N567WN

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 75,850 hrs · 40,130 cycles

FWD SERVICE DOOR GIRT HANGING LOW. SECURED THE GIRT BAR IAW AMM 25-66-01.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 73,888 hrs · 38,929 cycles

EMERGENCY LIGHT AT SEAT ROW 6DEF INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT LAMP AT SEAT ROW 6DEF. REF AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 73,888 hrs · 38,929 cycles

EMERGENCY LIGHT AT SEAT ROW 14ABC INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT LAMP AT SEAT ROW 14ABC. REF AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: SEAT BACK — OUT OF ADJUST (ZONE 200) · airframe 73,344 hrs · 38,596 cycles

SEATS RECLINING AT EMERGENCY EXIT ROW 12D; 12F. ADJUSTED 12D; 12F SEAT RECLINE REF AMM 25-22-00

Part: SLIDE — OUT OF POSITION (ZONE 800) · airframe 73,071 hrs · 38,443 cycles

R2 DOOR ESCAPE SLIDE DRAGS ON THE FLOOR<[01]. PROPERLY INSTALLED R2 DOOR ESCAPE SLIDE IAW AMM 25-66-01-400-801;[02] VERIFIED CORRETIVE ACTION ENTRY 1.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

EMERGENCY LIGHTS RELATED TO BATTERY PACK M2355 FAIL TEST<[01] REPLACED EMERGENCY BATTERY PACK M2335; PERFORMED GOOD EMEREGENCY LIGHT TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION. CARD COMPLETE.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

FWD ESCAPE EMEREGENCY LIGHT OUTSIDE FWD MAIN ENTRY DOOR INOP (L731)<[01] INSTALLED NEW LIGHT AT FWD ESCAPE EMEREGENCY OUTSIDE FWD MAIN ENTRY DOOR; PERFORMED GOOD TEST PER AMM 33-51-04-960-801.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.

Part: SCUFF PLATE — MISSING (ZONE 100) · airframe 73,071 hrs · 38,443 cycles

AFT AND FWD SCUFF PLATES (CORNERS) MISSING AT FWD CARGO BAY<[01] 01 - REMOVED AND REPLACED PER [AMM 53-11-02-420-801-NG (CARGO DOOR SCUFF PLATE - INSTALLATION - PERMANENT)];[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

CRACKED PANEL BREAK BS 540 BL 0 - RBL 25 WL 207 (MARKED)<[01] REMOVED AND REPLACED PANEL BREAK AT BS540 BL0-RBL25 WL207 PER SRM 51-40-02 AND DWG:143A0060 REV:A;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: FLOORBEAM — CANNING (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

CRACKED PANEL BREAK BS 540 BL 0 - LBL 25 WL 207 (MARKED)<[01] REMOVED AND REPLACED PANEL BREAK AT BS540 BL0-LBL25 WL207 PER SRM 51-40-02 AND DWG:143A0060 REV:A;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

CORROSION ON SEAT TRACK LBL 45.5 BS480+16.5; BS500A+5; BS500A+8; BS500B+16; BS500B+18.5; BS00D+9.5 WL 208 (MARKED)<[01] SEAT TRACK WILL REPLACE DUE TO MECHANICAL DAMAGE ACCORDING TO CUSTOMER # TTG8Q00Y9C43.;[02] VERIFIED ITEM 1

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

CORROSION ON SEAT TRACK LBL 24.75 BS500A+8; BS500A+11; BS500A+14.5; BS500A+17; BS500D+9.5; BS 520+5.5 TO BS520+11 WL 208 (MARKED)<[01] BS 480 TO BS 520 LBL25 SEAT TRACK WILL REPLACE DUE TO MECHANICAL DAMAGE ACCORDING TO CUST# TTG8Q00Y9C8F.<BR>UPON FURTHER INVESTIGATION NO CORROSION ON SEAT TRACK LBL 25 BS520+5.5 TO BS520+11 WL 208.;[02] VERIFIED ITEM 1

Part: SKIN — CRACKED (ZONE 300) · airframe 73,071 hrs · 38,443 cycles

CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN AT STAB STA 193.90; 18.5' FROM FWD EDGE; .35' IN LENGTH (MARKED) <[01]. REPAIRED R/H HORIZONTAL STAB LOWER SKIN AT STAB STA 193.90 IAW SRM 55-10-01-2R-11 REPAIR 11.; [02] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.

Part: WEB — CRACKED (ZONE 600) · airframe 73,071 hrs · 38,443 cycles

RIGHT WING T/E UPPER SURFACE PANEL AT ORSS 276; TRANSVERSE WEB IS CRACKED AT O/B UPPER FASTENER<[01] REMOVED R/W T/E UPPER SURFCE PANEL TRANSVERSE WEB AT ORSS 276 IAW SRM 51-40-02-OG-0 PARA. 4.;[02] VERIFIED ITEM 1

Part: RIB — CRACKED (ZONE 500) · airframe 73,071 hrs · 38,443 cycles

L-CLIP COMMON TO L/W I/B SIDE OF DEFLECTION CONTROL RIB AND UPPER SURFACE PANEL ORSS 271 IS CRACKED <[01]. REMOVED AND REPLACED L- CLIP COMMON TO L/W I/B SIDE OF DEFLECTION CONTROL RIB AND UPPER SURFACE PANEL AT ORSS 271 IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERIFIED ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231ZF; WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

FLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] ADDED PART INSTALL INFO.

Part: RIB — CRACKED (ZONE 300) · airframe 73,071 hrs · 38,443 cycles

LEFT HORIZONTAL STAB REMOVABLE L/E 331B RIB #5 IS CRACKED<[01] REMOVED AND REPLACED L/H HORIZONTAL STAB. L/E #5 RIB IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241DF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0128.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF UPPER SKIN; WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

FLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242AF; UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.

Part: PANEL — DEBONDED (ZONE 600) · airframe 73,071 hrs · 38,443 cycles

RIGHT WING L/E PANEL 621HB HAS DISBOND AT I/B FWD CORNER<[01] 04 - REPAIRED PER [SRM 51-70-05-2R-6-A00737 (REPAIR 6 - REPAIR OF DAMAGE TO THE EDGEBAND OF A HONEYCOMB PANEL - AIRFRAME - PERMANENT)];[02] VERIFEID CORRECTIVE ACTION 1

Part: RIB — CRACKED (ZONE 300) · airframe 73,071 hrs · 38,443 cycles

LEFT HORIZONTAL STAB REMOVABLE L/E 331B RIB #3 IS CRACKED<[01] 1. KENNETH RUDIO (TECHNICIAN); 24-JAN-2025 22:07 UTC<BR>REMOVED AND REPLACED L/H HORIZONTAL STAB. L/E #3 RIB IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.

Part: STRAP — CORRODED (ZONE 100) · airframe 73,071 hrs · 38,443 cycles

AFT CARGO BAY TENSION STRAP HAS CORROSION APPROX BS802; RBL25.<[01] CORROSION ON TENSION STRAP AT ACB BS 806 ; RBL 25 IN L=2' X W=1' X D=0.030' FROM ORIGINAL THICKNESS 0.100' THEREFORE FOUND TO BE OUT OF LIMITS; TENSION STRAP WILL BE REPAIRED BY REPLACEMENT OF PART PER SRM 53-60-15-1A-1 FIG 103 DETAIL G AND SRM 51-10-02 PAR 9.<BR> <BR>USED TOOL: ID:PER2335; DUE:06/2025;[02] VERIFIED CORRECTIVE ACTION 1;[03] REMOVED AND REPLACED TENSION STRAP AT ACB BETWEEN BS 767+7' TO BS 847+13' ;RBL 25' PER SRM 51-40-02 ; DWG:146A8120 REV-; DWG: 146A8340 REV-; DWG: 146A0081 REV A;[04] VERIFIED RII ITEMS COMPLETE

Part: PRESSURE DECK — CRACKED (ZONE 100) · airframe 73,071 hrs · 38,443 cycles

CRACK IN RH HORIZONTAL PRESSURE DECK BS 664.5 WL 202 RBL 43. CRACK IS .250 INCHES LONG AND MARKED IN RED INK.<[01] REMOVED THE DAMAGE PART OF THE WEB AT BS 663.75 - 6BS75; RBL38 - 60; WL 202; PER SRM 53-40-51-2R-2 PAR. 4. C. FIG. 202.<BR><BR>INSTALLED REPAIR RH HORIZONTAL PRESSURE DECK AT BS 663.75 - 6BS75; RBL38 - 60; WL 202; PER SRM 53-40-51-2R-2 PAR. 4. L. AND DWG 144A7700.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: WEB — CORRODED (ZONE 100) · airframe 73,071 hrs · 38,443 cycles

AFT CARGO SUBTHRESHOLD WEB HAVE CORROSION MULTIPLE AREAS.<[01] REMOVE AND REMPLACE AFT CARGO SUBTHRESHOLD WEB SRM 51-40-02 DWG 146A8340 ID:0024 REV: A;[02] REMOVED AND REMPLACED AFT CARGO SUBTHRESHOLD WEB BETWEEN BS 794 TO BS 847 PER SRM 51-40-02 DWG 146A8340 ID:0024 REV: A;[03] VERIFIED COMPLETION CORRECTIVE ACTION 2 AND MEASUREMENT TABLE.

Part: THRESHOLD — CORRODED (ZONE 100) · airframe 73,071 hrs · 38,443 cycles

FWD CARGO SUBTHRESHOLD HAS CORROSION IN MULTIPLE AREAS<[01] UPON FURTHER INVESTIGATION; FOUND TO BE OUT OF LIMIT AS PER SRM 53-30-15-1A-1. REPAIR BY REPLACEMENT.;[02] UPDATED STEP 4;[03] UPDATED STEP 5;[04] REPLACED FWD CARGO BAY SUB THRESHOLD IAW SRM 51-40-02 AND DWG 143A8330 REV A;[05] VERIFIED COMPLETION CORRECTIVE ACTION 4 AND MEASUREMENT TABLE.

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 73,071 hrs · 38,443 cycles

CRACK IN LH HORIZONTAL PRESSURE DECK BS 672 WL 202 LBL35. CRACK IS .650 INCHES IN LENGTH. MARKED IN RED INK.<[01] REPAIRED LH HORIZONTAL PRESSURE DECK WEB AT BS 663 TO BS 675 LBL 30 TO LBL 60 PER SRM 53-40-51-2R-2 REPAIR 2 FIG. 202.;[02] TASK CARD COMPLETED.;[03] TASK CARD COMPLETED.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 73,071 hrs · 38,443 cycles

AFT CARGO FWD SCUFF PLATE IS CRACKED <[01]. WELDED THE CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(4). REFERRED TO BAC 5975. EQUIPMENT USED; WELDING MACHINE I.D. 10583; CAL DATE 01/2025; APPLIED CHEMICAL CONVERSION COATING ON SCUFFPLATE PER SOPM 20-43-03; APPLIED PROTECTIVE COATING TO INNER SURFACE OF SCUFFPLATE PER AMM 51-21-72-370-804. SCUFFPLATE WILL BE PREPPED AND INSTALLED ON CUSTOMER CARD TTG8Q00Y5CAP; [02] VERIFIEC CORRECTIVE ACTION.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 73,071 hrs · 38,443 cycles

CRACKED VAPOR BARRIER IN THE MAIN WHEEL WELL BS663 LBL15 WL147. MARKED <[01]. CRACKED VAPOR BARRIER BS663 LBL15 WL147 WAS REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE ACTION.

Part: DOUBLER — DAMAGED (ZONE 100) · airframe 73,071 hrs · 38,443 cycles

CUSTOMER REQUEST: DOUBLER AT BS 407 BETWEEN S-1 AND S-2L REQUIRES REMOVAL AND REPAIR DOUBLER AT BS 407 STR 1 - STR 2L/H <[01]. `THE DAMAGE WAS REPAIRED PER EA 25-153-00120. CONTINUED AIRWORTHINESS REQUIREMENTS ARE TRACKING ON EA 25-153-00120-DTI.' ENSURE THE 'EA-GENERAL' REPAIR REFERENCE IS SELECTED.; [02] CARD COMPLETED; [03] CARD COMPLETED; [04] RII STEPS COMPLETED.

Part: GIRT BAR — UNSECURE (ZONE 800) · airframe 72,289 hrs · 37,974 cycles

R1 DOOR SLIDE GIRT IS NOT SECURED WITH VELCRO<[01] RE-SECURED R1 DOOR SLIDE GIRT WITH VELCRO PER AMM 25-66-01.

Part: BRACKET — CRACKED (ZONE 100) · airframe 72,289 hrs · 37,974 cycles

KEEL BEAM ACCESS PANEL 192E FWD RH ATTACH HANGAR BRACKET IS CRACKED.<[01] REMOVED AND REPLACED KEEL BEAM ACCESS PANEL 192E FWD R/H ATTACH HANGER BRACKET PER SRM 51-40-02

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 71,764 hrs · 37,650 cycles

LEFT OVERWING EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHTS PSU BATTERY PACK. TEST OK. REF AMM. 33-51-06.

Part: SIGN — BROKEN (AFT CABIN) · airframe 70,506 hrs · 36,860 cycles

AFT CEILING EMERGENCY EXIT SIGN BROKEN<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]

Part: HANDLE — LOOSE (ZN 800 DOOR) · airframe 67,166 hrs · 34,728 cycles

PER CUSTOMER WALK- L-1 DOOR AFT ASSIST HANDLE LOOSE.<[01] SECURED L-1 DOOR AFT ASSIST HANDLE AS PER AMM 25-21-31-420-802;[02] VERIFIED 1.

Part: FITTING — LOOSE (ZN 800 DOOR) · airframe 67,166 hrs · 34,728 cycles

CUSTOMER WALK - R-2 DOOR AFT GIRT BAR FLOOR FITTING LOOSE.<[01] RESECURED R 2 DOOR AFT GIRT BAR FLOOR FITTING AS PER REF B737AMM 25-66-01-000-804;[02] VERIFIED 1.

Part: LIGHT — INOPERATIVE (ZN 800 DOOR) · airframe 67,166 hrs · 34,728 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] RECONNECTED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP#1

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 67,166 hrs · 34,728 cycles

SEVERAL EMERGENCY LIGHTS FAILED OPERATIONAL TEST THROUGHOUT THE CABIN.<[01] REMOVED AND REPLACED AT LOCATIONS M1673; M1670 AND M1669 PERFORMED OPERATIONAL TEST NORMAL AS PER REF B737 AMM 33-51-06-960-805;[02] CORRECTION FOR STEP # 1 REMOVED AND REPLACED EMERGENCY BATTERY PACK AT LOCATIONS M1673; M1670 AND M1669 PERFORMED OPERATIONAL TEST NORMAL AS PER REF B737 AMM 33-51-06-960-805;[03] VERIFIED 2.

Part: PANEL — CRACKED (ZN 300 STABILIZE) · airframe 67,166 hrs · 34,728 cycles

LH HORIZONTAL STABILIZER PANEL 333AT TRACK ASSY FOUND CRACKED<[01] REMOVED PANEL 333AT AT LT HORIZONTAL STABILIZER FOR ACCESS TO DAMAGE IN AS PER B 737-700 SRM 51-40-02-0G-0;[02] REMOVED KEYWORD TRACK AT LT HORIZONTAL STABILIZER OF UPPER SIDE FOR DAMAGE IN AS PER B 737-700 SRM 51-40-02-0G-0;[03] RECEIVED NEW KEYWORD TRACK P/N 181A8060-15 PO# 1728471;[04] LOCATED AND DRILLED NEW KEYWORD TRACK AT LT HORIZONTAL STABILIZER AT UPPER SIDE IN AS PER B 737-700 SRM 51-40-05-0G-0;[05] VERIFIED 1-4. OK TO INSTALL NEW TRACK.;[06] INSTALLED NEW TRACK AT LT HORIZONTAL STABILIZER AT UPPER SIDE IN AS PER B 737-700 SRM 51-40-02-0G-0;[07] VERIFIED 6.;[08] OK TO INSTALL/CLOSE ACCESS PANEL 333AT.;[09] INSTALLED PANEL 333AT AT LT HORIZONTAL STABILIZER FOR ACCESS TO DAMAGE AS PER B 737-700 SRM 51-40-02-0G-0;[10] (FINAL) REMOVED AND REPLACED LH HORIZONTAL STABILIZER PANEL 333AT TRACK ASSY AS PER SRM 51-40-02-0G-0.;[11] VERIFIED STEPS#9 AND #10.

Part: SEAT — CRACKED (ZN 200 FUS TOP) · airframe 67,166 hrs · 34,728 cycles

COCKPIT 1ST OBS SEAT BOTTOM CRACKED ON RIGHT LWR SURFACE. 8-50<[01] REMOVED FLIGHT DECK 1ST OBS. SEAT AS PER B737 AMM 25-1102-000-801;[02] ACCOMPLISHED REPAIR DOUBLER TO 1ST OBSERVER SEAT AS PER EA-M-22-125-00561; WORK T/C: TTG8Q00HW8W5.;[03] VERIFIED AND INSPECTED STEP #1 AND #2.;[04] OK TO REINSTALL 1ST OBS SEAT.;[05] REINSTALLED FLIGHT DECK 1ST OBSERVER SEAT AS PER B737 AMM 25-11-02-400-801.;[06] VERIFIED 5.

Part: BATTERY — INOPERATIVE (ZN 200 FUS TOP) · airframe 67,166 hrs · 34,728 cycles

FWD LH WINDSCREEN : BATTERIES AT EMERGENCY FLASHLIGHTS DO NOT WORK (2 EACH)<[01] FLASHLIGHT BATTERIES AT FWD LH WINDSCREEN REMOVED AND REPLACED IAW CMM 25-60-02;[02] VERIFIED STEP 1.

Part: BATTERY — INOPERATIVE (ZN 200 FUS TOP) · airframe 67,166 hrs · 34,728 cycles

AFT LH WINDSCREEN : BATTERIES AT EMERGENCY FLASHLIGHTS DO NOT WORK (2 EACH)<[01] FLASHLIGHT BATTERIES AT AFT LH WINDSCREEN REMOVED AND REPLACED IAW CMM 25-60-02;[02] VERIFIED STEP 1.

Part: TRACK — CORRODED (ZN 200 FUS TOP) · airframe 67,166 hrs · 34,728 cycles

CAPT. FWD O/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-35<[01] RECEIVED PART; NEW TRACK INSTALLED ON TASK CARD TTG8Q001YDLC;[02] VERIFIED 1;

Part: TRACK — CORRODED (ZN 200 FUS TOP) · airframe 67,166 hrs · 34,728 cycles

F/O FWD I/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-36<[01] RECEIVED PART; NEW TRACK INSTALLED ON TASK CARD TTG8Q001YDLC.;[02] VERIFIED 1;

Part: TRACK — CORRODED (ZN 200 FUS TOP) · airframe 67,166 hrs · 34,728 cycles

F/O FWD O/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-34<[01] RECEIVED PART; NEW SEAT TRACK INSTALLED ON TASK CARD TTG8Q001YDLC.;[02] PARTS TRANS ACTION;[03] FINAL INSPECTION; RECEIVED NEW SEAT TRACK. WILL BE INSTALL ON TTG8Q001YDLC.

Part: SEAT TRACK — CORRODED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

LEFT OB CABIN SEAT TRACK HAS EXFOLIATING CORROSION BS 375. 8-26<[01] REMOVED FASTENERS FOR ACCESS TO REMOVE SEAT TRACK CORROSION PER B737-700 SRM 51-40-02-0G-0.;[16] VERIFIED STEP NO15. (FINAL) REMOVED CORROSION AT LEFT O/B CABIN SEAT TRACK BS 375 PER B737-700 SRM 51-10-02-0G-0. EVALUATED AREA; ORIGINAL MATERIAL 0.230'; MATERIAL REMOVED 0.045'; MATERIAL REMAINING 0.185'; MAXIMUM ALLOWABLE AT THE BOTTOM OF THE TRACK 0.040'; FOUND OUT OF LIMITS PER B737-700 SRM 53-00-52-1A-1 FIG. 103 A-A AND BAC1520-2789. TOOL USED B/C: 170642; CAL. DATE: 10/12/2022; CAL. DUE: 10/12/2023. REMOVED AND REPLACED SEAT TRACK PO#1792296 AS PER SRM 51-40-02-0G-0 AND IPC 53-42-11-17A.

Part: BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

RT BS 663 VAPOR BARRIER CRACK RBL 45.<[01] MEASUREMENTS;[02] PERFORMED VISUAL INSPECTION ON R/H VAPOR BARRIER AND FOUND CRACK OF 9' PER B737 NDTM 51-05-01;[03] PERFORMED STOP DRILL SIZE 0.25 DIAMETER AT THE END OF THE CRACK PER B737 SRM 57-10-10-2R-2 STEP 6.B;[04] PREPARED DAMAGED AREA ON VAPOR BARREIR FOR REPAIR PER B737 SRM 51-70-04-2R-10 AND 51-70-04-2R-0 PARAGRAPH 4.E;[05] VERIFIED STEP # 1;2; 3 AND 4;[06] OK TO INSTALL REPAIR;[07] REPAIRED R T BS 663 VAPOR BARRIER AS PER B737 SRM 51-70-04-2R-10 MATERIAL USED PO.1800112 AND PO.1690463;[08] VERIFIED STEP 7. OK TO APPLY TOP COAT.;[09] APPLIED PRIMER AND TOPCOAT ON RT VAPOR BARRIER REF B 737 AMM 21-21-81-370-801 AND 51-21-72-370-804;[10] LOCATED AND DRILLED VAPOR BARRIER AT BS 663 RBL 45 PER REF SRM 51-40-05-0G-0.;[11] VERIFIED STEPS #9 AND #10.;[12] FINAL INSPECTION; VAPOR BARRIER REPAIRED. ALL WORK PERFORMED.;[13] INSTALLATION OF VAPOR BARRIER AT STA 663 RBL 45 WILL BE ACCOMPLISH ON TASK CARD #TTG8Q00HL9HJ.;[14] ADD TO STEP #12. <BR> INSTALLATION OF VAPOR BARRIER AT STA 663 RBL 45 WILL BE ACCOMPLISH ON TASK CARD #TTG8Q00HL9HJ.

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 67,166 hrs · 34,728 cycles

RIGHT HORIZONTAL STILIZER RIB 4 CRACKED AT STIFFENER 2 LOWER RADIUS.<[01] REMOVED THE DAMAGE PART OF THE RIB 4 STIFFENER 2 LOWER RADIUS AS SHOW IN FIG. 202 PARA.4 LETTER B REF. SRM 55-10-09-2R-4 REPAIR 4;[02] PERFORMED HFEC INSP ON REWORKED; IAW B 737 NDT PART 6 51-00-00 PROCE 23. TOOL NORTEC 600. BC 166316. CALIB DUE 10-17-23. NO CRACKS FOUND.;[03] PERFORMED HFEC ROTO INSP ON FASTENER OPEN HOLES NEAR TO REWORKED AREA; IAW B 737 NDT PART 6 51-00-00 PROCE 16. TOOL NORTEC 600. BC 166316. CALIB DUE 10-17-23. NO CRACKS FOUND.;[04] VERIFIED STEP # 1;[05] LOCATED AND DRILLING PARTS OF THE REPAIR OF KIT P/N 55100003-01 PO#1792296 ON THE RIB 4 OF STIFFENER 2 LOWER RADIUS REF. SRM 55-10-09-2R-4 REPAIR 4 LETTERS (G;H;I;J);[06] VERIFIED STEP #5.<BR> OK TO TREAT AND PRIME DRILLED HOLES AND REPAIR PARTS AND AREA.;[07] (RII) PERFORMED A GENERAL VISUAL INSPECTION (GVI) OF ALL AREAS WITHIN THE REPAIR AREA; (INCLUDING UNDERLYING STRUCTURE) FOR CORROSION; EXISTING REPAIR OR ANY OTHER DEFECTS.;[08] APPLIED TREAT AND PRIMER TO PARTS OF THE REPAIR AND THE RIB 4 OF THE STIFFENER 2 LOWER RADIUS REF. SRM 55-10-09-2R-4 REPAIR 4 PARA. 4 LETTERS (K;L);[09] ADD TO STEP #7.<BR> PER REF. SRM 55-10-09-2R-4 STEP 4 E.;[10] (RII) VERIFIED STEP #8.<BR> OK TO INSTALL NEW REPAIR PARTS.;[11] INSTALLED REPAIR ON THE RIB 4 STIFFENER 2 LOWER RADIUS REF. SRM 55-10-09-2R-4 REPAIR 4 PARA. 4 LETTERS (M;N;O;P;Q;R);[12] (RII) FINAL INSPECTION; RIB REPAIR ACCOMPLISHED.

Part: CHANNEL — CORRODED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

AFT CARGO FLOOR SUPPORT 22' LEFT 'Z' CHANNEL IS CORRODED AT B/S 727-727B<[01] FOUND EXFOLIATED CRACKED CORROSION AT AFT CARGO FLOOR SUPPORT L/H Z CHANNEL STA 727-727B PER SRM 51-10-02-0G-0;[02] LOCATED AND DRILLED NEW L/H Z CHANNEL FROM STA 727- 847 PER REF SRM 51-40-05-0G-0 MATERIAL USED: BAC 1496-377 7075 T6 P.O:1782284;[03] EDIT STEP #1 : FOUND EXFOLIATED CRACKED CORROSION AT AFT CARGO FLOOR SUPPORT L/H Z CHANNEL STA 727-727B OUT OF LIMITS PER SRM 53-00-53-1A-2;[04] VERIFIED AND INSPECTED STEP #2 AND #3.;[05] TREATED AND PRIME REWORKED AREA PER AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[06] EDIT STEP #5 : TREATED AND PRIME NEW L/H Z CHANNEL STA 727 TO 847 PER AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[07] VERIFIED STEP #6.<BR> OK TO INSTALL NEW FASTENER NUT PLATES.;[08] INSTALLED NEW FASTENER NUTPLATES AT NEW L/H Z CHANNEL STA 727-847 PER SRM 51-40-02-0G-0;[09] FINAL INSPECTION; WORK PERFORMED.

Part: RETAINER — CRACKED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

LH VAPOR BARRIER SEAL RETAINER FOUND CRACKED<[01] RECIEVED; LOCATED AND DRILLED NEW L/H VAPOR BARRIER SEAL RETAINER PN: 111A1512U1 PO:1792296 PER REF SRM 51-40-05-0G-0.;[02] TREATED AND PRIMED NEW HOLES PER REF AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[03] FINAL INSPECTION; VERIFIED STEPS #1 AND #2.

Part: CHANNEL — CORRODED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

AFT CARGO FLOOR SUPPORT 22' LEFT 'Z' CHANNEL IS CORRODED AT B/S 767-807<[01] AFT CARGO L/H Z CHANNEL WILL BE REPLACED FROM STA 727-847 FOR WORK ACCOMPLISHED REFERENCE TASK CARD # TTG8Q00HKADG;[02] VERIFIED STEP #1.

Part: CHANNEL — BROKEN (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

RIGHT 'Z' CHANNEL AT FWD END B/S 727 ATTACHMENT IS BROKEN<[01] AFT CARGO R/H Z CHANNEL WILL BE REPLACED FROM STA 727-767 FOR WORK ACCOMPLISHED REFERENCE TASK CARD # TTG8Q00HKAET;[02] FINAL INSPECTION; AFT CARGO R/H Z CHANNEL WILL BE REPLACED FROM STA 727-767 FOR WORK ACCOMPLISHED REFERENCE TASK CARD # TTG8Q00HKAET.

Part: CHANNEL — CORRODED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

AFT CARGO FLOOR SUPPORT 22' RIGHT 'Z' CHANNEL IS CORRODED AT B/S 727C-727E<[01] AFT CARGO R/H Z CHANNEL WILL BE REPLACED FROM STA 727-767 FOR WORK ACCOMPLISHED REFERENCE TASK CARD #TTG8Q00HKAET;[02] VERIFIED STEP #1.

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

PASSENGER CABIN FLOOR PANEL #241XF; UPPER SURFACE DELAMINATED DOT 223-PCF241XF.<[01] RECEIVED NEW PANEL 241XF; PO#2005897. PANEL WILL BE INSTALLED ON TTG8Q00H2SLP.;[02] VERIFIED AND INSPECTED STEP #1.

Part: CHANNEL — CORRODED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

AFT CARGO FLOOR SUPPORT 22' LEFT 'Z' CHANNEL IS CORRODED AT B/S 77B-727E<[01] AFT CARGO L/H Z CHANNEL WILL BE REPLACED FROM STA 727-847 FOR WORK ACCOMPLISHED REFERENCE TASK CARD # TTG8Q00HKADG;[02] VERIFIED STEP #1.

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

LH VAPOR BARRIER SUPPORT BRACKET FOUND CRACKED AROUND FASTENER HOLE<[01] RECEIVED NEW BRACKET P/N 276A9183-5 AND LOCATED AND DRILL PER REF SRM 51-40-05-0G-0;[02] TREATED AND PRIME NEW FASTENER HOLES; PER REF AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[03] OK TO INSTALL NEW BRACKET;[04] VERIFIED. STEP 2;[05] INSTALLED SUPPORT BRACKED AT LH VAPOR BARRIER PER REF DWG NUMBER 111A1000;[06] VERIFIED STEP # 5

Part: FLOOR PANEL — CRACKED (ZN 200 FUS TOP) · airframe 67,166 hrs · 34,728 cycles

FLOOR PNL 242SF HAS CRACK ON UPPER SURFACE. 8-25<[01] RECEIVED NEW PANEL 242SF PO#2005895. PANEL WILL BE INSTALLED ON TTG8Q00H2URQ.;[02] VERIFIED AND INSPECTED STEP #1.

Part: FITTING — CRACKED (ZN 600 RIGHT WIN) · airframe 67,166 hrs · 34,728 cycles

RT WING TRAIL EDGE RIB WBL 201.90 HAS AFT UPPER FITTING CRACKED THRU. 8-24<[01] REMOVED AND REPLACED AFT UPPER FITTING AT RT WING TRAIL EDGE RIB WBL 201.90 PER REF SRM-51-40-02-0G-0.;[02] FINAL INSPECTION; T/E RIB REPLACED.

Part: CHANNEL — CORRODED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

AFT CARGO FLOOR SUPPORT 22' RIGHT 'Z' CHANNEL IS CORRODED AT B/S 727E-767<[01] FOUND EXFOLIATED CRACKED CORROSION AT AFT CARGO FLOOR SUPPORT Z-CHANNEL PER REF SRM 51-10-02-0G-0;[02] LOCATED AND DRILLED NEW R/H Z-CHANNEL FROM STA 727 TO 767 PER REF SRM 51-40-05-0G-0 MATERIAL USED: BAC1496-377 7075 T6 P.O.: 1782284;[03] EDIT STEP #1 : FOUND EXFOLIATED CRACKED CORROSION AT AFT CARGO FLOOR SUPPORT R/H Z CHANNEL STA 727E-767 OUT OF LIMITS PER SRM 53-00-53-1A-2;[04] VERIFIED AND INSPECTED STEP #2 AND #3.;[05] TREATED AND PRIMED NEW R/H Z CHANNEL STA 727-767 PER AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[06] VERIFIED STEP #5.<BR> OK TO INSTALL NEW NUT PLATES.;[07] INSTALLED NEW FASTENER NUTPLATES AT NEW R/H Z CHANNEL STA 727-767 PER SRM 51-40-02-0G-0;[08] VERIFIED STEP #7. NEW FASTENER NUT PLATES INSTALLED.;[09] FINAL INSPECTION; WORK PERFORMED.

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

COMP- REPAIR LH VAPOR BARRIER CRACK<[01] MEASUREMENTS.;[02] REMOVED THE DAMAGED PLIES AND PREPARED DAMAGED AREA TO APPLY THE GLASS FABRIC REPAIR PLIES; DRILLED 0.25 INHC DIAMETER STOP HOLES AT THE CRACK END. REF B737 SRM 51-70-04-2R-10 PARAGRAP 4 AND SRM 57-10-10-2R-2 PARAGRAPH 3 A.;[03] VERIFIED REMOVAL OF THE DAMAGED PLIES AND PREPARED DAMAGED AREA TO APPLY THE GLASS FABRIC REPAIR PLIES; DRILLED 0.25 INHC DIAMETER STOP HOLES AT THE CRACK END. REF B737 SRM 51-70-04-2R-10 PARAGRAP 4 AND SRM 57-10-10-2R-2 PARAGRAPH 3 A. OK TO INSTALL THE REPAIR.;[04] REPAIRED DAMAGED AREA AND TAP TEST INSPECTION AT LH VAPOR BARRIER AS PER B737SRM 51-70-04-2R-10 AND NTM 51-05-01 MATERIAL USE RESIN PO#1800112 FIBERGLASS PO#1690463;[05] VERIFIED STEP NO 4. OK TO DRILL HOLES.;[06] LOCATED AND DRILLED REPAIRED VAPOR BARRIER PER REF SRM 51-40-05-0G-0;[07] PRIMER AND TOPCOAT APPLICATION REF TASKCARD #TTG8Q00HH5FG;[08] VERIFIED 6-7.;[09] CORRECTION TO STEP #5.<BR>RII<BR>VERIFIED STEP NO 4. OK TO DRILL HOLES.;[10] (RII) FINAL INSPECTION; WORK PERFORMED.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

RT BS 663 VAPOR BARRIER UPPER SUPPORT ANGLE CRACKED.<[01] BEGAN REMOVED FASTENERS AT RT VAPOR BARRIER UPPER SUPPORT ANGLE BS 663 IN AS PER SRM 51-40-02-0G-0;18] COMPLETED INSTALLATION OF NEW REPAIR PARTS OF RT UPPER SUPPORT WING CENTER SECTION VAPOR BARRIER FROM RBL 5.00 TO RBL 65.00 IN AS PER SRM 51-40-02-0G-0 AND 57-10-10-2R-5 FIG 202 SHEET 3;[19] REINSTALLED SUPPORT STRAP; REMOVED ON STEP 2 FROM RBL 45.00 TO RBL 65.00 IN AS PER SRM 51-40-02-0G-0 AND 57-10-10-2R-5;[20] COMPLETED PERMANENT REPAIR VAPOR BARRIER UPPER SUPPORT ANGLES AT RT STA 663.75 AS PER B737-700 SRM 57-10-10-2R-5 FIG 202 SHEET 3.;[21] (RII) VERIFIED STEPS #16; #17; #18; #19. SQUEEZE OUT TIME AND 100% FASTENER INSTALLATION AND STRAP REINSTALLATION.;[22] (RII) FINAL INSPECTION; VAPOR BARRIER UPPER SUPPORT ANGLE REPAIRED ACCOMPLISHED. WORK PERFORMED.

Part: DOUBLER — CRACKED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

EGPR INTERNAL DOUBLER CRACKED AT FWD LOWER CORNER.<[01] REMOVED PAINT BY STRIPPING AT FUSELAGE SKIN R/H SIDE EGPR AREA REF B737-700 AMM 51-21-11-150-810.; LOCATED AND DRILLED NEW EGPR INTERNAL DOUBLER REF B737-700 SRM 51-40-05-0G-0.;[07] TREATED AND PRIMED DRILLED HOLES ON NEW EGPR INTERNAL DOUBLER REF B737-700 SRM 51-20-01-0G-0.;[08] VERIFIED STEPS 6 AND 7. OK TO INSTALL NEW EGPR DOUBLER.;[09] MIXED BMS 5-95 SEALANT 22:00 2/1/23. SQUEEZE OUT TIME BY 06:00 2/5/23.;[10] INSTALLED 90% OF FASTENERS AT EGPR INTERNAL DOUBLER REF B737-700 SRM 51-40-02-0G-0 AND DWG# 146A0640.;[11] COMPLETED INSTALLATION OF EGPR INTERNAL DOUBLER REF B737-700 SRM 51-40-02-0G-0 AND DWG# 146A0640.;[12] VERIFIED STEP # 10 AND 11;[13] VERIFIED STEP #9; SQUEEZE OUT TIME 100%; ALL FASTENERS INSTALLED.;[14] CORRECTION STEP 11 : COMPLETED INSTALLATION OF EGPR INTERNAL DOUBLER REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A0640 AND 141A3702.;] APPLIED TOP COAT AT FUSELAGE SKIN ON EGPR AREA REF B737-700 AMM 51-21-73-370-803.;[18] VERIFIED DRAWINGS STEP 14-15.;[19] VERIFIED 16-17.;[20] REMOVED AND REPLACED EGPR INTERNAL DOUBLER REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A0640.;[21] FINAL 20.

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 67,166 hrs · 34,728 cycles

RIGHT HORIZONTAL STABILIZER RIB 4 CRACKED AT STIFFENER 3 LOWER RADIUS.(51-025)<[01] REMOVED THE DAMAGE PART OF THE RIB 4 AT STIFFENER 3 LOWER RADIUS AS SHOW IN FIG. 202 PARA.4 LETTER B REF. SRM 55-10-09-2R-4 REPAIR 4;[02] VERIFIED 1. ACCOMPLISHED GVI OF REPAIR AREA PER SRM 55-10-09-2R-4 STEP 4.E. NO OTHER DEFECTS NOTED.;[03] PERFORMED HFEC INSP. OF THE CUT EDGES OF THE STIFFENER AND WEB IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. NO CRACKS NOTED<BR>TOOL: NORTEC 600 B/C: 166317 DUE: 10/31/23;[04] PERFORMED HFEC ROTO INSP. OF ALL EXISTING FASTENER HOLES WITHIN THE REPAIR AREA ON RIB#4; STIFFENER #3 IAW B737 NDT PART 6; 51-00-00; PROCEDURE 16. NO CRACKS NOTED <BR>TOOL: NORTEC 600 B/C: 166317 DUE: 10/31/23<BR>TOOL: OLYMPUS MINIMITE B/C: 172542 DUE: 09/02/23;[05] LOCATED AND DRILLING PARTS OF THE REPAIR OF KIT P/N 55100003-01 PO# 1728471 ON THE RIB 4 OF STIFFENER 3 LOWER RADIUS REF. SRM 55-10-09-2R-4 REPAIR 4 PARA. 4 LETTERS (G;H;I;J);[06] VERIFIED LOCATION AND DRILLING IN STEP # 5;[07] OK TO ALODINE AND PRIME REPAIR AREA.;[08] APPLIED TREAT AND PRIME TO PARTS OF THE REPAIR AND THE RIB 4 OF THE STIFFENER 3 LOWER RADIUS REF. SRM 55-10-09-2R-4 REPAIR 4 PARA. 4 LETTERS (K;L);[09] VERIFIED STEP # 8;[10] OK TO INSTALL REPAIR PARTS;;[11] INSTALLED REPAIR ON THE RIB 4 STIFFENER 3 LOWER RADIUS REF. SRM 55-10-09-2R-4 REPAIR 4 PARA. 4 LETTERS (M;N;O;P;Q;R);[12] VERIFIED STEP # 11;[13] JOB IS COMPLETE;[14] VERIFIED STEPS 5; 7;8; 10 AND 11 NOTE: RII

Part: BEAM — ELONGATED (ZN 500 LEFT WING) · airframe 67,166 hrs · 34,728 cycles

L/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL O/B SUPPORT ATTACHMENT POINT LOCATION ' A' ELONGATED HOLES ;EXCESSIVE PLAY MKD DOTS<[01] REMOVED HARDWARE AT L/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL O/B SUPPORT ATTACHMENT POING LOCATION 'A'AS PER B737-700 SRM 51-40-02-0G-0.[16] REMOVED AND REPLACED L/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB BEAM AS PER B737 SRM 51-40-05-0G-0.;[17] FINAL INSPECTION; REAR SPAR FIX T/E DEFLECTION CONTROL RIB BEAM REPLACED AND ADJUSTED.

Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 67,166 hrs · 34,728 cycles

MID FORWARD BODY FAIRING PANEL #191D; ALL FASTENER HOLES ELONGATED OR/AND SURFACE PROTRUDING DOT 223-MFF191D.<[01] PERFORMED VISUAL INSPECTION ON PANEL #191D AND FOUND NO ENTRY OF WATER; OIL; FUEL; OR OTHER UNWATED MATERIAL PER B737 NDTM 51-05-01;[02] PREPARED DAMAGED FASTENER HOLES FOR REPAIR ON PANEL #191D PER B737 SRM 51-70-04-2R-9 PARA 4.C;[03] VERIFIED STEP # 1 AND 2;[04] OK TO REPAIR;[05] REPAIRED PANEL #191D AT DAMAGED FASTENER HOLES PER B737 SRM 51-70-04-2R-9 PARA D-G. MATERIALS USED RESIN P/O#1800112 CLOTH P/O#1690463;[06] VERIFIED STEP # 5;[07] OK TO PAINT REPAIRED AREA;[08] PAINTED PANEL #191D PER B737 AMM 51-21-99-300-801. MATERIALS USED BLUEHEART PAINT P/O#1768107; WHITE PAINT P/O#1779132;[09] FINAL INSPECTION; VERIFIED STEP #8. WORK PERFORMED.

Part: ANGLE — ELONGATED (ZN 500 LEFT WING) · airframe 67,166 hrs · 34,728 cycles

L/W REAR SPAR FIXED T/E LOWER PANEL 551GB I/B ATTACHED ANGLE FWD FASTENER HOLE ELONGATED AND BUSING ; BOLT ; NUT MISSING MKD DOT<[01] REMOVED DAMAGE ANGLE AT LT WING T/E LOWER PANEL 551GB I/B SIDE PER REF B737 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW ANGLE AT LT WING T/E LOWER PANEL 551GB I/B SIDE PER REF B737 SRM 51-40-05-0G-0;[03] VERIFIED STEPS #1 AND #2; LOCATED AND DRILLED NEW ANGLE. <BR> OK TO INSTALL NEW ANGLE.;[04] INSTALLED NEW ANGLE AT LT WING T/E LOWER PANEL 551GB I/B SIDE PER REF B737 SRM-51-40-02-0G-0.;[05] VERIFIED STEP #4; NEW ANGLE INSTALLED.;[06] REMOVED PREVIOUSLY INSTALLED ANGLE PART3 115A2759-13 REF B737-700 SRM 51-40-02-0G-0.;[07] LOCATED AND DRILLED NEW ANGLE PART# 115A2759-5 REF B737-700 SRM 51-40-05-0G-0 AND DWG# 115A2714.;[08] VERIFIED STEPS #6 AND #7; LOCATED AND DRILLED NEW ANGLE. <BR> OK TO INSTALL NEW ANGLE.;[09] INSTALLED NEW ANGLE AT PANEL # 551GB REF B737-700 SRM 51-40-02-0G-0 AND DWG# 115A2714.;[10] VERIFIED STEP #9; INSTALLED NEW ANGLE P/N: 115A2759-5.;[11] INSTALLED NEW BOLT AND NUT MISSING AT I/B FWD ATTACHED ANGLE REF B737-700 SRM 1-40-02-0G-0 AND DWG# 115A2714.;[12] CORRECTING STEP 11: SRM REF 51-40-02-0G-0.;[13] VERIFIED STEPS #11 AND #12.;[14] REMOVED AND REPLACED FIXED T/E LOWER PANEL 551GB I/B ATTACHED ANGLE AND INSTALLED MISSING BOLT AND NUT REF B737-700 SRM 51-40-02-0G-0 AND DWG# 115A2714.;[15] FINAL 14.

Part: SKIN — CRACKED (ZN 300 STABILIZE) · airframe 67,166 hrs · 34,728 cycles

CRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 ; 17' FROM FRONT SPAR ; I/B ROW . CRACK LENGTH : 0.75' CRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 17' FROM FRONT SPAR I/B ROW .CRACK LENGTH : 0.75'.<[01] REMOVED PAINT BY STRIPPING SKIN CRACK AREA AT LEFT HORIZONTAL STABILIZER LOWER IN- SPAR SKIN AT STA 193.90; 17' FROM FRONT SPAR; I/B ROW AS PER B737-700 AMM 51-21-11-150-810.[15] INSTALLED REPAIR PARTS AT LT HORIZONTAL STAB LOWER SKIN STA 193.90 REF B737-700 SRM 55-10-01-2R-11 FIG 204.;[16] VERIFIED 14-15.;[17] APPLIED TOP COAT AT REPAIR AREA REF B737-700 AMM 51-21-73-370-803.;[18] ACCOMPLISHED PERMANENT REPAIR AT LT HORIZONTAL STAB LOWER SKIN STA 193.90 REF B737-700 SRM 55-10-01-2R-11 FIG 204.;[19] FINAL INSPECTION; LOWER IN-SPAR SKIN REPAIR. ALL WORK PERFORMED.

Part: TRAY — OUT OF ADJUST (SEAT 12C) · airframe 67,139 hrs · 34,709 cycles

ROW 12C TRAY TABLE WILL NOT STAY UP & PAX UNIT LIGHT FIXTURE MOVES.<[01] ADJUSTED TRAY TABLE @ 12C PER SIP. 12C READING LIGHT ASSEMBLY FOUND TO BE SECURE; FOUND 12C AIR OUTLET TO BE DAMAGED AND LOOSE. R&R 12C PSU AIR OUTLET PER AMM 21-24-04.

Part: SEAT — WRONG PART (CABIN) · airframe 67,147 hrs · 34,713 cycles

SEAT 11F RECLINES IN FRONT OF EXIT-SEAT 11F UNUSABLE SEAT 11F RECLINES IN FRONT OF EXIT-SEAT 11F UNUSABLE*** DO NOT CARRY ***<[01] ADJUSTED SEAT 11F HYDROLOCK TO DISABLE RECLINE IAW AMM 25-22-00. THIS CLEARS MEL.

Part: RESTRAINT — LOOSE (FWD MEGAPHONE) · airframe 66,576 hrs · 34,364 cycles

FWD GALLEY MEGAPHONE RESTRAINT LOOSE / [01] R/R?D FWD GALLEY MEGAPHONE BRACKET PER S.I.P

Part: MECHANISM — OUT OF ADJUST (COCKPIT) · airframe 66,303 hrs · 34,183 cycles

FIRST OFICER'S SLIDING WINDOW FAILS EMERGENCY EXIT RELEASE HANDLE OPS CHECK. / [01] ADJUSTED FIRST OFFICERS SLIDING WINDOW EMERGENCY EXIT RELEASE MECHANISM PER M/M 56-12-11.

Part: SLIDE — OUT OF POSITION · airframe 66,128 hrs · 34,058 cycles

FOWARD ENTRY DOOR ESCAPE SLIDE DISLODGED FROM IT'S CONTAINER / [01] REMOUNTED FWD DOOR ESCAPE SLIDE IAW S.I.P.

Part: NONE — INOPERATIVE · airframe 64,906 hrs · 33,247 cycles

AFT ENTRY DOOR EMERGENCY LIGHTS INOP / [01] REPLACED THE AFT L/H EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-06. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 64,449 hrs · 32,950 cycles

EMERGENCY LIGHT AFT OF L2 DOOR INOP / [01] R&R EMERGENCY LIGHT AFT OF L2 DOOR IAW AMM 33-51-04. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,030 hrs · 32,676 cycles

FWD CEILING EMERGENCY LIGHT INOP ; / [01] RELAMPED FWD CEILING AREA EMERGENCY LIGHT PER AMM 33-51-03. OPS CK GOOD

Part: STRAP — OUT OF ADJUST (L1 DOOR) · airframe 63,942 hrs · 32,624 cycles

FWD ENTRY DOOR UPPER STRAP NEEDS ADJUSTMENT ; / [01] REPLACED ATTACH SCREW PER SIP

Part: SLIDE — LOOSE (R1 DOOR) · airframe 63,829 hrs · 32,561 cycles

FSD ESCAPE SLIDE FELL FROM CLAM SHELL HOUSING ; FSD ESCAPE SLIDE FELL FROM CLAM SHELL HOSING / [01] REPACKED AND MOUNTED FSD ESCAPE SLIDE IAW AMM 25-66-01.

Part: PANEL — CRACKED (FUSELAGE) · airframe 63,777 hrs · 32,532 cycles

SUPPLEMENTAL INFORMATION: 193D PANEL HAS CRACKED HOLES / [01] REPLACED PANEL 193D PER AMM 53-51-21

Part: PANEL — CRACKED (FUSELAGE) · airframe 63,777 hrs · 32,532 cycles

SUPPLEMENTAL INFORMATION: 194E PANEL HAS CRACKED AND ELONGATED HOLES / [01] REPLACED PANEL 194E PER AMM 53-51-21

Part: ACM — FAULTED (LEFT) · airframe 62,490 hrs · 31,766 cycles

ON APPROACH CABIN AIR TEMPERATURE BECAME HOT. SMELL ACCOMPANIED THAT THROUGHOUT AIRCRAFT. AFTER LANDING; LEFT PACK TRIP OFF ILLUMINATED. ; / [01] C/W FUMES CONDITIONAL INSP IAW FIM 21-00 TASK 806; FOUND LH PACK CAUSING SMELL; OK TO CONTINUE PER MEL 21-1-01 SP1 AUTHORIZATION CODE 18262; [02] R&R LEFT HAND ACM PER AMM 21-51-04 REQUIRES CLAMP PART # BACC10CT2-400 ACM TO COLESSER BAG. REQUIRES LEAK CHECK AND OPS TO CLEAR MEL; [03] REF LOG PAGE 1651685 FOR WORK ACCOMPLISHED; REMOVED AND REPLACED LH ACM PER AMM 21-51-04. REQUIRES CLAMP ON BACC10CT2-400 ACM TO COALESCED BAG AND LEAK; OPS CHECK TO CLEAR MEL; [04] R&R CLAMP #1PACK ACM AT COALESCE BAG.OPS CHECH AND LEAK CHECK GOOD; [05] CERTIFIED

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 61,601 hrs · 31,241 cycles

FWD SERVICE DOOR SLIDE GIRT NEEDS ADJUSTMENT AND CLIP TIGHTED ADJUSTED SLIDE GIRT AND TIGHTENED CLIP ON FWD SERVICE PER AMM256601

Part: LIGHT — BROKEN (CABIN) · airframe 61,417 hrs · 31,143 cycles

EMERGENCY LIGHT LENSE AND BEZEL BROKEN AT 16 D-E-F / OK TO CONTINUE PER MEL 25-10-01 SP1B TRACKING #70711

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 61,361 hrs · 31,105 cycles

FWD SERVICE DOOR EXIT SIGN NOT INSTALLED / R/R RIGHT ASSY PER AMM 33-51-01

Part: SKIRT — OUT OF ADJUST (R2 DOOR SLIDE) · airframe 61,327 hrs · 31,086 cycles

QA WALK*** R2 DOOR ESCAPE SLIDE SKIRT RUB SCUFF PLATE WHEN CLOSING. / ADJUSTED R2 DOOR SLIDE SKIRT RUB AS PER TASK CARD 8725-61-06

Part: DOOR — OUT OF ADJUST (R1) · airframe 61,327 hrs · 31,086 cycles

R1 DOOR RIDES HARD ON AFT UPPER LATCH RECEIVER WHEN CLOSING / PERFORMED R1 DOOR ADJUSTMENT PER B737 AMM 52-41-00-820-801 ALL OPS NORMAL PERFORMED PRESSURIZATIONAL LEAK TEST OF R1 DOOR REF B737 AMM 25-51-91-790-801; NO LEAKS FOUND

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 61,327 hrs · 31,086 cycles

VERT STAB HAS ANGLE CRACKED ABOVE AND ON AFT SIDE OF FWD LEFT ATTACH LUG. / REMOVED AND REPLACED VERTICAL STAB LWR ANGLE ON FWD SIDE OF ATTACH LUG REF B737-700 SRM 51-40-02-0G-0 AND DWG #176A3101

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 61,327 hrs · 31,086 cycles

CABIN PANEL 241 RF IS DELAMINATED AT AFT RIGHT HAND CORNER. / ACCOMPLISHED PERMANENT REPAIR AT CABIN FLOOR PANEL 241RF AFT RIGHT HAND CORNER PER REF B737 SRM 53-00-50-2R-9

Part: BULKHEAD — DAMAGED (AFT CARGO) · airframe 61,327 hrs · 31,086 cycles

AFT CARGO COMPARTMENT; SHROUD 142NWA FOUND DAMAGED DURING INSPECTION. / RECEIVED NEW SHROUD 142NWA FROM STOCK .INSTALLATION WILL BE COMPLETED CUSTOMER CARD # JPANEL-141-CLOSE .

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,327 hrs · 31,086 cycles

CORROSION***ON LWR SURFACE OF LWR CTR WING SKIN AROUND 2 FWD BOLTS LBL 56 BS 541. / ACCOMPLISHED REPAIR OF CORROSION FOUND ON LWR SURFACE OF WING SKIN AROUND 2 FWD BOLTS LBL 56 BS 541 PER INSTRUCTIONS ON AAR RES-WI 2016690-11 REV IR AND SOUTHWEST EA 21-157-00233 REV IR. THIS IS AN INTERIM REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS.

Part: SUPPORT — CRACKED (FWD CARGO) · airframe 61,327 hrs · 31,086 cycles

FWD CARGO COMPARTMENT;GUSSET SUPPORT IS CRACKED AT STA 500D S-19LH. / REMOVED AND REPLACED GUSSET SUPPORT AT FWD CARGO COMP. AT STA 500D S-19LH AND TREATED ASS FASTENERS HOLES WITH ALODINE AND PRIME IN REF B737-700 SRM 51-40-02-0G-0; 51-20-01-0G-0 AND DWG# 143A7902.

Part: BRACKET — CRACKED (FWD CARGO) · airframe 61,327 hrs · 31,086 cycles

FWD CARGO COMPARTMENT HAS CRACKED BRACKET AFT SIDE OF FRAME BS 500C S-26L. / REMOVED AND REPLACED BRACKET AT FWD CARGO COMP AT BS 500C; S-26L AND TREATED ALL FASTNERS HOLES WITH ALODINE AND PRIMER IN REF BB 737-700 SRM 51-40-02-0G-0; 51-20-01-0G-0 AND DWG # 143A7505; 51-40-05-0G-0

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 61,327 hrs · 31,086 cycles

COCKPIT; CAPTIANS RACEWAYFOUND CRACKED. / REMOVED AND REPLACED COCKPIT; CAPTAINS RACEWAY WITH NEW RACEWAY AS PER REF B737-7 SRM 51-40-02-0G-0

Part: RIB — CRACKED (RT WING TE) · airframe 61,327 hrs · 31,086 cycles

RT WING UPPER T/E PNL AFT OF PYLON HAS CTR AFT RIB CRACKED AT FWD LWR BOLT HOLE. / REMOVED AND REPLACED CENTER AFT RIB AT RT. WING AFT OF PYLON IAW SRM 51-40-02-0G-0

Part: STRUCTURE — CRACKED (MAIN CABIN) · airframe 61,327 hrs · 31,086 cycles

CABIN HAS CHORD CRACKED AT END RADIUS BS 312 S5L-S6L. / CUT OUT DAMAGE AT CABIN CHORD AT END RADIUS BS 312 S5L-S6L; PERFORMED HFEC AND ROTO INSP NO CRACK NOTE AS PER NTM PART 6 51-00-00 PROCEDURE 23; FABRICATED ANGLE REPAIR MAT USED 7075-0 0.063 CLAD PO #1668003; PERFORMED HEAT TREAT; CONDUCTIVITY AND HARDNESS INSP AS PER BAC5946 FOUND IN LIMITS; DRILLED; DE-BURRED; TREAT; PRIMER AND INSTALLED REPAIR PART AS PER REF B737-700 SRM 53-10-07-2R-1 FIG A REPAIR 1; PERFORMED FPI SOPM 20-20-02; SRM 51-40-05-0G-0; AMM 51-21-41-701; AMM

Part: BUSHING — OUT OF TOLERANCE (VERTICAL STAB) · airframe 61,327 hrs · 31,086 cycles

FUSELAGE BULKHEAD FITTING LUG BS 1016 FOR VERTICAL STAB FRONT RIGHT ATTACHMENT HAS BUSHING OUT OF LIMITS. [0.8840'] [MAX ALLOWED 0.8835' TASK 55-30-00-200-801] / REMOVED AND REPLACED BUSHING AT FUSELAGE BULKHEAD FITTING LUG BS 1016 FOR VERTICAL STAB FRONT RIGHT ATTACHMENT AS PER EA 21-155-00122 REV IR RES 2016690-3A IR REV; VENDOR PREMIER AEROSPACE FABRICATED AND INSTALLED BUSHING RFF PO 1706834 ; PO 1707075

Part: SEAT TRACK — GOUGED (COCKPIT) · airframe 61,327 hrs · 31,086 cycles

F/O AFT OB SEAT TRACK GOUGED ON EDGE. / REMOVED AND REPLACED F/O AFT O/B SEAT TRACK IAW B737 AMM 25-11-11-400-801.

Part: SEAT TRACK — GOUGED (COCKPIT) · airframe 61,327 hrs · 31,086 cycles

CAPT AFT OB SEAT TRACK GOUGED ON EDGE. / REMOVED AND REPLACED CAPT AFT O/B SEAT TRACK IAW B737 AMM 25-11-11-400-801

Part: SUPPORT BRACKET — CRACKED (AFT CARGO) · airframe 61,327 hrs · 31,086 cycles

AFT OF AFT CARGO COMPMT. BILGE SUPPORT BRACKET CRACKED AT S-26L STA 867 BELOW WASTE TANK SUPPORT POST MKD DOT 60-014 / REMOVED AND REPLACED AFT CARGO COMPARTMENT BILGE SUPPORT BRACKET AT S-26L STA 87 BELOW WASTE TANK SUPPORT IAW B737-700 SRM 51-40-02-0G-0. PART USED: PO # 1698700

Part: FLOOR SUPPORT — CORRODED (FWD CARGO) · airframe 61,327 hrs · 31,086 cycles

FWD CARGO COMPARTMENT FLANGE SUPPORT FLOOR PANEL HAS CORROSION AT STA 490 CUTOUT TO STA 500B S-26 RT.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,327 hrs · 31,086 cycles

FWD WET AREA UNDER FLOOR PANEL 221BF AT STA # 300 LBL-55 INNER WEB WITH A CRACK. DOT # 208-61 / DAMAGED INNER CHORD AT L1 DOOR ON FWD WET AREA IT WAS REPLACED ON N.R W197743

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 61,327 hrs · 31,086 cycles

VERTICAL STAB FRONT SPAR LEFT FUSELAGE BULKHEAD ATTACH FITTING HAS PITTING CORROSION ON AFT SIDE OF AFT LUG AROUND BUSHING. / REMOVED CORROSION FROM VERTICAL STAB FRONT SPAR LEFT FUSELAGE BULKHEAD ATTACH FITTING AFT SIDE FACE AND REPLACED BUSHING ON ATTACH FITTING AS PER EA 21-153-00132 IR AND RES 2016690-5 REV IR. OUTSIDE VENDOR PREMIER AEROSPACE FABRICATED BUSHING AND INSTALLED BUSHING PO 1706328 ; PO 1706834. THIS IS A INTERIM REPAIR AND MUST BE INSPECTED AT DEFINED INTERVAL. AND PO 1707077

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 61,327 hrs · 31,086 cycles

FWD CARGO COMPARTMENT;GUSSET SUPORT IS CRACKED AT STA 500D;S-19 RH. / REMOVED AND REPLACED GUSSET AT FWD CARGO COMP. AT STA 500D STR 19RH AND TREATED ALL FASTENERS HOLES WITH ALODINE & PRIMED IN REF B737-700 SRM 57-40-02-0G-0 AND DWG #143A7902; 51-20-01-0G-0

Part: SUPPORT FRAME — CHAFED (BODY FAIRING) · airframe 61,327 hrs · 31,086 cycles

LOWER BODY FAIRING SUPPORT HAS DEEP CHAFE RBL 27 BS 663 -675. / REMOVED AND REPLACED NEW SUPPORT FRAME IAW B737-700 SRM 51-40-02-0G-0

Part: WEB — CORRODED (FWD WET AREA) · airframe 61,327 hrs · 31,086 cycles

**CORROSION** FWD WET AREA UNDER FLOOR PANEL 221DF INNER WEB ALONG L-1 DOOR CORRODED. DOT # 208-60 / CORROSION AT FWD WET AREA UNDER FLOOR PANEL 221DF INNER AREA OF L-1 DOOR FOUND LOCATED ON INNER CHORD (DOT 208-60). L1 DOOR INNER CHORD WILL BE REPLACED ON NR W197743

Part: FLOOR SUPPORT — CRACKED (FWD CABIN) · airframe 61,327 hrs · 31,086 cycles

FWD WET AREA BELOW FLOOR PANEL 222BF AT STA # 315 RBL-31 INTERCOSTAL HAS A CRACK. DOT # 208-57 / REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA BELOW FLOOR PANEL 222BF AT STA 315 RBL-31' AND LOCATED AND DRILL NEW INTERCOSTAL AND TREATED ALL FASTENERS HOLES WITH ALODINE AND PRIMED IN REF B737-700 SRM 51-40-05-0G-0 AND 51-20-01-0G-0 AND DWG # 141A5400

Part: ANGLE — CRACKED (BS 500C S25L) · airframe 61,327 hrs · 31,086 cycles

FWD CARGO COMPARTMENT;HAS CRACKED ANGLE AT STA 500C;S-25 LH. / REMOVED AND REPLACED ANGLE AT FWD CARGO COMP AT STA 500C STR26; LH AND TREATED FASTENERS HOLES WITH ALODINE AND PRIME IN REF B737-700 SRM 51-40-02-0G-0; 51-20-01-0G-0 AND DWG# 143A7505

Part: SUPPORT — CHAFED (FAIRING) · airframe 61,327 hrs · 31,086 cycles

LOWER BODY FAIRING SUPPORT HAS DEEP CHAFE LBL 27 BS 663 -675. / AFTER EVLAUATION OF LOWER BODY FAIRING SUPPORT ATLBL 27BS 663-675; THE FRAME WAS FOUND OUT OF LIMITS IAW B737-700 SRM 53-40-71-1A-1. REMOVED ;REPLACED ;LOCATED AND DRILLED AND INSTALLED NEW FAIRING SUPPORT IAW B737-700 SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND BOEING DWG#149A7216. MATERIAL USED: 149A7214-19; PO#1705074.

Part: FLOOR SUPPORT — CRACKED (AFT CABIN) · airframe 61,327 hrs · 31,086 cycles

AFT CABIN FLOOR STRUCTURE INTERCOSTAL CRACKED 2 EA PLACES BETWEEN BS 947.5 TO BS 927 BL-0 .MKD 126-32. / REMOVED INTERCOSTAL AT AFT CABIN FLOOR STRUCTURE BETWEEN STA 947.5 TO BS 927 BL-0 PER REF B737-700 SRM 51-40-02-0G-0. REMOVED AND REPLACED INTERCOSTAL'S CHORD PER REF B737-700 SRM 51-40-02-0G-0 AND DWG #147A5400. INSTALLED INTERCOSTAL AT AFT CABIN FLOOR STRUCTURE BETWEEN STA 947.5 TO BS 927 BL-0 PER REF B737-700 SRM 51-40-00-0G-0 AND DWG# 147A5400

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,327 hrs · 31,086 cycles

FUSELAGE - BS 540 S-22L REF FIG 2 CIRCLE NOTE 1 AD 2019-11-06; EO 14516. CRACK INDICATION FOUND. REF B737 NDT PART 4 53-20-02. B/C19498. REQ. REMOVE FASTENERS AND PERFORM A OHEC PROCEDURE TO VERIFY CRACK INDICATION IAW B737 NDT PART 6; 51-00-00 PROC. 16. / ACCOMPLISHED FUSELAGE BS 540 S22L DRAG LINE AND SKIN REPAIR PER INSTRUCTIONS ON EO 5331-E-14519-NG

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 61,327 hrs · 31,086 cycles

FWD PASSENGER CABIN FLOOR PANEL 222CF DELAMINATED. / RECEIVED FWD PASSENGER CABIN FLOOR 222CF. INSTALLATION WILL BE ACCOMPLISHED IN CUSTOMER CARD #JPANEL-222-CLOSE.

Part: ANGLE — WORN (FUSE TO STAB) · airframe 61,327 hrs · 31,086 cycles

RH FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE IS WORN TO STA 1016.00 THRU STA 1006.00. / REMOVED ANDREPLACED R/H FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE STA 1006 TO STA 1016 PER REF DWG 147A0030 AND B737-700 SRM 51-40-02-0G-0

Part: SEAT TRACK — WORN (MAIN CABIN) · airframe 61,327 hrs · 31,086 cycles

MAIN CABIN FLOOR SEAT TRACK CROWN AREA LBL-45.5 BS 520 WEAR MARK AT .MKD 126-031. / ACCOMPLISHED PERMANENT SEAT TRACK REPAIR AT MAIN CABIN BETWEEN STA 521.5 AND STA 500C+10.5' LBL 45.5 REF B737-700 SRM 53-00-52-2R-4 AND EA 1-A53-11779 REV 1

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 61,327 hrs · 31,086 cycles

FWD PASSENGER CABIN FLOOR PANEL 221BF DELAMINATED. / RECEIVED CABIN FLOOR PANEL 221BF. INSTALLATION WILL BE ACCOMPLISHED ON T/C JPANEL-221-CLOSE

Part: ANGLE — WORN (FUSE TO STAB) · airframe 61,327 hrs · 31,086 cycles

LH FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE IS WORN TO STA 1016.00 THRU STA 1006.00 / REMOVED AND REPLACED L/H FUSELAGE FIN BODY INTERFACE CLOSURE ANGLE STA 1006 TO STA 1016 PER REF DWG 147A0030 AND B737-700 SRM 51-40-02-0G-0

Part: DOOR SILL — CRACKED (L1 DOOR) · airframe 61,327 hrs · 31,086 cycles

L1 DOOR LOWER SILL INNER CHORD CRACKED AT FASTENER HOLE STA 312. / REMOVED AND REPLACED INNER CHORD AT L1 DOOR LOWER SILL BETWEEN STA 270 AND STA 360 LBL 55 WL 208 REF B737-700 SRM 51-40-02-0G-0 AND DWG #141A8110

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 61,327 hrs · 31,086 cycles

FWD PASSENGER CABIN FLOOR PANEL 221AF DELAMINATED. / RECEIVED FWD PASSENEGER CABIN FLOOR PANEL 221AF. INSTALLATION WILL BE ACCOMPLISHED IN CUSTOMER CARD #JPANEL-221-CLOSE

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 61,327 hrs · 31,086 cycles

FWD PASSENGER CABIN FLOOR PANEL 222AF DELAMINATED. / RECEIVED FWD PASSENGER CABIN FLOOR 222AF. INSTALLATION WILL BE COMPLETED IN CUSTOMER CARD #JPANEL-222-CLOSE.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 61,327 hrs · 31,086 cycles

FWD PASSENGER CABIN FLOOR PANEL 221CF DELAMINATED. / RECEIVED FWD PASSENGER CABIN FLOOR PANEL 221CF. INSTALLATION WILL BE ACCOMPLISHED IN CUSTOMER CARD #JPANEL-221-CLOSE.

Part: ANGLE — WORN (FUSE TO STAB) · airframe 61,327 hrs · 31,086 cycles

LH FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE IS WORN TO STA 1030.00 THRU STA 1132.02. / REMOVED AND REPLACED L/H FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE STA 1030.00 THRU STA 1132.02 PER REF B737-700 SRM 51-40-02-0G-0 AND DWG #148A8300

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 61,327 hrs · 31,086 cycles

FWD PASSENGER CABIN FLOOR PANEL 221EF DELAMINATED. / RECEIVED FWD PASSENGER CABIN FLOOR PANEL 221FF. INSTALLATION WILL BE ACCOMPLISHED IN CUSTOMER CARD #JPANEL-221-CLOSE.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 61,327 hrs · 31,086 cycles

FWD PASSENGER CABIN FLOOR PANEL 222DF DELAMINATED. / RECEIVED FWD PASSENGER CABIN FLOOR PANEL 222DF; INSTALLATION WILL BE ACCOMPLISHED IN CUSTOMER CARD #JPANEL-222-CLOSE.

Part: SEAT TRACK — WORN (MAIN CABIN) · airframe 61,327 hrs · 31,086 cycles

MAIN CABIN FLOOR SEAT TRACK CROWN AREA LBL-24.7 BS 520 WEAR MARK AT .MKD 126-030 / ACCOMPLISHED PERMANENT REPAIR AT MAIN CABIN SEAT TRACK BETWEEN STA 500C+10.5' AND STA 521.5 LBL 24.7 REF B737-700 SRM 53-00-52-2R-4

Part: STRUCTURE — CORRODED (FWD WET AREA) · airframe 61,327 hrs · 31,086 cycles

**CORROSION** FWD WET AREA STA # 344 LBL-62 UNDER FLOOR PANEL 221GF STRUCTURE HAS CORROSION. DOT # 208-53 / CORROSION FWD WET AREA STA 344 LBL 62 UNDER FLOOR PANEL 221GF LOCATE AT INNER CHORD L1 DOOR. INNER CHORD REPLACED ON NR W197743

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 61,327 hrs · 31,086 cycles

FWD PASSENGER CABIN FLOOR PANEL 221DF DELAMINATED. / THIS ITEM CLOSED; NEW PANEL WILL INSTALLED ON REFERENCE CUSTOMER CARD #JPANEL-221-CLOSE; PANEL HAS BEEN RECEIVED

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 61,327 hrs · 31,086 cycles

FWD PASSENGER CABIN FLOOR PANEL 221GF DELAMINATED. / RECEIVED FWD PASSENGER CABIN FLOOR PANEL 221GF; INSTALLATION WILL BE ACCOMPLISHED IN CUSTOMER CARD #JPANEL-221-CLOSE.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 61,327 hrs · 31,086 cycles

FWD PASSENGER CABIN FLOOR PANEL 222BF DELAMINATED. / RECEIVED FWD PASSENGER CABIN FLOOR 222BF. INSTALLATION WILL BE ACCOMPLISHED IN CUSTOMER CARD #JPANEL-222-CLOSE.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 61,327 hrs · 31,086 cycles

FWD PASSENGER CABIN FLOOR PANEL 221FF DELAMINATED. / RECEIVED FWD PASSENGER CABIN FLOOR PANEL 221FF; INSTALLATION WILLL BE ACCOMPLISHED IN CUSTOMER CARD #JPANEL-221-CLOSE

Part: BONDING STRAP — CORRODED (LT BOOST PUMP) · airframe 61,327 hrs · 31,086 cycles

CORROSION>>>>> LT WING REAR SPAR BOOST PUMP TANK 1 AFT UPPER BONDING STRAP EVIDENCE OF SURFACE CORROSION. / REMOVED AND REPLACED BONDING STRAP TO LT WING REAR SPARE BOOST PUMP TANK 1 AFT UPPER SURFACE IAW B737-700 AMM 28-22-41-000-802 / 28-22-41-400-802

Part: PRESSURE DECK — DAMAGED (COCKPIT FLOOR) · airframe 61,327 hrs · 31,086 cycles

FLIGHT DECK FLOOR WEB DAMAGE AT BS 260 / ACCOMPLISHED PERMAMENT FLIGHT DECK FLOOR WEB REPAIR REF EA 1-A53-33179 REV 1 BETWEEN STA 254 AND STA 270 LBL 20 AND RBL5.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,962 hrs · 30,233 cycles

AISLE EMERGENCY LIGHTS INOP AT ROWS 6;9; & 11 ON LT SIDE OF AIRCRAFT. / REMOVED & REPLACED EMERGENCY LIGHTS BATTERY PACK M2335 AT STA 500C+7.5 WL 213 LBL 67 I.A.W. AMM 33-51-06. OPS CHECK GOOD; ALL EMERGENCY LIGHT OPERATIVE AT THIS TIME.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 59,957 hrs · 30,229 cycles

SUPPORT BRACKET FOR R1 AND R2 DOOR SEAL DRAINS IN AFT AREA BEHIND AFT CARGO BULKHEAD CRACKED / REMOVED AND REPLACED SUPPORT BRACKET REF SRM 51-40-02

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 59,950 hrs · 30,225 cycles

FWD LAV SMOKE DETECTOR ALARM SOONDED DURING DESCENT. NO SMOKE DETECTED. OK TO CONTINUE PER MEL 26-15-02 SP1B TRACKING NO. 37069 / REMOVED AND REPLACED FWD LAV SMOKE DETECTOR PER M/M 26-14-01. CL #37111

Part: LIGHT — INOPERATIVE (ROW 6) · airframe 58,752 hrs · 29,461 cycles

L/H INTERIOR EMERGENCY AISLE LIGHT INOP AT ROW 6. / RELAMPED LIGHT PER AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,552 hrs · 29,335 cycles

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

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 57,984 hrs · 28,963 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 57,918 hrs · 28,920 cycles

AFT FLT ATT PANEL EMERGENCY LIGHT SWITCH COVER BROKEN. R&R COVER IAW CMM.

Part: LENS — DEFECTIVE (CABIN) · airframe 57,909 hrs · 28,914 cycles

RT OVERWING EXIT SIDEWALL LIGHTS DIM. R&R LENS PER AMM.

Part: LENS — DEFECTIVE (CABIN) · airframe 57,909 hrs · 28,914 cycles

LT OVERWING EXIT SIDEWALL LIGHTS DIM. R&R LENS PER AMM.

Part: LIGHT — DIM (CABIN) · airframe 57,909 hrs · 28,914 cycles

LT OVERWING EXIT SIDEWALL LIGHTS DIM. R&R BULBS PER AMM.

Part: LIGHT — DIM (CABIN) · airframe 57,909 hrs · 28,914 cycles

RT OVERWING EXIT SIDEWALL LIGHTS DIM. R&R BULBS PER AMM.

Part: SCREW — LOOSE (L2 DOOR) · airframe 57,335 hrs · 28,540 cycles

L2 DOOR EMERGENCY SLIDE COVER SCREWS CAME LOOSE. REATTACHED HARDWARE PER AMM.

Part: BOLT — LOOSE (L2 DOOR) · airframe 57,302 hrs · 28,521 cycles

L2 DOOR EMERGENCY SLIDE COVER LOOSE. SECURED BOLT IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,260 hrs · 27,865 cycles

FORWARD LT WINDSCREEN 1 FLASHLIGHT CHARGE INDICATOR WOULD NOT FLASH. R&R BATTERY IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 56,260 hrs · 27,865 cycles

AFT RT OF OVERWING EMERGENCY EXIT DOOR LIGHT LENS AND MOUNT CRACKED. R&R LIGHT IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 56,260 hrs · 27,865 cycles

G1 GALLEY EXIT LIGHT BASE AND LENS CRACKED. R&R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 56,260 hrs · 27,865 cycles

AFT LT OF OVERWING EMERGENCY EXIT DOOR LIGHT LENS AND MOUNT CRACKED. R&R LIGHT IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 56,260 hrs · 27,865 cycles

G1 GALLEY EXIT LIGHT BASE AND LENS CRACKED. R&R LIGHT IAW AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 56,260 hrs · 27,865 cycles

LT M1675 EMERGENCY BATTERY PACK WILL NOT CHARGE. R&R BATTERY PACK IAW AMM.

Part: COVER — BROKEN (CABIN) · airframe 56,260 hrs · 27,865 cycles

RT FORWARD LOWER OVERWING EXIT INDICATOR LENS PLASTIC MOUNT TAB BROKEN. R&R COVER IAW AMM.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 56,260 hrs · 27,865 cycles

AFT PIT FLOOR SUPPORT TRACK VERTICAL FLANGE CRACKED AT BS 727E, RBL 13.84. R&R TIE DOWN TRACK IAW SRM AND DWG.

Part: SKIN — NONE (FUSELAGE) · airframe 56,260 hrs · 27,865 cycles

REFERENCE DTIP NRC X898080: REPAIR ON FUSELAGE SKIN AT STA 460 STR 1 REQUIRES REPLACEMENT / REMOVED AND REPLACED FUSELAGE SKIN DOUBLER FROM STA 450-STA 465 S-1 IAW EA 190140 IR AND SWA EA NO. 1-753-34376 REV. IR.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 56,260 hrs · 27,865 cycles

REFERENCE DTIP NRC X898083- REPAIR ON AFT CARGO TIE DOWN TRACK AT STA 772.5 LBL 17.25 REQUIRES REPLACEMENT / REMOVED AND REPLACED REPAIR ON AFT CARGO TIE DOWN TRACK @ STA 772.5 LBL 17.25 IAW EA#1-A53-4982 + SRM 53-00-53-2R-3 (PER SA-M 735 SHAWN CHIRAYIL E104352)

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 56,260 hrs · 27,865 cycles

REFERENCE DTIP NRC X898085- REPAIR ON AFT CARGO FLOOR SUPPORT CHANNEL AT STA 772.5 LBL 8.1 REQUIRES REPLACEMENT / REMOVED AND REPLACED REPAIR ON AFT CARGO FLOOR SUPPORT CHANNEL AT STA 772.5 LBL 8.1 IAW B737-700 E.A 1-A53-4982 REV.3 AND SRM 53-00-53 REPAIR 2; 4

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 56,260 hrs · 27,865 cycles

REFERENCE DTIP NRC X898088- REPAIR ON AFT CARGO FLOOR SUPPORT CHANNEL AT STA 772.5 RBL 8.1 REQUIRES REPLACEMENT / REMOVED AND REPLACED REPAIR ON AFT CARGO FLOOR SUPPORT CHANNEL AT STA 772.5 RBL 8 IAW B737-700 E.A 1-A53-4982 REV. 3 AND SRM 53-00-53 REPAIR 2; 4

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 56,260 hrs · 27,865 cycles

REFERENCE DTIP NRC X898086- REPAIR ON AFT CARGO FLOOR SUPPORT CHANNEL AT STA 772.5 LBL 3.0 REQUIRES REPLACEMENT / REMOVED AND REPLACED REPAIR ON AFT CARGO FLOOR SUPPORT CHANNEL AT STA 772.5 LBL 3. IAW B737-700 E.A 1-A53-4982 REV 3; SRM 53-00-53 REPAIR 2 AND 4

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 56,260 hrs · 27,865 cycles

REFERENCE DTIP NRC X898084- REPAIR ON AFT CARGO FLOOR SUPPORT CHANNEL AT STA 772.5 LBL 12.5 REQUIRES REPLACEMENT / REMOVED AND REPLACED REPAIR ON AFT CARGO FLOOR SUPPORT CHANNEL AT STA 772.5 LBL 12.5 IAW B737-700 E.A 1-A53-4982 REV 3; AND SRM 53-00-53 REPAIR 2; 4

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 56,260 hrs · 27,865 cycles

FORWARD CARGO AFT CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA AND AMM.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 56,260 hrs · 27,865 cycles

LT SHEAR WEB CRACKED UNDER L2 CREASE BEAM, BS 986. R&R SHEAR WEB IAW DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,260 hrs · 27,865 cycles

FLOORBEAM UPPER FLANGE CORRODED AT BS 986, BETWEEN LBL 29 TO LBL 43. REPAIRED FLANGE IAW SRM AND EA.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 56,260 hrs · 27,865 cycles

AFT PIT DOOR RH CUTOUT ATTACH ANGLE IS CORRODED / REPLACED AFT PIT R/H CUTOUT ATTACH ANGLE W/NEW P/N 453A2611-1 ATAG A18227 IAW BOEING DWG 453A2600 REV

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 56,260 hrs · 27,865 cycles

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

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 56,260 hrs · 27,865 cycles

AFT PIT PANEL BOTTOM ATTACH STRIPS ARE CORRODED / RECEIVED 1EA-11 CAP STRIP FOR THE AFT CARGO PIT PANEL; NO ALLOWABLE LIMITS FOUND IN SRM PER DWG# 453A2600 SHEET 21 REV D ATAG A65014

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 56,260 hrs · 27,865 cycles

AFT PIT DOOR LH CUTOUT ATTACH ANGLE IS CORRODED / NO ALLOWABLE LIMITS FOUND IN SRM; RECIEVED 1EA-2 AFT PIT DOOR LH CUTOUT ATTACH ANGLE PER DWG # 454A2611 SHEET 2 REV C ATAG A89285

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 56,260 hrs · 27,865 cycles

AFT PIT FLOOR PANEL 140AF HAS CORROSION / REMOVED CORROSION IAW SEM 5-10-02-06-D EVALUATED FOUND TO BE OUT OF LIMITS IAW SRM 53-000-53-1A-A FABRICATED PANEL 140AF IAW 51-40-05 PG 1 TASK 4A TREATED AND PRIMED IAW AMM 51-21-72-370-804

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 56,260 hrs · 27,865 cycles

AFT CARGO FLOOR BOARD SPLICE T CORRODED BS 887 RBL 10' TO RBL 20'. / PART VERIFIED AS P/N:140A7401-37 FOR NEW T. SPLICE IAW B737-700 DRWG #; A46A7500 REV 6 - 39 T.SPLICE & FLOOR BOARD TO BE INSTALLED ON JPANEL - 141-CLOSE CARD W/0 #:38953/1600/0006

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 56,260 hrs · 27,865 cycles

AFT CARGO FLOOR BOARD T SPLICE AT BS 767 + 6' LBL 4' TO 10' CORRODED. / PART VERIFIED AS P/N:146A9401-4 FOR NEW T-SPLICE IAW B737-700 DRWG #:146A7500 REV. T -4 T.SPLICE & FLOOR BOARD TO BE INSTALLED ON JPANEL 141-CLOSE CARD W/O #:38953/1600/0006.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,260 hrs · 27,865 cycles

AFT CARGO RT Z ANGLE CORRODED BETWEEN BS 727C+10 TO BS 767, RBL 22. REPAIRED Z ANGLE IAW SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 56,260 hrs · 27,865 cycles

RIGHT ENGINE O/B FAN COWL; SUPPORT BRACKET AFT OF OIL ACCESS DOOR IS CRACKED. / REMOVED AND REPLACED R/H ENGINE O/B FAN COWL SUPPORT BRACKET AFT OF OIL DOOR IAW SRM 51-40-02-0G-0 AND CMM 71-13-30 A TAG A13657

Part: WEB — CRACKED · airframe 56,260 hrs · 27,865 cycles

#1 ENGINE FAN COWL AT 414 AR DOOR SURROUND VERTICAL WEB CRACKED. / REMOVED AND REPLACED VERTICAL WEB AT #1ENG FAN COWL 414AR DOOR SURROUND IAW B737 SRM 51-40-02-0G-0 & CMM 71-13-30

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 56,260 hrs · 27,865 cycles

LT MAIN LANDING GEAR WHEEL WELL LOWER LT VAPOR BARRIER WEB CRACKED AT BS 663, BETWEEN LBL 31 TO LBL 40. REPAIRED VAPOR BARRIER IAW SRM & DWG.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 56,260 hrs · 27,865 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 120AF HAS CORROSION ALONG EDGES / REMOVED CORROSION ON FWD CARGO COMPT FLOOR PANEL 120AF IAW SRM 51-10-02-0G-0. VISUAL INSPECTION WITH 10X MAG GLASS NO DEFECTS BLENDING AREAS EXCEED THE MAX ALLOW ABLE ; OUT OF LIMITS IAW SRM 53-00-53-1A-1; STEP 5A (1)(B)(1). - FABRICATED A REPLACEMENT PANEL 120AF IAW BOEING DWG- 453A1610 SHT 9 REV F. P/N 453A1610-14 TOOL 36646 CAL 02OCT19 ATAG A74221

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 56,260 hrs · 27,865 cycles

LEFT WING TO BODY FAIRING 193AL EXTERIOR SURFACE OUTER LAYER IS DELAMINATED AND PEELING AT FORWARD EDGE / REPAIRED OUTER MOST (LAYER FOIL MESH PLY) I/A/W SRM 51-70-14-2R-4 PAR 5 REV 66 ON LEFT WING TO BODY FAIRING 193AL EXTERIOR SURFACE FWD EDGE AS MARKED

Part: PLATE — CRACKED (RIGHT WING) · airframe 56,109 hrs · 27,773 cycles

RH FLAP UPPER SHELF PANEL DEFLECTION RIB SERRATED PLATE AREA CRACKED AT FASTENER HOLES / REPAIRED SHELF PANEL DEFLECTION RIB SERRATED PLATE AREA PER SRM 57-51-02-2R-1

Part: BRACKET — CRACKED (LEFT WING) · airframe 56,109 hrs · 27,773 cycles

L/H T/E REAR UPPER FIXED T/E PANEL HAS CRACKED SEAL RETAINER ABOVE #1 ENGINE PYLON AFT FAIRING / REMOVED AND REPLACED SEAL RETAINING BRACKET PER SRM 51-40-02

Part: RETAINER — CRACKED (RIGHT WING) · airframe 56,109 hrs · 27,773 cycles

RH FLAP UPPER SHELF PANEL FOR DEFLECTION RIB SEAL RETAINER CRACKED AT FASTENER HOLE / INSTALLED NEW RIB SEAL RETAINER ON RH FLAP UPPER SHELF PANEL PER SRM 51-40-02

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 55,282 hrs · 27,236 cycles

LT WHEEL WELL LOWER STIFFENER CRACKED AT BS 663, LBL 25. R&R STIFFENER PER SRM.

Part: SENSOR — FAULTY (LE FLAP) · airframe 54,110 hrs · 26,468 cycles

DIVERSION, ON TAKE-OFF GOT INTERMITTENT "LE FLAP TRANSIT" LIGHT ALONG WITH AN INTERMITTENT "GREEN EXT" LIGHT ON THE NR 3 LE FLAP. R&R NR 3 KRUGER FLAP EXTEND SENSOR PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 53,974 hrs · 26,381 cycles

EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATION M1672. R&R BATTERY PER AMM & DWG.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,790 hrs · 26,264 cycles

AFT CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,790 hrs · 26,264 cycles

AFT OF L2 DOOR LT EXTERIOR EMERGENCY EXIT LIGHT INOP. R&R LAMP PER AMM.

Part: SUPPORT — CRACKED (LWR FUSELAGE) · airframe 53,790 hrs · 26,264 cycles

BS 727 +2.7 RBL 35 FAIRING SUPPORT STRUCTURE PART NUMBER 149A7511-6 IS CRACKED / BS 727 & 2.7 RBL35 FAIRING SUPPORT STRUCTURE PART NUMBER 149A7511-6 WITH A CRACK WAS REPAIRED IAW SRM 51-70-05-2R-7

Part: FAIRING — BROKEN (LWR FUSELAGE) · airframe 53,790 hrs · 26,264 cycles

WING TO BODY FAIRING AT R/H AFT WHEEL WELL PART NUMBER 149A7656-6 IS BROKEN / REMOVED AND REPLACED WING TO BODY FAIRING PANEL AT R/H AFT MWW PART # 149A7656-6 IAW SRM 51-40-02-0G-0

Part: FORMER — CRACKED (LWR FUSELAGE) · airframe 53,790 hrs · 26,264 cycles

WING TO BODY FAIRING FORMER AT BS 727 +2.7 RBL 35 IS BROKEN / REMOVED AND REPLACED WING TO BODY FAIRING FORMER B.S 727 + 2.7 RBL 35 MWW IAW SRM 51-40-02-0G-0 AND DWG #149A7502

Part: GIRT BAR — STUCK (R1 DOOR) · airframe 52,503 hrs · 25,470 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STUCK WILL NOT STOW CORRECTLY. CLEANED GIRT BAR IAW SIP.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 52,503 hrs · 25,470 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE ATTACHMENT TO GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR IAW AMM.

Part: BRACKET — CRACKED (LEFT WING) · airframe 51,840 hrs · 25,044 cycles

L/H WING FLAP SEAL RETAINING BRACKET UNDER PNL 551GB IS CRACKED / REMOVED AND REPLACED L/H WING FLAP SEAL RETAINING BRACKET UNDER PANEL 551GB IAW SRM#51-40-02

Part: PANEL — BROKEN (LOWER EXT FUSELA) · airframe 51,591 hrs · 24,890 cycles

PANEL 194BR AFT CORNER BROKEN. / REPAIRED PANEL 194 BR IAW B737-700 SRM 51-70-05-2R-10 REV 62 RESTORED FINISH IAW B737 AMM 51-21-99-300-801 PARA E (6) TABLE 701

Part: LANYARD — LOOSE (R1 DOOR) · airframe 50,416 hrs · 24,163 cycles

R1 DOOR EMERGENCY EVAC SLIDE CABLE LOOSE. SECURED LANYARD PER SIP.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 49,731 hrs · 23,747 cycles

LT MAIN LANDING GEAR WHEEL WELL CENTER WING SECTION LOWER LT WEB VAPOR BARRIER CRACKED BETWEEN LBL 31.83 TO LBL 24.92 STIFFENERS. REPAIRED WEB PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,403 hrs · 23,558 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 46,611 hrs · 21,921 cycles

AFT GALLEY EMER EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 44,537 hrs · 20,701 cycles

R2 DOOR EVAC SLIDE LOOSE. SECURED SLIDE ASSEMBLY IAW MM.

Part: MODULE — FAULTY (COCKPIT) · airframe 44,513 hrs · 20,692 cycles

DECLARED EMER, DURING APPROACH, LANDING GEAR HANDLE WOULD NOT MOVE FROM THE OFF POSITION. CYCLED, NO HELP. R & R LANDING GEAR CONTROL LEVER MODULE IAW AMM.

Part: WIRE — DAMAGED (CABIN) · airframe 43,183 hrs · 19,929 cycles

L1 DOOR EMER EVAC SLIDE LIGHT WIRE INOPERATIVE. REPAIRED WIRE IAW SWPM & MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

WEB CORRODED BETWEEN BS 500 - 500A, STRINGER 26R. R & R WEB IAW SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 43,183 hrs · 19,929 cycles

R1 DOOR FWD FRAME LOWER CORNER CRACKED AT LOWER INBD FASTENER BS 295, WL 208. R & R FRAME IAW AMM & SRM.

Part: FAIRING — CRACKED (LT MLG WW) · airframe 43,183 hrs · 19,929 cycles

LEFT MAIN WW SURROUND FAIRING AFT OF WW CRACKED AT BS 727, LBL 48. R & R FAIRING IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

FUSELAGE STRINGER CORRODED AT STATION 312 - 328, STRINGER 29L. R & R STRINGER SECTION IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

FRAME CRACKED AT BS 827, STRINGER 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

FRAME CRACKED AT BS 747, STRINGER 9L. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO 360, BL 0. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO 294.5, WL 208. R & R INTERCOSTAL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

FUSELAGE FRAME CRACKED AT STATION 360, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

FRAME CRACKED AT BS 727D, STRINGER 9L. REPAIRED FRAME IAW EA.

Part: PLATE — CORRODED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727+4 TO BS 847, LBL 21. REPAIRED PLATE IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

INTERCOSTAL CORRODED AT BS 991, STRINGER 21L. R & R INTERCOSTAL IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727+4 TO BS 767, RBL 21. R & R SUPPORT IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

AFT CARGO BAY ON SUB THRESHOLD WEB CORRODED BETWEEN BS 792 - 847, BETWEEN RBL 20 - RBL 28. R & R WEB IAW SRM & DWG.

Part: PLATE — CORRODED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 887 TO 907, RBL 22. R & R PLATE IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

AFT CARGO BAY ON INTERCOSTAL CORRODED BETWEEN BS 747 - 767, STRINGER 25R. R & R INTERCOSTAL IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

CREASE BEAM WEB CRACKED BETWEEN BS 927 TO 947, WL 208 RT. R & R WEB IAW SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

AFT CARGO BAY ON SUB THRESHOLD INBD STRAP CORRODED BETWEEN BS 792 - 847, RBL 19. R & R STRAP IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

INTERIOR SEAT TRACK FLANGE FWD OF BS 727B, LBL 45 BOTH AFT HOLES CRACKED. REPAIRED FLANGE IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

INTERIOR SEAT TRACK FLANGE FWD OF BS 727B, RBL 45 INBD AFT HOLE CRACKED. REPAIRED FLANGE IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

INTERIOR SEAT TRACK FLANGE FWD OF BS 727B, LBL 25 BOTH AFT HOLES CRACKED. REPAIRED FLANGE IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

INTERIOR SEAT TRACK FLANGE FWD OF BS 727B, RBL 25, BOTH AFT HOLES CRACKED. REPAIRED FLANGE IAW ER & EA.

Part: RIB — CRACKED (RT WING) · airframe 43,183 hrs · 19,929 cycles

RIGHT WING FIXED TE SUPPORT RIB CRACKED ABOVE DEFLECTION ROLLER SUPPORT BETWEEN INBD & OTBD FLAPS. R & R RIB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 480 TO 500D, LBL 23. R & R SUPPORT IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,183 hrs · 19,929 cycles

FORWARD CARGO BAY ON INTERCOSTAL CORRODED BETWEEN BS 500B TO 500C, STRINGER 26R. R & R INTERCOSTAL IAW SRM & DWG.