N758SW

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 74,861 hrs · 44,169 cycles

SUPPLEMENTAL INFORMATION: FWD ENTRY; FWD SERVICE AND AFT ENTRY DOOR SLIDES MANUAL DEPLOY HANDLE NOT COVERED. ; / [01] REPOSITIONED SLIDE ON FWD ENTRY; FWD SERVICE AND AFT ENTRY DOOR AS REQ PER SIP.

Part: NONE — LOOSE (CABIN) · airframe 74,355 hrs · 43,873 cycles

EMERGENCY EXIT LIGHT COVER BY FWD FLIGHT ATTENDANT JUMP SEAT KEEPS FALLING OFF. ; / [01] REMOVED AND REPLACED FWD ENTRY EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-02.

Part: HANDLE — LOOSE (L1 DOOR ASSIST) · airframe 74,045 hrs · 43,671 cycles

LOOSE ASSIST HANDLE ON FWD ENTRY DOOR LINING AND GALLEY 1 ; 2021-384568 / [01] INSTALLED CORRECTLY ASSIST HANDLE ON FWD ENTRY DOOR LINING AND GALLEY 1 I.A.W B737-700 AMM 52-11-31-400-802 STEP 3G (2) AND ENCORE CMM 25-31-03 ASSEMBLY STEP 2A PAGE 7001 REV 6.; [02] INSTALLED CORRECTLY ASSIST HANDLE ON FWD ENTRY DOOR LINING AND GALLEY 1 I.A.W B737-700 AMM 52-11-31-400-802 STEP 3G (2) AND ENCORE CMM 25-31-03 ASSEMBLY STEP 2A PAGE 7001 REV 6.

Part: HANDLE — LOOSE (L2 DOOR ASSIST) · airframe 74,045 hrs · 43,671 cycles

LOOSE ASSIST HANDLE ON DOORWAY CUTOUT AT AFT ENTRY DOOR ; 2021-384567 / [01] TIGHTENED ASSIST HANDLE ON DOORWAY CUTOUT AT AFT ENTRY DOOR I.A.W B737-700 AMM-25-21-25-420-801 STEP 3.B(5); [02] TASK CARD COMPLETE.

Part: NONE — MISSING (CABIN) · airframe 74,045 hrs · 43,671 cycles

MISSING BLACK EMERGENCY EVACUATION ARROW ON SPOILER #7 ; 2021-384569 / [01] RESTORED PAINT BLACK EMERGENCY EVACUATION ARROW ON SPOILER #7 IAW B737-700 AMM 51-21-97-370-802; [02] RESTORED PAINT BLACK EMERGENCY EVACUATION ARROW ON SPOILER #7 IAW B737-700 AMM 51-21-97-370-802 AND DWG-11200003 REV F; [03] TASK CARD COMPLETE.

Part: ACCESS PANEL — ELONGATED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

ELONGATED HOLES ON ACCESS PANEL 194E AFT WING TO BODY FAIRING ; 2021-384558 / [01] PERFORMED VISUAL INSPECTION ON FASTENER HOLES OF ACCESS PANEL 194E AFT WING TO BODY FAIRING AND FOUND WITH CRACK AND EVALUATED AND FOUND OUT LIMITS TO REPAIR DUE TO EXCEED 50% OF FASTENER HOLES DAMAGED AS PER B737-700 SRM 51-70-05-2R-8 FIG 201. FWD SIDE IN DIAMETER ARE: #1= 0.45 IN. #2= 0.45 IN. #3= 0.35 IN. #4= 0.60 IN. #5= 0.50 IN. #6= 0.40 IN. #7= 0.40 IN. O/B SIDE IN DIAMETER IS: #8= 0.40 IN. AFT SIDE IN DIAMETER ARE: #9= 0.50 IN. #10= 0.45 IN. #11= 0.55 IN. #12= 0.50 IN. #13= 0.33 IN. TOOL USED: CALIPER P/N 500-197-30 S/N 15121550 DUE DATE: 03-AUG-22.; [02] STEP 1 COMPLETED.; [03] REPLACED ACCESS PANEL 194E AFT WING TO BODY FAIRING I.A.W B737-700 AMM 53-51-21-400-801; [04] REPLACED ACCESS PANEL 194E AFT WING TO BODY FAIRING I.A.W B737-700 AMM 53-51-21-400-801<BR>TASK COMPLETED

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK ANGLE LOCATED BETWEEN BS 907 AND BS 927 BETWEEN S-25R AND S-27R FWD LOCATION INTERNAL WATER SERVICE AREA AFT CARGO COMPARTMENT ; 2021-384547 / [11] REPLACED ANGLE AND FASTENERS LOCATED BETWEEN BS 907 AND BS 927 BETWEEN S-25R AND S-27R FWD LOCATION INTERNAL WATER SERVICE AREA AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 147A7221-32; [12] RII; STEP 10 COMPLETED. <BR>PENDING SEALANT APPLICATION ON RIVETS HEAD AND AROUND OF ANGLE.; [13] REPLACED ANGLE AND FASTENERS LOCATED BETWEEN BS 907 AND BS 927 BETWEEN S-25R AND S-27R FWD LOCATION INTERNAL WATER SERVICE AREA AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 147A7221-32 AND APPLIED SEALANT IAW B737-700 SRM 51-10-02; [14] TASK CARD COMPLETED <BR>RII

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK ANGLE LOCATED BETWEEN BS 907 AND BS 927 BETWEEN S-25R AND S-27R AFT LOCATION INTERNAL WATER SERVICE AFT CARGO COMPARTMENT ; 2021-384548 / [13] REPLACED ANGLE AND FASTENERS LOCATED BETWEEN BS 907 AND BS 927 BETWEEN S-25R AND S-27R AFT LOCATION INTERNAL WATER SERVICE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02<BR>AND DRAWING #147A7221-32 AND APPLIED SEALANT IAW B737-700 51-10-02; [14] TASK CARD COMPLETED <BR>RII

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK ANGLE - SUPPORT LOCATED AT BS 867 AT LEVEL STRINGER 26L AFT CARGO COMPARTMENT ; 2021-384546 / [01] REMOVED ANGLE - SUPPORT LOCATED AT BS 867 AT LEVEL STRINGER 26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND NOT FOUND ALLOWABLE DAMAGE LIMITS IN SRM B737-700 ANGLE - SUPPORT MUST BE REPLACED. PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUN ANY DAMAGE; [02] OK TO INSTALL SUPPORT LOCATED AT BS 867 AT LEVEL STRINGER 26L AFT CARGO COMPARTMENT GRANTED; [03] STEP 1;2 COMPLETED; [04] INSTALLED SUPPORT LOCATED AT BS 867 AT LEVEL STRINGER 26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; [05] REPLACED SUPPORT LOCATED AT BS 867 AT LEVEL STRINGER 26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02; [06] CERTIFIED WORK PERFORMED. <BR>STEPS 4 & 5 COMPLETED.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK TRACK RBBL 13.84 BS 767 AND BS 727E AFT CARGO COMPARTMENT ; 2021-384542 / [20] REPAIRED CARGO TRACK LOCATED BTW RBBL 13.84 BS 787 AND BS 727D AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3.; [21] CERTIFIED STEP 20 RII

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 787 AT LEVEL STRINGER 25R WL 156 AT AFT CARGO COMPARTMENT ; 2021-384543 / [01] MEASURES OF CORROSION ON SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 787 AT LEVEL STRINGER 25R WL 156 AT AFT CARGO COMPARTMENT ARE: L=0.276 W=0.122 Y=0.040TOOL USED CALIPER P/N 500-752-20 S/N B21038258 DUE DATE: 12-AUG-22; [02] REMOVED CORROSION OF SUPPORT ZEE I.A.W. B737-700 SRM 51-10-02 AND TOOK MEASURES REWORKED AREA L=1.057 W=0.747 Y=0.046 TOOL USED CALIPER P/N:500-752-20 S/N:B21038258 DUE DATE: 12-AUG-22. EVALUATED SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 787 AT LEVEL STRINGER 25R WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 53-00-53-1A-2 ALLOWABLE DAMAGE 2 STEP 4 A(2) AND NOT MEETS REQUIREMENTS. SUPPORT ZEE MUST BE REPLACE.; [03] CERTIFIED STEP 1 AND 2 SUPPORT ZEE OUT OF LIMITS.; [04] MADE AND DRILLED SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 787 AT LEVEL STRINGER 25R WL 156 AT AFT CARGO COMPARTMENT I.A.W B 737-700 DWG 146A7502 SHEET 33 AND SRM 51-40-05.; [05] CERTIFIED STEP 4 RII; [06] APPLIED PROTECTIVE TREATMENT ON SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 787 AT LEVEL STRINGER 25R WL 156 AT AFT CARGO COMPARTMENT I.A.W B 737-700 SRM 51-20-01; [07] CERTIFIED STEP 6; [08] FABRICATED SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 787 AT LEVEL STRINGER 25R WL 156 AT AFT CARGO COMPARTMENT I.A.W B 737-700 DWG 146A7502 SHEET 33 AND SRM 51-10-02 ITEM 9 SRM 51-40-05; [09] JOB TASK CARD COMPLETED AS RII.; [10] TASK CARD COMPLETED.

Part: WEB — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS400 TO BS420 AT LEVEL STR 26L FWD CARGO COMPARTMENT ; 2021-384485 / [01] REMOVED WEB LOCATED AT BS 400 TO BS 420 AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DUE TO NO FOUND ALLOWABLE DAMAGE DATA ON SRM; WEB MUST BE REPLACED. AND PERFORMED A GENEREAL VISUAL INSPECTION ON ADJACENT AREA AND NO FOUND MORE DAMAGE IAW SRM B737-700 51-10-02; [02] OK TO INSTALL WEB AND FASTENERS LOCATED AT BS 400 TO BS 420 AT STR 26L AT FWD CARGO COMPARTMENT IS GRANTED; [03] STEP 1 COMPLETED.; [04] RII; STEP 2 COMPLETED.; [05] INSTALLED NEW WEB-INTERCOSTAL AND FASTENERS LOCATED AT BS 400 TO BS 420 AT STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG # 143A7505 REV -; [06] REPLACED WEB-INTERCOSTAL LOCATED AT BS 400 TO BS 420 AT STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 DWG # 143A7505 REV - MEASURES OF CRACK IS:0.508 TOOL USED CALIPER P/N 700-113-10 S/N 0023256 DUE DATE 14-SEP-21; [07] STEP 5 COMPLETED RII; [08] STEP 6 COMPLETED RII <BR>TASK CARD COMPLETED

Part: WEB — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500A TO BS500B AT LEVEL STR26R FWD CARGO COMPARTMENT ; 2021-384504 / [13] REPLACED WEB-INTERCOSTAL LOCATED BTW BS500A TO BS500B AT LEVEL STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM-51-10-02; SRM-51-40-02 AND DWG 143A7505 REV: D; [14] CORRECTED STEP #12<BR>INSTALLED REPAIR PART (ANGLE) AND WEB-INTERCOSTAL LOCATED BTW BS500A TO BS500B AT LEVEL STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM-51-40-02; DWG 143A7505 REV: D AND SRM-53-30-53-2R-1 STEP 4 M; P; O AND FIG. 202 SHEET 4; [15] STEP 13 AND 14 COMPLETED; RII.<BR><BR>TASK COMPLETED; RII

Part: WEB — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500C TO BS500D AT LEVEL STR26L FWD CARGO COMPARTMENT ; 2021-384497 / [10] INSTALL NEW WEB - INTERCOSTAL LOCATED BETWEEN BS500C TO BS500D AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG. #143A7505 REV.A MEASURES OF CRACK L= 0.684 TOL USED CALIPER P/N 700-113-10 S/N 0023208 DUE DATE 31-DEC-21 MATERIAL USED 7075-T6 / 0.032ALUMINIUM SHEET; [11] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS500C TO BS500D AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG. #143A7505 REV.A; [12] STEP 10 COMPLETE.. RII ITEM; [13] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS500C TO BS500D AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG. #143A7505 REV.A.. RII ITEM

Part: WEB — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500A TO BS500B AT LEVEL STR26L FWD CARGO COMPARTMENT ; 2021-384490 / [20] REPLACEDWEB-INTERCOSTAL LOCATED BTW BS500A TO BS500B AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM-51-10-02; SRM-51-40-02 AND DWG 143A7505 REV: D; [21] STEP 19 COMPLETED; RII.; [22] CORRECTED STEP 4: MADE WEB-INTERCOSTAL LOCATED BTW BS 500A TO BS 500B AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 DWG 143A7510 REV. C DRILLED NEW HOLES ON WEB-INTERCOSTAL IAW B737-700 SRM 51-40 -05 TOOL USED CALIPER P/N 500-752-20 S/N B16101278 DUE DATE 14-SEP-21 RADIUS GAGE P/N 2204A3 S/N408649 DUE DATE 24-FEB-22; RII.<BR><BR>TASK CARD COMPLETED

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK STRINGER 26L ON BS 540 AT FWD CARGO COMPARTMENT ; 2021-384486 / INSTALLED REPAIR PARTS -7 STRINGER SECTION -2 CHANNEL -3 ANGLE (2EA) AND SHEAR TIE LOCATED STA 520 BETWEEN STR 25L AND STR 26L, TIE CLIP LOCATED STA 520 STR 26L FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 SRM 53-00-03-2R-1 REPAIR 1 FIG 206 DWG #143A3230 REV. J MEASURES OF CRACK IS:L=0.506Ï¿½ TOOL USED CALIPER P/N 500-464 S/N B17030924 DUE DATE 03-NOV-21

Part: WEB — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500 TO BS500A AT LEVEL STR26L FWD CARGO COMPARTMENT ; 2021-384489 / [01] REMOVED WEB INTERCOSTAL LOCATED BETWEEN BS500 TO BS500A AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM; WEB INTERCOSTAL MUST BE REPLACED AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND DAMAGE.; [02] STEP 1 COMPLETED; [03] MADE WEB-INTERCOSTAL LOCATED BETWEEN BS500 TO BS500A AT LEVEL STR26L FWD CARGO COMPARTMENT IAW DWG 143A7510 REV. C. DRILLED NEW HOLES ON WEB INTERCOSTAL IAW B737-700 SRM 51-40-05 TOLL USED CALIPER P/N 500-752-20 S/N B16101278 DUE DATE 14-SEP-21; [04] STEP 3 COMPLETE; [05] APPLIED PROTECTIVE TREATMENT ON WEB INTERCOSTAL IAW B737-700 SRM 51-20-01; [06] STEP 5 COMPLETED; [07] OBTAINED OK TO INSTALL NEW WEB - INTERCOSTAL LOCATED BETWEEN BS500 TO BS500A AT LEVEL STR26L FWD CARGO COMPARTMENT; [08] OK TO INSTALL GRANTED <BR>STEP 7 COMPLETE.. RII ITEM; [09] INSTALLED NEW WEB-INTERCOSTAL LOCATED BETWEEN BS500 TO BS500A AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG #143A7505 REV. D MEASURES OF CRACK 0.392 TOOL ISED CALIPER P/N 700-113-10 S/N 0023208 DUE DATE 31-DEC-21 MATERIAL USED 7075T6B0.020 ALUMINIUM SHEET; [10] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS500 TO BS500A AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG #143A7505 REV. D; [11] STEP 9 COMPLETED <BR>RII; [12] TASK CARD COMPLETED <BR>RII

Part: WEB — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500B TO BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT ; 2021-384493 / [12] REPLACED NEW WEB - INTERCOSTAL LOCATED BETWEEN BS500B TO 500C AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG. #143A7505 REV.B MEASURES OF CRACK L= 0.785 TOL USED CALIPER P/N 700-113-10 S/N 0023208 DUE DATE 31-DEC-21 MATERIAL USED 7075-T6 / 0.020 ALUMINIUM SHEET; [13] STEP 11 COMPLETE.. RII ITEM; [14] REPLACED NEW WEB - INTERCOSTAL LOCATED BETWEEN BS500B TO 500C AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG. #143A7505 REV.B MEASURES OF CRACK L= 0.785 TOL USED CALIPER P/N 700-113-10 S/N 0023208 DUE DATE 31-DEC-21 MATERIAL USED 7075-T6 / 0.020 ALUMINIUM SHEET.. RII ITEM

Part: WEB — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS460 TO BS480 AT LEVEL STR 26L FWD CARGO COMPARTMENT ; 2021-384488 / [01] REMOVED WEB INTERCOSTAL LOCATED BETWEEN BS460 TO BS480 AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM; WEB INTERCOSTAL MUST BE REPLACED AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND DAMAGE.; [02] OBTAINED OK TO INSTALL NEW WEB INTERCOSTAL LOCATED BETWEEN BS460 TO BS480 AT LEVEL STR 26L FWD CARGO COMPARTMENT.; [03] STEP 1 COMPLETED; [04] STEP 2 COMPLETED <BR>RII; [05] WEB-INTERCOSTAL LOCATED BETWEEN BS460 TO BS480 AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG #143A7505 REV. - MEASURES OF CRACK 0.440 TOOL ISED CALIPER P/N 700-113-10 S/N 0023208 DUE DATE 31-DEC-21; [06] CORRECTIVE STEP 5 INSTALLED WEB-INTERCOSTAL LOCATED BETWEEN BS460 TO BS480 AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG #143A7505 REV. - MEASURES OF CRACK 0.440 TOOL ISED CALIPER P/N 700-113-10 S/N 0023208 DUE DATE 31-DEC-21; [07] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS460 TO BS480 AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 DWG #143A7505 REV. -; [08] STEP 6 COMPLETED RII ITEM; [09] TASK COMPLETED RII

Part: WEB — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS440 TO BS460 AT LEVEL STR 26L FWD CARGO COMPARTMENT ; 2021-384487 / [10] INSTALLED NEW WEB-INTERCOSTAL LOCATED BETWEEN BS440 TO BS460 AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG # 143A7505REV. A; [11] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS440 TO BS460 AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG # 143A7505REV. A AND SRM 51-10-02 ITEM 9; [12] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS440 TO BS460 AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG # 143A7505REV. A AND SRM 51-10-02 ITEM 9 TOOL USED CALIPER P/N 700-113-10 S/N 0023208 DUE DATE 31-DEC-21; [13] CORRECTED STEP 11 AND STEP 12 REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS440 TO BS460 AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG # 143A7505REV. A AND SRM 51-10-02 ITEM 9 TOOL USED CALIPER P/N 700-113-10 S/N 0023208 DUE DATE 31-DEC-21; [14] STEP 10 COMPLETE.. RII ITEM; [15] STEP 13 COMPLETE.. RII ITEM <BR>TASK CARD COMPLETE..RII ITEM

Part: WEB — ELONGATED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

ELONGATED HOLE WEB - INTERCOSTAL LOCATED BETWEEN BS420 TO BS440 AT LEVEL STR26R FWD CARGO COMPARTMENT ; 2021-384506 / [08] INSTALLED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS420 TO BS440 AT LEVEL STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING 143A8120 REV -; [09] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS420 TO BS440 AT LEVEL STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DRAWING DRAWING 143A8122 REV A AND DRAWING 143A8120 REV - MATERIAL USED 7075T6-0.045 PO 2015 505829; [10] STEP 8 COMPLETED RII; [11] STEP 9 COMPLETED RII <BR>TASK CARD COMPLETED; [12] TASK CARD COMPLETED

Part: WEB — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500C TO BS500D AT LEVEL STR26R FWD CARGO COMPARTMENT ; 2021-384502 / [01] REMOVED WEB INTERCOSTAL LOCATED BETWEEN BS500C TO BS500D AT LEVEL STR26R FWD CARGO COMPARTMENT IAW SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM; WEB INTERCOSTAL MUST BE REPLACED AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND DAMAGE.; [02] STEP 1 COMPLETE; [03] DRILLED NEW HOLES ON NEW INTERCOSTAL IAW B737-700 SRM 51-40-05; [04] APPLIED PROTECTIVE TREATMENT ON NEW HOLES OF NEW INTERCOSTAL IAW B737-700 SRM 51-20-01; OBTAINED OK TO INSTALL OF NEW INTERCOSTAL AND FASTENERS.; [05] STEP 3 AND 4 COMPLETED <BR>OK TO INSTALL GRANTED RII; [06] INSTALLED NEW INTERCOSTAL LOCATED BETWEEN STA 500C TO STA 500D FWD CARGO COMPARTMENT AND FASTENERS IAW SRM B737-700 51-40-02 AND DRAWING 143A7505 REV. A; [07] CERTIFIED STEP 6 RII; [08] REPLACED INTERCOSTAL LOCATED BETWEEN STA 500C TO STA 500D FWD CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-10-02 AND DRAWING 143A7505 REV. A; [09] REPLACED INTERCOSTAL LOCATED BETWEEN STA 500C TO STA 500D FWD CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-10-02 AND DRAWING 143A7505 REV. A RII

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK EXTERNAL SKIN CLOSURE ANGLE LOCATED BETWEEN BS1088 TO BS1132 RH SIDE FUSELAGE EXTERIOR ; 2021-384481 / [01] REMOVED CLOSURE ANGLE LOCATED BETWEEN BS1088 TO BS1132 RH SIDE FUSELAGE EXTERIOR IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND ANY DAMAGE; [02] STEP 1 CERTIFIED; [03] DRILLED HOLES ON NEW CLOSURE ANGLE IAW B737-700 SRM 51-40-05 AND COUNTERSUNK HOLES IAW B737-700 SRM 51-40-08; [04] LATE ENTRY EVALUATED CLOSURE ANGLE LOCATED BETWEEN BS1088 TO BS1132 RH SIDE FUSELAGE EXTERIOR AND NOT FOUND ALLOWABLE DAMAGE MUST BE REPLACED; [05] COMPLETE STEP 3 AND 4. RII; [06] APPLIED PROTECTIVE TREATMENT ON HOLES OF NEW CLOSURE NGLE LOCATED BETWEEN BS1088 TO BS1132 RH SIDE IAW B737-700 SRM 51-20-01; [07] OBTAINED OK TO INSTALL NEW CLOSURE ANGLE LOCATED BETWEEN BS1088 TO BS1132 RH SIDE FUSELAGE EXTERIOR AND FASTENERS; [08] COMPLETED STEP #6; [09] OK TO INSTALL CLOSURE ANGLE.<BR>ITEM#7<BR>RII; [10] INSTALLED NEW CLOSURE ANGLE LOCATED BETWEEN BS1088 TO BS1132 RH SIDE FUSELAGE EXTERIOR AND FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING 148A8300-2 REV C; [11] COMPLETED STEP #10.<BR>RII ITEM; [12] REPLACED CLOSURE ANGLE LOCATED BETWEEN BS1088 TO BS1132 RH SIDE FUSELAGE EXTERIOR IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DRAWING 148A8300-2 REV C; [13] TASK COMPLETED RII

Part: ANGLE — CRACKED (CENTER WING) · airframe 74,045 hrs · 43,671 cycles

CRACK ANGLE LOCATED BS695 AND RBL24 AT CENTER WING BOX ; 2021-384461 / [01] REMOVED ANGLE LOCATED BS 695 AND RBL 24 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND NOT FOUND ALLOWABLE DAMAGE LIMITS IN SRM B737-700 ANGLE MUST BE REPLACED ; PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND MORE DAMAGE.; [02] REPAIR ANGLE (1 E/A) MATERIAL P/N: 7075-T0/0.050 (BAC1490-2782) PO: 2021-184600. HEAT TREATED AND CONVERTED FROM 7075T0 TO 7075T73 IAW BAC5602; TABLE IV AND TABLE XI. TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 21-JAN-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [03] STEP 1 COMPLETED; [04] STEP 2 COMPLETED.; [05] MADE ANGLE LOCATED BS695 AND RBL24 AT CENTER WING BOX IAW DRAWING #273A9112 REV:-; [06] VERIFIED STEP 5. COMPLETED<BR>MADE ANGLE LOCATED BS695 AND RBL24 AT CENTER WING BOX IAW DRAWING #273A9112 REV:-; [07] APPLIED PROTECTIVE TREATMENT ON ANGLE LOCATED BS695 AND RBL24 AT CENTER WING BOX IAW B737-700 SRM 51-20-01 AND OBTAIN OK TO INSTALL ANGLE; [08] STEP 7 CERTIFIED AS RII; [09] INSTALLED ANGLE LOCATED BS 695 AND RBL 24 AT CENTER WING IAW B737-700 SRM 51-40-02 DWG; [10] REPLACED ANGLE LOCATED BS 695 AND RBL 24 AT CENTER WING IAW B737-700 SRM 51-40-02; [11] CORRECTIVE ACTION STEP 9 INSTALLED ANGLE LOCATED BS 695 AND RBL 24 AT CENTER WING IAW B737-700 SRM 51-40-02; [12] STEP 10 AND 11 COMPLETED.ITEM RII.TASK COMPLETED

Part: ANGLE — CRACKED (LT WING) · airframe 74,045 hrs · 43,671 cycles

CRACKED ANGLE AT FUEL BOOST PUMP IFSS 120 APROX LT WING. MACHINED ANGLE SUPPORT IAW SRM 57-20-10-01-1 ITEM 4A TABLE 2 FIGURE 2 AND DWG 116A3939 REV A DWG 112A2004 REV A.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT ; 2021-384418 / [01] EVALUATED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT FOUND CRACK (1E/A) MEASURE IS: 1)L=2.6625 INCH; THIS CRACK MUST BE REPAIRED I.A.W 737-700 SRM BOEING 53-30-15-2R-1 REPAIR 1 TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N 15120589; DUE DATE 14-SEP-21; [02] EVALUATED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT FOUND CRACK (1E/A) MEASURE IS: 1)L=2.6625 INCH; THIS CRACK MUST BE REPAIRED I.A.W 737-700 SRM BOEING 53-30-15-2R-1 REPAIR 1 TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N 15120589; DUE DATE 14-SEP-21; [03] WELDED CRACK LOCATED AT AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4.B. STEP (4) AND BAC 5975 WELD ROD USED: AMS 4190K P.O. 2021 118316; [04] STEP 3 COMPLETED.; [05] LIQUID PENETRANT INSP ON AREA OF WELDED; CRACK NOT FOUND. IAW B SOPM 20-20-02.; [06] APPLIED CHEMICAL CONVERSION COATING (ALODINE) AND TWO LAYERS PRIMER ON INNER SURFACES OF THE AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700 SRM 53-30-15-2R-1; REPAIR 1; PARAGRAPH 4. B; STEPS (5) TO (7).; [07] STEP 6 COMPLETED; [08] REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4.B AND BAC 5975.; [09] VERIFIED TASK COMPLETE

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK STRINGER 26R AT LEVEL BS 540 AT FWD CARGO COMPARTMENT ; 2021-384401 / [23] INSTALLED REPAIR PARTS: -7 STRINGER SECTION; -2 CHANNEL; -3 ANGLE (2E/A) LOC BTW BS 500D TO BS 540 STR 26R AND TIE CLIP LOC BS 540 STR 26R IAW B737-700 SRM SRM 53-00-03-2R-1 REPAIR 1 DWG. 143A3230 REV. A; [24] CORRECTED STEP 23 <BR>INSTALLED REPAIR PARTS: -7 STRINGER SECTION; -2 CHANNEL; -3 ANGLE (2E/A) LOC BTW BS 500D TO BS 540 STR 26R AND TIE CLIP LOC BS 520 STR 26R IAW B737-700 SRM SRM 53-00-03-2R-1 REPAIR 1 DWG. 143A3230 REV. A; [25] RII; STEP 24 COMPLETED.; [26] OBTAINED OK TO INSTALL SHEAR TIE AND FASTENERS LOC BS 520 BTW STR 25R AND STR 26R; [27] RII; STEP 26 COMPLETED. <BR>OK2INS GRANTED.; [28] INSTALLED SHEAR TIE AND FASTENERS LOC BS 520 BTW STR 25R AND STR 26R IAW B737-700 SRM 51-40-02 DWG # 143A3230 REV. A; [29] STEP 28 COMPLETED AS RII.; [30] PERFORMED REPAIR LOCATED BTW BS 500D + 10 TO BS 540 STR 26R IAW B737-700 SRM SRM 53-00-03-2R-1 REPAIR 1 DWG. 143A3230 REV. A; [31] CORRECTED STEP 30 PERFORMED REPAIR LOCATED BTW BS 500D + 10 TO BS 540 STR 26R IAW B737-700 SRM SRM 53-00-03-2R-1 REPAIR 1 DWG. 143A3230 REV. A. MEASURED OF<BR>CRACK IS 0.482 TOOL USED CALIPER P/N 2340A1,NG,NRC,2021-09-14 15:43:37,22Y,Y,MX,0,0,,CRACK STRINGER 26R AT LEVEL BS 540 AT FWD CARGO COMPARTMENT ; 2021-384401"

Part: SUPPORT WEB — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK INBOARD FAN COWL SUPPORT WEB ON ENGINE 1 ; 2021-384389 / [01] REMOVED SUPPORT WEB INBOARD FAN COWL ON ENGINE 1 IAW SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 ITEM (9).PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND MORE DAMAGE.; [02] OBTAINED OK TO INSTALL NEW SUPPORT WEB INBOARD FAN COWL ON ENGINE 1; [03] STEP 1 AND 2 COMPLETED <BR><BR>PERFORMED VISUAL INSPECTION; NO DISCREPANCY FOUND <BR><BR>OK TO INSTALL GRANTED.; [04] INSTALLED NEW SUPPORT WEB INBOARD FAN COWL ON ENGINE 1 IAW SRM 51-40-02-0G-0 AND CMM 71-13-30.; [05] REPLACED SUPPORT WEB INBOARD FAN COWL ON ENGINE 1 IAW SRM 51-40-02-0G-0 AND CMM 71-13-30.; [06] CORRECTED STEP 4 AND 5; REPLACED SUPPORT WEB INBOARD FAN COWL ON ENGINE 1 IAW B737-700 SRM 51-40-02-0G-0 AND GOODRICH AEROSTRUCTURES CMM 71-13-30.; [07] CERTIFIED WORK PERFORMED.

Part: ACCESS PANEL — ELONGATED (R/H WING) · airframe 74,045 hrs · 43,671 cycles

ELONGATED HOLE ACCESS PANEL 621NB LEADING EDGE AT RT WING ; 2021-384373 / [24] REPAIRED ACCESS PANEL 621N,NG,NRC,2021-09-16 02:41:39,22Y,N,MX,0,0,,ELONGATED HOLE ACCESS PANEL 621NB LEADING EDGE AT RT WING ; 2021-384373"

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK STRINGER 24R AT LEVEL BS 540 AT FWD CARGO COMPARTMENT ; 2021-384334 / [26] INSTALLED INSTALL REPAIR PARTS -7 STRINGER SECTION -2 CHANNEL -3 ANGLE (2EA) AND SHEAR TIE LOCATED BETWEEN STR 24R AND STR 25R STA 520 ; TIE CLIP LOCATED STA 520 STR 24R FWD CARGO COMPARTMENT DWG #143A3230 REV. A MEASURES OF CRACK IS: 0.802 TOOL USED CALIPER P/N 500-464 S/N B17030924 DUE DATE 03-NOV-21; [27] CORRECTED STEP 26 INSTALLED REPAIR PARTS -7 STRINGER SECTION -2 CHANNEL -3 ANGLE (2EA) AND SHEAR TIE LOCATED BETWEEN STR 24R AND STR 25R STA 520 ; TIE CLIP LOCATED STA 520 STR 24R FWD CARGO COMPARTMENT DWG #143A3230 REV. A MEASURES OF CRACK IS: 0.802 TOOL USED CALIPER P/N 500-464 S/N B17030924 DUE DATE 03-NOV-21; [28] RII; STEP 27 COMPLETED.; [29] PERFORMED PERMANENT REPAIR ON STRINGER 24R BTW BS 500D TO BS540 AT FWD CARGO COMPARTMENT SRM 53-00-03-2R-1 REPAIR 1 SRM 51-10-02 ITEM 9 DWG # 143A3230 REV. A; [30] CORRECTED STEP 29 PERFORMED PERMANENT REPAIR ON STRINGER 24R BTW BS 500D TO BS540 AT FWD CARGO COMPARTMENT SRM 53-00-03-2R-1 REPAIR 1 SRM 51-10-02 ITEM 9 DWG # 143A,NG,NRC,2021-09-10 21:18:35,22Y,Y,MX,0,0,,CRACK STRINGER 24R AT LEVEL BS 540 AT FWD CARGO COMPARTMENT ; 2021-384334"

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK STRINGER 25R AT BS 540 AT FWD CARGO COMPARTMENT ; 2021-384332 / ALONG THE CUT EDGE ON STRINGER PER B737 NDT PART 6 51-00-00 PRO[26] LATE ENTRY REMOVED FASTENER BTW STR 20R TO 26R AND SPLICE LOC. BTW STR 25R TO 26R STA 500C IAW B737-700 SRM-51-40-02; [27] CORRECTED STEP #26 <BR>LATE ENTRY REMOVED FASTENER BTW STR 20R TO 26R AND SPLICE LOC. BTW STR 25R TO 26R STA 500C IAW B737-700 SRM-51-40-02 AND PERFORMED VISUAL INSPECTION ON OPEN HOLE AND NOT FOUND MORE DAMAGE; [28] COMPLETED STEP 27; [29] OK TO INSTALL SHEAR TIE (2EA) LOCATED STA 500D BETWEEN STRINGER 25R TO STRINGER 26R AND STRINGER 24R TO STRINGER 25R ; TIE CLIP (2EA) LOCATED STA 520 STRINGER 25R AND STA 500D STRINGER 25R; WEB LOCATED STRINGER 25R BETWEEN STA 500D TO STA 520; FASTENERS BTW STR 20R TO 26R BS 500C AND SPLICE LOC. BTW STR 25R TO 26R STA 500C.; [30] OK TO INSTALL GRANTED IN STEP 29<BR>RII ACCOMPLISHED; [31] MADE AND DRILLED REPAIR PARTS: -2 CHANNEL AND -3 ANGLE (2E/A) LOC BTW BS 500C TO BS 500D STR 25R IAW B-737-700 SRM 53-00-03-2R-1 REPAIR 1; [32] CERTIFIED STEP 31 RII; [33] APPLIED PROTECTIVE TREATMENT ON REPAIR AREA AND REPAIR PARTS: -2 CHANNEL AND -3 A,NG,NRC,2021-09-14 15:37:23,22Y,Y,MX,0,0,,CRACK STRINGER 25R AT BS 540 AT FWD CARGO COMPARTMENT ; 2021-384332"

Part: LENS — BROKEN (CABIN) · airframe 74,045 hrs · 43,671 cycles

BROKEN EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) ; 2021-384331 / [01] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-802 STEP 3C (10).; [02] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-802 STEP 3C (10)

Part: PLATE — CRACKED (L/H WING) · airframe 74,045 hrs · 43,671 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 220 AT LT WING ; 2021-384170 / [06] INSTALL NEW CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 220 AT LT WING : INSTALLED NEW CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 220 AT LT WING I.A.W. B737-700 SRM 51-40-02 AND DWG # 115A2001 REV B SHEET 1; [07] STEP 6 COMPLETED; [08] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 220 AT LT WING : INSTALLED NEW CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 220 AT LT WING I.A.W. B737-700 SRM 51-40-02 AND DWG # 115A2001 REV B SHEET 1; [09] VERIFIED STEP 8. COMPLETED<BR>REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 220 AT LT WING : INSTALLED NEW CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 220 AT LT WING I.A.W. B737-700 SRM 51-40-02 AND DWG # 115A2001 REV B SHEET 1

Part: ACCESS PANEL — CRACKED (R/H WING) · airframe 74,045 hrs · 43,671 cycles

CRACK ACCESS PANEL 661CB TRAILING EDGE LOC. HOLE ATTACH AERODINAMYC SEAL AT RT WING ; 2021-384157 / REPAIRED ACCESS PANEL 661CB AT RT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9.

Part: ACCESS PANEL — CRACKED (R/H WING) · airframe 74,045 hrs · 43,671 cycles

CRACK ACCESS PANEL 661BB TRAILING EDGE LOC. HOLE ATTACH AERODYNAMIC SEAL AT RT WING ; 2021-384160 / REPAIRED ACCESS PANEL 661BB AT RT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK FLOOR PANEL 232SF AT PASSENGER CABIN ; 2021-384074 / [22] REPAIRED FLOOR PANEL 232SF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [23] JOB TASK COMPLETED.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

MISSING MATERIAL FLOOR PANEL 231ZF AT PASSENGER CABIN ; 2021-384065 / [22] REPAIRED FLOOR PANEL 231ZF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [23] JOB TASK COMPLETED.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

DELAMINATED FLOOR PANEL 241BF AT PASSENGER CABIN ; 2021-384107 / [22] REPAIRED FLOOR PANEL 241BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [23] JOB TASK COMPLETED.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

MISSING MATERIAL FLOOR PANEL 242BF AT PASSENGER CABIN ; 2021-384115 / [23] REPAIRED FLOOR PANEL 242BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [24] JOB TASK COMPLETED.

Part: ANGLE — CRACKED (R/H WING) · airframe 74,045 hrs · 43,671 cycles

CRACK ANGLE TRAILING EDGE LOCATED ON ORSS 274 APROX. DEFLECTION CONTROL RIB RT WING ; 2021-384034 / [01] OK TO INSTALL ANGLE AND FASTENERS LOCATED ON ORSS 274 APROX. DEFLECTION CONTROL RIB RT WING; [02] STEP 1 COMPLETED; [03] LATE ENTRY : REMOVED ANGLE TRAILING EDGE LOCATED ON ORSS 274 APROX. DEFLECTION CONTROL RIB RT WING IAW B737-700 SRM 51-40-02 AND NOT FOUND ALLOWABLE DAMAGE LIMITS IN SRM B737-700 ANGLE MUST BE REPLACED; [04] INSTALLED ANGLE TRAILING EDGE LOCATED ON ORSS 274 APROX. DEFLECTION CONTROL RIB RT WING IAW B737-700 SRM 51-40-02 AND DRAWING 115A2930 REV; [05] REPLACED ANGLE TRAILING EDGE LOCATED ON ORSS 274 APROX. DEFLECTION CONTROL RIB RT WING IAW B737-700 SRM 51-10-02 ITEM 8 SRM 51-40-02 AND DRAWING 115A2930 REV-; [06] STEP 3 COMPLETED; [07] STEP 4 COMPLETED; [08] STEP 5 TASK CARD COMPLETED

Part: ANGLE — CRACKED (L/H WING) · airframe 74,045 hrs · 43,671 cycles

CRACK SUPPORT ANGLE FIXED TRAILING EDGE LOCATED ORSS 271 LT WING ; 2021-384033 / [01] REMOVED SUPPORT ANGLE FIXED TRAILING EDGE LOCATED ORSS 271 LT WING IAW B737-700 SRM 51-40-02 AND NOT FOUND ALLOWABLE DAMAGE LIMITS IN SRM B737-700 SUPPORT ANGLE MUST BE REPLACED; PERFOMED VISUAL INSPECTION ON ADJACENT AREA AND NOT FOUND ANY DAMAGE; [02] OK TO INSTALL SUPPORT ANGLE FIXED TRAILING EDGE LOCATED ORSS 271 LT WING GRANTED; [03] STEP 1 AND 2 CERTIFIED; [04] REPLACED SUPPORT ANGLE FIXED TRAILING EDGE LOCATED ORSS 271 LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02; [05] CORRECTLY ACTION STEP 4 : INSTALLED SUPPORT ANGLE FIXED TRAILING EDGE LOCATED ORSS 271 LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02; [06] STEP 4 CERTIFIED; [07] STEP 5 COMPLETED

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 74,045 hrs · 43,671 cycles

CRACK INSPAR RIB 129.50 AT 18 INCHES OF FRONT SPAR LT HORIZONTAL STAB ; 2021-384030 / [01] REMOVED INSPAR RIB 129.50 HORIZONTAL STAB AREA AND FASTENER IAW B737-700 SRM 51-40-02.; [02] VERIFYED STEP 1; [03] PERFORM CUT OUT DAMAGE : PERFORMED CUT OUT DAMAGE FROM VERTICAL STIFFENER OF THE RIB LOCATED RIB 129.50 AT 18 INCH OF FRONT SPAR ILIZER; [19] STEP 18 CERTIFIED RII.; [20] INSTALLED REPAIR PART;ANGLE (1E/A);FILLER. (1E/A);T-SECTION (1E/A); SHIM (2E/A); AND FASTENER ON INSPAR RIB LOC.STAB STA 129.50 AND AT 18 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 55-10-09-2R-5 REPIAR 5; [21] PERFORMED REPAIR ON INSPAR RIB 129.50 AT 18 INCHES OF FRONT SPAR LT HORIZONTAL STAB IAW B737-700 55-10-09-2R-5 REPIAR 5 THIS REPAIR IS CAT,NG,NRC,2021-09-07 21:23:35,22Y,N,,0,0,,CRACK INSPAR RIB 129.50 AT 18 INCHES OF FRONT SPAR LT HORIZONTAL STAB ; 2021-384030"

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 74,045 hrs · 43,671 cycles

CRACK INSPAR RIB 129.50 AT 27 INCH OF FRONT SPAR AT LT HORIZONTAL STABILIZER ; 2021-384031 / [18] INSTALLED REPAIR PART ;ANGLE (1E/A);FILLER. (1E/A);T-SECTION (1E/A); SHIM (2E/A) AND FASTENER ON INSPAR RIB LOC.STAB STA 129.50 AND AT 27 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5; [19] PERFORMED REPAIR ON INSPAR RIB 129.50 AT 27 INCH OF FRONT SPAR AT LT HORIZONTAL STAB,NG,NRC,2021-09-08 14:07:00,22Y,Y,MX,0,0,,CRACK INSPAR RIB 129.50 AT 27 INCH OF FRONT SPAR AT LT HORIZONTAL STABILIZER ; 2021-384031"

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT ; 2021-383982 / [01] FABRICATED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT; FROM MATERIAL: ALUMINUM; P/N:2024 T3 CLAD; 0.80 P/0:2021-138114; IAW B737-700 AMM 25-52-01-201-801 DWG: 453A1610 SHEET: 8 REV: C; [02] JOT TASK CARD COMPLETED.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT ; 2021-383983 / [01] FABRICATED FLOOR PANEL 140AF OF AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801DWG. # 453A2610 REV. C MATERIAL CONOLITE 0.090 P/N A90RG1W P/O 2021-152338; [02] VERIFIED STEP1.COMPLETED<BR>FABRICATED FLOOR PANEL 140AF OF AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801DWG. # 453A2610 REV. C MATERIAL CONOLITE 0.090 P/N A90RG1W P/O 2021-152338

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 74,045 hrs · 43,671 cycles

CRACK INSPAR RIB 129.50 AT 35 INCH OF FRONT SPAR AT LT HORIZONTAL STABILIZER ; 2021-384032 / [18] CERTIFIED STEP 14 AS RII. OK TO INSTALL GRANTED.; [19] INSTALLED REPAIR PART;A,NG,NRC,2021-09-07 21:25:09,22Y,Y,MX,0,0,,CRACK INSPAR RIB 129.50 AT 35 INCH OF FRONT SPAR AT LT HORIZONTAL STABILIZER ; 2021-384032"

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 74,045 hrs · 43,671 cycles

CRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT ; 2021-383985 / [01] FABRICATED FLOOR PANEL 140BF OF AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801DWG. # 453A2610 REV. C MATERIAL CONOLITE 0.090 P/N A90RG1W P/O 2021-152338; [02] VERIFIED STEP 1.COMPLETED<BR>FABRICATED FLOOR PANEL 140BF OF AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801DWG. # 453A2610 REV. C MATERIAL CONOLITE 0.090 P/N A90RG1W P/O 2021-152338

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 74,045 hrs · 43,671 cycles

CRACK INSPAR RIB 129.50 AT 27 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-384025 / [14] INSTALLED REPAIR PARTS; ANGLE (1E/A) FILLER (1E/A) T SECTION (1E/A) SHIM (2E/A) AND FASTENERS ON INSPAR RIB LOC. STAB STA 129;50 AND 27 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W. B737-700 SRM 55-10-09-2R-5 REPAIR 5; [15] CERTIFIED STEP 14; RII; [16] PERFORMED REPAIR LOC. INSPAR RIB 129.50 AT 27 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5.; [17] CERTIFIED WORK PERFORMED <BR>CERTIFIED RII INSPECTION

Part: SPAR WEB — CORRODED (L/H WING) · airframe 74,045 hrs · 43,671 cycles

CORROSION FRONT SPAR WEB LOC FUEL BOOST PUMP IFSS 120 APPROX AT LT WING ; 2021-384016 / PERFORMED REPAIR FRONT SPAR WEB LOC FUEL BOOST PUMP IFSS 120APPROX AT LT WING IAW EA 21-157-02611. RII

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,406 hrs · 43,302 cycles

AFT BATTERY PACK FAILED TEST (R) M1673 ; / R&R BATTERY PACK AT M 1673 PER AMM 33-51-06.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,406 hrs · 43,302 cycles

ROW 16 BATTERY PACK FAILED TEST M1670 ; / R AND R'D BATTERY M1670 PER AMM33-51-06

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,406 hrs · 43,302 cycles

AFT BATTERY PACK FAILED (L) M1672 ; / R&R BATTERY PACK AT M 1672 PER AMM 33-51-06.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,406 hrs · 43,302 cycles

OVER WING BATTERY PACK FAILED TEST (R) M1669 ; / R AND R'D BATTERY M1669 PER AMM33-51-06

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,406 hrs · 43,302 cycles

FWD BATTERY PACK FAILED TEST (R) M1675 ; / R AND R'D BATTERY M1675 PER AMM33-51-06

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,990 hrs · 42,493 cycles

RT EXTERIOR OVERWING EMERGENCY LIGHT INOPERABLE. RELAMPED RT EXTERIOR OVERWING EMERGENCY LIGHT, PER AMM 33-51-04. OPERATIONS CHECK GOOD.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 71,973 hrs · 42,483 cycles

RIGHT WING T/E UPPER FIXED PANEL SUPPORT BRACKET IS CRACKED / REMOVED AND REPLACED RIGHT WING T/E UPPER FIXED PANEL SUPPORT BRACKET PER SRM 51-40-02

Part: SEAT TRACK — LOOSE (ROW 18DEF) · airframe 71,219 hrs · 41,994 cycles

SEAT ROW 18DEF IS LOOSE IN THE FLOOR TRACKS. SECURED SEAT AND TRACKS IAW AMM 25-22-00

Part: BULB — INOPERATIVE (CABIN) · airframe 71,174 hrs · 41,964 cycles

SUPPLEMENTAL INFORMATION: EMERGENCY EXIT LIGHTS FWD OF L/H OWE & ON AFT LAV (L1189 & L1190) HAVE BULBS OUT. / RELAMPED EMERGENCY EXIT LIGHTS FWD OR L/H OVER WING EXIT AND AFT LAV PER AMM 33-51-01-960-801 PERFORMED GOOD TEST PER AMM 33-51-01-960-801 STEP 2.C 2.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,933 hrs · 41,158 cycles

FORWARD CABIN R/H BULLNOSE EMERGENCY LIGHT INOP AT SEAT 11. / RELAMPED LIGHT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,438 hrs · 40,852 cycles

EMERGENCY EXIT SIGN INOP. R&R BATTERY PACK IAW AMM.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 69,438 hrs · 40,852 cycles

EMERGENCY EXIT LIGHT INOP (EXTERIOR). REPLACED POWER SUPPLY FUSE PER AMM.

Part: FAIRING — DELAMINATED (L/H WING) · airframe 69,438 hrs · 40,852 cycles

L/H WING TO BODY FAIRING 192BL HAS DELAM AT L/H TOP CORNER / APPLIED RESIN SWEEP TO SMALL AREA ON CORNER TO L/H WING TO BODY FAIRING PANEL (192BL) I/A/W B737-700 SRM 51-70-08-0G-0 & TOUCHED UP FINISH I/A/W B737-700 AMM 51-21-99-300-801.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,438 hrs · 40,852 cycles

LT WING OUTBOARD AFT FLAP INBOARD CORNER, LOWER SURFACE SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

WING TO BODY PANEL 193AR; AFTER SMALL COMPOSITE REPAIR WAS PERFORMED FOUND 2 FOOT DIAMETER AREA OF DELAMINATION CENTERED IN PANEL / RECEIVED AND VERIFIED PNL PART 149A7655-14; PANEL NUMBER 193AR; PREPARED PNL FOR PAINT AND PAINTED HEART BLUE IAW SWA DRAWING 11100019 REV D BOEING AMM 53-14-00. ATAG A03212

Part: SUPPORT ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT AFT BULHEAD LOWER ANGLE AT STA 947; RBL12; WL 155 UNDER SIDE CORRODED / EVALUATED CORROSION ON AFT CARGO BULKHEAD LOWER ANGLE STA 947 RBL12; FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED LIMITS. LOCATED DRILLED AND INSTALLED NEW ANGLE P/N 149A8118-27 ATAG # A22917 I/A/W SRM 51-40-02-0G-0 & DWG 149A8117 SHEET 4 REV C APPLIED CIC I/A/W AMM 51-21-91-620-802.

Part: BULKHEAD — OUT OF TOLERANCE (AFT FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

SI# 112107 1016 BULKHEAD STEP 36D; BOLT HOLE 9R AT STR-3R IS OUT OF TOLERANCE. HOLE MEASURES .393; TOLAERANCE IS .3745-.3755 INCHES / REAMED HOLE TO 406 TO 1016 BULKHEAD HOLE 9L STR 3R I.A.W. SI #12107-53 STEP 40A. N.D.T FOR CRACKS NO DEFECTS NOTED I.A.W PT 6 51-00-00 PAR 23 USED AAR TOOL #36303 DUE 4-17-20 CONTINUED WITH SI 12107-53

Part: BULKHEAD — OUT OF TOLERANCE (AFT FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

SI# I12107;1016 BULKHEAD; STEP 29D; 9L HOLE AT STR-3L IS OUT OF TOLERANCE; HOLE MEASURES .390; TOLERANCE IS .3745-.3755 INCHES. / ACCOMPLISHED S.W EA 1-753-35539 REV IR FOR 9L HOLE AT 1016 BULKHEAD STR .3L

Part: BRACKET — CRACKED (FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

SUPPORT BRACKET AT STA 663 RBL 31 IS CRACKED (P/N 111A1304-2) / REMOVED AND REPLACED BRACKET AT STA 663; RBL 31 IAW BOEING DRAWING 111A1000 REV. F AND B737 SRM 51-40-02-0G-0

Part: DOUBLER — CRACKED (WHEEL WELL LH) · airframe 69,438 hrs · 40,852 cycles

L/H STA 663 VAPOR BARRIER HORSE SHOE SEAL DOUBLER CRACKED P/N 111A1512-1 / LOCATED AND DRILLED NEW SEAL DOUBLER PART # 111A1512-1 PER DWG 11A1000 REV A AND SRM 51-40-05-0G-0. HORSESHOE SEAL ASSY INSTALLED ON CARD NO. X999095

Part: ATTACH ANGLE — CRACKED (LT WNG - BDY) · airframe 69,438 hrs · 40,852 cycles

LEFT WING TO BODY FAIRING ATTACH ANGLE BS 649 TO 663, LBL 31.83 FOUND CRACKED. R & R THE ATTACH ANGLE IAW SRM.

Part: DOUBLER — CRACKED (WHEEL WELL RH) · airframe 69,438 hrs · 40,852 cycles

R/H VAPOR BARRIER STA 663 HORSE SHOE SEAL DOUBLER FOUND CRACKED. P/N 111A1512-2 / LOCATED AND DRILLED NEW -6 SEAL DOUBLER PER SRM 51-40-05-0G-0 AND DWG 111A1000 REV A. HORSESHOE SEAL ASSY INSTALLED ON CARD NO. X999097

Part: ANGLE — CRACKED (WHEEL WELL LH) · airframe 69,438 hrs · 40,852 cycles

L/H 663 VAPOR BARRIER ATTACH ANGLE P/N 111A1301-5 CRACKED ON I/B SIDE LBL 7 / LOCATED AND DRILLED NEW ATTACH ANGLE PART # 111A1301-5 DWG 111A1001 REV F AND SRM 51-40-05-0G-0. NEW -5 ANGLE INSTALLED ON CARD NO. X999095

Part: RETAINER — CRACKED (LEFT WING) · airframe 69,438 hrs · 40,852 cycles

LEFT WING CANOE FAIRING 543BB O/B AFT BULB SEAL RETAINER IS CRACKED. / INSTALLED NEW BULB SEAL RETAINER ON O/B AFT SEAL FOR #2 FLAP TRACK SUPPORT AFT FAIRING 543BB IAW BOEING 737-700 SRM 51-40-02-0G-0 PARA 9 A-TAG# A16558

Part: RETAINER — CRACKED (LEFT WING) · airframe 69,438 hrs · 40,852 cycles

LEFT WING CANOE FAIRING 542BB O/B HALF BULB SEAL RETAINER IS CRACKED. / REMOVED & REPLACED CRACKED BULB SEAL RETAINER ON L/H WING CANOE FAIRING 542BB IAW BOEING DWG 113A9350 REV F & B737 SRM 51-40-02-0G-0

Part: STRAP — CRACKED (VERTICAL STABILI) · airframe 69,438 hrs · 40,852 cycles

VERTICAL STAB PANEL 324AR; SUPPORT STRAP ON BACK OF PANEL IS CRACKED/BROKEN. / REMOVED AND INSTALLED NEW SUPPORT STRAP P/N 172A6124U10 ON THE PANEL # 324AR IAW B737-700 SRM 51-40-02-0G-0 AND DWG # 172A 6123 REV:A.

Part: CHANNEL — CRACKED (VERTICAL STABILI) · airframe 69,438 hrs · 40,852 cycles

VERTICAL STAB PANEL 324AR; SUPPORT CHANNEL ON BACK OF PANEL IS BROKEN. / EVALUATED DAMAGE. OUT OF LIMITS; REPLACED W/NEW SUPPORT CHANNEL P/N 172A6124U6 IAW BOIENG DWG 172A6124803 REV F AND SRM 51-40-02-0G-0 ATAG A20165.

Part: STRAP — CRACKED (VERTICAL STABILI) · airframe 69,438 hrs · 40,852 cycles

VERTICAL STAB PANEL 323CR; SUPPORT STRAP ON BACK OF PANEL IS CRACKED/BROKEN. / REMOVED AND INSTALLED NEW SUPPORT STRAP P/N 172A6124Y8 ON THE PANEL # 323CR IAW B737-700 SRM 51-40-02-0G-0 AND DWG #172A6124 REV: 'F'

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; CAPSTRIP NOT MARKED IS CORRODED.(DOT 39-061) / REPLACED AFT CARGO COMPARTMENT CAPSTRIP (DOT 39-061) W/ P/N 453A2411-1 ATAG #A22872 ON THE BENCH I/A/W AIPC 25-52-06-03. INSTALLED ON JPANEL-141-CLOSE N/R #39852/1600/0022.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; CAPSTRIP MARKED #2 L/H IS CORRODED. / BEGAN REMOVING CORROSION ON CAP STRIP IN AFT CARGO FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED LIMITS. REPLACED ON BENCH WITH P/N 453A2611-10 A TAG A13248 IAW AIPC 25-52-10-02 TO BE INSTALLED ON JPANEL-141-CLOSE

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; AFT FLOOR SPLICE PLATE IS CORRODED. / REPLACED AFT CARGO ENTRANCE AFT FLOOR SPLICE COMMON TO THRESHOLD ON BACK W / P/N 453A2611-2 I/A/W AIPC 25-52-10-02 ATAG # A82985

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; FLOORBOARD 140CF IS CORRODED ALONG TOP AND BOTTOM EDGES. / FABRICATED FLOOR PANEL 140CF FROM 2024-T3 .080 ATAG A23610 TREATED AND PRIMED; MARKED WITH P/N 453A2610-2 IAW DWG 453A2610 REV E. SHEET 9. SRM 51-40-05-0G; SRM 51-20-01-0G; REPLACED ON BENCH.

Part: PANEL — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; BULKHEAD PANEL 141PW IS CORRODED AT BOTTOM FWD END. / REMOVED CORROSION FROM AFT CARGO COMPARTMENT BULK HEAD PANEL 141 PW AT BOTTOM FWD END IAW SRM 51-20-02 ORIGINAL MATERIAL .105 LOSS OF .020 REMAINING .085 IS OUT OF LIMITS DUE TO NO PUBLISHED LIMITS FOUND REPAIRED PANEL IAW AAR EA 190693 REV P1 AND IR AND SWA EA 1-753-35492 REV IR FOR TREAT AND PRIME OF BLENDED AREA

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS 1006, STR 26R. R&R STRINGER CLIP IAW SRM, AMM, & DWG.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; CAPSTRIP MARKED #2 IS CORRODED. / BEGAN REMOVING CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA REPLACED ON BENCH WITH P/N 453A2611-11 ATAG A12441 IAW AIPC 25-52-10-02 TO BE INSTALLED ON PANEL 141 CLOSE

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; FLOOR SPLICE ON 140CF IS CORRODED. / REPLACT AFT CARGO COMPARTMENT FLOOR SPLICE FOR FWD SIDE OF PNL 140CF W/ P/N 146A9401-4 SI # 3530573 I/A/W BOEING DWG 146A 7500 SHEET 1 REV B.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; CAPSTRIP MARKED AFT R/H IS CORRODED. / STARTED REMOVING CORROSION ON AFT CARGO AFT R/H CAPSTRIP; FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED LIMITS. VERIFIED NEW CAPSTRIP P/N 453A2611-3; SI# 7252699 I/A/W AIPC 25-52-10-02 A TAG #WN 4120. LOCATED AND DRILLED NEW CAPSTRIP I/A/W SRM 51-40-05-0G-0 AD BOEING DWG 453A2611 SHEET 3 REV D. CAPSTRIP TO BE INSTALLED ON JPANEL-141-CLOSE; N/R #39852/1600/0022.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; CAPSTRIP MARKED #1 L/H IS CORRODED. / BEGAN TO REMOVE CORROSION ON CAPSTRIP IN AFT CARGO FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA REPLACED ON BENCH WITH P/N 453A2611-6 ATAG WN2449 IAW AIPC 25-52-10-02 TP BE INSTALLED ON JPANEL-141-CLOSE

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; CAPSTRIP FOR FWD EDGE OF 140AF IS CORRODED. / VERIFIED P/N 453A211-12 A AG A22793 IAW AIP C 25-52-10 -02 REPLACED ON BENCH AFT CARGO CAP STRIP FWD EDGE OF PAN 140AF.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; CAPSTRIP MARKED #1 R/H IS CORRODED. / BEGAN REMOVING CORROSION ON AFT CAGO CAP STRIP-FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA REPLACED ON BENCH P/N 453A2611-9 ATAG A13202

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; FLOOR SPLICE ON 140BF IS CORRODED. / REPALCED AFT CARGO FLOOR SPLICE ON PNL 140BS OF P/N 146A9401-8 SI # 3530741 ATAG # WN6638 I/A/W BOEING DWG 146A 7500 SHEET 1 REV B. ATAG # WN6638

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; FWD FLOOR SPLICE PLATE IS CORRODED. / VERIFIED FLOOR SPLICE P/N 453A2611-11 A TAG A22825 IAW AIPC 25-52-10-02 REPLACED ON BENCH.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

E&E COMPARTMENT HAD SPOT OF CORRODED AT BS 360 TO BS 380, STR 28L. R&R SPLICE IAW SRM AND DWG.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT; CAPSTRIP NOT MARKED IS CORRODED.(DOT 39-060) / BEGAN REMOVING CORROSION ON CAPSTRIP FROM AFT CARGO FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA REPLACED ON BENCH WITH P/N 453A2611-6 ATAG A13205 IAW AIPC 25-52-10-02 TP BE INSTALLED ON JPANEL-141-CLOSE

Part: WEB — CORRODED (FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

E&E COMPARTMENT WEB AT CORRODED BS 360, STR 28L. R&R WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

FORWARD PIT STRINGER CLIP CORRODED AT BS. 500B, STR. 22L. R&R STRINGER CLIP IAW SRM & DWG.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT AFT RH SKATE ANGLE WL 155 RBL 15.5 STA. 847+7.5 THERE IS A SCREW HOLE WITH CORROSION. / REMOVED CORROSION FROM AFT CARGO COMPARTMENT AFT R/H SKATE ANGLE (SHIELD) RBL 15.5 STA 847+7.5' FOUND ORIG 'T' .052; REMAINING .046 LOSS OF .006' OUT OF LIMITS I/A/W SRM 53-60-15-1A-1. REMOVED AND INSTALLED NEW SHIELD P/N 146A8127Y5 ATAG # WN9594 I/A/W SRM 51-40-02-0G-0 & DWG 146A0081 SHEET 7 REV C. APPLIED CIC TO NEW SHIELD I/A/ WAMM 51-21-91-620-802 PARA 3.

Part: ANGLE — CORRODED (AFT CARGO) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT STA. 947 RBL 11 WL 155 AFT BULKHEAD AREA HAS CORROSION ALONG THE BOTTOM. / REMOVED CORROSION ON AFT CARGO STA 947 RBL 11 BULKHD AREA; FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED LIMITS. REPLACED ANGLE W/NEW ANGLE P/N 149A8118U29; LOCATED; DRILLED AND INSTALLED I/A/W SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG 149A8117 SHEET 4 REV C. APPLIED CIC I/A/W AMM 51-21-91-620-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

PASSENGER CABIN SEAT TRACK CORRODED AT TOP OF CROWN AND BOTTOM OF CHANNEL BETWEEN BS 767 TO BS 887, LBL 45. REPAIRED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (MID FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

PASSENGER CABIN LBL45 STA 540 TO 639 WL 208; SEAT TRACK IS CORRODED AT TOP OF CROWN AND BOTTOM OF CHANNEL. / REMOVED CORROSION FROM TOP OF CROWN AND BOTTOM INSIDE OF CROWN IAW BOEING 737 SRM REF 51-10-02-0G-0 MAX LOSS ON CROWN TOP SURFACE .037 AT ST 540 LBL45 FOUND TO BE OUT OF LIMITS IAW BOEING 737 SRM REF 53-00-52-1A-1 FIG 103 AAR TOOL # 27213 D/D 05SEP19 MASS LOSS INSIDE BOTTOM OF CROWN .018 ALLOWED .040 FOUND TO BE WITHIN LIMITS IAW BOEING 737 SRM REF 53-00-52-1A-1 FIG 103 AAR TOOL # 21461 D/D 01AUG20 INSTALLED PASSENGER CABIN LBL45 STA 540 TO 639 WL208 SEAT TRACK MPN-144A5350-3 SI# 753738 ATAG 020448 IAW BOEING DWG NO 144A5300 ID: 0001 REV: E AND BOEING SRM REF 51-40-01-0G-0

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 69,438 hrs · 40,852 cycles

LEFT BS 663 VAPOR BARRIER CRACKED. R & R THE WEB IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

SEAT TRACK CORRODED BETWEEN BS 727C+5 TO BS 807, RBL 24, BOTTOM OF CHANNEL AND TOP OF CROWN. REPAIRED SEAT TRACT IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 69,438 hrs · 40,852 cycles

R/H BS 663 VAPOR BARRIER CRACKED. / REPAIRED BARRIER PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT CHANNEL CORRODED BS 727D, BETWEEN STR 25L TO STR 18L. R&R CHANNEL IAW SRM & DWG.

Part: MOUNT — CRACKED (R1 DOOR) · airframe 69,438 hrs · 40,852 cycles

R1 DOOR AFT SLIDE MOUNT UPPER ISOLATOR CRACKED. R&R AFT SIDE MOUNT IAW SRM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 69,438 hrs · 40,852 cycles

R1 DOOR #5 BEAM ASSEMBLY CRACKED APPROXIMATELY 3/8" LONG LOCATED CENTERED IN THE RADIUS NEXT TO THE MOST INBOARD HOLE. R&R #5 BEAM ASSEMBLY IAW SRM AND DWG.

Part: SUPPORT BRACKET — BROKEN (LWR FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

LOWER FUSELAGE STA 550 LBL5; FAIRING SUPPORT BRACKET IS BROKEN. / REMOVED AND REPLACED FAIRING SUPPORT BRACKET LOWER FUSELAGE STA 550 LBL 5 IAW B737 SRM 51-40-02; IPC 53-12-11-25

Part: RETAINER — CRACKED (LT WING) · airframe 69,438 hrs · 40,852 cycles

LH WING TRAILING EDGE WING PANEL BULB SEAL RETAINER CRACKED AFT OF #1 SAIL TAIL AREA / REMOVED AND REPLACED SEAL RETAINER AT L/H WING TRAILING EDGE WING PANEL AFT NO 1 SAIL TAIL IAW SRM 51-40-02-0G-0 A1230

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

AFT CARGO COMPARTMENT L/H Z ANGLE CORRODED BETWEEN BS. 727C+6 TO BS. 847, LBL 21. REPAIRED LT "Z" ANGLE IAW SRM.

Part: RETAINER — CRACKED (LT WING) · airframe 69,438 hrs · 40,852 cycles

LH WING TRAILING EDGE BULB SEAL RETAINER CRACKED AFT OF #1 SAIL TAIL AREA / REMOVED RETAINER; SEAL; AND FITTING. REPLACED WITH NEW RETAINER P/N 115A2951-15 ATAG 19457; SEAL P/N 115A2990-15 ATAG 19434; AND FITTING P/N 115A2953-1 ATAG 90707 IAW B737 SRM 51-40-02-0G-0.

Part: SKIN — CORRODED (EXT FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

EXTERIOR FUSELAGE SKIN STA 500B +12 STR 27L W/L 148 IS CORRODED AT FASTENER HOLE. / REMOVED CORROSION FROM EXTERIOR SKIN @ STA 500 B + 12 STR 27L IAW B737 SRM 51-10-02-0G-0. ORIG .063' REMAIN .054' LOSS .009' OUT OF LIMITS IAW B737 SRM 53-00-01-1A-5. REPAIRED AREA IAW EA 190658 REV P1; IR & SWA EA 1-753-35432 REV IR

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,438 hrs · 40,852 cycles

R1 DOOR CUTOUT UPPER FORWARD STUB FRAME CRACKED. R&R STUB FRAME IAW SRM & DWG.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 69,438 hrs · 40,852 cycles

R/H HORIZONTAL STABILIZER STA 92.70 RIB, AFT STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,644 hrs · 40,326 cycles

RT AREA EMERGENCY LIGHT INOP AT ROW 8. RELAMPED LIGHT PER AMM.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 68,157 hrs · 39,994 cycles

L2 DOOR SLIDE SIGHT GAUGE PROTECTOR OUT OF POSITION. R&R SLIDE PER MT.

Part: COVER — MISSING (CABIN) · airframe 68,138 hrs · 39,984 cycles

ROW 12 EMERGENCY EXIT ROW LIGHT COVER MISSING. R&R COVER PER AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 66,619 hrs · 39,000 cycles

R1 DOOR GIRT BAR LOOSE. REINSTALLED SLIDE IAW MT.

Part: COVER — LOOSE (R2 DOOR) · airframe 65,522 hrs · 38,275 cycles

R2 DOOR SLIDE COVER LOOSE. SECURED COVER PER MM.

Part: BULKHEAD — CRACKED (BS 663) · airframe 65,030 hrs · 37,954 cycles

RIGHT MLG WW CEILING WEB CRACKED AT BS 664, RBL 46. REPAIRED THE CEILING WEB IAW SWA EA.

Part: SUPPORT BRACKET — BROKEN (LT WING) · airframe 64,887 hrs · 37,856 cycles

L/H I/B FLAP CANOE FAIRING SUPPORT BRACKET BROKEN / DRILLED & INSTALLED NEW BRACKET REF SRM 50-40-02

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 64,455 hrs · 37,573 cycles

FORWARD BULKHEAD EMERGENCY LIGHT LENS FOUND LOOSE. REPAIRED THE LENS IAW EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 64,396 hrs · 37,539 cycles

AFT CARGO DOOR FORWARD SCUFF PLATE SECTION CRACKED. R & R THE SCUFF PLATE IAW AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 64,396 hrs · 37,539 cycles

FOUND CRACK INDICATION AT DENT DEFECT DOCUMENTED ON ORDER # W2591818 'AFT CARGO DOOR CENTER SCUFF PLATE' USING HFEC PART 6; 51-00-00 PROC. #3 / REMOVED AND REPLACED AFT CARGO DOOR CENTER SCUFF PLATE IAW AMM 53-11-02 REF SA-M 326 A1132970

Part: ACTUATOR — INOPERATIVE (CROSSFEED VALVE) · airframe 64,004 hrs · 37,297 cycles

FUEL CROSSFEED VALVE INOPERATIVE. DIVERTED. R & R THE FUEL CROSSFEED VALVE ACTUATOR IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,827 hrs · 37,187 cycles

R2 DOOR EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (ROW 1) · airframe 62,874 hrs · 36,551 cycles

LEFT EMERGENCY AISLE LIGHT INOPERATIVE AT ROW 1. REPLACED THE LIGHT IAW AMM.

Part: FITTING — LOOSE (R2 DOOR) · airframe 62,874 hrs · 36,551 cycles

R2 DOOR GIRT BAR FITTINGS LOOSE. SECURED FITTINGS IAW SRM.

Part: FITTING — LOOSE (L2 DOOR) · airframe 62,874 hrs · 36,551 cycles

L2 DOOR GIRT BAR FITTINGS LOOSE. SECURED FITTINGS IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 62,874 hrs · 36,551 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: FITTING — CRACKED (LT WING) · airframe 62,874 hrs · 36,551 cycles

LT WING CLIP ASSEMBLY CRACKED PANEL 551FB AT WSTA 220 1.3" AFT OF REAR SPAR. R&R CLIP ASSEMBLY IAW SRM AND DWG.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

FORWARD CARGO BAY BAFFLE CRACKED BETWEEN BS 500B TO BS 500C, RBL 14. R&R BAFFLE IAW SRM AND DWG.

Part: BRACKET — CRACKED (LT WING) · airframe 62,874 hrs · 36,551 cycles

O/B ATTACH BRACKET CRACKED FOR UPPER L/H WING T/E PANEL AT APPROX. RSS STA 280 (MARKED) / REMOVED CRACKED O/B ATTACH BRACKET FOR L/H WING UPPER TE PANEL AT APPROX. RSS STA 280 IAW SOPM 20-50-01. TRANSFERED HOLES TO NEW BRACKET IAW SRM 51-40-05-G-0. REMOVED SEAL AND RETAINER FROM OLD BRACKET AND INSTALLED ON NEW BRACKET IAW SRM 57-40-02-0G-0 PAR 4 AND FIG 8. INSTALLED NEW BRACKET AT APPROX RSS STA 280 IAW SOPM 20-50-01

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

FORWARD SIDE OF AFT PRESSURE BULKHEAD INTERCOSTAL CORRODED AT BS 1028, LBL 40. R&R INTERCOSTAL IAW SRM & DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

SHEAR WEB CORRODED BETWEEN BS 1006 TO BS 1016, LBL 60. R&R WEB PER SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,874 hrs · 36,551 cycles

CABIN FLOOR PANEL 241ABF HAS DAMAGE TO AFT O/B EDGE / CABIN FLOOR PANEL 241ABF DAMAGE TO AFT O/B EDGE REPAIRED IAW SRM 53-00-50-2R-6.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 62,874 hrs · 36,551 cycles

CABIN FLOOR BOARD PANEL 221DF HAS DAMAGE TO UPPER SURFACE MIDDLE OF PANEL SKIN CRACKED / REPAIRED DAMAGE TO UPPER SURFACE MIDDLE OF PANEL ON CABIN FLOOR BOARD PANEL 221DF IAW SRM 53-00-50-2R-1 REPAIR 1

Part: PANEL — BROKEN (RH PYLON) · airframe 62,874 hrs · 36,551 cycles

#2 ENGINE PYLON PANEL 441 BR CORNER BROKEN / REPAIRED BROKEN CORNER ON #2 ENGINE PYLON PANEL 441BR PER SRM 54-50-70-2R-1 AND SRM 51-70-05-2R-6 AND SRM 51-70-14-2R-4 PARA 5

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,874 hrs · 36,551 cycles

CABIN FLOOR PANEL 222CF HAS DAMAGE TO EXISTING REPAIR 20' FROM AFT EDGE UPPER SURFACE / REMOVED AND REPLACED EXISTING REPAIR WITH NEW REPAIR 20' FROM AFT EDGE UPPER SURFACE ON CABIN FLOOR PANEL 222CF IAW SRM 53-00-50-2R-3.

Part: PANEL — ELONGATED (LEFT WING) · airframe 62,874 hrs · 36,551 cycles

LOWER L/H WING PANEL 521RB HAS ENLARGED FASTENER HOLE / REPAIRED L/H WING LOWER L/E PANEL 521RB IAW SRM 57-41-01-2R-1 PARA 4E TABLE 202; IAW SRM 51-70-05-2R-0

Part: TRACK — DAMAGED (CABIN) · airframe 62,874 hrs · 36,551 cycles

SEAT TRACK HAS MECHANICAL DAMAGE AT BS 500D +13 RBL 45 WL 208 / SEAT TRACK AT BS 500D +13 RBL 45 WL 208 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK AT BS 500C+10' TO 520; RBL 45 PER SRM 53-00-52-1A-1; SRM 53-00-52-2R-4; SRM 53-00-52-2R-4; AND EA 1-A53-11779R1

Part: TRACK — DAMAGED (CABIN) · airframe 62,874 hrs · 36,551 cycles

SEAT TRACK HAS MECHANICAL DAMAGE AT BS 500D +19 LBL45 WL208 ( IN WELL AND CROWN OF TRACK) / MECHANICAL DAMAGED AT STA B500D+19 LBL45 WL208 IS OUT OF LIMITS PER SRM 53-00-52-1A-1 FIG 103 DETAIL A CUT AND REMOVED DAMAGED AREA PER SRM 53-00-52-2R-4; 4B AND 4D FABRICATED; LOCATED AND DRILLED REPAIR PART PER SRM 53-00-52-2R-4; REMOVED AND INSTALLED AFT END BOLT OF PIVOT LINK PER SRM 51-40-02-0G-0. INSTALLED REPAIR PER SRM 53-00-52-R4; AND EA 1-A53-11779REV IR REMOVED AND INSTALLED STIFFENER PER SRM 51-40-02-0G-0 AT SEAT TRACK BS500D+19 LBL45 WL208

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

INTERCOSTAL CORRODED AT BS 1028, LBL 24. R&R INTERCOSTAL IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

R1 DOOR STRAP ON INBOARD SIDE OF INNER CHORD CORRODED AT BS 294. R&R CHORD IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

STRINGER CLIP CRACKED AT BS 277, STR 10R. R&R CLIP IAW SRM & DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

L1 DOOR AFT GIRT BAR ATTACH ANGLE CORRODED AT BS 344. R&R ANGLE IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

L2 DOOR LOWER SILL WEB CORRODED BETWEEN BS 967 TO BS 986, LBL 47. R&R WEB IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

LOWER VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT BS 663, LBL 9. REPAIRED ANGLE IAW EA.

Part: FLOOR SUPPORT — CRACKED (BS 294-312) · airframe 62,874 hrs · 36,551 cycles

FLOOR SUPPORT CRACKED AT BS 294 TO 312, RBL 15, WL 208. R & R THE FLOOR SUPPORT IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

FORWARD CARGO COMPARTMENT LT FLOOR TO SIDEWALL SUPPORT Z CHANNEL CORRODED BETWEEN BS 465 TO BS 485. R&R Z CHANNEL IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

FORWARD CARGO COMPARTMENT RT FLOOR TO SIDEWALL SUPPORT PLATE Z CHANNEL CORRODED BETWEEN BS 500A+6 TO BS 500C. REPAIRED Z CHANNEL IAW SRM.

Part: SHIELD — ELONGATED (FWD CARGO RH) · airframe 62,874 hrs · 36,551 cycles

FWD CARGO FLOOR SHIELD HAS ELONGATED HOLE ON AFT END STA 440 RBL 24.5 / REMOVED DAMAGED SHIELD & REPLACED WITH NEW SHIELD P/N 143A8126V21 INSTALLED IAW SRM'S 51-40-02-0G-0; 51-40-05-0G-0 & BOEING DWS 143A0080

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 62,874 hrs · 36,551 cycles

FLOOR SUPPORT CRACKED AT BS 344 TO 360, LBL 11.5, WL 208. R & R THE FLOOR SUPPORT IAW SRM.

Part: PANEL — DELAMINATED (LEFT WING) · airframe 62,874 hrs · 36,551 cycles

FWD I/B CORNER; HAS DELAMINATION ON L/H WING L/E PANEL #521JB / REPAIRED FWD I/B CORNER OF L/H WING L/E PANEL 521JB IAW SRM 57-41-01-2R-1 REPAIR 1 PARA 4E TABLE 202 IAW SRM 51-70-05-2R-0

Part: STIFFENER — CORRODED (ASD THRESHOLD) · airframe 62,874 hrs · 36,551 cycles

***CORROSION*** ON LOWER STIFFENER AT STA 959; RBL53;WL206 / REMOVED CORROSION ON LOWER STIFFENER AT STA 959 RBL53 WL206 IN AN AREA OF 1'X2'X0.029' OF AN ORIGINAL THICKNESS OF 0.100'. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1 FIG 103 DETAIL E RECIEVED REPLACEMENT STIFFENER SI# 7530404 MPN 147A8530U10. STIFFENER TO BE INSTALLED ON CUSTOMER CARD DEFECT# N099648 SA-M 326 ITEM#5

Part: WEB — CORRODED (CABIN) · airframe 62,874 hrs · 36,551 cycles

***CORROSION*** ON FLOOR WEB AT STA1027; LBL6; WL207 / REMOVED DAMAGED WEB AT STA 1027; BL6; WL207. FOUND TO BE OUT OF LIMITS IN AN AREA 1X1.3X.004 ORG T=.020 IAW SRM 51-10-02-0G-0 WEB REPLACED ON DEFECT N099289 WEB STARTS AT BS 1006 TO BS 1027

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

R1 DOOR FORWARD LOWER EDGE FRAME CRACKED AT BS 291, RBL 54. REPAIRED STUB FRAME PER ER AND EA.

Part: DOUBLER — CORRODED (LOWER INT FUSELA) · airframe 62,874 hrs · 36,551 cycles

***CORROSION*** FOUND ON ANTENNA DOUBLER IN FWD CARGO BILGE STA 500A+9 TO 500A+18 LBL2 TO RBL2 / REMOVED DAMAGED ANTENNA DOUBLER AND REPLACED WITH REPLACEMENT SERVICABLE DOUBLER PN #143A3233-4 @ BS. 500A +9 TO 500A + 18; LBL2. IRIGINAL ANT. DOUBLER FOUND TO BE OUT OF LIMITS DUE TO NOR SRM LIMITS. PER SRM 51-40-02-0G-0 & DWG #143A3233 & 143A3230

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 62,874 hrs · 36,551 cycles

FLOOR SUPPORT CRACKED AT BS 344 TO 360, BL 0, WL 208. R & R THE FLOOR SUPPORT IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

R1 DOOR LOWER SILL INNER CHORD CORRODED BETWEEN BS 277 TO BS 360. R&R CHORD IAW SRM AND DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 62,874 hrs · 36,551 cycles

VAPOR BARRIER WEB CRACKED AT BS 663, RBL 36. REPAIRED WEB IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

FLOOR WEB CORRODED AT BS 1016, LBL 6. R&R WEB PER SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

AFT CARGO COMPARTMENT FLOORBOARD SUPPORT ASSEMBLY CORRODED AT BS 727D, WL 158. R&R SUPPORT ASSEMBLY IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

AFT CARGO COMPARTMENT SHIELD CORRODED BETWEEN BS 767 TO BS 794, WL 158 RT SIDE. R&R SHIELD PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

AFT CARGO COMPARTMENT FLOOR BOARD SUPPORT ASSEMBLY CORRODED AT BS 777, WL 158. R&R SUPPORT ASSEMBLY IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

FLOORBEAM T-CHORD CAP CORRODED AT BS 986, BETWEEN LBL 45 TO RBL 45. R&R FLOORBEAM PER SRM & EA.

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 62,874 hrs · 36,551 cycles

3 AREAS OF DELAMINATION ON R/H WING LOWER LEADING EDGE PANEL 621DB / REPIARED DELAMINATIONS ON R/H WING LOWER L/E PANEL 621DB IAW SRM 57-41-01-2R-1 TABLE 202; IAW SRM 51-70-05-2R-6

Part: PANEL — DELAMINATED (LEFT WING) · airframe 62,874 hrs · 36,551 cycles

3 AREAS OF DELAMINATION; 1 HAS MATERIAL MISSING ON L/H WING L/E PANEL #521DB / REPAIRED DELAMINATION ON L/H WING LOWER L/E PANEL 521DB IAW SRM 57-41-01-2R-1 PARA 4E TABLE 202; IAW SRM 51-70-05-2R-0

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

AFT CARGO COMPARTMENT FLOOR BOARD TO TRANSITION Z CHANNEL CORRODED BETWEEN BS 720 TO BS 767, WL 158. R&R Z CHANNEL IAW SRM AND DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

FORWARD L1 DOOR GIRT BAR ATTACHED ANGLE CORRODED AT BS 303. R&R ANGLE IAW SRM AND DWG.

Part: DOUBLER — CORRODED (LOWER INT FUSELA) · airframe 62,874 hrs · 36,551 cycles

***CORROSION*** FOUND ON ANTENNA DOUBLER IN FWD CARGO BILGE STA 505 TO 517 LBL 2 TO RBL 2 / REMOVED DAMAGE ANT. DOUBLER FCB BILGE AND REPLACED W/NEW ANT DOUBLER P/N 143A3233-4. ORIGINAL ANT DOUBLER FOUND TO BE OUT OF LIMITS IN AN AREA OF BS-505-517; LBL2 TO RBL2 PER SRM 51-40-02-0G-0 AND DWG# 143A3233 + 143A3230 NO LIMITS AVAILABLE

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

AFT CARGO COMPARTMENT FLOOR BOARD Z ANGLE CORRODED BETWEEN BS 720 TO BS 797, WL 158. R&R Z-ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

R1 DOOR LOWER SILL CHANNEL BETWEEN BS 290 TO BS 332. R&R CHANNEL IAW SRM AND DWG.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

AFT LAV AFT OUTBOARD FLOOR MOUNT CORRODED AT BS 1012, LBL 38. R&R MOUNT PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

AFT CARGO DOOR SUB THRESHOLD WEB CORRODED AT BS 827, RBL 28. R&R WEB IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

L2 DOOR INNER CHORD MOP SILL CORRODED INNER CHORD BETWEEN BS 957 TO BS 992. R&R CHORD IAW SRM AND DWG.

Part: STIFFENER — CRACKED (WHEEL WELL LH) · airframe 62,874 hrs · 36,551 cycles

STIFFENER CRACKED ON VAPOR BARRIER BS 663; LBL 36; WL 160. / REMOVED CRACKED STIFFENER; LOCATED + DRILLED NEW STIFFENER + INSTALLED IAW SRM 51-40-02-0G0; 51-40-03-0G-0 51-40-05-0G-0 AT BS663 LBL36 WL160 ON VAPOR BARRIER ALSO BOEING DWG# 111A1000 REV F

Part: STRAP — MISSING (FLASHLIGHT) · airframe 62,874 hrs · 36,551 cycles

LT AFT WINDSCREEN FLASHLIGHT STRAPS MISSING. INSTALLED STRAPS IAW AMM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

L1 DOOR LOWER SILL INNER CHORD CORRODED BETWEEN BS 277 TO BS 360. R&R CHORD IAW SRM AND DWG.

Part: STIFFENER — CORRODED (ASD THRESHOLD) · airframe 62,874 hrs · 36,551 cycles

***CORROSION*** ON LOWER STIFFENER AT STA 978; RBL47;WL206 / REMOVED CORROSION ON LOWER STIFFNER AT STA 978 RBL47 WL206 IN AN AREA OF 1'X2'X0.026' FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1 FIG 103 DETAIL E RECEIVED REPLACEMENT STIFFNER SI# 7531070 MPN 147A8530Y12. STIFFNER TO BE INSTALLED ON CUSTOMER CARD DEFECT #N099648. ORIGINAL THICKNESS OF STIFFENER IS 0.100'

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 62,874 hrs · 36,551 cycles

CABIN FLOOR BOARD '221DF' IS DAMAGE AT AFT O/B END. 'PUNCTURED' / REPAIRED PUNCTURE DAMAGE TO AFT O/B END OF CABIN FLOORBOARD 221DF IAW AMM 53-00-50-2R-1 REPAIR 1

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,874 hrs · 36,551 cycles

CABIN FLOOR BOARD '221BF' IS DAMAGED AT CORNER. / REPAIRED DAMAGED CORNER ON CABIN FLOOR BOARD 221BF IAW SRM 53-00-50-2R-1 REPAIR 1

Part: GUSSET — CRACKED (BS 500D) · airframe 62,874 hrs · 36,551 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,874 hrs · 36,551 cycles

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

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 62,874 hrs · 36,551 cycles

AFT CARGO FWD NET TIE DOWN IS CORRODED / REMOVED DAMAGED AFT CARGO FWD NET TIE DOWN PLATE IAW SRM 51-10-02-0G-0. INSTALLED NEW AFT CARGO FWD NET TIE DOWN PLATE P/N 453A2611-1 IAW SRM 51-10-02-0G-0 AND BOEING DWG 453A2600 1D 0027 REV D

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 62,874 hrs · 36,551 cycles

VAPOR BARRIER WEB CRACKED AT BS 663, LBL 36. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,874 hrs · 36,551 cycles

LT WING NR 2 LEADING EDGE SLAT SKIN CRACKED ON LOWER SURFACE. REPAIRED SKIN IAW ER AND EA.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 62,409 hrs · 36,252 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: CONNECTOR — DIRTY (CROSSFEED ACT) · airframe 61,499 hrs · 35,728 cycles

CROSSFEED VALVE CIRCUIT BREAKER TRIPPED INFLIGHT. CLEANED FUEL CROSSFEED ACTUATOR CONNECTOR IAW AMM.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 61,283 hrs · 35,609 cycles

LT WING TRAILING EDGE UPPER FIXED PANEL AFT OF NR 1 PYLON OUTBOARD SUPPORT FITTING CRACKED. REPAIRED FITTING PER EA.

Part: FITTING — CRACKED (LT MLG WW) · airframe 61,283 hrs · 35,609 cycles

LT MAIN LANDING GEAR WHEEL WELL FORWARD BULKHEAD UPPER PANEL SUPPORT BEAM CLIP CRACKED AT BS 140. R&R CLIP PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 59,049 hrs · 34,276 cycles

OVERWING LOWER EMER EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,104 hrs · 33,713 cycles

AFT PRESS BULKHEAD SKIN WEB CRACKED AT BS 1016, STRINGER 7L. REPAIRED WEB IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,104 hrs · 33,713 cycles

AFT PRESS BULKHEAD SKIN WEB CRACKED, AT BS 1016, STRINGER 7R. REPAIRED WEB IAW EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,561 hrs · 33,403 cycles

EMERGENCY EXIT LIGHT AT ROW 14 ABC INOPERATIVE. REPLACED THE LAMP IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,561 hrs · 33,403 cycles

EMERGENCY EXIT LIGHT AT ROW 18 DEF INOPERATIVE. REPLACE THE LAMP IAW MM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 57,017 hrs · 33,087 cycles

R1 DOOR HANDLE BOX LOWER SUPPORT, MACHINED BEAM CRACKED IN RADIUS, ADJACENT TO LOWER FWD INBD FASTENER. R & R DOOR IAW AMM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 56,976 hrs · 33,061 cycles

FORWARD GALLEY PHOTO LUMINESCENT STRIP LOOSE. SECURED STRIP IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,976 hrs · 33,061 cycles

INTERCOSTAL CRACKED AT BS 500D+10, RBL 7. R & R INTERCOSTAL IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,976 hrs · 33,061 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,976 hrs · 33,061 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,976 hrs · 33,061 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,976 hrs · 33,061 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,976 hrs · 33,061 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,976 hrs · 33,061 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,976 hrs · 33,061 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,976 hrs · 33,061 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,976 hrs · 33,061 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,976 hrs · 33,061 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 56,976 hrs · 33,061 cycles

RIGHT WING NR 6 SLAT, LOWER SKIN CRACKED AT FASTENER AT ACTUATOR ROD END ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 56,976 hrs · 33,061 cycles

BEAR STRAP CRACKED BELOW EXTERNAL POWER DOOR LOWER HINGE. REPAIRED BEAR STRAP IAW EA & ER.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 56,713 hrs · 32,904 cycles

R2 DOOR EXIT SIGN ON BULB INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 55,973 hrs · 32,475 cycles

RIGHT OVERWING LOWER EXIT SIGN LENS BROKEN. R & R SIGN LENS IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 55,480 hrs · 32,182 cycles

R1 DOOR EMER EXIT LIGHT LENS COVER BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 55,002 hrs · 31,920 cycles

VERTICAL STABILIZER SPRING BRACKET CRACKED. R & R BRACKET IAW SRM & EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,929 hrs · 31,330 cycles

L1 DOOR EMER EXIT FLOODLIGHT LAMP INOPERATIVE. R & R LAMPS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,355 hrs · 31,006 cycles

SKIN CHORD CRACKED AT BS 540 STRINGER 22R. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,355 hrs · 31,006 cycles

SKIN CRACKED AT BS 500A STRINGER 26R. REPAIRED SKIN IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 53,013 hrs · 30,836 cycles

LEFT EMER LIGHT FAILED CAPACITY CHECK BETWEEN ROW 1 TO ROW 4. R & R BATTERY PACK IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 52,797 hrs · 30,723 cycles

CENTER OVERHEAD EXIT SIGN FELL OUT. R & R EXIT SIGN ASSEMBLY IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 52,082 hrs · 30,285 cycles

R1 DOOR EMERGENCY LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 50,643 hrs · 29,440 cycles

WING CENTER SECTION REAR SPAR FIBERGLASS VAPOR BARRIER CRACKED APPROX 8" TOP TO BOTTOM BETWEEN LBL 31.8 & LBL 40. REPAIRED BARRIER IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,486 hrs · 29,354 cycles

SEAT TRACK FLANGE FOR THE SPLICE STRAP CRACKED AT STATION 727B, RBL 24.75. REPAIRED STRAP IAW EA.

Part: RIB — DAMAGED (RT HORIZ STAB) · airframe 50,486 hrs · 29,354 cycles

RT HORIZONTAL STABILIZER RIB DAMAGED AT STAB STATION 101.9 10" FWD OF REAR SPAR. REPAIRED RIB IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,486 hrs · 29,354 cycles

SEAT TRACK FLANGE FOR THE SPLICE STRAP CRACKED AT STATION 727B, LBL 45.5. REPAIRED STRAP IAW EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,486 hrs · 29,354 cycles

VERTICAL PRESSURE WEB CRACKED AT STATION 663, RBL 41. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,486 hrs · 29,354 cycles

SEAT TRACK FLANGE FOR THE SPLICE STRAP CRACKED AT STATION 727B, LBL 24.75. REPAIRED STRAP IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,486 hrs · 29,354 cycles

SEAT TRACK FLANGE FOR THE SPLICE STRAP CRACKED AT STATION 727B, RBL 45.5. REPAIRED STRAP IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,486 hrs · 29,354 cycles

RT NR 3 WINDOW FRAME E-F POST CRACKED AT FASTENER HOLES. REPAIRED POST IAW EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,486 hrs · 29,354 cycles

VERTICAL PRESSURE WEB CRACKED AT STATION 663, BETWEEN LBL 31.83 TO LBL 40. REPAIRED WEB IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,486 hrs · 29,354 cycles

LT NR 3 WINDOW FRAME E-F POST, NR 8 FASTENER HOLE, CRACKED 2ND FROM BOTTOM. REPAIRED POST IAW EA.

Part: STRUCTURE — CRACKED (RT HORIZ STAB) · airframe 50,486 hrs · 29,354 cycles

RT HORIZONTAL STABILIZER STATION 101.9, 1" CRACKED 10" FWD OF REAR SPAR. REPAIRED STABILIZER IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,486 hrs · 29,354 cycles

LT WING NR 1 SLAT LOWER SKIN CRACKED FROM FASTENER HOLE AT ACTUATOR FITTING. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,486 hrs · 29,354 cycles

LT WING NR 3 SLAT LOWER SKIN CRACKED FROM FASTENER HOLE AT ACTUATOR FITTING. REPAIRED SKIN IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 48,846 hrs · 28,406 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER M/M.

Part: BATTERY — FAILED (CABIN) · airframe 48,354 hrs · 28,134 cycles

EMERGENCY LIGHT BATTERY M01669 FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 48,099 hrs · 27,984 cycles

RIGHT EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM.

Part: WINDOW — LEAKING (COCKPIT) · airframe 46,520 hrs · 26,985 cycles

AIR TURNBACK -- DURING CLIMB AT FL 21.0 A LOUD NOSE WAS COMING FROM CAPTAIN SLIDING WINDOW. PRESSURIZATION CABIN RATE OF CLIMB INCREASED FROM 500 FPM TO 400 FPM - STABLE DURING CRUISE FLT. NOISE VERY LOUD - HARD TO HEAR RADIO'S. REMOVED AND REPLACED CAPTS SLIDING WINDOW IAW MM.

Part: LATCH — OUT OF ADJUST (L2 DOOR) · airframe 46,300 hrs · 26,847 cycles

L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR LATCH OUT OF ADJUST. ADJUSTED LATCH ASSY IAW DWG.

Part: LATCH — LOOSE (R1 DOOR) · airframe 46,300 hrs · 26,847 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOWER GIRT BAR LATCH ASSEMBLY LOOSE. SECURED LATCH ASSY IAW DWG.

Part: LATCH — OUT OF ADJUST (L1 DOOR) · airframe 46,300 hrs · 26,847 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOWER FWD GIRT BAR LATCH OUT OF ADJUST. ADJUSTED LATCH IAW DWG.

Part: SLIDE — UNWANTED DEPLOY (R2 DOOR) · airframe 46,300 hrs · 26,847 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY PARTIALLY DISCHARGED. REMOVED AND REPLACED SLIDE IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 46,300 hrs · 26,847 cycles

LEFT EMERGENCY LIGHT BATTERY PACK FAILS CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 46,300 hrs · 26,847 cycles

L1 WINDOW FRAME CRACKED. REMOVED AND REPLACED FRAME IAW BAC DWG & SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,259 hrs · 26,823 cycles

LEFT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 44,468 hrs · 25,493 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX BULKHEAD ATTACH ANGLE CRACKED AT BS 540, LBL 8. REMOVED AND REPLACED ANGLE PER ACO.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 44,468 hrs · 25,493 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX BULKHEAD ATTACH ANGLE CRACKED AT BS 540, LBL 54. REMOVED AND REPLACED ANGLE PER ACO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 44,104 hrs · 25,551 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CHORD CORRODED AT BS 270, BETWEEN LBL 10 TO RBL 11. REPAIRED CHORD IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,104 hrs · 25,551 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 40 TO LBL 45. REPAIRED BEAM IAW ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,104 hrs · 25,551 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 5 TO RBL 45. REPAIRED BEAM IAW ER AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 44,104 hrs · 25,551 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 259, BETWEEN LBL 10 TO RBL 11. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,104 hrs · 25,551 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1017, RBL 11. REPAIRED WEB IAW ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,104 hrs · 25,551 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,104 hrs · 25,551 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 44,104 hrs · 25,551 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO BAY SUB-THRESHOLD WEB CORRODED UPPER AND LOWER SURFACE. REPAIRED WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,104 hrs · 25,551 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,104 hrs · 25,551 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME IAW EA.

Part: RIB — CRACKED (HORIZ STAB) · airframe 44,104 hrs · 25,551 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.7. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 44,104 hrs · 25,551 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT HORIZ STAB RIB CRACKED AT STA 62.7. REPAIRED RIB IAW SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 39,400 hrs · 22,755 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT EEPLS DAMAGED AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 38,695 hrs · 22,351 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. REMOVED AND REPLACED HOOK PER SRM.

Part: STRIP — DELAMINATED (CABIN) · airframe 37,095 hrs · 21,395 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP DELAMINATED BETWEEN ROWS 6 AND 13. REMOVED AND REPLACED STRIP PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,004 hrs · 21,341 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 15.04. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,004 hrs · 21,341 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 6.14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,004 hrs · 21,341 cycles

DURING SCHEDULED 10Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 727D, LBL 2.5. REPAIRED BEAM PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,004 hrs · 21,341 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 6.14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,004 hrs · 21,341 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 32.40. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 37,004 hrs · 21,341 cycles

DURING SCHEDULED 10Y CHECK, FOUND NR 7 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,004 hrs · 21,341 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 15.04. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,004 hrs · 21,341 cycles

DURING SCHEDULED 10Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 727D, RBL 2.5. REPAIRED BEAM PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,004 hrs · 21,341 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 40.87. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,004 hrs · 21,341 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 54.6. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,004 hrs · 21,341 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 54.5. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 37,004 hrs · 21,341 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 32.4. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 36,661 hrs · 21,127 cycles

EEPLS LOOSE BETWEEN ROW 8 & 11. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,942 hrs · 20,671 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,942 hrs · 20,671 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER EA.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 35,088 hrs · 20,161 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 35,033 hrs · 20,119 cycles

DURING SCHEDULED HC2 CHECK, AFT LT EMERGENCY EXIT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 35,033 hrs · 20,119 cycles

DURING SCHEDULED HC2 CHECK, AFT RT EMERGENCY EXIT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,465 hrs · 18,562 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT 7 DEF. RELAMPED PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,002 hrs · 18,285 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 30,548 hrs · 17,417 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 29,883 hrs · 17,053 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 26. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,883 hrs · 17,053 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 5 TO RBL 40. REPAIRED FLOORBEAM PER SRM.

Part: CREASE BEAM — CORRODED (BS 986-997) · airframe 29,883 hrs · 17,053 cycles

DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 986 TO BS 997, RBL 48. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 29,883 hrs · 17,053 cycles

DURING SCHEDULED 8Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED INBOARD END. REPAIRED FLAP PER SRM.

Part: FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 29,883 hrs · 17,053 cycles

DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 26,136 hrs · 14,912 cycles

EEPLS COVER MISSING AT ROW 9 DEF. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 25,074 hrs · 14,307 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,074 hrs · 14,307 cycles

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

Part: SLIDE — LOW (R2 DOOR) · airframe 23,264 hrs · 13,286 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 19,204 hrs · 10,975 cycles

EMERGENCY EGRESS LIGHT LENS MISSING AT ROW 19. INSTALLED LENS COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 22,771 hrs · 13,007 cycles

DURING SCHEDULED HC 1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 18,015 hrs · 10,282 cycles

L2 DOOR EVAC SLIDE LOOSE. SECURED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 13,710 hrs · 7,923 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 13,271 hrs · 7,690 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: COVER — CRACKED (CABIN) · airframe 13,271 hrs · 7,690 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED IN SEVERAL AREAS. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: ROD — BROKEN (PAX DOOR) · airframe 12,676 hrs · 7,381 cycles

AFT ENTRY DOOR HARD TO OPEN. FOUND, AFT ENTRY DOOR LOWER GATE ACTUATING ROD BROKEN. REMOVED AND REPLACED ACTUATING ROD PER MM.

Part: COVER — CRACKED (CABIN) · airframe 10,873 hrs · 6,352 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS NR 1, NR 2, NR 4, NR 5, NR 6, NR 8, NR 9 AND NR 22. REMOVED AND REPLACED COVERS PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 9,516 hrs · 5,571 cycles

AIR TURN BACK, F/O SLIDING WINDOW CRACKED DURING CLIMB. REMOVED AND REPLACED F/O SLIDING WINDOW AND WINDOW HEAT CONTROLLER PER MM.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 9,374 hrs · 5,478 cycles

AIR TURNBACK, AFTER TAKEOFF L/E TRANSIT LIGHT ILLUMINATED, L/E DEVICES WOULD NOT FULLY RETRACT. REMOVED AND REPLACED NR 5, NR 7 AND NR 8 L/E SLAT ACTUATORS PER MM, ( S/N'S D00518, 2176 AND 5025 ).

Part: COVER — CRACKED (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED (6 EA). REMOVED AND REPLACED COVERS PER MM.

Part: LENS — MISSING (CABIN) · airframe 7,301 hrs · 4,265 cycles

AFT ENTRY EMERGENCY EXIT LIGHT LENS MISSING. R&R LENS PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 3,589 hrs · 2,155 cycles

EEPLS HAS EXPOSED WIRES AT EXIT ROW. REMOVED AND REPLACED TRACK COVER PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE)

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT OUT OF ADJUSTMENT. REINSTALLED SLIDE ASSY PER MM.