N785SW

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 77,501 hrs · 46,048 cycles

M1674 FAILED CAPACITY CHECK<[01] R/R M1674 BATTERY PACK PER AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 77,501 hrs · 46,048 cycles

M1669 FAILED CAPACITY CHECK<[01] R/R M1669 BATTERY PACK PER AMM 33-51-06

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 77,501 hrs · 46,048 cycles

-LH HORIZONTAL STABILIZER LOWER SLIDING SEAL CRACKED<[01] REMOVED AND REPLACED LH HORIZONTAL STAB LOWER SLIDING SEAL PER AMM 53-31-31

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 77,501 hrs · 46,048 cycles

M1673 FAILED CAPACITY CHECK<[01] R/R M1673 BATTERY PACK PER AMM 33-51-06

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 77,501 hrs · 46,048 cycles

-RH HORIZONTAL STABILIZER LOWER FWD SLIDING SEAL CRACKED<[01] REMOVED AND REPLACED RH HORIZONTAL STAB LOWER FWD SLIDING SEAL PER AMM 53-31-31

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 77,501 hrs · 46,048 cycles

-LH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED<[01] REMOVED AND REPLACED LH HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 77,501 hrs · 46,048 cycles

M1675 FAILED CAPACITY CHECK<[01] R/R M1675 BATTERY PACK PER AMM 33-51-06;[02] R/R M1675 BATTERY PACK PER AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 77,501 hrs · 46,048 cycles

M1672 FAILED CAPACITY CHECK<[01] R/R M1672 BATTERY PACK PER AMM 33-51-06

Part: HANDLE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 76,950 hrs · 45,694 cycles

PROVISIONING REPORTED A PROBLEM WITH FWD SERVICE EXTERNAL DOOR HANDLE<[01] ADJUSTED FWD SERVICE DOOR EXTERNAL DOOR HANDLE CAM PLATE TO ALLOW HANDLE TO FULLY STOW IN HANDLE PAN WHEN DOOR IS CLOSED PER AMM 52-41-00

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 76,634 hrs · 45,488 cycles

R1 DOOR OUTSIDE EMERGENCY EXIT LIGHT AND L1 OVER DOOR EMERGENCY EXIT LIGHT INOP.<[01] REPLACED M1674 BATTERY PACK IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 33-51-06; OPS CHECKED GOOD.

Part: SWITCH — INCORRECT (ZN 400 NACELLE/P) · airframe 76,461 hrs · 45,378 cycles

#1 COWL VALVE OPEN LIGHT ILLUMINATED BRIGHT BLUE WITH #1 ENG ANTI ICE SWITCH OFF AMBER TAI LIGHT WAS NOT ILLUMINATED<[01] FOUND WITH SWITCH OFF- PIN12/D462 OPEN; (SHOULD BE GRN). FOUND GOOD CONTINUITY PIN4/DP1303 TO PIN12/D462. FOUND GOOD CONTINUITY PIN 4 TO 5/DP1303 ON VALVE. FOUND GOOD GRN PIN5/DP1303 TO GD3838; REF:WDM 30-21-11. RECLOCKED #1 ENG COWL TAI VALVE TO ALLOW FULL ENGAGEMENT OF DP1303 & C/W COWL TAI VALVE INSTALL TEST PER AMM 30-21-11

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 74,446 hrs · 44,032 cycles

(CUSTOMER REQUEST) CRACK SUPPORT ANGLE LOC BS 663 LH SIDE AT CENTER WING BOX 2022-510772 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23.;[02] REPLACED SUPPORT ANGLE LOC BS 663 LH SIDE AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #111A1000 REV B .SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPLACED SUPPORT ANGLE LOC BS 663 LH SIDE AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #111A1000 REV B .SEE INDIVIDUAL SIGN OFFS BELOW .ITEM RII

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 74,446 hrs · 44,032 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500D TO BS520 AND STR28R FWD CARGO COMPARTMENT 2022-510733 /

Part: NONE — CRACKED (FWD CARGO) · airframe 74,446 hrs · 44,032 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500D TO BS520 AND STR28R FWD CARGO COMPARTMENT 2022-510733 / [01] REPLACED NEW WEB-INTERCOSTAL LOCATED BTW BS500D TO BS520 AND STR28R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 126 REV. A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED NEW WEB-INTERCOSTAL LOCATED BTW BS500D TO BS520 AND STR28R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 126 REV. A. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,446 hrs · 44,032 cycles

CRACK STRINGER 26R AT BS540 FWD CARGO COMPARTMENT 2022-510741 / [01] TOOL USED EDDY CURRENT PN/ NORTEC 600D; SN/ 190023010; DUE DATE/ 14-FEB-23.;[03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE: 01-FEB-23.;[04] REPAIRED STRINGER 26R AT BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. MATERIAL USED P/N 7075-T0/0.045? & /0.050?; HEAT TREATED AND CONVERTED FROM 7075-T0 TO CONDITION T6; IAW BAC5602 TABLE IV; PAGE 22 AND TABLE X PAGE 33. TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE: 01-FEB-23. TEMPERATURE 910F TO 930F FOR 30 TO 40 MINUTES PLUS ARTIFICIAL AGING.SEE INDIVIDUAL SIGNOFFS BELOW;[05] STEP 4 CORRECTED REPAIRED STRINGER 26R AT BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. MATERIAL USED P/N 7075-T0/0.045? PO 2022-183871 BATCH 202118387100101 & /0.050?; PO 2022-162992 BATCH 202216299200101 AND HEAT TREATED AND CONVERTED FROM 7075-T0 TO CONDITION T6; IAW BAC5602 TABLE IV; PAGE 22 AND TABLE X PAGE 33. TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE: 01-FEB-23. TEMPERATURE 910F TO 930F FOR 30 TO 40 MINUTES PLUS ARTIFICIAL AGING.SEE INDIVIDUAL SIGNOFFS BELOW

Part: PLATE — CRACKED (L/H WING) · airframe 74,446 hrs · 44,032 cycles

CRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL ORSS 214 AT LT WING 2022-510748 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL ORSS 214 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG# 115A2001 SHEET 1 REV: B; DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-20-01-1A-1 ; MESURE OF CRACK IS: 0.737' TOOL USED: P/N 700-113-10 S/N: 0023203 DUE DATE: 01/FEB/23;[02] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL ORSS 214 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG# 115A2001 SHEET 1 REV: B; DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-20-01-1A-1 ; MESURE OF CRACK IS: 0.737' TOOL USED: P/N 700-113-10 S/N: 0023203 DUE DATE: 01/FEB/23

Part: PLATE — CRACKED (R/H WING) · airframe 74,446 hrs · 44,032 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 214 AT RT WING 2022-510745 / [01] REPLACED CORRUGATED PLATE LOC. TRAILING EDGE LOCATED AT LEVEL ORSS 214 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 SEE INDIVIDUAL SING OFF BELOW.;[02] CORRECTED STEP 1<BR>REPLACED CORRUGATE PLATE LOC. TRAILING EDGE LOCATED AT LEVEL ORSS 214 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 SEE INDIVIDUAL SING OFF BELOW.;[03] CORRECTED STEP 1 <BR>REPLACED CORRUGATE PLATE LOC. TRAILING EDGE LOCATED AT LEVEL ORSS 214 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 SEE INDIVIDUAL SING OFF BELOW.

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 74,446 hrs · 44,032 cycles

CRACK STRINGER 26R AT BS540 FWD CARGO COMPARTMENT 2022-510741 / [01] TOOL USED EDDY CURRENT PN/ NORTEC 600D; SN/ 190023010; DUE DATE/ 14-FEB-23.;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE: 01-FEB-23.

Part: NONE — CRACKED (RH WING) · airframe 74,446 hrs · 44,032 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 214 AT RT WING 2022-510745 /

Part: PLATE — CRACKED (L/H WING) · airframe 74,446 hrs · 44,032 cycles

CRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL ORSS 214 AT LT WING 2022-510748 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL ORSS 214 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG# 115A2001 SHEET 1 REV: B; DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-20-01-1A-1 ; MESURE OF CRACK IS: 0.737' TOOL USED: P/N 700-113-10 S/N: 0023203 DUE DATE: 01/FEB/23;[02] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL ORSS 214 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG# 115A2001 SHEET 1 REV: B; DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-20-01-1A-1 ; MESURE OF CRACK IS: 0.737' TOOL USED: P/N 700-113-10 S/N: 0023203 DUE DATE: 01/FEB/23

Part: STRUCTURE — CRACKED (L/H WING) · airframe 74,446 hrs · 44,032 cycles

CRACK TRAILING EDGE SUPPORT STRUCTURE OF ACCESS PANEL 561AB AT LT WING 2022-510724 / [01] REPLACED SUPPORT STRUCTURE AND FASTENERS OF ACCESS PANEL 561AB AT LT WING IAW B737-700 51-10-02 ITEM 9; DUE TO NOT ALLOWABLE DAMAGE IAW B737-700 FOR CRACK; MEASURE OF CRACK IS: 1.060 TOOL USED PN:500-197-30 SN:B16144189 DUE DATE: 11-MAR-23;[02] CORRECTION ACTION 1: REPLACED SUPPORT STRUCTURE AND FASTENERS OF ACCESS PANEL 561AB AT LT WING IAW B737-700 51-10-02 ITEM 9; DUE TO NOT ALLOWABLE DAMAGE IAW B737-700 SRM 57-51-02 -1A-1 FOR CRACK; MEASURE OF CRACK IS: 1.060 TOOL USED PN:500-197-30 SN:B16144189 DUE DATE: 11-MAR-23;[03] CORRECTION ACTION 2: REPLACED SUPPORT STRUCTURE AND FASTENERS OF ACCESS PANEL 561AB AT LT WING IAW B737-700 51-10-02 ITEM 9 AND DWG 115A3700 SHEET 26 REV -; DUE TO NOT ALLOWABLE DAMAGE IAW B737-700 SRM 57-51-02 -1A-1 FOR CRACK; MEASURE OF CRACK IS: 1.060 TOOL USED PN:500-197-30 SN:B16144189 DUE DATE: 11-MAR-23;[04] CORRECTIVE ACTION STEP 3 CERTIFIED

Part: ANGLE — CRACKED (R/H WING) · airframe 74,446 hrs · 44,032 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS 270 DEFLECTION CONTROL RIB AT RT WING 2022-510717 / [01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 270 DEFLECTION CONTROL RIB AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. CRACK LENGTH IS: 0.950?. TOOL USED CALIPER P/N: 700-113-10; S/N: 0019289 AND DUE DATE: 04-JUL-23;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 270 DEFLECTION CONTROL RIB AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. CRACK LENGTH IS: 0.950?. TOOL USED CALIPER P/N: 700-113-10; S/N: 0019289 AND DUE DATE: 04-JUL-23

Part: STRUCTURE — CRACKED (R/H WING) · airframe 74,446 hrs · 44,032 cycles

CRACK TRAILING EDGE SUPPORT STRUCTURE OF ACCESS PANEL 621AB AT RT WING 2022-510721 / [01] REPLACED TRAILING EDGE SUPPORT STRUCTURE (BEAM) OF ACCESS PANEL 621AB AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A3700 SHEET 7 REV -; SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED TRAILING EDGE SUPPORT STRUCTURE (BEAM) OF ACCESS PANEL 621AB AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A3700 SHEET 7 REV -; SEE INDIVIDUAL SIGN OFF BELOW

Part: ANGLE — CRACKED (L/H WING) · airframe 74,446 hrs · 44,032 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS 270 DEFLECTION CONTROL AT LT WING 2022-510722 / [01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 270 DEFLECTION CONTROL AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. CRACK LENGTH IS: 0.885?. TOOL USED CALIPER P/N: 700-113-10; S/N: 0019289 AND DUE DATE: 04-JUL-23;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 270 DEFLECTION CONTROL AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. CRACK LENGTH IS: 0.885?. TOOL USED CALIPER P/N: 700-113-10; S/N: 0019289 AND DUE DATE: 04-JUL-23

Part: PLATE — CRACKED (R/H WING) · airframe 74,446 hrs · 44,032 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2022-510719 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS IN B737-700 SRM 57-20-01-1A. IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-05 AND DWG # 115A2001 SHEET 18 REV -. MEASURE OF CRACK IS L=0.623? TOOL USED CALIPER PN:500-197-30; SN:A18135101; DUE DATE 30/JUN/23;[02] TASK COMPLETED

Part: NONE — CRACKED (LH WING) · airframe 74,446 hrs · 44,032 cycles

CRACK TRAILING EDGE SUPPORT STRUCTURE OF ACCESS PANEL 561AB AT LT WING 2022-510724 /

Part: PLATE — CRACKED (R/H WING) · airframe 74,446 hrs · 44,032 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2022-510719 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS IN B737-700 SRM 57-20-01-1A. IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-05 AND DWG # 115A2001 SHEET 18 REV -. MEASURE OF CRACK IS L=0.623? TOOL USED CALIPER PN:500-197-30; SN:A18135101; DUE DATE 30/JUN/23;[02] TASK COMPLETED

Part: NONE — INOPERATIVE · airframe 74,446 hrs · 44,032 cycles

INOP LOWERED CEILING PANEL BATTERY PACK RT SIDE AT AFT GALLEY AREA (1 EA) 2022-510427 /

Part: BATTERY PACK — INOPERATIVE (L/H CABIN) · airframe 74,446 hrs · 44,032 cycles

INOP LOWER SIDEWALL BATTERY PACK LT SIDE WITHIN STA 578.45 TO STA 610 AT PASSENGER CABIN (1 EA) 2022-510430 / [01] REPLACED LOWER SIDEWALL BATTERY PACK LT SIDE WITHIN STA 578.45 TO STA 610 AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-06-960-805 TEST IS OK;[02] REPLACED LOWER SIDEWALL BATTERY PACK LT SIDE WITHIN STA 578.45 TO STA 610 AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-06-960-805 TEST IS OK

Part: NONE — BROKEN (CABIN) · airframe 74,446 hrs · 44,032 cycles

BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (7 EA) 2022-510673 / [01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (7 EA) I.A.W B737-700 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (7 EA) I.A.W B737-700 AMM 33-51-15-400-802

Part: NONE — INOPERATIVE (R/H CABIN) · airframe 74,446 hrs · 44,032 cycles

INOP LOWERED CEILING PANEL BATTERY PACK RT SIDE AT AFT GALLEY AREA (1 EA) 2022-510427 / [01] REPLACED LOWERED CEILING PANEL BATTERY PACK RT SIDE AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-06-960-805;[02] CORRECTED STEP 1 <BR>REPLACED LOWERED CEILING PANEL BATTERY PACK RT SIDE AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-06-960-805 TEST IS OK;[03] REPLACED LOWERED CEILING PANEL BATTERY PACK RT SIDE AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-06-960-805 TEST IS OK

Part: ANGLE — CRACKED (VERT. STAB.) · airframe 74,446 hrs · 44,032 cycles

CRACK LEADING EDGE SUPPORT ANGLE LOCATED AT BS 1016 BETWEEN S-2R AND S-2L WL 308.5 AT VERTICAL STABILIZER 2022-510342 / [01] REPLACED NEW LEADING EDGE SUPPORT ANGLE LOCATED AT BS 1016 BETWEEN S-2R AND S-2L WL 308.5 AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 176A3101 SHEET 4 REV - PART NUMBER USED: 176A3101U26 P.O: 2022 196014 SEE INDIVIDUAL SING OFFS BELOW.;[02] REPLACED NEW LEADING EDGE SUPPORT ANGLE LOCATED AT BS 1016 BETWEEN S-2R AND S-2L WL 308.5 AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 176A3101 SHEET 4 REV - PART NUMBER USED: 176A3101U26 P.O: 2022 196014 SEE INDIVIDUAL SING OFFS BELOW... RII ITEM

Part: VAPOR BARRIER — CRACKED (L/H MLG W/W) · airframe 74,446 hrs · 44,032 cycles

CUSTOMER REQUEST: CRACK VAPOR VARRIER LT SIDE AT MAIN WHEEL WELL COMPARTME 2022-510256 / [01] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18196127; DUE DATE: 16-JAN-23.;[02] TOOL USED SCALE P/N:91847 S/N: EA-409314 DUE DATE 06-JUN-23.;[03] TOOL USED SCALE P/N: 1863T62; AE-40571; DUE DATE: 09-JUN-23.;[04] REPAIRED VAPOR BARRIER LT SIDE AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10 TOOL USED CALIPER P/N: 500-193-30 S/N: 0000285 DUE DATE: 10-DEC-22. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] TASK COMPLETED.RII

Part: BARRIER — CRACKED (L/H MLG W/W) · airframe 74,446 hrs · 44,032 cycles

CUSTOMER REQUEST: CRACK VAPOR VARRIER LT SIDE AT MAIN WHEEL WELL COMPARTME 2022-510256 / [01] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18196127; DUE DATE: 16-JAN-23.;[02] TOOL USED SCALE P/N:91847 S/N: EA-409314 DUE DATE 06-JUN-23.;[03] TOOL USED SCALE P/N: 1863T62; AE-40571; DUE DATE: 09-JUN-23.;[04] REPAIRED VAPOR BARRIER LT SIDE AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10 TOOL USED CALIPER P/N: 500-193-30 S/N: 0000285 DUE DATE: 10-DEC-22. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] TASK COMPLETED.RII

Part: PANEL — PERFORATED (WTB) · airframe 74,446 hrs · 44,032 cycles

CUSTOMER REQUEST: PERFORATION ON ACCESS PANEL 191CL BODY FAIRING AT FUSELAGE EXTERIOR 2022-510212 / [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-409317; DUE DATE: 06-JUN-23.;[03] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18196127; DUE DATE: 16-JAN-23.;[04] TOOL USED: SCALE PN: 1863T62 SN: AE-40571 DUE DATE: 09-JUN-23;[05] TOOL USED: MICROBONDER P/N:HCS8800 S/N:01685794 DUE DATE: 16-JAN-23.;[06] REPAIRED ACCESS PANEL 191CL BODY FAIRING IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2 SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED

Part: SLIDE — LOW (AFT SERVICE DOOR) · airframe 74,388 hrs · 43,994 cycles

CREW REPORTS DOOR ESCAPE SLIDES APPEAR OUT OF GREEN BANDS. / [01] INSPECTED ALL 4 SLIDES AND FOUND ONLY AFT SERVICE DOOR SLIDE TO BE IN THE RED; ALL OTHERS OK FOR SERVICE PER MM 25-66-01.;[02] INSPECTED ALL 4 SLIDES AND FOUND ONLY AFT SERVICE DOOR SLIDE TO BE IN RED; ALL OTHERS OK FOR SERVICE PER MM 25-66-01; R&R AFT SERVICE DOOR SLIDE ASSY PER MT 725-61-06AS.

Part: LENS — MISSING (PAX CABIN) · airframe 74,280 hrs · 43,918 cycles

FWD ENTRY EMERGENCY LIGHT LENS MISSING / [01] R +R ?D FWD ENTRY EMERGENCY LIGHT LENSIAW AMM REF. 33-51?01

Part: SLIDE — OUT OF POSITION (FWD ENTRY DOOR) · airframe 74,024 hrs · 43,747 cycles

FORWARD ENTRY SLIDE NEEDS TO BE RE-SECURE / [01] RE-SECURE FWD ENTRY SLIDE PER AMM 25-66-01.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 73,962 hrs · 43,707 cycles

PROVO WHILE CLOSING FORWARD SERVICE DOOR; ESCAPE SLIDE BAR FELL OUT AND JAMMED INTO FLOOR AREA. / [01] RESECURED GIRT BAR ASSY. PER AMM 25-66-01

Part: LANYARD — OUT OF POSITION (L1 DOOR) · airframe 73,839 hrs · 43,618 cycles

FWD ENTRY GIRT BAR VELCRO HANGING OUT / [01] SECURED I/A/W S.I.P.

Part: PANEL — CRACKED (FWD CARGO) · airframe 73,815 hrs · 43,600 cycles

FWD BULKHEAD CEILING PANEL 120 YAC CRACK ON THE CURVATURE / [01] REMOVED AND REPLACED 120 YAC FWD CARGO BIN PANEL PER AMM 25-52-09

Part: SLIDE — OUT OF TOLERANCE (L1 DOOR) · airframe 73,807 hrs · 43,596 cycles

FORWARD ENTRY DOOR SLIDE PRESSURE BELOW LIMITS / [01] REMOVED AND INSTALLED FORWARD ENTRY(FE) DOOR SLIDE PER AMM 25-66-01-401-NG.

Part: GUARD — CRACKED (L/H OVERWING EXI) · airframe 73,309 hrs · 43,281 cycles

LEFT OVERWING DOOR GUARD ASSY CRACKED / [01] C/W 22-153-01272

Part: GUARD — CRACKED (R/H OVERWING EXI) · airframe 73,309 hrs · 43,281 cycles

RIGHT OVERWING DOOR GUARD ASSY CRACKED / [01] EA# 22-153-01272 AND FAULT TTG8Q00C4RFM

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 72,433 hrs · 42,727 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR ILLUMINATION LAMP BURNED OUT ; / [01] OK TO CONT PER MEL 33-2-03;SP1B;AUTH #42210. REPLACED THE LAMP, NO HELP. REPLACED FUSE ON RT OVERWING EXITSIGN LIGHT IAW AMM 33-21-00. OPS CHECK GOOD; OK FOR SERVICE.

Part: PLATE — PULLED (R/H WING) · airframe 72,163 hrs · 42,567 cycles

RH WING INBD FIXED TRAILING EDGE LOWER PANEL WIGGLE PLATE BEHIND #2 ENGINE HAS SEVERAL PULLED FASTENERS. ; / [01] C/W TASKCARD

Part: PANEL — CRACKED (FUSELAGE) · airframe 71,765 hrs · 42,322 cycles

SUPPLEMENTAL INFORMATION: 193D PNL TRAILING EDGE HAS 7 FASTENER HOLES THAT ARE CRACKED DIMPLED AND ELONGATED ; / [01] ACCOMPLISH EA 21-153-03040 ASSIGNED AS A SUBTASK.; [02] C/W EA 21-153-03040

Part: PANEL — CRACKED (FUSELAGE) · airframe 71,765 hrs · 42,322 cycles

SUPPLEMENTAL INFORMATION: 194E PNL HAS DENT WITH CRACK ; / [01] ACCOMPLISH EA 21-153-03041 ASSIGNED AS A SUBTASK.; [02] C/W EA 21-0153-03041

Part: MEGAPHONE — INOPERATIVE (AFT CABIN) · airframe 70,230 hrs · 41,403 cycles

AFT MEGAPHONE INOP R+R BATTERYS PER AMM 256400; OPS CHECK GOOD

Part: COVER — MISSING (L2 DOOR HANDLE) · airframe 70,121 hrs · 41,344 cycles

COVER FOR HANDLE ON AFT ENTRY. ESCAPE SLIDE MISSING RESECURED L2 DOOR ESCAPE SLIDE DOOR MANUAL INFLATION HANDLE COVER IAW MM 255601 OK TO CONTINUE IN SERVICE

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 69,513 hrs · 41,017 cycles

MISSING FO SIDE OVERWING EMERGENCY LIGHT COVER JUST AFT OF EXIT DOOR. REPLACED MISSING EMERGENCY LIGHT COVER AT RT OVERWING EMERGENCY EXIT DOOR, PER AMM 33-51-11.

Part: SHEAR TIE — CRACKED (BS 1104) · airframe 69,162 hrs · 40,803 cycles

CRACK INTERNAL STRUCTURE SECONDARY FINDINGS SHEAR TIE ON BS 1104 RT SIDE IN TAIL COMPARTMENT (1EA). REPLACED SHEAR TIE (1EA) LOCATED INTERNAL STRUCTURE ON BS 1104 BETWEEN STR 1 TO STR 3R RT SIDE IN TAIL COMPARTMENT, IAW B737-700 SRM 51-40-02, 51-10-02 AND DWG 148A1225 REV.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 69,162 hrs · 40,803 cycles

CORROSION FLOOR PANEL 120BF PLATE AT FWD CARGO COMPARTMENT (1 EA) / REPLACED PLATE FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT (1EA) IAW B737-700 SRM 51-10-02 ITEM 9

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 69,162 hrs · 40,803 cycles

CORROSION PLATE FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT (1 EA) / REPLACED PLATE FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT (1EA) IAW B737-700 SRM 51-10-02 ITEM 9

Part: FLOOR PANEL — ELONGATED (AFT CARGO) · airframe 69,162 hrs · 40,803 cycles

ELONGATED HOLE FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT / FABRICATED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT FROM MATERIAS AWM SHEET 2024-T3 CLAD 0.80' PO #2019-600941 IAW B737-700 DWG 453A2610 REV E AND SRM 51-10-02

Part: FRAME — CRACKED (BS 294) · airframe 69,163 hrs · 40,803 cycles

CRACK FRAME ON BS 294.5 STUB FRAME BETWEEN S-8R TO S9R FWD GALLEY AND LAV. REPLACED STUB FRAME BS 294.5 BETWEEN S-8R TO S-9R FWD GALLEY AND LAV, IAW B737-700 SRM 51-40-02 AND DRAWING 141A8370.

Part: SKIN — DAMAGED (R2 DOOR) · airframe 69,163 hrs · 40,803 cycles

ELONGATED HOLES EXTERNAL SKIN SERVICE DOOR LOCATED BETWEEN BS 291.5 AND BS 294.5 AND BETWEEN S-8R TO S-9R FWD GALLEY AND LAV. REPLACED GAP COVER WITH NEW FASTENERS LOCATED EXTERNAL SKIN, CUT OUT FWD SERVICE DOOR LOCATED BETWEEN BS 291.5 AND BS 294.5 BETWEEN STR 8R AND STR 9R, IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 'A' AND DWG 141A8350 REV.

Part: ANGLE — CRACKED (BS 294 S8-9R) · airframe 71,229 hrs · 41,994 cycles

CRACK FWD SERVICE DOOR REVEAL ANGLE LOCATED AT BS 294.5 BETWEEN S-8R AND S-9R AT PASSENGER CABIN / REPLACED REVEAL ANGLE LOCATED AT BS 294.5 BETWEEN S-8R AND S-9R AT PASSENGER CABIN FWD SERVICE DOOR IAW B737-700 SRM 51-40-02 AND DRAWING #141A8370 REV D

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,162 hrs · 40,803 cycles

CRACK SUPPORT ANGLE ON BS328 AT LEVEL STR22L AT EQUIPMENT ELECTRONIC COMP / REPLACED SUPPORT ANGLE ON BS328 AT LEVEL STR22L AT EQUIPMENT ELECTRONIC COMP. IAW SRM B737-700 51-40-02;51-10-02; ITEM 9 AND DWG. 141A8140 SHEET 8 REV.

Part: ANGLE — GOUGED (BS 1104-1121) · airframe 69,162 hrs · 40,803 cycles

GOUGE ON EXISTING REPAIR ON CLOSURE ANGLE LOCATED FROM BS 1104 TO BS 1121 BETWEEN STR 2R AND STR 3R AT UPPER FUSELAGE (1 EA). REMOVED AND REPLACED EXISTING REPAIR OF CLOSURE ANGLE LOCATED FROM BS 1104 TO BS 1121 BETWEEN STR 2R AND STR 3R AT UPPER FUSELAGE, IAW B737-700 SRM 53-00- 71-2R-6 AND EXISTING REPAIR WAS VERIFIED AND MET WITH REPAIR INSTRUCTION AND THIS REPAIR IS CATEGORY 'A' AND NOT REQUIRED INSPECTIONS.

Part: ANGLE — GOUGED (BS 1104-1121) · airframe 69,162 hrs · 40,803 cycles

GOUGE CLOSURE ANGLE LOCATED FROM BS 1104 TO BS 1121 BETWEEN STR 2L TO STR 3L AT UPPER FUSELAGE (1 EA). REPLACED EXISTING REPAIR ON CLOSURE ANGLE LOCATED FROM BS 1104 TO BS 1121 BETWEEN STR 2L TO STR 3L AT UPPER FUSELAGE, IAW B737-700 SRM 53-80-71-2R-6 REPAIR 6.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 69,162 hrs · 40,803 cycles

CRACK TIE CLIP ON BS 277 AND STRINGER 10R AT PASSENGER CABIN (1 EA). REPLACED TIE CLIP AT ON BS 277 AND STR 10R AT PASSENGER CABIN (1EA). IAW B737-700 SRM 51-40- 02-0G-0 PARA 4 ITEM B AND DWG 141A8380 SHEET 14 REV.

Part: STRINGER — CRACKED (BS 291) · airframe 69,162 hrs · 40,803 cycles

CRACK STRINGER 15L AND BS 291.5 AT PASSENGER CABIN. PERFORMED REPAIR ON STRINGER 15L AND BS 291.5 AT PASSENGER CABIN, IAW AEROMAN EA 53-0652-20 REV 0 AND SOUTHWEST EA NO.20-153-01930 REV IR.

Part: SHIELD — DAMAGED (BS 847-867) · airframe 69,162 hrs · 40,803 cycles

ELONGATED HOLE FLOOR STRUCTURE SHIELD LOCATED BTW BS 847 TO BS 867 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT / REPLACED FLOOR STRUCTURE SHIELD LOC BTW BS 847 TO BS 867 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02 AND DWG #146A0081 REV A

Part: BRACKET — CRACKED (RT WING SLAT) · airframe 69,162 hrs · 40,803 cycles

CRACK SLAT 7 AUXILIARY TRACK BRACKET LOCATED AT SLAT STATION 373 AT RT WING / REPLACED BRACKET LOCATED SLAT 7 AUXILIARY TRACK AT SLAT SATATION 373 AT RT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG 114A5020 SHEET 6 REV D

Part: SUPPORT ANGLE — CRACKED (BS 500B S26L) · airframe 69,162 hrs · 40,803 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS500B FWD AND AFT FACE AT LEVEL STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE - SUPPORT LOC BS 500B FWD AND AFT FACE AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG # 143A7505.

Part: SUPPORT ANGLE — CRACKED (BS 420 S26L) · airframe 69,162 hrs · 40,803 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS420 AFT FACE AND STR 26L FWD CARGO COMPARTMENT / REPLACED ANGLE-SUPPORT LOCATED ON 135420 FRONT FACE AND STR 26L CARGO COMPARTMENT I:A:W B737-700 SRM 51-40-02 AND DWG# 143A75 05 REV 'B'.

Part: SUPPORT ANGLE — CRACKED (BS 500C S26R) · airframe 69,162 hrs · 40,803 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS500C FWD FACE AND STR26R FWD CARGO COMPARTMENT / REPLACED ANGLE - SUPPORT LOCATED ON B5500C FWD FACE AND STR 26R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG # 143A7505 REV= 'D'.

Part: BEAR STRAP — CRACKED (BS 291-294) · airframe 69,162 hrs · 40,803 cycles

CRACK FORWARD GALLEY DOOR (RI) BEAR STRAP INTERNAL ARE LOCATED AT BS 291.5 TO BS 294.5 BETWEEN STR 8R AND STR 9R AT PASSENGER CABIN. REPAIRED FORWARD BELLY DOOR INTERNAL AREA AT BS 291.5 AND BETWEEN STR 7R AND STR 9R, IAW EA N. 20-153-01918 REVISION IR AND EA N 53-0635-20 REV 0.

Part: SUPPORT ANGLE — CRACKED (BS 440 S26L) · airframe 69,162 hrs · 40,803 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS440 FWD FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE - SUPPORT LOCATED ON BS440 FWD FACE AND STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG #143A7505 REV 'A' AND SRM B737-700 51-10-02 ITEM 9

Part: SUPPORT ANGLE — CRACKED (BS 500B) · airframe 69,162 hrs · 40,803 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS500B FWD FACE AND STR26R FWD CARGO COMPARTMENT / REPLACED NEW ANGLE SUPPORT WITH NEW FASTENER LOCA TED ON BS 500B FWD FACE AND STR 26R FWD CARGO IAW B737-700 SRM 51-40-02 DWG. 143A7505 REV. D.

Part: SUPPORT ANGLE — CRACKED (BS 460 S26L) · airframe 69,162 hrs · 40,803 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS460 FWD FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE - SUPPORT LOCATED ON BS 460 FWD FACE AND STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG #143A7505 REV 'A' AND B737-700 SRM 51-10-02 ITEM 9

Part: SUPPORT ANGLE — CRACKED (BS 400 S26R) · airframe 69,162 hrs · 40,803 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS400 AFT FACE AND STR26R FWD CARGO COMPARTMENT / REPLACED ANGLE LOCATED ON BS400 AFT FACE AND STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 5142-02 DGW 143A7505 REV B

Part: SUPPORT ANGLE — CRACKED (BS 500A S26L) · airframe 69,162 hrs · 40,803 cycles

CRACK ANGLE-SUPPORT LOCATED ON BS500A FWD FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE - SUPPORT LOC. ON BS 500A FWD FACE AND STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-42-02 AND DWG 143A7505- 60 SHEET 37 REV.

Part: GUSSET — CRACKED (500D S19R) · airframe 69,162 hrs · 40,803 cycles

CRACK GUSSET LOCATED ON BS500D AND STR19R AT FWD CARGO COMPARTMENT/ / REPLACED GUSSET AND FASTENERS LOC ON BS 500D AND STR 19R AD FWD CARGO COMPARTMENT IAW B737-700 DWG 143A902

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 69,162 hrs · 40,803 cycles

CRACK EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA). REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1EA), IAW B737-700 AMM 33-51-01-960-801.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 69,162 hrs · 40,803 cycles

INOPERABLE BATTERY EMERGENCY FLASHLIGHT ON WINDSCREEN LT AT FWD GALLEY AREA (1 EA). REPLACED BATTERY EMERGENCY FLASHLIGTH ON WINDSCREEN LT AT FDW GALLEY AREA (1AE), IAW B737-700 AMM 25.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 69,162 hrs · 40,803 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT / REPAIRED BY WELDS SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTAMENT IAW BOEING 737-700 SRM 53-60-15-2R-1; REPAIR 1 PARAGRAPH 4.B. STEP (4) AND BAC 5975

Part: GUSSET — CRACKED (BS 500D S21L) · airframe 69,162 hrs · 40,803 cycles

CRACK GUSSET LOCATED ON BS500D AND STR21L AT FWD CARGO COMPARMENT / REPLACED GUSSET LOCATED ON BS 500D AND STR 21L AT FWD CARGO COMPARTMENT IAW SRM B737- 700 51-10-02-0G ITEM 9 AND DRAWING 143A7902

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,162 hrs · 40,803 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AT 20 INCH FRONT SPAR AT LT HORIZONTAL STABILIZER. REPAIRED INSPAR RIB LOCATED STAB 129.50 AT 20 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER, IAW SRM B737-700 55-10-09-2R-4.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,162 hrs · 40,803 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FRONT SPAR AT RT HORIZONTAL STABILIZER. PERFORMED REPAIR RIB 120.30 BETWEEN 23' TO 38' FROM THE FRONT SPAR HORIZONTAL RT, IAW B737-700 SRM 55-10- 09 2R-5 REPAIR 5 FIG 204 SHEET 2 AND THE REPAIR STEPS WERE DOCUMENTED ON NRC L177845.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,163 hrs · 40,803 cycles

CRACK LEADING EDGE RIB LOC ON LEADING EDGE STA 105.26 AT RT HORIZONTAL STABILIZER (1 EA). REPLACED LEADING EDGE RIB LOCATED ON LEADING EDGE STA 105.26 AT RT HORIZONTAL STABILIZER (1EA), IAW B737-700 SRM 51-40-0; 51-10-02 ITEM 9 AND DWG 186A1001 SHEET 10 REV A.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,162 hrs · 40,803 cycles

CRACK LEADING EDGE RIB LOC ON LEADING EDGE STA 95.96 AT RT HORIZONTAL STABILIZER (1 EA). REPLACED TO RIB LOC ON LEADING EDGE DTA 95.96 AT RT HORIZONTAL STABILIZER (1EA), IAW B737-700 SRM 51-40-02 ITEM 9 AND DWG 186A1001 REV A.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,162 hrs · 40,803 cycles

CRACK LEADING EDGE RIB LOCATED ON LEADING EDGE STA 95.96 AT LT HORIZONTAL STABILIZER (1 EA). REPLACED LEADING EDGE RIB LOCATED ON LEADING EDGE STA 105.26 AT LT HORIZONTAL STABILIZER, IAW B737-700 SRM 51-10-02 ITEM 9, 51-40-02 AND DRAWING 186A1306 REV.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,162 hrs · 40,803 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FRONT SPAR AT RT HORIZONTAL STABILIZER. PERFORMED REPAIR RIB 120.30 BETWEEN 23' TO 38' FROM THE FRONT SPAR HORIZONTAL STABILIZER RT, IAW B737-700 SRM 55-10-09 2R-5 REPAIR 5 FIGURE 204 SHEET 2.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,163 hrs · 40,803 cycles

CRACK LEADING EDGE RIB LOC ON LEADING EDGE STA 86.66 AT RT HORIZONTAL STABILIZER (1 EA). REPLACED RIB LOC ON LEADING EDGE STA 86.66 AT RT HORIZONTAL STABILIZER (1EA), IAW B737-700, SRM 51- 40-02, ITEM 9 AND DWG 186A1001 REV A.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,162 hrs · 40,803 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 20 INCH FROM SPAR AT RT HORIZONTAL STABILIZER. REPAIRED INSPAR RIB LOCATED STAB STA 120.30 A 20 INCH FROM SPAR AT RT HORIZONTAL STAB, IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4.

Part: LIGHT — DETERIORATED (CABIN) · airframe 69,162 hrs · 40,803 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (5 EA). REPLACED PHOTOLUMINEXCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN, IAW WORK INSTRUCTION N MT 733-50-01.

Part: SIGN — LOOSE (CABIN) · airframe 69,133 hrs · 40,787 cycles

EXIT SIGN OVER AISLE FELL OFF / RESECURED EXIT SIGN OVER CENTER AISLE AS REQUIRED PER SIP

Part: COVER — DETACHED (SLIDE PULL) · airframe 68,741 hrs · 40,533 cycles

FA REPORTED THE SLIDE MANUAL PULL COVER WAS MISSING. THE COVER WAS FOUND UNDER COVER OF THE DOOR AND SECURED IAW AMM 25-66-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,573 hrs · 40,429 cycles

BATTERY M1670 DISCHARGED. / R&R BATTERY M1670 PER AMM 33-51-06 OPS CHECK GOOD P/N OFF/ON D717-01-100SWA S/N OFF 31217 S/N ON 34552

Part: TRUNNION — CORRODED (LT MLG) · airframe 68,478 hrs · 40,375 cycles

LH MLG LOWER OB TRUNION SUPPORT FITTING IB/OB FACE BORE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REVISION 11; REFERENCE D&M ENTERPRISES WORK ORDER # SSR 1217

Part: TRUNNION — CORRODED (LT MLG) · airframe 68,478 hrs · 40,375 cycles

LH MLG UPPER OB TRUNION SUPPORT FITTING OB FACE; BORE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REVISION 11; D&M ENTERPRISES WORK ORDER SSR# 1217

Part: TRUNNION — CORRODED (LT MLG) · airframe 68,478 hrs · 40,375 cycles

LH MLG LOWER IB TRUNNION SUPPORT FITTING OB FACE BORE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REVISION 11; REFERENCE D&M ENTERPRISES WORK ORDER # SSR 1217

Part: TRUNNION — CORRODED (RT MLG) · airframe 68,478 hrs · 40,375 cycles

RH MLG LOWER IB TRUNNION SUPPORT FITTING IB/OB FACE; BORE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REVISON 11; REFERENCE D&M ENTERPRISES WORK ORDER SSR 1218

Part: TRUNNION — CORRODED (RT MLG) · airframe 68,478 hrs · 40,375 cycles

RH MLG UPPER IB TRUNNION SUPPORT FITTING OB FACE; BORE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REVISION 11; REFERENCE D&M ENTERPRISES WORK ORDER SSR# 1218

Part: TRUNNION — CORRODED (LT MLG) · airframe 68,478 hrs · 40,375 cycles

LH MLG UPPER IB TRUNNION SUPPORT FITTING IB FACE; BORE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REVISION 11; REFERNCE D&M ENTERPRISES WORK ORDER # SSR 1217

Part: TRUNNION — CORRODED (RT MLG) · airframe 68,478 hrs · 40,375 cycles

RH MLG LOWER OB TRUNNION SUPPORT FITTING. IB/OB FACE; BORE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REVISON 11; REFERENCE D&M ENTERPRISES WORK ORDER SSR 1218

Part: TRUNNION — CORRODED (RT MLG) · airframe 68,478 hrs · 40,375 cycles

RN MLG UPPER OB TRUNNION SUPPORT FITTIN OB FACE BORE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REVISION 11; REFERENCE D&M ENTERPRISES WORK ORDER SSR 1218

Part: BATTERY PACK — FAILED (CABIN) · airframe 67,737 hrs · 39,873 cycles

EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATIONS M01672. / R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 67,737 hrs · 39,873 cycles

EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATIONS M01673. / R&R BATTERY PACK PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 67,431 hrs · 39,671 cycles

R1 DOOR SLIDE OUT OF POSITION IN BUSTLE. / REINSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,671 hrs · 39,198 cycles

EMERGENCY LIGHT AT SEAT 6C INOP. R&R BULB PER AMM.

Part: ACTUATOR — INOPERATIVE (PITCH TRIM) · airframe 66,437 hrs · 39,051 cycles

AIR TURNBACK/DECLARED EMERGENCY, ON CLIMB OUT MANUAL ELECTRIC PITCH TRIM NOT WORKING ENGAGED AUTO PILOT STILL NO PITCH TRIM COMPLIED WITH QRH NORMAL FLAPS IS LANDING OVERWEIGHT EST 132K LBS. / R&R STAB TRIM ACTUATOR PER AMM.

Part: COVER — UNSECURE (CABIN) · airframe 66,168 hrs · 38,878 cycles

EMERGENCY LIGHT CAP ABOVE ROW 7 FELL OFF. R&R EMERGENCY LIGHT COVER IAW AMM.

Part: RIB — CRACKED (LEFT WING) · airframe 65,712 hrs · 38,599 cycles

L/H WING; INBOARD FIXED TRAILING EDGE; DEFLECTION CONTROL RIB UPPER TAB IS CRACKED / REPAIRED CONTROL RIB UPPER TAB PER SRM 57-51-02-2R-3.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 65,712 hrs · 38,599 cycles

FORWARD CARGO DOOR CENTER THRESHOLD CRACKED WHERE STOP FITTINGS MADE CONTACT. R&R THRESHOLD PER AMM.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 65,712 hrs · 38,599 cycles

RIGHT WING VERTICAL BULB SEAL RETAINER AFT OF #1 LOWER STRUT CRACKED / REMOVED AND REPLACED RIGHT WING VERTICAL BULB SEAL RETAINER AFT OF #1 LOWER STRUT PER SRM 51-40-02 AND MM 20-50-11

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 65,633 hrs · 38,551 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE OUT OF POSITIONED INSIDE CASE. REPOSITIONED SLIDE PER MT.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 65,567 hrs · 38,505 cycles

R1 DOOR SLIDE PRESSURE IN THE RED (LOW). R&R SLIDE PER MT.

Part: BRACKET — CRACKED (LWR FUSELAGE) · airframe 64,113 hrs · 37,565 cycles

L/H WING TO BODY FWD UPPER SHELF BRACKET CRACKED / R&R L/H WING TO BODY BRACKET PER SRM 51-40-02

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,485 hrs · 37,163 cycles

RT OVER WING LOWER EXIT SIGN BULB INOP. SECURED BULB IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 63,485 hrs · 37,163 cycles

EMERGENCY EXIT SIGN IN CEILING AT OVERWING EXITS LOOSE. R&R SIGN IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,485 hrs · 37,163 cycles

EMERGENCY LIGHTS INOP AT M1674. R&R BATTERY PACK IAW AMM.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 63,485 hrs · 37,163 cycles

RIGHT WING; AFT #7 FLAP TRACK FAIRING; FWD ATTACH BOLT O/B ACCESS COVER; PANEL 643CR; CRACKED AT FASTENER HOLE. / REMOVED + REPLACED AFT #7 FLAP TRACK FAIRING O/B ACCESS PANEL 643CR IAW B737 AMM 27-51-28-400-804 ATAGS:A22137

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO SUPPORT ANGLE CRACKED AT BS 867, RBL 20. R&R ANGLE IAW EA.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

PASSANGER CABIN. FLOOR PANEL 231XF HAS MISSING FIBERS ON UPPER FACE SHEET IN MULTIPLE LOCATIONS. / FABRICATED NEW FLOORBOARD USING EXISTING BOARD 231XF AS TEMPLATE IAW SRM 53-00-50-2R-0 PAR 1 A NOTE AND 4A REV 65; BOEING DRAWING NUMBER 144A5810 ID: 126+0009 REV:- FLOORBOARD (WN5366); INSERTS 80(A83334); EPIBOARD 420 (A95390)

Part: LIGHT — CRACKED (CABIN) · airframe 63,485 hrs · 37,163 cycles

G1 GALLEY EMERGENCY EXIT LIGHT ASSEMBLY CRACKED AT MOUNT POINTS. R&R LIGHT ASSEMBLY IAW CMM AND AMM.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 63,485 hrs · 37,163 cycles

VERTICAL STAB LEADING EDGE. LEADING EDGE RIB IS CRACKED AT FASTNER HOLE ON RH SIDE AT LEADING EDGE STA 297.5 (MARKED) / REMOVED AND REPLACED RIB A VERTICAL STAB LEADING EDGE STA 297.5 PN 176A1410-11 IAW SRM 51-40-020-0G-0 AND DWG 176A1001 REV C

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

PASS CABIN. FLOOR PANEL 232SF UPPER FACE SHEET HAS MISSING FIBERS RUNNING FROM FWD END TO AFT END IN MULTIPLE AREAS / FABRICATED NEW FLOORBOARD 232SF USING EXISTING FLOORBOARD AS TEMPLATE IAW SRM 53-00-50-2R-0 PAR 1.A NOTE REV 65; BOEING DWG 144A5810 ID:0014 REV -FLOORBOARD (WN 5366); INSERTS (A83334) ; EPIBOND 420 (A95390)

Part: ANGLE — CRACKED (LT WING) · airframe 63,485 hrs · 37,163 cycles

LT WING TRAILING EDGE INBOARD DEFLECTOR RIB, UPPER FIXED PANEL, MID VERTICAL INTERCOSTAL, ANGLE CRACKED. R&R ANGLE IAW DWG AND SRM.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 63,485 hrs · 37,163 cycles

FWD CARGO BAFFLE AND CLIP BETWEEN STA 400-420 IS CRACKED AND BENT / REMOVED AND REPLACED FWD CARGO BAFFLE + CLIP BETWEEN STA 400-420 IAW 737-700 SRM 51-40-02-00 + DWG 143A1505 REV B. APPLIED CIC TO BAFFLE + CLIP IAW 737-700 AMM 51-21-41-620-802

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

FORWARD CARGO BAFFLE CLIP CRACKED AT BS 500C, LBL 25. R&R CLIP IAW SRM & DWG.

Part: SKIN — DENTED (AFT CARGO COMPT) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO DOOR LOWER FWD CORNER HAS MULTIPLE SMALL DENTS IN LARGE DENT / EVALUATED AFT CARGO DOOR LOWER FWD CORNER IAW B737 SRM 52-30-01-1A-1. OUT OF LIMITS. NO DAMAGE ALLOWED IN DENT. MULTIPLE DENTS IN LARGE DENT. REPAIRED AREA IAW EA 180463 REV A AND SWA EA 1-752-4197 REV 1 REMOVABLE COMPONENT P/N 146A6110-20 S/N 000666

Part: PANEL — CORRODED (NLG WHEEL WELL) · airframe 63,485 hrs · 37,163 cycles

NOSE WHEEL WELL PANEL 113AC HAS CORROSION ON THE INSIDE FLANGE SURFACE AROUND FASTENER HOLES AS MARKED. / REMOVED CORROSION ON NOSE WHEEL PANEL 113AC INSIDE FLANGE DEEPEST BLEND AREA WAS .004 MATERIAL LOSS. SRM HAS NO LIMITS IN THIS AREA REPAIRED IAW AAR EA 180462 IR AND SWA EA 1-753-33199 REV IR

Part: PANEL — CORRODED (NLG WHEEL WELL) · airframe 63,485 hrs · 37,163 cycles

NOSE WHEEL WELL PANEL 113BW HAS CORROSION ON THE INSIDE FLANGE SURFACE AROUND FASTENER HOLES AS MARKED. / REMOVED CORROSION BY BLENDING ON NOSE WHEEL WELL PNL 113BW INSIDE FLANGE IAW B737 SRM 51-10-02-0G-0. ACCOMPLISHED EA 180461 REV P1 & IR & SWA EA 1-753-33200 REV IR

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

POWER RECEPTACLE DOOR CUTOUT FORWARD LOWER CORNER INTERNAL DOUBLER CRACKED. REPAIRED DOUBLER IAW EA.

Part: PANEL — CRACKED (SLAT) · airframe 63,485 hrs · 37,163 cycles

RIGHT WING #6 SLAT; COVE PANEL (623DB) AT ACTUATOR IS CRACKED. / REMOVED FABRICATED AND REINSTALLED NEW RIGHT WING #6 SLAT; COVER PANEL (623DB) AT ACTUATOR. NEW PANEL FABRICATED IN BACKSHOP ON WORK ORDER 38038 6000 0001; IAW DWG 114A8131 REV B. ANODIZED ON VENDOR WORK ORDER 760174 412001 IAW DRW 114A8131 REV B. PRIMED AND TOP COATED IAW AMM 51-21-72-370-801AND 51-21-3-370-803 X

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

FOUND EXTERNAL FUSELAGE SKIN CORRODED BETWEEN BS 500A TO BS 500B. REMOVED SKIN IAW SRM & EA.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT BETWEEN STA 787 AND 827 AND BETWEEN STR 25R AND 26R FLOOR STRAP (LOWER) HAS CORROSION ON LOWER SIDE AROUND NUTPLATES IN SEVERAL PLACES. / REMOVED AND EVALUATED CORROSION . ORIGINAL THICKNESS .180' ;OSS OF .028' WITH .152 REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED -2 STRAP PER DWG 146A8120 REV A AND SRM 51-40-02-0G-0

Part: LIGHT — MISSING (CABIN) · airframe 63,485 hrs · 37,163 cycles

AFT OVERHEAD CEILING PANEL EMERGENCY EXIT LIGHT FASTENER MISSING. R&R LIGHT IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,485 hrs · 37,163 cycles

PASSENGER CABIN FLOORBOARD 221 BF PREVIOUS REPAIR IS DELAMED / REPAIRED DAMAGE ON FLOOR PANEL 221BF. BONDED PAIR REPAIR PLIES AND CURED. INSTALLED 1EA INSERT IAW B737-700 SRM 53-00-50-2R-0; SRM 53-00-50-2R-1 TAP TEST GOOD.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,485 hrs · 37,163 cycles

PASSENGER CABIN FLOORBOARD 221 GF HAS DELAMED CORNER / REPAIRED DAMAGE ON FLOOR PANEL 221GF. BONDED REPAIR PLIES AND CURED. INSTALLED 1EA INSERT IAW B737-700 SRM 53-00-50-2R-0; SRM 53-00-50-2R-1 TAP TEST GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

INTERCOSTAL CORRODED AT BS 335, STR 23L. R&R INTERCOSTAL IAW SRM & DWG.

Part: FITTING — CORRODED (GIRT BAR) · airframe 63,485 hrs · 37,163 cycles

R2 DOOR GIRT BAR FITTING CORRODED. R&R FITTING IAW AMM.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 63,485 hrs · 37,163 cycles

PASSENGER CABIN FLOORBOARD 241 AAF HAS DAMAGED INSERTS / REPAIRED 4 PUNCTURE AND 1 CRACK ON PANEL 241 AAF IAW SRM 53-00-50-2R-2. REPLACED 2 CORRODED INSERTS IAW SRM 5-00-50-2R-0 PARA 55.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

INTERCOSTAL CORRODED BETWEEN BS 312 TO BS 320, STR 23L. R&R INTERCOSTAL IAW SRM & DWG.

Part: ANGLE — CRACKED (FWD CARGO THRESH) · airframe 63,485 hrs · 37,163 cycles

WHILE DISPLACING WEB FOR ACCESS FOUND FWD CARGO UPPER MAIN SILL WEB AFT ATTACH ANGLE CRACKED. / REMOVED AND REPLACED FWD CARGO UPPER MAIN SILL WEB AFT ATTACH ANGLE IAW AAR EA 180452 REV IR STEPS 1-6; SWA EA 1-753-33176 REV IR STEPS 1-2.

Part: PLATE — CRACKED (RIGHT WING) · airframe 63,485 hrs · 37,163 cycles

RIGHT WING TRAILING EDGE; UNDER PANEL #651GB; INBOARD OF PYLON SAIL TAIL; WAFFLE PLATE COMMON TO LOWER REAR SPAR CHORD IS CRACKED WITH 2EA FASTENERS SHEARED. / REMOVED AND REPLACED WAFFLE PLATE COMMON TO LOWER REAR SPAR CHORD RH WING TRAILING EDGE UNDER PANEL #651GB INBD OF PYLON SILT TAIL PN 115A2781-14 IAW SRM 51-40-02-0G-0 AND DWG 115A2781 REV B ATAG WN3853

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT BETWEEN STA 867 AND 847 AFT FLOOR SHIELD IS CORRODED 2 EA AREAS AS MARKED TOP AND BOTTOM SIDES / REMOVED AND REPLACED AFT CARGO COMP BETWEEN STA 867-847 AFT FLOOR SHEILD WITH ATAG WN6505 IAW SRM 51-40-02 AND DWG 146A0081 REVA

Part: TRACK — CORRODED (AFT CARGO COMPT) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT BETWEEN STA 927 AND 947.5 AND BETWEEN STR 26R AND 25R FLOOR TRACK IS CORRODED TOP SURFACE AROUND 5 EA FASTENER NUT PLATE HOLES / REMOVED AND EVALUATED CORROSION. ORIGINAL THICKNESS .073' LOSS OF .012' WITH .061' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED -14 CARGO TRACK STA 947 TO FACTORY SPLICE AT STA 887 PER DWG 147A501 REV B AND SRM 51-40-02-0G-0

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

INTERCOSTAL CORRODED BETWEEN BS 300 TO BS 312, STR 23L. R&R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

INTERCOSTAL CORRODED BETWEEN BS 322 TO BS 328, STR 23L. R&R INTERCOSTAL IAW SRM & DWG.

Part: TRACK — CORRODED (AFT CARGO COMPT) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT BETWEEN STA 927 AND 947.5 AND BETWEEN STR 27L AND 27R FLOOR TRACK IS CORRODED TOP SURFACE AROUND 5 EA FASTENER NUT PLATE HOLES / REMOVED AND EVALUATED CORROSION ORIGINAL MATERIAL .073' LOSS OF .014' REMAINING .059'; BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED CARGO TRACH STA 947 TO FACTORY SPLICE AT STA 887 PER DWG 147A7501 REV B

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED AT BS 847, BETWEEN STR 26R TO STR 25R. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT SHROUD SUPPORT BRACKET CRACKED AT BS 727, STR 27R. R&R BRACKET PER SRM AND DWG.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT BETWEEN STA 727 AND 767 R/H Z ANGLE IS CORRODED TOP AND BOTTOM SURFACES IN SEVERAL AREAS / REMOVED CORROSION FOUND 100% MATERIAL OSS. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED Z-ANGLE STA 727 TO 767 PER DWG 146A7500 REV C; AND SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CORRODED (AFT CARGO COMPT) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT BETWEEN STA 767 AND 787 STR 27R AREA INTERCOSTAL IS CORRODED AS MARKED / REMOVED AND REPLACED INTERCOSTAL IN AFT CARGO PIT BETWEEN STA 767-787 STR 27R IAW SRM 5140-02 AND DWG 146A8130 REV B WITH BACKSHOP W/O 38038/1600/0002.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT FRAME CRACKED AT BS 947.5, STR 26L. R&R FITTING PER AIPC AND SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT LT Z ANGLE CORRODED BETWEEN BS 727 TO BS 847. R&R Z-ANGLE PER DWG AND SRM.

Part: INTERCOSTAL — CORRODED (LOWER INT FUSELA) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT BETWEEN STA 927 AND 907 AND STR 27R AND 25R POTABLE WATER PAN SUPPORT INTERCOSTAL IS CORRODED AROUND SEVERAL FASTENERS / REMOVED AND EVALUATED CORROSION ORIGINAL .040' LOSS OF .006' WITH .034' REMAINING BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED STIFFENER PER SRM 51-40-02-0G-0 AND AIPC 52-49-00-02

Part: INTERCOSTAL — CORRODED (AFT CARGO COMPT) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT BETWEEN STA 787 AND 767 AND BETWEEN STR 25R AND 26R INTERCOSTAL WEB IS CORRODED UNDER FWD FLOOR STRUCTURE SHIELD / REMOVED AND EVALUATED CORROSION FOUND 100% MATERIAL LOSS BLENDED FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED -8 INTERCOSTAL PER DWG 146A8123 REV A AND SRM 51-40-02-0G-0

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT BETWEEN STA 793 AND 767 FWD FLOOR SHIELD IS CORRODED TOP AND BOTTOM SURFACES AS MARKED / REMOVED AND REPLACED AFT CARGO COMP BETWEEN 793 AND 767 FWD FLOOR SHIELD WITH ATAG WN2907 IAW SRM 51-40-02 AND DWG 146A0081 REV A

Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT UNDER LOWER DOOR TRESHOLD PLATE; WEB IS CORRODED IN SEVERAL AREAS TOP SURFACE AS MARKED BETWEEN STA 793 AND 847 / REMOVED AND REPLACED AFT CARGO COMP UNDER LOWER DOOR THRESHOLD PLATE; WEB WITH ATAG A44661 IAW SRM 51-40-02 AND DWG 146A8170 REV A.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

L1 DOOR MOST INBOARD THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 312 TO BS 344. R&R ANGLE IAW SRM AND DWG.

Part: SKIN — CORRODED (LH PYLON) · airframe 63,485 hrs · 37,163 cycles

#1 ENGINE STRUT BOX/ PYLON ACCESS THROUGH PNL# 431DR; PYLON STRUCTURE IS CORRODED IN SEVERAL AREAS AS MARKED / REMOVED CORROSION ON #1 ENGINE STRUTBOX PYLON SKIN UNDERNEATH ACCESS PANEL 431DR. VERIFIED MATERIAL LOSS IN DEEPEST AREA. ORIGINAL THICKNESS IS .135 MATERIAL LOSS OF .035. REMAINING .100. OUT OF LIMITS IAW SRM 54-50-70-1A-1 REPAIRED IAW AAR EA 180458 IR AND SWA EA 1-754-2329 REV IR

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

R2 CREASE BEAM CORRODED BETWEEN BS 992+6 TO BS 951. R&R CREASE BEAM IAW SRM.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,485 hrs · 37,163 cycles

PASSENGER COMPARTMENT FWD WET AREA BETWEEN STA 360 AND 344 RBL 14 AREA INTERCOSTAL IS CRACKED AS MARKED / REMOVED & REPLACED INTERCOSTAL BETWEEN STA 344-360 RBL 14 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; DWG 11A5400 SHT 13 REV -

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

L2 CREASE BEAM CORRODED BETWEEN BS 957 TO BS 986. R&R CREASE BEAM IAW SRM & DWG.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 63,485 hrs · 37,163 cycles

AFT BULKHEAD TOP CHORD ANGLE CRACKED AT BS 663, LBL 8. R&R ANGLE IAW EA.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,485 hrs · 37,163 cycles

PASSENGER COMPARTMENT FWD WET AREA BETWEEN STA 312 AND 328 LBL 44 AREA INTERCOSTAL IS CRACKED AS MARKED / REMOVED AND REPLACED PAX COMPARTMENT FWD WET AREA BETWEEN STA 312 AND 328 LBL 64 AREA INTERCOSTAL IAW SRM 51-40-02-060 & BOEING DWG NO 141A5400 ID 0026 REV:-

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,485 hrs · 37,163 cycles

PASSENGER COMPARTMENT FWD WET AREA BETWEEN STA 328 AND 344 LBL 44 AREA INTERCOSTAL IS CRACKED AS MARKED / REMOVED AND REPLACED PAX COMPARTMENT FWD WET AREA BETWEEN STA 328 AND 344 LRL44 AREA INTERCOSTAL IAW SRM 51-40-02-0G0 AND BOEING DWG # 141A400 REV:- ID0001

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

LT CREASE BEAM CHORD CRACKED AT BS 301. R&R CREASE BEAM IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

MAIN CABIN FLOORBEAM CORRODED AT BS 967, RBL 28. R&R FLOORBEAM IAW SRM & EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

RT CREASE BEAM CHORD INBOARD SIDE SUPPORT STRAP CORRODED BETWEEN BS 291 TO BS 301. R&R STRAP IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,485 hrs · 37,163 cycles

PASSENGER COMPARTMENT FWD WET AREA BETWEEN STA 312 AND 328 RBL 31 INTERCOSTAL IS CRACKED / CABIN FLOOR CRACKED INTERCOSTAL BETWEEN STA 312 AD STA 328 RBL 31'. REMOVED CRACKED INTERCOSTAL I/A/W SRM 51-40-02-0G-0. LOCATED; DRILLED; AND INSTALLED NEW INTERCOSTAL WEB I/A/W SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND BOEING DWG 141A5400 REV: - . CIC AREA I/A/W AMM 51-21-91-620-802.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,485 hrs · 37,163 cycles

PASSENGER COMPARTMENT FWD WET AREA BETWEEN STA 360 AND 344 RBL 2 AREA INTERCOSTAL IS CRACKED AS MARKED / REMOVED AND REPLACED INTERCOSTAL AT CABIN STA 360 TO 344 RBL 2 PN 141A5410-23 IAW DWG 141A5400 REV- AND SRM 51-4-02-0G-0 ATAG WN7734

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,485 hrs · 37,163 cycles

PASSENGER COMPARTMENT FWD WET AREA BETWEEN STA 294.5 AND 277.5 RBL 2 AREA INTERCOSTAL IS CRACKED AS MARKED / REMOVED & REPLACED INTERCOSTAL BETWEEN 277 & 294 EA SRM 51-40-05-0G-0 + SRM 51-40-02-0G-0G-0 & DMG 141A 5400 5H & 20 REV

Part: ANGLE — CORRODED (FWD CARGO LH) · airframe 63,485 hrs · 37,163 cycles

FWD CARGO; LH Z-ANGLE HAS CORROSION AT STA 500B TO 500D / REMOVED CORROSION ON LH Z ANGLE AT STA 500B TO 500D IAW 737-700 SRM 51-10-02-0G-0 BLEND FOUND OUT OF LIMITS WITH 100% MATERIAL LOSS PER SRM 53-00-53-1A-2 LH Z ANGLE REMOVED AND REPLACED FROM STA 400 TO 500D ON NON ROUTINE NO.X799671

Part: ANGLE — CORRODED (FWD CARGO LH) · airframe 63,485 hrs · 37,163 cycles

FWD CARGO; LOWER CURVED BULKHEAD SUPPORT ANGLE HAS CORROSION AT STA 500D STR 26L / REMOVED CORROSION PER SRM 51-10-02-0G-0 INSPECTED WITH 10X MAGNIFIED NO FURTHER DAMAGE FOUND BLEND DIMENSIONS 1'X1' WITH MAX DEPTH OF .010' FROM ORIGINAL MAT. .071' .061' MAT REMAINING BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 AAR TOOL 36649 DUE 05AUG19. REMOVED AND REPLACED LOWER CURVED BULKHEAD ANGLE SUPPORT AT STA 500D STR 26L IAW B737-700 SRM 51-40-05-0G-0; 51-40-02-0G-0+ 25-52-19-420-001

Part: DOUBLER — CORRODED (FWD FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

FWD CARGO; AIRPHONE DOUBLER BETWEEN STA 500A TO 500B; BL0 HAS CORROSION ON UPPER SURFACE WITH EVIDENCE OF CORROSION BETWEEN FUSELAGE SKIN AND AIRPHONE DOUBLER. ( DOUBLE BULGING FROM SKIN) / REMOVED AIRPHONE DOUBLER BETWEEN STA 500A - 500B BL0; LOCATED; DRILLED AND INSTALLED NEW PART IAW B737-700 SRM 71-40-02-0G-0; 51-40-05-0G-0 DWG:143A3230 REV:A P/N 143A3233-4. A TAG# WN8329.

Part: ANGLE — CORRODED (FWD CARGO COMPT) · airframe 63,485 hrs · 37,163 cycles

FWD CARGO; LOWER BULKHEAD SUPPORT ANGLE HAS CORROSION ON HORIZONTAL AND VERTICAL FLANGE AT STA 500D; STR 26R TO 26L / REMOVED CORROSION IAW SRM 51-10-02-06-0 INSPECTED WITH 10X. BLENDED DIMENSIONS 1'X2' ITH DEPTH OF .036' FROM ORIGINAL .071' .035' REMAINING FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-. REMOVED AND REPLACED FWD CARGO LOWER BULKHEAD SUPPORT ANGLE AT STA 500D IAW 737-700 SRM 51-40-07-02-0G-0& DWG 143A0485 REV B.

Part: SHIELD — CORRODED (FWD CARGO RH) · airframe 63,485 hrs · 37,163 cycles

FWD CARGO; RH SPLASH SHIELD HAS CORROSION FROM STA 420 TO 440 / FWD CARGO R/H SPLASH SHEILD REPLACED OM NR CARD 38036 1400/0054 SWA X799669

Part: FLOOR PANEL — CRACKED (AFT CARGO COMPT) · airframe 63,485 hrs · 37,163 cycles

AFT CARGO COMPARTMENT FLOOR PNL# 140CF HAS A CRACK IN THE BASE OF A DENT / LOCATED AND DRILLED NEW AFT CAROG COMPARTMENT FLOOR PNL # 140CF AND FABRICATED WITH A TAG A98893 IAW SRM 51-40-05 AND BOEING DWG 453A2610 REV D.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

FORWARD CARGO UPPER DOOR SILL WEB, UPPER SURFACE CORRODED BETWEEN BS 480 TO BS 280+3. REPAIRED WEB IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

FORWARD CARGO LT Z-ANGLE CORRODED ON UPPER SURFACE BETWEEN BS 400 TO BS 420. R&R Z ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 63,485 hrs · 37,163 cycles

RT WING FIXED TRAILING EDGE PANEL SUPPORT ANGLE CRACKED. R&R ANGLE IAW DWG & SRM.

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 63,485 hrs · 37,163 cycles

FWD CARGO BAY FLOOR PNL #120BF HAS CORROSION ON TOP SKIN SURFACE THE LENGTH OF PNL CORNER EDGE AS MARKED / RECIEVED NEW FWD CARGO BAY FLOOR PNL 120BF REPLACEMENT. PN 453A1610-4/7570679 TAG #WN6090 VERIFIED IAW AIPC 25-52-10-01 PG 20.

Part: BEAM — CRACKED (R1 DOOR) · airframe 63,485 hrs · 37,163 cycles

R1 DOOR NR 4 BEAM CRACKED AT FORWARD ATTACHMENT POINT TO HANDLE BOX. R&R NR 4 BEAM IAW DWG AND SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 63,485 hrs · 37,163 cycles

FWD CARGO BAY LOWER DOOR CUTOUT; CENTER TRESHOLD PLATE IS CRACKED IN BASE OF LARGE DENT / RECEIVED NEW FWD CARO BAY LOWER DOOR CUTOUT ; CENTER THRESHOLD PLATE REPLACEMENT VERIFIED P/N 143A8333-8/7530099 TAG # LP1053 IAW 737-700 AIPC 53-13-00-008.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

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

Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 63,485 hrs · 37,163 cycles

FWD CARGO; LOWER SILL WEB IS CORRODED FROM STA 440 TO 490 / BLENDED REMOVED CORROSION LOSS OF 100% FOUND TO BE OUT OF LIMITS LOCATED DRILLED NEW SILL WEB @FWD CARGO DOOR OPENING AND INSTALLED I.A.W. B737 SRM 53-30-15-1A-1 AND SRM 51-40-02-0G-0 ATAGE #A94597

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,485 hrs · 37,163 cycles

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

Part: SCUFF PLATE — BROKEN (FWD CARGO THRESH) · airframe 63,485 hrs · 37,163 cycles

FWD CARGO AFT CORNER SCUFF BROKEN. / REPLACED FWD CARGO AFT CORNED SCUFF IAW AIPC 53-13-00-08 & SRM 51-40-05-0G-0.

Part: FLOOR PANEL — CRUSHED (CABIN) · airframe 63,485 hrs · 37,163 cycles

PASSENGER CABIN FLOOR BOARD 231YF IS CRUSHED AT FORWARD INBOARD CORNER / REPAIRED PASSENGER CABIN FLOORBOARD 231YF AS MARKED I/A/W SRM 53-00-50-2R-4 REV 65; SRM 53-00-50-2R-0 REV 65

Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 63,485 hrs · 37,163 cycles

FWD CARGO RH Z-ANGLE IS CORRODED FROM STA 500A TO 500B / REMOVED AND REPLACED FWD CARGO RH Z-ANGLE FROM STA 500A TO 500D IAW B737-700 SRM 51-40-02 PG 13 AND DWG 143A7501/REV H. REMOVED CORROSION IAW SRM 51-10-02-0G-0. REMOVED .010' MATERIAL ORIG MAT .040' MAT REMAINING. .030' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-IA-2 APPLIED CIC IAW 737-700 SRM 51-20-01-0G-0.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,485 hrs · 37,163 cycles

RT WING NR 5 SLAT LOWER NOSE SKIN AT ACTUATOR ATTACH POINT CRACKED AT FASTENER. REPAIRED SKIN IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 63,485 hrs · 37,163 cycles

G1 GALLEY CLOSE OUT PANEL EMERGENCY EXIT LIGHT HOUSING LENS BROKEN. R&R LENS IAW CMM.

Part: SKIN — CRACKED (SLAT) · airframe 63,485 hrs · 37,163 cycles

LEFT WING #2 SLAT; LOWER NOSE SKIN AT ACTUATOR ATTACH POINT IS CRACKED AT FASTENER. / REPAIRED CRACKED L/H WING #2 SLAT LOWER NOSE SKIN I/A/W B737-700 SRM 57-42-01-2R-8

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 62,076 hrs · 36,275 cycles

FORWARD EMERGENCY EXIT LIGHT LENS BROKEN. R & R THE LENS IAW AMM.

Part: FLOORBEAM — CORRODED (AFT CARGO BAY) · airframe 61,632 hrs · 35,989 cycles

CARGO TRACK AT 13.8 RBL IS CORRODED STA 794-STA 847 / R & R AFT CARGO BAY TRACK AT 13.8 RBL FROM STA 779.5 -887 PER SRM 530-00-53-2R-3R REPAIR 3 & EA 1-A53-8210 REV 5 779.5 (CATEGORY A REPAIR; NO OTHER ACTIONS ARE NECESSARY) SEE SAM 326 A1045745

Part: TRANSITION PANEL — CORRODED (AFT CARGO BAY) · airframe 61,632 hrs · 35,989 cycles

CARGO FLOOR TRANSITIUON STRIP IS CORRODED AT STA 887; 9 LBL- 21.5 RBL / R & R CARGO FLOOR TRANSITION STRIP AT STATION 887 PER SRM 51-40-02 AND SRM 51-40-10

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 60,614 hrs · 35,346 cycles

(CUT OUT) PANEL 193AL HAS DELAMINATION ON FWD EDGE OF PANEL / SEE SA-M 326 FOR PANEL REPAIR SIGN OFF

Part: ANGLE — CRACKED (WHEEL WELL RH) · airframe 60,614 hrs · 35,346 cycles

'L' ANGLE ON 663. 75 BLO APROX 26.5 INCHES FROM CENTER RH SIDE CRACKED APROX 3.5 INCHES LOCATED OUT BOARD SIDE OF AC PAC EXAUST / RMEOVED & REPLACED ANGLA PER SRM 51-40-02

Part: WEB — CRACKED (WHEEL WELL RH) · airframe 60,614 hrs · 35,346 cycles

VAPOR BARRIER IS CRACKED @ AFT SPAR WEB 663.75 BLO 663.75 BLO APROX 26.5 INCHES FROM CENTER R/H SIDE. / APPLIED INTERIM PATCH REPAIR IAW SRM 57-10-10-2R-2 REPAI 2 OPTION C. CRACK LOCATION RBL 26.5-29.5 AND 14.5 IN LONG.

Part: ANGLE — CRACKED (WHEEL WELL LH) · airframe 60,614 hrs · 35,346 cycles

'L'ANGLE ON 663.75 BLO APROX 26.5 INCHES FROM CENTER LH SIDE CRACKED APROX 2 INCHES LOCATED OUTBOURD SIDE OF AC PAC EXAUST / REMOVED & REPLACED ANGLE PER SRM 51-40-02

Part: CONTAINER — LOOSE (L2 DOOR) · airframe 60,139 hrs · 35,035 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. R&R SLIDE CONTAINER PER MT.

Part: COVER — MISSING (EXIT SIGN) · airframe 59,605 hrs · 34,724 cycles

RT OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 57,981 hrs · 33,758 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R&R SLIDE PER AMM & MT.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,233 hrs · 33,326 cycles

OVERWING EXIT SIDEWALL EXIT LIGHT INOPERATIVE. R & R THE FUSE IAW AMM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,233 hrs · 33,326 cycles

LEFT OVER WING EXIT SIDEWALL LOWER LIGHT INOPERATIVE. R & R THE FUSE IAW AMM.

Part: FRAME — CRACKED (BS 663) · airframe 57,233 hrs · 33,326 cycles

RIGHT A/C BAY UPPER BULKHEAD FRAME CRACKED AT BS 663, RBL 8. REPAIRED THE FRAME IAW ER AND EA.

Part: BATTERY — FAILED (CABIN) · airframe 55,615 hrs · 32,379 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 55,615 hrs · 32,379 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 55,615 hrs · 32,379 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 55,615 hrs · 32,379 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 55,615 hrs · 32,379 cycles

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

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 54,590 hrs · 31,782 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STATION 147. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 54,590 hrs · 31,782 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED AT STATION 147. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,517 hrs · 31,739 cycles

RIGHT BULLNOSE EMER EXIT LIGHT INOPERATIVE AT ROW 16. RELAMPED LIGHT IAW AMM.

Part: FIRE LOOP — FAULTY (CABIN) · airframe 52,981 hrs · 30,847 cycles

DIVERSION, DECLARED EMER. INTERMITTENT WW WARNING LIGHT, ON P8 PANEL, ILLUMINATED INFLIGHT & THE MASTER CAUTION & FIRE WARNING LIGHTS. R & R WW FIRE LOOP IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,564 hrs · 29,454 cycles

LEFT WING OTBD AFT FLAP DELAMINATED AT TE. R & R AFT FLAP ASSEMBLY IAW MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,563 hrs · 29,454 cycles

AFT CARGO FLOORBEAM CORRODED BETWEEN BS 794.5 TO 847 RBL 13.8. REPAIRED BEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,563 hrs · 29,454 cycles

AFT SEAT TRACK INBD & OTBD FLANGES CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW ACO & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,564 hrs · 29,454 cycles

CABIN FLOORBEAM FITTING CRACKED AT STATION 727B RBL 45.5. R & R FITTING IAW SRM & ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,563 hrs · 29,454 cycles

AFT SEAT TRACK INBD & OTBD FLANGES CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,563 hrs · 29,454 cycles

RIGHT NR 3 WINDOW FRAME 2ND HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,563 hrs · 29,454 cycles

LEFT NR 3 WINDOW FRAME 2ND HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,564 hrs · 29,454 cycles

RIGHT COCKPIT NR 1 WINDOW POST CRACKED. REPAIRED POST IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,563 hrs · 29,454 cycles

RIGHT HORIZONTAL STABILIZER SKIN CRACKED AT STAB STATION 101.9, 19.75 INCHES FROM TE. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,563 hrs · 29,454 cycles

RIGHT HORIZONTAL STABILIZER SKIN CRACKED AT STAB STATION 101.9, 11.25 INCHES FROM TE. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 48,717 hrs · 28,349 cycles

NUMBER 6 LE SLAT LOWER SKIN CRACKED AT ACTUATOR CUT OUT. REPAIRED SKIN IAW SRM.

Part: TRANSMITTER — FAULTY (E&E BAY) · airframe 47,338 hrs · 27,560 cycles

DECLARED EMERGENCY WITH FLAP HANDLE AT 5, FLAPS STOPPED AT LESS THAN 1, LE FLAP TRANSIT LIGHT ILLUMINATED, NO ROLL TENDENCY. USED ALT FLAP EXTENSION TO FLAPS 15 POSITION. LE FLAP TRANSIT LIGHT OUT, LANDED FLAPS 15. R & R LT FLAP POSITION TRANSMITTER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,288 hrs · 26,348 cycles

CABIN AFT GALLEY OVERHEAD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 43,662 hrs · 25,374 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT LOWER END OF 1ST VERTICAL STIFFENER AFT AT STA 101.90. REPAIRED RIB PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,662 hrs · 25,374 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 96 TO STA 98. REPAIRED SKIN PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 43,662 hrs · 25,374 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT LOWER END OF 2ND AND 3RD VERTICAL RIBS AFT STAB STA 92.7. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 43,662 hrs · 25,374 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.3. REPAIRED RIB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,662 hrs · 25,374 cycles

SKIN CRACKED BETWEEN BS 663 TO BS 887, BETWEEN STR 4L TO STR 4R. REPAIRED SKIN IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,662 hrs · 25,374 cycles

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

Part: FITTING — CORRODED (L1 DOOR) · airframe 43,662 hrs · 25,374 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED AT BS 343, LBL 59. REMOVED AND REPLACED FITTING IAW SOPM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,662 hrs · 25,374 cycles

CREASE BEAM CORRODED AT BS 299, RBL 56. REMOVED AND REPLACED BEAM IAW SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 43,662 hrs · 25,374 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED AT BS 312, LBL 56. REMOVED AND REPLACED FITTING IAW SOPM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,662 hrs · 25,374 cycles

FLOORBEAM CORRODED AT BS 328, LBL 51. REPAIRED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,662 hrs · 25,374 cycles

CREASE BEAM CORRODED AT BS 327, RBL 60. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,662 hrs · 25,374 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986, BETWEEN RBL 45 TO LBL 45. REPAIRED CHORD PER SRM AND EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,662 hrs · 25,374 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED JUST FWD OF AFT SPAR BETWEEN STA 125 TO STA 126.2. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,662 hrs · 25,374 cycles

LOWER BULKHEAD CRACKED AT BS 663, RBL 12. REPAIRED BULKHEAD PER EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,662 hrs · 25,374 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,662 hrs · 25,374 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED JUST I/B OF RIB AT STATION 147.9. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 43,662 hrs · 25,374 cycles

NR 1 COCKPIT WINDOW FRAME CRACKED AT UPPER O/B CORNER. REPAIRED FRAME IAW ER AND EA.

Part: SLIDE — OUT OF LIMITS (L1 DOOR) · airframe 43,425 hrs · 25,212 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — BROKEN (CABIN) · airframe 40,404 hrs · 23,421 cycles

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

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 40,092 hrs · 23,230 cycles

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

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,649 hrs · 21,230 cycles

DURING SCHEDULED 10Y CHECK, FOUND INTERCOSTAL CORRODED BETWEEN BS 260 TO BS 270, BL 0. REMOVED AND REPLACED INTERCOSTAL PER SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,649 hrs · 21,230 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 270, BETWEEN LBL 6 TO RBL 6. REMOVED AND REPLACED FLOOR SUPPORT PER SRM AND EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,640 hrs · 20,645 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,640 hrs · 20,645 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,563 hrs · 20,598 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP AT ROW 11. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,421 hrs · 19,906 cycles

DURING SCHEDULED CV CHECK, FOUND LT AFT BULLNOSE EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 34,421 hrs · 19,906 cycles

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

Part: BRACKET — LOOSE (GIRT BAR) · airframe 34,180 hrs · 19,755 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER BRACKET LOOSE. SECURED BRACKET PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 33,417 hrs · 19,291 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 32,754 hrs · 18,872 cycles

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

Part: GASPER FAN — FAULTY (CABIN) · airframe 30,815 hrs · 17,696 cycles

AIR TURNBACK/DECLARED EMERGENCY. FLIGHT ATTENDANTS REPORTED STRONG "SMOKY ACID" TYPE SMELL IN CABIN, WORSE IN AFT CABIN. SUBSIDED WHEN GASPER AND RECIRC FANS TURNED OFF, SMELL CONTINUED IN CABIN, NO VISIBLE. WILL REPLACED GASPER FAN PER MM.

Part: LENS — LOOSE (CABIN) · airframe 30,143 hrs · 17,275 cycles

DURING SCHEDULED 8Y CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT FWD LAV. SECURED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 30,143 hrs · 17,275 cycles

DURING SCHEDULED 8Y CHECK, FOUND EMERGENCY EXIT LIGHT LENS COVER LOOSE AT AFT GALLEY. SECURED COVER PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 30,143 hrs · 17,275 cycles

DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CHORD CORRODED AT BETWEEN BS 291 TO BS 328, RBL 54. REMOVED AND REPLACED BEAM PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 24,936 hrs · 14,123 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 24,902 hrs · 14,104 cycles

DECLARED EMERGENCY, AT FL 410 ENGINE DRIVEN HYDRAULIC -B- SYSTEM LIGHT ILLUMINATED, -B- SYSTEM INDICATES ZERO. INSPECTED HYDRAULIC SYSTEM FOUND -B- SYSTEM ELECTRIC PUMP LEAKING. REMOVED AND REPLACED ELECTRIC PUMP AND CASE DRAIN FILTERS PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 21,374 hrs · 12,098 cycles

DURING SCHEDULED HC2 CHECK, ALL EMERGENCY EXIT BATTERY PACKS FAILED TIMED TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,736 hrs · 11,151 cycles

DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 19,249 hrs · 10,894 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED EXIT LIGHT ASSY IAW MM.

Part: COMBUST CHAMBER — CRACKED (NR 1 ENGINE) · airframe 18,976 hrs · 10,739 cycles

DURING SCHEDULED HC1 CHECK, FOUND NR 1 ENGINE, NR 8 FUEL NOZZLE BELOW IGNITER HOLE SECONDARY SWIRL NOZZLE VENTURI AREA OF MATERIAL CRACKED AND MISSING. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 18,976 hrs · 10,739 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 14 ABC. INSTALLED COVER PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 18,894 hrs · 10,691 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 16,314 hrs · 9,278 cycles

EEPLS OUT OF ADJUST ON LT SIDE AT ROW 8. REINSTALLED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 13,795 hrs · 7,786 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 13,743 hrs · 7,757 cycles

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

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 13,551 hrs · 7,653 cycles

AIR TURNBACK, ON TAKEOFF WITH FLAP RETRACTION L/E FLAPS TRANSIT LIGHT REMAINED ILLUMINATED WITH T/E FLAPS UP. CONFIRMED PARTIALLY EXTENDED. REMOVED AND REPLACED ALL EIGHT L/E SLAT ACTUATORS PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 13,101 hrs · 7,423 cycles

EEPLS COVER AT RT OVERWING EXIT, MISSING. INSTALLED EEPLS COVER PER MM.

Part: SLIDE — DISCHARGED (R1 DOOR) · airframe 12,109 hrs · 6,864 cycles

R1 DOOR EVAC SLIDE PRESSURE IND LOW. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 10,201 hrs · 5,794 cycles

DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 5,386 hrs · 3,120 cycles

DURING SCHEDULED A2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: SLIDE — OUT OF ADJ (CABIN DOOR) · airframe 4,557 hrs · 2,661 cycles

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

Part: SLIDE — OUT OF ADJ (R2 DOOR) · airframe 4,239 hrs · 2,476 cycles

AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — LOOSE (AFT SVC DOOR) · airframe 3,513 hrs · 2,046 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 3,505 hrs · 2,039 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 3,333 hrs · 1,947 cycles

DURING SCHEDULED C3 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED. R&R COVERS PER MM.

Part: PANEL — LOOSE (NOSE WW) · airframe 12 hrs · 12 cycles

AIR TURNBACK, AFTER T/O AIRCRAFT FAILED TO PRESSURIZE. INSTALLED NOSE WHEEL WELL PANEL NR 114AW PER MM.