VERIFIED CORRECTIVE ACTION 1;2 AND 4;[06] HFEC INSPECTED BLENDED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR><BR>HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16. <BR>NO CRACKS NOTED.<BR><BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS1465 CAL DUE: 09/23;[07] FABRICATED REPAIR PARTS (1) T-SECTION FROM 60-5872 7075 T76511 LOT# 1449876-1 (2) ANGLE FROM BAC 1490-2793 7075 T62 CLAD LOT# 1442205-1 (3) SHIM FROM 7075 T6 0.020' CLAD LOT# 1381332-1; APPLIED CHEMICAL CONVERSION COATING IAW SRM 55-10-09-2R-4 OK TO PRIME.;[08] VERIFIED CORRECTIVE ACTION 7.<BR>OK TO PRIME;[09] PRIMED REPAIR PARTS AND COMMON AREA IAW SRM 55-10-09-2R-4 OK TO INSTALL.;[10] VERIFIED CORRECTIVE ACTION 9.<BR>OK TO INSTALL;[11] INSTALLED REPAIR PARTS AT LH HORIZONTAL STABILIZER STA 120.30 RIB 4TH VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[12] RII VERIFIED CORRECTIVE ACTION ITEM 11.;[13] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE.

ATA 5320

WING CENTER SECTION - BREAK DOWN SUPPORT HAS CRACK BS 540 LBL 38.25 WL 208<[01] REMOVED WING CENTER SECTION - BREAK DOWN SUPPORT BS 540 LBL25 TO LBL 45 WL 208 DUE TO NO ALLOWABLE DAMAGE FOUND FOR THIS ITEM ; IAW SRM 51-10-02 AND SRM 51-40-02;[02] LOCATED AND DRILLED NEW WING CENTER SECTION - BREAK DOWN SUPPORT FROM BS 540 LBL 25 TO LBL 45 WL 208 PER B737-700 DWG 143A5240 REV B. OK TO INSTALL.;[03] INSTALLED NEW WING CENTER SECTION - BREAK DOWN SUPPORT FROM BS 540 LBL 25 TO LBL 45 WL 208 PER B737-700 DWG 143A5240 REV B.;[04] VERIFIED CORRECTIVE ACTION 2.<BR>OK TO INSTALL;[05] REJECTION OF INSTALLATION AS PART HAS NOT BEEN DRILLED TO RECEIVE THE AFT FLOORBOARD.STEP WILL BE CREATED FOR CORRECTION.;[06] COMPLETED STEP 1. VERIFY INSTALLATION FROM CORRECTIVE ACTION 3.;[07] VERIFIED CORRECTIVE ACTION STEP 6.;[08] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

ATA 5320

WING CENTER SECTION - BREAK DOWN SUPPORT HAS CRACK BS 540 LBL 1.5 WL 208<[01] REMOVED WING CENTER SECTION - BREAK DOWN SUPPORT BS 540 BL0 TO LBL 25 WL 208 DUE TO NO ALLOWABLE DAMAGE FOUND FOR THIS ITEM ; IAW SR 51-10-02 AND SRM 51-40-02;[02] REMOVED WING CENTER SECTION - BREAK DOWN SUPPORT BS 540 BL0 TO LBL 25 WL 208 DUE TO NO ALLOWABLE DAMAGE FOUND FOR THIS ITEM ; IAW SRM 51-10-02 AND SRM 51-40-02;[03] LOCATED AND DRILLED WING CENTER SECTION - BREAK DOWN SUPPORT FROM BS 540 LBL0 TO LBL25 WL 208 PER B737-700 DWG 143A5240 REV -.OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION 3. OK TO INSTALL IS GIVEN.;[05] INSTALLED NEW WING CENTER SECTION - BREAK DOWN SUPPORT BS 540 LBL0 TO LBL 25 WL 208 PER B737-700 DWG 143A5240 REV -.;[06] VERIFIED MEASUREMENT TABLE.;[07] RII; VERIFIED CORRECTIVE ACTION 5.;[08] UPDATED PARTS USAGE;[09] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

ATA 5730

PANEL 561AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED) FOUND PANEL TO BE 661AB. PANEL 561AB FASTENER HOLES WILL BE REPAIRED ON FAULT TTG8Q00KCULF<OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PARA 4B(5).REPAIRED PER SRM 51-70-04-2R-9 AS DIRECTED BY SRM 57-51-01-2R-1 PARA 4C AND TABLE 202 REMOVED DAMAGE TO ALL FASTENER HOLES ON AFT EDGE AND CLEANED AREA IAW SRM 51-70-04-2R-9 PARA 4A-C.APPLIED SLURRY MIX OF BMS8-301 LOT#JH2EAA8895 AND MILLED FIBERS LOT#1437038-1 TO ALL DAMAGED FASTENER HOLES IAW SRM 51-70-04-2R-9 PARA 4D-E.;[05] CURED THE SLURRY MIXTURE THEN PERFORMED THE SURFACE PREPARATION PROCEDURES IAW SRM 51-70-04-2R-9 PARA 4. STEPS F-I. REF CAL TOOL HOT BONDER ID ATS532 CAL DUE 06/2023.<BR><BR>USING BMS9-3 STYLE 1581 GLASS LOT 1522395-2 & BMS8-301 EA9390 RESIN LOT JH2EAA8895 FABRICATED REPAIR PLIES IAW SRM 51-70-04-2R-9 PARA 4. STEP J.;[06] IMPREGNATED AND INSTALLED REPAIR PLIES; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD USING VACUUM GAUGE ATS2441 CAL DUE DATE 08/2023 IAW SRM 51-70-04-2R-9 PARA 4J-L.;[07] CURED REPAIR USING HOT BONDER ATS532 CAL DUE DATE 06/2023; UNBAGGED AND LIGHTLY SANDED REPAIR IAW SRM 51-70-04-2R-9 PARA 4M LOCATED; DRILLED; AND COUNTERSUNK FASTENER HOLES IAW SRM 51-70-04-2R-9;COMPLETED REFINISH OF PANEL SURFACE IAW AMM 51-21-99-300-802 PARA 3.C(3(E AND F)).;[17] VERIFIED CORRECTIVE ACTION #12-16

ATA 5753

PANEL 661BB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PARA 4B( REPAIRED PER SRM 51-70-04-2R-9 AS DIRECTED BY SRM 57-51-01-2R-1 PARA 4C AND TABLE 202. <BR><BR>REMOVED DAMAGE TO ALL FASTENER HOLES ON AFT EDGE AND CLEANED AREA IAW SRM 51-70-04-2R-9 PARA 4A-C APPLIED SLURRY MIX OF BMS8-301 LOT#JH2EAA8895 AND MILLED FIBERS LOT#1437038-1 TO ALL DAMAGED FASTENER HOLES IAW SRM 51-70-04-2R-9 PARA 4D-E.;[05] CURED THE SLURRY MIXTURE THEN PERFORMED THE SURFACE PREPARATION PROCEDURES IAW SRM 51-70-04-2R-9 PARA 4. STEPS F-I. REF CAL TOOL HOT BONDER ID ATS532 CAL DUE 06/2023.<BR><BR>USING BMS9-3 STYLE 1581 GLASS LOT 1522395-2 & BMS8-301 EA9390 RESIN LOT JH2EAA8895 FABRICATED REPAIR PLIES IAW SRM 51-70-04-2R-9 PARA 4. STEP J.;[06] IMPREGNATED AND INSTALLED REPAIR PLIES; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD USING VACUUM GAUGE ATS2441 CAL DUE DATE 08/2023 IAW SRM 51-70-04-2R-9 PARA 4J-L.;[07] CURED REPAIR USING HOT BONDER ATS532 CAL DUE DATE 06/2023; UNBAGGED AND LIGHTLY SANDED REPAIR IAW SRM 51-70-04-2R-9 PARA 4M.; LOCATED; DRILLED; AND COUNTERSUNK FASTENER HOLES IAW SRM 51-70-04-2R-9;[12] ADDING 'PARA 4.N.' TO LINE 11.;[13] APPLIED FINISH TO REPAIR AREA IAW SRM 51-70-04-2R-9 PARA 4.P.;[14] VERIFIED CORRECTIVE ACTION 11; 12; 13

ATA 5321

FLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIGURE 4 TABLE 4 UNDER SEAT LOW TRAFFIC SECTION 44.<BR>MULTIPLE PULLED STRANDS; DENTS & OTHER DEFECTS EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-50-1A-1 PARA 4.A-D. PANEL REPLACEMENT REQUIRED.;[02] PANEL FABRICATION/REPLACEMENT IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE.<BR>USING BMS4-23 TYII PANEL MATERIAL LOT 1508290-1 FABRICATED PERFORMED NET TRIM & LOCATED FASTENER HOLES PER DWG 144A5810-116;[03] INSTALLED SL5107A3-410 INSERTS USING BMS5-107 ADHESIVE LOT AK2KP838K-1 THEN CURED IAW SRM 53-00-50-2R-0 PARA 5. S. FIGURE 213 PAGE 30 PER DWG 144A5810-I6 REF CAL TOOL THERMOMETER ID ATS1776 CAL DUE 08/2023;[04] PART MARKED PANEL IAW BOEING DWG 144A5810 ID:0016.;[05] UPDATED MEASUREMENTS;[06] CORRECTION TO CORRECTIVE ACTION 2: DRAWING SHOULD BE 144A5810 ID:0016;[07] CORRECTION TO CORRECTIVE ACTION 3: DRAWING SHOULD BE 144A5810 ID:0016;[08] VERIFIED CORRECTIVE ACTIONS 1-7<BR><BR>VERIFIED MEASUREMENTS TABLE;[09] UPLOADED CURE SHEET. JOB COMPLETE;[10] VERIFIED CORRECTIVE ACTION 9

ATA 5321

FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 4; TABLE 4.<BR><BR>UPON INVESTIGATION; PANEL DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM<BR>53-00-50-1A-1 PAR. 4. E. & 4. F.<BR><BR>DUE TO SIZE OF DAMAGE FABRICATING NEW PANEL FOLLOWING IAW SRM 53-00-50-2R-0 PAR. 1.A. NOTE:<BR><BR>FABRICATED NEW FLOOR BOARD USING BMS4-23 TY II LOT# 1508291-1; <BR>SANDED EDGES AND CLEANED IAW SRM 53-00-50-2R-0 PAR. 4.A.(2) <BR>TABLE 204; & 5.E. STILL NEED LOCATED INSERT DRILLING.<BR><BR>UPDATED MEASUREMENTS TABLE.;[02] LOCATED AND INSTALLED ALL INSERTS USING BMS 5-107 LOT#AK2KP8383K-1; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023; PART MARKED PANEL IAW SRM 53-00-50-2R-0 PARA 5.S AND BOEING DWG 144A5810 ID:0020.;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2<BR><BR>VERIFIED MEASUREMENTS TABLE;[04] UPLOADED CURE SHEET. JOB COMPLETE;[05] VERIFIED CORRECTIVE ACTION 4

ATA 5330

PANEL 191FR OUTER SKIN IS DISBONDED. (MARKED)<[01] IDENTIFIED PANEL 191FR IAW SRM 53-30-70-0I-1; FIGURE 2; SHEET 1; TABLE 2; ITEM 4.<BR><BR>CLEANED PANEL FOR EVALUATION IAW AMM 51-21-11-150-815 PARA 17. C.<BR><BR>VISUALLY EXAMINED DAMAGE AND TAP TESTED WITH DISBOND NOTED IAW SRM 53-30-70-1A-1 PARA 2. A. (1) (A) THAT EXCEEDS ALLOWABLE LIMITS PER SRM 53-30-70-1A-1 PARA 4. B. (6).<BR> <BR>REPAIR TO BE PERFORMED IAW SRM 51-70-05-2R-2 AS GIVEN IN SRM 53-30-70-2R-1 TABLE 201.<BR><BR>REPAIR WILL BE ACCOMPLISHED IAW SRM 51-70-05-2R-2 IAW SRM 53-30-70-2R-1 PARA 4.D. AND TABLE 201.<BR><BR>REMOVE 1' DIA AREA OF OUTER SKIN AND FULL DEPTH CORE THEN CLEANED AND PREPARED REPAIR AREA WITH NO MOISTURE OR CONTAMINATION NOTED IAW SRM 51-70-05-2R-2 PARA 4. A. - C.;[04] APPLIED POTTING BMS 5-28 TY7 LOT#AK1AP8072K AND CURED UNDER HEAT LAMP USING THERMOMETER ID:ATS2209 DUE:10/23; SANDED POTTING SMOOTH; AND CLEANED REPAIR AREA IAW SRM 51-70-05-2R-11 PARA 4.A-E<BR><BR>FABRICATED REPAIR PLIES OUT OF BMS 8-79 CL3 ST120 LOT#1520138-1; AND BMS 5-129 TY2 GR05 LOT#1521552-3. INSTALLED REPAIR PLIES; VACUUM BAGGED; LEAK CHECK GOOD USING VACUUM GAUGE ID:ATS2441 DUE:08/23 IAW SRM 51-70-05-2R-2 PARA 4.D(NOTE)G AND H. <BR>REPAIR PLIES NEED CURE.[10] POST REPAIR UT INSPECTED PER 737NDT PART 4 51-00-02. NO DEFECTS FOUND. TOOL S650 ATS2341 DUE 06/2023.;[11] REFINISHED REPAIR AREA IAW SRM 51-70-05-2R-2 PARA 4.K;[12] VERIFIED CORRECTIVE ACTION 11

ATA 5321

FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 232SF IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. FLOOR PANEL IS DAMAGED BEYOND ECONOMICAL REPAIR; AND EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. FLOOR PANEL REQUIRES REPLACEMENT IAW SRM 53-00-50-2R-0 PARAGRAPH 1.A NOTE.<BR><BR>ROUGH CUT FLOOR PANEL 232SF USING BMS4-17 TY6 LOT# 1522265-1 AND LOCATED HOLES IAW SRM 53-00-50-2R-0 PARAGRAPH 4.A TABLE 204; AND BAC DWG 144A5810 ID:0014.;[02] COUNTERBORED HOLES AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING THERMOMETER ID: ATS2209 CAL DUE: 10/2023 AND PART MARKED FLOOR PANEL AS REQUIRED IAW SRM 53-00-50-2R-0 PARAGRAPH 3.S(1); AND DWG 144A5810 ID:0014.;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2<BR><BR>VERIFIED MEASUREMENTS TABLE;[04] UPLOADED CURE SHEET: JOB COMPLETE;[05] VERIFIED CORRECTIVE ACTION 4

ATA 5321

FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL IAW SRM 53-00-50-0I-1 FIGURE 4. DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL WITH BMS4-23 TYPE II LOT 1508290-1 USING BMS5-107 LOT AK2KP8383K-1 RESIN WITH THE INSERTS; CURED THE RESIN UNDER A HEAT LAMP USING THERMOMETER ID: ATS2208 DUE: 10/2023; ALL IAW SRM 53-00-50-2R-0 PARAGRAPH 4.A.(1) AND TABLE 204 ALSO IAW DRAWING 144A5810-9.;[02] DRAWING USED FOR FABRICATION IS: 144A5810-7.;[03] VERIFIED CURE TAPE<BR>VERIFIED CORRECTIVE ACTION #1;[04] JOB COMPLETE

ATA 5321

FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241AF IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. FLOOR PANEL IS DAMAGED BEYOND ECONOMICAL REPAIR; AND EXCEEDS ALLOWABLE DAMGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. FLOOR PANEL REQUIRES REPLACEMENT IAW SRM 53-00-50-2R-0 PARAGRAPH 1.A NOTE.<BR><BR>ROUGH CUT FLOOR PANEL 241AF USING BMS4-17 TY6 LOT# 1522265-1 AND LOCATED HOLES IAW SRM 53-00-50-2R-0 PARAGRAPH 4.A TABLE 204; AND BAC DWG 144A5810 ID:0008.;[02] COUNTERBORED HOLES AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING THERMOMETER ID: ATS2209 CAL DUE: 10/2023 AND PART MARKED FLOOR PANEL AS REQUIRED IAW SRM 53-00-50-2R-0 PARAGRAPH 3.S(1); AND DWG 144A5810 ID:0008.;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2<BR><BR>VERIFIED MEASUREMENTS TABLE;[04] UPLOADED CURE SHEET: JOB COMPLETE;[05] VERIFIED CORRECTIVE ACTION 4

ATA 5321

FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241BF IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. FLOOR PANEL IS DAMAGED BEYOND ECONOMICAL REPAIR; AND EXCEEDS ALLOWABLE DAMGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. FLOOR PANEL REQUIRES REPLACEMENT IAW SRM 53-00-50-2R-0 PARAGRAPH 1.A NOTE.<BR><BR>ROUGH CUT FLOOR PANEL 241BF USING BMS4-17 TY6 LOT# 1522265-1 AND LOCATED HOLES IAW SRM 53-00-50-2R-0 PARAGRAPH 4.A TABLE 204; AND BAC DWG 144A5810 ID:0018.;[02] COUNTERBORED HOLES AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING THERMOMETER ID: ATS2209 CAL DUE: 10/2023 AND PART MARKED FLOOR PANEL AS REQUIRED IAW SRM 53-00-50-2R-0 PARAGRAPH 3.S(1); AND DWG 144A5810 ID:0018.;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2<BR><BR>VERIFIED MEASUREMENTS TABLE;[04] UPLOADED CURE SHEET: JOB COMPLETE;[05] VERIFIED CORRECTIVE ACTION 4

ATA 5321

FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL WITH BMS4-17 LOT 1522265-1 USING BMS5-107 LOT AK2KP8383K-1 RESIN WITH THE INSERTS; CURED THE RESIN UNDER A HEAT LAMP USING THERMOMETER ID: ATS2208 DUE: 10/2023 TO MONITOR THE TEMPERATURE OF THE CURE; ALL IAW SRM 53-00-50-2R-0 PARAGRAPH 4.A.(1) AND TABLE 204 ALSO IAW DRAWING 144A5810-9.;[02] IDENTIFIED PANEL IAW SRM 53-00-50-0I-1 FIGURE 4. FLOORBOARD MATERIAL USED TO FABRICATE NEW PANEL IS BMS4-17 TYPE VI LOT 1522265-1.;[03] VERIFIED CURE TAPE<BR>VERIFIED CORRECTIVE ACTION #1; 2;[04] JOB COMPLETE

ATA 5340

CORROSION ON STRINGER CLIP AT ACB BS827 LBL6 WL157.<[01] FOUND TO BE WITH NO LIMITS PER SRM 53-00-53-1A2;[02] REMOVED STRINGER CLIP IAW SRM 51-40-02;[03] RECEIVED NEW STRINGER CLIP LOCATED AND DRILLED<BR>AT ACB BS827 LBL6 WL 157<BR>P/N 146A1010-10 LOT# 1478113-2 IAW SRM 51-40-05<BR>AND DWG 146A1280 REV:A OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION 3. OK TO INSTALL.;[05] INSTALLED STRINGER CLIP AT BS 827 LBL6 WL 157<BR>IAW SRM 51-40-02 AND DWG 146A1280 REV:A.<BR>JOB COMPLETED;[06] VERIFIED CORRECTIVE ACTION 5.;[07] VERIFIED THE MEASUREMENT TABLE. WORKSCOPE COMPLETE.

ATA 5347

CORROSION ON TRACK AT ACB BS787+12 RBL14 WL157.<FOUND TO OUT OF LIMITS ORIGINAL MATERIAL .070 REMAINING MATERIAL .060 ALLOWABLE DAMAGE LIMITS IS .007.;[13] UPDATED CORRECTIVE ACTION 5. REMOVED NUTPLATE PER B737-700 SRM 51-40-02-0G-0.;[14] OBTAINED LOCATED AND DRILLED NEW ACB TRACK BS 747 + 12 TO BS 887 RBL 14 WL 157 IAW SRM 51-40-05 AND DWG # 146A7501 ; OK TO INSTALL;[15] INSTALLED ACB TRACK BS 747 + 12 TO BS 887 RBL 14 WL 157 IAW SRM 51-40-02-0G-0 AND DWG#146A7501.;[16] VERIFIED CORRECTIVE ACTION 14 AND 15.;[17] VERIFIED APPLICABILITY SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 - FORWARD AND AFT CARGO COMPARTMENT FLOOR STRUCTURE;[18] UPDATE TO STEP 12; REMOVED CARGO TRACK DUE TO AFTER EVALUATION WAS FOUND OUT OF LIMITS IAW SRM 51-40-02-0G-0.;[19] UPDATE REFERENCE USED ON EVALUATION.<BR>EVALUATED CORROSION ON TRACK AT ACB BS787+12 RBL14 WL157 PER B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 FOUND TO OUT OF LIMITS ORIGINAL MATERIAL .070 REMAINING MATERIAL .060 ALLOWABLE DAMAGE LIMITS IS .007.;[20] VERIFIED CORRECTIVE ACTIONS 10; 11; 12; 17; 18; 19; AND MEASUREMENT TABLE.

ATA 5320

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB LBL21 BS727A - BS807 WL156.<[01] SRM 53-60-53-0I-2 IDENTIFICATION AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 ARE APPLICABLE;[02] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT UPPER SURFACE 03 EACH LOCATIONS L=19' ; W=1.7'; D=0.013' ; L=10.2'; W=1.3'; D= 0.019'; L=6'; W=1.1'; D=0.016'. LOWEST REMAINING THICKNESS 0.021' ORIGINAL THICKNESS 0.040'. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG 103 DETAIL E. <BR>TOOL ID: ATS1672; DUE DATE MAR-31-2024;[05] LOCATED AND DRILLED NEW SIDEWALL SUPPORT FROM ACB LBL21 BS727 - BS847 WL156. PER B737-700 DWG 146A7502 AND SRM 53-00-53-2R-5 REPAIR 5.;[06] OK TO TREAT AND PRIME.;[07] LOCATED AND DRILLED NEW SIDEWALL SUPPORT SPLICE REPAIR IAW SRM 5140-05-0G-0 AND SRM AND SRM 53-00-53-2R-5 REPAIR 5 DWG 146A7502.;[08] MATERIAL USED ON SIDEWALL SUPPORT SPLICE REPAIR BAC1496-377#7075T62 LOT#1521599-1;[09] VERIFIED CORRECTIVE ACTIONS 5 AND 7.;[10] VERIFIED CORRECTIVE ACTIONS 4; 6; AND 8. OK TO TREAT AND PRIME NEW SIDEWALL SUPPORT AND SPLICE.;[11] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01 AND SOPM 20-41-02<BR>OK TO INSTALL OF SPLICE SIDEPLATE;[12] VERIFIED CORRECTIVE ACTION STEP 11. VERIFIED OK TO INSTALL SPLICE SIDEPLATE.;[13] INSTALLED ON FLOOR TO SIDEWALL SUPPORT SPLICE SIDEPLATE IAW SRM 51-40-02 AND SRM 53-00-53-2R-5 REPAIR 5;

ATA 5320

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS400 - BS500D LBL23 WL156.<OUT OF LIMITS; WILL BE REPAIR BY REPLACEMENT PER SRM 51-10-02 PARAG. 9.C;[05] RECEIVED EXTRUSION P/N BAC1496-444 LOT. 1524635-1. LOCATED AND DRILLED (2EA) EXTRUSION (FORMED CHANNEL) ON FWD CARGO BAY L/H FROM BS 400 - 500D LBL23 WL 156 IAW SRM 51-40-05; SRM 53-00-53-2R-6 AND DWG'S 143A7501 REV: B. <BR>MADE (1EA;) SPLICE SIDEPLATE FROM BAC1496-444 LOT:1524635-1 LOCATED AT BS 480+10 LBL23; WL 156 IAW SRM 53-00-53-2R-6 REPAIR 6 TABLE 201 ITEM [2].<BR> APPLIED CHEMICAL CONVERSION COATING TO REPAIR PARTS IAW SRM 51-20-01. OK TO APPLY PRIMER TO REPAIR PARTS.;[06] VERIFIED APPLICABILITY OF SRM 53-00-53-2R-6 REPAIR 6 CARGO COMPARTMENT SIDEPLATE REPAIR AT A FLOOR PANEL SPLICE;[07] VERIFIED CORRECTIVE ACTIONS 4 AND 6;[08] VERIFIED CORRECTIVE ACTION 5. OK TO PRIME REPAIR PARTS.;[09] APPLIED PRIME ON NEW FLOOR TO SIDEWALL SUPPORT AND SPLICE REPAIR IAW SRM 51-20-01-0G-0.<BR>OK TO ASSEMBLY NEW SIDEWALL SUPPORT AND SPLICE REPAIR.;[10] VERIFIED CORRECTIVE ACTION 9; OK TO ASSEMBLE SIDEWALL SUPPORT AND SPLICE REPAIR;[11] NUT PLATES INSTALLED AND REPAIR SPLICE LOCATED AT BS 480+10 IAW SRM 51-40-02 AND SRM 53-00-53-2R-6 REPAIR 6 AND DWG# 143A7501 REV:B<BR>DISASSEMBLY AND INSTALLATION IS DONE BY CUSTOMER CARD NO. TTG8Q004CCXJ STEP NO. 10 & 38;[12] VERIFIED CORRECTIVE ACTION 11 AND COMPLETED ALL STEPS.;[13] VERIFIED MEASUREMENT TABLE.

ATA 5320

CRACKED INTERCOSTAL AT AREA AFT OF FCB BS500D+18 RBL31 S-25R WL159.<[01] REMOVED INTERCOSTAL AT AREA AFT OF FCB BS500D+18 RBL31 S-25R WL159 IAW SRM 51-40-02.-;[02] RECEIVED NEW INTERCOSTAL HFAB53-AN-011 (7075T0#0.032'') PER DWG# 143A9803-58 HEAT TREATED TO T62 CONDITION PER BAC5602 LOT# 1525181-1 IAW CUSTOMER RO# 915251-SWA JOB# 558816.;[03] FABRICATED; LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-05-0G-0 AND DWG# 143A9803.OK TO TREAT AND PRIME.;[04] VERIFIED CORRECTIVE ACTIONS 1-3.<BR>OK TO TREAT AND PRIME;[05] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON NEW INTERCOSTAL AT AREA AFT OF FCB BS500D+18 RBL31 S-25R WL159 .- IAW 737-700; AMM 51-21-72-370-804; AMM 51-21-41-370-802;[06] VERIFIED CORRECTIVE ACTION 5;[07] OK TO INSTALL NEW INTERCOSTAL AT AREA AFT OF FCB BS500D TO 520 RBL31 S-25R WL159;[08] VERIFIED CORRECTION ACTION ITEM 7; OK TO INSTALL.;[09] INSTALLED NEW INTERCOSTAL AT AREA AFT OF FCB BS500D - BS 520 RBL31 S-25R WL159 IAW SRM 51-40-02 AND DWG # 143A7902 AND DWG # 143A9803;[10] VERIFIED CORRECTIVE ACTION 9.;[11] VERIFIED MEASUREMENT TABLE.

ATA 5320

CORROSION ON FLOOR SUPPORT SPLICE AT ACB BS727D+6 LBL20 TO RBL20 WL156.<[01] THIS PART DOES NOT ALLOWABLE DAMAGE LIMITS; IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] RECEIVED NEW SPLICE STRIP ASSY AT AFT CARGO BAY BS 727B LBL 20 TO RBL 20 WL 156 P/N 146A9401-8 PO NUMBER 897803/1 AND DWG 146A9401;[04] VERIFIED CORRECTIVE ACTION STEP 3. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

ATA 5340

FWD CARGO BAY BAFFLE ATTACH ANGLE CRACKED BS500A FWD SIDE LBL25 WL155.<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02 PARAG 9.REPAIRABLE BY REPLACEMENT.;[02] PRIOR TO REMOVAL FOUND PART HAS NOT ALLOWABLE DAMAGE ON SRM;PART WILL BE REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02 PARAG 9.;[03] REMOVED ANGLE DAMAGED PER SRM 51-40-02.;[04] CONCUR WITH APPLICABILITY OF SRM 51-10-02 PARA. 9. PART MUST REPLACED DAMAGE LIMITS GIVEN IN SRM.;[05] CORRECTED STATEMENT FOR CORRECTIVE ACTION ITEM 4. 'CONCUR WITH APPLICABILITY OF SRM 51-10-02 PARA. 9. PART MUST BE REPLACED AS NO DAMAGE LIMITS ARE GIVEN IN SRM.;[06] RECEIVED;LOCATED AND DRILLED NEW CLIP(ANGLE) WITH P/N 143A7502-159;LOT#1524970-1 PER SRM 51-40-05 AND DWG#143A7505 REV B.OK TO INSTALL;[07] VERIFIED CORRECTIVE ACTION 6. OK TO INSTALL.;[08] INSTALLED NEW CLIP(ANGLE) ON FCB AT BS500A;LBL25 WL155 PER SRM 51-40-02 AND DGW#143A7505 REV B.;[09] VERIFIED CORRECTIVE ACTION 8.;[10] VERIFIED THE MEASUREMENT TABLE.

ATA 5320

CORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 RBL24 WL156.<[01] AFT SHIELD AT FORWARD CARGO BAY LOCATED BETWEEN BS492.4- BS500A RBL 24 WL 156 NOT HAS ENTRIES ALLOWABLE DAMAGE IN SRM. MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 PARAGRAPH 9.C.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.<BR>CONCUR WITH APPLICABILITY OF SRM 51-10-02 PARAGRAPH 9.C.;[03] VERIFIED APPLICABILITY OF SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 - FORWARD AND AFT CARGO COMPARTMENT FLOOR STRUCTURE;[04] LOCATED AND DRILLED NEW FCB AFT SHIELD IAW SRM 51-40-05-0G-0 AND DRAWING#143A0080.;[05] INSTALLATION OF FCB AFT SHIELD IS DOCUMENTED ON CUSTOMER CARD# 5330-E-16461-NG (CPCP/AD MOC - FWD CARGO COMPARTMENT FLOOR STRUCTURE CORROSION PROTECTION) -TTG8Q004CCXJ-;[06] UPDATED STEP 5. <BR>CUSTOMER#TTG8Q004CCXJ STEP 40;[07] UPDATE STEP 3.<BR>VERIFIED NO ENTRIES FOR FCB AFT SHIELD IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 - FORWARD AND AFT CARGO COMPARTMENT FLOOR STRUCTURE.;[08] VERIFIED CORRECTIVE ACTIONS 7; 5; AND 6;[09] VERIFIED CORRECTIVE ACTION 4

ATA 5313

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26R WL153. MARKED<[01] CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26R WL153 FOUND TO BE OUT OF LIMITS DUE TO CRACKS ARE NOT ALLOWED IAW SRM 53-00-03-1A-1 .<BR>CUT AND REMOVED THE DAMAGED PART OF STR 26R BETWEEN BS 500D +11 AND BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.;[03] REQUEST NDI TO DO A HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE REPAIR AREA TO MAKE SURE THAT ALL OF THE DAMAGE IS REMOVED. REFER TO 737 NDT PART 6; 51-00-00; FIGURE 4.;[04] HFEC INSPECTED CUTOUT AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS1465 CAL DUE: 09/23;[05] UPDATED STEPS 1 AND 2;[06] RECIVED FROM OSS STRIGER SECTION 26R FROM MATERIAL 7075T0#0.045' CLAD TO 7075T6 CONDITION LOT# 1525204-1 CUSTOMER RO NO 915427-SWA; AND HAT CHANNEL FROM MATERIAL 7075T0#0.050' CLAD TO 7075T6 CONDITION LOT# 1525263-1 CUSTOMER RO NO 915439-SWA IAW SRM 53-00-03-2R-1 REPAIR 1;[07] FABRICATED -7 STRINGER SECTION 26R FROM MATERIA 7075T6#0.045' LOT# 1525204-1; -1 HAT SECTION CHANNEL FROM MATERIAL 7075T6#0.050' LOT# 1525263-1 LOCATED AND DRILLED REPAIR PARTS AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 53-00-03-2R-1 REPAIR 1; OK TO PRIMER;[11] INSTALLED REPAIR PARTS; STRINGER SECTION 26R BS 500D+10 TO BS 540 AND HAT SECTION CHANNEL AT BS 500D+10 IAW SRM 53-00-03-2R-1 REPAIR 1

ATA 5320

CORROSION ON INTERCOASTAL AT ACB BS847+9 RBL6 WL159.<[01] VERIFY APPLICABILITY PER SRM53-60-15-0I-1 AND SRM 53-60-15-1A-1<BR>REMOVED CORROSION AT DISCREPANCY AREA L=3'; W=1.5' PER SRM 51-10-02-0G-0 AND SRM 53-60-15-1A-1;[02] VERIFIED CORRECTIVE ACTION 1.;[03] HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16. <BR>NO CRACKS NOTED. <BR><BR>UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2.<BR>REMAINING MATERIAL THICKNESS IS 0.031' ADJACENT TO 0.040'.<BR><BR>EQUIP USED: <BR>-NORTEC 600 ID: ATS1465 CAL DUE: 09/23<BR>-EPOCH 650 ID: ATS2342 CAL DUE: 07/23;[04] EVALUATED CORROSION AT DISCREPANCY AREA L=3.' X W=1.5' X D=0.009' ORIGINAL THICKNESS 0.040'; REMAINING MATERIAL THICKNESS IS 0.031'; FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1; FIG 103; DETAIL G.;[05] VERIFIED REWORK IS OUT OF LIMITS PER SRM 53-60-15-1A-1; FIG 103; DETAIL G.;[06] REMOVED INTERCOSTAL AT ACB B/S 847 TO BS 867 RBL 6 WL 159 IAW SRM 51-40-02;[07] FABRICATED NEW INTERCASTALL PER DWG# 146A8132-19 MATERIAL ID 7075- O .040 LOT # 1501155-1 PER DWG# 146A8132-19 OK TO HEAT AND TREAT TO T6;[13] OK TO INSTALL NEW FRABICATED INTERCOSTAL;[14] OK TO INSTALL NEW FRABICATED INTERCOSTAL GIVEN.;[15] INSTALLED NEW FRABICATED INTERCOSTAL I.A.W SRM 51-40-02-0G-0 AND DWG 146A8130.;[16] ALL STEPS COMPLETED;[17] VERIFIED CORRECTIVE ACTIONS STEP 15 AND MEASUREMENTS TABLE.

ATA 5340

CORROSION ON ATTACH ANGLE AT ACB BS727E LBL7 WL152.<[01] FOUND TO BE WITH NO LIMITS IAW SRM 53-00-53-1A-2;[02] PART TO BE REPAIR BY REPLACEMENT PEER SRM 51-10-02 PARAGRAPH 9.C;[03] REMOVED ATTACH ANGLE AT ACB BS 727E LBL7 WL 152 IAW SRM 51-40-02;[04] RECEIVED NEW CLIP TA ACB BS 727E LBL7 WL 152 ITEM146A1320-82 PO#821987. LOCATED AND DRILLED IAW SRM 51-40-05;DWG 146A1320.<BR>OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 4. OK TO INSTALL THE NEW ANGLE.;[06] INSTALLED CLIP AT ACB BS727E LBL7 WL152 IAW SRM 51-40-02 AND DWG146A7810;[07] REQUEST INSPECTIOIN;[08] VERIFIED CORRECTIVE ACTION 6.;[09] VERIFIED MEASUREMENT TABLE.

ATA 5340

CORROSION ON INTERCOSTAL TO WEB ATTACH ANGLE BS767+2; 767+5; 767+9; 767+16; 767+19 RBL21 WL156.<[01] FOUND TO BE OUT OF LIMITS EXFOLIATED CORRODED WITH MORE THE 50 % OF MATERIAL LOST IWA B 737-700 SRM 53-60-15 REMOVED DAMAGE PART PER SRM 51-40-02;[02] SRM 53-60-15-1A-1 IS THE ALLOWABLE APPLICABILITY;[03] RECEIVED NEW ATTACH ANGLE LOCATED AND DRILLED <BR>AT FCB BS767+2 TO -BS767+19 RBL21 WL 156<BR>P/N 146A8125-53 LOT# 1522951-1 IAW SRM 51-40-05<BR>AND DWG 146A0081 REV:A OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION 3 AND THE MEASUREMENT TABLE.;[05] INSTALLED ATTACH ANGLE AT BS 767+2 TO 767+19 RBL21 WL 156<BR>IAW SRM 51-40-02 AND DWG 146A0081 REV:A JOB COMPLETED;[06] VERIFIED CORRECTIVE ACTION 5.;[07] VERIFIED MEASUREMENT TABLE.

ATA 5320

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB RBL21 BS727B+4; BS727C+14 - BS767 WL156.<[01] VERIFY APPLICABILITY PER SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2.<BR>REMOVED CORROSION ON DISCREPANCY AREA L=0.800';W=0.700';D=0.010'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 AND SRM 51-10-02.<BR>TOOL USED: ID:ATS1672; DUE:MAR-31-2024;[02] VERIFIED CORECTIVE ACTION 1 AND THE MEASUREMENT TABLE.;[03] FABRICATED NEW FLOOR TO SIDEWALL SUPPORT AT ACB RBL 21 BS 727 TO BS 767 ITEM BAC1496-377#7075T62 LOT#1521599-1 IAW SRM 51-40-05 AND DWG 146A7502.<BR>OK TREAT AND PRIMER;[04] VERIFIED CORRECTIVE ACTION 3. OK TO TREAT AND PRIME.;[05] VERIFIED THE MEASUREMENT TABLE.;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01 AND SOPM 20-41-02;[07] VERIFIED CORRECTIVE ACTION 6;[08] CORRECTED STEP 19 OF MESUREMENTS;[09] VERIFIED STEP 19 CORRECTION. CARD COMPLETE

ATA 5313

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-27R WL150. MARKED<[01] CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-267R WL150 FOUND TO BE OUT OF LIMITS DUE TO CRACKS ARE NOT ALLOWED IAW SRM 53-00-03-1A-1 .<BR>CUT AND REMOVED THE DAMAGED PART OF STR 27R BETWEEN BS 500D +11 AND BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1;[02] CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-27R WL150 FOUND TO BE OUT OF LIMITS DUE TO CRACKS ARE NOT ALLOWED IAW SRM 53-00-03-1A-1 .<BR>CUT AND REMOVED THE DAMAGED PART OF STR 27R BETWEEN BS 500D +11 AND BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1;[08] FABRICATED -7 STRINGER SECTION 27R FROM MATERIA 7075T6#0.056' LOT# 1525203-1; -1 HAT SECTION CHANNEL FROM MATERIAL 7075T6#0.063' LOT# 1525260-1 LOCATED AND DRILLED REPAIR PARTS AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 53-00-03-2R-1 REPAIR 1; OK TO PRIMER[12] INSTALLED REPAIR PARTS; STRINGER SECTION 27R BS 500D+10 TO BS 540 AND HAT SECTION CHANNEL AT BS 500D+10 IAW SRM 53-00-03-2R-1 REPAIR 1;

ATA 5340

FWD CARGO BAY BAFFLE ATTACH ANGLE CRACKED BS500B FWD SIDE RBL25 WL155.<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02 PARAG 9.REPAIRABLE BY REPLACEMENT.;[02] PRIOR TO REMOVAL;FOUND PART HAS NOT ALLOWABLE DAMAGE ON SRM;PART WILL BE REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02 PARAG 9.;[03] REMOVED ANGLE DAMAGED;PER SRM 51-40-02.;[04] CONCUR WITH APPLICABILITY OF SRM 51-10-02 PARA. 9. PART MUST BE REPLACED AS NO DAMAGE LIMITS ARE GIVEN IN SRM.;[05] RECEIVED;LOCATED AND DRILLED NEW CLIP (ANGLE) WITH P/N 143A7502-160;LOT#148544-3 PER SRM 51-40-05 AND DWG#143A7505 REV B.OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION 5. OK TO INSTALL.;[07] INSTALLED NEW CLIP (ANGLE) ON FCB;AT BS500B RBL25 PER SRM 52-40-02 AND DWG#143A7505.;[08] VERIFIED CORRECTIVE ACTION 7.;[09] VERIFIED THE MEASUREMENT TABLE.

ATA 5311

CRACK ON PASSENGER CABIN FRAME AT BS 727B STRINGER BETWEEN 8L-9L.(MARKED)<[01] FORMED ANGLE REPAIR PART B PER EA 1-A53-12114 APPENDIX REV A OK TO HEAT AND TRAET;[02] MATERIAL ID 7075-0 .050 LOT # 1517365-2;[03] REMOVED DAMAGE PER EA 1-A53-12114;[04] WORK ACCOMPLISHED ON CARD # TTG8Q00KH5YE;[05] VERIFIED CORRECTIVE 4.WORK ACCOMPLISHED ON CARD # TTG8Q00KH5YE.

ATA 5510

CRACK INDICATIONS ON L/H H-STAB RIB 4 STIFFENERS 2 & 3 LOWER RADII.<REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 120.30 RIB 2ND AND 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[03] HFEC REQUEST ON 2ND AND 3RD VERTICAL STIFFENER ON CUT OUT EDGES; WEB AND EXISTING FASTENERS HOLES WITHIN THE REPAIR AREA TO ENSURE NO CRACKS EXIST.;[04] PERFORMED GVI OF ALL AREAS WITHIN THE REPAIR AREA; NO DEFECTS NOTED IAW SRM 55-10-09-2R-4 STEP E.;[05] VERIFIED CORRECTIVE ACTION 1;2 AND 4.; FABRICATED REPAIR PARTS FOR STIFFENERS 2 AND 3; (1) T-SECTION FROM 60-5872 7075 T76511 LOT# 1449876-1 (2) ANGLE FROM BAC 1490-2793 7075 T62 CLAD LOT# 1442205-1 (3) SHIM FROM 7075 T6 0.020' CLAD LOT# 1381332-1; APPLIED CHEMICAL CONVERSION COATING IAW SRM 55-10-09-2R-4 OK TO PRIME.;[08] VERIFIED CORRECTIVE ACTION 7.<BR>OK TO PRIME;[09] PRIMED REPAIR PARTS FOR STIFFENERS 2 AND 3 AND COMMON AREA IAW SRM 55-10-09-2R-4 OK TO INSTALL.;[10] VERIFIED CORRETIVE ACTION 9.<BR>OK TO INSTALL;[11] INSTALLED REPAIR PARTS ON STIFFENERS 2 AND 3 AT LH HORIZONTAL STABILIZER STA 120.30 RIB IAW SRM 55-10-09-2R-4;[12] RII VERIFIED CORRECTIVE ACTION ITEM 11.;[13] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE.

ATA 5300

CRACK ON ST B PULLEY ATTACH ANGLE AT BS 1040 RBL 8 ABOVE STRINGER 25R.(MARKED)<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02 PARAG. 9; REPAIRABLE BY REPLACEMENT.;[02] REMOVED STB PULLEY ATTACH CLIP AT BS 1040 RBL 8 ABOVE STRINGER 25R PER SRM 51-40-02.;[03] FABRICATED NEW CLIP FROM LOT # 1517370-1 2024-T3 0.063'; LOCATED AND DRILLED PER SRM 51-40-05 AND DWG 251A4921 REV A.;[04] VERIFIED CORRECTIVE ACTION 3 AND THE MEASUREMENT TABLE.;[05] RECEIVED CLIP FROM O.S.S. ITEM HFAB53-CL-002 PO# 915446/1; OK TO PRIME.;[06] VERIFIED CORRECTIVE ACTION 5.<BR>OK TO PRIME;[07] APPLIED PRIMER ON CLIP IAW AMM 51-21-99 OK TO INSTALL.;[08] VERIFIED CORRECTIVE ACTION 7. OK TO INSTALL.;[09] INSTALLED CLIP IAW SRM 51-40-02 AND DWG 251A3340;[10] VERIFIED CORRECTIVE ACTION #9

ATA 5314

WING CENTER SECTION - LH VAPOR BARRIER HAS A CRACK BS 663 LBL 15 WL 148 (MARKED)<DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR.4 D(1) TO BE REPAIRED IAW SRM 51-70-04-2R-10 AS DIRECTED BY SRM 57-10-10-2R-2 PAR.1 C(NOTE)<BR><BR>REMOVED DAMAGED FIBERS; CLEANED AND PREPARED BOTH SURFACES IAW SRM 51-70-04-2R-10 PAR.4 A-C;[02] VALIDATED APPLICABILITY OF REPAIR TO BE COMPLETED IAW SRM 51-70-04-2R-10.;[03] VERIFIED CORRECTIVE ACTION 1 AND 2 <BR><BR>VALIDATED APPLICABILITY OF REPAIR TO BE COMPLETED IAW SRM 51-70-04-2R-10.;[04] FABRICATED REPAIR PLIES FOR BOTH SURFACES FROM BMS 9-3 ST1581 LOT#1522395-2 IAW SRM 51-70-04-2R-10 PAR.4 D< INSTALLED REPAIR PLIES ON BOTH SURFACES USING BMS8-301 CL1 LOT#JH2EAA8895; VACUUM BAGGED; LEAK CHECKED GOOD USING VACUUM GAUGE ID:ATS2441 DUE:08/2023 IAW SRM 51-70-04-2R-10 PAR.4 D-E SET REPAIR PLIES TO CURE USING HOT BONDER ID:ATS883 DUE:10/2023 IAW SRM 51-70-04-2R-10 PAR.4 F;[09] CURED REPAIR PLIES; REMOVED VACUUM BAGGING MATERIALS AND LIGHTLY SANDED REPAIR AREA IN PREPARATION FOR REFINISHING. WORK ACCOMPLISHED IAW SRM 51-70-04-2R-10 PAR 4.F+H.; RII VERIFIED GOOD INSTALLATION OF REPAIR PARTS IAW SRM 51-70-04-2R-10.;[12] NDT UT INSPECTED REPAIR AREA PER SRM 51-70-04-2R-10 AND SRM 51-70-04-2R-0 PARA 4. O; AND 737 NDTM PART 4; 51-00-02; NO DEFECTS NOTED.<BR>EQUIP ID ATS2341 DUE 06/23;[13] INSPECTED REPAIR AREA PER SRM 51-70-04-2R-10 AND SRM 51-70-04-2R-0 PARA 4. O; REFINISHED REPAIR AREA IAW SRM 51-70-04-2R-10 PAR 4.H.

ATA 5340

INTERNAL - HORIZONTAL PRESSURE DECK WEB STA 663 TO STA 675 - LBL 30 TO LBL 45. MULTIPLE CRACKS NOTED. MARKED AREAS.<[01] SRM 53-40-51-2R-2 REPAIR 2 IS APPLICABLE TO THIS A/C;[02] CUT AND REMOVED THE DAMAGED PART OF WEB IAW SRM 53-40-51-2R-2 REPAIR 2 STEP 4C(3) VIEW B FIGURE 203;[09] FABRICATED A -1 DOUBLER AND -4 & -7 FILLERS FROM 2024T3#0.080' CLAD LOT#1497191-1; -2 (7EA) STIFFERNERS FROM BAC1505-100052 7075-T6511 EXTRUSION LOT#1508574-1; -3 WEB AND -8 & -9 FILLERS FROM 2024T3#0.063' CLAD LOT# 1524605-1; -6 (3EA) FILLERS FROM 2024T3#0.090' CLAD LOT# 1501154-1 PLUS 2024T3#0.020 CLAD LOT# 1515185-1; -5 (3EA) FILLERS FROM 2024T3#0.020' CLAD LOT# 1515185-1 IAW SRM 53-40-51-2R-2 REPAIR 2. OK TO TREAT AND PRIME REPAIR PARTS;16] INSTALLED REPAIR PARTS IAW SRM 53-40-51-2R-2 REPAIR 2;[17] VERIFIED CORRECTION ACTION ITEM 16.;[18] VERIFIED ALL CORRECTION ACTIONS CARD COMPLETE.

ATA 5753

PANEL 561CB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B(5).WILL BE REPAIRED IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 2.B(2) AND TABLE 202.<BR>REMOVED ALL DAMAGE AT FASTENER HOLES TO .5' DIAMETER; CLEANED REPAIR AREA IAW SRM 51-70-04-2R-9 PARA 4.A-C.[04] APPLIED SLURRY MIXTURE OF BMS 8-301CL1 LOT#JH2EAA8895 AND CHOPPED FIBERS TO FASTENER HOLES; CURED WITH HEATLAMP; MONITORED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023; SANDED CONTOUR TO SURFACE AND CLEANED REPAIR AREA IAW SRM 51-70-04-2R-9 PARA 4.D-I.;[05] FABRICATED AND INSTALLED REPAIR PLIES USING BMS 9-3 TYH2 CL7 STY1581 LOT# 1522395-2 AND BMS 8-301 CL1 GR1 LOT# JH2EAA8895 IAW SRM 51-70-04-2R-9 PARA 4.J-K. VACUUM BAGGED REPAIRS. LEAK CHECKED GOOD USING VACUUM GAUGE ID: ATS2441 CAL DUE: 08/2023. SET REPAIR TO CURE BY HEAT LAMP USING THERMOMETER ID: ATS2209 CAL DUE: 10/2023 IAW SRM 51-70-04-2R-9 PARA 4.L-M.;[06] COMPLETED CURE; UNBAGGED AND TRIMMED EXCESS MATERIAL IAW SRM 51-70-04-2R-9 PARA 4.M;P.POST REPAIR UT INSPECTED PER 737NDT PART 4 51-00-02. NO DEFECTS FOUND. TOOL N650 ATS2341 DUE 06/2023.;[09] LOCATED AND DRILLED FASTENER HOLES IN REPAIR AREA IAW SRM 51-70-04-2R-9 PARA 4.N.;[10] COUNTERSUNK FASTENER HOLES IAW SRM 51-70-04-2R-9 PARA 4.N;[11] APPLIED CONDUCTIVE COATING; RESISTIVITY TESTED GOOD WITH MULTIMETER ID:ATS1499 CAL DUE 11/30/23 IAW AMM 51-21-71-370-801 PARA 3.D(1-4)(7).<BR>REFINISHED PANEL IAW SRM 51-70-04-2R-9 PARA 4.P

ATA 3350

REMOVE EMERGENCY LIGHTS BATTERY PACK M1675 FOR USE ON A/C 8574 **CORRECTED FAULT DESCRIPTION **REMOVE EMERGENCY LIGHTS BATTERY PACK M1675 FOR USE ON A/C 8527<[01] REMOVED BATTERY PACK M1675 IAW AMM 33-51-06-960-805 STEP E. (1 - 4);[02] INSTALLED SERVICEABLE EMERGENCY BATTERY INTO M1675 AND TESTED PER AMM 33-51-06-960-805; NO DEFECTS NOTED.;[03] VERIFIED CORRECTIVE ACTIONS STEP 2.

ATA 5753

PANEL 561AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B(5).REPAIRED IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 2.B(2) AND TABLE 202.REMOVED ALL DAMAGE AT FASTENER HOLES TO .5' DIAMETER; CLEANED REPAIR AREA IAW SRM 51-70-04-2R-9 PARA 4.A-C.APPLIED SLURRY MIXTURE OF BMS 8-301CL1 LOT#JH2EAA8895 AND CHOPPED FIBERS TO FASTENER HOLES; CURED WITH HEATLAMP; MONITORED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023; SANDED CONTOUR TO SURFACE AND CLEANED REPAIR AREA IAW SRM 51-70-04-2R-9 PARA 4.D-I.;[05] FABRICATED AND INSTALLED REPAIR PLIES USING BMS 9-3 TYH2 CL7 STY1581 LOT# 1522395-2 AND BMS 8-301 CL1 GR1 LOT# JH2EAA8895 IAW SRM 51-70-04-2R-9 PARA 4.J-K. VACUUM BAGGED REPAIRS. LEAK CHECKED GOOD USING VACUUM GAUGE ID: ATS2441 CAL DUE: 08/2023. SET REPAIR TO CURE BY HEAT LAMP USING THERMOMETER ID: ATS2209 CAL DUE: 10/2023 IAW SRM 51-70-04-2R-9 PARA 4.L-M.;[06] COMPLETED CURE; UNBAGGED AND TRIMMED EXCESS MATERIAL IAW SRM 51-70-04-2R-9 PARA 4.M;PLOCATED AND DRILLED FASTENER HOLES IN REPAIR AREA IAW SRM 51-70-04-2R-9 PARA 4.N.;[10] COUNTERSUNK FASTENER HOLES IAW SRM 51-70-04-2R-9 PARA 4.N;[11] APPLIED CONDUCTIVE COATING; RESISTIVITY TESTED GOOD WITH MULTIMETER ID:ATS1499 CAL DUE 11/30/23 IAW AMM 51-21-71-370-801 PARA 3.D(1-4)(7).<BR>REFINISHED PANEL IAW SRM 51-70-04-2R-9 PARA 4.P

ATA 3350

OVER WING EXIT SIGN; RIGHT SIDE MISSING / [01] INSTALLED RT SIDE OVER WING EXIT SIGN LEN ONLY PER AMM 33-51-01; OPS CHECK EMERGENCY LIGHT; LIGHT CHECK OUT GOOD

ATA 2740

LOSS OF STAB TRIM ON T/O (ELEC) RAN CHKLST NORMAL LANDIN (15 FLAPS) NO BRK COOLING REQ'D AUTOPILOT TRIM O.K. / [01] REMOVED AND REPLACED STAB TRIM MOTOR AS PER AMM 27-41-71 OPS CHECK GOOD

ATA 3350

FWD SERVICE DOOR OVER DOOR; FWD EXIT DOOR LOCATOR; FWD ENTRY DOOR SLIDE EMERGENCY LIGHTS ONLY ILLUMINATE BRIEFLY / [01] REMOVED AND REPLACED M1675 EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.

ATA 3320

ON INITIAL CLIMB OUT AN ELECTRICAL SMELL WAS REPORTED IN AFT CABIN-NO SMOKE NOTED - SMELL DISAPATED / [01] C/W CONDITIONAL INSP PER AMM 05-51-56 - FOUND SMELL SOURCE TO BE CEILING LIGHTS AT 19-22 ABC (2 LIGHTS) INOP AND OK TO CONTINUE PER MEL 33-2-03 SP 1. REPLACED 2EA CEILING LIGHT ASSEMBLY @ 19-22ABC IAW AMM 33-22-00.OP?S CHECKED NORMAL.

ATA 5350

PANEL 193 B HAS NUMEROUS FASTENER HOLES ELONGATED / [01] R & R PANEL PER SRM 51-40-02.

ATA 2565

FA REPORT R2 DOOR EVAC SLIDE GAGE READING LOW OUTSIDE GREEN BAND ; / [01] R&RD AFT SERVICE DOOR SLIDE PER MT#725-61-06-AS

ATA 3350

PASSENGER CABIN EMERGENCY LIGHT BULB OUT AT ROW 7 L/H ; / [01] REMOVED AND REPLACED PASSENGER CABIN EMERGENCY LIGHT BULB AT ROW 7 L/H IAW AMM 33-51-03

ATA 2740

AFTER TAKE OFF THE MAIN ELECTRIC TRIM FAILED ; / REMOVED AND REPLACED HORIZONTAL STAB TRIM MOTOR PER AMM 27-41-71

ATA 3350

EMERGENCY EXIT LIGHT BATTERY ATTACH POINT BROKEN ON BATTERY CHARGER M1672 / REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY POWER SUPPLY AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-806. 56489U 12APR21 (M1672)

ATA 3397

RH OVERWING ESCAPE LIGHT IS INOP. / UPON FURTHER INVESTIGATION; FOUND CONNECTOR D11076; OVERWING ESCAPE LIGHT R/H; TO BE DISCONNECTED. CONNECTED CONNECTOR D11076; PERFORMED A GOOD OPERATIONAL CHECK PER AMM 33-51-04-960-801 STEP 2.F.(2) 59234U 12APR21

ATA 3350

EXIT INDICATOR LIGHT L1188 AT STA 606; WL 224; RBL 70 IS INOP. / REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY M1669; PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-806. 59234U 12APR21

ATA 3350

AFT SERVICE ENTRY SLIDE LIGHT IS INOP. / RELAMPED AFT SERVICE ENTRY SLIDE LIGHT; PERFORMED A GOOD OPERATIONAL CHECK PER AMM 33-51-04-900-801 STEPS 2.1.(A)-(B);(D)-(2) 59234U 12APR21

ATA 5320

FWD CARGO BAY INTERCOSTAL HAS A ELONGATED HOLE COMMON TO THE WEB BS500C+10' LBL 18 WL155 / REMOVED AND INSTALLED NEW FWD CARGO BAY INTERCOSTAL AT BS 500C TO 500D; LBL 18 WL 155 ITEM# HFAB53-IN-010; PO# 820459; IAW SRM 53-00-53-1A-2; SRM 51-40-02-0G-0 DWG# 143A7503 R.V.D; SRM 51-40-05-0G-0; DWG# 143A7505; DWG# 143A7500 R.V.A.

ATA 5711

RH OUTER WING FRONT SPAR ANGLE ABOVE FUEL BOOST PUMP AT IFSS 120 IS CRACKED / REMOVED AND REPLACED R/H OUTER WING FRONT SPAR ANGLE ABOVE FUEL BOOST PUMP AT IFSS 120 IAW SWA EA 21-157-00983; REV IR AND ATS ER 21-01563; REV IR

ATA 5320

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-24L. REMOVED DAMAGED BKD SUPPORT GUSSET AND INSTALLED NEW BKD SUPPORT GUSSET BS 500D S24L IAW SRM 5140020G0 AND DWG 143A7902

ATA 5340

P18 BULKHEAD ATTACH BRACKET IS CHAFED AT STRINGER 6 LEFT; B.S. 259. REMOVED & REPLACED P18 BULKHEAD ATTACH BRACKET 2 PER SRM 5140020G0 & DWG #'S 141A9502 & 141A0720

ATA 5321

FORWARD PASSENGER CABIN FLOORBOARD 221GF FORWARD O/B CORNER (TANG) IS BROKEN / DUE TO THE EXTENT OF DAMAGE ON FORWARD PASSENGER CABIN FLOORBOARD 221GF; REPLACED FLOOR PANEL 221GF IAW SRM 51-10-02-0G-0 PAR 9A(1); AND AIPC 53-21-51-20 ITEM 340. 56563U 23MAR21

ATA 5321

AFT PASSENGER CABIN FLOORBOARD 241XF HAS DAMAGED UPPER SURFACE PLIES / DUE TO THE EXTENT OF DAMAGE ON AFT PASSENGER CABIN FLOORBOARD 241XF; REPLACED FLOORBOARD 241XF IAW SRM 51-10-02-0G-0 PAR 9A(1); AND AIPC 53-21-00-26 ITEM 59 56563U 23MAR21

ATA 5350

FAIRING 643AB HAS EROSION DAMAGE ON OUTER SKIN FAIRING 643AB WITH EROSION DAMAGE ON OUTER SKIN WAS REPALCED WITH A SERVICEABLE FAIRING. (POS: #7; TAG NO.: 782236; PN OFF: 113A92102; SN OFF: WN551; PN ON: 113A92102; SN ON: 7827 #1)

ATA 5321

FORWARD PASSENGER CABIN FLOORBOARD 221BF HAS DAMAGED UPPER SURFACE SKIN / DUE TO THE EXTENT OF DAMAGE ON FORWARD PASSENGER CABIN FLOORBOARD 221BF; REPLACED FLOORBOARD 221BF IAW SRM 51-10-02-0G-0 PAR 9A(1); AND AIPC 53-21-51-20 ITEM 80. 56563U 23MAR21

ATA 5321

FORWARD PASSENGER CABIN FLOORBOARD 221DF HAS DAMAGED UPPER SURFACE SKIN / DUE TO THE EXTENT OF DAMAGE ON FORWARD PASSENGER CABIN FLOORBOARD 221DF; REPLACED FLOORBOARD 221DF IAW SRM 51-10-02-0G-0 PAR 9A(1) AND AIPC 53-21-51-20 ITEM 175 56563U 23MAR21

ATA 5321

AFT PASSENGER CABIN FLOORBOARD 241ZF HAS DAMAGED UPPER SURFACE PLIES / DUE TO THE EXTENT OF DAMAGE ON AFT PASSENGER CABIN FLOORBOARD 241ZF; REPLACED FLOORBOARD 241ZF IAW SRM 51-10-02-0G-0 PAR 9A(1); AND AIPC 53-21-00-26 ITEM 76. 56563U 23MAR21

ATA 5321

AFT PASSENGER CABIN FLOORBOARD 241YF HAS DAMAGED UPPER SURFACE PLIES / DUE TO THE EXTENT OF DAMAGE ON AFT PASSENGER CABIN FLOOR PANEL 241YF; REPLACED FLOORBOARD 241YF IAW SRM 51-10-02-0G-0 PAR 9A(1); AND AIPC 53-21-00-26 ITEM 66 56563U 23MAR21

ATA 5330

CORROSION ON EXTERNAL CROWN SKIN BS 1027-1035 STR 2 L/H - STR 2 R/H LBL14-RBL-14 WL308.5 / REPAIRED EXTERNAL CROWN SKIN BS 1027-1035 STR 2 L/H- STR 2 RH LBL14-RBL14 WL 308.5 IAW EA 21-153-01059 REV IR DATED 04/14/2021 & ATS ER 21-01566 REV IR DATED 04/15/2021

ATA 5320

CORROSION ON SUPPORT ANGLE ON CROWN SKIN BS 1036 STR 2 LH STR 2 RH WL 310 THIS SUPPORT ANGLE DOES NOT HAVE SRM ALLOWABLE DAMAGE THEREFORE WILL BE REPAIRED BY REPLACEMENT PER REF SRM 5110020G0 PARAGRAPH 9C. REMOVED AND REPLACED SUPPORT ANGLE AT CROWN SKIN BS1036 STR 2LH STR 2RH PER REF SRM 5140020G0 AND DWG NBR. 148A3110

ATA 5340

***CORROSION*** ON STRINGER ATTACH ANGLE AT AFT CARGO BAY BS787 S-27L WL151. / REMOVED AND REPLACED STRINGER ATTACH ANGLE AT AFT CARGO BAY 787 S-27L I.A.W SRM 51-40-02-0G-0 AND DRAWING # 146A7810. VERIFIED APPLICABILITY PER SRM. NO ALLOWABLE DAMAGE PART DON'T HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G-0 PART 9.C.

ATA 5347

CHAFING DAMAGE ON RAIL AT AFT CARGO BAY BS767+9 RBL8 WL157. REJECTED DUE TO SRM 53-00-53-2R-2 STEPS 4.Q.(3); 4.R.; AND 4.S. HAVE NOT BEEN ACCOMPLISHED INSP 267 4-10-21 / SEALED THE GAP ON ACB RAIL REPAIR PARTS AND APPLIED CHEMICAL CONVERSION COATING TO REPAIR PARTS IAW SRM 53-00-53-2R-2 REPAIR 2 STEP 4Q TO R5

ATA 5311

CRACKED FRAME AT B.S. 727B AT STRINGER 8R AIR CONDITIONING ATTACH BRACKET. / REPAIRED FRAME ON BS 727B AT STR 8R PER EA 1-A53-12114 REV 5. 57006U 26MAR21

ATA 5320

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727B - BS787 LBL21 WL157. / REMOVED AND REPLACED FLOOR SIDEWALL SUPPORT AT AFT CARGO BAY BS 727 - 847 LBL 21. WL. 157 I.A.W SRM 51-40-02-0G-0. AND DRAWING # 146A7500. FOOR TO SIDEWALL SUPPORT WAS EVALUATED. AND FOUND TO BE OUT OF LIMITS. I.A.W SRM 53-00-53-1A-2; L=1.1' X W=0.7' X D=0.007' FROM ORIGINAL THICKNESS OF 0.040' PART CALLED REPAIRABLE BY REPLACEMENT

ATA 5311

CRACKED FRAME AT B.S. 867 AT STRINGER 8R AIR CONDITIONING ATTACH BRACKET. / REPAIRED FRAME ON BS 867 AT STR 8R PER EA 1-A53-12114 REV 5. 57006U 26MAR21

ATA 5340

***CORROSION*** ON STRINGER ATTACH ANGLE AT AFT CARGO BAY BS727D S-27L WL150. / REMOVED & REPLACED ATTACH ANGLE -11 AT DISCREPANCY AREA; PER SRM 51-40-06 & DWG 146A7810 REV A.

ATA 5313

CORROSION ON STRINGER SPLICE AT AFT CARGO BAY BS885 S-22L WL176. / CORROSION FOUND ON STR. SPLICE BS 885 STR-22L WL-176 FOUND TO BE OUT OF LIMITE IAW SRM 53-00-03-1A-1 FORMED STR. SPLICE MADE FROM BAC 1498 -270#7075 TO LOT # 1A55882-1 IAW DWG # 147A3288 REV A SENT TO OSS AND RECIEVED IN THE FORM OF 7075T62 WITH PO. # 1456076 LOCATED AND DRILLED IAW SRM 51-40-05-0G-0 AND DWG # 147A3288 APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW AMM 51-21-41-370-802 & AMM 51-21-72-370-804 AND INSTALLED IAW DWG # 147A0060 AND SRM 51-40-02-0G-0

ATA 5320

BENT SIDEWALL SUPPORT AT AFT CARGO BAY BS727D RBL25 WL157. / REMOVED AND REPLACED ON ACB SIDEWALL SUPPORT BS727D RBL 25 ITEM 7531775. LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 146A1220 80641U 06APR21

ATA 5347

BENT RAIL AT AFT CARGO BAY BS727A - BS727C RBL3 WL156. / INSTALLED REPAIR PARTS ON RAIL FROM BS 727 TO BS 727C + 10 FABRICATED SPLICE FROM P/N 7530199 RAIL SECTION FROM BAC 1509-100146 LOCATED AND DRILLED AND APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 53-00-53-2R-2 AND DWGS 146A7503 AND DWG 146A7500 80641U 08APR21

ATA 5320

BENT INTERCOSTAL AT AFT CARGO BAY BS727A - BS727B RBL3 WL154. / REMOVED & REPLACED INTERCOSTAL AT AFT CARGO BAY BS 727A - 727B RBL 3 WL 154 IAW SRM 51-40-02 & REF BOEING DWG 146A7500 SHT 19 REV -

ATA 5340

BENT INTERCOSTAL ATTACH ANGLE AT AFT CARGO BAY BS727B RBL3 WL156. / REMOVED AND INSTALLED NEW INTERCOSTAL ATTACH ANGLE AT AFT CARGO BAY BS 727B RBL 3 WL 156 PO# 819972-SWA PN 146A1310-26 IAW SRM 53-00-53-1A-2; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG # 146A1310; DWG# 146A7810 57319U 09APR21 ITEM # HFAB53-CL-012

ATA 5322

CORROSION ON SHEAR TIE AT AFT CARGO BAY BS927 JUST ABOVE S-22L WL179. / REMOVED AND REPLACED ACB SHEAR TIE AT BS927; S-226; WL179 PER ER 21-01665 REV IR AND SWA EA 21-153-01013 REV IR.

ATA 5347

CRACKED TRACK AT AFT CARGO BAY BS767 LBL17 WL156. / REMOVED AND INSTALLED NEW TRACK AT AFT CARGO BAY BS 727 TO BS 867 LBL 17 WL 156 ITEM # 7531208; P/O# 820236 IAW SRM 53-00-53-1A-2; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG# 146A7501; DWG# 146A7500

ATA 5340

***CORROSION*** ON STRINGER CLIP AT AFT CARGO BAY BS727C RBL15 WL154. / REMOVED AND REPLACED ON ACB STRINGER CLIP BS 727C RBL 15 WL 154 P/N 146A1010-34 PO# 819707 IAW SRM 51-40-02 AND DWG 146A1010- 80640U 03APR21

ATA 5320

***CORROSION*** ON STRINGER CLIP AT AREA AFT OF ACB BS1006 LBL9 WL187. / REMOVED AND REPLACED STRINGER CLIP AT AREA AFT OF ACB BS1006 LBL9 WL187 PER REF SRM 51-40-02-0G AND DWG NBR 147A0040

ATA 5340

***CORROSION*** ON STRINGER CLIP AT AFT CARGO BAY BS887 S-22L WL176. / CORROSION FOUND ON STR. CLIP BS 887 STR 22L WL 176 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL REPAIRED BY REPLACMENT IAW SRM 51-10-02-0G-0 PAR-9C LOCATED AND DRILLED NEW STR CLIP P/N 147A3500Y50 LOT# 1455105-1 IAW SRM 51-40-05-0G-0 AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG # 147A0060 REV-A; DWG # 147A3287 REV.

ATA 5340

***CORROSION*** ON STRINGER CLIP AT AFT CARGO BAY BS907 S-22L WL177. / CORROSION ON STRINGER CLIP AT ACB BS 907 S-22L WL 177 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM DOES NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED BS 907 S-22L STRINGER CLIP PN# 147A3500-22; PO# 819573 IAW SRM 51-40-02 AND IAW DWG# 147A0010

ATA 5340

***CORROSION*** ON STRINGER CLIP AT AFT CARGO BAY BS907 S-21L WL183. / ORIGINAL PART FOUND TO BE OUT OF LIMITS. REMOVED; LOCATED & DRILLED; AND INSTALLED NEW PER SRM 51-40-05; SRM 51-40-02-0G-0 STEP 4; & BOEING DRAWING 147A0010.

ATA 5340

***CORROSION*** ON STRINGER CLIP AT AFT CARGO BAY BS927 S-22L WL180. / CORROSION ON STRINGER CLIP AT ACB BS 927 S-22L WL 180 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM DOES NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED BS 927 S-22L STRINGER CLIP PN# 147A3500-6; PO# 819574 IAW SRM 51-40-02 AND IAW DWG# 147A0010

ATA 5340

***CORROSION*** ON STRINGER CLIP AT AFT CARGO BAY BS927 S-23L WL176. / CORROSION ON STRIGER CLIP AT ACB BS 927 S-23L WL 176 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM PART REPAIRABLE BY REPLACEMENT. REMOVED AND REPLACED STRINGER CLIP BS 927 S-23L WL 176 I.A.W SRM 51-10-02 STEP 9.C; SRM 51-40-02-0G-0 AND BOEING DWG # 147A0010

ATA 5320

***CORROSION*** ON INTERCOSTAL AT AFT CARGO BAY BS927 - BS947 LBL3 WL174. / REMOVED AND INSTALLED NEW INTERCOSTAL ON ACB INTERCOSTAL BS927 - BS947 LBL3 ITEM HFAB53-IN-011 PO# 820647 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 147A7580; DWG 147A7500 80641U 10APR21

ATA 5340

PASSENGER CABIN S-1 STRINGER CLIP CRACKED AT BS294. MARKED / REMOVED; FABRICATED; & INSTALLED PASSENGER CABIN S-1 STRINGER CLIP AT BS 294 PER SRM 51-40-02-0G-0 STEP 4 FIGURE 8; BOEING DRAWING: 141A1250; & BOEING DRAWING: 141A0741. CORROSION INHIBITING COMPOUND RESTORED PER AMM 51-21-91-620-802. STRINGER CLIP FABRICATED USING 7075-T62 EXTRUSION LOT# 1388621-1.

ATA 5511

R/H HORIZ STAB LEADING EDGE HAS CRACKED RIB AT L/E STA 95.96 / REMOVED AND REPLACED R/H HORIZ STAB LEADING EDGE RIB AT L/E STA 95.96 IAW SRM 51-40-02 AND DWG 186A1001 88920U 05APR21

ATA 5320

CRACKED INTERCOSTAL AT PASSENGER CABIN BS328 - BS344 LBL44 WL208. / REMOVED AND REPLACED INTERCOSTAL AT PASSANGER CABIN BS 328 - BS 344 LBL 44; WL. 208 I.A.W SRM 51-40-02-0G-0 AND DRAWING # 141A5900. INTERCOSTAL WAS REPLACED DUE TO NO FOUND ALLOWABLE DAMAGE ON SRM 53-10-51-0I-2 PART CALLED REPAIRABLE BY RAPLACEMENT I.A.W SRM 51-10-02-0G-0 PARAGRAPH 9.C.

ATA 5320

CRACKED INTERCOSTAL AT PASSENGER CABIN BS312 - BS328 LBL44 WL208. / REMOVED AND REPLACED INTERCOSTAL AT PASSENGER CABIN BS 312 - BS 328 LBL 44. WL. 208. I.A.W SRM 51-40-02-0G-0 AND DRAWING # 141A5400.; INTERCOSTAL WAS REPLACED DUE TO NO FOUND ALLOWABLE DAMAGE ON SRM 53-10-51-0I-2. PART CALLED REPAIRABLE BY REPLACEMENT

ATA 5320

CRACKED INTERCOSTAL AT PASSENGER CABIN BS277 - BS294 BL0 WL208. / REMOVED AND REPLACED INTERCOSTAL AT PASSENGER CABIN BS 277 - BS 294 BL 0 WL 208 I.A.W SRM 51-40-02-0G-0 AND DRAWING # 141A5400; INTERCOSTAL WAS REPLACED DUE TO NO FOUND ALLOWABLE DAMAGE ON SRM 53-10-51-0I-2 PART CALLED REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G-0 PARAGRAPH. 9.C.

ATA 5320

***CORROSION*** ON INTERCOSTAL AT AFT CARGO BAY BS927 - BS947 RBL3 WL174. / REMOVED CORROSION ON ACB INTERCOSTAL BS 927 - BS 947 RBL 3 WL 174 BLEND WAS 1.9' X .4' X .005 ORIGINAL THICKNESS .045 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ACB INTERCOSTAL BS 927 - BS 947 RBL 3 WL 174 I.A.W SRM 51-10-02; SRM 53-00-53-1A-2; SRM 51-40-02-0G-0 AND BOEING DWG# 147A7500

ATA 5340

***CORROSION*** ON STRINGER CLIP AT AFT CARGO BAY BS807 S-26L WL156. / REMOVED AND REPLACED STRINGER CLIP P/N 146A1010-27 AT AFT CARGO BAY B/S 807 S-26L WL 156 IAW SRM 51-10-02 PARAGRAPH 9 SRM 51-40-02 AND DWG 146A1263 REV: 59900U 27MAR21

ATA 5340

***CORROSION*** ON STRINGER CLIP AT AFT CARGO BAY BS807 S-26R WL156. / REMOVED AND REPLACED STRINGER CLIP AT ACB BS 807 S-26R. WL 156. I.A.W SRM 51-40-02-0G-0 AND DRAWING# 146A1263; VERIFIED APPLICABILITY PER SRM. NO ALLOWABLE DAMAGE PART DON'T HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT

ATA 5320

SUPPORT ANGLE BEHIND WATER SERVICE PANEL CRACKED AT AFT CARGO BAY BS918 RBL11 WL171. REMOVED AND REPLACED ACB SUPPORT ANGLE BEHIND WATER SERVICE PANEL BS 918 RBL 11 WL 171 IAW SRM 514002 AND DWG # 147A7221 84632U 26MAR21

ATA 5320

SUPPORT ANGLE BEHIND WATER SERVICE PANEL CRACKED AT AFT CARGO BAY BS914 RBL11 WL171. REMOVED AND REPLACED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS914 RBL 11 WL 171 IAW SRM 514002 AND DWG# 147A7221 84632U 26MAR21

ATA 5340

CRACKED BULKHEAD SUPPORT ATTACH ANGLE AT AFT CARGO BAY BS865 LBL11 WL166. REMOVED AND REPLACED BULKHEAD SUPPORT ATTACH ANGLE AT BS865 LBL11 WL166 PER SRM 514002; SRM 514005; DWG #149A8103 REV D AND DWG # 149A8102 REV A

ATA 5320

***CORROSION*** ON GUSSET AT AREA AFT OF ACB BS990 BS990 RBL22 WL188. THIS GUSSET DOES NOT HAVE ALLOWABLE DAMAGE LIMITS PER SRM THEREFORE WILL BE REPAIRED BY REPLACEMENT IAW SRM 511002 STEP 9C REMOVED AND REPLACED GUSSET AT AREA AFT OF ACB BS990 RBL 22 WL188 PER REF SRM 5140020G AND DWG NBR 147A7427; 147A0002 (PART WAS HEAT TREATED TO T62 CONDITION PER BAC5602 ON ATS W.O. 538465)

ATA 5320

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727 BS767 RBL21 WL157. ORIGINAL AFT CARGO BAY FLOOR SIDEWALL SUPPORT; BS727 BS767 FOUND TO BE OUT OF LIMITS. REMOVED ORIGINAL; LOCATED & DRILLED NEW PART; AND INSTALLED PER: SRM 5140020G0; BOEING DRAWING: 146A7500; & SRM 5140050G0.

ATA 5320

***CORROSION*** ON SIDEWALL SUPPORT AT AFT CARGO BAY BS727D LBL26 WL157. REMOVED AND REPLACEMENT ON ACB SIDEWALL SUPPORT NEW BS 727D S 19L S 26L. ITEM 7531776 IAW SRM 514005; SRM 514002 AND DWG 146A1220 80641U 06APR21

ATA 5320

***CORROSION*** ON GUSSET AT AREA AFT OF ACB BS990 RBL28 WL187. THIS ITEM DOES NOT HAVE SRM ALLOWABLE DAMAGE EVALUATION; THEREFORE WILL BE REPAIRED BY REPLACEMENT PER REF SRM 5110020G0 PARAGRAPH 9C. REMOVED AND REPLACED GUSSET AT AREA AFT OF ACB BS 990 RBL28 WL187 PER REF SRM 5140020G AND DWG NBR 147A0002 AND 147A7427

ATA 5313

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS540 S-26R WL153. / REMOVED DAMAGED STR SECTION AND INSTALLED REPAIR PARTS BS 540 - 500D+6' S-26R IAW SRM 53-00-03-2R-1 & DWG 143A3230; 143A1215

ATA 5320

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / REMOVED DAMAGED BKD SUPPORT GUSSET AND INSTALLED NEW BKD SUPPORT GUSSET BS 500D S-19R WL 193 IAW SRM 51-40-02-0G-0 AND DWG 143A7902

ATA 5320

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-21L WL177. MARKED / REMOVED DAMAGED BKD SUPPORT GUSSET AND INSTALLED NEW BKD SUPPORT GUSSET BS 500D S-21L WL177 IAW SRM 51-40-02-0G-0 AND DWG 143A7902

ATA 5320

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-22L WL172. MARKED / REMOVED DAMAGED BKD SUPPORT GUSSET AND INSTALLED NEW BKD SUPPORT GUSSET AT BS 500D S-22L IAW SRM 51-40-02-0G-0 AND DWG 143A7902

ATA 5320

FWD CARGO BAY INTERCOSTAL ATTACH ANGLE IS CRACKED BS500C FWD SIDE RBL25 WL155. / REMOVED FCB INTERCOSTAL ATTACH ANGLE BS 500C FWD SIDE RBL 25 IAW SRM 51-40-02-0G-0. 80512R 24MAR21 AND INSTALLED NEW INTERCOSTAL ATTACH ANGLE BS 500C FWD SIDE RBL 25 WL 155 IAW SRM 51-40-02-0G-0 AND DWG 143A7505

ATA 5320

FWD CARGO BAY INTERCOSTAL ATTACH ANGLE IS CRACKED BS400 RBL25 WL155. / REMOVED FCB INTERCOSTAL ATTACH ANGLE BS400 RBL25 WL155 I.A.W SRM 51-40-02-0G-0 80512R 24MAR21 LOCATED; DRILLED NEW INTERCOSTAL ATTACH ANGLE BS400 RBL25 WL155 I.A.W BOEING DWG 143A7505; SRM 51-40-05-0G-0 OK TO INSTALL 80512R 24MAR21 INSP 357 MAR 24 2021 INSTALLED NEW INTERCOSTAL ATTACH ANGLE BS400 RBL25 WL155 I.A.W BOEING DWG 143A7505 AND SRM 51-40-02-0G-0.

ATA 5320

FWD CARGO BAY INTERCOSTAL ATTACH ANGLE IS CRACKED BS400 LBL25 WL155. / REMOVED FCB INTERCOSTAL ATTACH ANGLE BS 400 LBL 25 WL 155 I.A.W SRM 51-40-02-0G-0 80512R 24MAR21 LOCATED AND DRILLED NEW FCB INTERCOSTAL ATTACH ANGLE BS400 LBL25 WL155 I.A.W BOEING DWG 143A7505; SRM 51-40-05-0G-0 OK TO INSTALL 80512R 24MAR21 INSP 357 MAR 24 2021 INSTALLED FCB INTERCOSTAL ATTACH ANGLE BS 400 LBL25 WL155 I.A.W BOEING DWG 143A7505 AND SRM 51-40-02-0G-0

ATA 5320

VERTICAL STAB SKATE ANGLE ( INTERFACE CLOSURE ANGLE) CHAFED; LH SIDE BS 1120 TO BS 1132 / REMOVED AND REPLACED VERTICAL STAB L/H SKATE ANGLE BS1016 TO BS1132 DUE TO NO ALLOWABLE LIMIT IN THE SRM IAW SRM 51-40-02 AND DWG # 148A8300

ATA 5320

VERTICAL STAB SKATE ANGLE ( INTERFACE CLOSURE ANGLE) CHAFED; RH SIDE BS 1120 TO BS 1132 / REMOVED AND REPLACED VERTICAL STAB R/H SKATE ANGLE BS 1016 TO BS 1132 DUE TO NO ALLOWABLE LIMIT IN THE SRM IAW SRM 51-40-02 DWG # 148A8300

ATA 5340

BENT STRINGER CLIP AT FWD CARGO BAY BS500A S-25R WL156. / THE STRINGER CLIP DOES NOT HAVE ALLOWABLE DAMAGE LIMITS THEREFORE WILL BE REPAIRED BY REPLACEMENT. PER REF SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND REPLACED NEW STRINGER CLIP PER REF SRM 51-40-02-0G-0 AND DWG NBR 143A1222

ATA 5313

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS540 S-25R WL156. / REPAIRED CRACKED STRINGER FCB BS540; S-25R; WL156. PER ATS ER 21-01574 REV IR AND SWA EA 21-153-00961 REV IR

ATA 5313

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS540 S-27L WL150. / REMOVED DAMAGED STR SECTION S-27L AND INSTALLED REPAIR PARTS BS 540 - 500D+6' S-27L IAW SRM 53-00-03-2R-1 & DWG 143A3230; 143A1215.

ATA 5313

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS540 S-26L WL153. / REMOVED DAMAGED STR. SECTION S-26L AND INSTALLED REPAIR PARTS BS 540 - 500D+6' IAW SRM 53-00-03-2R-1 AND DWG 143A3230; 143A1215.

ATA 5313

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS540 S-25L WL156. / REMOVED DAMAGED STR. SECTION S-25L AND INSTALLED REPAIR PARTS BS 540 - 500D+6' IAW SRM 53-00-03-2R-1 & DWG 143A3230; 143A1215

ATA 5320

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / REMOVED BKD SUPPORT GUSSET AND INSTALLED NEW BKD SUPPORT GUSSET BS 500D S-19L WL 193 IAW SRM 51-40-02-0G-0 AND DWG 143A7902

ATA 5320

***CORROSION*** AT FWD CARGO BAY ON AFT BULKHEAD TO FLOOR PANEL SUPPORT ANGLE BS500D LBL23 TO RBL23 WL157. REMOVED DAMAGED BKD TO FLOOR PANEL SUPPORT ANGLE BS 500D LBL 23RBL 23 WL 157 AND INSTALLED NEW BKD TO FLOOR PANEL SUPPORT ANGLE IAW SRM 5140020G0 & DWG 143A7902

ATA 5320

***CORROSION*** ON BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL25 WL157. REMOVED DAMAGED BKD TO SIDEWALL SUPPORT ANGLE AND INSTALLED NEW BKD TO SIDEWALL SUPPORT ANGLE BS 500D S19L S25L IAW SRM 5140020G0 AND DWG 143A7902

ATA 5340

SIDEWALL ATTACH ANGLE BENT AT FWD CARGO BAY BS500B JUST BELOW S24L WL161. REMOVED SIDEWALL ATTACH ANGLE FCB BS 500B BELOW STR 24L WL 161 I.A.W SRM 5140020G0. 80512R 24MAR21 FORMED SIDEWALL ATTACH ANGLE FROM 6013 T4 #0.040' LOT# 13411471 IAW SRM 5130010G0 AND DWG# 417A2106. SENT TO OSS AND RECIEVED IN THE FORM OF T6 LOCATED AND DRILLED IAW SRM 5140050G0 AND DWG# 411A2106. APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 5120010G0 AND SOPM 204404. INSTALLED SIDEWALL ATTACH ANGLE IAW BOEING DWG# 417A2150 REV. B AND SRM 5140020G0. 59577U 04APR21

ATA 5340

SIDEWALL ATTACH ANGLE BENT AT FWD CARGO BAY BS420 JUST ABOVE S23L WL168. REMOVED SIDEWALL ATTACH ANGLE AT FCB BS420 JUST ABOVE STR23L WL168 I.A.W SRM 5140020G0. 80512R 24MAR21 LOCATED AND DRILLED SIDEWALL ATTACH ANGLE FCB BS420 ABOVE STR 23L I.A.W SRM 5140050G0; SRM 5140020G0 AND BOEING DWG 417A2150

ATA 5530

VERTICAL STAB SKATE ANGLE ( INTERFACE CLOSURE ANGLE) CHAFED; LH SIDE BS 1009 TO BS 1016. REMOVED AND REPLACED VERTICAL STAB LH SKATE ANGLE BS1009 TO BS1016 DUE TO NO ALLOWABLE LIMIT FOUND IN THE SRM IAW 514002 AND DWG #147A0030

ATA 5530

VERTICAL STAB SKATE ANGLE ( INTERFACE CLOSURE ANGLE) CHAFED; RH SIDE BS 1009 TO BS 1016. REMOVED AND REPLACED VERTICAL STAB SKATE ANGLE R/H SIDE BS 1009 TO BS 1016 DUE TO NO ALLOWABLE LIMIT FOUND IN THE SRM IAW SRM 514002 AND DWG #147A0030

ATA 5313

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS540 S-23L WL166. / ACCOMPLISHED; REPAIR TO FWD CARGO BAY BS 540 STR 23 L/H WL166 AND RAM AIR INLET SUPPORT STRUCTURE IAW EA 21-153-00871 REV IR AND ATS ER 21-01575 REV IR

ATA 5340

FWD CARGO BAY AFT BULKHEAD SUPPORT ATTACH ANGLE IS MISSING AT BS500D S19R WL193. MARKED INSTALLED ON FCB AFT BULKHEAD SUPPORT ATTACH ANGLE AT BS 500D S19R. WL 193 IAW SRM 514002. ITEM 7510026 PO# 820232 AND DWG 143A7902. LOCATED AND DRILLED IAW SRM 514005

ATA 5347

***CORROSION*** ON TRACK AT FWD CARGO BAY BS400 - BS 500 LBL18 WL157. / REMOVED AND INSTALLED NEW FCB TRACK AT BS 396 TO BS 500D LBL 18 WL 157 ITEM # 7535311 IAW 53-00-53-1A-2; SRM 51-10-02-0G-0; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG# 143A7500 57319U 02-APR21

ATA 5320

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL157. / REMOVED DAMAGED FLOOR TO SIDEWALL SUPPORT AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT BS 500A-500D RBL23 WL157 IAW SRM 51-40-02-0G-0 AND DWG 143A7500; 143A7501

ATA 5210

AFT ENTRY DOOR HINGE ACCESS PANEL HAS A BENT AT THE LOWER CORNER EDGE / AFT ENTRY DOOR HINGE ACCESS PANEL WAS REPLACED IAW SWA EA 21-152-01079 REV IR DATED 04/16/2021 & ATS ER 21-01652 REV. IR DATED 04/16/2021

ATA 5320

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS420 RBL23 WL157. / REMOVED FLOOR TO SIDEWALL SUPPORT AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT BS 400-420 RBL23 WL157 IAW SRM 51-40-02-0G-0 AND DWG 143A7500; 143A7501

ATA 5320

***CORROSION*** ON AFT SHIELD AT FWD CARGO BAY BS493 - BS500A RBL24 WL157. / REMOVED DAMAGED AFT SHIELD AND INSTALLED NEW AFT SHIELD BS 493 - 500A RBL WL 157 IAW SRM 51-40-02-0G-0 AND DWG 143A0080

ATA 5320

***CORROSION*** ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS440 - BS493 RBL28 WL157. / REMOVED AND REPLACED SUBTHRESHOLD WEB AT FCB BS 440 - BS 493 RBL 28 WL 157 PER BOEING DWG 143A8330; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0

ATA 5510

RH HORIZONTAL STAB RIB 5 (STAB STA 129.50) HAS CRACK ON 2ND STIFFENER AT LOWER EDGE / REMOVED THE DAMAGED PART AT RH HORIZ. STAB RIB 5 STAB STD 129.50 2ND STIFFENER AT LOWER EDGE AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4. 88920U 22MAR21

ATA 5312

AFT CARGO BAY FWD BULKHEAD PANEL 142NWB IS CRACKED / RECEIVED NEW AFT CARGO BAY FWD BULKHEAD PANEL 142NWB ITEM # 7253772. ACCOMPLISHED ON COSTUMER CARD # JPANEL-141-CLOSE 57319U 15APR21

ATA 5510

LT HORIZONTAL STAB RIB 3 (STAB STA 110.10) HAS CRACK ON 3RD STIFFENER; LOWER EDGE / REMOVED THE DAMAGED PART AT LT HORIZ. STAB RIB 3 STAB STA 110.10 3RD STIFFENER LOWER EDGE AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4 88920U 22MAR21

ATA 5610

GRAB BAR HANDLE ABOVE FO'S WIND SCREEN BROKE / R & R'D F/O'S GRAB BAR HANDLE REF. IPC 56-11-11-01 ITEM 195 PER SIP.

ATA 5753

L/H WING OUTBOARD AFT FLAP IS DELAMINATED AT INBOARD TRAILING EDGE 1.25' INBD LOWER EDGE. LENGTH = 3.25'; WIDTH = .50' MOD / C) INSPECTION COMPLIED WITH; ADDITIONAL DAMAGE OR DETERIORATION WAS FOUND. CONDITION HAS BEEN CORRECTED AS NOTED ON: NEW NRC: U293604 MECHANIC: 0 LEAD/SUPERVISOR/INSPECTOR: 0 ***************** COMPLIED WITH ******************* MOD TYPE: 7 NBR: 178923 REV: POS: 1

ATA 2612

WHEEL WELL FIRE LIGHT ILLUMINATED DURING CLIMB. COMPLIED WITH QRH AND LANDED AT NEAREST SUITABLE AIRPORT. LIGHT REILLUMINATED 2 MORE TIMES IN DESCENT AND THEN STAYED EXTINGUISHED. CFR FOUND NO HOT SPOTS. R & R M270 SENSING ELEMENT, IAW MM 26-18-02. OPERATIONS CHECK OK. R & R FIRE LOOP DETECTION UNIT, IAW M/M 26-10-01 RAR 81244 POS 1 P/N 35008-307 S/N OFF 1004 S/N ON 0696.

ATA 2612

WHEEL WELL FIRE LIGHT ILLUMINATED DURING CLIMB. COMPLIED WITH QRH AND LANDED AT NEAREST SUITABLE AIRPORT. LIGHT REILLUMINATED 2 MORE TIMES IN DESCENT AND THEN STAYED EXTINGUISHED. CFR FOUND NO HOT SPOTS. R & R M270 SENSING ELEMENT, IAW MM 26-18-02. OPERATIONS CHECK OK. R & R FIRE LOOP DETECTION UNIT, IAW M/M 26-10-01 RAR 81244 POS 1 P/N 35008-307 S/N OFF 1004 S/N ON 0696.

ATA 3350

LEFT EMERGENCY EXIT SIDEWALL LIGHT INOPERABLE. RELAMPED LEFT EMERGENCY EXIT SIDEWALL LIGHT, PER AMM 33-21-00.

ATA 5330

FUSELAGE SKIN DAMAGE AT BS 794.6 ABOVE STR 24L FOUND TO BE OUT OF LIMITS. REPAIRED SKIN PER SRM 53-00-01-2R-3 REPAIR 3.

ATA 5720

LEFT WING I/B UPPER TRAILING EDGE PANEL FWD. SEAL BRACKET CRACKED / REMOVED AND REPLACED LEFT WING I/B UPPER TRAILING EDGE PANEL FWD SEAL BRACKET PER AMM 20-50-11 AND SRM 51-40-02

ATA 3350

RH OVERWING EMERGENCY EXIT INTERIOR SIGN HAS BULBS BURNT OUT / RELAMPED RH OVERWING EMERGENCY EXIT INTERIOR SIGN AND PERFORMED A GOOD INSTALLATION TEST PER AMM 33-51-01-960-801

ATA 3350

AFT SERVICE DOOR SLIDE EMERGENCY LIGHT DOES NOT ILLUMINATE / RELAMPED AND PERFORMED A GOOD INSTALLATION TEST OF THE AFT SERVICE DOOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04-960-801

ATA 3350

AFT ENTRY DOOR SLIDE EMERGENCY LIGHT DOES NOT ILLUMINATE / RELAMPED AFT ENTRY DOOR SLIDE EMERGENCY LIGHT AND PERFORMED A GOOD INSTALLATION TEST PER AMM 33-51-960-801

ATA 3397

EMERGENCY EXIT SIGN ABOVE FWD SERVICE DOOR INOP. / REMOVED AND REPLACED CONNECTOR D40042J WITH NEW CONNECTOR AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT SIGN ABOVE FWD SERVICE DOOR AS DOCUMENTED ON SA-M326 S/N A1292369

ATA 5514

LT HORIZONTAL STAB RIB AT STAB STA 129.50 4TH-FROM- FWD STIFFENER CRACKED / REPAIRED DAMAGE TO 4TH FROM FWD STIFFENER ON L/H HORIZ STAB INSPAR RIB AT STAB STA 129.50. IAW SRM 55-10-09-2R4 AND SRM 55-10-09-2R5

ATA 5514

LT HORIZONTAL STAB RIB AT STAB STA 129.50 2ND-FROM- FWD STIFFENER CRACKED / REPAIRED DAMAGE TO 2ND FROM FWD STIFFENER ON L/H HORIZ STAB INSPAR RIB AT STAB STA 129.50 IAW SRM 55-10-09-2R4 AND SRM 55-10-09-2R5

ATA 5514

LT HORIZONTAL STAB RIB AT STAB STA 129.50 3RD-FROM-FWD STIFFENER CRACKED / REPAIRED LT HORIZ. STAB RIB AT STAB STA 129.50 3RD STIFFENER IAW SRM 55-10-09-2R-4; DWG; 182A7401; DWG 182A1500; DWG 182A3001; DWG 002A0001; MM 27-31-41-400-801; SRM 55-10-09-7R-5 AND SOPM 20-50-01.

ATA 5320

FORWARD CARGO BAY BAFFLE CLIP IS CRACKED BS 500C LBL 21 WL 158 FWD SIDE OF FRAME / REMOVED CRACKED CLIP; LOCATED DRILLED & INSTALLED NEW CLIP PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 & DWG 143A7505

ATA 5320

FORWARD CARGO BAY BAFFLE CLIP IS CRACKED BS 500C LBL 21 WL 158 AFT SIDE OF FRAME / REMOVED CRACKED CLIP; LOCATED DRILLED & INSTALLED NEW CLIP PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 & DWG 143A7505

ATA 5320

***CORROSION*** FCB LH FLOOR-TO-SIDEWALL SUPPORT HAS CORROSION ON FASTENER HOLES; BS 500C-500D; LBL 21; WL 156 / CORROSION ON SIDEWALL SUPPORT FOUND OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES BS500C-500D; CUT & REMOVED BS480+10'-500D FABRICATED NEW PART FROM BAC 1496-444 M# 1428695-1; FABRICATED SPLICE @ BS 480+10' FROM BAC 1498-444 M1428895-1; LOCATED; DRILLED APPLIED CHEMICAL CONVERSION COATING PRIMED & INSTALLED PER SRM 53-00-53-2R-5; SRM 51-40-05-0G-0 SRM 51-40-02-0G-0; DWG 143A7501; DWG 143A9481

ATA 5320

BS 727A FRAME AT STR 4R STANDOFF DAMAGED / REPLACED STANDOFF AT BS 727A AT STR 4R PER SRM 51-40-02-0G-0 AND AIPC 53-11-00-10. 57449U 31MAR20

ATA 5320

***CORROSION*** CORROSION ON WEB UPPER SURFACE AT BS 260-270; LBL 0; WL 208 / REMOVED AND REPLACED CHANNEL SUPPORT BS 259-270 LBL 3-RBL3 WL 207.5 I.A.W BOEING DWG 141A5210 AND SRM 51-40-02-0G-0

ATA 5320

***CORROSION*** CORROSION ON UPPER SURFACE OF WEB AT BS 344-351.2 STRINGER 23L WL 166 / REMOVED AND REPLACED WEB AT B.S 314-360; S-23L; WL 166 IAW SRM 51-40-02-0G-0 AND DWG 141A8131

ATA 5320

***CORROSION*** CORROSION ON UPPER SURFACE OF WEB AT BS 330- BS 344 STRINGER 23L WL 166 / REMOVED AND REPLACED WEB AT BS 344-330; S-23L; WL 166 IAW SRM 51-40-02-0G-0 AND DWG 141A8131

ATA 5320

***CORROSION*** CORROSION ON UPPER SURFACE OF WEB AT BS 320- BS 325 STRINGER 23L WL 166 / REMOVED AND REPLACED WEB AT B.S 328-312; S-23L; WL 166 IAW SRM 51-40-02-0G-0 AND DWG 141A8131

ATA 5753

WIGGLE PLATE AT I/B SIDE OF RIGHT WING TRAILING EDGE PANEL (651GB) HAS PULLED FASTENER S / REMOVED AND REPLACED WIGGLE PLATE AT I/B SIDE OF RIGHT WING TRAILING EDGE PANEL 651GB; IAW SRM 51-40-02-0G-0. 84036U; 25MAR20.

ATA 5320

(SKYLINE DTIP) PREVIOUS REPAIR AFT CARGO BAY FLOOR SUPPORT; STA 787-856; RBL 14; CORROSION REPAIRED / UPON FURTHER INVESTIGATION NO REPAIR AT NOTED LOCATION

ATA 5320

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; L.B.L. 14; W.L. 207.45 / ACCOMPLISHED FLIGHT DECK FLOOR REPAIR IAW EA 1-A53-33179

ATA 3241

DECLARED EMERGENCY-------------------------------------------------------ANTI-SKID INOP LIGHT CAME ON DURING THE DESCENT INTO KSAN AND REMAINED ON THROUGH LANDING INTO KSAN. / R&R #3 ANTI SKID VALVE IAW AMM.

ATA 3350

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M668 IN CABIN. R&R BATTERY PER AMM.

ATA 3234

WHILE ON FINIAL LANDING GEAR DOWN HAD A LANDING GEAR POSITION DISAGREE WITH THE LANDING GEAR LEVER POSITION. MADE A GO AROUND. FOLLOWED THE QRH AND LANDING GEAR POSITION WAS NORMAL. R&R THE LANDING GEAR CONTROL LEVER MODULE IAW AMM.

ATA 3230

SELECTED GEAR DOWN FLAPS GEAR WARNING HORN SOUNDED AND ALL THREE RED GEAR UNSAFE LIGHTS ILLUMINATED WITH ALL THREE GREEN GEAR SAFE LIGHTS ILLUMINATE. RECYCLE GEAR, RED WARNING LIGHTS EXTINGUISHED AND HORN SILENCED. ADJUSTED LANDING GEAR CONTROL HANDLE REFLEX CABLE IAW MM.

ATA 5320

ACB FORWARD SCUFF PLATE IS BROKE / ACB FORWARD SCUFF PLATE REMOVED AND REPLACED IN ACCORDANCE WITH AMM TASK 53-11-02-020-801 AND AMM TASK 53-11-02-420-801. 59351U 02MAY19

ATA 3397

RT FORWARD OVER DOOR EXIT SIGN INOP. RESEATED CONNECTOR D40042P PER SWPM & AMM.

ATA 3350

EMERGENCY EXIT LIGHTING BATTERY PACK INOP (M1674). R&R LIGHT ASSEMBLY IAW AMM.

ATA 3350

LT OVERWING GROUND PROXIMITY EXIT LIGHTS HAD 2 BURNED BULBS. R&R BULBS PER AMM.

ATA 3350

R2 DOOR EMERGENCY LIGHT LENS COMMON TO G4 CRACKED. R&R LENS IAW AMM.

ATA 5320

AFT CARGO THRESHOLD ANGLE SUPPORT FOR/UNDER AFT SHIELD CORRODED BETWEEN BS. 847 TO BS. 857, RBL 22. R&R SHIELD IAW SRM AND DWG.

ATA 5320

AFT CARGO BAY THRESHOLD-SUPPORT INTERCOSTAL UNDER AFT SHIELD CORRODED BETWEEN BS. 847 TO BS. 855, RBL 23. R&R INTERCOSTAL IAW SRM AND DWG.

ATA 5320

AFT CARGO BAY AFT SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 22. R&R SHIELD IAW SRM AND DWG.

ATA 5320

AFT CARGO BAY LOWER THRESHOLD AFT SIDE INTERCOSTAL CORRODED BETWEEN BS. 847 TO BS. 855, RBL 20. R&R INTERCOSTAL IAW SRM & DWG.

ATA 5310

AFT CARGO BAY LOWER THRESHOLD VERTICAL BEAM CRACKED BETWEEN BS. 794 TO BS. 847, RBL 20. R&R BEAM IAW SRM AND DWG.

ATA 5311

AFT CARGO BAY FRAME CORRODED AT BS. 787+7, RBL 16. REPAIRED FRAME IAW ER AND EA.

ATA 5311

FRAME TAPERED STRAP CORRODED AT BS. 794, RBL 16. R&R TAPERED STRAP PER SRM AND DWG.

ATA 5320

T BRACKET COMMON TO INNER SURFACE OF LOWER FUSELAGE SKIN CORRODED AT BS. 1088, RBL 15. / R&R T BRACKET PER SRM AND DWG.

ATA 5320

AFT CARGO BAY FOUND INTERCOSTAL CRACKED BETWEEN BS. 927 TO BS. 947, RBL 22. / R&R INTERCOSTAL PER SRM AND DWG.

ATA 5330

EXTERNAL SKIN DAMAGED BETWEEN BS. 380 TO BS. 440, BETWEEN STR. 21R TO STR. 22R. REPAIRED SKIN PER EA AND ER.

ATA 5320

FORWARD CARGO BAY INTERCOSTAL UNDER SHIELD CORRODED BETWEEN BS. 500 TO BS. 500A, STR. 26R. R&R INTERCOSTAL PER SRM AND DWG.

ATA 5330

FUSELAGE SKIN DENT AT STA 1064+21' S-25R (REF:8353403) AND STA 1064+16 S-25R (REF:8353 404) REQUIRES A PERMANENT REPAIR PER CARD# J9987755 / THE DENT DAMAGE HAS BEEN TRIMMED OUT. UPON DAMAGE REMOVAL; S-25R (P/N 148A3370-14) WAS FOUND WITH DENT DAMAGE AS WELL. AN EXTERNAL REPAIR WAS INSTALLED PER EA 1-753-34703 REV IR (ATS ER 19-02537 REV IR)

ATA 5755

#3 SPOILER HAS 1 EACH AREA DISBONDED; LOCATION IS AS FOLLOWS; 11.5IN INBOARD OF OUTBOARD EDGE 8 IN FROM T/E / REPAIRED DISBONDED AREA ON #3 SPOILER AT 11.5' I/B OF O/B EDGE; 8' FROM T/E PER SRM 51-70-10-2R-2 AND SRM 51-70-10-2R-0.

ATA 5755

#3 SPOILER HAS 1 EACH AREA DISBONDED; LOCATION IS AS FOLLOWS; 12IN INBOARD OF OUTBOARD EDGE 18 IN FROM T/E / REPAIRED DISBONDED AREA ON #3 SPOILER AT 12' I/B OF O/B EDGE; 18' FROM T/E PER SRM 51-70-10-2R-2 AND SRM 51-70-10-2R-0.

ATA 5755

DENT FOUND WITH DISBOND ON #9 SPOILER UPPER SURFACE AREA MARKED / REPAIRED DISBONDED DENT ON #9 SPOILER UPPER SURFACE AREA PER SRM 51-70-10-2R-2 AND SRM 51-70-10-2R-0.

ATA 5320

INTERCOSTAL SPLICE CORRODED AT BS. 967, STR. 21R. / R&R INTERCOSTAL SPLICE PER SRM AND DWG.

ATA 5320

AFT CARGO BAY 1016 Y CHORD SPLICE CORRODED AT BS. 1016, BETWEEN STR. 26L TO STR. 26R. / R&R Y CHORD IAW SRM AND DWG.

ATA 5311

FRAME SPLICE CORRODED AT BS. 967, BETWEEN STR. 24R TO STR. 25R. R&R FRAME SPLICE IAW SRM AND DWG.

ATA 5320

L1 DOOR Z ANGLE CORRODED AT BS 328, LBL 65. R&R "Z" ANGLE IAW SRM AND DWG.

ATA 5321

CABIN FLOOR PANEL 241DF IS DELAMINATED ON TOP FACE (MARKED) / DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 241DF; FABRICATED NEW PANEL FROM BMS 4-23 T2 LOT# 332553/1 AND INSTALLED ALL INSERTS WITH RESIN USING BMS 5-107 LOT# AK8KD4895K AND PART MARKED IAW SRM 53-00-50-2R-0 PAR 1 NOTE & DWG 144A5810-9. 59401U 21MAR19.

ATA 5321

CABIN FLOOR PANEL 241EF IS DELAMINATED ON TOP FACE (MARKED) / DUE TO EXTENT OF DAMAGE FABRICATED A REPLACEMENT FOR PANEL 241EF; IAW SRM 53-00-50-2R-0 AND BAC DWG# 144A5810-23. 59644U 3/21/19

ATA 5320

ACB FWD FLOOR PANEL FWD CAPSTRIP ASSY IS BROKEN / REMOVED AND REPLACED ACB FWD FLOOR PANEL FWD CAPSTRIP ASSY. IAW SOPM 20-50-01. 59396U 30APR19

ATA 5321

CABIN FLOOR PANEL 231FF IS DELAMINATING (MARKED) / DELAMINATION ON UPPER SURFACE EDGE CABIN FLOOR PANEL 231FF REPAIRED IAW SRM 53-00-50-2R-1 DWG# 143A5810- 28 59268U 3/21/19

ATA 5720

CRACK ON R/H WING TRAILING EDGE LOCATED ON STRUCTURE DIRECTLY ABOVE IB AND OB FLAP ROLLER SUPPORT ORSS 297 (MARKED) / REMOVED & REPLACED BEAM IAW SRM 51-40-02 & DWG. 115A2512; RH WING T.E. STRUCTURE DIRECTLY ABOVE I/B AND O/B OF FLAP ROLLER SUPPORT ORSS 297

ATA 5320

FLOOR TRACK CRACKED BS. 460 TO BS. 480, RBL 14 IN RADIUS OF FRAME ATTACH POINT. / R&R FLOOR TRACK SUPPORT IAW SRM AND DWG.

ATA 5320

AFT CARGO BAY THRESHOLD SUPPORT CORRODED AT BS. 787+7, RBL 16. / R&R SUPPORT IAW SRM AND DWG.

ATA 5320

***CORROSION*** ON ACB T SPLICE STA 767+4 RBL 20 LBL 20 WL 156 / REMOVED AND REPLACED ACB T SPLICE STA 767+4 RBL 20 LBL 20 WL 156 IAW SOPM 20-50-01 59563U 28APR19

ATA 5320

***CORROSION*** ON HORIZONTAL PRESSURE WEB SHEAR TIE AT B.S 667; L.B.L. 65-71; W.L. 200. / CORROSION ON HORIZONTAL PRESSURE WEB SHEAR TIE AT BS 667; LBL 65-71; WL 200 WAS REPAIRED IAW ATS ER 19-02468 REV IR DATED 17APR19 AND EA 1-753-34610 REV IR

ATA 5313

FORWARD CARGO BAY BILGE STRINGER CORRODED BETWEEN BS. 500C TO BS. 500D, RBL 14. REPAIRED STRINGER IAW SRM.

ATA 5347

FLOOR TRACK CRACKED AT BS. 727E, RBL 14. R&R FLOOR TRACK IAW SRM AND DWG.

ATA 5320

FORWARD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT CORRODED AT BS. 500D, RBL 24. / R&R SUPPORT IAW SRM AND DWG.

ATA 5320

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS. 787+7 TO BS. 847, RBL 22. R&R WEB PER SRM AND DWG.

ATA 5320

AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 767 TO BS. 787+7, RBL 22. R&R WEB PER SRM AND DWG.

ATA 5320

AFT CARGO BAY ON R/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 887+7 TO BS. 947, RBL 22. REPAIRED SUPPORT PER SRM AND DWG.

ATA 5320

FORWARD CARGO BAY BILGE INTERCOSTAL CORRODED BETWEEN BS. 500C TO BS. 500D, RBL 14. / R&R INTERCOSTAL PER SRM AND DWG.

ATA 5320

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 420 TO BS. 440, RBL 22. R&R SHIELD IAW SRM & DWG.

ATA 5320

AFT CARGO BAY ON L/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 847, LBL 22. R&R SUPPORT IAW SRM & DWG.

ATA 5320

AFT CARGO BAY ON R/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 767, RBL 22. R&R SUPPORT IAW DWG & SRM.

ATA 5320

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 500 TO BS. 500A, RBL 22. / R&R SHIELD PER SRM AND DWG.

ATA 5320

FLOOR TRACK CORRODED BETWEEN BS. 787 TO BS. 887, RBL 14. / R&R FLOOR TRACK IAW SRM AND DWG.

ATA 5312

HORIZONTAL PRESSURE WEB SHEAR TIE CORRODED AT BS. 667, RBL 71. / REPAIRED SHEAR TIE IAW ER AND EA.

ATA 5310

***CORROSION*** AT FWD PASSENGER CABIN ON RADIUS FILLER BS360 RBL43 WL208.1. / REMOVED AND REPLACED FWD PASSENGER CABIN RADIUS FILLER AT BS 360 RBL 43 WL 208.1 DUE TO NO ALLOWABLE LIMIT FOUND IN THE SRM FOR THIS ITEM IAW SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0

ATA 5320

FORWARD PASSENGER CABIN INTERCOSTAL CRACKED BETWEEN BS. 344 TO BS. 360, LBL 11. / R&R INTERCOSTAL PER SRM AND DWG.

ATA 5310

AFT CABIN WEB CORRODED AT BS. 986+3, RBL 40. R&R WEB PER SRM AND DWG.

ATA 5320

R1 DOOR MOP SILL CORRODED AT BS. 312, RBL 55. R&R MOPSILL PER SRM & DWG.

ATA 5320

INTERCOSTAL CRACKED BETWEEN BS. 344 TO BS. 360, LBL 1. R&R INTERCOSTAL PER SRM AND DWG.

ATA 5320

L2 DOOR MOP SILL CORRODED AT BS. 967, RBL 52. / R&R MOPSILL PER DWG AND SRM.

ATA 5320

R2 DOOR MOP SILL CORRODED AT BS. 967, LBL 52. / R&R MOPSILL PER SRM AND DWG.

ATA 5320

AFT CABIN WEB CORRODED AT BS. 1016+11, LBL 6. R&R WEB PER DWG AND SRM.

ATA 5315

FORWARD PASSENGER CABIN ON FLOORBEAM CORRODED AT BS. 328, RBL 55. REPAIRED FLOORBEAM IAW ER AND EA.

ATA 5315

AFT CABIN FLOORBEAM CORRODED AT BS. 986, BETWEEN LBL 44 TO RBL 44. REPAIRED FLOORBEAM IAW ATS ER AND EA.

ATA 5311

FRAME CRACKED AT BS. 312, STR. 5L. / REPAIRED FRAME IAW ER AND EA.

ATA 5340

FORWARD PASSENGER CABIN ON GIRT BAR FITTING ATTACH POINT CORRODED AT BS. 312, LBL 55. / R&R ATTACH POINT IAW SRM.

ATA 5340

FORWARD PASSENGER CABIN ON GIRT BAR FITTING ATTACH POINT CORRODED AT BS. 344, LBL 59. / R&R ATTACH POINT IAW SRM.

ATA 5320

AFT CABIN INTERCOSTAL CORRODED BETWEEN BS 967 TO BS 986, RBL 16. R&R FLOOR PANEL SUPPORT PER SRM AND DWG.

ATA 5320

L1 DOOR MOPSILL CORRODED AT BS 328, LBL 58. R&R MOPSILL IAW SRM AND DWG.

ATA 5320

AFT CABIN INTERCOSTAL CORRODED BETWEEN BS. 967 TO BS. 947, RBL 45. / R&R SUPPORT PER SRM AND DWG.

ATA 5320

FORWARD PASSENGER CABIN ON ENTRY DOOR SCUFF PLATE SUPPORT CORRODED AT BS 328, LBL 62. R&R SUPPORT IAW SRM AND DWG.

ATA 5320

***CORROSION*** ON TENSION STRAP AT AFT CABIN BS1016+11 LBL3 WL208. / REMOVED AND REPLACED TENSION STRAP AT AFT CABIN BS 1016+11 LBL 3 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 147A5600 59205U 03APR19

ATA 5320

FCB FWD FLOOR TIE DOWN STRAP IS BROKEN / FABRICATED NEW FCB FWD FLOOR TIE DOWN STRAP PER EA 1-753-34755 REV IR AND ER 19-02952 REV IR.

ATA 5320

FORWARD CABIN INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 46. R&R INTERCOSTAL IAW SRM & DWG.

ATA 5320

FORWARD CABIN INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

ATA 5320

FORWARD CABIN INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

ATA 5320

FORWARD PASSENGER CABIN INTERCOSTAL CRACKED AT BS 312+6, RBL 31. R&R INTERCOSTAL IAW SRM AND DWG.

ATA 5312

HORIZONTAL PRESSURE WEB AROUND THE STIFFENING BEAD CRACKED AT BS 665, RBL 40. REPAIRED HORIZONTAL PRESSURE WEB IAW SRM.

ATA 5321

AFT FLOOR PANEL 241YF UPPER SKIN HAS AN AREA OF PULLED STRANDS ON AFT END. / REPAIRED AREA OF PULLED STRANDS ON AFT END ON AFT FLOOR PANEL 241YF IAW SRM 53-00-50-2R-1 59278U 3/13/19

ATA 5321

FWD FLOOR PANEL 222G (AFT) UPPER SKIN HAS AREAS OF PULLED STRANDS. / REPAIRED UPPER SKIN AREAS OF PULLED STRANDS ON FWD FLOOR PANEL 222G IAW SRM 53-00-50-2R-1 AND DWG 141A5810-144 7062U 3-16-19

ATA 5321

FWD FLOOR PANEL 221CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD FLOOR PANEL 221CF WITH UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1 AND DWG 141A5810-250. 57543C 14MAR19.

ATA 5321

FORWARD FLOOR PANEL 222CF (FORWARD) LOWER INBOARD EDGE DELAMINATED. REPAIRED PANEL IAW SRM. (BETWEEN BS. 270 TO BS. 420)

ATA 5711

***CORROSION*** ON AILERON BALANCE WEIGHTS AT RIGHT WING REAR SPAR ORSS532. MARKED / REMOVED AND REPLACED; WITH SERVICABLE PART; RT AILERON I/B BALANCE PANEL I/B WEIGHT AT ORSS532 IAW SOPM 20-50-01 & AMM 20-50-11-910-801 TABLE 208. PERFORMED 10X VISUAL INSPECTION IAW SRM 51-10-02-0G-0. NO FURTHER DAMAGE NOTED. 7641U 05APR19

ATA 5720

WS 253 #1 ENG PYLON TIP FAIRING BULB SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED WS 253 #1 ENG PYLON FAIRING - BULB SEAL RETAINER P/N 115A2953-1 IAW. AIPC 57-50-00-25 AND SRM 51-40-02 R.O. 88920U 19APR19

ATA 5720

LH DEFLECTION PANEL ATTACH ANGLE IS CRACKED; ATTACHED TO TRANSVERSE WEB. / REMOVED & REPLACED ANGLE IAW SRM 51-40-02 & IPC 57-42-51-02; LH WING DEFLECTION PANEL ANGLE ATTACHED TO TRANSVERSE WEB

ATA 5720

RH WING LEADING EDGE PANEL 621DB FWD I/B CORNER IS DELAMENATED / REPAIRED DELAMINATION DAMAGE TO FWD I/B CORNER ON RH WING LEADING EDGE PANEL 621DB IAW SRM 51-70-05-2R-6. 59049U 03/10/19

ATA 5720

RH WING LEADING EDGE PANEL 621HB FWD I/B CORNER IS DELAMENATED / RH WING LEADING EDGE PANEL 621HB DELAMINATED CORNER WAS REPAIRED IAW SRM 51-70-05-2R-6

ATA 5754

RT WING NR 8 SLAT NOSE SKIN AT ACTUATOR RIB CRACKED. REPAIRED SKIN IAW SRM.

ATA 5754

L/H WING #2 SLAT NOSE SKIN AT ACTUATOR RIB CRACKED. / REPAIRED SKIN IAW SRM.

ATA 2565

L1 DOOR EMERGENCY SLIDE LOWER END DISPLACED. REPOSITIONED SLIDE PER MT.

ATA 5753

LEFT WING OUTBOARD AFT FLAP; INBOARD TRAILING EDGE DISBONDED / REPAIRED PER SRM 51-70-10 REPAIR #1.

ATA 2565

R1 DOOR ESCAPE SLIDE SKIRT TORN. R&R SLIDE IAW MT.

ATA 3350

LT OVERWING EXIT LIGHT DIM. RELAMPED WINDOW LIGHT PER MM.

ATA 5330

FWD CARGO SCUFF PLATE HAS A CRACK IN IT / R&R FWD CARGO SCUFF PLATE PER AMM 53-11-02

ATA 5524

LEFT ELEVATOR BALANCE BAY #4 FWD BALANCE PANEL (183A9130Y7) IS CRACKED / R&R LEFT ELEVATOR BALANCE BAY #4 BALANCE PANEL 183A9130Y7 AND FWD BALANCE BAY CURTAIN PER AMM 27-31-41.

ATA 3350

BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER MM AND DWG.

ATA 3350

BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PER MM AND DWG.

ATA 2560

AFT FLASHLIGHT HOLDER ASSEMBLY BROKEN. R & R THE STRAP PER MM.

ATA 5743

LEFT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE FITTING IAW EA.

ATA 5743

RIGHT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE FITTING IAW EA.

ATA 5743

RIGHT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE TRUNNION FITTING IAW EA.

ATA 3350

FORWARD ENTRY EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

ATA 3350

R1 DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

ATA 3350

RIGHT EMERGENCY LIGHT INOPERATIVE AT ROW 6. R & R THE BATTERY PACK IAW AMM.

ATA 3350

AFT LEFT WING EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

ATA 5312

BULKHEAD CRACKED AT BS 663. REPAIRED THE BULKHEAD IAW SRM.

ATA 5312

RIGHT BS 663 BULKHEAD WEB CRACKED. REPAIRED THE BULKHEAD WEB IAW SRM AND DWG.

ATA 5320

MAIN WHEEL WELL FORWARD BULKHEAD STIFFENER CRACKED AT BS 663, LBL 26. R&R STIFFENER PER SRM.

ATA 5320

MAIN WHEEL WELL FORWARD BULKHEAD STIFFENER CRACKED AT BS 663, RBL 26. R&R STIFFENER PER SRM.

ATA 5753

RT WING OUTBOARD MAIN FLAP DELAMINATED. REPAIRED MAIN FLAP PER EA.

ATA 2560

R2 DOOR SLIDE AFT GIRT BAR FLOOR BRACKET ADAPTER PLATE DAMAGED. R & R THE PLATE IAW AMM.

ATA 5312

FORWARD SIDE OF BULKHEAD ANGLE CRACKED AT BS 663, RBL 9. REPAIRED ANGLE IAW ER & EA.

ATA 5330

DOUBLER CRACKED AT BS 520, AFT OF RAM AIR DOOR GROUND STUD BRACKET. REPAIRED THE DOUBLER IAW EA AND ER.

ATA 5311

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

ATA 5311

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

ATA 5312

RT WHEEL WELL BULKHEAD VAPOR BARRIER CORRODED AT BS 663, RBL 12. REPAIRED BARRIER IAW SRM.

ATA 5754

LEFT WING NR 1 LEADING EDGE SLAT LOWER NOSE SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED THE SKIN IAW SRM.

ATA 5312

VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 42.5. REPAIRED WEB PER SRM.

ATA 5320

L1 DOOR FRAME REVEAL ANGLE CRACKED ON THE UPPER SIDE OF UPPER PRESSURE FLAP CONTACT AREA. R & R THE ANGLE IAW SRM.

ATA 3350

AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT LOOSE. R & R THE LIGHT IAW AMM.

ATA 3350

AFT GALLEY EMERGENCY EXIT CEILING SIGN LOOSE. R & R THE SIGN IAW SIP.

ATA 3297

UPON LANDING GEAR LEVER DOWN GOT 3 GREEN. 3 RED LANDING GEAR LIGHTS WITH BRIEF WARNING HORN. CYCLED GEAR GOT 3 GREEN LIGHTS. CLEANED CONNECTOR IAW AMM.

ATA 2565

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

ATA 2824

FUEL CROSS FEED VLV CB POPPED DURING CRUISE. R & R FUEL CROSS FEED VLV IAW MM.

ATA 2560

L1 DOOR EMER EVAC SLIDE GIRT BAR SUPPORT HOLDER LOOSE. SECURED HOLDER IAW SIP.

ATA 3350

EMERGENCY LIGHTS BATTERY FAILED CAPACITY CHECK AT LOCATION M1675. R & R BATTERY PACK IAW MM.

ATA 5320

MAIN CABIN KEPT ANGLE 3RD FASTENER HOLE FROM TOP CRACKED AT BS 727B, RBL 45.5. R & R ANGLE IAW SRM.

ATA 5320

LEFT SIDE UPPER AFT FASTENER DRAG LINK CRACKED AT BS 540. REPAIRED DRAG LINK IAW EA.

ATA 5347

MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, LBL 23.75, HOLE D. REPAIRED SEAT TRACK IAW EA.

ATA 5347

MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, LBL 23.75, HOLE D. REPAIRED SEAT TRACK IAW EA.

ATA 5347

MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, LBL 25.75, HOLE D. REPAIRED SEAT TRACK IAW EA.

ATA 5347

MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 46.5, BOTTOM OF HOLE ON FWD SIDE. REPAIRED SEAT TRACK IAW EA.

ATA 5347

MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, LBL 46.5, HOLE D. REPAIRED SEAT TRACK IAW EA.

ATA 5320

FLOORBEAM AFT BATHTUB FITTING CRACKED AT BS 727B, LBL 25. R & R FITTING IAW SRM.

ATA 5347

MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, LBL 44.5, HOLE D. REPAIRED SEAT TRACK IAW EA.

ATA 5320

BELLY ACCESS PANEL T CHORD CORRODED AT BS 727, BETWEEN LBL 23 TO RBL 23. R & R T CHORD IAW SRM.

ATA 5320

FLOORBEAM AFT BATHTUB FITTING CRACKED AT BS 727B, RBL 25. R & R FITTING IAW SRM.

ATA 5347

MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, LBL 46.5, HOLE D. REPAIRED SEAT TRACK IAW EA.

ATA 5320

FLOORBEAM AFT BATHTUB FITTING CRACKED AT BS 727B, LBL 45. R & R FITTING IAW SRM.

ATA 5320

LEFT SIDE UPPER FWD FASTENER IN DRAG LINK CRACKED AT BS 540. REPAIRED DRAG LINK IAW EA.

ATA 5347

AFT SEAT TRACK HOLE CRACKED AT BS 727B, RBL 25, IN THE HOLE ON THE OTBD FLANGE. REPAIRED SEAT TRACK IAW EA.

ATA 5320

KEPT ANGLE CRACKED AT BS 727B, LBL 25. R & R ANGLE IAW SRM.

ATA 5310

RIGHT NR 1 WINDOW FRAME CRACKED INSIDE THE RADIUS. REPAIRED FRAME IAW EA.

ATA 5330

RIGHT NR 3 WINDOW FRAME E - F POST CRACKED, SECOND FROM THE BOTTOM HOLE. REPAIRED POST IAW EA.

ATA 5330

LEFT NR 3 WINDOW FRAME E - F POST CRACKED, SECOND FROM THE BOTTOM HOLE. REPAIRED POST IAW EA.

ATA 5330

LEFT SKIN LOWER BULKHEAD CHORD CRACKED AT BS 540, UPPER HOLE 2ND FROM THE TOP. REPAIRED CHORD IAW EA.

ATA 5330

LEFT SKIN LOWER BULKHEAD CHORD CRACKED AT BS 540, AT B HOLE. REPAIRED SKIN IAW EA.

ATA 3350

RIGHT OVERWING EMER EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.

ATA 3350

OVERHEAD CTR EXIT SIGN LIGHT BROKEN. R & R LIGHT IAW MM.

ATA 3350

LEFT EMER BULLNOSE LIGHT INOPERATIVE AT ROW 1. REPAIRED LIGHT IAW MM.

ATA 3350

LEFT OVERWING EMER EXIT BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

ATA 3350

RT LOWER EMERGENCY EXIT SIGN LENS MISSING AT ROW 11. INSTALLED LENS IAW SIP.

ATA 3350

RT OVERWING EMERGENCY SIGN LIGHT INOPERATIVE. RELAMPED SIGN IAW MM.

ATA 3350

L2 DOOR LOWER EMERGENCY LIGHT BULB INOP. RELAMPED LIGHT PER AMM.

ATA 5512

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR BETWEEN STAB STA 96 TO STA 99. REPAIRED SKIN IAW CCO.

ATA 5511

LEFT HORIZONTAL STABILIZER RIB AT STAB STA 129.5 CRACKED O/B FLANGE 7.5" AFT OF FWD SPAR. REPAIRED RIB IAW EA.

ATA 5511

LEFT HORIZONTAL STABILIZER RIB AT STAB STA 92.7 CRACKED AT NR 2 STIFFENER. REPAIRED RIB PER SRM.

ATA 3350

CENTER OVERWING EMERGENCY EXIT CEILING LIGHT HOUSING BROKEN. REMOVED AND REPLACED LIGHT HOUSING IAW AMM.

ATA 5311

FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME IAW EA.

ATA 5311

FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA.

ATA 5311

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

ATA 5311

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

ATA 5311

FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME IAW EA.

ATA 5311

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

ATA 5330

EXTERNAL POWER DOOR CUTOUT CRACKED AT AFT EDGE. REMOVED & REPAIRED CUTOUT IAW SRM.

ATA 5730

RIGHT WING PANEL 643AB DELAMINATED AT LOWER L/E SKIN. REPAIRED PANEL PER ATS ER.

ATA 5311

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

ATA 5311

FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER EA.

ATA 5311

FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER EA.

ATA 5311

FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME IAW EA.

ATA 5311

FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.

ATA 5320

LONGITUDINAL FLOORBEAM SPLICE CRACKED AT BS 727B, RBL 46. REPAIRED SPLICE IAW ER AND EA.

ATA 5311

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

ATA 5311

FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER EA.

ATA 5311

FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME IAW EA.

ATA 5534

VERTICAL STABILIZER FITTING ASSY FOR CROSSMEMBER CRACKED AT BS 1016. REMOVED AND REPLACED FITTING ASSY IAW SRM.

ATA 5523

RIGHT ELEVATOR TAB DELAMINATED ON UPPER O/B SURFACE. REMOVED AND REPLACED TAB IAW SRM.

ATA 5540

RUDDER WEIGHT AREAS CORRODED. REMOVED AND REPLACED WEIGHT PER MM.

ATA 5311

FRAME CRACKED AT STA 295, RBL 56. REPAIRED FRAME IAW ER AND EA.

ATA 5320

INTERCOSTAL CRACKED AT STA 303, RBL 13. REPAIRED INTERCOSTAL IAW SRM.

ATA 5320

INTERCOSTAL CORRODED BETWEEN STA 847 TO STA 857, RBL 22. REPAIRED INTERCOSTAL IAW SRM.

ATA 5320

BRACKET CRACKED AT BS 500A, STR 24L. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

ATA 5320

BRACKET PUNCTURED AT STA 500A, STR 24L. REMOVED AND REPLACED BRACKET IAW SRM & DWG.

ATA 5347

AFT CARGO CARGO TIE DOWN TRACK CORRODED AT BS 943, LBL 10. REMOVED AND REPLACED TRACK PER SRM.

ATA 5321

PASSENGER CABIN FLOOR 221GF BROKEN O/B FORWARD CORNER. REPAIRED PANEL IAW SRM.

ATA 5321

PASSENGER CABIN FLOOR 222CF BROKEN INSERTS. REPAIRED PANEL IAW SRM.

ATA 5321

PASSENGER CABIN FLOOR 221BF BROKEN INSERTS. REPAIRED PANEL 221BF IAW SRM.

ATA 5340

STRINGER CLIP CORRODED AT BS 727D, STR 24L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

ATA 5340

STRINGER CLIP CORRODED AT BS 727D, STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

ATA 5320

SUPPORT BRACKET CRACKED AT BS 727, RBL 8. REMOVED & REPLACED BRACKET PER DWG & SRM.

ATA 5321

PASSENGER CABIN FLOOR 221CF INSERTS BROKEN. REPAIRED FLOOR IAW SRM.

ATA 5720

LEFT WING UPPER AFT FIXED T/E PANEL SUPPORT CRACKED ABOVE NR 1 PYLON AFT TIP. REMOVED AND REPLACED PANEL IAW SRM.

ATA 2750

RIGHT WING I/B MAIN FLAP I/B AND O/B AFT FLAP BELL CRANKS CHAFED AT CLEVIS ATTACH POINTS. REPAIRED BELL CRANKS IAW EA.

ATA 5511

RIGHT HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 92.70 CRACKED AT THE LOWER END OF THE 3 FWD VERTICAL STIFFENERS. REPAIRED RIB IAW SRM.

ATA 5312

BULKHEAD SUPPORT BRACKET CORRODED AT BS 947.5, LBL 8. REMOVED AND REPLACED BRACKET IAW SRM & DWG.

ATA 5312

BULKHEAD FITTING CORRODED AT BS 1016, STR 21L. REMOVED AND REPLACED FITTING IAW ER & EA.

ATA 5320

STRAP CORRODED AT BS 947.5, LBL 8. REMOVED AND REPLACED STRAP IAW SRM.

ATA 5512

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT I/B SIDE OF RIB STAB STA 138.70. REPAIRED SKIN IAW CCO.

ATA 5512

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT I/B SIDE OF RIB STAB STA 147.9. REPAIRED SKIN IAW CCO.

ATA 5512

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT I/B SIDE OF RIB STAB STA 138.70. REPAIRED SKIN IAW CCO.

ATA 5512

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR STAB STA 142.75 TO STA 114.5. REPAIRED SKIN IAW CCO.

ATA 5240

R2 DOOR SLIDE COVER TRIM AFT END CAP MISSING. REMOVED AND REPLACED CAP IAW SRM.

ATA 5210

L2 DOOR EMERGENCY EVAC SLIDE COVER TRIM AFT END CAP MISSING. REMOVED AND REPLACED CAP IAW SRM.

ATA 2560

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR RETAINER LOOSE. REMOVED & REPLACED FASTENERS IAW SRM.

ATA 5610

CAPTAIN'S 1 WINDOW CASTING CRACKED AT UPPER CORNER MOD. REPAIRED CASTING IAW EA.

ATA 2121

ELECTRICAL SMELL NOTED IN CRUISE FLIGHT ROW 5, FWD GALLEY, & FLIGHT DECK SMELL NOT ACRID BUT NOT STRONG. REMOVED AND REPLACED RECIRCULATION FAN IAW MM.

ATA 5512

RIGHT HORIZ STAB LOWER IN-SPAR SKIN CRACKED AT STAB STA 157.1. REPAIRED SKIN PER SRM.

ATA 5512

LEFT HORIZ STAB LOWER IN-SPAR SKIN CRACKED AT STAB STA 157.1. REPAIRED SKIN PER SRM.

ATA 5512

RIGHT HORIZ LOWER IN-SPAR SKIN CRACKED AT STAB STA 111.1. REPAIRED SKIN PER SRM.

ATA 2565

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER M/M.

ATA 3350

RIGHT OVERWING EMERGENCY EXIT DOOR LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER AMM.

ATA 5753

DURING SCHEDULED 10Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED AT I/B LOWER CORNER. REMOVED AND REPLACED AFT FLAP IAW MM.

ATA 2560

DURING SCHEDULED 10Y CHECK FOUND, LT EMERGENCY EXIT ESCAPE HATCH LIFE LINE STRAP CORRODED. REMOVED AND REPLACED STRAP IAW MM.

ATA 5743

DURING SCHEDULED MV3 CHECK FOUND, LT MLG TRUNNION FITTING LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER EA.

ATA 5512

DURING SCHEDULED HC2 CHECK FOUND, LT HORIZONTAL STABILIZER CRACKED AT THE LOWER IN-SPAR SKIN AT STA 129.5. REPAIRED SKIN PER SRM.

ATA 3350

RT EMERGENCY EXIT LIGHT COVER MISSING AT ROW 11. INSTALLED COVER PER MM.

ATA 2710

AILERONS BINDING AT 30 DEGREE LEFT CONTROL WHEEL ON GROUND CYCLED TO FULL LEFT AILERON SEVERAL TIMES. FELT THE BIND AND A POP ON RETURN TO CENTER. REMOVED AND REPLACED CAM FOLLOWER BEARING ON AILERON FEEL AND CENTERING MECHANISM PER MM.

ATA 3350

EMERGENCY EXIT LIGHT CHARGER INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

ATA 5512

DURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER EA.

ATA 5755

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED NR 1 SPOILER PER MM.

ATA 5340

DURING SCHEDULED 8Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

ATA 5312

DURING SCHEDULED 8Y CHECK, FOUND FWD CARGO BAY BULKHEAD ANGLE CORRODED AT BS 500D, RBL 25. REPAIRED ANGLE PER SRM.

ATA 5311

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO BAY FRAME CORRODED AT BS 947, BETWEEN BL 0 TO RBL 9. REPAIRED FRAME PER SRM.

ATA 3350

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

ATA 5753

DURING SCHEDULED MV2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

ATA 5312

DURING SCHEDULED MV2 CHECK, FOUND BULKHEAD OIL CANNED AT BS 1016, STR 3L. REPAIRED PER SWA EA.

ATA 3350

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS PER MM.

ATA 3350

DURING SCHEDULED MV2 CHECK, FOUND EGRESS TRACK COVER MISSING AT SEAT 11 ABC. REPLACED COVER PER MM.

ATA 3222

AFTER LANDING RT NLG WHEEL CAME OFF, AXLE FAILURE. REMOVED AND REPLACED NLG INNER CYLINDER ASSY PER MM.

ATA 2565

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SIDE PER MM.

ATA 3350

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 15 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

ATA 3350

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

ATA 3350

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

ATA 3397

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT MID CABIN. FOUND LOOSE WIRE. SECURED LOOSE WIRE PER MM.

ATA 3350

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 20 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

ATA 5512

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 147.90 AND STA 157.10. REPAIRED SKIN PER SRM.

ATA 5512

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

ATA 5512

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147.90. REPAIRED SKIN PER SRM.

ATA 3350

DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

ATA 5610

FLIGHT DECK L2 WINDOW ARCING. REMOVED AND REPLACED WINDOW PER MM.

ATA 2560

DURING SCHEDULED BRDG CHECK, FOUND FWD OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

ATA 2560

DURING SCHEDULED BRDG CHECK, FOUND FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.