N265WN

Part: STOP PIN — BROKEN (GIRT BAR) · airframe 61,835 hrs · 37,422 cycles

FWD SERVICE DOOR ESCAPE SLIDE GIRT BAR BROKEN; PLASTIC STOP RING BROKE OFF. INSTALLED NEW STOP PINS PER AMM 25-66-01

Part: PLATE — BULGED (ZONE 100) · airframe 61,077 hrs · 36,922 cycles

DOUBLER FOR LAV SERVICE PAN ASSY HAS BULGING AROUND LOWER ROW OF FASTNERS DUE TO CORROSION FROM BS 847 - 867 JUST ABOVE S25L. THERE IS ALSO HEAVY INTERGRANULAR CORROSION ON THE METAL STRIP DOUBLER FOR LAV SERVICE PAN ASSY HAS BULGING AROUND LOWER ROW OF FASTNERS DUE TO CORROSION FROM BS 847 - 867 JUST ABOVE S25L. THERE IS ALSO HEAVY INTERGRANULAR CORROSION ON METAL STRIP AT THE LOWER AFT CORNER OF THE PAN AT BS 847 + 18 INCHES. REMOVED LOWER LAV SERVICE PAN DOUBLER IAW SRM 51-40-02. NDT HOLES PER 51-00-00 FIG 16. NO DEFECTS NOTED. FABRICATED LAV PLATE-HINGE CLOSEOUT IAW DWG 146AA7401 IN CONJUNCTION WITH PL 146A7401-10. INSTALLED LAV SVC DOOR CLOSE HINGE CLOSE OUT PLATE REF DWG 146AA7401 AND SRM 51-40-02.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 60,148 hrs · 36,340 cycles

L2 OUTSIDE EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-04 OPS CHECK GOOD

Part: SEAT BACK — OUT OF ADJUST (ZONE 200) · airframe 59,341 hrs · 35,863 cycles

PASSENGER SEAT 11D RECLINES INTO AN EXIT ROW<[01] LOCKED OUT RECLINE HYDROLOK PER CMM 25-22-46.;[02] INSPECTED PER CMM 25-22-46

Part: MOUNT — CRACKED (ZONE 800) · airframe 59,341 hrs · 35,863 cycles

AFT ENTRY DOOR FWD SLIDE MOUNT; UPPER ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR FWD SLIDE MOUNT; UPPER ISOLATOR IAW SRM 51-40-02.;[02] INSPECTED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M1670 INOP<[01] REPLACED POWER SUPPLY - BATTERY PACK M1670 PER AMM 33-51-06-960-805. GOOD TEST.;[02] CERTIFIED CARD COMPLETED;[03] VERIFIED CORRECTIVE ACTION 1-2.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M1674 INOP<[01] REPLACED BATTERY PACK M1674 AND PERFORMED A GOOD FUNCTIONAL TEST PER AMM 33-51-06-960-805 & WDM 33-51-12-2;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M1668 INOP<[01] REPLACED BATTERY PACK M1668 PER AMM 33-51-06-960-805 & WDM 33-51-13<BR><BR>ASILE LIGHTS ON ROW 9-12 L/H STILL INOP DURING FUNCTIONAL CHECK; TROUBLESHOOTED BY RELAMPING AND RECONNECTING. BAD FUSE IS SUSPECTED.;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION ITEM 1.;[04] REPLACED BATTERY CHARGER FUSES M1668 AND PERFORMED GOOD FUNCTIONAL TEST PER AMM 33-51-06-960-804 & WDM 33-51-13;[05] VERIFIED CORRECTIVE ACTION ITEM 4; CARD COMPLETE.

Part: SKIN — CORRODED (ZONE 100) · airframe 58,179 hrs · 35,149 cycles

WI-FI ANTENNA SKIN DOUBLER HAS SEVERAL CORROSION SPOTS (FASTENERS AND SKIN) BS 727B+12 TO BS 747+6; STR 3L TO STR 3R CROWN AREA.<[01] 'REPAIRED PER EA 24-153-02600 WITH AN INSPECTION THRESHOLD/PROGRAM DEFINED IN 24-153-02600-INSP.';[02] 'REPAIRED PER EA 24-153-02600 WITH AN INSPECTION THRESHOLD/PROGRAM DEFINED IN 24-153-02600-INSP.';[03] VERIFIED CORRECTIVE ACTION 2

Part: PLATE — CORRODED (ZONE 100) · airframe 58,179 hrs · 35,149 cycles

PLATE UNDER PSC ANTENNA HAS CORROSION AT BS 727E+15; LBL5 AND WL 306<[01] 'REFER TO FAULT TTG8Q00VV56H.';[02] VERIFIED ITEM 1

Part: FRAME — CRACKED (ZONE 100) · airframe 58,179 hrs · 35,149 cycles

CRACKED FRAME BS 312 COMMON TO STR 6L LBL 33 WL 282.<[01] REPAIRED FRAME BS 312 COMMON TO STR 6L; LBL33; WL 282 PER EA M-22-153-01244 CUSTOMER SYSTEM ID: TTG8Q00VWUP8.;[02] VERIFIED CORRECTIVE ACTION #1

Part: SUPPORT PLATE — CORRODED (ZONE 100) · airframe 58,179 hrs · 35,149 cycles

CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] EVALUATION AND REMOVED DAMAGED FLOOR TO SIDEWALL SUPPORT. LOCATED; DRILLED; APPLIED WHITE ENAMEL AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 53-00-53-1A-2; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 DWG 146A7500 REV: A; AND DWG 146A0061 REV: A;[02] CORRECTIVE ACTION COMPLETED.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 58,179 hrs · 35,149 cycles

CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] REMOVED AND REPLACE FLOOR TO SIDEWALL SUPPORT AS PER SRM 50-40-02-0G-0; DWG 146A0061 REV. A. 146A7500 REV. A.;[02] CORRECTIVE ACTION 1 SHOLD BE IAW SRM 51-40-02-0G-0 CORRECTION.;[03] VERIFIED CORRECTIVE ACTION COMPLETED THROUGH STEPS 1-5

Part: SPLICE STRAP — CORRODED (ZONE 100) · airframe 58,179 hrs · 35,149 cycles

CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6 RBL11.5 WL156<[01] CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. RECEIVED NEW FLOOR SPLICE STRAP ON PO# 889099; AND NEW STRAP TO BE INSTALLED ON FAULT TTG8Q00US9J8.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-4

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CRACKED ATTACH ANGLE AT FWD WET AREA BS294 RBL53 WL208. MARKED<[01] CRACKED ATTACH ANGLE WILL BE REPLACED ON TTG8Q00VPT1S.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: WEB — CORRODED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

WHILE WORKING R/H OVERWING EXIT DUE TO CORROSION EVAL; REMOVED SEALANT AROUND CORRODED AREAS; AND NOTICED A DRILLED START AT BS 616+20; WL221; RBL70.<[01] COMPLETED STEPS 1 AND 2;[02] APPLICABILITY AND LIMIT STATEMENTS.;[03] BLENDED AND REMOVED DRILL START DAMAGE AT STA 616+20 WL 221 RBL 70 R/H OVERWING EXIT LOWER SILL IAW SRM 53-40-15-1A-1 FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED R/H OWE LOWER SILL PER SRM 51-40-02-0G-0 INSTALLED NEW WEB AT BS 616+20; WL221; RBL70. IAW SRM 51-40-02; BOEING DWG# 144A8201 REV :-;[04] VERIFIED CORRECTIVE ACTION #3

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CRACKED INTERCOSTAL BS 344-360 RBL 11 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 344-360 RBL 11 WL 208 IAW SRM 51-40-02-0G-0 REF DWG 141A5400 NO REV; DATE 02-24-96;[02] VERIFIED CORRECTIVE ACTION 1

Part: ANGLE — CRACKED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CRACKED ANGLE BS 294 O/B OF MOPSILL RBL 53 WL 208.<[01] REMOVE AND REPLACED NEW REPAIR ANGLE BS 294 O/B OF MOPSILL RBL 53 WL 208 IAW SRM 53-10-15-2R-7 AND SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION 1

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 58,179 hrs · 35,149 cycles

CRACKED INTERCOSTAL BS 344-360 LBL 12 WL 208.<[01] UPDATED STEP 3.;[02] REMOVED CRACKED INTERCOSTAL BS 344-360 LBL 12 WL 208 IAW SRM 51-40-02-0G-0 AND REPLACED INTERCOSTAL AT BS 344-360 LBL 12 WL 208 PER SRM 51-40-05-0G-0 AND DWG 141A5400 REV=A.;[03] VERIFIED CORRECTIVE ACTION 2

Part: GIRT BAR — CORRODED (ZONE 800) · airframe 58,179 hrs · 35,149 cycles

CORROSION ON FWD ENTRY DOOR FWD GIRT BAR FITTING BS 312 LBL 50 WL 208.<[01] REMOVED & REPLACED FWD ENTRY DOOR FWD GIRT BAR FITTING BS 312 LBL 50 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5220 REV=-.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CRACKED INTERCOSTAL BS 328-344 LBL 45 WL 208. EDIT: INTERCOSTAL IS AT BS 312-328 LBL 45 WL 208<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 312-328 LBL 45 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5400 REV: - DATE 10/08/96;[02] VERIFIED CORRECTIVE ACTION 1

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CRACKED INTERCOSTAL BS 312-328 LBL 45 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS312-BS328 LBL45 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV - OK;[02] CORRECTIVE ACTION COMPLETED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CRACKED INTERCOSTAL BS 294-297 RBL 1 WL 208.<[01] UPDATED STEP 1.;[02] UPDATED STEP 3.;[03] UPDATED STEP 3.;[04] REMOVED & REPLACED INTERCOSTAL BS 294-297 RBL 1 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5400 REV=-.;[05] VERIFIED ACTION 4.<BR>JOB COMPLETE.

Part: STRAP — CORRODED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CORROSION ON REINFORCEMENT STRAP BS 1016-1029 LBL 2 WL 208.<[01] REMOVED AND REPLACED REINFORCEMENT STRAP AT BS 1016-1029 LBL 2 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 147A5600 REV B DATE 05/06/09;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: SHEAR WEB — CORRODED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CORROSION ON AFT L/H SHEAR WEB BS 1016 LBL 11-LBL 22 WL 208.<[01] UPDATED STEP 1;[02] REMOVED AND REPLACED AFT L/H SHEAR WEB AT BS 1016-1026 LBL 0 - LBL 38 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 147A5600 REV B DATE 05/06/09;[03] VERIFIED CORRECTIVE ACTION ENTRY 2.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CABIN FLOOR PANEL 241ABF O/B EDGE IS DELAMINATED (AS MARKED)<[01] FLOOR PANEL 241ABF O/B EDGE DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-10-A00948 (REPAIR 10 - REPAIR OF DAMAGE TO THE CORE ON AN EDGE IN COMPOSITE FLOOR PANELS - PERMANENT] ATTACHED CURE SHEET TO THIS FAULT. VERIFIED CORRECTIVE ACTION ITEM 1.;[03] ADDED OMITTED FAILURE TYPE 05 AND UPDATED MEASUREMENT FIELDS.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CORROSION ON FLOOR BEAM BS 986 RBL 45 WL 208.<[01] CORROSION ON FLOOR BEAM BS 986 RBL 45 WL 208 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AND REPAIRED IAW SRM 53-70-51-2R-6 REPAIR 6 ALT. 4.;[02] CORRECTIVE ACTION COMPLETED;

Part: REINFORCEMENT — CORRODED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CORROSION ON REINFORCEMENT STRAP BS 1016-1026 RBL 3 WL 208.<[01] REMOVED AND REPLACED REINFORCEMENT STRAP BS 1016-1026 RBL 3 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 147A5730 REV C DATE 02/25/08;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CRACK FOUND ON FSD STUB FRAME AT BS291.5 + 8; 0.8' ABOVE SEAL DEPRESSOR 1.2' IN LENGTH (MARKED)<[01] REMOVED FSD STUB FRAME IAW SRM 51-40-02-0G-0 AND INSTALLED NEW FSD STUB FRAME IAW SRM 51-40-02-0G-0 AND DWG 141A8370 REV. D.;[02] CORRECTIVE ACTION COMPLETED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CRACKED INTERCOSTAL BS 927-947 LBL 3 WL 208. CRACKED ATTACH UPPER ANGEL ON INTERCOSTAL AT BS 927-947 LBL 3 WL 208.<[01] REMOVED AND REPLACED CRACKED INTERCOSTAL BS 927-947 LBL 3 WL 208. IAW SRM 51-40-02; BOEING DWG# 147A5400 REV :-;[02] VERIFIED CORRECTIVE ACTION 1.

Part: DOOR — CORRODED (ZONE 100) · airframe 58,179 hrs · 35,149 cycles

LAV SERVICE DOOR INNER SURFACE HAS CORROSION ON AFT EDGE<[01] REMOVED AND REPLACED DAMAGED LAV SERVICE PANEL PER AMM 52-49-07-000-801; 52-49-07-400-801; AMM 20-50-11-910-801; PERFORMED A GOOD RESISTANCE CHECK ON BONDING JUMPER PER AMM 52-49-07-400-801 STEP 3.C(1;E). TORQUE WRENCH ID: ATS2659 DUE DATE 04/2025; BONDING METER ID: ATS 312 DUE DATE 12/2025.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: WEB — CORRODED (ZONE 200) · airframe 58,179 hrs · 35,149 cycles

CORROSION ON R/H OVERWING EXIT CUT-OUT SILL AT STA 616+8; 616+9M 616+14; 616+15; 616+20; WL 221; RBL 70.<[01] COMPLETED STEPS 2 AND 3;[02] REMOVED CORROSION FROM R/H OVERWING EXIT CUT-OUT LOWER SILL AT STA 616+8; 616+9; 616+14; 616+15 AND 616+20 WL 221 RBL 70 AND FOUND TO BE WITHIN LIMITS IAW SRM 51-10-02-0G-0 AND SRM 53-40-15-1A-1;[03] THIS FAULT HAS DAMAGE REMOVAL IN LIMITS; AND REQUIRES FOLLOW-ON TASK RE-INSPECTION PER SRM 53-40-15-1A-1. AMT FAILED TO STATE THAT WEB IS BEING REPLACED DUE TO ADJACENT DAMAGE; SO THE FOLLOW-ON INSPECTIONS NO LONGER APPLY. REQUIRES ACTION BY THE AMT TO CONTACT ADMINISTRATOR AND MXI ADJUSTMENT.;[04] REMOVED CORROSION FROM R/H OVERWING EXIT CUT-OUT LOWER SILL AT STA 616+8; 616+9; 616+14; 616+15 AND 616+20 WL 221 RBL 70 IAW SRM 51-10-02-0G-0 AND THE REMOVAL AND REPLACEMENT OF THE R/H OWE LOWER SILL WILL BE ACCOMPLISHED ON FAULT# TTG8Q00VQLP6;[05] VERIFIED ACTION 4.<BR>JOB COMPLETE.

Part: VAPOR BARRIER — DEBONDED (ZONE 100) · airframe 58,179 hrs · 35,149 cycles

STA 663 VAPOR BARRIER PREVIOUS REPAIR IS DISBONDED AT WL 160; LBL 40.<[01] VAPOR BARRIER PREVIOUS REPAIR REMOVED & REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 58,179 hrs · 35,149 cycles

CRACKED LOWER R/H COMPOSITE BULKHEAD AT BS663 RBL36 WL163.<[01] CRACKED LOWER R/H BULKHEAD BS663 WAS REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: ATTACH ANGLE — CRACKED (ZONE 600) · airframe 58,179 hrs · 35,149 cycles

(RIGHT WING) UPPER WING PANEL SUPPORT U CHANEL AT 9-INCH O/B OF FUSELAGE; ATTACH ANGLE CRACKED AT REAR SPAR ATTACH POINT<[01] REMOVED AND REPLACED ANGLE P/N 115A5582-2 AT R/WING PANEL SUPPORT U CHANEL AND REAR SPAR ATTACH POINT IAW SRM 51-40-02-0G-0.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: ATTACH ANGLE — CRACKED (ZONE 500) · airframe 58,179 hrs · 35,149 cycles

LT WING T/E DEFLECTION CONTROL RIB I/B ATTACHED ANGLE CRACK<[01] VERIFIED;[02] VERIFIED;[03] REMOVED AND REPLACED LEFT WING T/E DEFLECTION CONTROL RIB I/B ATTACHMENT ANGLE IAW SRM 51-40-02-0G-0 PAR 4.;[04] REJECT ACTION 3: MISSING INSTALLATION DRAWING ON STATEMENT;[05] REMOVED AND REPLACED LEFT WING T/E DEFLECTION CONTROL RIB I/B ATTACHMENT ANGLE IAW SRM 51-40-02-0G-0 AND DWG. 115A6200; REV. B.;[06] VERIFIED CORRECTIVE ACTION 5

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 56,969 hrs · 34,406 cycles

EMX LIGHT BATT PACK M01672 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX LIGHT BATT PACK M01672 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Part: THRESHOLD — CRACKED (FWD CARGO) · airframe 56,969 hrs · 34,406 cycles

FUSELAGE FORWARD CARGO CENTER THRESHOLD IS CRACKED AT AFT DOOR STOP.<[01] R/R FWD CARGO DOOR CENTER THRESHOLD PER AMM 53-11-02

Part: PANEL — CRACKED (ZN 800 DOOR) · airframe 53,256 hrs · 32,067 cycles

AFT SERVICE R2 DOOR LOWER PANEL 844DZ AFT BRACKET CRACKED<[01] REMOVED AND REPLACED AFT SERVICE DOOR LOWER PANEL 844DZ PAN REF AMM 52-41-31.

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 53,256 hrs · 32,067 cycles

MID CABIN RH SIDE EMERGENCY BATTERY FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1669 IAW AMM 33-51-06.

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 53,256 hrs · 32,067 cycles

AFT CABIN LH SIDE EMERGENCY BATTERY FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1673 IAW AMM 33-51-06.

Part: NONE — INOPERATIVE · airframe 52,234 hrs · 31,391 cycles

INOP BATTERY PACK LOCATED LT SIDE AT FWD GALLEY AREA 2022-467055 / [01] REPLACED BATTERY PACK P/N AD-B717-01-100SWA S/N 41847 OFF; P/N AD-B717-01-100SWA S/N BN 265159 ON; IAW B737-700 AMM 33-51-06-960-805 TEST NEW BATTERY PACK OK.;[02] REPLACED BATTERY PACK P/N AD-B717-01-100SWA S/N 41847 OFF; P/N AD-B717-01-100SWA S/N BN 265159 ON; IAW B737-700 AMM 33-51-06-960-805 TEST NEW BATTERY PACK OK.

Part: ANGLE — BROKEN (FUSELAGE) · airframe 52,234 hrs · 31,391 cycles

BROKEN BODY FAIRING SUPPORT ANGLE LOCATED AT BS 500D LT SIDE AT LOWER FUSELAGE 2022-467011 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT BS 500D LT SIDE AT LOWER FUSELAGE BODY FAIRING IAW B737-700 SRM 51-40-02 AND DWG# 116A3010; SHEET: 3; REV: - AND DWG# 116A3010; SHEET: 7; REV: B.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[02] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT BS 500D LT SIDE AT LOWER FUSELAGE BODY FAIRING IAW B737-700 SRM 51-40-02 AND DWG# 116A3010; SHEET: 3; REV: - AND DWG# 116A3010; SHEET: 7; REV: B. <BR>SEE INDIVIDUAL SIGNS-OFF BELOW

Part: STUD — BROKEN (FUSELAGE) · airframe 52,234 hrs · 31,391 cycles

BROKEN STUD RECEPTACLE ON BRACKET AE0502A E5-2 2022-467012 / [01] REPLACED STUD RECEPTACLE LOCATED ON BRACKET AE0502A E5-2 I.A.W B737-700 SRM 51-40-02-0G-0.;[02] REPLACED STUD RECEPTACLE LOCATED ON BRACKET AE0502A E5-2 I.A.W B737-700 SRM 51-40-02-0G-0.

Part: BRACKET — BROKEN · airframe 52,234 hrs · 31,391 cycles

BROKEN STUD RECEPTACLE ON BRACKET AE0502A E5-2 2022-467012 /

Part: SUPPORT ANGLE — BROKEN (LH WING) · airframe 52,234 hrs · 31,391 cycles

BROKEN BODY FAIRING SUPPORT ANGLE LOCATED AT BS 500D LT SIDE AT LOWER FUSELAGE 2022-467011 /

Part: STRAP — CRACKED (FWD CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK STRAP AT FLOOR AREA BS 500 BTW STR 25R TO STR 25L AT FWD CARGO COMPARTMENT 2022-467013 / [01] REPLACED STRAP AT FLOOR AREA BS 500 BTW STR 25R TO STR 25L AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING #143A7500; SHEET 58; REV -.<BR>SEE INDIVIDUAL SING-OFFS BELOW;[02] REPLACED STRAP AT FLOOR AREA BS 500 BTW STR 25R TO STR 25L AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING #143A7500; SHEET 58; REV -. <BR>SEE INDIVIDUAL SING-OFFS BELOW RII CERTIFIED

Part: NONE — CRACKED (AFT CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 11 INCHES AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT 2022-467005 / [01] REPLACED ANGLE-SUPPORT LOCATED BS907 PLUS 11 INCHES AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 AND DWG 147A7221 REV:D.;[02] REPLACED ANGLE-SUPPORT LOCATED BS907 PLUS 11 INCHES AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 AND DWG 147A7221 REV:D. SEE INDIVIDUAL SING OFFS BELLOW .;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SING OFFS BELLOW

Part: NONE — CRACKED (AFT CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 7 INCHES AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT 2022-467004 / [01] REPLACED SUPPORT ANGLE LOCATED BS907 PLUS 7 INCHES AND BETWEEN STR25R TO STR27R <BR>AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. AND DWG 147A7221 REV:D;[02] CORRECTED STEP 1.<BR>REPLACED SUPPORT ANGLE LOCATED BS907 PLUS 7 INCHES AND BETWEEN STR25R TO STR27R <BR>AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. AND DWG 147A7221 REV:D SEE INDIVIDUAL SING OFFS BELLOW;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SING OFFS BELLOW

Part: NONE — CRACKED (AFT CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 7 INCHES AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT 2022-467004 / [01] REPLACED SUPPORT ANGLE LOCATED BS907 PLUS 7 INCHES AND BETWEEN STR25R TO STR27R <BR>AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. AND DWG 147A7221 REV:D;[02] CORRECTED STEP 1.<BR>REPLACED SUPPORT ANGLE LOCATED BS907 PLUS 7 INCHES AND BETWEEN STR25R TO STR27R <BR>AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. AND DWG 147A7221 REV:D SEE INDIVIDUAL SING OFFS BELLOW;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SING OFFS BELLOW

Part: NONE — CRACKED (AFT CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 11 INCHES AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT 2022-467005 / [01] REPLACED ANGLE-SUPPORT LOCATED BS907 PLUS 11 INCHES AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 AND DWG 147A7221 REV:D.;[02] REPLACED ANGLE-SUPPORT LOCATED BS907 PLUS 11 INCHES AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 AND DWG 147A7221 REV:D. SEE INDIVIDUAL SING OFFS BELLOW .;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SING OFFS BELLOW

Part: FITTING — CRACKED (AFT CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK ON FITTING LOCATED BS 947.5 AND STR 26L AT AFT CARGO COMPARTMENT 2022-467006 / [01] TOOL USED: DIGITAL CALIPER; P/N:500-197-30;S/N:A21143495;DUE DATE:29-JUN-23.;[02] REPLACED FITTING AND FASTENERS LOCATED BS 947.5 AND STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9. PART NUMBER USED: 149A8113U6 P.O: 2022-197003.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED FITTING AND FASTENERS LOCATED BS 947.5 AND STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9. PART NUMBER USED: 149A8113U6 P.O: 2022-197003. <BR>SEE INDIVIDUAL SIGN OFFS BELOW.<BR>AS RII

Part: FLANGE — DEBONDED (FUSELAGE) · airframe 52,234 hrs · 31,391 cycles

DELAMINATED DISTRIBUTION BAY MIX MANIFOLD 2022-466992 / [01] TOOL USED: CALIPER P/N:500-197-30 S/N:15120589 DUE DATE: 28-NOV-22;[02] TOOL USED: SCALE P/N:91847 S/N:AE-409318 DUE DATE: 06-JUN-23;[03] PERFORMED VISUAL AND TAP TEST INSPECTION ON REPORTED AREA AND ONLY FOUND DEBONDED FLANGE ON DISTRIBUTION BAY MIX MANIFOLD IAW B737 NDT 51-05-01. BONDED FLANGE ON DISTRIBUTION BAY MIX MANIFOLD IAW DWG 65C28007;[04] CORRECTIVE ACTION 3 ENTRY BY ERROR <BR><BR>THE CORRECTED IS:PERFORMED VISUAL AND TAP TEST INSPECTION ON REPORTED AREA AND ONLY FOUND DEBONDED FLANGE ON DISTRIBUTION BAY MIX MANIFOLD IAW B737 NDT 51-05-01. BONDED FLANGE ON DISTRIBUTION BAY MIX MANIFOLD IAW DWG 65C28007. SEE INDIVIDUAL SIGNOFFS BELOW;[05] CORRECTIVE ACTION 3 AND 4 ENTRY BY ERROR <BR><BR>THE CORRECTED IS:PERFORMED VISUAL AND TAP TEST INSPECTION ON REPORTED AREA AND ONLY FOUND DEBONDED FLANGE ON DISTRIBUTION BAY MIX MANIFOLD IAW B737 NDT 51-05-01. BONDED FLANGE ON DISTRIBUTION BAY MIX MANIFOLD IAW DWG 65C28007. AND BAC5010. SEE INDIVIDUAL SIGNOFFS BELOW;[06] TASK COMPLETED.

Part: NONE — CRACKED (VERTICAL STAB) · airframe 52,234 hrs · 31,391 cycles

CRACK ACCESS PANEL 321A RIB 8 ON INTERNAL AREA FWD POSITION AT VERTICAL STABILIZER 2022-466985 / [01] REPLACED RIB 8 LOC ACCES PANEL 321A INTERNAL AREA FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02;[02] REPLACED RIB 8 LOC ACCES PANEL 321A INTERNAL AREA FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02

Part: VAPOR BARRIER — CRACKED (WHEEL WELL) · airframe 52,234 hrs · 31,391 cycles

CUSTOMER REQUEST CRACK ON VAPOR BARRIER LOCATED LBL 40 AT BS 663.75 MAIN WHEEL WELL 2022-466986 / [01] TOOL USED. CALIPER P/N:500-197-30. S/N:A18135097. DUE DATE:12/FEB/23;[02] TOOL USED: HOT BONDER P/N HCS9200B-AV S/N: 18196126 DUE DATE: 24 FEB 23.;[03] TOOL USED: SCALE P/N 91847 S/N AE-409316 DUE DATE 06 JUN 23.;[04] REPAIRED VAPOR BARRIER LOCATED LBL 40 AT BS 663.75 MAIN WHEEL WELL IAW B737-700 SRM 57-10-10-1A-2 PARAGRAPH 2.C.(4)(B). THIS IS AN INTERIM REPAIR AND REQUIRES A DETAILED VISUAL INSPECTION ON THE REPAIRED AREA AT 1;200 FLIGHT CYCLES INTERVALS OR MORE FREQUENTLY IAW B737-700 SRM 57-10-10-1A-2 PARAGRAPH 2.C.(4)(B)6) AND 7). SEE INDIVIDUAL SIGNOFFS BELOW.;[05] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2022-466984 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189520;DUE DATE:03-DEC-22.;[02] REPAIRED BY WELDING FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975 ; SEE INDIVIDUAL SIGNOFFS BELOW;[03] JOB TASK COMPLETED.

Part: VAPOR BARRIER — CRACKED (CENTER WING) · airframe 52,234 hrs · 31,391 cycles

CUSTOMER REQUEST CRACK ON VAPOR BARRIER LOCATED LBL 40 AT BS 663.75 MAIN WHEEL WELL 2022-466986 / [01] TOOL USED. CALIPER P/N:500-197-30. S/N:A18135097. DUE DATE:12/FEB/23;[02] TOOL USED: HOT BONDER P/N HCS9200B-AV S/N: 18196126 DUE DATE: 24 FEB 23.;[03] TOOL USED: SCALE P/N 91847 S/N AE-409316 DUE DATE 06 JUN 23.;[04] REPAIRED VAPOR BARRIER LOCATED LBL 40 AT BS 663.75 MAIN WHEEL WELL IAW B737-700 SRM 57-10-10-1A-2 PARAGRAPH 2.C.(4)(B). THIS IS AN INTERIM REPAIR AND REQUIRES A DETAILED VISUAL INSPECTION ON THE REPAIRED AREA AT 1;200 FLIGHT CYCLES INTERVALS OR MORE FREQUENTLY IAW B737-700 SRM 57-10-10-1A-2 PARAGRAPH 2.C.(4)(B)6) AND 7). SEE INDIVIDUAL SIGNOFFS BELOW.;[05] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: NONE — CRACKED (VERT. STAB.) · airframe 52,234 hrs · 31,391 cycles

CRACK ACCESS PANEL 321A RIB 8 ON INTERNAL AREA FWD POSITION AT VERTICAL STABILIZER 2022-466985 / [01] REPLACED RIB 8 LOC ACCES PANEL 321A INTERNAL AREA FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02;[02] REPLACED RIB 8 LOC ACCES PANEL 321A INTERNAL AREA FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02

Part: ANGLE — BROKEN (CABIN FLOOR) · airframe 52,234 hrs · 31,391 cycles

BROKEN ANGLE LOCATED BS693 AT LEVEL BL0 AT PASSENGER CABIN 2022-466947 / [01] REPLACED ANGLE LOCATED BS693 AT LEVEL BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV A. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SUPPORT ANGLE — BROKEN (CABIN FLOOR) · airframe 52,234 hrs · 31,391 cycles

BROKEN SUPPORT ANGLE LOCATED BS540 AT LEVEL RBL24.75 TO RBL45.50 AT PASSENGER CABIN 2022-466946 / [01] REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL RBL24.75 TO RBL45.50 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] STEP 1 CORRECTED <BR>REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL RBL24.75 TO RBL45.50 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A0060; SHEET 46; REV-<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL RBL24.75 TO RBL45.50 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A0060; SHEET 46; REV-; RII SEE INDIVIDUAL SIGN OFFS BELOW.

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK STRINGER 19R GUSSET AND LOCATED AT LEVEL OF BS500D AT FWD CARGO COMPARTMENT 2022-466956 / [01] REPLACED GUSSET LOCATED STRINGER 19R AT LEVEL OF BS500D AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902; SHEET 21; REV E.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED GUSSET LOCATED STRINGER 19R AT LEVEL OF BS500D AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902; SHEET 21; REV E. <BR>SEE INDIVIDUAL SIGNS-OFF BELOW.<BR>RII

Part: ANGLE — BROKEN (CENTER WING BOX) · airframe 52,234 hrs · 31,391 cycles

BROKEN SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO RBL24.75 AT PASSENGER CABIN 2022-466945 / [01] REPLACED SUPPORT ANGLE SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] STEP 1 CORRECTED.<BR>REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] STEP 2 CORRECTED. <BR>REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS540 AT LEVEL BL0 TO RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A0060 SHEET 46; REV- <BR>SEE INDIVIDUAL SIGN OFFS BELOW;[04] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS540 AT LEVEL BL0 TO RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A0060 SHEET 46; REV-; RII SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — BROKEN (CENTER WING BOX) · airframe 52,234 hrs · 31,391 cycles

BROKEN SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO LBL24.75 AT PASSENGER CABIN 2022-466943 / [01] REPLACED SUPPORT ANGLE SUPPORT ANGLE SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO LBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] STEP 1 CORRECTED.<BR>REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO LBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] STEP 2 CORRECTED. <BR>REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO LBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A0060 SHEET 46; REV - <BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[04] REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO LBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A0060 SHEET 46; REV - RII ACCOMPLISHED SEE INDIVIDUAL SIGN OFFS BELOW.

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK STRINGER 19R GUSSET AND LOCATED AT LEVEL OF BS500D AT FWD CARGO COMPARTMENT 2022-466956 / [01] REPLACED GUSSET LOCATED STRINGER 19R AT LEVEL OF BS500D AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902; SHEET 21; REV E.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED GUSSET LOCATED STRINGER 19R AT LEVEL OF BS500D AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902; SHEET 21; REV E. <BR>SEE INDIVIDUAL SIGNS-OFF BELOW.<BR>RII

Part: BRACKET — CRACKED (FWD CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK BRACKET AT LEVEL OF STRINGER 28R AND BS 500D AT FWD CARGO COMPARTMENT 2022-466967 / [01] TOOL USED DIGITAL CALIPER P/N:500-752-20; S/N:B16101278; DUE DATE:26-OCT-22<BR><BR>GAUGE RADIUS P/N: 2204A3; S/N:AE-408656; DUA DATE:29-JAN-23;[02] REPLACED BRACKET AT LEVEL OF STRINGER 28R AND BS 500D AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7810; SHEET 7 ; REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED BRACKET AT LEVEL OF STRINGER 28R AND BS 500D AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7810; SHEET 7 ; REV -. SEE INDIVIDUAL SIGN OFFS BELOW.<BR>RII

Part: ANGLE — BROKEN (FUSELAGE) · airframe 52,234 hrs · 31,391 cycles

BROKEN SUPPORT ANGLE LOCATED BS540 AT LEVEL RBL24.75 TO RBL45.50 AT PASSENGER CABIN 2022-466946 / [01] REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL RBL24.75 TO RBL45.50 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] STEP 1 CORRECTED <BR>REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL RBL24.75 TO RBL45.50 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A0060; SHEET 46; REV-<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL RBL24.75 TO RBL45.50 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A0060; SHEET 46; REV-; RII SEE INDIVIDUAL SIGN OFFS BELOW.

Part: BRACKET — CRACKED (FWD CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK BRACKET AT LEVEL OF STRINGER 28R AND BS 500D AT FWD CARGO COMPARTMENT 2022-466967 / [01] TOOL USED DIGITAL CALIPER P/N:500-752-20; S/N:B16101278; DUE DATE:26-OCT-22<BR><BR>GAUGE RADIUS P/N: 2204A3; S/N:AE-408656; DUA DATE:29-JAN-23;[02] REPLACED BRACKET AT LEVEL OF STRINGER 28R AND BS 500D AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7810; SHEET 7 ; REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED BRACKET AT LEVEL OF STRINGER 28R AND BS 500D AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7810; SHEET 7 ; REV -. SEE INDIVIDUAL SIGN OFFS BELOW.<BR>RII

Part: SUPPORT ANGLE — BROKEN · airframe 52,234 hrs · 31,391 cycles

BROKEN SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO LBL24.75 AT PASSENGER CABIN 2022-466943 / [01] REPLACED SUPPORT ANGLE SUPPORT ANGLE SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO LBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] STEP 1 CORRECTED.<BR>REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO LBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] STEP 2 CORRECTED. <BR>REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO LBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A0060 SHEET 46; REV - <BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[04] REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO LBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A0060 SHEET 46; REV - RII ACCOMPLISHED SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SUPPORT ANGLE — BROKEN (CABIN FLOOR) · airframe 52,234 hrs · 31,391 cycles

BROKEN SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO RBL24.75 AT PASSENGER CABIN 2022-466945 / [01] REPLACED SUPPORT ANGLE SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] STEP 1 CORRECTED.<BR>REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] STEP 2 CORRECTED. <BR>REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS540 AT LEVEL BL0 TO RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A0060 SHEET 46; REV- <BR>SEE INDIVIDUAL SIGN OFFS BELOW;[04] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS540 AT LEVEL BL0 TO RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A0060 SHEET 46; REV-; RII SEE INDIVIDUAL SIGN OFFS BELOW

Part: BRACKET — CRACKED (FWD CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK BRACKET LOCATED AT LEVEL OF BS 500D AND STRINGER 28L AT FWD CARGO COMPARTMENT 2022-466966 / [01] TOOL USED DIGITAL CALIPER P/N:500-752-20; S/N:B16101278; DUE DATE:26-OCT-22<BR><BR>GAUGE RADIUS P/N: 2204A3; S/N:AE-408656; DUA DATE:29-JAN-23;[02] REPLACED BRACKET LOCATED AT LEVEL OF BS 500D AND STRINGER 28L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7810; SHEET 7 ; REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED BRACKET LOCATED AT LEVEL OF BS 500D AND STRINGER 28L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7810; SHEET 7 ; REV -. SEE INDIVIDUAL SIGN OFFS BELOW.<BR>RII

Part: BRACKET — CRACKED (FWD CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK BRACKET LOCATED AT LEVEL OF BS 500D AND STRINGER 28L AT FWD CARGO COMPARTMENT 2022-466966 / [01] TOOL USED DIGITAL CALIPER P/N:500-752-20; S/N:B16101278; DUE DATE:26-OCT-22<BR><BR>GAUGE RADIUS P/N: 2204A3; S/N:AE-408656; DUA DATE:29-JAN-23;[02] REPLACED BRACKET LOCATED AT LEVEL OF BS 500D AND STRINGER 28L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7810; SHEET 7 ; REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED BRACKET LOCATED AT LEVEL OF BS 500D AND STRINGER 28L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7810; SHEET 7 ; REV -. SEE INDIVIDUAL SIGN OFFS BELOW.<BR>RII

Part: ANGLE — BROKEN (CABIN FLOOR) · airframe 52,234 hrs · 31,391 cycles

BROKEN ANGLE LOCATED BS693 AT LEVEL BL0 AT PASSENGER CABIN 2022-466947 / [01] REPLACED ANGLE LOCATED BS693 AT LEVEL BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV A. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: CHANNEL — CORRODED (FWD CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CORROSION CHANNEL SIDEPLATE LOCATED FROM BS492 TO BS500A AND AT LEVEL OF STRINGER 26RT AT FWD CARGO COMPARTMENT 2022-466961 / [01] REPLACED CHANNEL SIDEPLATE AND FASTENERS LOCATED FROM BS492 TO BS500A AND AT LEVEL OF STRINGER 26RT AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; DWG 143A0080 SHEET 23 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED CHANNEL SIDEPLATE AND FASTENERS LOCATED FROM BS492 TO BS500A AND AT LEVEL OF STRINGER 26RT AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; DWG 143A0080 SHEET 23 REV - RII <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 52,234 hrs · 31,391 cycles

CRACK GUSSET LOC BS 500D AND STR 19L FWD CARGO COMPARTMENT 2022-466858 / [01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D AND STR 19L FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A7902 SHEET 21; REV ?E?.<BR>SEE INDIVIDUAL SING-OFFS BELOW;[02] REPLACED GUSSET AND FASTENERS LOCATED BS 500D AND STR 19L FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING #143A7902 SHEET 21; REV ?E?. <BR>SEE INDIVIDUAL SING-OFFS BELOW<BR>RII

Part: NONE — CRACKED (FWD SERVICE DOOR) · airframe 52,234 hrs · 31,391 cycles

CRACK INDICATION FOUND ON FORWARD SERVICE DOOR BEAM 5 AT LEVEL OF HANDLE PASSENGER CABIN 2022-466846 / [01] REPLACED BEAM LOCATED AT FWD SERVICE DOOR AT LEVEL OF HANDLE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A6516 REV:- (BEAM 5);[02] CORRECTIVE ACTION 1 CORRECTED: REPLACED BEAM LOCATED AT FWD SERVICE DOOR AT LEVEL OF HANDLE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A6516 REV:- (BEAM 5)<BR>SEE INDIVIDUAL SIGNS OFF BELOW;[03] CORRECTED 1 REPLACED BEAM LOCATED AT FWD SERVICE DOOR AT LEVEL OF HANDLE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A6516 REV:- (BEAM 5) . RII .SEE INDIVIDUAL SIGNS OFF BELOW.

Part: BEAM — CRACKED (R1 DOOR) · airframe 52,234 hrs · 31,391 cycles

CRACK INDICATION FOUND ON FORWARD SERVICE DOOR BEAM 5 AT LEVEL OF HANDLE PASSENGER CABIN 2022-466846 / DRILLED NEW BEAM I.A.W B737-700 SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT ON OPEN HOLES AND HOLES ON AREA LOC. FWD SERVICE DOOR AT LEVEL OF HANDLE I.A.W B737-700 SRM 51-20-01. RII INSTALLED BEAM LOCATED AT FWD SERVICE DOOR AT LEVEL OF HANDLE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A6516 REV:- (BEAM 5)

Part: BEAM — CRACKED (R1 DOOR) · airframe 52,234 hrs · 31,391 cycles

CRACK INDICATION FOUND ON FORWARD SERVICE DOOR BEAM 4 AT LEVEL OF HANDLE PASSENGER CABIN 2022-466845 / DRILLED NEW BEAM I.A.W B737-700 SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT ON OPEN HOLES AND HOLES ON AREA LOC. FWD SERVICE DOOR AT LEVEL OF HANDLE I.A.W B737-700 SRM 51-20-01. INSTALLED BEAM ,STOP PIN AND STIFFENER LOCATED AT FWD SERVICE DOOR. IAW B737-700 SRM 51-40-02. AND DWG 141A6535 REV:C (BEAM 4)

Part: NONE — CRACKED (FWD SERVICE DOOR) · airframe 52,234 hrs · 31,391 cycles

CRACK INDICATION FOUND ON FORWARD SERVICE DOOR BEAM 4 AT LEVEL OF HANDLE PASSENGER CABIN 2022-466845 / [01] REPLACED BEAM LOCATED AT FWD SERVICE DOOR. IAW B737-700 SRM 51-40-02. AND DWG 141A6535 REV:C (BEAM 4).;[02] CORRECTIVE ACTION 1 CORRECTED: REPLACED BEAM LOCATED AT FWD SERVICE DOOR. IAW B737-700 SRM 51-40-02. AND DWG 141A6535 REV:C (BEAM 4).<BR>SEE INDIVIDUAL SIGNS OFF BELOW;[03] CORRECTED 1 : REPLACED BEAM LOCATED AT FWD SERVICE DOOR. IAW B737-700 SRM 51-40-02. AND DWG 141A6535 REV:C (BEAM 4). RII .SEE INDIVIDUAL SIGNS OFF BELOW.

Part: NONE — CRACKED (RH HOR STAB) · airframe 52,234 hrs · 31,391 cycles

CRACK INSPAR RIB 120.30 AT 28 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2022-466792 / PERFORMED PERMANENT REPAIR ON INSPAR RIB 120.30 AT 28 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 AND SRM 51-40-02. T-SECTION MATERIAL USED KIT 55100003-01; ANGLE MATERIAL USED BAC1490-2738 P.O: 2021227850;FILLER MATERIAL USED 7075-T6 0.050? P.O: 2012531826 AND SHIM (2 E/A) MATERIAL USED 7075-T6 0.020? P.O:2021142563. CRACK LENGTH IS: 0.280 INCHES; TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N:B16152123; DUE DATE: 09-APR-23.;[05] CORRECTED CORRECTIVE ACTION. <BR>PERFORMED PERMANENT REPAIR ON INSPAR RIB 120.30 AT 28 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. MATERIAL USED: T-SECTION MATERIAL USED KIT 55100003-01; ANGLE MATERIAL USED BAC1490-2738 P.O: 2021227850;FILLER MATERIAL USED 7075-T6 0.050? P.O: 2012531826 AND SHIM (2 E/A) MATERIAL USED 7075-T6 0.020? P.O:2021142563. CRACK LENGTH IS: 0.280 INCHES; TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N:B16152123; DUE DATE: 09-APR-23.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[06] PERFORMED PERMANENT REPAIR ON INSPAR RIB 120.30 AT 28 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5.

Part: NONE — CRACKED (RH HOR STAB) · airframe 52,234 hrs · 31,391 cycles

CRACK INSPAR RIB 120.30 AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2022-466793 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138503; CAL DUE DATE: 19-MAY-23;[02] TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N:B16152123; DUE DATE: 09-APR-23 AND PRECISION RADIUS GAUGE P/N:2204A3; S/N:AE-408652; DUE DATE: 29-JAN-23.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138503; CAL DUE DATE: 19-MAY-23;[04] PERFORMED PERMANENT REPAIR ON INSPAR RIB 120.30 AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. MATERIAL USED: KIT T-SECTION P/N:55100003-01. CRACK LENGTH IS: 0.280 INCHES. TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N:B16152123; DUE DATE: 09-APR-23. <BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[05] PERFORMED PERMANENT REPAIR ON INSPAR RIB 120.30 AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. MATERIAL USED: KIT T-SECTION P/N:55100003-01. CRACK LENGTH IS: 0.280 INCHES. TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N:B16152123; DUE DATE: 09-APR-23. <BR>SEE INDIVIDUAL SIGN OFFS BELOW.<BR>RII

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 52,234 hrs · 31,391 cycles

CRACK INSPAR RIB 120.30 AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2022-466793 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138503; CAL DUE DATE: 19-MAY-23;[02] TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N:B16152123; DUE DATE: 09-APR-23 AND PRECISION RADIUS GAUGE P/N:2204A3; S/N:AE-408652; DUE DATE: 29-JAN-23.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138503; CAL DUE DATE: 19-MAY-23;[04] PERFORMED PERMANENT REPAIR ON INSPAR RIB 120.30 AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. MATERIAL USED: KIT T-SECTION P/N:55100003-01. CRACK LENGTH IS: 0.280 INCHES. TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N:B16152123; DUE DATE: 09-APR-23. <BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[05] PERFORMED PERMANENT REPAIR ON INSPAR RIB 120.30 AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. MATERIAL USED: KIT T-SECTION P/N:55100003-01. CRACK LENGTH IS: 0.280 INCHES. TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N:B16152123; DUE DATE: 09-APR-23. <BR>SEE INDIVIDUAL SIGN OFFS BELOW.<BR>RII

Part: SKIN PANEL — CRACKED (RH HOR STAB) · airframe 52,234 hrs · 31,391 cycles

CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 AND 16 INCH. FROM FRONT SPAR. CRACK LENGTH = 1.100 INCH. APPROX. 2022-466843 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] PERFORMED REPAIR ON LT HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STAB STA 193.9 IAW B737-700 SRM SRM 55-10-01-2R-11 REPAIR 11.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[03] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 52,234 hrs · 31,391 cycles

CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 AND 16 INCH. FROM FRONT SPAR. CRACK LENGTH = 1.100 INCH. APPROX. 2022-466843 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] PERFORMED REPAIR ON LT HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STAB STA 193.9 IAW B737-700 SRM SRM 55-10-01-2R-11 REPAIR 11.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[03] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: NONE — CRACKED (R/H WING) · airframe 52,234 hrs · 31,391 cycles

CRACK EXTERNAL SKIN SLAT 8 LOCATED ON THE WING LEADING EDGE SLAT NOSE SKIN AT THE ACTUATOR RIB ON THE SKIN AROUND THE FASTENERS THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 451.97. AT RT WING 2022-466700 / [01] TOOL USED. EDDY CURRENT EQUIPMENT. P/N: NORTEC 500D. S/N: N500X11290U021704. DUE DATE: 01-FEB-23.;[02] TOOL USED DIGITAL CALIPER P/N: 500-752-20; S/N:B16101278; DUE DATE:26/OCT/22;[03] PERFORMED PERMANENT REPAIR PARTS DOUBLER AND FILLER AND FASTENERS LOC. RT WING SLAT 8 NOSE SKIN ATTACH ACTUATOR FITTING SLAT STATION 451.97 IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; FIGURE 202; SHEET 1 ALTERNATIVE 1; MATERIAL USED: ALUMINUM SHEET 7075-T6 0.071? P/O: 2021-203793; ALUMINUM SHEET 7075-T6 0.063? P/O 2021-152041.<BR>SEE INDIVIDUAL SIGNOFFS BELOW.;[04] PERFORMED PERMANENT REPAIR PARTS DOUBLER AND FILLER AND FASTENERS LOC. RT WING SLAT 8 NOSE SKIN ATTACH ACTUATOR FITTING SLAT STATION 451.97 IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; FIGURE 202; SHEET 1 ALTERNATIVE 1; MATERIAL USED: ALUMINUM SHEET 7075-T6 0.071? P/O: 2021-203793; ALUMINUM SHEET 7075-T6 0.063? P/O 2021-152041. RII .SEE INDIVIDUAL SIGNOFFS BELOW.

Part: NONE — OUT OF POSITION (FWD ENTRY DOOR) · airframe 52,156 hrs · 31,339 cycles

FORWARD ENTRY DOOR EXIT SIGN COVER CAME OFF / [01] R&R FWD ENTRY DOOR EXIT SIGN LIGHT ASSY. PER A.M.M. 33-51-01.

Part: STRAP — LOOSE (L/H OVERWING EXI) · airframe 50,998 hrs · 30,609 cycles

F/A FOUND THE OVERWING EXIT ESCAPE STRAP HOUSING(BOTH LEFT AND RIGHT) NEEDS TO BE SECURED TO THE OVERWING EXIT DOOR / [01] INSTALLED MISSING HARDWARE AND SECURED BOTH LEFT AND RIGHT OVERWING EXIT ESCAPE STRAP HOUSINGS PER SOPM 20-50-01.

Part: STRAP — LOOSE (R/H OVERWING EXI) · airframe 50,998 hrs · 30,609 cycles

F/A FOUND THE OVERWING EXIT ESCAPE STRAP HOUSING(BOTH LEFT AND RIGHT) NEEDS TO BE SECURED TO THE OVERWING EXIT DOOR / [01] INSTALLED MISSING HARDWARE AND SECURED BOTH LEFT AND RIGHT OVERWING EXIT ESCAPE STRAP HOUSINGS PER SOPM 20-50-01.

Part: OIL SYSTEM — LEAKING (#1 ENGINE) · airframe 49,311 hrs · 29,571 cycles

PASSENGER REPORTED FLAMES COMING FROM NUMBER #1 ENGINE JUST BEFORE TAKEOFF. WE CLEARED THE RUNWAY AND CALLED FOR CFR. CFR REPORTED NO DAMAGE FROM THE SHUT (#1) DOWN ENGINE. NO ABNORMAL ENGINE INDICATIONS. CFR REPORTED NO DAMAGE FROM THE SHUT DOWN ENGINE. TAXIED BACK TO GATE SINGLE ENGINE. NO ABNORMAL ENGINE INDICATIONS. PERFORMED FIM 71-05 TASK811, PARAGRAPH C1 AND D1 THRU 4. PERFORMED ENG VENT AND DRAIN INSPECTION IAW AMM 71-71-00 PARAGRAPH 2G8. DUE TO HISTORY OF OIL PUDDLING IN TAIL PIPE, PP ENGINEERING WILL SCHEDULE AFT SUMP REPACK AND CENTER VENT TUBE CLEANING.

Part: BRACKET — BROKEN (EMERGENCY LIGHT) · airframe 49,194 hrs · 29,498 cycles

OVERWING EXIT OVERHEAD LIGHT MOUNTING BRACKET BROKEN ; / [01] R&R OVERWING EXIT OVERHEAD LIGHT MOUNTING BRACKET IAW 33-51-01. OP CHECK GOOD.

Part: HOUSING — LOOSE (DOOR HANDLE) · airframe 48,618 hrs · 29,139 cycles

EMERGENCY PULL HANDLE HOUSING HAS SCREW MIGRATING OUT @ 11CB. RESECURED HANDLE HOUSING REF AMM 25-21-20.

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR) · airframe 46,964 hrs · 28,192 cycles

CUSTOMER WALK L2 DOOR GIRT BAR HITTING SCUFF PLATE. READJUSTED GIRT Z-FOLD IN RF WORK CARD 725-61-06.

Part: BARRIER — CRACKED (FUSELAGE) · airframe 46,964 hrs · 28,192 cycles

CUSTOMER WORK REQUEST ; LEFT HAND STA. 663 VAPOR BARRIER WEB IS CRACKED AT APROX. LBL 40 / CLEANED DAMAGE L/H VAPOR BARRIER AT STA 663 FOR REPAIR. LBL 401; STOP DRILL CRACK; PERFORMED DRY OUT FOUND NO WATER. AND REPAIRED DAMAGE AREA. SIZE 10'' CRACK AS PER. B737 SRM 51-70-04-2R-10. REPAIR/A PRIME & TOP COAT BOTH SIDES OF VAPOR BARRIER. AS PER B737 AMM 51-21-72-370-804 & AMM 51-21-81-370-802 MATERIAL USED PO# 1691708; PO# 1480720; PO# 1661878; PO# 1686125

Part: BULKHEAD WEB — CRACKED (FUSELAGE) · airframe 46,964 hrs · 28,192 cycles

CUSTOMER REQUEST RIGHT HAND STA 663 VAPOR BARRIER WEB IS CRACKED AT APPROXIMATELY RBL40. CLEANED DAMAGE RT VAPPOR BARRIER FOR REPAIR, AS MARKED. PERFORMED DRY-OUT NO WATER FOUND, STOP DRILL CRACK. INSTALLED REPAIR ON RT VAPOR BARRIER, AS PER B737 SRM 51-70-04-2R-10 REPAIR 10. MATERIAL USED P/O 1691708 & P/O 1480720.

Part: FAIRING — DELAMINATED (WING TO BODY) · airframe 46,964 hrs · 28,192 cycles

WING TO BODY PANEL ON RACK 192BL FWD CORNER HAS DELAMANATION / REPAIRED DAMAGED AREA AT WING TO BODY FAIRING PANEL 192BL REF B737-7 SRM 53-40-70-2R-1 MATERIAL USED: PO#: 1691708

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 46,964 hrs · 28,192 cycles

FLIGHT DECK FLOOR WEB DENTED AT STA 260. EVALUATED DENTED AREA AT FLIGHT DECK FLOOR WEB STA 260 AND FOUND OF OUT OF LIMITS, PER B737-700 SRM 53-10-51-1A-1. ACCOMPLISHED PERMANENT REPAIR ON FLOOR WEB STA 260 BETWEEN LBL 20 AND RBL 5, PER EA 1-A53-33179 REV 1 FIG 1.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 46,964 hrs · 28,192 cycles

LT HORIZONTAL STAB INSPAR RIB ASSEMBLY STA 129.50 NR 5 2ND STIFFNER LOWER AREA CRACKED. REPAIRED STIFFENER NR 2 AT LEFT HORIZONTAL STA INSPAR RIB ASSEMBLY STA 129.50 NR 5, AS PER REF B737-700 SRM 55-10-09-2R-4.

Part: BRACKET — LOOSE (R1 DOOR GIRT BAR) · airframe 44,341 hrs · 26,549 cycles

R1 DOOR SLIDE AFT RETAINING BRACKET FOR GIRT BAR LOOSE AND GIRT BAR POPPED OUT. / SECURED AFT CLIP PER SIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,497 hrs · 25,331 cycles

L2 DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. RELAMPED PER AMM 33-51-04

Part: SLIDE — TORN (R2 DOOR) · airframe 42,409 hrs · 25,274 cycles

R2 DOOR SLIDE GIRT PROTECTIVE COVER TORN. R&R SLIDE IAW MT.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 42,244 hrs · 25,167 cycles

193B PANEL ON LOWER SURFACE HAS A 1/2 INCH PUNCTURE WITH DELAM 1/2' IN DIAMETER. 7' FROM L/E OF PANEL 18' FROM T/E OF PANEL JUST L/H SIDE OF CENTER LINE OF PANEL. MOD / R/R CENTER WING TO BODY PANEL 193B IAW AMM 53-51-21.

Part: BRACKET — BROKEN (E&E DOOR) · airframe 41,661 hrs · 24,784 cycles

FORWARD E&E DOOR FORWARD BRACKET BROKEN. R&R BRACKET IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,329 hrs · 24,558 cycles

RT OVERWING ESCAPE GROUND ILLUMINATION LAMP INOP. R&R LAMP PER AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, STR 28L. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

FLOOR SUPPORT CRACKED AT BS 540, BETWEEN BL 0 TO RBL 25. R&R SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

FLOOR SUPPORT CRACKED AT BS 540, BETWEEN BL 0 TO LBL 25. R&R SUPPORT IAW SRM AND DWG.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO BAY WATER TANK GROUNDING BRACKET CORRODED AT BS 947, LBL 6. R&R BRACKET PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FWD FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

***CORROSION*** FWD SIDE 967 FRAME WEB I/B OF INTERCOSTAL AT STR 26L (MARKED) / FWD SIDE OF BS 967 FRAME AT STR 26L WAS REPAIRED PER: EA 1-753-33626 REV IR AND ATS ER 18-05289 REV IR

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 492 TO BS 500A. R&R SHIELD PER DWG & SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

STRINGER CLIP CORRODED AT BS 947.5, STR 26R. R&R CLIP PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

FRAME WEB CORRODED AT BS 947.5, BETWEEN STR 27L TO STR 25R. R&R FRAME PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D. R&R SUPPORT PER SRM.

Part: SPLICE — CORRODED (AFT CARGO) · airframe 41,329 hrs · 24,558 cycles

***CORROSION*** IN MULTIPLE AREAS ON ACB FLOOR SUPPORT T SPLICE LOCATED AT STA 767+4 / RECEIVED NEW SERVICEABLE ACB FLOOR SPLICE FOR BS 767+4. FOR TRACKING ONLY. RECEIVED ON SWA P.O. 715112

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO FLOOR STRUCTURE, NUT PLATE STRIP CORRODED BETWEEN BS 787 TO BS 793, RBL 20. R&R STRAP PER SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO FORWARD SHIELD FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 793, RBL 22. R&R SHIELD PER SRM & DWG.

Part: FRAME — CORRODED (AFT CARGO) · airframe 41,329 hrs · 24,558 cycles

***CORROSION*** ON TOP OF ACB FRAME STA 947 STR 24R / REMOVED CORROSION - OUT OF LIMITS - DUE TO DAMAGE OVER FASTENER HOLES. LOWEST READING IS 0.037' OUT OF .063' ORIGINAL THICKNESS OF 1' X 3' AREA ON TOP AND AFT SIDE OF ACB FRAME STA.947 STR 24R PER SRM 53-00-07-1A-1. WORK TO BE COMPLETED ON SWA CARD NUMBER T851676.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO BAY FLOOR TRACK AT CORRODED AT BS 787+9, RBL 15. R&R FLOOR TRACK PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 887 TO BS 947, RBL 22. R&R SUPPORT PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 22. R&R SUPPORT PER SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

FORWARD CARGO BAY AFT BULKHEAD GUSSET AT BS 500D, STR 19L. R&R GUSSET PER SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 787+7, RBL 18.5. R&R STRAP PER SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO FLOOR STRUCTURE STRAP CORRODED BETWEEN BS 774.5 TO BS 872.5, RBL 20. R&R STRAP PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT CORRODED AT BS 947, BETWEEN RBL 21 TO LBL 10. R&R SUPPORT PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO FLOOR STRUCTURE INTERCOSTAL UPPER ANGLE CORRODED, BETWEEN BS 767 TO BS 787, RBL 21. R&R ANGLE PER SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO DOOR SURROUND STRUCTURE LOWER SILL WEB CORRODED. R&R WEB PER DWG AND SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

FORWARD CARGO INTERCOSTAL ATTACH ANGLE CRACKED AT BS 400, STR 26L. R&R CLIP PER DWG & SRM.

Part: SPLICE — CORRODED (AFT CARGO BAY) · airframe 41,329 hrs · 24,558 cycles

***CORROSION*** IN MULTIPLE AREAS ON ACB FLOOR SUPPORT T SPLICE LOCATED AT STA 727D+7 / RECEIVED NEW SERVICEABLE ACB FLOOR T SPLICE FOR BS 727D+7. FOR TRACKING ONLY. RECEIVED ON SWA P.O. 709587

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED. R&R WEB PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO BAY UNDER FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 927+18, RBL 22. R&R INTERCOSTAL PER SRM AND DWG.

Part: STRIP — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO FLOOR STRUCTURE, NUT PLATE STRIP CORRODED BETWEEN BS 795 TO BS 803, RBL 20. R&R STRIP PER SRM & DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO BAY FLOOR SUPPORT T SPLICE CORRODED AT BS 887. R&R "T" SPLICE PER SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

FORWARD CARGO BAY AFT BULKHEAD GUSSET AT BS 500D-2, STR 19R. R&R GUSSET PER SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

AFT CARGO AFT SHIELD/ FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 TO BS 867, RBL 21. R&R SHIELD PER SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

FORWARD CARGO INTERCOSTAL ATTACH ANGLE CRACKED AT BS 440, STR 26L. R&R CLIP PER DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

INTERCOSTAL CRACKED AT BS 348, RBL 32. R&R INTERCOSTAL IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

RT CREASE BEAM CORRODED BETWEEN BS 616 TO BS 639, WL 208. R&R CREASE BEAM IAW SRM AND AMM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

R1 DOOR THRESHOLD ATTACH ANGLE CORRODED BETWEEN BS 305 TO BS 328, RBL 55. R&R ANGLE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, LBL1. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, LBL 14. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, LBL 1. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, RBL 40. R&R INTERCOSTAL PER SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

R1 DOOR MOPSILL VERTICAL FLANGE CORRODED AT BS 328, RBL 55. R&R MOPSILL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, RBL 9. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

FWD PASSENGER CABIN FLOOR PANEL 221GF FWD O/B CORNER IS BROKEN / DUE TO THE EXTENT OF DAMAGE TO THE FWD O/B CORNER; REPLACED FWD PASESNGER CABIN FLOOR PANEL 221GF WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-50D ITEM 295. 57066U 10/30/18

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

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

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

L1 DOOR MOPSILL ON VERTICAL FLANGE CRACKED AT BS 303, LBL 55. R&R MOPSILL IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

STRAP CORRODED AT BS 1026, LBL 3. R&R STRAP PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,329 hrs · 24,558 cycles

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

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 41,329 hrs · 24,558 cycles

SUPPLEMENTAL INFORMATION: RUDDER COUNTER WEIGHT HAS CORROSION / REMOVED AND REPLACED RUDDER COUNTER WEIGHT IAW CMM 55-40-09 STEP 2.C.(2) PG 301 AND 302 AND CMM 55-40-09 STEP 2.C.(3) PG. 703.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,329 hrs · 24,558 cycles

LT HORIZONTAL STAB LEADING EDGE 4TH RIB FROM INBOARD END STA 105.26 CRACKED. R&R RIB PER SRM AND DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,329 hrs · 24,558 cycles

LT HORIZONTAL STAB LEADING EDGE 5TH RIB FROM INBOARD END STA 114.55 CRACKED. R&R RIB PER SRM AND DWG.

Part: RIB — CORRODED (LEFT WING) · airframe 41,329 hrs · 24,558 cycles

***CORROSION*** LT WING TIP RIB 27 O/B SURFACE (WINGLET MOUNTING) AT FWD LWR MOUNTING BOLT HOLE / REPAIRED LT WING TIP RIB 27 OB SURFACE AT FWD LWR MOUNTING HOLE IAW ER 18-05119 REV IR AND EA 1-757-15708 REV IR

Part: RIB — CORRODED (LEFT WING) · airframe 41,329 hrs · 24,558 cycles

***CORROSION*** LT WING TIP RIB 27 O/B SURFACE (WINGLET MOUNTING) AT 1' AFT OF AFT UPR MOUNTING BOLT HOLE / REPAIRED LT WING TIP RIB 27 OB SURFACE AT 1' AFT OF AFT UPR MOUNTING HOLE IAW ER 18-05119 REV IR AND EA 1-757-15708 REV IR

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,329 hrs · 24,558 cycles

LT HORIZONTAL STABILIZER RIB AT STAB STA 120.30 CRACKED AT 2ND STIFFENER. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,329 hrs · 24,558 cycles

LT HORIZONTAL STABILIZER RIB AT STAB STA 120.30 CRACKED AT 4TH STIFFENER. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,329 hrs · 24,558 cycles

LT HORIZONTAL STABILIZER RIB AT STAB STA 120.30 CRACKED AT 3RD STIFFENER. REPAIRED RIB IAW SRM.

Part: MOUNT — CORRODED (LEFT WING) · airframe 41,329 hrs · 24,558 cycles

***CORROSION*** LT WINGLET MOUNTING SURFACE HAS MULITPLE SPOTS OF PITTING / WINGLET WAS REPAIRED AND MADE SERVICABLE ON ATS W.O. 510912 CUSTOMER PO# 0570159-B8R (POS: LT; TAG NO: 488179; P/N OFF/ON: 737-0010-335; S/N OFF/ON: NO369;)

Part: RETAINER — CRACKED (LEFT WING) · airframe 41,329 hrs · 24,558 cycles

SUPPLEMENTAL INFORMATION: L/W TRAILING EDGE SEAL RETAINER ABOVE #1 PYLON AFT TIP AT AFT SIDE OF TRANSVERSE WEB CRACKED / REMOVED AND REPLACED L/WING T/E SEAL RETAINER ABOVE #1 PYLON AFT SIDE OF TRANSVERSE WEB. IAW SRM 51-40-02-0G-0 AND SOPM 20-50-01 4036U 04NOV18

Part: RETAINER — CRACKED (RIGHT WING) · airframe 41,329 hrs · 24,558 cycles

SUPPLEMENTAL INFORMATION: R/W TRAILING EDGE BULB SEAL RETAINER CRACKED AT FWD SIDE OF TRANSVERSE WEB ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED R/WING T/E BULB SEAL RETAINER AT FWD SIDE OF TRANSVERSE WEB ABOVE #2 PYLON IAW SOPM 20-50-01 4036U 04NOV18 AND SRM 51-40-02 4036U 04NOV18

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 41,329 hrs · 24,558 cycles

VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT BS 663, LBL 10. REPAIRED ANGLE PER EA.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 41,329 hrs · 24,558 cycles

VAPOR BARRIER CRACKED AT BS 663, LBL 32. REPAIRED BARRIER IAW SRM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 41,329 hrs · 24,558 cycles

VAPOR BARRIER CRACKED AT BS 663, RBL 30. REPAIRED BARRIER IAW SRM.

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 41,329 hrs · 24,558 cycles

LAV SERVICE DOOR HAS CORROSION AT BONDING WIRE ATTACH FASTENER / CORROSION AT BONDING WIRE ATTATCH FASTENER OUT OF LIMITS; DAMAGE OVER FASTENER HOLE PER SRM 52-40-01-1A-4. REMOVED AND REPLACED LAV DOOR PER AMM 52-49-07-000-801 AND AMM 52-49-07-400-801. BONDING RESISTANCE CHECKED GOOD PER AMM 52-49-07-400-801 STEP 3.C(1)(E)(1). 57546U 19NOV18

Part: LENS — LOOSE (CABIN) · airframe 40,732 hrs · 24,164 cycles

LT EMERGENCY LIGHT LENS COVER LOOSE AT ROW 4. SECURED LENS PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,732 hrs · 24,164 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 40,732 hrs · 24,164 cycles

LT AFT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R&R BATTERY PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 39,772 hrs · 23,547 cycles

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

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 38,905 hrs · 23,016 cycles

LEFT WHEEL WELL PRESSURE BULKHEAD WEB CRACKED AT BS 663, LBL 36. REPAIRED THE BULKHEAD WEB IAW EA.

Part: ROLLER — CRACKED (R1 DOOR) · airframe 38,617 hrs · 22,809 cycles

R1 DOOR CENTERING GUIDE ROLLER CRACKED. R & R THE ROLLER IAW AMM.

Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 36,423 hrs · 21,443 cycles

LEFT MAIN LANDING GEAR FORWARD WALL BULKHEAD WEB CRACKED AT LBL 34, APPROX. 10.5" FROM BOTTOMS OF FUSELAGE. REPAIRED THE WEB IAW SRM.

Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 36,423 hrs · 21,443 cycles

LEFT MAIN LANDING GEAR FORWARD WALL BULKHEAD WEB CRACKED AT LBL 46, APPROX. 13" FROM BOTTOM OF FUSELAGE. / REPAIRED WEB PER SRM.

Part: STARTER — UNKNOWN (NR 1 ENGINE) · airframe 35,391 hrs · 20,834 cycles

DIVERSION/DECLARED EMERGENCY, NR 1 ENGINE LOW OIL QUANTITY AS LOW AS 10 % ON APPROACH OIL PRESSURE AND OIL TEMP REMAINED NORMAL. R&R NR 1 ENGINE STARTER PER AMM.

Part: STRAP — CORRODED (CABIN) · airframe 34,721 hrs · 20,438 cycles

RT OVERWING EMERGENCY ESCAPE HATCH STRAP CORRODED ON THE HOOK ASSEMBLY. R&R STRAP IAW MM.

Part: COVER — LOOSE (RT OVERWING) · airframe 34,665 hrs · 20,401 cycles

RIGHT OVERWING EMERGENCY EXIT STRAP COVER LOOSE. R & R THE COVER IAW SIP.

Part: TRUNNION — CORRODED (RT MLG) · airframe 34,540 hrs · 20,322 cycles

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

Part: TRUNNION — CORRODED (LT MLG) · airframe 34,540 hrs · 20,322 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 32,047 hrs · 18,880 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 32,047 hrs · 18,880 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1669. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 32,047 hrs · 18,880 cycles

EMERGENCY LIGHT BATTERY M1669 FAILED FUNCTIONAL TEST. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 32,047 hrs · 18,880 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1670. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 32,047 hrs · 18,880 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 32,047 hrs · 18,880 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1673. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 32,047 hrs · 18,880 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1672. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 32,047 hrs · 18,880 cycles

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

Part: COVER — MISSING (EXIT SIGN) · airframe 30,501 hrs · 17,987 cycles

LEFT EXIT SIGN LIGHT COVER MISSING AT EXIT ROW. INSTALLED COVER IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 29,617 hrs · 17,497 cycles

RIGHT OVERWING EMER EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: COVER — MISSING (EMERGENCY EXIT) · airframe 29,430 hrs · 17,394 cycles

RIGHT EMER EXIT DOOR CLOSING STRAP COVER MISSING. INSTALLED COVER IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 29,137 hrs · 17,221 cycles

L2 DOOR AFT SIDE EXIT LIGHT LENS COVER MISSING. R & R LENS IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 29,108 hrs · 17,206 cycles

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

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 28,225 hrs · 16,710 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED GIRT BAR IAW SIP.

Part: LIGHT — BROKEN (CABIN) · airframe 28,143 hrs · 16,663 cycles

MID CABIN OVERHEAD EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,143 hrs · 16,663 cycles

RIGHT OVERWING SIDEWALL EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 28,143 hrs · 16,663 cycles

LEFT HORIZONTAL STAB RIB CRACKED AT STATION 129.5. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,143 hrs · 16,663 cycles

RIGHT HORIZONTAL STAB RIB CRACKED AT STATION 129.5. REPAIRED RIB IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 28,143 hrs · 16,663 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,143 hrs · 16,663 cycles

INTERCOSTAL CRACKED BETWEEN BS 300.5 TO 306.5, RBL 16. R & R INTERCOSTAL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,143 hrs · 16,663 cycles

FORWARD SEAT TRACK FLANGE CRACKED AT BS 727B, FASTENER HOLES INBD & OTBD. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,143 hrs · 16,663 cycles

FORWARD SEAT TRACK FLANGE AFT TWO HOLES CRACKED AT BS 727B, RBL 24.75 FASTENER HOLES INBD & OTBD. REPAIRED FLANGE IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,143 hrs · 16,663 cycles

INTERCOSTAL CRACKED AT BS 330, LBL 2. R & R INTERCOSTAL IAW SRM.

Part: SKIN — DELAMINATED (RT HORIZ STAB) · airframe 28,143 hrs · 16,663 cycles

RIGHT HORIZONTAL STABILIZER UPPER SKIN DELAMINATED JUST INBD OF LOGO LIGHT. REPAIRED SKIN IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,143 hrs · 16,663 cycles

FORWARD SEAT TRACK FLANGE CRACKED AT BS 727B, RBL 45.5 FASTENER HOLES INBD & OTBD FLANGE. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,143 hrs · 16,663 cycles

FORWARD SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 24.75 FASTENER HOLES INBD & OTBD. REPAIRED FLANGE IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 28,143 hrs · 16,683 cycles

AFT CARGO FITTING CRACKED AT STATION 947, LBL10. R & R FITTING IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,143 hrs · 16,663 cycles

LEFT FUSELAGE SKIN LOWER BULKHEAD AFT FASTENER SECOND FROM TOP HOLE CRACKED AT BS 540. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,143 hrs · 16,663 cycles

LEFT FUSELAGE SKIN LOWER BULKHEAD AFT UPPER FASTENER HOLE CRACKED AT BS 540. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,143 hrs · 16,663 cycles

RIGHT FUSELAGE SKIN LOWER BULKHEAD AFT UPPER FASTENER HOLE CRACKED AT BS 540. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,143 hrs · 16,663 cycles

RIGHT FUSELAGE SKIN LOWER BULKHEAD AFT UPPER FASTENER SECOND FROM TOP HOLE CRACKED AT BS 540. REPAIRED SKIN IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 27,506 hrs · 16,297 cycles

RIGHT OVERWING LOWER EXIT LENS BROKEN. REPAIRED LENS IAW MM.

Part: SIGN — CRACKED (CABIN) · airframe 27,334 hrs · 16,190 cycles

AFT EMER EXIT SIGN BACK PLATE CRACKED. R & R SIGN IAW AMM.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 27,208 hrs · 16,118 cycles

L2 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY STILL OPERATIONAL. INSTALLED SLIDE ASSEMBLY IAW MT.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 26,620 hrs · 15,763 cycles

R1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE ASSEMBLY IAW MT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,730 hrs · 15,271 cycles

FORWARD FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,276 hrs · 15,016 cycles

RT EMERGENCY BATTERY FAILED CAPACITY CHECK BETWEEN ROW 8 TO ROW 13. R & R BATTERY PACK IAW AMM.

Part: FLAP TRACK — LOOSE (RT WING) · airframe 23,133 hrs · 13,721 cycles

RT WING INBD AFT FLAP INBD MAIN TRACK AFT ATTACH POINT LOOSE. R&R TRACK IAW AMM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 21,307 hrs · 12,645 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 138.70. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 21,307 hrs · 12,645 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,307 hrs · 12,645 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 184.70. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 20,980 hrs · 12,442 cycles

EEPLS LENS CRACKED BETWEEN ROW 4 TO ROW 10. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 20,980 hrs · 12,442 cycles

EEPLS LENS CRACKED BETWEEN ROW 14 TO ROW 23. REMOVED AND REPLACED LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 20,776 hrs · 12,299 cycles

EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 19,866 hrs · 11,724 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 19,866 hrs · 11,724 cycles

LEFT EEPLS COVERS CRACKED BETWEEN ROW 1 TO ROW 15. REMOVED AND REPLACED COVERS PER AMM.

Part: COVER — BROKEN (CABIN) · airframe 19,517 hrs · 11,516 cycles

FORWARD EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 18,922 hrs · 11,187 cycles

EGRESS LIGHTING FLOOR COVER PLATE CRACKED. REPLACED CRACKED FLOOR COVER PLATE PER M/M.

Part: BATTERY — FAILED (CABIN) · airframe 18,696 hrs · 11,068 cycles

LT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM AND SSM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,442 hrs · 10,337 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.

Part: COVER — BROKEN (CABIN) · airframe 16,551 hrs · 9,829 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 16,551 hrs · 9,829 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERIES FAILED CAPACITY TEST AT M1669 AND M1674. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 16,551 hrs · 9,829 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER BROKEN AT ROW 23. REMOVED AND REPLACED COVER PER MM.

Part: FUSE — BLOWN (CABIN) · airframe 15,967 hrs · 9,486 cycles

DURING SCHEDULED MV2 CHECK FOUND, LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FUSE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 14,926 hrs · 8,890 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT LOOSE. SECURED LIGHT PER MM.

Part: COVER — CRACKED (CABIN) · airframe 14,926 hrs · 8,890 cycles

LT EEPLS COVER CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 14,195 hrs · 8,464 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT AFT GALLEY EMERGENCY EXIT LIGHT BATTERY PACK FAILED. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 14,195 hrs · 8,464 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT AFT GALLEY EMERGENCY EXIT LIGHT BATTERY PACK FAILED. REMOVED AND REPLACED BATTERY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 14,195 hrs · 8,464 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED CHARGER ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,195 hrs · 8,464 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 14,195 hrs · 8,464 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,195 hrs · 8,464 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 14,195 hrs · 8,464 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED CHARGER ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,642 hrs · 8,145 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,446 hrs · 7,420 cycles

DURING SCHEDULED SPV CHECK, FOUND LT AFT EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 11,740 hrs · 6,993 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: COVER — BROKEN (CABIN) · airframe 11,139 hrs · 6,629 cycles

FWD EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: WINDOW — CRACKED (EVAC SLIDE) · airframe 11,139 hrs · 6,629 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE WINDOW CRACKED. REMOVED AND REPLACED WINDOW PER MM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 9,757 hrs · 5,775 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED SLIDE PER MT.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 9,534 hrs · 5,639 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 7,875 hrs · 4,649 cycles

DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED CHARGER ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 7,732 hrs · 4,559 cycles

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

Part: COVER — MISSING (CABIN) · airframe 6,885 hrs · 4,050 cycles

FOUND FWD EEPLS LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 5,385 hrs · 3,142 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 4,045 hrs · 2,345 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.