N763SW

Part: SLIDE — OUT OF ADJUST (ZN 800 DOOR) · airframe 79,926 hrs · 47,481 cycles

FWD SERVICE DOOR EMERGENCY EXIT SLIDE VISIABLE UNDER DOOR<[01] READJUSTED SLIDE IN CONTAINER PER 25-66-01

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 79,560 hrs · 47,265 cycles

EMX BATT PACK M01675 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01675 PER AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 79,560 hrs · 47,265 cycles

EMX BATT PACK M01668 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01668 PER AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 79,560 hrs · 47,265 cycles

EMX BATT PACK M01674 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01674 PER AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 79,560 hrs · 47,265 cycles

EMX BATT PACK M01673 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01673 PER AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 79,560 hrs · 47,265 cycles

EMX BATT PACK M01670 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01670 PER AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 79,560 hrs · 47,265 cycles

EMX BATT PACK M01672 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01672 PER AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 79,560 hrs · 47,265 cycles

EMX BATT PACK M01669 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01669 PER AMM 33-51-06

Part: GIRT BAR — OUT OF ADJUST (RT FWD DOOR) · airframe 76,739 hrs · 45,445 cycles

RT FOWARD DOOR-FOWARD SIDE GIRT BAR HOLDER HOLDSIT LOOSLY. GIRT BAR COULD FALL OUT. / [01] ADJUSTED FWD R/H SERVICE DOOR FWD GIRT BAR HOLDER PER S.I.P.. IT CAN HOLD GIRT BAR NOW.

Part: PANEL — DELAMINATED (NR 1 NACELLE) · airframe 76,293 hrs · 45,137 cycles

#1ENG PLYON PANEL 431ER IS DELAM'ED LOWER FWD PORTION OF THE PANEL / [01] REMOVED AND REPLACED #1 ENGINE FWD STRUT FAIRING PANEL 431ER PER AMM 54-53-02

Part: NONE — CRACKED (AFT CARGO BAY) · airframe 74,817 hrs · 44,183 cycles

AFT CARGO BAY R/H CAP STIP SPLICE PLATE CRACKED BS 767 / [01] INSTALLED NEW ACB RH CAPSTRIP SPLICE PLATE IAW AMM 25-52-10-400-801 STEP 3. F. (10);[02] INSPECTION COMPLETE

Part: NONE — INOPERATIVE · airframe 74,817 hrs · 44,183 cycles

AFT SERVICE DOOR EMERGENCY EXIT LOCATOR HAS 1 EA. LAMP INOP / [01] RELAMPED AFT SERVICE DOOR EXIT LOCATOR AND PERFORMED SATISFACTORY OPERATIONAL TEST PER AMM 33-51-01-960-801.;[02] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 1.

Part: TRACK — CRACKED (FWD CARGO BAY) · airframe 74,817 hrs · 44,183 cycles

CRACK FWD CARGO TRACK AT STA 460; RBL 14. / [01] REMOVED FWD CARGO TRACK BS 395 TO BS 500D RBL14 WL 156 IAW SRM 51-40-02.;[02] REMOVED TO FOM FLOOR SUPPORT BS 395 RBL AND LBL P/N 284A3603-116 IAW SRM 51-40-02;[03] REMOVED FWD CARGO TRACK BS 395 TO BS 500D RBL14 WL 156 IAW SRM 51-40-02;[04] CRACK ON FWD CARGO BAY TRACK BS 460 RBL 14 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4. B. (1);[05] LOCATED AND DRILLED NEW TIE DOWN TRACK IAW SRM 51-40-05 AND DWG 143A7500 REV: A;[06] OK TO INSTALL FWD CARGO TRACK ASSY 143A7501-10.;[07] VERIFIED CORRECTIVE ACTION 6.;[08] INSTALLED FWD CARGO NEW TRACK BS 395 TO BS 500D RBL 14 WL 156 IAW SRM 51-40-02 AND DWG 143A7500 REV:A.;;[09] UPDATED PART INSTALLED;[10] VERIFIED CORRECTIVE ACTION 8.;[11] INSTALLED FWD CARGO FLOOR SUPPORT BS 395 RBL 23 AND LBL 23 WL 156 P/N 284A3603-116 IAW SRM 51-40-02 AND DWG 284A0603 REV:A.;[12] CERTIFIED- INSTALLATION OF FWD CARGO FLOOR SUPPORT BS 395 RBL 23 AND LBL 23 WL 156 P/N 284A3603-116 IAW SRM 51-40-02 AND DWG 284A0603 REV:A. ITEM PREVIOUSLY REMOVED FOM CORRECTIVE ACTION# 2.;[13] VERIFIED CORRECTIVE ACTION 12. <BR><BR>FLOOR SUPPORT REINSTALLED;[14] MEASUREMENTS;[15] MEASUREMENT FIELDS;[16] VERIFIED ALL WORK ACCOMPLISHED.

Part: PANEL — DELAMINATED · airframe 74,817 hrs · 44,183 cycles

PANEL 193AR HAS DELAMINATION TO OUTER SKIN OVER CORE AREA (MARKED) / [01] IDENTIFIED PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 18. DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4A(6). REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05-2R-1 PER SRM 53-40-70-2R-1 PAR 4B(1).;[02] REMOVED DAMAGED SKIN PLIES ABOVE HONEYCOMB CORE; NO CORE DAMAGE NOTED; CLEANED; IAW SRM 51-70-05-2R-1 PAR 4A-B.;[03] VALIDATED APPLICABILITY OF REPAIR TO BE COMPLETED IAW SRM 51-70-05-2R-1.;[04] VERIFIED CORRECTIVE ACTION 1-3;[05] FABRICATED REPAIR PLIES OUT OF BMS 8-79 ST 120 LOT#1483750-1; BMS 8-79 ST 1581 LOT#1479026-1; AND BMS 5-129 GR5 LOT#1483858-1; INSTALLED; VACUUM BAGGED AND CHECKED FOR LEAKS USING PRESSURE GAGE ID:ATS2441 S/N:UNKNOWN IAW SRM 51-70-05-2R-1 PAR 4C-D.;[06] REPAIR CURED IAW SRM 51-70-05-2R-1 PARA 4 STEP E ; REF CAL TOOL HOT BONDER ID ATS8883 SN 15112530.;[07] VERIFIED CORRECTIVE ACTIONS 5 AND 6;[08] ACCOMPLISHED UT INSPECTION IAW D6-37239 PART 4; 51-00-02; NO DISBONDS. ATS2342 E650;[09] APPLIED BMS10-21 TYPE III CONDUCTIVE COATING ; CURED THEN TESTED GOOD IAW AMM 51-21-71-370-801 PARA 3 D STEPS 1-4 & 7 REF CAL TOOL MULTIMETER ID ATS1508 SN 32130497 .<BR>RESTORED THE FINISH IAW SRM 51-70-05-2R-1 PARA 4 STEP G & AMM 51-21-99-300-802 PARA 3 C (3) (A)-(F) .;[10] VERIFIED CORRECTIVE ACTION #9

Part: INTERCOSTAL — CORRODED (AFT CARGO BAY) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON INTERCOSTAL BS 847 TO 850 RBL 18 W/L 153 / [01] APPLICABILITY STATEMENT: ALLOWABLE DAMAGE IAW SRM 53-60-15-1A-1;[02] REMOVED WEB AT ACB BS 847 TO BS 855; RBL 18; IAW SRM 51-40-02-0G-0. REMOVED CORROSION AT WEB L-3'; W-2'; D-0.007'; FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1; PARA 4 (G);[03] USED TOOL CALIPER ID- ATS2502; S/N AT9335659; DUE 04/2022;[04] LOCATED AND DRILLED NEW WEB P/N 146A8123U4 PO # 771166; IAW SRM 5-40-05-0G-9; OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 4.;[06] INSTALLED NEW WEB AT ACB BS 847 TO BS 855.95 RBL 18 WL 153 IAW SRM 51-40-02 AND DWG :146A0081 ID:0001 REV:B AND DWG:146A8120 ID:0001 REV:E.;[07] VERIFIED COMPLETION OF STEP 1 AND CORRECTIVE ACTION 6.

Part: SKIN — CRACKED (R/H HORIZ. STAB.) · airframe 74,817 hrs · 44,183 cycles

RH HORIZONTAL STAB LWR SKIN CRACKED AT STAB STA 184.7; AFT END IB OF RIB; MARKED / [01] STRIPPED PAINT IN DISCREPANT AREA AT STAB STA 184.7 IN ROUGHLY A 2'X2' AREA PER AMM 51-21-11-150-801 PARA. 3D;[20] ' DAMAGE REPAIRED PER EA 22-155-00745. REPETITIVE INSPECTION PROGRAM DEFINED IN EA 22-155-00745-INSP.';[21] INSPECTION COMPLETE

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON FUSELAGE SKIN BETWEEN STA 886 - STA 888; STRINGER 25L. / [01] VERIFIED APPLICABILITY IAW SRM 53-00-01-1A-5;[15] AS PER EA 22-153-00763; THE DAMAGE IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.;[16] INSPECTION COMPLETE

Part: ATTACH ANGLE — CRACKED (AFT CARGO BAY) · airframe 74,817 hrs · 44,183 cycles

CRACK ON AFT CARGO WATER SERVICE TO STRINGER ATTACH ANGEL AT RBL 12 BS 907+8. / [01] RECEIVED A NEW STIFFENER P/N 147A7221-32 FROM STORES. REF: PO 855759. <BR>REMOVED CRACKED STIFFENER IAW SRM 51-40-02.;[02] LOCATED AND DRILLED NEW STIFFENER IAW SRM 51-40-05 AND DWG 147A7221. OK TO INSTALL.;[03] NO ALLOWABLE DAMAGE FOUND FOR THIS PART IN B737-700 SRM. REPAIR BY REPLACEMENT IAW SRM 51-10-02.;[04] VERIFIED CORRECTIVE ACTIONS 1-3. OK TO INSTALL;[05] ENTERED MEASUREMENTS.;[06] INSTALLED STIFFENER IAW SRM 51-40-02 AND DWG 147A7221 REV:-;[07] VERIFIED CORRECTIVE ACTION 6.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON UPPER FUSELAGE SKIN AT BS 1016+20 LBL 3; BS 1016+23 LBL 3; BS 1016+23 LBL 5. ACCESS FROM 323BL / [01] REMOVED 17 FASTENERS; B.S. 1016+20-B.S. 1016+24 STR 1- LBL 5.5 TO FACILITATE CORROSION REMOVAL PER SRM 51-40-02-0G-0.;[02] REMOVED CORROSION; B.S. 1016+20- B.S. 1016+24; STR 1-LBL 5.5 PER SRM 51-10-02-0G-0.;[03] VERIFIED CORRECTIVE ACTION #2;[04] ACCOMPLISHED UT INSPECTION IAW NDTM D6-37239 PART 4; 51-00-00 PROC 2. LOWEST THICKNESS READING IS .037; SEE GRID. ATS2341 E650;[05] FUSELAGE SKIN DOUBLER (PLATE) REPAIRED AND RESTORED ON EA 22-153-00735 REV: A BARCODE TTG8Q00B8YU1;[06] VERIFIED CORRECTIVE ACTION 5.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON UPPER FUSELAGE SKIN AT BS 1016+25 LBL 8; BS 1016+25 RBL 6; BS 1016+29 LBL 4; BS 1016+30 LBL 6. ACCESS FROM 232BL / [01] REMOVED CORROSION ON FUSELAGE CROWN SKIN; B.S. 1040+.5 TO B.S. 1064+13; STR2L TO STR2R PER SRM 51-10-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] ACCOMPLISHED UT INSPECTION IAW NDTM D6-37239 PART 4; 51-00-00 PROC 2; LOWEST REMAINING THICKNESS IS .059 ADJACENT TO .063. ATS2341 E650;[04] ADDITION TO ACTION 3; 'SEE GRID';[05] CERTIFY ACTION 4;[06] CORROSION REMOVAL REQUIRED BLENDING OVER 17 FASTENERS AND THEREFORE IS OUT OF LIMITS PER SRM 53-00-01-1A-1.;[07] VERIFIED CORRECTIVE ACTION 6.;[08] PERFORM NDI (UT) OF SKIN IS (ATTACHED GRIDS) ORIGINAL THICKNESS IS 0.080.;[09] UT THICKNESS TESTED BLENDED AREAS MARKED WITH 1/2' GRID PER 737NDT PART 4 51-00-00 PROCEDURE 2. FILLED OUT GRID MAP WITH ALL DIMENSIONS. LOWEST REMAINING THICKNESS AS FOLLOWS: <BR>BS 1064 LH .078'; BS 1064 RH .076; BS1064+3 .077'.<BR><BR>TOOL E650 ATS2341;[10] FUSELAGE SKIN CORROSION REPAIRED AND RESTORED ON EA 22-153-00760 REV: A BARCODE TTG8Q00B9J6P.;[11] VERIFIED CORRECTIVE ACTION 10.

Part: STUB FRAME — CRACKED (R1 DOOR) · airframe 74,817 hrs · 44,183 cycles

FWD SERVICE DOOR FWD UPPER STUB FRAME IS CRACKED / [01] ACCOMPLISHED LOCATED AND DRILLED IN TASK CARD TTG8Q00B0AYZ STEP 13.;[08] INSTALLED FWD UPPER STUB FRAME WITH 100% TEMPORARY FASTENERS AND SEALANT BMS 5-95 C20; SQUEEZE OUT AT 3/19/2021 09:20 UTC.;[09] VERIFIED CORRECTIVE ACTION 8;[10] INSTALLED 100% PERMANENT FASTENERS PER SRM 51-40-02 AND DWGS 141A8370 AND 141A8380.;[11] VERIFIED CORRECTIVE ACTION 8. 100% TEMP FASTENERS WERE INSTALLED. 19-MAR-2022 09:22 UTC.;[12] ADDED SPECIFIC TIME AND DATE WHEN TEMP FASTENERS WERE VERIFIED PRIOR TO SEALANT CURE TIME.;[13] VERIFIED INSTALLATION OF PERMANENT FASTENERS PER SRM 51-40-02 AND DWGS 141A8370 AND 141A8380; FOR CORRECTIVE ACTION 10.;[14] VERIFIED INSTALLATION OF PERMANENT FASTENERS PER SRM 51-40-02 AND DWGS 141A8370 AND 141A8380 VERIFIES CORRECTIVE ACTION ITEMS 10 AND 13.;[15] JOB COMPLETE;[16] INSTALLATION ONLY COMPLETE;[17] STEP 15 IS NOT ACCOMPLISHED;[18] FILLED AND LEVELED FOR SEAL CONTACT AND APPLIED TOPCOAT TO STUB FRAME IAW BOEING DRAWING # 141A8370 AND AMM CH 51-21-73.;[19] VERIFIED CORRECTIVE ACTION #18;[20] COMPLETE

Part: ATTACH ANGLE — CRACKED (AFT CARGO BAY) · airframe 74,817 hrs · 44,183 cycles

CRACK ON AFT CARGO WATER SERVICE TO STRINGER ATTACH ANGEL AT RBL 12 BS 907+12. / [01] RECEIVED A NEW STIFFENER P/N 147A7221-32 FROM STORES. REF: PO 855759. <BR>REMOVED CRACKED STIFFENER IAW SRM 51-40-02.;[02] LOCATED AND DRILLED NEW STIFFENER IAW SRM 51-40-05 AND DWG 147A7221. OK TO INSTALL.;[03] NO ALLOWABLE DAMAGE FOUND FOR THIS PART IN B737-700 SRM. REPAIR BY REPLACEMENT IAW SRM 51-10-02.;[04] VERIFIED CORRECTIVE ACTIONS 1-3. <BR><BR>OK TO INSTALL NEW PART.;[05] ENTERED MEASUREMENTS.;[06] INSTALLED STIFFENER IAW SRM 51-40-02 AND DWG 147A7221 REV:-;[07] VERIFIED CORRECTIVE ACTION 6.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 420+5; BS 440+14; BS 460+10; BS 460+10; BS 460+14; BS 500+10; BS 500+14; BS 500+18. / [01] REMOVED CORROSION FWD CARGO BAY TO SIDEWALL SUPPORT AT LBL 24 BS 420+5;TO BS 500+18;IAW SRM 51-10-02; PARAGRAPH 15;EVALUATED ALL REWORKED AREAS;THE DEPPEST AREA BS 420+5 LBL 24;DIMENSION L=1' X W=.8' X DEPTH=.9' ORIGINAL THICKNESS 0.040' REMAINING THICKNESS 0.031' ;FOUND TO BE DAMAGE OUT LIMITS IAW SRM 53-00-53-1A-2 ALLOWAB LE DAMAGE 2 FIG#103 DEATIL 'E' TOOL USED MICROMETER ID ATS499 S/N UNKNOWN DATE 2022.[04] FABRICATED REPLACEMENT FLOOR TO SIDEWALL SUPPORT USING ITEM: BAC1496-444#7075T62 LOT: 1479718-1 IAW SRM 51-40-05 SRM 51-40-02 SRM 51-40-08 AND DWG 143A7501 ID:0001 REV: B. FABRICATED FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR AT BS 500B +10 USING BAC1496-444#7075T62 LOT: 1479718-1 IAW SRM 53-00-53-2R-5 SECTION 4.D-H; SRM 51-40-08 AND 51-40-05.;[05] CERTIFIED CORRECTIVE ACTION #4. CORRECTED ENTRY- APPLICABLE REFERENCE FOR THIS REPAIR IS SRM 53-00-53-2R-6 REPAIR 6. REPAIR SPLICE LOCATED BETWEEN FRAMES. BS 500B +10'.;[06] VERIFIED APPLICABLE REFERENCE FOR THIS REPAIR IS SRM 53-00-53-2R-6 REPAIR 6. REPAIR SPLICE LOCATED BETWEEN FRAMES. STA 500B + 10'.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500A+2; BS 500A+7; BS 500A+12; BS 500A+16; BS 500B+6; BS 500B+10; BS 500B+14; BS 500B+18; BS 500C+1. CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500A+2 BS 500A+7 BS 500A+12 BS 500A+16 BS 500B+6 BS 500B+10 BS 500B+14 BS 500B+18 BS 500C+1. / [01] REMOVED CORROSION FROM FCB R/H FLOOR TO SIDEWALL SUPPORT BS 500A -500D <BR><BR>BS500A+2 MEASURED 1.3'L X 1.1'W AND 0.013'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2<BR><BR>BS500A+7 MEASURED 1.4'L X 0.9'W AND 0.003'DEEP ORIGINAL THICKNESS OF 0.040' FOUND IN LIMITS PER SRM 53-00-53-1A-2<BR><BR>BS500A+12 MEASURED 1.5'L X 0.9'W AND 0.008'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2BS500C+1 MEASURED 1.5'L X 0.7'W AND 0.006'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2[05] FABRICATED REPLACEMENT SIDEWALL SUPPORT FROM BAC1496-444#7075T6; LOT 1479718-1 IAW PL143A7501 ID: REV:H; DWG 143S7501 ID:003 REV:A; SRM 51-40-05; SRM 51-40-06; SRM 51-40-08 APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01 OK TO PRIME.

Part: GUSSET — CRACKED (FWD CARGO) · airframe 74,817 hrs · 44,183 cycles

CRACK ON FWD CARGO BAY GUSSET AT BS 500D R/H STRINGER 19. / [01] NO ALLOWABLE DAMAGE FOUND IN B737-700 SRM FOR A CRACK ON FWD CARGO BAY GUSSET AT BS 500D R/H STRINGER 19. REPAIR BY REPLACEMENT IAW SRM 51-10-02.;[02] RECEIVED NEW GUSSET ASSY P/N 143A9481-5 FROM STORES. REF PO 855495. REMOVED CRACKED GUSSET IAW SRM 51-40-02.;[03] LOCATED AND DRILLED ON FWD CARGO BAY GUSSET AT BS 500D R/H STRINGER 19 IAW SRM 51-40-05 AND DWG 143A7902 REV:E.;[04] VERIFIED CORRECTIVE ACTION 1-3. OK TO INSTALL NEW GUSSET;[05] INSTALLED ON FWD CARGO BAY NEW GUSSET AT BS 500D R/H STRINGER 19 P/N 143A9481-5;IAW SRM 51-40-02 AND DWG 143A7902 REV:E.;[06] VERIFIED CORRECTIVE ACTION 5.

Part: STRAP — CORRODED (FWD CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON FWD CARGO BAY DOOR CUTOUT AFT STRAP AT BS 480+13 JUST ABOVE R/H STRINGER 24.(MARKED) CORROSION ON FWD CARGO BAY DOOR CUTOUT AFT STRAP AT BS 480+13 JUST ABOVE R/H STRINGER 24. / [01] SRM 53-30-15-1A-1 HAS BEEN FOUND TO BE APPLICABLE FOR THIS EVALUATION.;[09] REMOVED EDGE BLEND DAMAGE IN AN AREA OF .85L X .11 PART IS 1.23' WIDE. IAW SRM 51-10-02 AND SRM 53-30-15-1A-1 FIG 103 (I) WITH LESS THEN 10% DAMAGE REMOVAL. BLEND IS FOUND TO BE (IN LIMITS) OK TO APPLY CHEMICAL CONVERSION COATING AND PRIME.;[10] FACE BLEND IN AREA OF 1' SQUARE JUST FWD OF EDGE DAMAGE REMOVAL. ORIGINAL THICKNESS IS .142 AND LOWEST IS .139. FACE BLEND FOUND TO BE (IN LIMITS)IAW SRM 53-30-15-1A-1;[11] VERIFIED CORRECTIVE ACTION #9 AND 10; ORIGINAL OUT OF LIMITS AREA WAS BLENDED ON AN EDGE TO REMOVE DAMAGE; SURFACE BLEND IS IN LIMITS;[12] CORRECTION TO LINE 2. MEASUREMENT 10 CHANGE TO 143A8206-10;[13] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01;[14] VERIFIED CORRECTIVE ACTION #13

Part: THRESHOLD WEB — CORRODED (FWD CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON FWD CARGO BAY DOOR THRESHOLD AT RBL 29 BS 460+12. / [01] SRM 53-30-15-1A-1 IS APPLICABLE<BR><BR>REMOVED CORROSION FROM FWD CARGO BAYI DOOR THRESHOLD WEB AT RBL29 BS460+12 N AREA OF 2.2'X1.2'X.005' ORIGINAL MATERIAL THICKNESS .045' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0 AND SRM 53-30-15-1A-1<BR><BR>DEPTH GAUGE<BR>ATS2677<BR>S/N UNKNOWN<BR>11/2022;[02] VERIFIED CORRECTIVE ACTION 1;[03] RECEIVED NEW WEB P/N: 654A0003-58 PO NUMBER: P2455495-1. LOCATED AND DRILL NEW WEB IAW SRM 51-40-02; SRM 51-40-05; SRM 51-40-08 AND DWG 143A8122 ID:0010 REV: -.;[04] RECEIVED NEW WEB P/N: 654A0003-58 PO NUMBER: P2455495-1. LOCATED AND DRILL NEW WEB IAW SRM 51-40-02; SRM 51-40-05; SRM 51-40-08 AND DWG 143A8122 ID:0010 REV: -.;[05] PART REQUIREMENT;[06] VERIFIED CORRECTIVE ACTIONS 3-5. ALL WORK ACCOMPLISHED.

Part: NONE — CORRODED (FWD CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON FWD CARGO BAY FWD DOOR SHIELD AT RBL 23 BS 420+7; BS 420+12; BS 420+19. / [01] REMOVED FWD DOOR SHIELD AT FCB RBL 23 BS420 - BS440. RECEIVED NEW SHIELD ASSY ITEM: 143A8126U21ATSMRO LOT: 1474950-1. LOCATED AND DRILLED NEW SHIELD IAW SRM 51-40-02; SRM 51-40-05; SRM 51-40-08 AND DWG 143A8126 ID:0002 REV: D;[02] RECEIVED NEW SHIELD ASSY ITEM: 143A8126U21ATSMRO LOT: 1474950-1. LOCATED AND DRILLED NEW SHIELD IAW SRM 51-40-02; SRM 51-40-05; SRM 51-40-08 AND DWG 143A8126 ID:0002 REV: D;[03] FWD CARGO BAY FWD SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM; PART TO BE REPAIRED BY REPLACEMENT. RECEIVED NEW SHIELD ASSY ITEM: 143A8126U21ATSMRO LOT: 1474950-1. LOCATED AND DRILLED NEW SHIELD IAW SRM 51-40-02; SRM 51-40-05; SRM 51-40-08 AND DWG 143A8126 ID:0002 REV: D. INSTALLATION ACCOMPLISHED ON CUST CARD TTG8Q004E57C;[04] UPDATED WORK ACCOMPLISHED;[05] VERIFIED CORRECTIVE ACTIONS 1-4. PART OUT OF LIMITS AND REPLACED.<BR><BR>REMOVAL AND INSTALLATION DOCUMENTED ON TTG8Q004E57C

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 74,817 hrs · 44,183 cycles

CRACK ON FWD CARGO BAY STRINGER AT BS 540 L/H STRINGER 26. / CRACK ON FCB STR 26 L/H BS 536 ; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103;[02] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 1.;[03] VERIFIED APPLICABILITY FOR STR 26 L/H IAW SRM 53-00-03-2R-1 FIG 205.;[04] REMOVED DAMAGE BY TRIMMING OUT STRINGER SECTION AT BS 500D+11' TO 536 STR 26L. IAW SRM 53-00-03-2R-1 PAR. 4. STEP A -B.;[05] VERIFIED CORRECTIVE ACTION 3 AND 4.;[06] HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; NO CRACKS NOTED. <BR>EQUIP USED: NORTEC 600 ID: ATS1465 EQUIP USED: MINIMITE ID: ATS240;[07] CORRECTION : HFEC INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP USED: NORTEC 600 ID: ATS1465;[08] RECEIVED; AND VERIFIED FOR STRINGER SECTION HFAB53-STS-011 FORMED; HEAT TREATED AND DRY PEN INSPECTED ; LOCATED BTW B/S 500D+10'-540 STR 26 L/H ON CUSTOMER RO NO :859020-SWA PO: 859020/1 AND HAT SECTION :HFAB53-HS-011 LOCATED BTW B/S 500D-520 CUSTOMER RO NO :859021-SWA RECEIPT #1484330<BR>LOCATED AND DRILLED IAW SRM 53-00-03-2R-1 REPAIR 1 AND DWG 143A3230 REV:;[09] VERIFIED CORRECTIVE ACTION 8. OK TO TREAT AND PRIME.;[10] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON REPAIR PARTS IAW SRM 53-00-03-2R-1 INSTALLED REPAIR PARTS AT FCB BS 500D+5' TO BS 536 STR 26 L/H IAW SRM 53-00-03-2R-1 FIG 205.

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 74,817 hrs · 44,183 cycles

CRACK ON FWD CARGO BAY STRINGER AT BS 540 L/H STRINGER 23. / [01] EVALUATED CRACK ON FCB STR 23 L/H BS 536 ; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103;[02] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 1.;[03] VERIFIED APPLICABILITY FOR STR 23 L/H IAW SRM 53-00-03-2R-1 FIG 205.;[04] REMOVED DAMAGE BY TRIMMING OUT STRINGER SECTION AT BS 500D+11' TO 536 STR 23L. IAW SRM 53-00-03-2R-1 PAR. 4. STEP A -B;[05] VERIFIED CORRECTIVE ACTION 3 AND 4.;[06] HFEC INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP USED: NORTEC 600 ID: ATS1465;[07] RECEIVED NEW STRINGER SECTION ITEM: HFAD53-ATS-011 PO/N: 859035/1 AND HAT SECTION ITEM: HFAD53-HS-011 LOT: 1484334-1 PO/N: 859039/1. <BR><BR>LOCATED AND DRILLED NEW STRINGER SECTION AND HAT SECTION AT ACB BS 500D+6' TO 536 STR 23 L/H IAW SRM 53-00-03-2R-1 PAR. 4. STEP D - H;[08 APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON REPAIR PARTS IAW SRM 53-00-03-2R-1 STEPS I-J.;[10] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 9.;[11] OK TO INSTALL REPAIR PARTS;[12] NO OK TO INSTALL ; STRUCTURE NOT READY . AWAITING ENG REPAIR INSTRUCTION;[13] REQUEST OK TO INSTALL REPAIR PARTS.;[14] VERIFIED OK TO INSTALL;[15] ENTRY STEP 1 -2.;[16] PARTIAL UPDATES ON STEPS 1 AND 2; OK TO INSTALL;[17] INSTALLED REPAIR PARTS AT FCB BTW BS 500D+6' TO BS 536 STR 23 L/H IAW SRM 53-00-03-2R-1. DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 22-153-00783 REV: A.

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 74,817 hrs · 44,183 cycles

CRACK ON FWD CARGO BAY STRINGER AT BS 540 L/H STRINGER 25. / CRACK ON FCB STR 25 L/H BS 536 ; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103 REMOVED DAMAGE BY TRIMMING OUT STRINGER SECTION AT BS 500D+11' TO 536 STR 25L. IAW SRM 53-00-03-2R-1 PAR. 4. STEP A -B] RECEIVED; AND VERIFIED FOR STRINGER SECTION HFAB53-STS-011 FORMED; HEAT TREATED AND DRY PEN INSPECTED ; LOCATED BTW B/S 500D+10'-540 STR 25 L/H ON CUSTOMER RO NO :859012-SWA RECEIPT # 1484421 AND HAT SECTION :HFAB53-HS-011 LOCATED BTW B/S 500D-520 CUSTOMER RO NO :859000-SWA RECEIPT #1484330 <BR>LOCATED AND DRILLED IAW SRM 53-00-03-2R-1 REPAIR 1 AND DWG 143A3230 REV:; VERIFIED FOR STRINGER SECTION HFAB53-STS-011 FORMED; HEAT TREATED AND DRY PEN INSPECTED ; LOCATED BTW B/S 500D+10'-540 STR 25 L/H ON CUSTOMER RO NO :859012-SWA RECEIPT # 1484421 AND HAT SECTION :HFAB53-HS-011 LOCATED BTW B/S 500D-520 CUSTOMER RO NO :859000-SWA RECEIPT #1484344<BR>LOCATED AND DRILLED IAW SRM 53-00-03-2R-1 REPAIR 1 AND DWG 143A3230 REV:;[09] VERIFIED CORRECTIVE ACTION 8. OK TO TREAT AND PRIME.;[10] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON REPAIR PARTS IAW SRM 53-00-03-2R-1 PAR. 4 STEPS I -J . REQUES OK TO INSTALL. INSTALLED REPAIR PARTS AT FCB BTW BS 500D+6' TO BS 536 STR 25 LH IAW SRM 53-00-03-2R-1 FIG 205;UPDATE STEP#15 : INSTALLED REPAIR PARTS AT FCB BTW BS 500D+6' TO BS 540 STR 25 LH IAW SRM 53-00-03-2R-1 REPAIR 1 FIG 205 AND DWG 143A3230 REV: AND 143A0060 REV:A;

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,817 hrs · 44,183 cycles

DAMAGE ON FWD CARGO BAY STRINGER AT BS 540 R/H STRINGER 22. / [01] EVALUATED CRACK ON FCB STR 22 R/H BS 536 ; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103;[12] FABRICATED AND LOCATED AND DRILLED NEW REPAIR PARTS AT FCB BTW BS 500D+6' TO BS 536 ON STR 22R/H A ; APPLIED CHEMICAL CONVERSION COATING ON REPAIR PARTS AND BARE SURFACES OF THE INITIAL PARTS IAW SRM 53-00-03-2R-1 PAR. 4 STEP D-I FIG . 206. AND EA NO: 22-153-00737 REV:A. REQUEST OK TO PRIMER.;[13] RECEIVED NEW STRINGER SECTION P/N: HFAB53-STS-011 ;PO/N: 860979/1.<BR><BR>FABRICATED AND LOCATED AND DRILLED NEW REPAIR PARTS AT FCB BTW BS 500D+6' TO BS 536 ON STR 22R/H ; APPLIED CHEMICAL CONVERSION COATING ON REPAIR PARTS AND BARE SURFACES OF THE INITIAL PARTS IAW SRM 53-00-03-2R-1 PAR. 4 STEP D-I FIG . 206. AND EA NO: 22-153-00737 REV:A. REQUEST OK TO PRIMER.;[14] VERIFIED CORRECTIVE ACTION #13;[15] APPLIED PRIMER ON REPAIR PARTS AND BARE SURFACES OF THE INITIAL PARTS IAW SRM 53-00-03-2R-1 PAR. 4 STEP J FIG . 206. AND EA NO: 22-153-00737 REV:A. REQUES OK TO INSTALL REPAIR PARTS.;[16] ENTRY PARTIAL STEP 1-3;[17] VERIFIED CORRECTIVE ACTION #15;[18] VERIFIED STEPS 1 AND 3.;[19] PARTIAL ENTRY STEPS 4-5.;[20] ENTRY PARTIAL STEPS 1;3;6.;[21] COMPLETED STEP1; 4; 5; 6 ; PARTIAL UPDATE TO STEP 2;[22] REPAIR PARTS INSTALLED WITH TTG8Q00BE6K0.<BR>ENTRY PARTIAL STEP.1;[23] STEP 2 COMPLETE;[24] ALLL STEPS COMPLETED;[25] VERIFIED ALL STEPS COMPLETE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,817 hrs · 44,183 cycles

CRACK ON FWD CARGO BAY STRINGER AT BS 540 R/H STRINGER 26. / [01] EVALUATED CRACK ON FCB STR 26 R/H BS 536 ; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103;[08] RECEIVED NEW STRINGER SECTION ITEM: HFAB53-STR-011 LOT: 1484419-1 PO/N: 859066; HAT SECTION PO/N: 859067 ITEM: HFAB53-HS-011 LOT: 1484336-1 . LOCATED AND DRILLED NEW STRINGER SECTION AND HAT SECTION IAW SRM 53-00-03-2R-1;[09] RECEIVED NEW STRINGER SECTION ITEM: HFAB53-STR-011 LOT: 1484419-1 PO/N: 859066; HAT SECTION PO/N: 859067 ITEM: HFAB53-HS-011 LOT: 1484336-1 . LOCATED AND DRILLED NEW STRINGER SECTION AND HAT SECTION IAW SRM 53-00-03-2R-1;[10] ACCOMPLISHED HFEC INSPECTION OF CUT EDGE IAW NDTM D6-37239 PART 6; 51-00-00 PROC 23; NO CRACKS FOUND ATS2353 N600;[11] OK TO TREAT AND PRIME REPIAR PARTS AND REPAIR AREA;[12] VERIFIED STEPS 9 AND 11.;[13] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON REPAIR PARTS IAW SRM 53-00-03-2R-1 PAR. 4 STEPS I -J . REQUES OK TO INSTALL.;[14] VERIFIED CORRECTIVE ACTION 13 AND STEP 1 PARTIAL.;[15] INSTALLED STRINGER SECTION AND HAT SECTION IAW SRM 53-00-03-2R-1 4 STEP K.;[16] INSTALLED STRINGER 26R SECTION AT BS 500D+10 TO BS 540 AND HAT SECTION AT BS500D+10 IAW SRM 53-00-03-2R-1 4 STEP K.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 74,817 hrs · 44,183 cycles

CRACK ON FWD CARGO BAY STRINGER AT BS 540 R/H STRINGER 25. / [01] EVALUATED CRACK ON FCB STR 25 R/H BS 536 ; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103;[08] RECEIVED NEW STRINGER SECTION (1 EA ) P/N: HFAB53-STR-011 ; LOT:1484566-1 ; PO/N:859325/1 ; U CHANNEL SECTION ( 1 EA ) P/N: HFAB53-UC-011 ; LOT: 1484347-1 ; PO/N: 859323/1 ; J SECTION ( 2 EA ) P/N: HFAB53-JC-011 ; LOT: 1484350-1 ; PO/N: 859324/1.;[09] VERFIED APPLICABILITY FOR STRINGER 25R ON SRM 53-00-03-2R-1 FIG 206.<BR><BR>LOCATED AND DRILLED REPAIR PARTS AT FCB BTW BS 500D+5' TO BS 536 ON STR 25 R/H IAW SRM 53-00-03-2R-1 PAR. 4 STEPS D -I AND EA NO: 22-153-00694 REV:A . REQUIRED OK TO PRIMER.;[10] VERIFIED CORRECTIVE ACTION 9.;[11] APPLIED PRIMER AT REPAIR PARTS AND REPAIR AREA IAW SOPM 20-41-02; REQ OK TO INSTAL REPAIR PARTS;[12] VERIFIED CORRECTIVE ACTION 11.;[13] UPDTED STEP 1 ND 2 ;OK TO INSTALL;[14] VERIFIED STEPS 1 AND 2. AND CORRECTIVE ACTION 13.;[15] VERIFIED PARTIAL STEPS 1 AND 2.;[16] ENTRY PARTIAL 1 - 2.;[17] INSTALLED REAPAIR PARTS ON FCB BTW BS 500D+5' TO BS 536 ON STR 25 R/H IAW SRM 53-00-03-2R-1 FIG 206 AND EA 22-153-00694 REV:A.;[18] INSTALLED REAPAIR PARTS ON FCB BTW BS 500D+5' TO BS 536 ON STR 25 R/H IAW SRM 53-00-03-2R-1 FIG 206 AND EA 22-153-00694 REV:A. AND DWG 143A3230 REV: ; DWG 143A0060 REV:A;[19] VERIFIED STEPS 1 AND 2 AND CORRECTIVE ACTIONS 17 AND 18.;[20] REPAIRED STR 25R/H BS 540 IAW EA 22-153-00694 REV A;[21] INSPECTION COMPLETE

Part: STRINGER — CRACKED (FWD CARGO BAY) · airframe 74,817 hrs · 44,183 cycles

CRACK ON FWD CARGO BAY STRINGER AT BS 540 L/H STRINGER 27. / CRACK ON FCB STR 27 L/H BS 536 ; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103. REMOVED DAMAGE BY TRIMMING OUT STRINGER SECTION AT BS 500D+11' TO 536 STR 27L. IAW SRM 53-00-03-2R-1 PAR. 4. STEP A -B. HFEC INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP USED: NORTEC 600 ID: ATS1465;[08] RECEIVED ; LOCATED ; DRILLED; ; FORMED; HEAT TREATED AND DRY PEN INSPECTED NEW SECTION OF THE INITIAL STRINGER BTW B/S 500D+10' TO B/S 540 STR 27 L/H . HFAB53-STS-011 MATERIAL USED (7075TO #0.056' TREATED TO T6 ) ON CUSTOMER RO#831380-SWA RECEIPT NUMBER 1464414 IAW SRM 53-00-03-2R-1 FIG 205 AND DWG 143A3241 REV:K;[09] VERIFIED CORRECTIVE ACTION 8;[10] CORRECTIVE ACTION STEP 8<BR><BR>RECEIVED NEW STRINGER SECTION P/N:HFAB53-STS-011 PO/N: 831380 AND HAT SECTION P/NHFAB53-HS-011 LOT: 148527-1 PO/N: 860467/1.<BR><BR>LOCATED AND DRILLE REPAIR PARTS AT FCB BTW BS 500D+6' TO BS 536 ON STR 27 L/H AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 53-00-03-2R-1 PAR. 4. STEP D -I ; INSTALLED REPAIR PARTS AT FCB BTW BS 500D+6' TO BS 536 ON STR 27 L/H IAW SRM 53-00-03-2R-1 FIG 205 INSTALLED REPAIR PARTS AT FCB BTW BS 500D+6' TO BS 540 ON STR 27 L/H IAW SRM 53-00-03-2R-1 REPAIR 1 FIG 205. AND DWG 143A3230 REV:- AND DWG 143A0060 REV:A

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 500A+2; BS 500A+10; BS 500A+14; BS 500A+18; BS 500B+7; BS 500B+10; BS 500C+2; BS 500C+10. / [01] REMOVED CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT;AT LBL 24 ;BTW BS500A+2 TO BS 500C+10; LBL 24 IAW SRM 51-10-02 PARAGRAPH 15; EVALUATED ALL REWORKED AREA ;THE DEPPEST AREA BS 500A+2 LBL 24; DIMENSION: L=2' X W=1' X DEPTH=.008';ORIGINAL THICKNESS 0.040 REMAINING THICKNESS .032 FOUND TO BE DAMAGE OUT LIMITS IAW SRM 53-00-53-1A-2; ALLOWABLE DAMAGE 2;FIG#103;DEATIL 'E' TOOL USED MICROMETER ID ATS400;S/N UNKNOWN DATE DUE 08/2022;[02] VERIFIED CORRECTIVE ACTION 1. OUT OF LIMITS;[03] ACCOMPLISHED WORK AT CUST SYSTEM ID:TTG8Q00B49NH;[04] UPDATED MEASUREMENTS;[05] VERIFIED CARD COMPLETE.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 74,817 hrs · 44,183 cycles

DAMAGE ON FWD CARGO BAY STRINGER AT BS 540 R/H STRINGER 24. / [01] EVALUATED CRACK ON FCB STR 24 R/H BS 536 ; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103[07] RECEIVED; AND VERIFIED NEW STRINGER SECTION HFAB53-STS-011 FORMED; HEAT TREATED AND DRY PEN INSPECTED ; LOCATED BTW B/S 500D+10'-540 STR 24R/H ON CUSTOMER RO NO :859027-SWA PO: 859027/1 AND HAT SECTION :HFAB53-HS-011 LOCATED BTW B/S 500D-520 CUSTOMER RO NO :859025-SWA PO:859025/1. <BR>LOCATED AND DRILLED IAW SRM 53-00-03-2R-1 REPAIR 1 AND DWG 143A3230 REV:B; DWG 143A0060 REV:A.<BR> OK TO PRIMER;[08] VERIFIED CORRECTIVE ACTION 7.;

Part: STRINGER — CRACKED (FWD CARGO) · airframe 74,817 hrs · 44,183 cycles

CRACK ON FWD CARGO BAY STRINGER AT BS 540 R/H STRINGER 23. / [01] EVALUATED CRACK ON FCB STR 23 R/H BS 536 ; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103[17] INSTALLED NEW STRINGER SECTION AND HAT SECTION REPAIR BTW B/S 500D-540 STR 23R/H IAW SRM 53-00-03-2R-1 REPAIR 1 AND DWG 143A3250 REV:C AND 143A0060 REV:A;[18] UPDATE STPE 2 PARTIAL;[19] VERIFIED STEPS 2 AND 3 AND CORRECTIVE ACTION 17.;[20] UP DATED STEP 4 ; REQ. OK TO INSTALL RETACTABLE LANDING LIGHT R/H.;[21] VERIFIED STEP 4 PARTIAL; OK TO INSTALL.;[22] UPDATE STEP 4 PARTIAL;[23] VERIFIED STEP 4 PARTIAL.;[24] STATUS COMPLETED STEP 4.;[25] ENTRY PARTIAL STEP 1.;[26] COMPLETED STEP 1

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON FWD CARGO BAY LOWER BULKHEAD SUPPORT AT BS 395 LBL 23-RBL 22. / [01] REMOVED LOWER BULKHEAD SUPPORT IAW SRM 51-40-02.;[02] CORROSION ON FWD CARGO BAY LOWER BULKHEAD SUPPORT AT BS 395 LBL23 - RBL 22. NO ALLOWABLE DAMAGE PER SRM.<BR> <BR>PART TO BE REPLACED IAW SRM 51-10-02-0G-0 GENERAL - INSPECTION AND REMOVAL OF DAMAGE (PAR.9. REPLACEMENT OF THE PART);[03] VERIFIED ITEM 2 CORRECTIVE ACTIONS.;[04] RECEIVED NEW PART FROM STORES; REF: PO 856302. DRILLED FASTENER HOLES IAW SRM 51-40-05. COUNTERSUNK FASTENER HOLES IAW SRM 51-40-08. REF DWG 284A0603 REV :-;[05] VERIFIED CORRECTIVE ACTION #4;[06] OK TO ISNTALL.;[07] OK TO INSTALL GIVEN.;[08] INSTALLED NEW SUPPORT AT FWD CARGO BAY LOWER BULKHEAD BS 395 LBL;RBL IAW SRM 51-40-02 AND DWG 284A0603 REV:-;[09] ADDED LBL 23 - RBL 22 TO CORRECTIVE ACTION #8.;[10] VERIFIED CORRECTIVE ACTIONS 8 AND 9.

Part: PANEL — CORRODED (FUSELAGE) · airframe 74,817 hrs · 44,183 cycles

PANEL 113AC MATING SURFACE HAS MINOR FRETTING CORROSION AND BARE METAL / [01] REMOVED MINOR FRETTING CORROSION FROM PNL 113AC MEASURED 6'L X 1'W AND 0.003' DEEP FOUND IN LIMITS PER SRM 53-10-14-1A-2;[02] REMOVED MINOR FRETTING CORROSION FROM PNL 113AC MEASURED 6'L X 1'W AND 0.003' DEEP FOUND IN LIMITS PER SRM 53-10-14-1A-2;[11] RECEIVED REPLACEMENT 113AC PNL. PNL TO BE INSTALLED ON CUSTOMER CARD TTG8Q00B2M9W;[12] RECEIVED REPLACEMENT 113AC PNL. PNL TO BE INSTALLED ON CUSTOMER CARD TTG8Q00B2M9W;[13] PART REQUIREMENT;[14] VERIFIED CORRECTIVE ACTION #11

Part: SHIELD — CORRODED (FWD CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 23 BS 480+13; BS 500+6; BS 500+10; BS 500+14; BS 500+18. / [01] NOT ALLOWABLE DAMAGE FOUND ON SRM ; PART MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] LOCATED AND DRILLED ON FWD CARGO BAY AFT DOOR NEW SHIELD AT RBL 23 BTW B/S 480 TO 500A LOT# 1484215-1 PO#:859629/1 IAW SRM 51-40-05 AND DWG 143A0080 REV:-;[03] VERIFIED CORRECTIVE ACTION 2

Part: BULKHEAD — CORRODED (AFT CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON AFT CARGO BAY LOWER BULKHEAD AT BS 947 RBL 21-LBL 10. / [01] LOCATED AND DRILLED NEW TRACK P/N149A8118 IAW SRM 51-40-02 OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION 1.;[03] INSTALLED 10 HI-LOCK IAW SRM 51-40-02 AND DWG 149A8110 ID:0013 REV:B;[04] APPLICABILITY STATEMENT NO FOUND ALLOWABLE DAMAGE IN THE SRM; REPLACEMENT THE PART FOR REPAIR IAW SRM 51-10-02;[05] INSTALLED ACB LOWER BULKHEAD BRACKET AT BS947 RBL21 TO LBL10 IAW NSRM 51-40-02; BOEING DWG 149A8110 REV:B AND BOEING DWG 149A8117 REV:C;[06] VERIFIED CORRECTIVE ACTIONS 3-5. <BR><BR>NEW PART INSTALLED;[07] MEASUREMSNTS;[08] MEASUREMENT FIELDS;[09] PART REQUIREMENT;[10] VERIFIED ALL WORK COMPLETE

Part: SHIELD — CORRODED (AFT CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON AFT CARGO BAY FWD SHIELD AT RBL 21 BS 787+2; BS 787+4; BS 787+5; BS 787+7; BS 787+12; BS 787+15; BS 787+19. / [01] APPLICABILITY STATEMENT;NOT FOUND ALLOWABLE DAMAGE ON SRM;REPAIR BY REPLACEMENT PART IAW SRM 51-10-02-0G-0 PARA.9;[02] LOCATED AND DRILLED NEW SHIELD P/N 146A8127-1 SRM 51-40-05-0G-0;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2.;[04] VERIFIED COMPLETE.;[05] UPDATED MEASUREMENTS

Part: ANGLE — CORRODED (AFT CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON AFT CARGO BAY FRAME TO FWD SHIELD ATTACH ANGLE AT RBL 24 BS 787. / [01] APPLICABILITY STATEMENT;NOT FOUND ALLOWABLE DAMAGE ON SRM;REPAIR BY REPLACEMENT PART IAW SRM 51-10-02-0G-0 PARA.9;[02] REMOVED CLIP AT AFT CARGO BAY FRAME TO FWD SHIELD ATTACH ANGLE AT RBL 24 BS 787 IAW SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW CLIP P/N 146A8125-39; IAW SRM 51-40-05-0G-0 . OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2.;[04] INSTALLED CLIP AT AFT CARGO BAY FRAME TO FWD SHIELD AT RBL 24 BS 787 IAW SRM 51-40-02-0G-0 AND DWG 146A0081 REV.-C;[05] VERIFIED CORRECTIVE ACTION 4.;[06] UPDATED MEASUREMENTS;[07] UPDATED MEASUREMENTS;[08] UPDATED MEASUREMENTS PARAMETERS.

Part: RAIL — CORRODED (AFT CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON AFT CARGO BAY RAIL AT LBL 3 BS 927. / [01] ENTERED MEASUREMENTS;[02] VERIFIED SRM 53-00-53-1A-2 ALLOWABLE DAMAGE IS APPLICABLE<BR>REMOVED CORROSION IAW SRM 51-10-02.<BR>BLENDED AREA MEASURES 0.75' X 1.00' X 0.018' <BR>ORIGINAL MATERIAL THICKNESS 0.80'<BR>REMOVED 0.018' REMAINING MATERIAL 0.062'<BR>DAMAGE FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2. MATERIAL LOSS IS MORE THAN 10% OF ORIGINAL THICKNESS. <BR>REPAIR BY REPLACEMENT IAW SRM 51-10-02.;[03] DIAL DEPTH GAGE: <BR>ATS1225<BR>S/N UNKNOWN<BR>CAL DUE 07/2022;[04] CORRECTION TO ITEM 2. ORIGINAL THICKNESS = 0.080';[05] INSPECTED & VERIFIED CORRECTIVE ACTION ITEMS 1 - 4.;[06] LOCATED AND DRILLED NEW TRACK P/N149A8118 IAW SRM 51-40-02 OK TO INSTALL;[07] LOCATED AND DRILLED NEW TRACK P/N147A7501 IAW SRM 51-40-02 OK TO INSTALL;[08] VERIFIED CORRECTIVE ACTION 7.;[09] REMOVED TRACK AT CB BS887 TO BS947 IAW SRM 51-40-02;[10] INSTALLED NEW TRACK P/N147A7501 AT ACB BS887 TO BS947 LBL 3 WL 156 IAW SRM 51-40-02 AND BOEING DWG 147A7500 REV:-;[11] VERIFIED ITEM 10 CORRECTIVE ACTIONS.;[12] UPDATE PARTS;[13] VERIFIED ITEM 12 CORRECTIVE ACTIONS.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 20 BS 847+5; BS 847+19. / [01] APPLICABILITY STATEMENT;NOT FOUND ALLOWABLE DAMAGE ON SRM;REPAIR BY REPLACEMENT PART IAW SRM 51-10-02-0G-0 PARA.9;[02] LOCATED NEW SHIELD P/N 146A8127-5 IAW SRM 51-40-05-0G-0;[03] UPDATED MEASUREMENTS;[04] SIGN FOR PART;[05] VERIFIED CORRECTIVE ACTIONS 1 AND 2.

Part: ATTACH ANGLE — CRACKED (AFT CARGO BAY) · airframe 74,817 hrs · 44,183 cycles

CRACK ON AFT CARGO BAY LOWER BULKHEAD ATTACH ANGLE AT LBL 11 BS 947+1. / [01] ENTERED MEASUREMENTS;[02] NO ALLOWABLE DAMAGE FOUND FOR THIS PART IN B737-700 SRM.<BR>REPAIR BY REPLACEMENT IAW SRM 51-10-02.<BR>RECEIVED A NEW SUPPORT FITTING P/N 149A8113U6 FROM STORES. REF: PO 841401.<BR>REMOVED DAMAGED FITTING IAW SRM 51-40-02.;[03] VERIFIED CORRECTIVE ACTION #2;[04] LOCATED AND DRILLED NEW SUPPORT FITTING IAW SRM 51-40-05 AND DWG 149A8103 REV:-.<BR>OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION #4; OK TO INSTALL;[06] INSTALLED NEW SUPPORT FITTING IAW SRM 51-40-02 AND DWG 149A8103 REV :-;[07] VERIFIED CORRECTIVE ACTION #6

Part: NONE — CORRODED (AFT CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON AFT CARGO BAY FRAME CHORD AT RBL 4 BS 847. / [01] SRM 53-00-07-1A-1 IS APPLICABLE FOR THIS;[02] REMOVED CORROSION ON AFT CARGO BAY FRAME CHORD AT RBL 4 BS 847 ; WORK AREA; WORK AREA L 1.0' X W 1.0'; ORIGINAL THICKNESS 0.090' ; IAW SRM 53-00-07-1A-1;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2;[14] INSTALLED REPAIR PARTS ON ACB ON FRAME CHORD AT RBL 4 BS 847 . IAW SRM 51-40-02 AND DWG: 146A8130 ID:0001 REV:C . AND EA NO. 22-153-00758 REV:A.;[15] RII INSPECTED STEP 14;[16] VERIFIED FAULT TTG8Q00B3FVF IS COMPLETE.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 20 BS 747+5; BS 747+6; BS 747+8; BS 747+12; BS 747+14; BS 747+19; BS 767+3; BS 767+5; BS 767+8; BS 767+13. / [01] REMOVED CORROSION FROM BS747+5 TO BS767+13 LBL 20 IAW SRM 51-10-02-0G-0 STEP 15<BR><BR>747+5=0.005' L=1.5' W=1'<BR>747+6=0.004' L=1.5' W=.5'<BR>747+8=0.004 L=1' W=.5'<BR>747+12=0.007' L=2' W=.8'<BR>747+14=0.005' L=.5' W=.5'<BR>747+19=0.005' L=1' W=1'<BR>767+3=0.004' L=2' W=1'<BR>767+5=0.004' L=1' W=.5'<BR>767+8=0.005' L=1' W=.5'<BR>767+13=0.006' L=2' W=1'<BR><BR>DEEPEST DAMAGED IS AT BS 747+12; 0.007' MATERIAL REMOVED. ORIGINAL THICKNESS 0.040'. REMAINING MATERIAL 0.033' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2<BR><BR>TOOL USED<BR>DIAL DEPTH GAUGE ID: ATS1225 S/N: UNKNOWN;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] THIS JOB CARD WILL BE REPAIRED WITH THE NEXT JOB CARD TTG8Q00B3FUV;[04] VERIFIED CORRECTIVE ACTION ENTRY 3.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 20 BS 787+2; BS 787+6; BS 787+10; BS 787+14; BS 807+2; BS 807+6; BS 807+10; BS 807+14. / [01] REMOVED CORROSION FROM BS787+2 TO BS807+14 LBL 20 IAW SRM 51-10-02-0G-0 STEP 15<BR><BR>787+2=0.004' L=.5' W=.5'<BR>787+6=0.003' L=2' W=1'<BR>787+10= 0.005' L=.5' W=.5'<BR>787+14=0.006' L=.5 W=.5'<BR>807+2=0.003' L=.5' W=.5'<BR>807+6=0.007' L=.5' W=.5'<BR>807+10=0.004' L=1' W=.5'<BR>807+14=0.006' L=.5' W=.5'<BR><BR>DEEPEST DAMAGED IS AT BS 807+10; 0.007' MATERIAL REMOVED. ORIGINAL THICKNESS 0.040'. REMAINING MATERIAL 0.033' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2<BR><BR>TOOL USED<BR>DIAL DEPTH GAUGE ID: ATS1225 S/N: UNKNOWN;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] FABRICATED LOCATED AND DRILLED AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT LBL 20 BS 727 TO BS TO 847 MATERIAL USED BAC1496-377=7075T62 EXTRUSION LOT:1477731-1 IAW SRM 51-40-05 AND DWG 146A7502 REV:A.;[04] FABRICATED LOCATED AND DRILLED AFT CARGO BAY SPLICE TO SIDEWALL SUPPORT AT LBL 20 BS 727E+10 MATERIAL USED BAC1496-377=7075T6 EXTRUSION LOT#1477731-1 IAW SRM 51-40-05 AND SRM 53-00-53-2R-6 REPAIR 6.;[05] VERIFIED CORRECTIVE ACTION 3 AND 4;[06] APPY CHEMICAL CONVERSION COATING AND PRIMER.13] INSTALLED FLOOR TO SIDEWALL SPLICE REPAIR BETWEEN BS 727E TO 747 L/H LBL 20 IAW SRM 53-00-53-2R-6 REPAIR 6.;[14] VERIFIED CORRECTIVE ACTIONS 12 AND 13.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 20 BS 727C+10; BS 727C+18; BS 727D+6; BS 727D+8; BS 727D+18; BS 727E+2; BS 727E+6; BS 727E+14; BS 727E+18; BS 747+2. / [01] REMOVED CORROSION FROM BS727C+10 TO BS747+2 LBL 20 IAW SRM 51-10-02-0G-0 STEP 15<BR><BR>727C+10=0.002' L=.5' W=.5'<BR>727C+18=0.005' L=.5' W=.5'<BR>727D+6=0.004' L=1' W=.5'<BR>727D+8=0.004' L=.5' W=1'<BR>727D+18=0.005' L=.5' W=.5'<BR>727E+2=0.002' L=.5' W=.3'<BR>727E+6=0.003' L=1.5' W=1'<BR>727E+14=0.003' L=1.5' W=.5'<BR>727E+18=0.005' L=1.5' W=1'<BR>742+2=0.006' L=2' W=1'<BR><BR>DEEPEST DAMAGED IS AT BS 747+2; 0.006' MATERIAL REMOVED. ORIGINAL THICKNESS 0.040'. REMAINING MATERIAL 0.034' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2<BR><BR>TOOL USED<BR>DIAL DEPTH GAUGE ID: ATS1225 S/N: UNKNOWN;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] THIS JOB CARD WILL BE REPAIRED WITH THE NEXT JOB CARD TTG8Q00B3FUV;[04] VERIFIED CORRECTIVE ACTION ENTRY 3.

Part: FRAME — CRACKED (AFT CARGO BAY) · airframe 74,817 hrs · 44,183 cycles

CRACK ON AFT CARGO FRAME AT RBL 17 BS 907. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-07-1A-1 ALLOWABLE DAMAGE 1 AND SRM 53-70-07-0I-1 IDENTIFICATION 1;[02] EVALUATED FRAME ; CRACK LENGTH: 1' FOUND OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-07-1A-1 ALLOWABLE DAMAGE 1 FIGURE 102 . TOOL USED CALIPER :ID:ATS2502 DATE DUE:04/2022;[03] VERIFIED CORRECTIVE ACTION ITEM 2.;[04] PARTIAL UPDATED STEP 4.;[05] PARTIAL UPDATED STEPS 1;2 AND 3;[06] PARTIAL UPDATED STEPS; 5;6;7 AND 8;[07] PARTIAL UPDATED STEP 9;[08] REMOVED ACB FRAME AT RBL 17 ; BS 907 IAW SRM 51-40-02-0G-0;[09] RECEIVED NEW FRAME P/N: 147AA1007U57 ; LOT: 1483838-1 ; PO/N: 859032/1.<BR><BR>LOCATED AND DRILLED NEW FRAME AT ACB BS 907 BTW STR 24R TO 24L IAW SRM 51-40-05 REQUEST OK TO INSTALL NEW FRAME .;[10] PARTIAL ENTRY STEPS 1-9 . REQUEST OK TO RE-INSTALL.;[11] VERIFIED CORRECTIVE ACTION #9 AND 10; OK TO INSTALL;[12] BEGAN INSTALL PERMANENT FASTENERS AND 100% TEMPORALLY FASTENERS AT ACB FRAME BS 907 BTW STR 24R TO 24L ; C-20 SEALANT USED AT 09-MAR-2022 04:13 UTC IAW SRM 51-40-02 AND DWG:147A0040 ; ID:0042 ; REV: A.COMPLETED NEW FRAME INSTALLATION BS 907; BETWEEN STR 24L - 24R. I.A.W DWG:147A0040 ID:0042 REV:A; DWG: 147A9409REV: -; DWG: 147A1007 REV:D AND SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 907+6; BS 907+10; BS 907+13; BS 907+17. / [01] REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT RBL21 BS 907+6 MEASURED 1.3'L X 1'W AND 0.005' DEEP FOUND OUT OF LIMITS<BR><BR>REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT RBL21 BS 907+6 MEASURED 1'L X 1'W AND 0.0035' DEEP FOUND IN LIMITS<BR><BR>REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT RBL21 BS 907+6 MEASURED 2'L X 1'W AND 0.0025' DEEP FOUND IN LIMITS<BR><BR>REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT RBL21 BS 907+6 MEASURED 0.8'L X 0.5'W AND 0.0065' DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2<BR><BR>CAL ID DIAL DEPTH GAUGE<BR>ATS1225<BR>S/N UNKNOWN<BR>DUE 07/2022;[05] FABRICATED REPLACEMENT FLOOR TO SIDEWALL SUPPORT USING ITEM: BAC1496-377#7075T62 LOT: 1477731-1 IAW SRM 51-40-02; SRM 51-40-08 SRM 51-40-05 AND DWG 147A7501 ID:0006 REV: A. APPLIED CHEMICAL CONVERSION COATING TO REPLACEMENT SIDEWALL SUPPORT IAW SOPM 20-41-02. OK TO APPLY PRIMER.;[06] FABRICATED REPLACEMENT FLOOR TO SIDEWALL SUPPORT USING ITEM: BAC1496-377#7075T62 LOT: 1477731-1 IAW SRM 53-60-53-0I-2 TABLE 2 ITEM 2; SRM 51-40-02; SRM 51-40-08 SRM 51-40-05 AND DWG 147A7501 ID:0006 REV: A. APPLIED CHEMICAL CONVERSION COATING TO REPLACEMENT SIDEWALL SUPPORT IAW SOPM 20-41-02. OK TO APPLY PRIMER.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL RBL 21 BS 727B+15; 727C+12; BS 727D+5; BS 727D+13; BS 727D+14; BS 727D; BS 727D+8; BS 727E+3; BS 727E+15. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT RBL 21 IAW SRM53-00-53-1A-2 ALLOWABLE DAMAGE 2;[02] REMOVED CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT RBL21 BS727B+15;727C+12;BS 727D+5; BS727D+13;BS 727D+14;BS727D;BS727D+8;BS 727E+3;BS 727E+15 IAW SRM 51-10-02 PARAGRAPH 15;BTW BS 727B+15 TO BS727+15;EVALUATED ALL REWORKED AREAS;THE DEPPEST AREA BS 727B+15 RBL21;DIMENSION L=3'X W:1'X DEPTH=0.009;ORIGINAL THICKNESS 0.040' REMAINING THICKNESS 0.031' FOUND TO BE OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 FIG#103 DEATIL'E' TOOL USED;IDATS400 S/N UNKNOWN DUE 08/2022.;[03] UPDATED MEASUREMENTS;[04] VERIFIED CORRECTIVE ACTIONS 1 AND 2.;[05] FABRICATED LOCATED AND DRLLED AFT CARGO BAY NEW FLOOR TO SIDEWALL SUPPORT RBL 21 BS 727 TO BS767 MATERIAL USED BAC1496-377=7075T62 LOT#1477731-1 IAW SRM 51-40-05 AND DWG 146A7502 REV:A;OK APPLY CHEMICAL COATING AND PRIMER.;[06] VERIFIED CORECTIVE ACTION 5.;[07] APPLIED CHEMICAL CONVERSION COATING AND PRIMER AFT CARGO BAY NEW FLOOR TO SIDEWALL SUPPORT RBL 21 BS 727 TO BS767 IAW SRM 51-20-01 AND AMM51-21-72-370-804.;[08] VERIFIED CORRECTIVE ACTION 7.;[09] REPAIR COMPLETE.;[10] VERIFIED CORRECTIVE ACTION 9. NO FURTHER ACTION REQUIRED.<BR><BR>PART TO BE INSTALLED ON TTG8Q004G921.

Part: RAIL — CORRODED (AFT CARGO) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON AFT CARGO BAY RAIL AT RBL 13 BS 907; BS 927+7. / [01] VERIFIED SRM 53-00-53-1A-2 ALLOWABLE DAMAGE IS APPLICABLE<BR>REMOVED CORROSION IAW SRM 51-10-02<BR><BR>BS907 TIE DOWNS TOP SURFACE OF TRACK; REWORKED AREA MEASURES 1.20' X 2.20' X 0.015 DAMAGE FOUND TO BE IN LIMITS IAW SRM 53-00-53-1A-2<BR>BS 927+7 FLANGE REWORKED AREA MEASURES 1.20' X 1.50' X 0.004' DAMAGE FOUND IN LIMITS IAW SRM 53-00-53-1A-2<BR>TOOL DEPTH GAGE; ID: ATS2677 S/N UNKNOWN DATE: 11/2021 DUE: 11/2022<BR>CALIPER ID: ATS2502 S/N A19335659 DATE: 04/2021 DUE: 04/2022;[09] INSTALLED NEW TRACK ASSEMBLY IAW SRM 51-40-02 AND DWG 147A7500 REV :-

Part: RAIL — CRACKED (AFT CARGO BAY) · airframe 74,817 hrs · 44,183 cycles

CRACK ON AFT CARGO BAY RAIL AT LBL 17 BS 767. / [01] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS;[02] CRACK ON AFT CARGO BAY RAIL AT LBL 17; BS 767 ; L 0.500 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2;[03] VERIFIED CORRECTIVE ACTION STEP 1 AND 2.;[04] REMOVED CARGO BAY RAIL FROM BS727 TO BS867; LBL17 AT ABC IAW SRM 51-40-02;[05] LOCATED AND DRILLED NEW RAIL TRACK P/N 146A7501 PO NUMBER 851044/1 IAW SRM 51-10-02 OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION 4 AND 5- OK TO INSTALL AFT LBL CARGO TRACK.;[07] INSTALLED NEW RAIL IAW SRM 51-40-02 AND DOCUMENT NUMBER 146A7500 REV: C.;[08] VERIFIED CORRECTIVE ACTION 7.;[09] CORRECTION TO LINE 4. UP DATED MEASUREMENTS 2; 4; 5; 9; 11;[10] VERIFIED ALL WORK ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (CABIN FLOOR) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 45 BS 360+9-360+13; BS 420+13; BS 440+5. / REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 45 WL 208; BS 360+9 TO 360+13 D: 0.056' L: 4' W: 0.90'; BS 420+13 D: 0.020' L: 1' W: 0.90'; BS 440+5 D: 0.012' L: 1' W: 0.90' FOUND SEAT TRACK TO BE OUT LIMITS PER SRM 53-00-52-1A-1. USED TOOL ID:ATS1738 S/N UNKNOWN DUE: 09/2022 REMOVED PASSENGER CABIN SEAT TRACK LBL45; BS360+10 - BS480; WL208 PER SRM 51-40-02-0G-0.;[05] LOCATED AND DRILLED NEW SEAT TRACK BS 360+10 TO 480 LBL 45 WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5300.INSTALLED NEW PASSENGER CABIN SEAT TRACK LBL45; BS360+10 - BS480; WL 208 PER SRM 51-40-02-0G-0 & BOEING DWG 143A5300; REV. J<BR>ID TOOL: ATS2657; S/N: 0821900635; D/D: 08/2022;<BR>ID TOOL: PER1780; S/N: A97G23122; D/D: 02/2023.<BR>ID TOOL: E12062; S/N: SP02F31924; D/D: 12/2022.;[10] MATCH DRILLED FLOOR BOARD HOLES IAW SRM 51-40-05;[11] MATCH DRILLED FLOOR BOARD HOLES IAW SRM 51-40-05 AND UPDATED PARTS.;[12] CORRECTLY UPDATED PARTSINSTALLED NEW PASSENGER CABIN SEAT TRACK LBL45; BS360+10 - BS480; WL 208 PER SRM 51-40-02-0G-0 & BOEING DWG 143A5300; REV:-<BR>ID TOOL: ATS2657; S/N: 0821900635; D/D: 08/2022; <BR>ID TOOL: PER1780; S/N: A97G23122; D/D: 02/2023. <BR>ID TOOL: E12062; S/N: SP02F31924; D/D: 12/2022.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT RBL 45 BS 500D+1. / [01] VERIFIED EFFECTIVITY FOR SRM 53-00-52-1A-1. <BR>REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK AT RBL 45 WL 208 BS 500C+18 TO 500D+2 IN WELL AREA L:4' W:0.90' MAX. DEPTH:0.043' FOUND OUT LIMITS PER SRM 53-00-52-1A-1. USED TOOL ID: ATS1738 S/N UNKNOW DUE: 09/2022.[09] INSTALLED PASSENGER CABIN SEAT TRACK REPLACEMENT AT RBL45; BS480 - BS520; WL208; PER SRM 51-40-02-0G-0 AND BOEING DRAWING 143A5300.<BR>ID TOOL: ATS2686; S/N: 1021903733; D/D:11/2022.<BR>ID TOOL: E11969; S/N: SP02F31939; D/D: 12/2022.<BR>ID TOOL: PER1780; S/N: A97G23122; D/D: 02/2023.;[10] TORQUED ALL BOLTS COMMON TO PASSENGER CABIN SEAT TRACK RBL45; BS480 - BS520; WL208; PER SRM 51-40-04-0G-0; ID TOOLS USED MENTIONED ON STEP 9.;[11] REMOVED EWIS FOD PROTECTION FROM WORK AREA; BS480 - BS520; RBL20 - RBL68; WL200; PER AMM 20-60-07-913-801.;[12] INSPECTED & VERIFIED CORRECTIVE ACTION ITEMS 9 & 10.;[13] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 11.;[14] UPDATED MEASUREMENTS STEPS 5;6;23 AND 24.;[15] VERIFIED FAULT TTG8Q00B2S5E IS COMPLETE.

Part: SEAT TRACK — CORRODED (CABIN FLOOR) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 25 BS 360+15-380; BS 400+1; BS 420+11. / REMOVED CORROSION FROM WELL OF PASSENGERS CABIN SEAT TRACK LBL 25; FROM BS360+10 - BS380; L=10.0' X W=0.900' X D=0.045.<BR>AND FROM BS400+1 - BS420+11; L=30.0' X W=0.900' X D=0.012'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1.<BR>ID TOOL: ATS1738; S/N: UNKNOWN; D/D:09/2022.<BR>ID TOOL: ATS2472; S/N: UNKNOWN; D/D: 12/2022REMOVED PASSENGER CABIN SEAT TRACK LBL25 FROM BS360+10 - BS480; WL208; PER SRM 51-40-02-0G-0.; LOCATED AND DRILLED NEW SEAT TRACK BS 360+10 TO 480 LBL 25 WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5300] INSTALLED FASTENERS COMMON TO FLOOR BEAMS BS 400-480 LBL25 WL208 IAW DWG 143A5300; SRM 51-40-02-0G-0;[08] INSTALLED NEW PASSENGER CABIN SEAT TRACK LBL25; BS360+10 - BS480; WL 208 PER SRM 51-40-02-0G-0 & BOEING DWG. 143A5300; REV. J<BR>ID TOOL: ATS2657; S/N: 0821900635; D/D: 08/2022;<BR>ID TOOL: PER1780; S/N: A97G23122; D/D: 02/2023.<BR>ID TOOL: E12062; S/N: SP02F31924; D/D: 12/2022.;[09] MATCH DRILLED FLOOR BOARD HOLES IAW SRM 51-40-05;[10] UPDATED PARTS.;[11] VERIFIED MATCH DRILL;[12] VERIFIED;[13] VERIFIED STEP ACTION ITEM #1;[14] UPDATED STEP 8.<BR>INSTALLED NEW PASSENGER CABIN SEAT TRACK LBL25; BS360+10 - BS480; WL 208 PER SRM 51-40-02-0G-0 & BOEING DWG. 143A5300; REV:-<BR>ID TOOL: ATS2657; S/N: 0821900635; D/D: 08/2022;<BR>ID TOOL: PER1780; S/N: A97G23122; D/D: 02/2023.<BR>ID TOOL: E12062; S/N: SP02F31924; D/D: 12/2022.

Part: SEAT TRACK — CORRODED (CABIN FLOOR) · airframe 74,817 hrs · 44,183 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT RBL 25 BS 727C+16; BS 727C+19; BS 727D+18; BS 827; BS 827+14; BS 847+12; BS 887. / REMOVED CORROSION FROM TOP AND WELL OF PASSENGER CABIN SEAT TRACK RBL 25; FROM BS727C TO BS887;IAW SRM 53-00-52-1A-1; FOUND TO BE OUT OF LIMITS; MEASUREMENTS ON TOP OF SEAT TRACK FROM BS727C+16 TO BS727C+19 <BR>; L=3.0' X W=0.400' X D=0.029'(MATERIAL REMOVED).<BR> ON WELL OF SEAT TRACK FROM BS727D+18 TO BS727E+2; L=4.0' X W=0.900' X D=0.10'.<BR>ON WELL OF SEAT TRACK FROM BS827 TO BS827+14; L=14.0' X W=0.900' X D=0.010'.<BR>ON WELL OF SEAT TRACK; FROM BS847+12 TO BS867+4 L=12.0' X W=0.900' X D=0.012'.<BR>ON TOP OF SEAT TRACK; BS867; L=1.0' X W=0.400' X D=0.022'.<BR>ON WELL OF SEAT TRACK; BS887; L=2.0' X W=0.900' X D=0.010'.<BR>ID TOOL: ATS1225; S/N: UNKNOWN; D/D: 07/2022<BR>ID TOOL: ATS1738; S/N: UNKNOWN; D/D: 09?2022.;[02] VERIFIED CORRECTIVE ACTION #1REMOVED SEAT TRACK BS 727B - 887 RBL 25 PER SRM 51-40-02-0G-0ENSURED SEAT TRACK WAS FABRICATED PER DWG# 146A5350 REV-; REFER TO ATS BUILD RECORD 527987 COMPLETED DRILLING OF REPLACEMENT SEAT TRACK IAW SRM 51-40-05 AND DWG 146A5350.] INSTALLED PASSENGER CABIN SEAT TRACK REPLACEMENT AT RBL25; BS727B - BS887; WL208; PER SRM 51-40-02-0G-0 AND BOEING DRAWING 146A5300. TORQUED ALL FASTENER CABIN SEAT TRACK PER SRM 51-40-04. <BR>ID TOOL: ATS2686; S/N: 1021903733; D/D:11/2022. <BR>ID TOOL: E11969; S/N: SP02F31939; D/D: 12/2022.

Part: SUPPORT — CRACKED (R/H WING) · airframe 74,817 hrs · 44,183 cycles

R/H WING LOWER T/E PANEL SUPPORT IS CRACKED AT RSS 280. (MARKED) / [01] UPDATED PARTS REQUIREMENT;[02] REMOVED AND REPLACED R/W LOWER T/E PANEL SUPPORT AT RSS 280 IAW SRM 51-40-02-0G-0;[03] VERIFIED CORRECTIVE ACTION STEP 2.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 74,817 hrs · 44,183 cycles

CRACK IN BEAR STRAP BS294 BETWEEN STR 8R AND 9R AT FWD GALLEY DOOR. MARKED IN RED. CRACK LENGTH .250 IN FROM EDGE OF FASTENER GOING AFT AND UP. FOUND ON HFEC INSP / [01] VERIFIED SRM 53-10-01-2R-6 IS APPLICABLE FOR REPAIR TO FUSELAGE SKIN AND BEAR STRAP AT FWD GALLEY DOOR UPPER FWD CUTOUT CORNER.;[09] FABRICATED 1 EA. DOUBLER WITH 2024-T3#0.100 IN.; LOT # 1443470-1; 1 EA. TRIPLER WITH 2024-T3#0.063 IN. LOT #1478284-1; 1 EA. TAPERED SHIM WITH 2024-T3#0.160 IN. LOT #1419195-1 & 1 EA. FLAT SHIM WITH 2024T3#0.063 IN. LOT #1478284-1; PER SRM 53-10-01-2R-6; TABLE 201; OK TO APPLY CHEMICAL CONVERSION COATING AND IMPACT PRIMER.;[10] VERIFIED CORRECTIVE ACTION ITEM 9.<BR>OK TO APPLY CHEMICAL CONVERSION COATING AND IMPACT PRIMER.14] FABRICATED 1 EA. FILLER FROM 2024-T3 0.090' LOT # 1468724-1 PER SRM 53-10-01-2R-6; TABLE 201; APPLIED CHEMICAL CONVERSION COATING AND PRIMER.;

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 74,817 hrs · 44,183 cycles

CRACK ON PASSENGER CABIN FLOOR PANEL SUPPORT AT RBL 1 BS 540.(MARKED) / [01] REMOVED AND REPLACED PANEL SUPPORT AT RBL 1 BS 540 IAW SRM 51-40-02 AND SRM 51-40-05 AND BOEING DWG 143A0060.;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION 1; 2. NEW PART INSTALLED. <BR><BR>STILL REQUIRE LOCATING OF FLOOR BOARD PANEL FASTENER HOLES.;[04] MATCH DRILLED FLOOR BOARD HOLES IAW SRM 51-40-05.;[05] VERIFIED;[06] VERIFIED CORRECTIVE ACTIONS 4 AND 5

Part: SUPPORT BRACKET — CRACKED · airframe 74,817 hrs · 44,183 cycles

CRACK ON AFT UNPRESSURIZED COMPARTMENT FIRE DETECTOR SENSOR SUPPORT BRACKET AT BS 1064 LBL 3 JUST ABOVE L/H STRINGER 26. / [01] EVALUATED CRACK ON AFT UNPRESSURIZED COMPARTMENT FIRE DETECTOR SENSOR SUPPORT BRACKET AT BS 1064 LBL 3 JUST ABOVE L/H STRINGER 26. NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED ON AFT UNPRESSURIZED COMPARTMENT FIRE DETECTOR SENSOR SUPPORT BRACKET AT BS 1064 LBL 3 JUST ABOVE L/H STRINGER 26. IAW SRM 51-40-02;[03] VERIFIED CORRECTIVE ACTION #1 AND #2;[04] FABRICATED; LOCATED AND DRILLED NEW SUPPORT BRACKET AT BS 1064 LBL 3 JUST ABOVE L/H STRINGER 26. MATERIAL USED:BAC1490-2723 LOT#: 1483942-1 IAW SRM 51-40-05 AND DWG: REV:148A9805 REV:B AND DWG:148A1900 REV:A AND APPLIED CHEMICAL CONVERTION AND PRIMER IAW SRM 51-20-01 AND AMM 51-21-72-370-804 . <BR>OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 4; OK TO INSTALL GIVEN.;[06] INSTALLED NEW SUPPORT BRACKET AT BS 1064 LBL 3 JUST ABOVE L/H STRINGER 26. IAW SRM 51-40-02 AND DWG: REV:148A9805 REV:B AND DWG:148A1900 REV:A;[07] VERIFIED CORRECTIVE ACTION 6.

Part: NONE — CRACKED (FUSELAGE) · airframe 74,817 hrs · 44,183 cycles

UPON INSPECTION OF CCN:753-201-00-02; FOUND 5 EA CRACKS AT BS 665 LBL 30 WL 201 AND BS 672.5 LBL 32 - 35 WL 201; COMMON TO THE HORIZONTAL PRESSURE DECK; AREAS MARKED. / [01] REMOVED FLOOR SUPPORT AT BS 663 LBL45-LBL 60 WL 208 PER SRM 51-40-02-0G-0;[02] INSTALLED FOD PROTECTION AT REPAIR AREA PER MM 20-60-02-100-80[15] FABRICATED REPAIR PARTS -1 DOUBLER .080 2024-T3 LOT #1478284-1; -2 STIFFENERS 7-EA BAC1550-100052 7076-T6511 LOT #1462982-1; -3 REPLACEMENT WEB .063 2024-T3 LOT #1478284-1; -4 FILLER .080 2024-T3 LOT #1478284-2;-5 FILLER 2024-T LOT #1478284-1; -6 FILLERS .090 2024-T3 LOT # 1468724-1 AND .020 2924-T3 LOT # 1194858; -7 FILLER .080 2024-T3 LOT # 1478284-2 ; -8 FILLER .063 2024-T3 LOT #1478284-1; -9 FILLER .063 2024-T3 LOT # 1478284-1 AND APPLIED CHEMICAL CONVERSION COATING PER SRM 53-40-51-2R-2 STEPS 4 E-J[26] FABRICATED REPAIR PARTS -1 DOUBLER .080 2024-T3 LOT # 1481648-1; -2 STIFFENERS 7 EA BAC1505-100052 7075-T6 LOT # 1459415-1; -3 WEB .063 2024-T3 LOT # 1478284-1 ;-6 FILLERS 3 EA .090 2024-T3 LOT # 1468724-1; AND -6 FILLERS 3 EA .020 2024-T3 LOT # 1194858 ; AND APPLIED CHEMICAL CONVERSION COATING PER SRM 53-40-51-2R-2 STEP 4 E-

Part: SEAL — DEFORMED (HORIZONTAL STAB) · airframe 74,175 hrs · 43,790 cycles

LEFT HORIZONTAL STABILIZER FWD LOWER SLIDING SEAL DEFORMED AT UPPER END ; / [01] R&R LEFT HORIZONTAL STABILIZER FWD LOWER SLIDING SEAL PER MM REF 53-31-31

Part: COVER — OUT OF POSITION (R1 DOOR SLIDE) · airframe 72,486 hrs · 42,764 cycles

R1;R2; AND L2 DOORS MANUAL DEPLOY HANDLE COVERS ON SLIDES NOT VISIBLE. PULLED DOWN HOOK AND LOOP FLAPS FROM SLIDE COVERS AND ATTACHED THE HOOK AND LOOP PER SIP

Part: COVER — OUT OF POSITION (R2 DOOR SLIDE) · airframe 72,486 hrs · 42,764 cycles

R1;R2; AND L2 DOORS MANUAL DEPLOY HANDLE COVERS ON SLIDES NOT VISIBLE. PULLED DOWN HOOK AND LOOP FLAPS FROM SLIDE COVERS AND ATTACHED HOOK AND LOOP PER SIP

Part: COVER — OUT OF POSITION (L2 DOOR SLIDE) · airframe 72,486 hrs · 42,764 cycles

R1;R2; AND L2 DOORS MANUAL DEPLOY HANDLE COVERS ON SLIDES NOT VISIBLE. PULLED DOWN HOOK AND LOOP FLAPS FROM SLIDE COVERS AND ATTACHED HOOK AND LOOP PER SIP

Part: LAMP — INOPERATIVE (OVRWG EMER LGT) · airframe 72,420 hrs · 42,728 cycles

L/H OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED PER AMM

Part: LENS — DIRTY (CABIN) · airframe 70,234 hrs · 41,391 cycles

DIRTY DOOR EMERGENCY LIGHT LENS RH SIDE AT AFT GALLEY AREA / CLEANED DOOR EMERGENCY LIGHT LENS RH SIDE AT AFT GALLEY AREA IAW AMM 20-30-82-910-801

Part: FLOOR PANEL — DETERIORATED (CARGO BAY) · airframe 70,234 hrs · 41,391 cycles

DETERIORATED FLOOR PANEL 140DF AT AFT CARGO COMPARTMENT (1 EA) REPLACED FLOOR PANEL 140DF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01 DRAWING 453A2610 REV C

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 70,234 hrs · 41,391 cycles

CRACK INBOARD THRUST REVERSE BRACKET INTERNAL AREA COMMON TO RT PYLON ON ENGINE 2 (1 EA) / REPLACED INBOARD THRUST REVERSE BRACKET INTERNAL AREA COMMON TO RT PYLON ON ENGINE 2 (1EA) IAW SPM 70-43-00 AND DWG 311A2683 SHEET 14 REV

Part: SKIN — DENTED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

FUSELAGE EXTERNAL SKIN HAS A DENT WITH OIL CAN LOCATED AT BS 390.5 APPRX AND BETWEEN STRINGERS 16 AND 17L. THE DENT MEASURES L=3.254 IN W=1.910 IN Y=0.028 W/Y=68 FUSELAGE EXTERIOR (1 EA) / PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN 380 AND BSTA 440 AND BETWEEN STR14L AND STR18L IAW EA . N.1-753-36788 REV IR AND EA 53-0249-20 REV O PAGE 1-3 AND EA PART 1 AND PART 2 FOR INSPECTION REQUIRED SEE TLD #T078748

Part: SUPPORT — CRACKED (LT WING) · airframe 70,234 hrs · 41,391 cycles

CRACK TRAILING EDGE BEAM ASSY SUPPORT AT LT WING (1EA) REPLACED TRAILING EDGE BEAM ASSY SUPPORT AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 115A3712 REV.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

ELONGATED HOLE FRAME BS500D AT STR 19L AT FWD CARGO COMPARTMENT (1 EA) / PERFORMED REPAIR FRAME BS 500D AT S-19L AT FWD CARGO COMPARTMENT IAW EA NO.1-753-36789 REV.1 AND E.A #53-0214-20 REV.#1

Part: FASTENER — CORRODED (R2 DOOR) · airframe 70,234 hrs · 41,391 cycles

RUST ON FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKE HARDWARE OF AFT SERVICE DOOR AT AFT GALLEY AREA REPLACED HARDWARE ON FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKET OF AFT SERVICE DOOR AT AFT GALLEY AREA IAW AMM 25-66-02-400-801 STEP 3D1(G)

Part: FASTENER — CORRODED (L2 DOOR) · airframe 70,234 hrs · 41,391 cycles

RUST ON FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKE HARDWARE OF AFT ENTRY DOOR AT AFT GALLEY AREA REPLACED HARDWARE ON FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKET OF AFT ENTRY DOOR AT AFT GALLEY AREA IAW AMM 25-66-02-400-801

Part: BRACKET — CORRODED (L1 DOOR) · airframe 70,234 hrs · 41,391 cycles

RUST ON FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKE HARDWARE OF FWD ENTRY DOOR AT FWD GALLEY AREA REPLACED HARDWARE SLIDE BRACKET FLOOR DOOR MOUNTED OF FWD ENTRY DOOR AR AFT GALLEY AREA IAW B737-700 AMM 25.66.02.400.801

Part: BRACKET — CORRODED (L1 DOOR) · airframe 70,234 hrs · 41,391 cycles

RUST ON FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKE HARDWARE OF FWD SERVICE DOOR AT FWD GALLEY AREA REPLACED HARDWARE SLIDE BRACKET FLOOR DOOR MOUNTED OF FWD ENTRY DOOR AT AFT GALLEY AREA IAW B737-700 AMM 25.66.02.400.801

Part: PLATE — CORRODED (L1 DOOR) · airframe 70,234 hrs · 41,391 cycles

RUST ON PLATE ASSY ADAPTER FLOOR DOOR MOUNTED EVACUATION SLIDE BRAKET FWD ENTRY DOOR AT FWD GALLEY AREA (2 EA) REPLACED PLATE ASSY ADAPTER FLOOR MAUNTED EVACUATION SLIDE BRACKET FWD ENTRY DOOR AT FWD GALLEY AREA (2EA) IAW B737-700 AMM 25-66-02-400-801

Part: PLATE — CORRODED (L2 DOOR) · airframe 70,234 hrs · 41,391 cycles

RUST ON PLATE ASSY ADAPTER FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKE AFT ENTRY DOOR AT AFT GALLEY AREA (2 EA) REPLACED PLATE ASSY ADAPTER FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKET AFT ENTRY DOOR AT AFT GALLEY AREA (2EA) IAW AMM 25-66-02-400-801

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 70,234 hrs · 41,391 cycles

CRACK FRONT SPAR VERTICAL ANGLE AT STAB STA 138.70 AT LT HORIZONTAL STABILIZER / REPLACED VERTICAL ANGLE LOC. RIB STA 138.70 AT FRONT SPAR LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #182A5306 REV.C AND FASTENERS MATERIAL USED BAC1506-4343 P.O #2020-128219/1

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 70,234 hrs · 41,391 cycles

CRACK INSPAR RIB INBOARD LOWER HORIZONTAL FLANGE STAB STA 129.50 AT 3 5 INCH FROM FRONT SPAR LT HORIZONTAL STAB PERFORMED PERMANENT REPAIR ON RIB INBOARD LOWER HORIZONTAL FLANGE STAB STA 129.50 AT 35 INCH FROM SPAR LT HORIZONTAL STAB ASPER SRM B737-700 55-10-09-2R-5 REPAIR 5 FIGURE 203

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 70,234 hrs · 41,391 cycles

CRACK VERTICAL ANGLE LOC RIB 129.50 AT FRONT SPAR AT RT HORIZONTAL STABILIZER / REPLACED VERTICAL ANGLE LOC. RIB 129.50 AT FRONT SPAR AT RT HORIZONTAL IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #182A5305 REV.C AND FASTENERS MATERIAL USED BAC1506-4343 PO#2020-128219/1

Part: SKIN — DENTED (RT HORIZ STAB) · airframe 70,234 hrs · 41,391 cycles

LEADING EDGE SKIN HAS A DENT LOCATED AT LE STA 219 AT RT HORIZON TAL STABILIZER (THE DENT MEASURES L=4.3 IN A=2.9 IN Y=0.13 IN A/Y=2 2) PERFORMED PERMANENT REPAIR ON LEADING EDGE SKIN LOCATED AT LE STA 219 AT RT HORIZONTAL STABILIZER IAW SRM B737-700 55-10-01-2R-1

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 70,234 hrs · 41,391 cycles

CRACK INSPAR RIB INBOARD HORIZONTAL FLANGE AT FRONT SPAR LT HORIZONTA L STAB PERFORMED PERMANENT REPAIR ON INSPAR RIB 138.70 INBOARD HORIZONTAL FLANGE AT FRONT SPAR LT HORIZONTAL IAW B737-700 SRM 55-10-09-2R-2 FIGURE 205, SHEET 3 DETAIL B

Part: STIFFENER — DAMAGED (BS 907) · airframe 70,234 hrs · 41,391 cycles

ELONGATED HOLE INTERNAL STRUCTURE VERTICAL STIFFENER LOC WASTE TANK AREA BS 907 AT AFT CARGO COMPARTMENT / REPLACED INTERNAL STRUCTURE VERTICAL STIFFENER LOC WASTE TANK AREA BS 907 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG # 149A8103 SHEET 6 RV

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CRACK GROUND SERVICE DOOR 114AR DOUBLER CUT OUT INTERNAL SKIN AT LOWER FUSELAGE / REPAIRED GROUND SERVICE DOOR 114AR DOUBLER CUT OUT INTERNAL SKIN AT LOWER IAW B737-700 SRM 53-10 -15-2R-4 REPAIR 4 FIGURE 204 SHEET 3; 4 THIS REPAIR IS CATEGORY A

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 70,234 hrs · 41,391 cycles

CRACK VAPOR BARRIER ANGLE LBL 31.83 TO LBL 6.13 AT MAIN WHEEL WELL COMPARTME (1 EA) REPLACED ANGLE (STIFFENER) P/N 111A1301U5 LOC VAPOR BARRIER LBL 31.83 TO LBL 6.13 AT MAIN WHEEL WELL COMPARTMENT DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM FOR CRACK IAW B737-700 SRM 51-10-02, 51-40-05 AND DWG # 111A1001 REV F

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CRACK STRINGER 28R LOCATED BS294.5 EQUIPMENT/ ELECTRONIC COMPARTMENT REPLACED STRINGER 28R LOCATED BS 294.5 EQUIPMENT ELECTRONIC COMPARTMENT IAW SRM B737-700 51-10-02, SRM 51-40-02 AND DRAWING #141A3502 REV:-

Part: GUSSET — CORRODED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CORROSION GUSSET LOCATED BS294.5 TO BS303 BETWEEN STRINGER 21L TO 22L AND WL 172.1 AT EQUIPMENT ELECTRONIC COMPRTMENT REPLACED GUSSET LOCATED BS 294.5 TO BS 303 BETWEEN STRINGER 21L TO 22L AND WL 172.1 AT EQUIPMENT ELECTRONIC COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1350 REV -

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CRACK SUPPORT ANGLE LOCATED BS325.3 TO BS 330 BETWEEN STRINGER 21L EQUIPMENT/ELECTRONIC COMPARTMENT REPLACED SUPPORT ANGLE LOCATED BS 3253 TO BS 330 BETWEEN STRINGER 21L EQUIPMENT ELECTRONIC COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 SRM 51-40-02 AND DRAWING # 191A8190 RE:-

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CRACK SUPPORT ANGLE LOCATED BS312 TO BS320 BETWEEN STRINGER 21L EQUIPMENT/ELECTRONIC COMPARTMENT (1 EA) REPLACED SUPPORT ANGLE LOCATED BS 312 TO BS320 BETWEEN STRINGER 21L EQUIPMENT ELECTRONIC COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 ISRM B737-700 51-40-02 AND DRAWING # 191A8190 RE:-

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 70,234 hrs · 41,391 cycles

TIE CLIP CRACKED AT BS. 277, STR. 10R. / R&R TIE CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CRACK FRAME ON BS 294.5 AT LEVEL STR3L AT FWD GALLEY AREA / PERFORMED REPAIR ON FRAME ON BS 294.5 AT LEVEL STR 3L AT FWD GALLEY AREA IAW EA #1-753-36780 REV IR AND EA # 53-0182-20 REV # 0 FOR INSPECTION REQUIREMENT SEE TLD # T078747

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CRACK WEB - INTERCOSTAL ENTRY DOOR CUTOUT BETWEEN BS294.5 TO BS303.9 STR16L AT FORWARD GALLEY AREA REPLACED WEB INTERCOSTAL ENTRY DOOR CUT OUT BETWEEN BS294 STA BS 303.9 STR16L AT FORWARD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 SRM 51-40-02 AND DRAWING N.141A8180

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 70,234 hrs · 41,391 cycles

CRACK INSPAR RIB LOC STAB STATION 129.50 AT 18 INCH FROM FRONT SPAR L T HORIZONTAL STAB PERFORMED PERMANENT REPAIR LOC INSPAR RIB STAB STA 129.50 AT 18" FROM FRONT SPAR LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09 REPAIR #5

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS727B TO BS847 AND BETWEEN STR25L TO STR26L AND WL155.5 APPROX AFT CARGO COMPARTMENT REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727B TO BS 847 AND BETWEEN STR 25L AND STR 26L AND WL 155.5 APPROX. AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DRAWING # 146A7502 REV.A

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 70,234 hrs · 41,391 cycles

CRACK INSPAR RIB LOCATED STAB STATION 129.50 AT 27 INCH FROM FRONT SP AR LT HORIZONTAL STAB PERFORMED PEERMANENT REPAIR LOC INSPAR RIB STAB STA 129.50+27" FROM FRONT SPAR LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09 REPAIR #5

Part: STRAP — CORRODED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CORROSION ON STRAP LOC BS 540 AT LEVEL STRINGER 10R AND WL 256 AT PASSENGER CABIN REPLACED STRAP LOCATED BS 540 AT LEVEL STRINGER 10R AND WL 256 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-OG-0 AND DWG 144A2101 REV B

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS767 TO BS787 AT LEVEL ST R25R AND WL155.5 APPROX AFT CARGO COMPARTMENT REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS767 TO BS787 AT LEVEL STR 25R AND WL 155.5 APPROX IAW B737-700 SRM 51-40-02-0G-0 & DWG 141A0081 REV C

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS727B TO BS767 AND BETWEEN STR25R TO STR 26R AND WL155.5 APPROX AFT CARGO COMPARTMENT / REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727B TO BS 767 BETWEEN STR 25R TO STR 26R AND WL 155.5 APPROX AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; 51-10-02 AND DRAWING # 146A7500/146A7502 REV B

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CRACK ANGLE - SUPPORT LOCATED BS867 AND BETWEEN STR26L TO STR27L AFT CARGO COMPARTMENT (1 EA) / REPLACED ANGLE-SUPPORT LOCATED BS867 AND BETWEEN STR26L TO STR27L AFT CARGO COMPARTMENT ASPER SRM 51-40-02; 51-10-02 AND DWG #149A8102 REV

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 70,234 hrs · 41,391 cycles

CRACK PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH AT PASSENGER CABIN (5EA) / REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH AT PASSENGER CABIN (5 EA) IAW B737-700 AMM 33-51-15-400-802 AND DWG 33500007 REV 2

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 70,234 hrs · 41,391 cycles

CRACK LEADING EDGE RIB LE STA 78.29 ON ACCESS PANEL 341B AT RT HORIZO NTAL STABILIZER / REPLACED LEADING EDGE RIB LOC. STA 78.29 ON ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 186A1301; DWG 186A1001

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 70,234 hrs · 41,391 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 32 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 120.30 AT 32 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ASPER SRM B737-700 55-10-09 -2R-5 REPAIR 5

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 70,234 hrs · 41,391 cycles

CRACK PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AT PASSENGER CABIN (5EA) / REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AT PASSENGER CABIN (5 EA) IAW B737-700 AMM 33-51-15-400-802 AND DWG 33500007 REV 2

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 70,234 hrs · 41,391 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ASPER SRM B737-700 55-10-09 -2R-5 REPAIR 5

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 70,234 hrs · 41,391 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FRONT SPAR AT RT HORIZONTAL STABILIZER PERFORMED PERMANENT REPAIR LOC INSPAR RIB STAB STA 120.30 AT 19" FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09 REPAIR #4

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CRACK ANGLE - SUPPORT LOCATED AT LEVEL STR26L AND BS440,BS460 AND BS50 0C FORWARD CARGO COMPARTMENT (3 EA) REPLACED ANGLE SUPPORT LOCATED AT LEVEL STR 26L AND BS 440, BS 460 AND BS 500C FORWARD CARGO COMPARTMENT IAW B737-700 SRM 51-10-2 PARAGRAPH 9 SRM 51-40-02 AND DRAWING 143A7505 SHEET 5 REV B (ANGLE 3EA)

Part: STRAP — CRACKED (FLOOR PANEL) · airframe 70,234 hrs · 41,391 cycles

CRACK STRAP FLOOR PANEL 140AF LOCATED BS727 BETWEEN STR25L TO STR25R A T AFT CARGO COMPARTMENT REPLACED STRAP FLOOR PANEL 140AF LOCATED BS727 BETWEEN STR25L TO STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02

Part: GUSSET — DAMAGED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

ELONGATED HOLE GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED BS500D AND STR.19L FWD CARGO COMPARTMENT IAW EA NO.1-753-36789 REV.1 AND EA #53-0214-20 REV.1

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CRACK ANGLE - SUPPORT LOCATED BS400 AT LEVEL STR26L FORWARD CARGO COMPARTMENT REPLACED ANGLE - SUPPORT LOCATED BS400 AT LEVEL STR26L FORWARD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9, SRM 51-40-02 AND DRAWING NO. 143A7505 SHEET 2 REV. B

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,234 hrs · 41,391 cycles

CORROSION STRINGER 27R LOCATED BS540 AND WL 148 FWD CARGO COMPARTMENT REPAIRED STRINGER 27R LOCATED BTW BS 500D AND BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1

Part: BARRIER — CRACKED (LT MLG WW) · airframe 70,234 hrs · 41,391 cycles

CRACK VAPOR BARRIER BS 663 AT LBL 10 AT MAIN WHEEL WELL COMPARTMENT REPAIRED VAPOR BARRIER BS 663 AT LBL 10 MAIN WHEEL WELL COMPARTMENT ASPER B737-700 SRM 51-70-04-2R-10 REP 10 TOOL USED CALIPER P/N 700-113-10 S/N 0026569 DUE DATE 16-JAN-21 SCALE P/N CL5000 S/N AE-39882 DUE DATE 05-NOV-20 HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 02-DEC-20

Part: ACCESS PANEL — DELAMINATED (BODY FAIRING) · airframe 70,234 hrs · 41,391 cycles

DELAMINATED ACCESS PANEL 191CL BODY FAIRING AT LOWER FUSELAGE / REPAIRED ACCESS PANEL 191CL BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-04-2R-2 REP 2. TOOL USED CALIPER PN 700-113-10 SN 0008567 DUE DATE 04-FEB-21; HOT BONDER PN HCS9200B SN 18165044 DUE DATE 02-DEC-20; SCALE PN CL5000 SN AE-39882 DUE DATE 05-NOV-20; SCALE PN CL5000 SN AE-407340 DUE DATE 03-JUL-20

Part: PANEL — ELONGATED (FUSELAGE) · airframe 69,069 hrs · 40,655 cycles

PNL 193B HAS SEVERAL FASTENER HOLES THAT ARE ELONGATED. NOTED ON PNL AND TABLE 1 OF EO I14108 / REMOVED AND REPLACED PNL 193B PER M/M 53-51-21

Part: LENS — FADED (EMERGENCY LIGHT) · airframe 67,987 hrs · 39,943 cycles

R/H EMERGENCY EXIT LIGHT LENS YELLOWED. R&R LENS PER AMM.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,833 hrs · 39,839 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD SIDE CORRODED. / REPAIRED FITTING PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,833 hrs · 39,839 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD BORE CORRODED. / REPAIRED FITTING PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,833 hrs · 39,839 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD BORE CORRODED. / REPAIRED FITTING PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,833 hrs · 39,839 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD BORE CORRODED. / REPAIRED FITTING PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,833 hrs · 39,839 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,833 hrs · 39,839 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD SIDE CORRODED. / REPAIRED FITTING PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,833 hrs · 39,839 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,833 hrs · 39,839 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD BORE CORRODED. / REPAIRED FITTING PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,833 hrs · 39,839 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD SIDE CORRODED. / REPAIRED FITTING PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,833 hrs · 39,839 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,833 hrs · 39,839 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: BATTERY — FAILED (CABIN) · airframe 65,859 hrs · 38,538 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 65,859 hrs · 38,538 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 65,859 hrs · 38,538 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PER AMM.

Part: LENS — MISSING (CABIN) · airframe 65,508 hrs · 38,302 cycles

LT OVERHEAD BIN EMERGENCY EXIT LIGHT MISSING CLEAR LENS AT ROW 9. INSTALLED LENS IAW AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,813 hrs · 37,837 cycles

R1 DOOR ESCAPE SLIDE OUT OF ADJUST. READJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (RT SPOILER) · airframe 64,397 hrs · 37,585 cycles

RT WING NR 10 SPOILER UPPER SKIN CRACKED. R&R NR 10 SPOILER IAW MM.

Part: RETAINING CLIP — LOOSE (R2 DOOR) · airframe 64,374 hrs · 37,571 cycles

R2 DOOR GIRT BAR RETAINER AFT CLIPS LOOSE ON COMPARTMENT DOOR. REPAIRED CLIP IAW AMM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 64,374 hrs · 37,571 cycles

R1 DOOR GIRT BAR BRACKETS LOOSE. REPAIRED RETAINER CLIPS IAW AMM.

Part: RETAINING CLIP — DAMAGED (L1 DOOR) · airframe 64,374 hrs · 37,571 cycles

L1 DOOR GIRT BAR BRACKETS LOOSE. REPAIRED RETAINER CLIPS IAW AMM.

Part: RETAINING CLIP — LOOSE (L2 DOOR) · airframe 64,374 hrs · 37,571 cycles

L2 DOOR GIRT BAR RETAINER AFT CLIPS LOOSE ON COMPARTMENT DOOR. REPAIRED CLIP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,712 hrs · 37,161 cycles

LEFT EMERGENCY LIGHT ON STOW BIN INOPERATIVE, BETWEEN ROWS 6 & 7. R & R THE LIGHT IAW AMM.

Part: SPLICE — CRACKED (AFT CARGO COMPT) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO PIT PANEL SPLICE AT STA 727D CRACKED / REMOVED AND REPLACED AFT CAARGO IT PANEL SPLICE AT BS727D IAW SRM 51-40-02-0G-0 & BOEING DWG 146A7500 REV A

Part: CARGO TRACK — CORRODED (BS 727-887) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO BAY CAROG TRACK CORRODED BETWEEN BS 727+4 TO 887, RBL 13.8. R & R CARGO TRACK IAW SRM AND DWG.

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

CORROSION FOUND ON VERTICAL WEB AT AFT CARGO THRESHOLD. STA 795-847 RBL 19. / EVALUATED CORROSION ON AFT CARGO THRESHOLD STA 795-847 RBL19 FOUND 100% MATERIAL LOSS OUT OF LIJMITS IAW B737 SRM 53-60-15-1A-1 REMOVED & REPLACED VERTICAL WEB IAW B737 SRM 51-40-02-0G-1 & BOEING DWG 146A8123 REV A & 146A8120 REV A. ATAG R50989

Part: TRUNNION — CORRODED (RT MLG) · airframe 63,712 hrs · 37,161 cycles

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

Part: BRACKET — ELONGATED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO TRACK ATTACH BRACKET AT STA 887 RBL 13.5 HAS OUT OF ROUND HOLES / REMOVED TRACK ATTACH BRACKET AND INSTALLED NEW ATTACH BRACKET STA 787 RBL 13.5 IAW SRM 51-40-02-0G-0 STEP 4B AND DWG#146A1262REV-.

Part: BRACKET — ELONGATED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO TRACK ATTACH BRACKET AT STA 807 RBL 13.5 HAS HOLES OUT OF ROUND / FABRICATED AND INSTALLED AFT CARGO PIT ATTACH BRACKET AT STA 807 RBL 13.5 I/A/W DWG 146A1310; AND APPLIED CONVERSION COATING AND PRIMER I/A/W EA 180097 REV IR AND S/W EA 1-753-32296 REV IR

Part: BRACKET — ELONGATED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO TRACK ATTACH BRACKET AT STA 855 RBL 13.5 HAS OUT OF ROUND HOLES / REMOVED TRACK ATTACH BRACKET AND INSTALLED NEW TRACK ATTACH BRACKET STA 855 RBL 13.5 IAW SRM 51-40-02-0G-0 STEP 4B AND DWG#146A8232 REV-. TAG RS1045

Part: BRACKET — ELONGATED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO TRACK ATTACH BRACKET AT STA 827 RBL 13.5 HAS OUT OF ROUND HOLES / REMOVED TRACK ATTACH BRACKET AND INSTALLED NEW TRACK ATTACH BRACKET STA 827 RBL 13.5 IAW SRM 51-40-02-0G-0 STEP 4B1 AND DWG 146A1280 REV A.

Part: BRACKET — ELONGATED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO TRACK ATTACH BRACKET AT STA 867 RBL 13.5 HAS OUT OF ROUND HOLES / REMOVED TAIL ATTACH BRACKET AND ISNATLLED NEW TRACK ATTACH BRACKET STA 867 RBL 13.5 IAW SRM 51-40-02-0G-0STEP 4B AND DWG#146A1282 REVA. TAG RS1044

Part: BRACKET — ELONGATED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO CARGO RAIL ATTACH BRACKET AT STA 887 RBL 13.5 HAS OUT OF ROUND HOLES / REMOVED TAIL ATTACH BRACKET AND INSTALLED NEW RAIL ATTACH BRACKET STA 887 RBL 13.5 IAW SRM 51-40-02-0G-0 STEP 4B1 AND DWG# 147A3287 REV- AND DWG#147A0060 REV-. TAG RS1043

Part: SEAL — CRACKED (MAIN CABIN) · airframe 63,712 hrs · 37,161 cycles

FWD ENTRY DOOR FWD LOWER SEAL LOCATOR IS CRACKED / REMOVED AND INSTALLED NEW FWD ENTRY DOOR FWD LOWER SEAL LOCATOR I/A/W CMM 52-16-12

Part: TRANSITION PANEL — CORRODED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO COMPARTMENT FLOOR PANEL TRANSITION STRIP AT STA 767 IS CORRODED / EVALUATED TRANSITION STRIP @STA 767; NO WRITTEN LIMITS; REPLACED W/NEW PART 146A9401-4 IAW BOEING DWG 146A9401 REV C

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 63,712 hrs · 37,161 cycles

PASSENGER CABIN SEAT TRACK STATION 712; RBL 45; IS CORRODED INSIDE THE SEAT TRACK CHANNEL AND ON TOP OF THE CROWN. / REPAIRED SEAT TRACK SECTION AT BS 708-BS727B RBL 45' IAW SRM 53-00-52-2R-3 REPAIR 3 ON NON ROUTINE X692886

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 63,712 hrs · 37,161 cycles

FORWARD CABIN FLOOR PANEL 221GF UPPER SURFACE HAS DAMAGED FIBERS FROM TAPE REMOVAL / REPAIRED FWD CABIN FLOOR PANEL 221 GF UPPER SURFAE IAW B737 SRM 53-00-50-2R-1 REV 63. CURED IN OVEN FOR 1 HR AT 150'; IN AT 9:30AM-OUT AT 10:30 AM (OVEN E0-01 EXP 4/23/18)

Part: SEAT TRACK — CORRODED (BS 695-707) · airframe 63,712 hrs · 37,161 cycles

SEAT TRACK CORRODED BETWEEN BS 695 TO 707, RBL 45. REPAIRED THE SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 63,712 hrs · 37,161 cycles

PASSENGER CABIN SEAT TRACK STATION 395; RBL 24; IS CORRODED INSIDE THE SEAT TRACK CHANNEL AND ON TOP OF THE CROWN. / BLENDED CORROSION PASSENGER CABIN SEAT TRACK BS 395 RBL 24 IAW B737-700 SRM 53-00-52-1D-1 STEP 2.A. EVALUATED MATERIAL LOSS. MAX LOSS .045' ALLOWABLW .040' FOUND TO BE OUT OF LIMITS IAW B 737-700 SRM 53-00-52-1D-1 FIG 103. REMOVED AND REPLACED SEAT TRACK FROM BS 360+6 TO BS 480 RBL 24 IAW BOEING DWG # 143A5300 REV - AND B737-700 AMM 20-50-11-910-801 AND APPLIED C.I.C. IAW B737-700 AMM 51-21-91

Part: STUB FRAME — CRACKED (BS 295) · airframe 63,712 hrs · 37,161 cycles

R1 DOORWAY STUB FRAME CRACKED AT BS 295, STRINGER 17R. R & R THE STUB FRAME IAW SRM.

Part: BEAM — CRACKED (MAIN CABIN) · airframe 63,712 hrs · 37,161 cycles

R1 DOOR; BEAM BELOW HANDLE BOX IS CRACKED AT FWD I/B MOST UPPER FASTENER HOLE / REMOVED AND REPLACED R1 DOOR BEAM BELOW HANDLE BOX P/N 141A6536-20 IAW BOEING DWG#141A6516 REV D AND B737-700 SRM 51-40-02

Part: INTERCOSTAL — CORRODED (BS 561) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO BAY INTERCOSTAL CORRODED, BS 561, BETWEEN STRINGERS 23L TO 25L. R & R THE INTERCOSTAL IAW DWG.

Part: LIGHT — BROKEN (BS 616) · airframe 63,712 hrs · 37,161 cycles

EMERGENCY EXIT LIGHT FIXTURE ATTACH MOUNTS BROKEN AT BS 616+11. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: FRAME — CORRODED (BS 303) · airframe 63,712 hrs · 37,161 cycles

L1 DOORWAY FUSELAGE FRAME CORRODED AT BS 303.9, LBL 56. REPAIRED THE FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,712 hrs · 37,161 cycles

R1 CREASE BEAM CORRODED ON UPPER SURFACE. R & R THE R1 CREASE BEAM IAW SRM AND DWG.

Part: PANEL — CRACKED (LT WING) · airframe 63,712 hrs · 37,161 cycles

LH WING LOWER SURF PANEL 661CB; COMPOSITE MATERIAL UNDER COUNTERSINKS CRACKED; AND PULLED THROUGH. / EVALUATED; CLEANED; PREPPED AND REPAIRED DAMAGED FASTENER HOLES ON L/H WING PANEL 661CB IAW B737 SRM 51-70-04-2R-9; PAR 4 (A-0) REV 63

Part: WEB — CORRODED (BS 1016) · airframe 63,712 hrs · 37,161 cycles

AFT WET AREA WEB AT THE LAVATORY PIPE CUTOUT, CORRODED AT BS 1016+2, BETWEEN LBL 9 TO LBL 11. R & R THE WEB IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (MAIN CABIN) · airframe 63,712 hrs · 37,161 cycles

FWD WET AREA; FLOORBOARD SUPPORT ANGLE CRACKED AT 1EA HOLE 312 + 9' LBL 45';MARKED. / REMOVED AND REPLACED 1EA. INTERCOSTAL @ STA. 312+9' LBL 45 PER DWG# 141A 5400 SHEET 4 AND SRM 51-40-02-0G-0

Part: SUPPORT ANGLE — CORRODED (BS 312) · airframe 63,712 hrs · 37,161 cycles

FORWARD WET AREA, L1 DOOR CREASE BEAM THRESHOLD SUPPORT ANGLE CORRODED AT BS 312, LBL 58. R & R THE SUPPORT ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,712 hrs · 37,161 cycles

FORWARD WET AREA FLOOR BOARD SUPPORT ANGLE CRACKED BETWEEN BS 277 TO BS 294.5, RBL 1. R&R INTERCOSTAL PER DWG AND SRM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 63,712 hrs · 37,161 cycles

FORWARD WET AREA FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, RBL 33. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (MAIN CABIN) · airframe 63,712 hrs · 37,161 cycles

AFT WET AREA FLOORBOARD SUPPORT STIFFNER CORRODED UPPER SURFACE AT BS 947 TO BS 967 RBL 45. MARKED. / REMOVED CORROSION FLOOR BOARD SUPPORT STIFFENER AND OUT OF LIMITS MATERIAL ORIGINAL .94' REMAINING .080'; LOSS .014'; AND REMOVED STIFFENER; LOCATED; DRILLED AND INSTALLED NEW STIFFENER AND APPLIED CIC AREA IAW B737-700 AMM 51-40-02-0G-0; 51-40-05-0G-0; 51-10-02-0G-0; 53-70-51-1A-1 AMM 51-21-91 DWG: 147A5760 REV: -

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,712 hrs · 37,161 cycles

R1 CREASE BEAM OTBD ATTACH ANGLE CORRODED ON THE UPPER SURFACE. R & R THE CREASE BEAM IAW SRM AND DWG.

Part: WEB — CORRODED (MAIN CABIN) · airframe 63,712 hrs · 37,161 cycles

AFT WET AREA WEB STRAP AT BS 1016 + 2' LBL 3' CORRODED UPPER SURFACE. MARKED. N / REPLACED STRAP AT AFT WEB AREA WEB AT BS 1016 + 15 LBL - 3 AND APPLIED CIC AREA IAW B737-700 SRM 51-40-02-0G-0; 51-40-05-0G-0; 51-10-02-0G-0; 53-70-51-1A-1 AMM 51-21-91-620-802 DWG: 147A5600 REV: H TAG: A13731

Part: TRUNNION — CORRODED (RT MLG) · airframe 63,712 hrs · 37,161 cycles

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

Part: CREASE BEAM — CORRODED (BS 294-340) · airframe 63,712 hrs · 37,161 cycles

L1 CREASE BEAM CORRODED BETWEEN BS 294.5 TO 340. R & R THE CREASE BEAM IAW DWG.

Part: PANEL — CRACKED (LT WING) · airframe 63,712 hrs · 37,161 cycles

LH WING LOWER SURF PANEL 661AB; COMPOSITE MATERIAL UNDER COUNTERSINKS CRACKED; AND PULLED THROUGH. / EVALUATED; CLEANED; PREPPED AND REPAIRED DAMAGED FASTENER HOLES ON L/H WING PANEL 661AB IAW B737 SRM 51-70-04-2R-9; PAR 4 (A-0) REV 63

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,712 hrs · 37,161 cycles

R2 CREASE BEAM CORRODED. R & R THE CREASE BEAM IAW SRM, AMM, AND DWG.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 63,712 hrs · 37,161 cycles

LH HORIZ STAB LWR GAP COVER; 333AB SLIDING SEAL WORN THRU. CRACKED AT CORNER. / REMOVED & REPLACED SLIDING SEAL IAW B737-700 SRM 51-40-02-0-0G / AIPC 55-10-52-01H. (333AB) ATAG # WN5581

Part: SUPPORT ANGLE — CORRODED (BS 312-344) · airframe 63,712 hrs · 37,161 cycles

L1 DOOR CREASE BEAM CENTER THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 312 TO 344, LBL 61. R & R THE SUPPORT ANGLE IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO COMPARTMENT FLOOR RAIL CORRODED AT BS 767+5, RBL 8. REPAIRED FLOOR RAIL IAW SRM AND EA.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO BAY, CARGO TRACK CORRODED AT BS 767+5, LBL 3. REPAIRED CARGO TRACK IAW EA.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO COMPARTMENT BETWEEN STA 727 +5' AND 727E + 11' R/H/S Z ANGLE IS CORRODED TOP AND BOTTOM SURFACES AS MARKED / REMOVED CORROSION AT STA 727+5 AND 727E+11 R/H 'Z' ANGLE I/A/W SRM SRM 51-10-02-06 VERIFIED MATERIAL LOSS ORIG .040 LOSS .008 REMAINING .032 OUT OF LIMITS I/A/W SRM 53-00-53-1A-2; REMOVAL AND INSTALLED NEW 'Z' ANGLE ON W/O X692555

Part: SUPPORT BRACKET — CRACKED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO COMPARTMENT STA 867 -2' LBL 11 AREA; LAV TANK BULKHEAD FRAME SUPPORT BRACKET IS CRACKED ON INSIDE AS MARKED / REMOVED AND REPLACED SUPPORT BRACKET PN 149A8109-114 AT AFT CARGO STA 867 - 2' LBL 11 IAW SRM 51-40-02-0G-0 AND DWG 149A8102 REV - A53652

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO COMPARTMENT STA 887 TRANSITION NUT PLATE STRIP FOR CARGO BAY FLOOR PNL'S; NUTPLATES ON BOTTOM OF STRIP ARE CORRODED THE LENGTH OF STRIP / EVALUATED CORROSION;FOUND NO LIMITS; PART 100% MATERIAL LOSS IAW SRM 51-10-02-0G-0 PARA 9 RECEIVED A NEW TRANSITION FLOOR SUPPORT @ STA 887 IAW DWG #146A9401 SHEET 12 REV A INSTALLED 1 EA NEW TRANSITION FLOOR SUPPORT IAW DW#146A9401 SHEET 12 REV A

Part: FLOOR SUPPORT — CORRODED (BS 727D) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO BAY, FLOOR SUPPORT CORRODED BETWEEN BS 727D+5 TO 727D-7, RBL 8.50. REPAIRED FLOOR SUPPORT IAW EA.

Part: CARGO TRACK — CORRODED (BS 727D) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO BAY, CARGO TRACK CORRODED AT BS 727D+5, LBL 8. REPAIRED CARGO TRACK IAW EA.

Part: CARGO TRACK — CORRODED (BS 727D) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO BAY, CARGO TRACK CORRODED AT BS 727D+5, RBL 3. REPAIRED THE CARGO TRACK IAW SRM AND EA.

Part: INTERCOSTAL — CORRODED (BS 849.5) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO BAY INTERCOSTAL CORRODED AT BS 849.5, BETWEEN STRINGERS 23L TO 25L. R & R THE INTERCOSTAL IAW DWG.

Part: CARGO TRACK — CORRODED (BS 727D) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO BAY, CARGO TRACK CORRODED AT BS 727D+5, LBL 2.50. REPAIRED THE CARGO TRACK IAW EA.

Part: ANGLE — CORRODED (BS 727E-767) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO BAY RT ZEE ANGLE CORRODED BETWEEN BS 727E+11 TO 767. R & R THE ZEE ANGLE IAW SRM.

Part: DOUBLER — CORRODED (BS 847) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO BAY INNER DOUBLER OF THE LAVATORY SERVICE PAN CORRODED BETWEEN BS 847 TO 867, STRINGERS 23L TO 25L. R & R THE DOUBLER IAW DWG.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO BAY, CARGO TRACK CORRODED AT BS 767+5, RBL 3. REPAIRED IAW EA.

Part: FLOOR MAT — CORRODED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO COMPARTMENT BETWEEN STA 767 AND 787+6' FWD FLOOR SHIELD IS CORRODED TOP AND BOTTOM SURFACES AS MARKED / VALUATED CORROSION ON AFT CARGO COMPARTMENT SHIELD STA 767 - 787 + 6 FOUND TO BE 100% OUT OF LIMITS IAW B737 SRM 53-00-53-1A-2. REMOVED & REPLACED WITH NEW SHIELD IAW B737 SRM 51-40-02-0G-0 & BOEING DWG 146A0081 REV C WN 8363

Part: FLOORBEAM — CORRODED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO COMPARTMENT BETWEEN STA 787+7' AND 827 RBL 14; FLOOR TRACK TOP SURFACE AROUND NUTPLATE HOLES IS CORRODED AS MARKED / CARGO TRACK FROM STA 727+4 TO 887 RBL 13.8 WILL BE REPLACED ON N/R X693058 TAG: RS10B; A10219

Part: TIE DOWN — CORRODED (AFT CARGO BAY) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO FWD AND AFT CARGO NET TIE DOWN PLATES ARE CORRODED / EVLAUATED AFT CARGO FWD AFT TIE DOWN PLATES; FOUND NO WRITTEN LIMITS; PARTS OUT OF LIMITS; REPLACED W/NEW P/N 453A2611-24 453A2611-1 IAW BOEING DWG 453A2600 REV D

Part: WEB — CORRODED (BS 787) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO BAY FLOOR WEB CORRODED AT BS. 787+8, RBL 19. R & R THE WEB IAW SRM & DWG.

Part: PLATE — CRACKED (LT WING) · airframe 63,712 hrs · 37,161 cycles

LEFT WING WAFFLE PLATE CRACKED INBOARD OF SAIL TAIL COMMON TO THE AFT SPAR. R & R THE PLATE IAW SRM & DWG.

Part: GUSSET — CRACKED (FWD CARGO LH) · airframe 63,712 hrs · 37,161 cycles

FORWARD CARGO BAY AFT BULKHEAD GUSSET AT STR19L STA 500D IS CRACKED. / REMOVED AND REPLACED 1 EA -6 GUSSSET @ STA 500D STR. 19L PER DWG# 143A7902 AND SRM 51-40-02-0G-0 CIC'ED IAW AMM 51-21-91

Part: BRACKET — CRACKED (LEFT WING) · airframe 63,712 hrs · 37,161 cycles

LEFT WING; SEAL RETAINER COMMON TO DEFLECTOR RIB; OTBRD BRACKET OF SEAL RETAINER IS CRACKED / REMOVED AND REPLACED NEW LEFT WING SEAL RETAINER COMMON TO DEFLECTOR RIB; OTBRD BRACKET OF SEAL RETAINER IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A6200 REV :1 ATAG #A06504

Part: RETAINER — CRACKED (RIGHT WING) · airframe 63,712 hrs · 37,161 cycles

RIGHT WING; DEFLECTOR PANEL; SEAL RETAINER IS CRACKED AT UPPER; OTBRD AFT SIDE LOCATION / REPLACED SEAL RETAINER AT R/H WING; DEFLECTOR PANEL IAW B737-700 SRM 51-40-02-0G-0 DWG: 115A2512 REV: B AMM 51-21-91-620-802 TAG: NX1517

Part: BULKHEAD WEB — CRACKED · airframe 63,712 hrs · 37,161 cycles

PRESSURE BULHEAD WEB CRACKED AT BS 668, RBL 40.5. REPAIRED THE BULKHEAD WEB IAW EA.

Part: GUSSET — CRACKED (FWD CARGO RH) · airframe 63,712 hrs · 37,161 cycles

FORWARD CARGO BAY AFT BULKHEAD GUSSET AT STR19R STA 500D IS CRACKED. / REMOVED & REPLACED GUSSET AT FWD CARGO AFT BULKHEAD ATR 19R STA 500D A-TAG WN0758

Part: ANGLE — CRACKED (FWD CARGO RH) · airframe 63,712 hrs · 37,161 cycles

FORWARD CARGO BAY STA400 TO STA420 RBL26 Z ANGLE CRACKED. / REPLACED Z-ANGLE AT FWD CARGO BAY STA:400 TO 420 RBL26 AND APPLIED CIC AREA IAW B737-700 SRM 51-40-02-0G-0; 51-40-05-0G-0; 53-00-93-2R-6; AMM 51-21-72-370-804; 51-21-41-370-803; 51-21-91-620-802 TAG :A06297

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO PIT FLOOR LONGERON STRAP CORRODED BETWEEN BS 807+9 TO BS 827+11, RBL 19. R&R STRAP IAW DWG.

Part: ANGLE — CORRODED (BS 500A-500D) · airframe 63,712 hrs · 37,161 cycles

FORWARD CARGO BAY ZEE ANGLE CORRODED BETWEEN BS 500A TO 500D, RBL 26. R & R THE ANGLE IAW SRM.

Part: ANGLE — CORRODED (FWD CARGO COMPT) · airframe 63,712 hrs · 37,161 cycles

FORWARD CARGO BAY STA 500D LBL26 TO RBL26 AFT BULKHEAD ATTACH LOWER ANGLE CORRODED. / EVALUATED STA. 500D BULKHEAD LOWER ATTACH ANGLE; NO PUBLISHED SRM LIMITS. REMOVED LOWER ATTACH ANGLE IAW B737 SRM 51-40-02-0G-0; PAR 7D; VERIFIED NEW RAIL ASSY AS P/N 143A9485-35. PER BOEING DWG NO. 143A9485 REV: B; AND BOEING PL 143A 9485 REV: F. LOCATED AND DRILLED NEW PART IAW B737 SRM 51-40-05-0G-0; COUNTERSUNK HOLES IAW B737 SRM 51-40-02-0G-0; AND BOEING DWG. NO 143A0495 REV: B. APPLIED CIC IAW B737-700 AMM 51-21-91-620-802. A-TAG # WN0849

Part: SHIELD — CRACKED (FWD CARGO RH) · airframe 63,712 hrs · 37,161 cycles

FORWARD CARGO BAY DOOR AFT SHIELD CRACKED. / REPLACED SHIELD AT FWD PIT BAY DOOR AFT; R/H SIDE APPLIED CIC AREA IAW B737-700 SRM 51-40-02-0G-0; 51-40-05-0G-0; AMM 51-21-91-620-802 TAG: WN6196

Part: RETAINER — CRACKED (RIGHT WING) · airframe 63,712 hrs · 37,161 cycles

RIGHT WING; DEFLECTOR PANEL CENTER BULB SEAL RETAINER ON FWD SIDE IS CRACKED AT LWR FASTENER / REMOVED AND REPLACED RIGHT WING; DEFLECTOR PANEL CENTER BULB SEAL RETAINER IAW SRM 51-40-02; 51-40-05 AND DWG 115A2930 REV- ATAG A03376

Part: RETAINER — CRACKED (RIGHT WING) · airframe 63,712 hrs · 37,161 cycles

RIGHT WING; DEFLECTOR PANEL SEAL RETAINER OTBRD END HAS CRACK AT LWR FASTENER / REMOVED AND REPLACED CRACKED RT WING DEFLECTOR PANEL OUTBOARD SEAL RETAINER BRACKET IAW SRM 51-40-02-0G-0 AND BOING DWG 115A6200 REV A

Part: RIB — CRACKED (RT WING) · airframe 63,712 hrs · 37,161 cycles

RIGHT WING DEFLECTOR PANEL OTBD RIB CRACKED. R & R THE RIB IAW SRM & DWG.

Part: RIB — ELONGATED (LEFT WING) · airframe 63,712 hrs · 37,161 cycles

LEFT WING; T/E DEFLECTOR PANEL AFT OF SAIL TAIL; AFT SUPPORT RIB FASTENER HOLES ARE ELONGATED / REMOVED AND REPLACED LEFT WING T/E DEFLECTOR PANEL AFT OF SAIL TAIL;AFT SUPPORT RIB IAW B737-700 SRM 51-40-02;DWG 115A2982 RE:C; 115A2930 REV:- ATAG A06295

Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 63,712 hrs · 37,161 cycles

AAI INSPECTION: AFT CARGO LOWER SILL WEB NEEDS REMOVED TO ACCESS REPAIR AT STA 798-817 FOR AGING ACFT INSPECTION UPON REMOVAL FOUND CORROSION ON UPPER SURFACE / REMOVED CORROSION ON UPPER SURFACE OF AFT CARGO LOWER SILL WEB ORIGINAL THICKNESS .045' MATERIAL REMOVED .006' ; MATERIAL REMAINING .039' MATERIAL IS OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVED AND REPLACED AFT CARGO LOWER SILL WEB IAW SRM 51-40-02-0G-0 & BOEING DWG 146A8123 ATAG#WN7393

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO PIT FWD SCUFF PLATE CRACKED / CRACKED AFT CARGO PIT FWD SCUFF PLATE REPAIRED WITH WELD REPAIR IAW EA 1-A53-2076 REV 11 ON BACK SHOP WORK ORDER 36955-1600-0002

Part: BRACKET — CRACKED (RT WING) · airframe 63,712 hrs · 37,161 cycles

RT WING FAIRING SUPPORT BRACKET CRACKED AT LEADING EDGE TO WING TO BODY BRACE, BS 500D. R&R BRACKET IAW DWG AND SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 63,712 hrs · 37,161 cycles

AFT CARGO PIT AFT SCUFF PLATE CRACKED / CRACKED AFT CARGO PIT AFT SCUFF PLATE REPAIRED WITH WELD REPAIR IAW EA 1-A53-2076 REV 11 WORK ACCOMPLISHED ON BACK SHOP W/O 36955-1600-0001

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 63,712 hrs · 37,161 cycles

FWD CARGO PIT FWD SCUFF PLATE CRACKED / ACCOMPLISHED SW EA 1-A53-2076 REV II

Part: BULKHEAD — CRACKED (BS 663) · airframe 63,712 hrs · 37,161 cycles

RIGHT AIR CONDITION BAY BULKHEAD CRACKED AT BS 663. REPAIRED THE BULKHEAD IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 63,712 hrs · 37,161 cycles

RIGHT AIR CONDITION BAY BULKHEAD ANGLE CRACKED AT BS 663. R & R THE ANGLE IAW SRM AND DWG.

Part: FLOOR PANEL — CRACKED (FWD CARGO COMPT) · airframe 63,712 hrs · 37,161 cycles

FWD CARGO FLOOR PANEL 120BF HAS MULTIPLE DENTS AND A CRACK / EVALUATED CARGO FLOOR PANEL 120BF FOUND CRACKS IN DENT 100% THROUGH MATERIAL IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 SEE WORK CARD JPANEL-12-CLOSE FOR INSTALL ATAG# WN8953

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 63,712 hrs · 37,161 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL; STATION 663; ''U'' SHAPED STIFFENER ABOVE THE AIR CONDITION PACK EXHAUST INBOARD ANGLE IS CRACKED. / REMOVED CRACKED U-SHAPED STIFFENER AND INSTALLED NEW U-SHAPE STIFFENER STA 663 RBL 25-RBL15 ALL IAW SRM 51-40-02-0G-0 STEP 4B1 AND DWG #111A1512 REV- AND DWG #111A1000 REV B.__ATG#NX1508

Part: ANGLE — CRACKED (BS 663) · airframe 63,712 hrs · 37,161 cycles

R/H AIR CONDITION BAY OUTBOARD OF THE RT KEEL BEAM WEB L ANGLE CRACKED AT BS. 663. REPAIRED THE ANGLE IAW EA.

Part: SIGN — MISSING (CABIN) · airframe 62,751 hrs · 36,541 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROW. R&R SIGN PER AMM.

Part: LENS — MISSING (CABIN) · airframe 62,641 hrs · 36,466 cycles

RT EMERGENCY EXIT LIGHT COVER LENS MISSING AT ROW 12. INSTALLED LENS PER AMM.

Part: BEAM — ELONGATED (RIGHT WING) · airframe 61,743 hrs · 35,907 cycles

RT WING UPPER TRAILING EDGE SKIN PANEL OB SUPPORT BEAM BOLT HOLES TO DEFLECTION CONTROL TAB ARE ELONGATED. / REPAIRED PER SRM.57-51-02

Part: LINE — OUT OF POSITION (LT OVERWING DOOR) · airframe 61,743 hrs · 35,907 cycles

LEFT OVERWING EMERGENCY EXIT DOOR LIFE LINE OUT OF POSITION. REPOSITIONED THE LIFE LINE IAW AMM.

Part: FLAP — CRACKED (LH OUTBD AFT FLA) · airframe 61,743 hrs · 35,907 cycles

L/H OUTBOARD AFT FLAP; 2ND FROM INBD TRACK CUTOUT; THE LOWER CUTOUT FILLER IS BROKEN OUT AND CRACKED. / REMOVED AND REPLACED PER SRM 51-40-02.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 60,844 hrs · 35,359 cycles

CENTER WING SECTION REAR SPAR VAPOR BARRIER CRACKED AT BS 663, BETWEEN RBL 6.15 TO RBL 15.54. REPAIRED PER EA.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 59,728 hrs · 34,710 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R & R THE BATTERY IAW DWG AND AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,728 hrs · 34,710 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER DWG AND AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,728 hrs · 34,710 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PER DWG AND AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 57,889 hrs · 33,647 cycles

R1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 57,669 hrs · 33,526 cycles

AFT AISLE OVERHEAD CEILING EMER EXIT SIGN LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,602 hrs · 33,481 cycles

M10672 EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 57,602 hrs · 33,481 cycles

R1 DOOR EMER EVAC SLIDE GIRT OUT OF ADJUSTMENT. ADJUSTED SLIDE GIRT IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,602 hrs · 33,481 cycles

M10670 EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 57,358 hrs · 33,341 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,302 hrs · 33,305 cycles

LEFT OVERWING EXIT UPPER SURROUND PANEL, FWD EMER LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

LEFT LOWER FRAME CRACKED, AT BS 727, WL 200 IN THE OPEN FASTENER HOLE, 5TH FROM THE OTBD SIDE. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

RIGHT LOWER FRAME CRACKED AT BS 272, WL 200. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

FUSELAGE FRAME CRACKED AT BS 520, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

FUSELAGE FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

FUSELAGE FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

FUSELAGE FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,302 hrs · 33,305 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,847 hrs · 32,478 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M01675. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,847 hrs · 32,478 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M01674. R & R BATTERY PACK IAW MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 51,228 hrs · 29,872 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: SLIDE — FAILED (R1 DOOR) · airframe 51,109 hrs · 29,796 cycles

R1 DOOR EMERGENCY EVAC SLIDE BREAKAWAY STRAPS FAILED TO RELEASE DURING DEPLOYMENT TEST. R & R SLIDE IAW MT.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,445 hrs · 29,413 cycles

RT HORIZONTAL STABILIZER RIB AT STATION 92.7 HORIZONTAL FLANGE CRACKED AT FIRST STIFFENER FROM FRONT SPAR. REPAIRED RIB IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,445 hrs · 29,413 cycles

RT HORIZONTAL STABILIZER RIB STIFFENER CRACKED AT STAB STATION 129.50. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,445 hrs · 29,413 cycles

RT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70 CRACKED AT SECOND FROM FRONT VERTICAL STIFFENER JUST ABOVE LOWER CHORD. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,445 hrs · 29,413 cycles

RT HORIZONTAL STABILIZER RIB STIFFENER CRACKED AT STAB STATION 92.70. REPAIRED STIFFENER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,445 hrs · 29,413 cycles

RT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70, RIB CRACKED IN FRONT VERTICAL STIFFENER. REPAIRED RIB IAW EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,445 hrs · 29,413 cycles

RT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70, CRACKED AT THIRD FROM FRONT VERTICAL STIFFENER JUST ABOVE LOWER CHORD. REPAIRED STIFFENER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,445 hrs · 29,413 cycles

RT HORIZONTAL STABILIZER RIB AT STAB STATION 129.50, RIB CRACKED IN SECOND FROM FRONT VERTICAL STIFFENER. REPAIRED RIB IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,445 hrs · 29,413 cycles

RT LOWER BULKHEAD CHORD CRACKED AT BS 540 FWD & AFT SECOND FROM BOTTOM. REPAIRED CHORD IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,445 hrs · 29,413 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 27. REPAIRED WEB AT BS 663, LBL 27.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,445 hrs · 29,413 cycles

RT WING NR 8 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,445 hrs · 29,413 cycles

RT NR 3 WINDOW FRAME E - F WINDOW POST SKIN CUTOUT CRACKED. REPAIRED POST IAW ACO.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,445 hrs · 29,413 cycles

LT WING NR 1 SLAT LOWER SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,445 hrs · 29,413 cycles

RT WING NR 7 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,445 hrs · 29,413 cycles

LT NR 3 WINDOW FRAME E F WINDOW POST CRACKED INDICATIONS IN 1ST & 2ND FASTENER HOLES FROM BOTTOM. REPAIRED POST IAW ACO.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,445 hrs · 29,413 cycles

LT WING NR 3 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 49,063 hrs · 28,579 cycles

FWD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. R & R LIGHT IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 47,334 hrs · 27,567 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,703 hrs · 27,206 cycles

LEFT WING TRAILING EDGE OUTBOARD AFT FLAP DELAMINATED AT AFT INBOARD CONNER 3.5" LONG X 1.0" WIDE MOD. PERFORMED INTERIM REPAIR PER SRM REF 57-53-01-1A-4 PARA.5. SEALED DAMAGED AREA WITH SPEED TAPE. MAKE AN INSPECTION OF DELAMINATION AND TAPE

Part: HOUSING — DAMAGED (EXIT SIGN) · airframe 46,651 hrs · 27,166 cycles

OVERWING EMERGENCY EXIT SIGN OVER CENTER AISLE NOT SECURED. REMOVED AND REPLACED OVERWING EMERGENCY EXIT SIGN HOUSING PER MM. OPS CHECK NORMAL.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 46,643 hrs · 27,163 cycles

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

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 46,643 hrs · 27,163 cycles

RIGHT HORIZONTAL STABILIZER LOWER FWD SLIDE SEAL CRACKED. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER LOWER FWD SLIDE SEAL REF MM.

Part: COMPUTER — FAILED (CABIN) · airframe 46,269 hrs · 26,916 cycles

FUMES DETECTED ON AIRCRAFT. INSPECTED COMPUTER PER 05-51-56 FOUND OPC TO BE THE CAUSE OF ODOR.

Part: LENS — BROKEN (CABIN) · airframe 44,753 hrs · 25,953 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER M/M.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 43,761 hrs · 25,376 cycles

LT EMERGENCY EXIT LIGHT INOP AT ROW 11. RECONNECTED CONNECTOR IAW AMM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 43,761 hrs · 25,376 cycles

RT EMERGENCY EXIT LIGHT INOP AT ROW 8. RECONNECTED CONNECTOR IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 43,761 hrs · 25,376 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED & REPLACED SIGN IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 43,761 hrs · 25,376 cycles

G1 GALLEY MOUNTED EMERGENCY EXIT SIGN BROKEN. REMOVED & REPLACED SIGN IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 43,761 hrs · 25,376 cycles

AFT LAV EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

AFT BULKHEAD WEB CRACKED AT BS 663, BETWEEN STR 1R TO STR 2R. REPAIRED WEB IAW SRM & AMM.

Part: GROUND WIRE — BROKEN (CABIN) · airframe 43,761 hrs · 25,376 cycles

FWD LAVATORY EMERGENCY LIGHT GROUND WIRE IS BROKEN FWD OF L1 DOOR. REPAIRED CONNECTOR IAW SWPM & AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

SKIN CORRODED AT BS 986, BETWEEN LBL 37 TO LBL 49. REPAIRED SKIN IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

CABIN FLOOR WEB CORRODED BETWEEN BS 1006 TO BS 1016, LBL 39.5. REMOVED AND REPLACED WEB IAW SRM & AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 35 TO RBL 44. REMOVED AND REPLACED BEAM IAW SRM, MM, & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

CABIN STA 986, LBL 5 TO RBL 5 FLOORBEAM UPPER T-CAP CORRODED AT NUT CLIP HOLES. REMOVED AND REPLACED UPPER T-CAP PER SRM AND BAC DRAWING.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

RT CREASE BEAM, BETWEEN STATIONS 328 AND 360 CORRODED. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

FLOORBOARD SUPPORT BEAM CORRODED AT BS 270, BETWEEN RBL 10 TO LBL 10. REPAIRED BEAM IAW EA &SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

AFT CARGO THRESHOLD FLOOR SUPPORT SKIN CORRODED BETWEEN BS 797 TO BS 857, RBL 21. REPAIRED SKIN IAW SRM AND DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

FRAME ATTACH CLIP CRACKED AT 500B, LBL 25. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,761 hrs · 25,376 cycles

LT WING, NR 2 SLAT LOWER SKIN SURFACE CRACKED. REPAIRED SKIN IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

WHEEL WELL BULKHEAD VERTICAL WEB CRACKED AT BS 663, RBL 36. REPAIRED WEB IAW AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

STR CLIP CRACKED AT BS 827, LBL 14, AFT CARGO FLOOR AREA. REMOVED AND REPLACED STR CLIP PER SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 43,761 hrs · 25,376 cycles

LT WING O/B AFT FLAP I/B CORNER TRAILING EDGE WEDGE DELAMINATED. REPAIRED WEDGE IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,376 cycles

RT STIFFENER CRACKED AT BS 663 BETWEEN THE A/C BAY AND RT WHEEL WELL. REMOVED AND REPLACED STIFFENER IAW SRM AND AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,538 hrs · 24,638 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 40,920 hrs · 23,726 cycles

DURING SCHEDULED MV2 CHECK FOUND, EEPLS STRIP AT ROW 8 LOOSE. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,549 hrs · 22,926 cycles

LT EEPLS LOOSE AT ROW 7. SECURED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 37,973 hrs · 21,989 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 37,973 hrs · 21,989 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 37,569 hrs · 21,746 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 37,473 hrs · 21,685 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MT.

Part: COVER — MISSING (CABIN) · airframe 36,910 hrs · 21,361 cycles

EEPLS COVER MISSING AT L1 DOOR. REMOVED AND REPLACED COVER PER EA.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,724 hrs · 21,245 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 41.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,724 hrs · 21,245 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,724 hrs · 21,245 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,724 hrs · 21,245 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,724 hrs · 21,245 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,724 hrs · 21,245 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,724 hrs · 21,245 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 41.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,724 hrs · 21,245 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 34,997 hrs · 20,152 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT FITTING LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 34,997 hrs · 20,152 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT FITTING LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 33,506 hrs · 19,272 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 33,506 hrs · 19,272 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 29,876 hrs · 17,039 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,865 hrs · 17,031 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CABIN EEPLS INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CHARGER — FAULTY (CABIN) · airframe 29,865 hrs · 17,031 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK CHARGER PER MM.

Part: LENS — CRACKED (CABIN) · airframe 29,839 hrs · 17,009 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. R7R LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,839 hrs · 17,009 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 41 TO RBL 39. REPAIRED FLOORBEAM PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 29,839 hrs · 17,009 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 29,839 hrs · 17,009 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,839 hrs · 17,009 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 990, RBL 38. REPAIRED WEB PER SRM AND BOEING DRAWING.

Part: BELTFRAME — WORN (FUSELAGE) · airframe 29,839 hrs · 17,009 cycles

DURING SCHEDULED 8Y CHECK, FOUND BELTFRAME WORN AT BS 335, STR 5R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,839 hrs · 17,009 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 47R. REPAIRED FRAME PER SRM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 29,744 hrs · 16,955 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,106 hrs · 14,297 cycles

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

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 23,541 hrs · 13,384 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 21,921 hrs · 12,442 cycles

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

Part: LIGHT — WORN (CABIN) · airframe 21,148 hrs · 11,999 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP WORN AT ROW 13 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 21,064 hrs · 11,952 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM.

Part: PUMP — LEAKING (NR 1 ENGINE FUEL) · airframe 20,878 hrs · 11,852 cycles

NR 1 ENGINE FUEL PUMP LEAKING. REMOVED AND REPLACED FUEL PUMP PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 19,902 hrs · 11,277 cycles

BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 9 ABC. SECURED LENS PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,872 hrs · 11,261 cycles

DURING SCHEDULED MV2 CHECK, FOUND CABIN EMERGENCY LIGHTS INOP BETWEEN ROW 6 ABC TO ROW 10 ABC. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,389 hrs · 10,985 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 16,297 hrs · 9,276 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 15,812 hrs · 9,003 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (SERVICE DOOR) · airframe 12,299 hrs · 7,120 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,048 hrs · 5,270 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP AND COVER MISSING AT ROW NR 1. RELAMPED AND INSTALLED COVER PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 6,595 hrs · 3,883 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 5,371 hrs · 3,184 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED IN FWD CABIN. R&R COVERS PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 974 hrs · 574 cycles

AFT SERVICE DOOR EVACUATION SLIDE CAME OUT OF CONTAINER AS PROVO TRUCK PULLED AWAY FROM ACFT. REINSTALLED SLIDE ASSY PER MM.

Part: RELIEF VALVE — FAILED (RT MLG WW) · airframe 689 hrs · 380 cycles

AIR TURNBACK. DURING CLIMB WHEN LANDING GEAR WERE RAISED, A-SYS HYD LOW PRESSURE LIGHT ILLUMINATED. RESET BOTH HYDRAULIC SYS PNEUMATIC HEAD PRESSURE RELIEF VALVES. OPS CHECK GOOD.