N226WN

Part: RIVET — LOOSE (ZONE 800) · airframe 64,554 hrs · 38,857 cycles

LOOSE RIVETS ON FED EMERGENCY ESCAPE SLIDE AFT HOLDER BAR <[01]. REMOVED AND REPLACED RIVETS ON FED EMERGENCY ESCAPE SLIDE AFT HOLDER BAR I.A.W SRM 51-40-02-0G-0 AND AIPC 25-66-00-13.; [02] REMOVED AND REPLACED RIVETS ON FED EMERGENCY ESCAPE SLIDE AFT HOLDER BAR I.A.W SRM 51-40-02-0G-0 AND AIPC 25-66-00-13. FED SLIDE WAS REMOVED AND REINSTALLED ON FAULT 725-61-06 (REM/INST - SLIDE REMOVAL AND INSTALLATION) TTG8Q010KQ5G AND AMM 25-66-01-000-802.; [03] VERIFIED CORRECTIVE ACTION 2.

Part: FITTING — LOOSE (ZONE 800) · airframe 64,554 hrs · 38,857 cycles

FED AFT GIRT BAR FITTING IS LOOSE. <[01] SECURED FED AFT GIRT BAR FITTING PER AMM 25-66-02-400-801; [02] VERIFIED ACTION 1. JOB COMPLETE.

Part: HANDLE — LOOSE (ZONE 800) · airframe 64,554 hrs · 38,857 cycles

AED ASSIST HANDLE LOOSE ON DOOR. <[01] TIGHTENED AED ASSIST HANDLE PER AMM 25-21-25-420-801; [02] VERIFIED ACTION 1. JOB COMPLETE.

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 64,554 hrs · 38,857 cycles

AFT CABIN EMERGENCY LIGHTS INOP <[01] REMOVED; REPLACED; AND PERFORMED GOOD INSTALLATION TEST OF M1672 BATTERY CHARGER PER AMM 33-51-06-960-806; [02] CORRECTIVE ACTION COMPLETED.

Part: HOOK — CORRODED (ZONE 200) · airframe 64,554 hrs · 38,857 cycles

LH EMERGENCY EXIT HATCH ESCAPE LIFE LINE HAS WORN AREAS AND KEEPER SNAP HOOK WITH CORROSION. <[01] REMOVED AND INSTALLED HATCH; IAW AMM 25-21-20-000-801 AND AMM 25-21-20-400-801 AND REMOVED AND INSTALLED L/H EMERGENCY EXIT HATCH ESCAPE LIFE LINE; IAW AMM 25-61-10-000-801 AND AMM 25-61-10-400-802.; [02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

AFT CARGO BAY AFT SCUFF PLATE IS CRACKED<[01] THIS SCUFF PLATE WAS INSTALLED ON CUSTOMER CARD:TTG8Q005QZ2P;[02] CORRECTION TO ACTION 1: REPAIRED SCUFF PLATE IAW SRM 53-60-15-2R-1. SCUFF PLATE RE-INSTALLED ON TASK CARD TTG8Q005QZ2P.;[03] VERIFIED CORRECTIVE ACTION #2

Part: BRACKET — CRACKED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

RT AC BAY BRACKET ASSY PN: 212A1116-1 IS CRACKED (MARKED) <[01]. REMOVED AND REPLACED RT AC BRACKET ASSY I.A.W. B737 AMM 20-50-11-910-801; TABLE 204. T/W ID: ATS348 DATE:11/2025; [02] CORRECTIVE ACTION COMPLETED.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 64,554 hrs · 38,857 cycles

CAPTAIN'S FWD I/B SEAT TRACK CRACKED <[01]. CAPTAIN'S FWD I/B SEAT TRACK CRACKED WAS REPLACED PER IPC 25-11-01-55. THIS COMPONENT WILL BE INSTALLED IN TASKCARD TTG8Q003JZYU; [02] VERIFIED ACTION 1. JOB COMPLETE.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 64,554 hrs · 38,857 cycles

PASSENGER CABIN FED UPPER FRAME BS 312 STR 5L CRACKED<[01] REPAIR ACCOMPLISHED AT M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L)<BR>'EA-GENERAL' REPAIR REFERENCE IS SELECTED.

Part: SHIELD — CORRODED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

MULTIPLE AREAS OF CORROSION ON ACB FWD SHIELD BETWEEN BS767-BS792 RBL21; WL156 <[01] REMOVED AND REPLACED ACB FWD SHIELD BETWEEN BS767-BS792 RBL21; WL156 IAW SRM 51-40-02 AND DWG# 146A0081 REV:A; [ 02] VERIFIED CORRECTIVE ACTION 1.

Part: SCUFF PLATE — CRACKED (ZONE 200) · airframe 64,554 hrs · 38,857 cycles

FSD SCUFF PLATE IS CRACKED.<[01] REMOVED AND INSTALLED SCUFF PLATE GALLERY SERVICE DOOR

Part: SKIN — DEBONDED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

PANEL 194FR OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 194FR OUTER SKIN DIS BOND WAS REPAIRED IAW SRM 51-70-05-2R-2;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 64,554 hrs · 38,857 cycles

CRACKED STR CLIP AT PAX CABIN BS727B S-6L. MARKED<[01] REMOVED AND INSTALLED NEW STR CLIP ITEM# 143A1010U1; LOT#1602791-1 AT DISCREPANCY AREA PER SRM 51-40-05; SRM 51-40-02; DWG# 146A1102 REV:-. ALL WORK COMPLETED.;[02] JOB COMPLETE

Part: PANEL — CRACKED (ZONE 600) · airframe 64,554 hrs · 38,857 cycles

PANEL 192CR O/B LATCH 2ND FROM AFT END IS CRACKED. (MARKED)<[01] REMOVED AND REPLACED PANEL 192CR O/B LATCH 2ND FROM AFT IAW SOPM 20-50-01.<BR>CALIBRATED TOOL USED:<BR>ID :ATS2427<BR>DATE :02/2025<BR>DUE :02/2026;[02] VERIFIED CORRECTIVE ACTION COMPLETE

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

FLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] FABRICATION OF NEW 241FF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]; [02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: SHIELD — CORRODED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

MULTIPLE AREAS OF CORROSION ON AFT CARGO BAY RH FLOOR SHIELD - BS [727B+5; 727B+12; 727C+10; 727D-787]; WL 156; RBL 21<[01]. REMOVED AND REPLACED ON AFT CARGO COMPARTMENT FLOOR TO SIDEWAL SUPPORT FROM BS727 TO BS767 RBL21 WL156 IAW SRM 51-40-02; SRM 51-40-05 AND DWG 146A7500 REV: A; [02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

FLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] FLOOR PANEL 241EF WAS REPLACED IAW SRM 53-00-50-2R-0 PARA 1. A NOTE:; [02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] FLOOR PANEL 241DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT FO ALL DAMAGE.

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

FLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] FLOOR PANEL 242DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT FO ALL DAMAGE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

MULTIPLE AREAS OF CORROSION ON AFT CARGO LH SHIELD - BS [727A-727B; 727B+2; 727B+6; 727B+18; 727C+2; 727C+5; 727D-787]; LBL 21; WL 156. <[01] REMOVED AND REPLACED AFT CARGO L/H FLOOR-TO-SIDEWALL SUPPORT FROM STA 727- STA 847; LBL 21; WL 156 IAW SRM 51-40-02-0G-0; SRM 51-40-02 AND DWG 146A7500 ID:0085 REV: A.; [02] VERIFIED CORRECTIVE ACTION #1.

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

FLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] FABRICATION OF NEW 242CF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]; [02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

FCB - CORROSION ON SIDEWALL SUPPORT BS 500+10; BS500+14; BS500+18; BS500A+2; BS500A+6; BS500A+10; BS500C+2; BS500C+6; BS500C+10 LBL 24.5 WL 156.5 (MARKED)<[01] THIS FAULT WILL BE ACCOMPLISHED ON CARD TTG8Q00ZWH9X.

Part: SHIELD — CORRODED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

FCB - CORROSION ON FWD SHIELD BS 420+17 RBL 23 WL 156.5 (MARKED) <[01] REMOVED AND REPLACED FWD SHIELD AT FCB BS420-BS440 RBL23 WL156.5 IAW SRM 51-40-02-0G-0 AND DWG 143A0080.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

FCB - CORROSION ON SIDEWALL SUPPORT BS 400+10 RBL 23 WL 156.5 (MARKED) <[01]. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT FCB FROM BS 400 TO BS420 RBL 23 WL 156.5 IAW SRM 51-40-02 & DWG# 143A7500 REV: -. ID: 0071.

Part: FLOOR PANEL — FAILED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF A FAILED PREVIOUS REPAIR. <[01] FLOOR PANEL 241AF WAS REPLACED IAW SRM 53-00-50-2R-0 PARA 1. A NOTE:; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] VERIFIED CORRECTIVE ACTION ITEM 1. JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] FLOOR PANEL 231ZF WAS REPLACED IAW SRM 53-00-50-2R-0 PARA 1. A NOTE:; [02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 64,554 hrs · 38,857 cycles

FLOOR SUPPORT CROSSBEAMS AT MID CABIN ABOVE FWD SPAR CRACKED - BS 539; LBL 1 AND RBL 1.<[01] REMOVED AND REPLACED 2EA PANEL BREAK. P/N: 143A5240U33 LOT: 1602183-5 AND P/N: 143A5240U34 LOT: 1591872-1 AND 2EA PLATE P/N 143A5240U12 LOT: 1598027-6 AND P/N: 143A5240U11 IAW B737-7 SRM 51-40-02-0G-0 AND DWG 143A5240 REV: - ID: 0013 AND DWG 143A5240 ID: 0014 REV: -

Part: SUPPORT — CORRODED (ZONE 100) · airframe 64,554 hrs · 38,857 cycles

FCB - CORROSION ON SIDEWALL SUPPORT BS 440+2; BS440+10; BS440+18; BS460+6; BS460+10; BS460+14; BS460+18 LBL 24.5 AND BS440+2 LBL23.5 WL 156.5 (MARKED) <[01]. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT FCB BETWEEN BS 396 TO BS 500D RBL 25 WL 156 IAW SRM 51-40-02 & DWG# 143A7500 REV:-. ID: 0058; [02] VERIFIED ACTION 1. JOB COMPLETE.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 63,957 hrs · 38,468 cycles

PASSENGER CABIN; EMERGENCY LIGHTS BATTERY PACK M1675 FAILED CAPACITY TEST.<[01] R&R EMERGENCY LIGHTS BATTERY PACK M1675 IAW AMM 33-51-06.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 63,957 hrs · 38,468 cycles

PASSENGER CABIN; EMERGENCY LIGHTS BATTERY PACK M1673 FAILED CAPACITY TEST<[01] R&R EMERGENCY LIGHTS BATTERY PACK M1673 IAW AMM 33-51-06.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 62,853 hrs · 37,776 cycles

MULTIPLE R/H OVERWING EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED R/H OVERWING EMERGENCY EXIT LIGHT POWER SUPPLY FUSE REF AMM 33-51-06. OPS TEST GOOD.

Part: BRACKET — OUT OF ADJUST (GIRT BAR) · airframe 62,690 hrs · 37,667 cycles

BRACKET THAT HOLDS GIRT BAR ON FORWARD SERVICE DOOR; NOT SECURE<[01] RESECURED BRACKET ON FWD SERVICE DOOR GIRT BAR BRACKET PER SRM 51-40-02

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 62,610 hrs · 37,614 cycles

EMERGENCY LIGHTS FWD AND TOP OF FO EMERGENCY EXIT DOOR INOP<[01] R/R EMERGENCY LIGHT CHARGER ASSY AT FO SIDE EMERGENCY DOOR IAW AMM 33-51-06

Part: LANDING GEAR — FAILED (ZN 700 LANDING G) · airframe 59,013 hrs · 35,401 cycles

LEFT MLG FAILED TO RETRACT AFTER TAKE-OFF, GEAR PINS INSTALLED & ALTERNATE MLG DOWN SWITCH IN ALTN POSITION. OK TO CONTINUE IAW MEL 32-16-01. SP1 C/W. REMOVED LT MLG DOWNLOCK ACT IAW AMM 32-32-51. C/BS PULLED & COLLARED IAW AMM 32-09-00-840-801. HYD SYS A & B RESERVOIRS DEPRESSURIZED & HYD QUICK DISCONNECTS DISCONNECTED IAW AMM 32-32-51. MLG PINS INSTALLED IAW AMM 32-00-01. PARTIALLY LH MLG DOWNLOCK ACTUATOR PER AMM 32-32-51. INSPECTION FOUND MISSING WASHER ON DOWNLOCK ACTUATOR HEAD PIN BUILD UP. AOG ON WASHER. INSTALLED LH MLG DOWN LOCK ACTUATOR IAW AMM 32-32-51. OPS/LEAK CHECK GOOD.

Part: WEB — CRACKED (ZN 600 RIGHT WIN) · airframe 58,497 hrs · 35,066 cycles

CRACK WEB TRAILING EDGE ORSS 278 AT RT WING 2023-295602<[01] REPLACED WEB LOCATED ON TRAILING EDGE ORSS 278 AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 115A2512 SHEET 13 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK CARD COMPLETED <BR>REPLACED WEB LOCATED ON TRAILING EDGE ORSS 278 AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 115A2512 SHEET 13 REV - <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 58,497 hrs · 35,066 cycles

CRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORRSS 279 AT LT WING 2023-295600<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE LOCATED AT LEVEL ORRSS 279 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A6200 REV:-.;[02] TASK CARD COMPLETED

Part: PLATE — CORRODED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

FUSELAGE LOWER LOBE - ANTENNA AT STA 410 S-28L HAS EVIDENCE OF CORROSION AAI:2023-295598<[01] REPLACED COVER PLATE AT LOWER FUSELAGE LOWER LOBE IAW B737-700 SRM-51-40-02-0G-0 AND DGW- 143N3403;[02] REPLACED COVER PLATE AT LOWER FUSELAGE LOWER LOBE IAW B737-700 SRM-51-40-02-0G-0 AND DGW- 143N3403 SHEET: 1 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: PLATE — CORRODED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

FUSELAGE LOWER LOBE- ANTENNA AT STA 450 S-28L HAS EVIDENCE OF CORROSION AAI:2023-295599<[01] REPLACED COVER PLATE AT LOWER FUSELAGE LOWER LOBE IAW B737-700 SRM-51-40-02-0G-0 AND DGW- 143N3403;[02] REPLACED COVER PLATE AT LOWER FUSELAGE LOWER LOBE STA 450 S-28L IAW B737-700 SRM-51-40-02-0G-0 AND DGW- 143N3403 SHEET: 1 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK FRAME ON BS 947.5 LOCATED LBL10 AND WL178 AFT CARGO COMPARTMENT 2023-295529<[01] REPLACED FRAME LOCATED ON BS947.5 BTW STR23L TO STR23R LBL10 AND WL178 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; DWG 147A1047; SHEET: 107; REV: ?. DWG 147A002; SHEET: 104; REV: ?. AND DWG 147A1047; SHEET: 70 AND REV: ?.;[02] CORRECTED STEP 1 <BR>REPLACED FRAME LOCATED ON BS947.5 BTW STR23L TO STR23R LBL10 AND WL178 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; DWG 147A1047; SHEET: 107; REV: ?. DWG 147A002; SHEET: 104; REV: ?. AND DWG 147A1047; SHEET: 70 AND REV: ?; SEE INDIVIDUAL SIGNOFF BELOW.;[03] CERTIFIED STEP 2; COMPLETED <BR>RII

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK WEB - INTERCOSTAL LOCATED BS947.5 RBL21 AND WL178 AT AFT CARGO COMPARTMENT 2023-295524<[01] REPLACED INTERCOSTAL-WEB LOCATED BS947.5 RBL21 AND WL178 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 147A7500; SHEET 24 AND REV -:; SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK CARD COMPLETED <BR>REPLACED INTERCOSTAL-WEB LOCATED BS947.5 RBL21 AND WL178 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 147A7500; SHEET 24 AND REV -:; SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK ANGLE LOCATED BS907 PLUS 11 INCH RBL13 AND WL171 AT AFT CARGO COMPARTMENT 2023-295523<[01] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[02] REPLACED FASTENER 1 E/A ON ANGLE LOCATED BS907 PLUS 11 INCH RBL13 AND WL171 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED FASTENER 1 E/A ON ANGLE LOCATED BS907 PLUS 11 INCH RBL13 AND WL171 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK ANGLE - SUPPORT LOCATED BS947.5 LBL10 AND WL178 AT AFT CARGO COMPARTMENT 2023-295522<[01] REPLACED ANGLE-SUPPORT LOCATED BS947.5 LBL10 AND WL178 AT AFT CARGO COMPARTMEN IAW B737-700 SRM 51-40-02 AND DWG 149A8103 REV:A. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED ANGLE-SUPPORT LOCATED BS947.5 LBL10 AND WL178 AT AFT CARGO COMPARTMEN IAW B737-700 SRM 51-40-02 AND DWG 149A8103 REV:A. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (ZN 300 STABILIZE) · airframe 58,497 hrs · 35,066 cycles

CRACK LEADING EDGE ANGLE LOC BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER 2023-295520<[01] REPLACED LEADING EDGE ANGLE LOC BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; AND DWG 176A3101 REV: -. DWG: 176A3001 REV: D.;[02] REPLACED LEADING EDGE ANGLE LOC BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; AND DWG 176A3101 REV: -. DWG: 176A3001 REV: D.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 58,497 hrs · 35,066 cycles

CRACK CORRUGATED PLATE TRAILING EDGE ORSS 233 AT LT WING 2023-295510<[01] REPLACED CORRUGATED PLATE LOC. TRAILING EDGE ORSS 233 AT LT WING AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 115A3700 SHEET: 39 REV: - SEE INDIVIDUAL SIGN OFF BELLOW;[02] REPLACED CORRUGATE PLATE LOC. TRAILING EDGE ORSS 233 AT LT WING AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 115A3700 SHEET: 39 REV: - SEE INDIVIDUAL SIGN OFF BELLOW.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 58,497 hrs · 35,066 cycles

CRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 AT LT WING 2023-295508<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 261 AT LT WING I.A.W SRM B737-700 51-40-0 115A2001 REV:-;[02] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 261 AT LT WING I.A.W SRM B737-700 51-40-0 115A2001 REV:-

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 58,497 hrs · 35,066 cycles

CRACK CORRUGATED PLATE TRAILING EDGE IRSS 217 AT RT WING 2023-295514<[01] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ON TRAILING EDGE IRSS 217 AT RT WING IAW B737-700 SRM 51-40-02 AND 51-10-02.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE IRSS 217 AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] CERTIFIED STEP 2 COMPLETED

Part: FAIRING — CRACKED (ZN 400 NACELLE/P) · airframe 58,497 hrs · 35,066 cycles

CRACK INBOARD THRUST REVERSE ON PANEL UPPER AREA RT ENGINE 2023-295411<[01] REPLACED ACCESS PANEL FAIRING INBOARD THRUST REVERSE UPPER AREA RT ENGINE IAW B737-700 AMM 78-31-09-010-801-F00 AND IAW B737-700 AMM 78-31-09-420-801-F00. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ACCESS PANEL FAIRING INBOARD THRUST REVERSE UPPER AREA RT ENGINE IAW B737-700 AMM 78-31-09-010-801-F00 AND IAW B737-700 AMM 78-31-09-420-801-F00. SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK BRACKET LOCATED AT LEVEL STA 727 AND BETWEEN RBL3.00 AND RBL8.10 AT AFT CARGO COMPARTMENT 2023-295358<[01] REPLACED ANGLE ON AFT CARGO COMP I.A.W SRM B737-700 51-40-02 AND DRAWING 144A2600 REV:-;[02] TASK CARD COMPLETED

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CORROSION CHANNEL SUPPORT FROM STA 767 TO STA 794 AT RBL 21.00 AT AFT CARGO COMPARTMENT 2023-295372<[01] REPLACED CHANNEL SUPPORT AND FASTENER I.A.W SRM B737-700 51-40-02 AND DRAWING 146A0081 REV:A.SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETED <BR>REPLACED CHANNEL SUPPORT AND FASTENER I.A.W SRM B737-700 51-40-02 AND DRAWING 146A0081 REV:A.SEE INDIVIDUAL SIGN OFF BELOW<BR>RII

Part: COVER — BROKEN (ZN 200 FUS TOP) · airframe 58,497 hrs · 35,066 cycles

BROKEN EMERGENCY EXIT LIGHT COVER ON HEADER PANEL RH SIDE AT FWD GALLEY AREA (1 EA) 2023-295361<[01] REPLACED EMERGENCY EXIT LIGHT COVER ON HEADER PANEL RH SIDE AT FWD GALLEY AREA (1 EA) IAW B737 AMM 33-51-01-960-802 STEP 3.C (5)(A) AND (7)(10).;[02] TASK CARD COMPLETED

Part: FLOOR SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CORROSION ANGLE FLOOR STRUCTURE LOCATED BETWEEN BS303.9 TO BS344; WL208.1 AND LBL58 AT FWD GALLEY AREA 2023-295354<[01] REPLACED NEW ANGLE FLOOR STRUCTURE LOCATED BETWEEN BS303.9 TO BS344; WL208.1 AND LBL58 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8110 SHEET:11 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED NEW ANGLE FLOOR STRUCTURE LOCATED BETWEEN BS303.9 TO BS344; WL208.1 AND LBL58 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8110 SHEET:11 REV:- SEE INDIVIDUAL SIGN OFF BELOW AS RII

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2023-295270<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:15121570;DUE DATE:05-NOV-23.;[02] REPAIRED BY WELDING FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975 SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPAIRED BY WELDING FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 AND RBL31 FWD GALLEY AND LAV 2023-295266<[01] REPLACED NEW WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 AND RBL31 FWD GALLEY AND LAV AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED NEW WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 AND RBL31 FWD GALLEY AND LAV AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -SEE INDIVIDUAL SIGN OFF BELOW. RII.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK SCUFF PLATE CENTER POSITION ON FWD SERVICE DOOR AT FWD GALLEY AREA 2023-295245<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189515;DUE DATE:19-DEC-23.;[02] TOOL USED RADIOMETER PHOTOMETER PN:XRP-3000; SN: 1753759; DUE DATE: 14-OCT-23;[03] REPAIRED SCUFF PLATE CENTER POSITION ON FWD SERVICE DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.SEE INDIVIDUAL SIGN OFFS BELOW.;[04] REPAIRED SCUFF PLATE CENTER POSITION ON FWD SERVICE DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK ON FLOOR STRUCTURE INNER CHORD LOCATED BS 303.9 AT LEVEL STR 17L AT FWD GALLEY AREA 2023-295254<[01] REPLACED INNER CHORD LOCATED ON FLOOR STRUCTURE LOCATED ON BS 303.9 AT LEVEL STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; DWG 141A8110; SHEET 11; REV: ?. AND DWG 141A8110; SHEET 9; REV: A.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] INSTALLED NEW INNER CHORD LOCATED ON FLOOR STRUCTURE LOCATED ON BS 303.9 AT LEVEL STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; DWG 141A8110; SHEET 11; REV: ?. AND DWG 141A8110; SHEET 9; REV: A. RII.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,497 hrs · 35,066 cycles

CRACK ENTRY DOOR CUT OUT INTERCOSTAL LOCATED BETWEEN BS294.5 TO BS303.9 AND STR16L AT FWD GALLEY AREA 2023-295284<[01] REPLACED INTERCOSTAL WEB AND FASTENERS LOCATED ENTRY DOOR CUT OUT BETWEEN BS294.5 TO BS303.9 AND STR16L AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG 141A8180 REV-C. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED AS RII <BR>REPLACED INTERCOSTAL WEB AND FASTENERS LOCATED ENTRY DOOR CUT OUT BETWEEN BS294.5 TO BS303.9 AND STR16L AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG 141A8180 REV-C. SEE INDIVIDUAL SIGN OFF BELOW.

Part: STRINGER CLIP — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK FRAME ON BS 277 TIE CLIP AT STR10R AT FWD GALLEY AREA 2023-295258<[01] REPLACED TIE CLIP LOCATED ON BS 277 AT STR10R AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02 AND DWG# 141A1110; SHEET 18; REV.-. SEE INDIVIDUAL SIGN OFF BELLOW;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 58,497 hrs · 35,066 cycles

BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2023-295238<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW MT 733-50-01 WITH TTG8Q005L765 STEP 4;[02] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW MT 733-50-01 WITH TTG8Q005L765 STEP 4

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 AND BL0 FWD GALLEY AND LAV 2023-295269<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 AND BL0 FWD GALLEY AND LAV. IAW B737-700 SRM 51-40-02 AND DWG 141A5400; SHEET 20 AND REV ?. <BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 AND BL0 FWD GALLEY AND LAV. IAW B737-700 SRM 51-40-02 AND DWG 141A5400; SHEET 20 AND REV ?. RII<BR>SEE INDIVIDUAL SIGN-OFF BELOW.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-295274<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:15121570;DUE DATE:05-NOV-23.;[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<BR>INDIVIDUAL SIGNOFFS BELOW;[03] 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

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS328 TO BS344 AND LBL45 FWD GALLEY AND LAV 2023-295272<[01] REPLACED WEB-INTERCOSTAL LOCATED FLOOR STRUCTURE BETWEEN BS328 TO BS344 AND LBL45 FWD GALLEY AND LAV. IAW B737-700 SRM:51-40-02 AND DWG: 141A5400 SHET: 44 REV.- SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] REPLACED WEB-INTERCOSTAL LOCATED FLOOR STRUCTURE BETWEEN BS328 TO BS344 AND LBL45 FWD GALLEY AND LAV. IAW B737-700 SRM:51-40-02 AND DWG: 141A5400 SHET: 44 REV.- SEE INDIVIDUAL SIGN-OFFS BELOW. AS RII

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS344 TO BS360 AND LBL13 FWD GALLEY AND LAV 2023-295287<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS344 TO BS360 AND LBL13 FWD GALLEY AND LAV IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 141A5400 REV:A; SEE INDIVIDUAL SIGNOFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED <BR>RII

Part: INTERCOSTAL — CORRODED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CORROSION WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS294.5 TO BS312; WL208.1 AND LBL11 FWD GALLEY AND LAV 2023-295271<[01] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS294.5 TO BS312; WL208.1 AND LBL11 FWD GALLEY AND LAV. IAW B737-700 SRM: 51-10-02 AND DWG: 141A5600 SHEET 2 REV. N. SEE INDIVIDUAL SING-OFF BELLOW.;[02] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS294.5 TO BS312; WL208.1 AND LBL11 FWD GALLEY AND LAV. IAW B737-700 SRM: 51-10-02 AND DWG: 141A5600 SHEET 2 REV. N. SEE INDIVIDUAL SING-OFF BELLOW. AS RII

Part: SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK BS 294.5 ANGLE - SUPPORT AND STR17R FWD GALLEY AND LAV 2023-295282<[01] REPLACED NEW BS 294.5 ANGLE - SUPPORT AND STR17R FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEE:25 REV- SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED AS RII <BR>REPLACED NEW BS 294.5 ANGLE - SUPPORT AND STR17R FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEE:25 REV- SEE INDIVIDUAL SIGN OFF BELOW

Part: FLOOR SUPPORT — CRACKED (ZN 200 FUS TOP) · airframe 58,497 hrs · 35,066 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 TO BS 360 AND RBL 34 FWD GALLEY AREA 2023-295285<[01] REPLACED WEB-INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 TO BS 360 AND RBL 34 FWD GALLEY AREA IAW: 51-10-02 AND DWG: 141A5400 SHEET 33 RV.? SEE INDIVIDUAL SING-OFF BELLOW.;[02] REPLACED WEB-INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 TO BS 360 AND RBL 34 FWD GALLEY AREA IAW: 51-10-02 AND DWG: 141A5400 SHEET 33 RV.? SEE INDIVIDUAL SING-OFF BELLOW. AS RII

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 AND RBL31 FWD GALLEY AND LAV 2023-295265<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 AND RBL31 FWD GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETE RII <BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 AND RBL31 FWD GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 REV-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOORBEAM — CORRODED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BETWEEN BS986.5; WL208.1 AND RBL44 AT AFT GALLEY AREA 2023-295231<[01] EQUIPMENT P/N 45MG; S/N 130063701; DUE DATE 16-JUN-23 WAS USED.;[02] TOOL USED PN:38DL PLUS; SN:120398603; DUE DATE:07-NOV-23;[03] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 600D; S/N 60009161631 DUE DATE 31/JAN/24;[04] INSPECTION REJECT IN STEP 12<BR>SEE TTG8Q00KWUHT;[05] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24.;[06] REPAIRED FLOOR BEAM LOC 986.5 AND WL208.1 AND RBL 8 TO RBL64 I.A.W B737-700 SRM 53-70-51-2R-4 REPAIR 4 ;EA NÏ¿½: 1-753-31349 AND EA 23-153-01501.SEE INDIVIDUAL STEP SIGN OFFS BELOW;[07] REPAIRED FLOOR BEAM LOC 986.5 AND WL208.1 AND RBL 8 TO RBL64 I.A.W B737-700 SRM 53-70-51-2R-4 REPAIR 4 ;EA NÏ¿½: 1-753-31349 AND EA 23-153-01501.SEE INDIVIDUAL STEP SIGN OFFS BELOW.. RII ITEM

Part: FLOORBEAM — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK FLOOR STRUCTURE BEAM LOCATED BETWEEN BS294.5 AND RBL51 AT FWD GALLEY AREA 2023-295235<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC500D; S/N: N500X12101V022240; CAL DUE DATE: 12-MAR-24;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24.;[03] TOOL USED: FLAPSPEED; PN: FPK-PR0-104; SN: PR0-3448; DUE DATE: 27-JUN-23; CALIPER; PN: 500-196-30; B22072617; DUE DATE: 26-JUN-23;[04] PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE BEAM BETWEEN BS294.5 AND RBL16 TO RBL51 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16 AND DWG 141A5502 REV-. THIS REPAIR IS CATEGORY A NOT FURTHER ACTIONS OR INSPECTIONS REQUIRED. SEE INDIVIDUAL SIGN OFF BELOW.;[05] CERTIFIED STEP 4 COMPLETE RII <BR>PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE BEAM BETWEEN BS294.5 AND RBL16 TO RBL51 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16 AND DWG 141A5502 REV-. THIS REPAIR IS CATEGORY A NOT FURTHER ACTIONS OR INSPECTIONS REQUIRED. SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,497 hrs · 35,066 cycles

CRACK SERVICE DOOR CUT OUT ANGLE LOCATED BETWEEN BS294.5 AND STR8R TO STR10R AT FWD GALLEY AREA 2023-295233<[01] REPLACED ANGLE AND FASTENER I.A.W SRM B737-700 51-40-032 AND DRAWING 141A8370 REV:D LOC BS294.5 AND BTW S-8R TO S-10R . SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] REPLACED ANGLE AND FASTENER I.A.W SRM B737-700 51-40-032 AND DRAWING 141A8370 REV:D LOC BS294.5 AND BTW S-8R TO S-10R . SEE INDIVIDUAL STEP SIGN OFFS BELOW

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 58,497 hrs · 35,066 cycles

DETERIORATED GIRT BAR FITTING HARDWARE AT FWD GALLEY AREA 2023-295225<[01] REPLACED GIRT BAR FITTING HARDWARE AT FWD GALLEY AREA I.A.W. B737-700 AMM 25-66-02-400-801 STEP 3 D (1) (G)(H)(I);[02] REPLACED GIRT BAR FITTING HARDWARE AT FWD GALLEY AREA I.A.W. B737-700 AMM 25-66-02-400-801 STEP 3 D (1) (G)(H)(I)

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 58,497 hrs · 35,066 cycles

CRACK ANGLE FLOOR STRUCTURE LOC BTW STA 685 TO STA 706 RBL 0 AT PASSENGER CABIN 2023-295171<[01] REPLACED NEW ANGLE FLOOR STRUCTURE LOC BTW STA 685 TO STA 706 RBL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110 SHEET:6 REV:-SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP:1.<BR>REPLACED ANGLE FLOOR STRUCTURE LOC BTW STA 685 TO STA 706 RBL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110 SHEET:6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTIVE ACTION STEP 2 CERTIFIED RII

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 58,497 hrs · 35,066 cycles

INOP EMERGENCY LIGHT BATTERY PACK AT PASSENGER CABIN (3 EA) 2023-295078<[01] REPLACED EMERGENCY LIGHT BATTERY PACK AT PASSENGER CABIN (3 EA) M1669; M1675; M1674; IAW B737-700 AMM 33-51-06-960-805 TEST IS OK;[02] REPLACED EMERGENCY LIGHT BATTERY PACK AT PASSENGER CABIN (3 EA) M1669; M1675; M1674; IAW B737-700 AMM 33-51-06-960-805 TEST IS OK SEE INDIVIDUAL SIGNOFF BELOW;[03] REPLACED EMERGENCY LIGHT BATTERY PACK AT PASSENGER CABIN (3 EA) M1669; M1675; M1674; IAW B737-700 AMM 33-51-06-960-805 TEST IS OK SEE INDIVIDUAL SIGNOFF BELOW

Part: VAPOR BARRIER — CRACKED (BS 663 BULKHEAD) · airframe 57,452 hrs · 34,381 cycles

RIGHT MLG WW HAS A 1 INCH CRACK ON UPPER VAPOR BARRIER WEB BS 663, RBL 38, WL 168. EVALUATED DAMAGE TO VAPOR BARRIER WEB, CRACK IS REPAIRABLE IAW B737 SRM 57-10-10-2R-2. CLEANED AND PREPPED REPAIR AREA IAW SRM 51-70-04-2R-10, PAR 4 STEPS A, B, AND C. BONDED REPAIR PLIES INSTALLED IAW SRM 51-70-04-2R-10, PAR 4, STEPS D, E, F, AND G, AND SRM 51-70-04-2R-0. PERFORMED NDT IAW NDT PT 1, 51-01-01. NO DEFECTS NOTED.

Part: ANGLE — CRACKED (BS 663) · airframe 57,452 hrs · 34,381 cycles

CRACK FOUND ON UPPER ATTACH ANGLE AT BS 663, RBL 39, WL167.

Part: FLOORBOARD — DAMAGED (MD CABIN) · airframe 57,452 hrs · 34,381 cycles

MID CABIN FLOORBOARD 231XF HAD COMPOSITE PULLED FIBERS ON UPPER SIDE OF PANEL. REPAIRED THE DAMAGE TO THE UPPER SURFACE OF FLOORBOARD IAW SRM 53-00-50-2R-0, REPAIR GENERAL, AND SRM 53-00-50-2R-1, REPAIR 1.

Part: FLOORBOARD — DAMAGED (MID CABIN) · airframe 57,452 hrs · 34,381 cycles

MID CABIN FLOORBOARD 231YF HAD COMPOSITE PULLED FIBERS ON UPPER SIDE. EVALUATED AND FOUND MISSING PLIES. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1. CLEANED AND PREPPED IAW SRM 53-00-50-2R-1, STEP 3 A, C, E & F. BONDED REPAIR IAW SRM 53-00-50-2R-1, STEP 3, K - M. TAP TESTED GOOD. REPAIRED THE FLOORBOARD IAW SRM 53-00-50-2R-1, AND SRM 53-00-50-2R-0, REPAIR GENERAL

Part: FLOORBOARD — DAMAGED (MID CABIN) · airframe 57,452 hrs · 34,381 cycles

MID CABIN FLOORBOARD 232RF HAD COMPOSITE PULLED FIBERS ON UPPER SIDE. EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1. CLEANED AND PREPPED IAW SRM 53-00-50-2R-1, STEP 3, A, C, E, & F. BOND REPAIR IAW SRM 53-00-50-2R-1, STEP 3, K - M. TAP TESTED GOOD. REPAIRED MID CABIN FLOORBOARD IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0, REPAIR GENERAL.

Part: FLOORBOARD — DAMAGED (MID CABIN) · airframe 57,452 hrs · 34,381 cycles

MID CABIN FLOORBOARD 241BF HAD COMPOSITE PULLED FIBERS ON UPPER SIDE. EVALUATED DAMAGE, REPAIRABLE IAW SRM 53-00-50-2R-1, REPAIR 1. TAP TESTED GOOD, NO DELAMINATION NOTED. CLEANED, AND PREPPED IAW SRM 53-00-50-2R-1, PAR 3, STEPS A, C, E, AND J. BONDED REPAIR PLIES IAW SRM 53-00-50-2R-1, PAR 3, STEPS K, L, AND M. TAP TESTED GOOD. REPAIRED THE MID CABIN FLOORBOARD IAW SRM 53-00-50-2R-1.

Part: FLOORBOARD — DAMAGED (MID CABIN) · airframe 57,452 hrs · 34,381 cycles

MID CABIN FLOORBOARD 242AF HAD COMPOSITE PULLED FIBERS ON UPPER SIDE. EVALUATED DAMAGE, REPAIRABLE IAW SRM 53-00-50-2R-1, REPAIR 1, TAP TESTED GOOD NO DELAMINATION NOTED. CLEANED, AND PREPPED IAW SRM 53-00-50-2R-1, PAR 3, STEPS A, C, E, AND J. BONDED REPAIR PLIES IAW SRM 53-00-50-2R-1, PAR 3, STEPS K, L, AND M. TAP TESTED GOOD. REPAIRED THE FLOOR BOARD IAW SRM 53-00-50-2R-1.

Part: FLOORBOARD — PULLED (MID CABIN) · airframe 57,452 hrs · 34,381 cycles

MID CABIN FLOORBOARD 232SF HAD COMPOSITE PULLED FIBERS ON UPPER SURFACE. REPAIRED THE FLOORBOARD 232SF IAW SRM 53-00-50-2R-1, SRM 53-00-50-2R-0.

Part: FLOORBOARD — DAMAGED (MID CABIN) · airframe 57,452 hrs · 34,381 cycles

MID CABIN FLOORBOARD 241AF HAD COMPOSITE PULLED FIBERS ON UPPER SIDE. EVALUATED AND FOUND DAMAGE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0, REPAIR GENERAL, TABLE 201, REPAIR 1. CLEANED AND PREPPED IAW SRM 53-00-50-2R-1, STEPS 3A, C, E, & F. BONDED REPAIR IAW SRM 53-00-50-2R-1, STEPS 3J - M. TAP TESTED GOOD. REPAIRED THE FLOORBOARD IAW SRM 53-0-50-2R-0, REPAIR GENERAL, AND SRM 53-00-50-2R-1.

Part: FLOORBOARD — DAMAGED (MID CABIN) · airframe 57,452 hrs · 34,381 cycles

MID CABIN FLOORBOARD 231ZF HAD COMPOSITE PULLED FIBERS ON UPPER SIDE. CLEAN AND PREPPED IAW SRM 53-00-50-2R-1, PAR 3, A, C, E & F. BONDED REPAIR INSTALLED IAW SRM 53-00-50-2R-1, PAR 3 K-M. REPAIRED IAW SRM 53-00-50-2R-1, SRM 53-00-50-2R-0.

Part: ATTACH ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 57,452 hrs · 34,381 cycles

CRACK FOUND ON UPPER ATTACH ANGLE AT BS 663 LBL 39, WL167.

Part: FLOORBOARD — DAMAGED (MID CABIN) · airframe 57,452 hrs · 34,381 cycles

MID CABIN FLOORBOARD 241CF HAD COMPOSITE PULLED FIBERS ON UPPER SIDE OF PANEL. REPAIRED THE FLOORBOARD IAW SRM 53-00-50-2R-0, REPAIR GENERAL, AND SRM 53-00-50-2R-1, REPAIR 1. TAP TESTED GOOD.

Part: ANGLE — CRACKED (ZONE 500) · airframe 57,452 hrs · 34,381 cycles

LEFT INBD WING L/E SUPPORT ANGLE CRACKED AT FASTENER HOLE COMMON TO WTB FARING PANELS 191AL AND LOWER FWD CORNER OF 195AL. ] REMOVED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0. DRILLED A NEW SUPPORT ANGLE IAW SRM 51-40-02-0G-0 AND DWG 116A3110, REV A. PAINTED THE SUPPORT ANGLE IAW AMM 51-21-99-300-801. INSTALLED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0 AND DWG 116A3110, REV A.

Part: HANDLE — BROKEN (AFT ENTRY DOOR) · airframe 55,765 hrs · 33,260 cycles

AFT PASSENGER ENTRY DOOR; INTERIOR DOOR ASSIST HANDLE IS BROKEN. / [01] REMOVED AND REPLACED AFT PASSENGER ENTRY DOOR; INTERIOR DOOR ASSIST HANDLE PER AMM 52-13-31

Part: LENS — LOOSE (R/H CABIN) · airframe 55,312 hrs · 32,976 cycles

O/H LIGHTS TRIM ROW 10 FO'S SIDE BECAME LOOSE DURING FLIGHT / [01] TAPED ROW10 PSI BIN PANEL EMERGENCY LIGHT ASSY LENS AT RIGHT HAND SIDE. REMOVED TAPE RESECURED BULLNOSE EMERGENCY EXIT LENS AT ROW 10 F/OS SIDE PER AMM 33-51-03.

Part: LIGHT — INOPERATIVE (L/H OVERWING) · airframe 55,156 hrs · 32,886 cycles

L/H OVER-WING EMERGENCY LIGHT INOP. / [01] CLEANED LIGHT FIXTURE CORROSION AND RE-LAMPED THE L/H OVERWING EMERGENCY EXIT LIGHT PER SWPM 20-10-04 AND AMM 33-51-04. OPS CHECK GOOD.

Part: PANEL — CORRODED (FUSELAGE) · airframe 54,932 hrs · 32,752 cycles

193D PANEL ; AFT EDGE OF 193D PANEL HAS FRETTING WEAR. / [01] REPLCED PANEL REF AMM 53-51-21

Part: PANEL — CORRODED (FUSELAGE) · airframe 54,907 hrs · 32,739 cycles

193D PANEL ; AFT EDGE OF 193D PANEL HAS FRETTING WEAR. / [01] REPLCED PANEL REF AMM 53-51-21

Part: LENS — LOOSE (CABIN) · airframe 54,907 hrs · 32,739 cycles

OVERHEAD BIN EMERGENCY LIGHT LENS LOOSE AT 18/19DEF. ; OVERHEAD BIN EMERGENCY LIGHT LENS LOOSE AT 1819DEF. / [01] REPLACED RETAINER AND SPRING; CHECK GOOD REF MM33-51-03

Part: NONE — CRACKED (FUSELAGE) · airframe 54,907 hrs · 32,739 cycles

193D PANEL STA 727 T CLIP CRACKED ON LEFT SIDE / [01] REPLACED LEFT HAND T-CLIP REF SRM 51-40-02 AND EA 22-153-00313

Part: NONE — CRACKED (FUSELAGE) · airframe 54,907 hrs · 32,739 cycles

193D PANEL STA 727 VERTICAL CLIP CRACKED ; 193D PANEL STA 727 VERTICAL CLIP CRACKED ON LEFT SIDE / [01] VERTICAL CLIP FABRICATED FROM 0.050 2024T3 REF. TSR 202200826; [02] INST. VERTICAL CLIP REF SRM 51-40-02

Part: NONE — CRACKED (FUSELAGE) · airframe 54,932 hrs · 32,752 cycles

193D PANEL STA 727 T CLIP CRACKED ON LEFT SIDE / [01] REPLACED LEFT HAND T-CLIP REF SRM 51-40-02 AND EA 22-153-00313

Part: NONE — BROKEN (CABIN) · airframe 54,705 hrs · 32,611 cycles

SUPPLEMENTAL INFORMATION: LH OVERWING SIDEWALL EXIT LIGHT LENS BROKEN ; / [01] R&R LENS AND BASE ASSY PER AMM 33-51-02

Part: NONE — LOOSE (CABIN) · airframe 54,009 hrs · 32,200 cycles

SUPPLEMENTAL INFORMATION: ROW 12 F.O. SIDE EXIT SIGN FELL OFF ; / [01] SECURED EXIT SIGN COVER I.A.W. A.M.M. 33-51-01

Part: WARNING LIGHT — FALSE ACTIVATION (TE FLAPS) · airframe 53,596 hrs · 31,942 cycles

AFTER FULLY CONFIGURED FOR LANDING THE LE FLAPS TRANSIT LIGHT ILLUMINATED. ; / [01] CW FIM TASK 27-51 TASK 801 NO DEFECTS NOTED

Part: LIGHT — MISSING (CABIN) · airframe 53,110 hrs · 31,655 cycles

AFT GALLEY RIGHT HAND SIDE L1191 EMERGENCY EXIT LOCATOR MISSING LIGHT ASSEMBLY ; / [01] REPLACED L1191 EMERGENCY EXIT LOCATOR ASSEMBLY WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-802.<BR>NO FURTHER FAULTS FOUND.; [02] VERIFIED; REPLACED L1191 EMERGENCY EXIT LOCATOR ASSEMBLY WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-802.NO FURTHER FAULTS FOUND.; [03] VERIFIED; REPLACED L1191 EMERGENCY EXIT LOCATOR ASSEMBLY WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-802.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 53,110 hrs · 31,655 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED ; / [01] WELDED CRACKED ACB; FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4)<BR>WELDING MACHINE CAL INFO E10583 S/N KJ256554; [02] ADDED MEASUREMENTS; [03] VERIFIED WELD PER SRM 53-60-15-2R-1; [04] PT INSPECTED REPAIR IAW SOPM 20-20-02; NO CRACKS NOTED. <BR><BR>CAL ID ATS2561 DLM-1000; [05] SANDED REPAIR AREA ON SCUFF PLATE PER SRM 53-60-15-2R-1 PARA 4.B (5); [06] VERIFIED SANDED REPAIR AREA ON SCUFF PLATE PER SRM 53-60-15-2R-1 PARA 4.B.(5).; [07] APPLIED CHEMICAL CONVERSION COATING AND PRIME ON SCUFF PLATE PER REF SRM 53-60-15-2R-1 REPAIR 1 STEP 4B(6) AND (7).; [08] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIME ON SCUFF PLATE PER REF SRM 53-60-15-2R-1 REPAIR 1 STEP 4B(6) AND (7).; [09] APPLIED CHEMICAL CONVERSION COATING AND PRIME ON SCUFF PLATE PER SRM 53-60-15-2R-1 REPAIR 1 STEP 4B (6) AND (7).; [10] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIME ON SCUFF PLATE PER SRM 53-60-15-2R-1 REPAIR 1 STEP 4B (6) AND (7).

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 53,110 hrs · 31,655 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED ; / [01] WELDED CRACKED ACB;AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4)<BR>WELDING MACHINE CAL INFO E10583 S/N KJ256554; [02] ADDED MEASUREMENTS; [03] VERIFIED WELD PER SRM 53-60-15-2R-1; [04] PT INSPECTED REPAIR IAW SOPM 20-20-02; NO CRACKS NOTED.<BR><BR>CAL ID ATS2561 DLM-1000; [05] SANDED REPAIR AREA ON SCUFF PLATE PER SRM 53-60-15-2R-1 PARA 4.B.(5); [06] VERIFIED SANDED REPAIR AREA ON SCUFF PLATE PER SRM 53-60-15-2R-1 PARA 4.B.(5).; [07] APPLIED CHEMICAL CONVERSION COATING AND PRIME ON SCUFF PLATE PER REF SRM 53-60-15-2R-1 REPAIR 1 STEP 4B(6) AND (7).; [08] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIME ON SCUFF PLATE PER REF SRM 53-60-15-2R-1 REPAIR 1 STEP 4B(6) AND (7).; [09] APPLIED CHEMICAL CONVERSION COATING AND PRIME ON SCUFF PLATE PER SRM 53-60-15-2R-1 REPAIR 1 STEP 4B (6) AND (7).; [10] APPLIED CHEMICAL CONVERSION COATING AND PRIME ON SCUFF PLATE PER SRM 53-60-15-2R-1 REPAIR 1 STEP 4B (6) AND (7).

Part: WEB — CORRODED (FUSELAGE) · airframe 53,110 hrs · 31,655 cycles

ACB LOWER CHORD UNDER THE SUB THRESHOLD WED HAS CORROSION AT BS 787+10 RBL 21 WL 156. REMOVED CORROSION ON ACB LOWER CHORD UNDER THRESHOLD WEB PER REF SRM 53-60-15-1A-1, FOUND TO BE OUT OF LIMITS. REPAIRED THE THRESHOLD WEB.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,110 hrs · 31,655 cycles

LIGHT ASSOCIATED WITH EMERGENCY LT BATTERY PACK M1670 INOP. / [01] TROUBLE SHOT DOWN TO FAULTY BATTERY AT M1670; PER AMM 33-51-06/20. BATTERY IS ON ORDER.; [02] REMOVED AND REPLACED M1670 EMERGENCY EXIT LIGHT BATTERY PACK AND PERFORMED GOOD INSTALLTION TEST OF APPLICABLE EMERGENCY EXIT LIGHTS IAW AMM 33-51-06-960-805.; [03] VERIFIED; MOVED AND REPLACED M1670 EMERGENCY EXIT LIGHT BATTERY PACK AND PERFORMED GOOD INSTALLTION TEST OF APPLICABLE EMERGENCY EXIT LIGHTS IAW AMM 33-51-06-960-805.; [04] VERIFIED; MOVED AND REPLACED M1670 EMERGENCY EXIT LIGHT BATTERY PACK AND PERFORMED GOOD INSTALLTION TEST OF APPLICABLE EMERGENCY EXIT LIGHTS IAW AMM 33-51-06-960-805.

Part: WEB — CORRODED (BS 794-800) · airframe 53,110 hrs · 31,655 cycles

AFT CARGO BAY VERTICAL THRESHOLD WEB AT BS 794-BS 800 RBL 21 WL 156-WL 152 IS CORRODED ; / [01] REMOVED CORROSION ON AFT CARGO VERTICAL THRESHOLD WEB PER REF SRM 53-60-15-1A-1.MATERIAL LOST IS MORE THAN 10% .THEREFORE; FOUND TO BE OUT OF LIMIT .[03] VERIFIED OUT OF LIMITS PER SRM 53-60-15-1A-1; [04] REMOVED AFT CRAGO BAY VERTICAL THRESHOLD WEB FROM BS 794 TO BS 847 RBL 21 WL 156-152 IAW SRM 51-40-02-0G-0; [05] LOCATED AND DRILLED NEW AFT CARGO BAY VERTICAL THRESHOLD WEB PER REF SRM 51-40-05 AND DWG NBR 146A8120 REV - OK TO INSTALL NEW VERTICAL WEB.; [06] LOCATED AND DRILLED NEW AFT CARGO BAY VERTICAL THRESHOLD WEB PER REF SRM 51-40-05 AND DWG NBR 146A8120

Part: BEAM — CRACKED (R1 DOOR) · airframe 53,110 hrs · 31,655 cycles

#4 LOWER SERVICE DOOR BEAM CRACKED IN RADIUS AT I/B SIDE OF BEAM NEXT TO FASTENER ROW. / [01] REMOVED FSD PER AMM 52-41-00-000-801.; [02] OK TO INSTALL FWD SERVICE DOOR; [03] INSTALLED FWD SERVICE DOOR PER AMM 52-41-00-400-801 STEPS 3. F. (1)-(6); [04] VERIFIED INSTALLED FWD SERVICE DOOR PER AMM 52-41-00-400-801 STEPS 3. F. (1)-(6); [05] ADJUSTED FORWARD SERVICE DOOR PER AMM 52-41-00-820-801 STEP 2.G(1-3); 2.H(1A-B); 2.I(1A-B); 2.J(1A-C); 2.K(1A-B); 2.L(1B)(4A-D); 2.M(1B)(3A-C); 2.N(1A-B); 2.O(1A-B); 2.P(1A-B); 2.Q(1A-D); 2.R(1A-D); 2.S(1A-B) NO OTHER ADJUSTMENT NEEDED <BR>PERFORMED FORWARD SERVICE DOOR INDICATION SENSOR ADJUSTMENT PER AMM 52-71-11-820-801 OPS CHECK GOOD <BR>USED DIGITAL CALIPER <BR>ID:PER2059<BR>S/N:C011903743M<BR>DATE:10/2020<BR>DUE:10/2021; [06] PERFORMED FORWARD SERVICE DOOR SYSTEM TEST PER AMM 52-41-00-700-801 <BR>USED TORQUE WRENCH <BR>ID:ATS2321<BR>SN:0119121014<BR>DATE:05/2021<BR>DUE:05/2022; [07] UPDATED MEASUREMENTS AND INSTALLED DOOR IN MXI.;

Part: SEAT TRACK — CORRODED (BS 773) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON RAIL AT BS 773 RBL 2.5 WL 156. CORRODED AREA ON RAIL FOUND TO BE OUT OF LIMITS DUE TO EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 PART 4A(2) DETAIL D. INSTALLED NEW SPLICE REPAIR AT RAIL IAW SRM 53-00-53-2R-2 ALTERNATIVE 5.

Part: TRACK — CORRODED (BS 749) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON TRACK AT BS 749 RBL 13 WL 156. REMOVED CORROSION ON TRACK AT BS 749 RBL 13 WL 156. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4.B (2). REMOVED ACB TRACK FROM BS 727 TO BS 887 RBL 13 WL 156 IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW ACB TRACK IAW SRM 51-40-05-0G-0 AND DRAWING #146A7501.

Part: SKATE ANGLE — CHAFED (BS 1007-1016) · airframe 53,110 hrs · 31,655 cycles

FIN TO BODY SKATE ANGLE IS CHAFED AT B.S. 1007-1016; L.B.L. 14; W.L. 306.5. ; / [01] FIN TO BODY SKATE ANGLE AT BS 1007-1016; LBL 14; WL 306.5 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM; IT'LL BE REAPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; [02] REMOVED FIN TO BODY SKATE ANGLE AT BS 1007-1016; LBL 14; WL 306.5 IAW SRM 51-40-02-0G-0; [03] VERIFIED ITEM 2.; [04] LOCATED AND DRILLED NEW SKATE ANGLE AT BS 1007 TO BS 1016 LBL 14 WL 306.5 IAW SRM 51-40-05-0G-0<BR>AND OK TO INSTALL; [05] VERIFIED OUT OF LIMITS; DRILL OF NEW PART; OK TO INSTALL; [06] INSTALLED NEW SKATE ANGLE AT BS 1007 TO BS 1016 IAW SRM 51-40-02-0G-0 AND DWG 147A0030; [07] VERIFIED INSTALLATION NEW SKATE ANGLE AT BS1007-1016 LBL14 WL306.5 PER SRM 51-40-02-0G-0 AND BOEING DWG 147A0030; [08] APPLIED ABRASION RESISTANT TEFLON COATING ON NEW SKATE ANGLE PER REF SOPM 20-44-01; [09] VERIFIED TEFLON COATING ON SKATE ANGLE PER SOPM 20-44-01; [10] JOB TASK IS ACCOMPLISHED PER SRM 51-40-02 AND BOEING DWG 147A0030

Part: SKATE ANGLE — CHAFED (BS 1016-1019) · airframe 53,110 hrs · 31,655 cycles

FIN TO BODY SKATE ANGLE IS CHAFED AT B.S. 1016-1019; L.B.L. 14; W.L. 306.5. ; / [01] VERIFY SRM 53-80-71-2R-6 REPAIR 6 IS APPLICABLE FOR THIS AIRCRAFT.; [02] FIN TO BODY SKATE ANGLE AT BS 1016-1019 LBL 14; WL 306.5 FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-OG-O; [03] CUT AND REMOVED DAMAGE ON FIN TO BODY SKATE ANGLE AT BS 1016-1025 LBL 14; WL 306.5 IAW SRM 53-80-71-2R-6; REPAIR 6.; [04] FORMED ANGLE REPAIR; FROM MATERIAL 2024T0; 0.063' CLAD SHEET LOT# 1375061-1 IAW SRM 53-80-71-2R-6 REPAIR 6 REQ. HT TO T42 CONDITION; [05] VERIFIED PART IS OUT OF LIMITS; AND NEW PART FORMED AWAITING HEAT TREAT; [06] REQ; HFEC ON CUT OUT FOR FREE CRACK CONDITION; ALL OPEN HOLE AND COUNTERSINK OPEN HOLE. 53-80-71-2R-6 REPAIR 6; [07] HFEC INSP CUT OUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [08] HFEC INSP OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071 EQUIP ID#: ATS2407 S/N: MM1591DD064104; [09] HFEC INSP COUNTERSINKS IAW 737 NDTM PART 6 53-30-00 PROCEDURE 3; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071 EQUIP ID#: ATS2407 S/N: MM1591DD064104; [10] RECEIVED FORMED ANGLE REPAIR FROM OSS TO HEAT TREATMENT T42 PO NBR 827968 IAW SRM 53-80-71-2R-6 REPAIR 6; [11] LOCATED AND DRILLED REPAIR ANGLE IAW SRM 53-80-71-2R-6 REPAIR 6 FABRICATED STRAP FROM MATERIAL 2024T3; 0.080' CLAD SHEET LOT# 1447572-1 IAW SRM 53-80-71-2R

Part: SUPPORT ANGLE — CRACKED (BS 915) · airframe 53,110 hrs · 31,655 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS915 RBL14 WL170. ; / [01] NO ALLOWABLE DAMAGE FOUND AT SRM FOR THIS PART; PART REQUIRED TO BE REMOVE AND REPLACE PER SRM 51-10-02-0G-0 PAR 9.; [02] VERIFIED; [03] REMOVED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS 915 RBL 14 WL 170 IAW SRM 51-40-02-0G-0<BR><BR>LOCATED AND DRILLED NEW SUPPORT ANGLE P/N 147A7221Y32 AND PO # 820970/6; BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS 915 RBL 14 WL 170 IAW SRM 51-40-05 AND DWG 147A7221.<BR><BR>OK TO INSTALL.; [04] VERIFIED - REMOVED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS 915 RBL 14 WL 170 IAW SRM 51-40-02-0G-0 <BR><BR>LOCATED AND DRILLED NEW SUPPORT ANGLE P/N 147A7221Y32 AND PO # 820970/6; BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS 915 RBL 14 WL 170 IAW SRM 51-40-05 AND DWG 147A7221. <BR><BR>OK TO INSTALL.; [05] INSTALLED SUPPORT ANGLE P/N 147A7221Y32 AND PO # 820970/6; BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS 915 RBL 14 WL 170 IAW SRM 51-40-02-0G-0 AND DWG 147A7221 REV:-; [06] VERIFIED THE INSTALLATION OF THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0 AND DWG 147A7221 REV-

Part: ATTACH ANGLE — CRACKED (BS 866) · airframe 53,110 hrs · 31,655 cycles

CRACKED BULKHEAD SUPPORT ATTACH ANGLE AT AFT CARGO BAY BS866 LBL10 WL166. ; / [01] NO ALLOWABLE DAMAGE FOUND IN SRM FOR THIS PART . PART REQUIRED TO BE REMOVED AND REPLACE IAW SRM 51-10-02-0G-0 PAR 9.; [02] VERIFIED; [03] REMOVED BULKHEAD SUPPORT ATTACH ANGLE AT AFT CARGO BAY BS 866 LBL10 WL 166 IAW 51-40-02-0G-0; [04] LOCATE AND DRILL NEW BULKHEAD SUPPORT ATTACH ANGLE AT AFT CARGO BAY BS 866 LBL10 WL 166; ITEM# 149A8109U114 IAW 51-40-05-0G-0; [05] LOCATE AND DRILL NEW BULKHEAD SUPPORT ATTACH ANGLE AT AFT CARGO BAY BS 866 LBL10 WL 166; ITEM# 149A8109U114 IAW 51-40-05-0G-0 OK TO INSTALL; [06] VERIFIED LOCATE AND DRILL OF NEW BULKHEAD SUPPORT ATTACH ANGLE AT AFT CARGO BAY BS 866 LBL10 WL 166<BR>OK TO INSTALL; [07] INSTALLED NEW BULKHEAD SUPPORT ATTACH ANGLE AT AFT CARGO BAY BS 866 LBL10 WL 166; ITEM#149A8109U114 IAW 51-40-02-0G-0 ; AIPC 53-42-51-06; [08] UPDATED MEASUREMENT; [09] VERIFIED INSTALLED NEW BULKHEAD SUPPORT ATTACH ANGLE AT AFT CARGO BAY BS 866 LBL10 WL 166; ITEM#149A8109U114 IAW 51-40-02-0G-0.

Part: SHIELD — CORRODED (BS 767-787) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767 - 787 RBL22 WL157. ; / [01] NO ALLOWABLE DAMAGE FOUND ON SRM ; REMOVED SHIELD FROM AFT CARGO BAY BS 767-787 RBL22 WL 157<BR>IAW SRM 51-40-02; [02] CORROSION ON SHIELD NO ALLOWABLE DAMAGE FOUND ON SRM THEREFORE IS OUT OF LIMITS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9 C; [03] VERIFIED SHIELD IS OUT OF LIMITS PER SRM 51-10-02.; [04] RECEIVED NEW SHIELD ITEM# 7531132 LOCATED AND DRILLED AT BS767 -BS794 RBL 22 WL 157 IAW SRM 51-40-05-0G-0 AND DWG# 146A127; [05] VERIFIED - RECEIVED NEW SHIELD ITEM# 7531132 LOCATED AND DRILLED AT BS767 -BS794 RBL 22 WL 157 IAW SRM 51-40-05-0G-0 AND DWG# 146A127; [06] OK TO INSTALL SHIELD AT BS767 -BS794 RBL 22 WL 157; [07] OK TO INSTALL SHIELD AT BS767 -BS794 RBL 22 WL 157 GIVEN; [08] CIC APPLICATION AND CURED DID BUY ON NRC FUSELAGE 1112; [09] INSTALLED FWD SHIELD AT AFT CARGO BAY FROM BS767 -BS794 RBL 22 WL 157 IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A0081 REV:A; [10] VERIFIED INSTALLED FWD SHIELD AT AFT CARGO BAY FROM BS767 -BS794 RBL 22 WL 157 IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A0081 REV:A; [11] VERIFIED CARD COMPLETE

Part: FRAME SPLICE — CORRODED (BS 787-S24R) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON FRAME AT AFT CARGO BAY BS787 S-24R WL161. ; / [01] ON FURTHER INVESTIGATION CORROSION FOUND ON ACB FRAME SPLICE BS 787 STR 24R WL 161 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9C; [02] VERIFIED - CORROSION FOUND ON ACB FRAME SPLICE BS 787 STR 24R WL 161 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9C; [03] REMOVED ACB FRAME SPLICE BS 787 STR 24R WL 161 IAW SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW FRAME SPLICE P/N 146A1300U3 LOT#1461884-1 IAW SRM 51-40-05 FIG 3 AND DWG #146A1262. OK TO INSTALL; [05] VERIFIED LOCATE AND DRILL OF NEW FRAME SPLICE IAW SRM 51-40-05 FIG 3 AND DWG #146A1262. OK TO INSTALL; [06] INSTALLED NEW FRAME SPLICE AT BS 787; STR 24R PER SRM 51-40-02 AND DWG#146A1262; [07] VERIFIED INSTALLED NEW FRAME SPLICE AT BS 787; STR 24R PER SRM 51-40-02 AND DWG#146A1262.; [08] VERIFIED CARD COMPLETE; [09] VERIFIED CARD COMPLETE

Part: SKATE ANGLE — CHAFED (BS 1007-1016) · airframe 53,110 hrs · 31,655 cycles

FIN TO BODY SKATE ANGLE IS CHAFED AT B.S. 1007-1016; R.B.L. 14; W.L. 306.5. FIN TO BODY SKATE ANGLE IS CHAFED. FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM. LOCATED AND DRILLED NEW SKATE ANGLE IAW SRM 51-40-05-0G-0. INSTALLED NEW SKATE ANGLE IAW SRM 51-40-02-0G-0 AND DWG 147A0030. APPLIED ABRASION RESISTANT TEFLON COATING ON NEW SKATE ANGLE IAW SOPM 20-44-01.

Part: SIDEWALL SUPPORT — CORRODED (BS 945) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS945 RBL21 WL180. REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AND FOUND TO BE OUT OF LIMITS IAW SRM53-00-53-1A-2. REMOVED SIDEWALL SUPPORT, FABRICATED FLOOR TO SIDEWALL SUPPORT, LOCATED AND DRILLED IAW SRM 51-40-05 ;DWG# 147A7501 REV A.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS947 LBL8 TO RBL15 WL180. ; / [01] NO ALLOWABLE DAMAGE FOUND AT SRM FOR THIS PART; PART REQUIRED TO BE REMOVED AND REPLACE IAW SRM 51-10-02-0G-0 PAR 9.; [02] VERIFIED; [03] REMOVED AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS 947; LBL8 TO RBL 15 WL 180; IAW SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS 947; LBL8 TO RBL 15 WL 180 ITEM# 149A8118U29 LOT#1461545 IAW SRM 51-40-05-0G-0 ; OK TO INSTALL; [05] NO ALLOWABLE DAMAGE FOUND AT SRM FOR THIS PART; PART REQUIRED TO BE REMOVED AND REPLACE IAW SRM 51-10-02-0G-0 PAR 9.; [06] VERIFIED OK TO INSTALL.; [07] INSTALLED NEW AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS 947; LBL8 TO RBL 15 WL 180 ITEM# 149A8118U29 LOT#1461545 ; IAW SRM 51-40-02-0G-0; DWG#149A8117; [08] UPDATED PARTS USAGE; [09] VERIFIED INSTALLED NEW AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS 947; LBL8 TO RBL 15 WL 180 ITEM# 149A8118U29 LOT#1461545 ; IAW SRM 51-40-02-0G-0; DWG#149A8117.; [10] RE-VERIFIED INSTALLED NEW AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS 947; LBL8 TO RBL 15 WL 180 ITEM# 149A8118U29 LOT#1461545 ; IAW SRM 51-40-02-0G-0; DWG#149A8117.

Part: FLOOR SUPPORT — CORRODED (BS 887) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS887 BL0 WL168. ; / [01] CORROSION FOUND ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS887 BL0 WL168 FOUND TO BE OUT LIMITS DUE TO NO LIMITS ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9.C; [02] FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS887 BL0 WL168 FOUND TO BE OUT LIMITS DUE TO NO LIMITS ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9.C; [03] VERIFIED OUT OF LIMITS AND PART TO BE REPLACED; [04] ADD P/N; [05] RECEIVED AND REPLACED NEW AFT CARGO BAY FLOOR SUPPORT SPLICE BS 887 BL0 WL 168 ITEM #7530863 ; PART# 146A9401U39 IAW SRM 51-10-02-0G-0 PAR 9.C; [06] RECEIVED AND REPLACED NEW AFT CARGO BAY FLOOR SUPPORT SPLICE BS 887 BL0 WL 168 ITEM #7530863 ; PART# 146A9401U39 IAW SRM 51-10-02-0G-0 PAR 9.C PART WILL BE INSTALLED ON CUSTOMER CARD TTG8Q004CEMC; [07] VERIFIED RECEIPT OF NEW PART AND INSTALLATION FAULT

Part: STRINGER CLIP — BENT (BS 747 S23R) · airframe 53,110 hrs · 31,655 cycles

BENT STRINGER CLIP AT AFT CARGO BAY BS747 S-23R WL164. ; / [01] BENT STRINGER CLIP AT BS 747; S23R; WL 164 WILL BE REPLACED ON CUSTOMER CARD# TTG8Q005L9ML; EA 21-153-01805-WIP1 STEP 14; [02] VERIFIED BENT STRINGER CLIP AT BS 747; S23R; WL 164 WILL BE REPLACED ON CUSTOMER CARD# TTG8Q005L9ML; EA 21-153-01805-WIP1 STEP 14; [03] BENT STRINGER CLIP AT BS 747; S23R; WL 164 WILL BE FABRICATED ON STEP 14 AND INSTALLED ON STEP 18 ON CUSTOMER CARD# TTG8Q005L9ML; EA 21-153-01805-WIP1.; [04] ADDED STEP 18 FOR INSTALLATION OF STRINGER CLIP.; [05] EDIT TO CORRECT DOCUMENTATION TO: VERIFIED BENT STRINGER CLIP AT BS 747; S23R; WL 164 WILL BE FABRICATED ON STEP 14 AND INSTALLED ON STEP 18 ON CUSTOMER CARD# TTG8Q005L9ML; EA 21-153-01805-WIP1

Part: SEAT TRACK — CORRODED (BS 773) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON RAIL AT BS 773 LBL 2.5 WL 156 ; / [01] EVALUATED CORRODED AREA ON RAIL AT BS 773 LBL 2.5 WL 156; <BR>AND FOUND TO BE OUT OF LIMITS DUE TO EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 PART 4A(2) DETAIL 'D'; MEASURES L=2.1 X W=0.9 X D= 0.016'' FROM ORIGINAL THICKNESS OF TH=0.063'' TOOL USED DIAL DEPTH GAUGE P/N 643JZ(ATS400); PIN POINT MICROMETER P/N 112-225(ATS1671) S/N 65093024; [02] EVALUATED CORRODED AREA ON RAIL AT BS 773 LBL 2.5 WL 156; <BR>AND FOUND TO BE OUT OF LIMITS DUE TO EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 PART 4A(2) DETAIL 'D'; MEASURES L=2.1 X W=0.9 X D= 0.016'' FROM ORIGINAL THICKNESS OF TH=0.063''. FOUND TO BE OUT OF LIMITS DUE TO EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 STEP 4. A. (2) DETAIL 'D'; MEASURES L=2.1 X W=0.9 X D=0.016'' FROM ORIGINAL THICKNESS OF TH=0.063''. VERIFY SRM 53-00-53-2R-2 REPAIR 2; IS APPLICABLE TO THIS A/C. REMOVED DAMAGE CUT OUT THE UPPER FLANGE ON RAIL AT BS 773 LBL 2.5 WL 156 IAW SRM 53-00-53-2R-2 REPAIR 2. LOCATED AND DRILLED NEW SPLICE REPAIR ON RAIL AT BS 773 LBL 2.5 WL 156 IAW SRM 53-00-53-2R-2 ALTERNATIVE 5.

Part: WEB — CORRODED (BS 796) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON WEB AT AFT CARGO BAY BS796 RBL19 WL157. ; / [01] EVALUATED CORRODED AREA ON WEB AT ACB BS796 RBL19 WL157 AND FOUND TO BE OUT OF LIMITS DUE TO CORROSION IS OVER FASTENER HOLE IAW SRM 53-60-15-1A-1 PART 4G(2) DETAIL D.; [02] VERIFIED EVALUATION OF CORRODED AREA ON WEB AT ACB BS796 RBL19 WL157 AND FOUND TO BE OUT OF LIMITS DUE TO CORROSION IS OVER FASTENER HOLE IAW SRM 53-60-15-1A-1 PART 4G(2) DETAIL D.; [03] REMOVED WEB ON ACB BS794 TO 847 RBL19 WL157 IAW SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW WEB P/N 146A8123-25 AT ACB BS794 TO 847 RBL19 WL157 IAW SRM 51-40-05-0G-0 AND DRAWING# 143A8123; [05] VERIFIED LOCATED AND DRILLED NEW WEB P/N 146A8123-25 AT ACB BS794 TO 847 RBL19 WL157 IAW SRM 51-40-05-0G-0 AND DRAWING# 143A8123; [06] OK TO INSTALL NEW WEB P/N 146A8123-25 AT ACB BS794 TO 847 RBL19 WL157; [07] GAVE OK TO INSTALL NEW WEB P/N 146A8123-25 AT ACB BS794 TO 847 RBL19 WL157; [08] INSTALLED NEW WEB P/N 146A8123-25 AT ACB BS794 TO 847 RBL19 WL157 IAW SRM 51-40-02-0G-0 AND DRAWING# 143A8120 REV -; [09] VERIFIED INSTALLED NEW WEB P/N 146A8123-25 AT ACB BS794 TO 847 RBL19 WL157 IAW SRM 51-40-02-0G-0 AND DRAWING# 143A8120 REV -; [10] VERIFIED ALL STEPS COMPLETE.

Part: SUPPORT — CORRODED (BS 757-807 LBL21) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 757-807 LBL 21 WL 156 ; / [01] REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT ANGLE BS 757 TO BS 807 LBL 21 WL 156 IN AREA OF 1''X1'X 0.020' DEEP FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 DETAIL 4A(2)A FIG 103-D; [02] TOOLS USED MICR0METER ID ATS1671; S/N 65093024; [03] ORIGINAL MATERIAL THICKNESS 0.040'; [04] VERIFIED REMOVAL OF CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT ANGLE BS 757 TO BS 807 LBL 21 WL 156 IN

Part: SUPPORT — CORRODED (BS 727C-767) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727C+9-767 RBL 22 WL 156 ; / [01] REMOVED CORROSION FROM ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727C+9 TO BS 767 RBL 22 WL 156 IN AREA OF 2' X 2' X 0.015' DEEP FOUND TO BE OUT OFF LIMIT IAW 53-00-53-1A-1 DETAIL 4A(2)A FIG.103-D<BR>TOOLS USED MICR0METER ID ATS1671; S/N 65093024; [02] ORIGINAL MATERIAL THICKNESS 0.040'; [03] VERIFIED REMOVAL OF CORROSION FROM ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727C+9 TO BS 767 RBL 22 WL 156 IN AREA OF 2' X 2' X 0.015' DEEP FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 DETAIL 4A(2)A FIG.103-D<BR>TOOLS USED MICR0METER ID ATS1671; S/N 65093024; [04] FABRICATED; LOCATED AND DRILLED ACB FLOOR TO SIDEWALL SUPPORT ANGLE MADE FROM BAC1496-377#7075T62 LOT#1459405-1 AT BS 727 TO BS 767 RBL 22 WL 156 IAW SRM 51-40-05-0G-0 AND DWG# 146A7502

Part: SUPPORT — CORRODED (BS 727B-767) · airframe 53,110 hrs · 31,655 cycles

CORROSION AT AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 727B+9-767 LBL 22 WL 156 ; / [01] REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT ANGLE BS 727B+9 TO BS 767 LBL 22 WL 156 IN AREA OF 2''X1'X 0.025' DEEP FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 DETAIL 4A(2)A FIG 103-D<BR>TOOLS USED MICR0METER ID ATS1671; S/N 65093024; [02] ORIGINAL MATERIAL THICKNESS 0.040'; [03] VERIFIED REMOVAL OF CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT ANGLE BS 727B+9 TO BS 767 LBL 22 WL 156 IN AREA OF 2''X1'X 0.025' DEEP FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 DETAIL 4A(2)A FIG 103-D <BR>TOOLS USED MICR0METER ID ATS1671; S/N 65093024; [04] FABRICATED NEW SECTION OF SIDEWALL SUPPORT FROM MATERIAL BAC1496-377 7075T62 LOT NBR 1459405-1PER REF SRM 53-00-53-2R-5 OK TO TREAT AND PAINT; [05] VERIFIED FABRICATION PER SRM. VERIFIED OK TO TREAT AND PRIME.; [06] APPLIED CHEMICAL CONVERSION COATING AND PRIMED NEW ACB FLOOR TO SIDE SIDEWALL SUPPORT ANGLE AND SPLICER ANGLE BS 727 TO BS 847 LBL 22 WL 156 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02; [07] VERIFIED APPLICATION OF CHEMICAL CONVERSION COATING AND PRIMER TO NEW ACB FLOOR TO SIDE SIDEWALL SUPPORT ANGLE AND SPLICE ANGLE BS 727 TO BS 847 LBL 22 WL 156 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02.; [08] APPLIED PAINT ON AFT CARGO BAY FLLOR TO SIDEWALL SUPPORT ANGLE AND SPLICE ANGLE AT BS727-BS847 LBL22 WL156 IAW AMM 51-21-99-300-801; TIME OF APPLICATION:22:00HRS.

Part: FLOORBEAM — CORRODED (BS 773) · airframe 53,110 hrs · 31,655 cycles

CORROSION AT AFT CARGO BAY FLOOR SUPPORT SPLICE BS 773 LBL 20-RBL 19 WL 157 ; / [01] CORROSION FOUND ON AFT CARGO BAY FLOOR SUPPORT SPLICE BS773 LBL20-RBL19 WL157 FOUND TO BE OUT LIMITS DUE TO NO LIMITS ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9.C .; [02] RECEIVED AND REPLACED NEW AFT CARGO BAY FLOOR SUPPORT SPLICE BS 773 LBL 20- RBL 19 WL 157 ITEM #3530573 ; PART# 146A9401-4 IAW SRM 51-10-02-0G-0 PAR 9.C; [03] ADDED PART INFORMATION USAGE; [04] RECEIVED AND REPLACED NEW AFT CARGO BAY FLOOR SUPPORT SPLICE BS 773 LBL 20- RBL 19 WL 157 ITEM #3530573 ; PART# 146A9401-4 IAW SRM 51-10-02-0G-0 PAR 9.C; [05] VERIFIED OUT OF LIMITS DUE TO NO LIMITS. NEW PART RECEIVED

Part: SUPPORT — CORRODED (BS 869 RBL21) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS896 RBL21 WL169. ; / [01] REMOVED CORROSION FROM ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 896 RBL 21 WL 169 IN AREA OF 2.5' X 1.2' X 0.008' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BE OUT OFF LIMIT IAW 53-00-53-1A-1 DETAIL 4A(2)A FIG.103-D<BR>TOOLS USED MICR0METER ID ATS1671; S/N 65093024; [02] VERIFIED REMOVAL OF CORROSION FROM ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 896 RBL 21 WL 169 IN AREA OF 2.5' X 1.2' X 0.008' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-1 DETAIL 4A(2)A FIG.103-D <BR>TOOLS USED MICR0METER ID ATS1671; S/N 65093024; [03] WORK WILL BE ACCOMPLISHED IN CUSTOMER CARD # TTG8Q005GV0N; [04] CORRECTION STEP 3 WORK WILL BE ACCOMPLISHED IN CUSTOMER CARD TTG8Q005GVMC; [05] VERIFIED INSTALLATION OF ACB FLOOR TO SIDE WALL SUPPORT ANGLE WILL BE ACCOMPLISHED IN CUSTOMER CARD TTG8Q005GVMC; [06] VERIFIED CARD COMPLETE; [07] CORRECTED MEASUREMENTS SECTION ITEM #15; [08] COMPLETE

Part: ATTACH ANGLE — CRACKED (BS 440) · airframe 53,110 hrs · 31,655 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS440 LBL25 WL155. MARKED ; / [01] REMOVED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS440 LBL25 WL155 IAW SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW INTERCOSTAL ATTACH ANGLE P/N143A7502-19 AT FWD CARGO BAY BS440 LBL25 WL155 IAW SRM 51-40-05-0G-0 AND DWG# 143A7505; OK TO INSTALL.; [03] VERIFIED LOCATE AND DRILL OF NEW INTERCOSTAL ATTACH ANGLE P/N143A7502-19 AT FWD CARGO BAY BS440 LBL25 WL155 IAW SRM 51-40-05-0G-0 AND DWG# 143A7505; OK TO INSTALL; [04] INSTALLED NEW INTERCOSTAL ATTACH ANGLE P/N #143A7502-19 AT FWD CARGO BAY BS440 LBL25 WL155 IAW SRM 51-40-02-0G-0 AND DWG# 143A7505; [05] INSTALLED NEW INTERCOSTAL ATTACH ANGLE P/N #143A7502-19 AT FWD CARGO BAY BS440 LBL25 WL155 IAW SRM 51-40-02-0G-0 AND DWG# 143A7505; [06] INSPECTED; [07] RII INSPECTED

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 53,110 hrs · 31,655 cycles

AFT CARGO BAY FLOOR PANEL; 140CF; IS DAMAGED. ; / [01] FABRICATED NEW ACB FLOOR PANEL 140CF FROM 080 2024T-3; LOT# 1461546-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] VERIFIED PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 53,110 hrs · 31,655 cycles

AFT CARGO BAY FLOOR PANEL; 140DF; IS DAMAGED. ; / [01] FABRICATED NEW ACB FLOOR PANEL 140DF FROM 090 CONOLITE; LOT# 1458090-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] VERIFIED PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 53,110 hrs · 31,655 cycles

WHILE ACCOMPLISHING HFEC INSPECTION; FOUND 1 EA CRACK ON R/H HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB 4 IN. AFT OF THE DRAIN HOLE; AREA MARKED ; / [01] REMOVED PANEL 341BZ AT R/H STAB FRONT SIDE IAW SRM 51-42-02; [02] TRIMMED OUT THE DAMAGED PART AT R/H HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB 4 IN. AFT OF THE DRAIN HOLE DIMENSIONS L=1.6 '<BR> W= 0.8' IAW SRM 51-10-02; [03] VERIFIED DAMAGE REMOVED AT RH HORIZONTAL STAB LOWER IN SPAR SKIN STATION 184.70 IAW SRM 51-10-02<BR><BR>NO OTHER DEFECTS NOTED.; [04] HFEC REQUEST AT THE EDGES OF THE CUT OUT TO ENSURE NO CRACKS EXIST.; [05] ET INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>CAL ID IS000450 N500D; [06] REMOVED AFT O/B DOUBLER AT R/H HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 175 IAW SRM 51-42-02. [11] DAMAGE REPAIRED PER EA 21-155-01748. REPETITIVE INSPECTION PROGRAM DEFINED IN EA 155-01748-INSP; [12] VERIFIED DAMAGE REPAIRED PER EA 21-155-01748. REPETITIVE INSPECTION PROGRAM DEFINED IN EA 155-01748-INSP

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON SUPPORT INTERCOSTAL AT B.S. 259-270 AT L.B.L. 3 - R.B.L. 3; W.L. 207.54. REMOVED CORROSION ON SUPPORT INTERCOSTAL AT B.S. 259-270 AT LBL-3 TO RBL-3 WL 207.54. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1 STEP 4.B.(2)(A)(C). LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-02-0G-0 AND DWG 141A5211. INSTALLED INTERCOSTAL IAW SRM 51-40-02-0G-0 AND DWG141A5210.

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 53,110 hrs · 31,655 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED ; / [01] REMOVED GUSSET AT FWD CARGO BAY LOCATED BTW BS.500D WL193;S-19L PER SRM 51-40-02.; [02] LOCATED AND DRILLED GUSSET WITH P/N 143A9481-6; LOT#1457203-12 IAW SRM 51-40-05; AND DWG# 143A7902. OK TO INSTALL.; [03] VERIFIED LOCATED AND DRILLED GUSSET WITH P/N 143A9481-6; LOT#1457203-12 IAW SRM 51-40-05; AND DWG# 143A7902. OK TO INSTALL.; [04] INSTALLED NEW FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET BS500D; S-19L; WL193. P/N 143A9481-6; LOT#1457203-12 IAW SRM 51-40-02; AND DWG# 143A7902.; [05] INSTALLED NEW FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET BS500D; S-19L; WL193. P/N 143A9481-6; LOT#1457203-12 IAW SRM 51-40-02; AND DWG# 143A7902; [06] VERIFIED INSTALLATION OF NEW FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET BS500D; S-19L; WL193. P/N 143A9481-6; LOT#1457203-12 IAW SRM 51-40-02; AND DWG# 143A7902; [07] VERIFIED COMPLETION OF CUSTOMER CARD TTG8Q005GJ7X

Part: SHIELD — CORRODED (BS 500-500A) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL156. CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C. INSTALLED AFT SHIELD AT FWD CARGO BAY BS.500-BS500A RBL.23 WL156 PER SRM 51-40-02, DWG#143A0080.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 53,110 hrs · 31,655 cycles

AFT CARGO BAY FLOOR PANEL; 14OAF; IS DAMAGED. ; / [01] FABRICATED NEW ACB FLOOR PANEL 140AF FROM 090 CONOLITE; LOT# 1458090-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] VERIFIED PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 53,110 hrs · 31,655 cycles

AFT CARGO BAY FLOOR PANEL; 140BF; IS DAMAGED. ; / [01] FABRICATED NEW ACB FLOOR PANEL 140BF FROM 090 CONOLITE; LOT# 1458090-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] VERIFIED PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 53,110 hrs · 31,655 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25 WL155. ; / [01] REMOVED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25; WL155 IAW SRM 51-40-02.<BR><BR>LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05 OK TO INSTALL; [02] LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05 AND DWG 143A7505<BR> OK TO INSTALL; [03] VERIFIED LOCATION AND DRILLING OF ANGLE PER SRM AND DWG. VERIFIED OK TO INSTALL.; [04] INSTALLED NEW INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25; WL155 IAW SRM 51-40-02 AND DWG 143A7505; [05] VERIFIED ATTACH ANGLE INSTALL PER SRM AND DWG.; [06] COMPLETE

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 53,110 hrs · 31,655 cycles

FORWARD CARGO BAY FLOOR PANEL; 120AF; IS DAMAGED. ; / [01] FABRICATED NEW FCB FLOOR PANEL 120AF FROM 090 CONOLITE ; LOT# 1458090-1 PER AMM 25-52-01-201-801 AND DWG 453A1610; [02] VERIFIED PER AMM 25-52-01-201-801 AND DWG 453A1610

Part: WEB — CORRODED (BS 440-490) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS440 - BS490 RBL27 WL156. REMOVED CORROSION ON SUBTHRESHOLD WEB , FOUND TO BE OUT OF LIMITS REWORKED AREAS SRM 53-30-15-1A-1. INSPECTED REMOVED CORROSION ON SUBTHRESHOLD WEB IAW SRM 51-10-02. REMOVED FCB SUBTHRESHOLD WEB IAW SRM 51-40-02. LOCATED AND DRILLED NEW FCB SUBTHRESOLD FROM BS440 - BS490 IAW SRM 51-40-05 AND IAW DWG#143A8330. INSTALLED FCD SUBTHRESHOLD WEB FROM BS440-BS490 IAW SRM 51-40-02 AND IAW DWG#143A8330.

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156. ; / [01] REMOVED SIDEWALL SUPPORT ANGLE AT BS500A-500D; RBL23; WL156 IAW SRM 51-40-02 <BR>REMOVED CORROSION ON SIDEWALL SUPPORT ANGLE L:2'; W:1'; D:0.009';WAS FOUND OUT OF LIMIT DUE MATERIAL LOSS EXCEED 10% OF THICKNESS IAW SRM 53-00-53-1A-2; [02] VERIFIED; [03] FABRICATED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A-BS500D RBL23 WL156; FROM EXTRUSION BAC1496-444#7075T62 LOT#1440365-1; IAW SRM 51-40-05-0G-0 AND DWG 143A7500;

Part: SUPPORT — CORRODED (BS 500-500D) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500 - BS500D LBL23 WL156. ; / [01] SIDEWALL SUPPORT WAS REPLACED FRON BS 400- 500D LBL 23 ; WL 156; ON COSTUMER CARD TTG8Q005GER7; [02] SIDEWALL SUPPORT WAS REPLACED FROM BS 400- 500D LBL 23 ; WL 156; ON COSTUMER CARD TTG8Q005GER7; [03] VERIFIED FLOOR TO SIDEWALL SUPPORT IN FCB BS 400-BS 500D LBL 23 WL 156 WILL BE REPLACED ON CUSTOMER CARD TTG8Q005GER7.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 53,110 hrs · 31,655 cycles

FORWARD CARGO BAY FLOOR PANEL; 120CF; IS DAMAGED. ; / [01] FABRICATED NEW FCB FLOOR PANEL 120CF FROM 090 CONOLITE; LOT# 1458090-1 PER AMM 25-52-01-201-801 AND DWG 453A1610; [02] VERIFIED PER AMM 25-52-01-201-801 AND DWG 453A1610

Part: BEAM — CORRODED (BS 270) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON B.S. 270 LATERAL BEAM AT L.B.L. 10 - R.B.L. 10; W.L. 207.54. REMOVED EXISTING REPAIR AT BS 270 LBL.10 TO RBL.10 WL.207.54 IAW SRM 51-40-02-0G-0. FABRICATED A -1 STRAP AS SHOW IN SKETCH 2 REPAIR SKETCH FROM 0.063'' IAW EA-1-753-28470 STEP 8. VERIFIED FABRICATED A -1 STRAP. INSTALLED LATERAL BEAM STRAP IAW SRM 51-40-02-0G-0 AND EA 1-753-28470.

Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 53,110 hrs · 31,655 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE RBL25 WL155. ; / [01] REMOVED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE RBL25 WL155 IAW SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW INTERCOSTAL ATTACH ANGLE P/N143A7502-20 AT FWD CARGO BAY BS500C RBL25 WL155 IAW SRM 51-40-05-0G-0 AND DWG# 143A7505; OK TO INSTALL.; [03] VERIFIED LOCATE AND DRILLED NEW INTERCOSTAL ATTACH ANGLE P/N143A7502-20 AT FWD CARGO BAY BS500C RBL25 WL155 IAW SRM 51-40-05-0G-0 AND DWG# 143A7505; OK TO INSTALL.; [04] INSTALLED NEW INTERCOSTAL ATTACH ANGLE P/N143A7502-20 AT FWD CARGO BAY BS500C RBL25 WL155 IAW SRM 51-40-02-0G-0 AND DWG# 143A7505.; [05] INSTALLED NEW INTERCOSTAL ATTACH ANGLE P/N143A7502-20 AT FWD CARGO BAY BS500C RBL25 WL155 IAW SRM 51-40-02-0G-0 AND DWG# 143A7505.; [06] INSPECTED; [07] RII INSPECTED

Part: SUPPORT — CORRODED (BS 400-480) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400- BS480 LBL23 WL156. ; / [01] REMOVED SIDEWALL SUPPORT ANGLE AT BS400-480; LBL23; WL156 IAW SRM 51-40-02 <BR>REMOVED CORROSION ON SIDEWALL SUPPORT ANGLE L:1'; W:1'; D:0.008';WAS FOUND OUT OF LIMIT DUE MATERIAL LOSS EXCEED 10% OF THICKNESS IAW SRM 53-00-53-1A-2.; [02] VERIFIED; [03] FABRICATED; LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 400-BS500D LBL23 WL156 MADE FROM EXTRUSION BAC1496-444#7075T62; LOT#1457306-1 AND FABRICATED SPLICE ANGLE AT BS 480+9 LBL 23 WL 156 MADE FROM EXTRUSION BAC1496-444#7075T62; LOT#1457306-1 IAW SRM 51-40-05-0G-0 ;SRM 53-00-53-2R-5 REPAIR-5 AND DWG# 143A7501

Part: SIDEWALL SUPPORT — CORRODED (BS 400-420) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400-BS420 RBL23 WL156. ; / [01] REMOVED SIDEWALL SUPPORT ANGLE AT BS420; RBL23; WL156 IAW SRM 51-40-02<BR>REMOVED CORROSION ON SIDEWALL SUPPORT ANGLE L:1'; W:1'; D:0.010';WAS FOUND OUT OF LIMIT DUE MATERIAL LOSS EXCEED 10% OF THICKNESS IAW SRM 53-00-53-1A-2; [02] VERIFIED; [03] FABRICATED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400-BS420D RBL23 WL156; FROM EXTRUSION BAC1496-444#7075T62 LOT#1440365-1; IAW SRM 51-40-05-0G-0 AND DWG 143A7500; APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01-0G-0; OK TO PRIME.; [04] VERIFIED FABRICATED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400-BS420D RBL23 WL156; FROM EXTRUSION BAC1496-444#7075T62 LOT#1440365-1; IAW SRM 51-40-05-0G-0 AND DWG 143A7500;

Part: ATTACH ANGLE — CRACKED (BS 400) · airframe 53,110 hrs · 31,655 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155. ; / [01] REMOVED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155; IAW SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW INTERCOSTAL ATTACH ANGLE P/N143A7502-19 AT FWD CARGO BAY BS400 LBL25 WL155 IAW SRM 51-40-05-0G-0 AND DWG# 143A7505; OK TO INSTALL.; [03] VERIFIED LOCATE AND DRILL OF NEW INTERCOSTAL ATTACH ANGLE P/N143A7502-19 AT FWD CARGO BAY BS400 LBL25 WL155 IAW SRM 51-40-05-0G-0 AND DWG# 143A7505; OK TO INSTALL; [04] INSTALLED NEW INTERCOSTAL ATTACH ANGLE P/N143A7502-19 AT FWD CARGO BAY BS400 LBL25 WL155 IAW SRM 51-40-02-0G-0 AND DWG# 143A7505.; [05] INSTALLED NEW INTERCOSTAL ATTACH ANGLE P/N143A7502-19 AT FWD CARGO BAY BS400 LBL25 WL155 IAW SRM 51-40-02-0G-0 AND DWG# 143A7505.; [06] INSPECTED; [07] RII INSPECTED

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 53,110 hrs · 31,655 cycles

FORWARD CARGO BAY FLOOR PANEL; 120BF; IS DAMAGED. ; / [01] FABRICATED NEW FCB FLOOR PANEL 120BF FROM 080 2024T-3; LOT# 1461546-1 PER AMM 25-52-01-201-801 AND DWG 453A1610; [02] VERIFIED PER AMM 25-52-01-201-801 AND DWG 453A1610

Part: SHIELD — CORRODED (FUSELAGE) · airframe 53,110 hrs · 31,655 cycles

CORROSION ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL23 WL156. CORROSION FOUND ON FWD CARGO BAY BS420-BS440 RBL23 WL156 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C. VERIFIED - CORROSION FOUND ON FWD CARGO BAY BS420-BS440 RBL23 WL156 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ON SRM PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C. LOCATED AND DRILLED FWD SHIELD WITH P/N 143A8126-21; LOT.1461620-1 FROM FWD CARGO BAY BTW BS.420-440; PER SRM. 51-40-05;DWG# 143A0080. VERIFIED LOCATE AND DRILL FORWARD SHIELD BETWEEN BS.420-440 PER SRM 51-40-05;DWG# 143A0080. INSTALLED ON FWD. CARGO BAY FWD. SHIELD BTW. BS.420-BS 440;RBL.23;WL.156. PER SRM. 51-40-02; DWG#143A0080. REMOVED AND REPLACED FCB SHIELD BS420--440 RBL23WL 156.

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 53,110 hrs · 31,655 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8; W.L. 164. ; / [01] REMOVED DAMAGE; CUT OUT UPPER ANGLE AT BS 663; LBL 14 IAW 57-10-10-2R-5 REPAIR 5; RE 16; NO CRACKS NOTED.<BR><BR>CAL ID IS000450 N500D; [06] REQUEST A DETAIL INSPECTION OF THE REPAIR AREA AND UNDERLYING STRUCTURE TO MAKE SURE THAT THERE IS NOT A DAMAGE WITHIN THE REPAIR AREA IAW SRM 51-00-06.; [07] LOCATED AND DRILLED ANGLE REPAIR PARTS -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE AT BS 663; LBL 8; WL 164 IAW SRM 57-10-10-2R-5 REPAIR 5; SRM 51-40-05 AND DWG 111A1322. OK TO INSTALL.<BR><BR>APPLIED CHEMICAL CONVERSION COATING AND PRIMER ALL BARE METAL AND TRIM OUT AREA IAW SRM 51-20-01 AND SOPM 20-41-02.<BR><BR>-1 ANGLE VAPOR BARIER DOUBLER REPAIR ANGLE P/N ATSHFAB-101-351 LOT # 5082375-1. DWG 111A1322<BR><BR>-2 ANGLE VAPOR BARIER P/N ATSHFAB-101-351 LOT # 5082375-1. DWG 111A1322;

Part: PANEL — PULLED (RT WING TE) · airframe 53,110 hrs · 31,655 cycles

R/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES ; / [01] IDENTIFIED MATERIAL OF PANEL 661BB IAW SRM 57-51-01-0I-1 FIGURE 1 & 3; ITEM #9; TABLE 3<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 TABLE 101; PARA 4.B(5)<BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 4.B(2); 4.C(2) AND TABLE 202; [02] VALIDATED REPAIR TO T/E PANEL 661BB TO BE COMPLETED IAW SRM 51-70-04-2R-9 AS GIVEN IAW SRM 57-51-01-2R-1.; [03] VISUALLY EXAMINED EXTENT OF DAMAGE; TAP TESTED - DISBONDS NOTED; REMOVED DAMAGE BY UPSIZING FASTENER HOLES; LARGEST HOLE MEASURES 0.5' DIA; PREPPED AND CLEANED HOLES IAW SRM 51-70-04-2R-9 PARA 4.A-C; [04] VERIFIED;<BR><BR>IDENTIFIED MATERIAL OF PANEL 661BB IAW SRM 57-51-01-0I-1 FIGURE 1 & 3; ITEM #9; TABLE 3 <BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 TABLE 101; PARA 4.B(5) <BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 4.B(2); 4.C(2) AND TABLE 202 <BR><BR>VISUALLY EXAMINED EXTENT OF DAMAGE; TAP TESTED - DISBONDS NOTED; REMOVED DAMAGE BY UPSIZING FASTENER HOLES; LARGEST HOLE MEASURES 0.5' DIA; PREPPED AND CLEANED HOLES IAW SRM 51-70-04-2R-9 PARA 4.A-C; [05] SLURRIED FASTENER HOLES WITH 9390 RESIN LOT# JH1CAA0868 AND MILLED GLASS FIBERS LOT# 1437038-1 AND SET FOR CURE IAW SRM 51-70-04-2R-9 PARA 4.D-F;

Part: PANEL — DELAMINATED (RT WING LE) · airframe 53,110 hrs · 31,655 cycles

R/W L/E PANEL 621CB HAS CORNER DELAMINATED (MARKED) ; / [01] IDENTIFIED PANEL MATERIAL IAW SRM 57-41-01-0I-4 FIG 5 TABLE 5 ITEM 3.<BR>FOUND DELAMINATION DAMAGE TO 2EA CORNERS TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4A(5).<BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-05-2R-6 PER SRM 57-41-01-2R-1 TABLE 202.<BR>REMOVED 2EA BACKUP PLATES TO FACILITATE REPAIR IAW SRM 51-40-02-0G-0 PARA 4E.<BR>REMOVED ENTIRE ALUMINUM FOIL BACKING PLY TO FACILITATE REPAIR IAW SRM 51-70-14-2R-3 PARA 4A(2)(E).<BR>REMOVED ALL DAMAGE FROM INNER SURFACE; CLEANED REPAIR AREA; NO CONTAMINATION NOTED IAW SRM 51-70-05-2R-6 PARA 4A-D.; [02] VALIDATED REPAIR SRM 51-70-05-2R-6 PER SRM 57-41-01-2R-1.; [03] VERIFIED DELAMINATION DAMAGE TO 2EA CORNERS TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4A(5). <BR>VALIDATED REPAIR IAW SRM 51-70-05-2R-6 PER SRM 57-41-01-2R-1 TABLE 202. VERIFIED DAMAGE REMOVAL PER SRM 51-70-05-2R-6 PARA 4. [05] COMPLETED FABRICATION OF REPAIR PLIES USING BMS 8-79 ST 1581 LOT#1455461-1; AND BMS 5-129 LOT#1457270-4; INSTALLED; VACUUM BAGGED; CHECKED FOR LEAKS; AND SET TO CURE USING HEATCON HOTBONDER ID:IS000678 S/N:12071586 IAW SRM 51-70-05-2R-6 PAR 4E-G.;[13] REPAIRED DELAMINATED CORNERS ON PANEL 621CB IAW SRM 57-41-01; SRM 51-70-05-2R-6 AND SRM 51-70-14-2R-3; [14] VERIFIED REINSTALLATION OF BACKING PLATES PER SRM 51-40-02-0G-0 AND BOEING DWG 116A9110<BR><BR>VERIFIED REPAIR OF PANEL 621CB IAW SRM 57-41-01; SRM 51-70-05-2R-6 AND SRM 51-70-14-2R-3

Part: PANEL — PULLED (LT WING TE) · airframe 53,110 hrs · 31,655 cycles

L/W T/E PANEL 561BB HAS SEVERAL PULLED FASTENER HOLES ; / [01] IDENTIFIED MATERIAL OF PANEL 561BB IAW SRM 57-51-01-0I-1 FIGURE 1 & 3; ITEM #9; TABLE 3<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 TABLE 101; PARA 4.B(5)<BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 4.B(2); 4.C(2) AND TABLE 202; [02] VALIDATED REPAIR TO T/E PANEL 561BB TO BE COMPLETED IAW SRM 51-70-04-2R-9 AS GIVEN IAW SRM 57-51-01-2R-1.; [03] VISUALLY EXAMINED EXTENT OF DAMAGE; TAP TESTED - DISBONDS NOTED; REMOVED DAMAGE BY UPSIZING FASTENER HOLES; LARGEST HOLE MEASURES 0.5' DIA; PREPPED AND CLEANED HOLES IAW SRM 51-70-04-2R-9 PARA 4.A-C; [04] VERIFIED;<BR><BR>IDENTIFIED MATERIAL OF PANEL 561BB IAW SRM 57-51-01-0I-1 FIGURE 1 & 3; ITEM #9; TABLE 3 <BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 TABLE 101; PARA 4.B(5) <BR>VISUALLY EXAMINED EXTENT OF DAMAGE; TAP TESTED - DISBONDS NOTED; REMOVED DAMAGE BY UPSIZING FASTENER HOLES; LARGEST HOLE MEASURES 0.5' DIA; PREPPED AND CLEANED HOLES IAW SRM 51-70-04-2R-9 PARA 4.A-C <BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 4.B(2); 4.C(2) AND TABLE 202; [06] HOT BONDER ID ATS532; S/N 15092117 (SLURRY CURE)<BR><BR>CURED SLURRY; SANDED SLURRY TO CONTOUR; CLEANED REPAIR AREA; FABRICATED REPAIR PLIES FROM BMS 9-3 (1581) LOT# 1458851-1; INSTALLED REPAIR PLIES WITH 9390 RESIN LOT# JH1CAA0868;

Part: BLADE — DAMAGED (NR 1 ENGINE FAN) · airframe 51,365 hrs · 30,662 cycles

NR 1 ENG FAN BLADE NR 10 HAS DAMAGED CU-NI-IN COATING ON CONCAVE SIDE OUTSIDE AREA X. REMOVED AND REPLACED NR 10 FAN BLADE, IAW MT 772-21-20. SEE BLADE MAP FOR PROPER BLADE LOCATION. P/N OFF 340-001-038-0 S/N OFF DC973198-0 P/N ON 340-001-036-0 S/N ON DM019798-7.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,601 hrs · 30,188 cycles

AFT ENTRY DOOR INTERIOR/EXTERIOR EMERGENCY LIGHTS INOP. R/R BATTERY PACK AT POSITION M1673 PER AMM 33-51-06 PN OFF/ON D717-01-100SWA SN OFF 46464 SN ON 208967.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 49,306 hrs · 29,369 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 49,306 hrs · 29,369 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 49,306 hrs · 29,369 cycles

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

Part: LENS — DIRTY (EMERGENCY LIGHT) · airframe 47,843 hrs · 28,384 cycles

R/H SIDE FUSELAGE EXTERIOR LIGHT LENS FORWARD OF AFT CARGO BAY DOOR DIRTY. CLEANED LENS IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,843 hrs · 28,384 cycles

R/H OVERWING EXIT ESCAPE SLIDE LIGHT FORWARD OF AFT CARGO BAY DOOR INOP. R&R LAMP IAW AMM.

Part: SHIELD — CORRODED (BS 767-787) · airframe 47,843 hrs · 28,384 cycles

SHIELD CORRODED BETWEEN BS. 767 TO BS. 787, RBL 20. R&R SHIELD PER SRM.

Part: BRACKET — CRACKED · airframe 47,843 hrs · 28,384 cycles

BRACKET BS 663 RBL 45-54 WL 161 IS CRACKED / FORMED NEW BRACKET FROM 6013T4#0.063' LOT #1257343 IAW SRM 51-30-01 AND DWG 276A9183 REV -. REMOVED AND REPLACED BRACKET BS 663 RBL 45 TO RBL 54 WL 161 IAW SRM 51-40-02 AND DWG 111A1000 REF F 89004U 15JUN19

Part: NONE — CORRODED · airframe 47,843 hrs · 28,384 cycles

***CORROSION*** ON INTERCOSTAL BS 747-767 RBL22 WL 151 / REMOVED DAMAGED INTERCOSTAL AB BS 747 TO BS 767; RBL 22; WL 151; AND LOCATED; DRILLED AND INSTALLED NEW INTERCOSTAL PER SRM 51-40-02-0G AND SRM 51-40-05-0G

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 47,843 hrs · 28,384 cycles

VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT BS. 663, RBL 7. REPAIRED VAPOR BARRIER PER EA.

Part: SUPPORT — CORRODED (BS 727E-767) · airframe 47,843 hrs · 28,384 cycles

L/H AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS. 727E TO BS. 767. R&R SUPPORT IAW SRM & DWG.

Part: PLATE — CRACKED (R/H WING) · airframe 47,843 hrs · 28,384 cycles

RIGHT WING TRAILING WIGGLE PLATE IS CRACKED AT RSS 261 / WIGGLE PLATE RW T/E IS TO BE REPLACED ON CARD # T938670.

Part: RETAINER — CRACKED (LT WING) · airframe 47,843 hrs · 28,384 cycles

L/W T/E NO STEP PANEL SEAL RETAINER IS CRACKED AT ORSS 271. / REMOVED AND REPLACED FORWARD AND AFT SEAL RETAINERS ON LW TE NO STEP PANEL AT ORSS 271 PER SRM 51-40-02-0G-0; STEP 4 AND 9; AND AIPC 57-50-00-25.

Part: SKIN — DENTED (BS 360) · airframe 47,843 hrs · 28,384 cycles

FUSELAGE SKIN DENTED AT BS. 360+8.5, BELOW STR. 5L. / REPAIRED SKIN PER EA.

Part: SUPPORT — CORRODED (BS 727E-767) · airframe 47,843 hrs · 28,384 cycles

RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727E TO BS. 767. R & R SUPPORT IAW SRM AND DWG.

Part: SKIN — DENTED (BS 350) · airframe 47,843 hrs · 28,384 cycles

EXTERNAL SKIN DENTED AT BS. 350+5, BELOW STR. 5L. REPAIRED SKIN PER EA.

Part: PLATE — CRACKED (LT WING) · airframe 47,843 hrs · 28,384 cycles

L/H WING TRAILING EDGE WIGGLE PLATE AT ORSS. 261 CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: SKIN — DENTED (BS 360) · airframe 47,843 hrs · 28,384 cycles

FUSELAGE SKIN DENTED AT BS. 360+8, BELOW STR. 5L. REPAIRED SKIN PER EA.

Part: SKIN — DENTED (BS 360) · airframe 47,843 hrs · 28,384 cycles

FUSELAGE SKIN DENTED AT BS. 360+5, BELOW STR. 5L. REPAIRED SKIN PER EA.

Part: WEB — DAMAGED (DOOR FRAME) · airframe 47,843 hrs · 28,384 cycles

MAIN ELECTRONIC AND EQUIPMENT DOORWAY R/H FRAME HAD MECHANICAL DAMAGE ABOVE LATCH FITTING. R&R WEB IAW SRM AND DWG.

Part: SEAT TRACK — CRACKED (BS 480-520) · airframe 47,843 hrs · 28,384 cycles

CABIN SEAT TRACK HAD MECHANICAL DAMAGE AND APPEARED TO BE CRACKED BETWEEN BS. 480 TO BS. 520, LBL 45. / R&R SEAT TRACK PER SRM & DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 47,843 hrs · 28,384 cycles

FWD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / FORWARD CARGO BAY AFT CORNER SCUFF PLATE CRACK REPAIRED PER EA NO: 1-A53-2076 REV 11 59531U 06-11-2019.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 47,843 hrs · 28,384 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / REMOVED AFT CARGO BAY AFT CORNER SCUFF PLATE IAW EA NBR 1-A53-2076 REV 11. REPAIRED AFT CARGO BAY AFT CORNER SCUFF PLATE IAW EA NBR. 1-A53-2076 REV 11. REINSTALLED REPAIRED SCUFF PLATE IAW EA NBR. 1-A53-2076 REV 11. AND AMM 53-11-02-520-801 54819U 14JUN19

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 47,843 hrs · 28,384 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / REMOVED AFT CARGO BAY FWD CORNER SCUFF PLATE IAW EA NBR. 1-A53-2076 REV 11. REPAIRED AFT CARGO BAY FWD CORNER SCUFF PLATE IAW EA NBR. 1-A53-2076 REV 11. REINSTALLED REPAIRED SCUFF PLATE IAW EA NBR. 1-A53-2076 REV 11 AND AMM 53-11-02-420-801. 59817C 14JUN19

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 47,843 hrs · 28,384 cycles

CABIN SEAT TRACK HAD MECHANICAL DAMAGE AT BS. 520, LBL 25. REMOVED SEAT TRACK IAW SRM AND DWG.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 47,713 hrs · 28,302 cycles

R2 DOOR SLIDE CAUGHT ON DOOR SILL WHILE CLOSING. ADJUSTED R2 DOOR SLIDE PER MT.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 47,341 hrs · 28,049 cycles

DECLARED EMERGENCY, FLIGHT ATTENDANT REPORTED A BURNING ELECTRICAL ODOR IN THE FORWARD GALLEY AREA. RECIRCULATION FAN WAS LEFT ON GALLEY WORK LIGHT, TRIPPED CIRCUIT BREAKER. R&R GALLEY WORK LIGHT BALLAST PER AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 47,121 hrs · 27,905 cycles

R2 DOOR EXIT SIGN MISSING (NOT THE BIG ONE OVERHEAD BUT THE SMALL ONE ON THE SIDE OF THE DOOR). INSTALLED COVER PER AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 46,986 hrs · 27,813 cycles

L1 DOOR SLIDE Z FOUND LOOSE. REFOLDED SLIDE PER AMM..

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,484 hrs · 27,512 cycles

LT OVERWING EXIT LIGHT BULBS INOP. RELAMPED PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 46,484 hrs · 27,512 cycles

FWD ZONE EMERGENCY LIGHTS BATTERY PACK FAILED TEST. R&R BATTERY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,475 hrs · 27,503 cycles

L1 DOOR OVERHEAD EXIT LIGHT INOP. R&R M1674 BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,475 hrs · 27,503 cycles

L2 DOOR EVAC SLIDE LIGHT INOP. R&R M1674 BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 46,475 hrs · 27,503 cycles

L2 DOOR EMERGENCY ESCAPE SLIDE OUT OF POSITION. R&R SLIDE ASSEMBLY PER MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,475 hrs · 27,503 cycles

2 EA EMERGENCY EXIT AISLE LIGHTS INOP. R&R M1674 BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,028 hrs · 27,238 cycles

RT FORWARD EXTERIOR SLIDE EMERGENCY LIGHT INOP. R&R LIGHT PER AMM.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 45,391 hrs · 26,810 cycles

RIGHT WING FIXED PANEL ABOVE NACELLE STRUT FAIRING BRACKET CRACKED ON AFT SIDE / R/R BRACKET IAW SRM 51-40-02.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 44,099 hrs · 25,953 cycles

EMERGENCY EXIT SIGN AT OVERWING EXIT LOOSE ON LANDING. R & R THE SIGN IAW AMM.

Part: VAPOR BARRIER — CRACKED (RT WHEEL WELL) · airframe 43,525 hrs · 25,591 cycles

R/H WHEEL WELL FWD WALL HAS VAPOR BARRIER CRACK / 9.25' CRACK LOCATED ON BAY 9R BETWEEN RBL 45.64 AND RBL 54.21. APPLIED INTERIM PATCH REPAIR PER SRM 57-10-10-2R-2 PARA. 6

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,570 hrs · 25,003 cycles

LT OVERHEAD BIN EMERGENCY LIGHT INOP AT ROW 9. RELAMPED LIGHT IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 42,326 hrs · 24,827 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,059 hrs · 24,658 cycles

LT OVER WING EMERGENCY EXIT UPPER LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 41,438 hrs · 24,278 cycles

R2 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED THE SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,235 hrs · 24,162 cycles

LT OVERWING EXIT EMERGENCY LIGHT ON AFT SIDE OF DOOR LIGHT ASSEMBLY INOP. RELAMPED LIGHT PER AMM.

Part: WIRE — DAMAGED (CABIN) · airframe 41,235 hrs · 24,162 cycles

LT EMERGENCY LIGHT WIRED DAMAGED AT ROW 9. REPAIRED WIRE PER SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 41,235 hrs · 24,162 cycles

CABIN FLOOR PANEL 241DF HAS DAMAGE AT AFT RH CORNER. / CABIN FLOOR PANEL 241DF DAMAGE AT AFT RH CORNER WAS REPAIRED IAW SRM 53-00-50-2R-10 56144U 31MAY17

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,235 hrs · 24,162 cycles

LT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STA 120.3, NR 2 FROM THE FRONT VERTICAL STIFFENER. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,235 hrs · 24,162 cycles

LT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STA 120.3, NR 3 FROM THE FRONT VERTICAL STIFFENER. REPAIRED RIB PER SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 41,235 hrs · 24,162 cycles

CABIN FLOOR PANEL 232SF HAS VARIOUS DAMAGE AT FWD I/B CORNER AND AFT AND I/B EDGES. / CABIN FLOOR PANEL 232SF WITH VARIOUS DAMAGE AT FWD I/B CORNER AND AFT I/B EDGES WAS REPAIRED PER SRM 53-50-2R-10

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,235 hrs · 24,162 cycles

LT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STA 120.3, NR 4 FROM THE FRONT VERTICAL STIFFENER. REPAIRED RIB PER SRM.

Part: SUPPORT — CRACKED (CABIN) · airframe 41,235 hrs · 24,162 cycles

FLOOR SUPPORT CRACKED BS 344-360 RBL 12-WL 208. / REMOVED CRACKED FLOOR SUPPORT B.S. 344-360; RBL 12; WL 208 AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0

Part: PLATE — CRACKED (LT WING) · airframe 41,235 hrs · 24,162 cycles

LT WING FIXED TRAILING EDGE WAFFLE PLATE AT REAR SPAR LOWER CHORD ORSS 250 CRACKED. R&R WAFFLE PLATE IAW SRM.

Part: SUPPORT — CRACKED (LEFT WING) · airframe 41,235 hrs · 24,162 cycles

LEFT WING T/E BULB SEAL RETAINER; SUPPORT ASSY (ORSS 272 / 15' AFT OF REAR SPAR) CRACK NOTED. / REMOVED AND REPLACED LEFT WING T/E BULB SEAL RETAINER; SUPPORT ASSY (ORSS 272) 15' AFT OF REAR SPAR) IAW SRM 51-40-02-0G-0 STEP 4

Part: WEB — CRACKED (LT WING) · airframe 41,235 hrs · 24,162 cycles

LT WING TRAILING EDGE WEB ASSEMBLY AFT OF REAR SPAR CRACKED ORSS 275. R&R WEB ASSEMBLY IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 41,235 hrs · 24,162 cycles

LT WING FIXED TRAILING EDGE WAFFLE PLATE AT REAR SPAR LOWER CHORD IRSS 207 CRACKED. R&R WAFFLE PLATE IAW SRM.

Part: SUPPORT — CRACKED (CABIN) · airframe 41,235 hrs · 24,162 cycles

FLOOR SUPPORT CRACKED BS 344-360 BL 0 WL 208. / REMOVED CRACKED FLOOR SUPPORT BS. 344-360; BL-0 WL. 208 AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0.

Part: PLATE — CRACKED (LT WING) · airframe 41,235 hrs · 24,162 cycles

LT WING FIXED TRAILING EDGE WAFFLE PLATE AT REAR SPAR LOWER CHORD IRSS 230 CRACKED. R&R WAFFLE PLATE PER SRM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 41,235 hrs · 24,162 cycles

FRAME DAMAGED AT BS 277, RBL 9. REPAIRED FRAME IAW SRM.

Part: BRACKET — ELONGATED (LEFT WING) · airframe 41,235 hrs · 24,162 cycles

LEFT WING LOWER FIXED T/E PANEL SUPPORT ROD; BRACKET ASSY (ORSS 243) HOLES ELONGATED. / REMOVED LEFT WING LOWER FIXED T/E PANEL SUPPORT ROD BRACKET ASSY IAW. SRM 51-40-02. 24952U INSTALLED LEFT WING LOWER FIXED T/E PANEL SUPPORT ROD BRACKET ASSY. I.A.W. SRM 51-40-02. 24952U 31MAY2017

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,235 hrs · 24,162 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D TO BS 787, LBL 23. REPAIRED SUPPORT IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,235 hrs · 24,162 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET PER SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,235 hrs · 24,162 cycles

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

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,235 hrs · 24,162 cycles

REINFORCEMENT STRAP CORRODED AT BS 1030, RBL 3. R&R STRAP IAW SRM AND DWG .

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,235 hrs · 24,162 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 50 TO LBL 44. REPAIRED FLOOR BEAM IAW EA & ER.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,235 hrs · 24,162 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R&R SUPPORT IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 41,235 hrs · 24,162 cycles

FWD PASSENGER CABIN FLOOR PANEL 221FF HAS DAMAGED UPPER SURFACE ON FWD EDGE / REPAIRED DAMAGED UPPER SURFACE ON FWD EDGE ON FWD PASSENGER CABIN FLOOR PANEL 221FF IAW SRM 53-00-50-2R-9. 57066U 06/01/17

Part: SILL DRAIN — CORRODED (ASD THRESHOLD) · airframe 41,235 hrs · 24,162 cycles

CORROSION ON AFT SERVICE DOOR MOPSILL BS 963-982 WL 208 RBL 53. / REMOVED AND REPLACE AFT SERVICE DOOR MOPSILL AT BS 897 TO 1006 WL 208 RBL 53. IAW SRM 51-40-02-0G-0. AND DWG. 147A8540.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,235 hrs · 24,162 cycles

FORWARD CARGO BAY AFT LOWER CENTER BULKHEAD SUPPORT CORRODED AT BS 500D. R&R SUPPORT PER SOPM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,235 hrs · 24,162 cycles

REINFORCEMENT STRAP CORRODED BETWEEN BS 1016 TO BS 1030, LBL 3. R&R STRAP IAW SRM AND DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 41,235 hrs · 24,162 cycles

FWD CARGO BAY; FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED FWD CARGO BAY FWD CORNER SCUFF PLATE IAW EA 1-A53-2076 REV 11

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 41,235 hrs · 24,162 cycles

LT WINDSCREEN FORWARD ATTENDANT FLASHLIGHT BASE ASSEMBLY BROKEN. R&R FLASHLIGHT ASSEMBLY IAW SOPM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 41,235 hrs · 24,162 cycles

FWD CARGO BAY; AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED FWD CARGO BAY AFT CORNER SCUFF PLATE IAW EA 1-A53-2076 REV 11

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 41,050 hrs · 24,047 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOW PRESSURE. R&R SLIDE PER MT.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 36,941 hrs · 21,680 cycles

RIGHT WING UPPER TE PANEL, AFT OF NR 2 PYLON SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: SUPPORT — CRACKED (LT WING) · airframe 36,941 hrs · 21,680 cycles

LEFT WING UPPER TE FIXED PANEL, L ANGLE SUPPORT CRACKED BELOW SERRATED PLATE. R & R SUPPORT IAW SRM.

Part: HOOK — CORRODED (CABIN) · airframe 35,215 hrs · 20,686 cycles

LEFT EMER EXIT HATCH, ESCAPE STRAP HOOK AT END OF STRAP CORRODED. R & R STRAP IAW AMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,215 hrs · 20,686 cycles

FLOOR STRUCTURE CORRODED AT BS 270, BETWEEN LBL 10 - RBL 7. REPAIRED INTERCOSTAL IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,215 hrs · 20,686 cycles

RIGHT MLG WW LOWER FUSELAGE SKIN CRACKED AT BS 727, BETWEEN RBL 19 TO RBL 37. REPAIRED SKIN IAW SRM & DWG.

Part: POST — CRACKED (FUSELAGE) · airframe 35,215 hrs · 20,686 cycles

LEFT NR 3 WINDOW CRACKED AT THE 2ND LOWER CORNER FASTENER HOLE POST E - F. REPAIRED POST IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 34,896 hrs · 20,504 cycles

RIGHT MLG WW FWD VERTICAL PRESS WEB CRACKED AT STATION 663, RBL 36. REPAIRED WEB IAW EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 34,896 hrs · 20,504 cycles

EEPLS DAMAGED AT SEAT ROW 1. R & R EEPLS IAW MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 34,896 hrs · 20,504 cycles

EEPLS DAMAGED AT ROW 24 DEF. R & R EEPLS IAW MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 34,896 hrs · 20,504 cycles

EEPLS DAMAGED AT LT AFT WINDSCREEN. R & R EEPLS IAW MM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 34,126 hrs · 20,076 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY & STILL OPERATIONAL. REINSTALLED SLIDE ASSEMBLY IAW MT.

Part: LENS — MISSING (CABIN) · airframe 34,110 hrs · 20,063 cycles

RIGHT OVERWING EMER EXIT SIGN LENS MISSING. INSTALLED LENS IAW SIP.

Part: FITTING — CORRODED (RT MLG) · airframe 33,544 hrs · 19,729 cycles

RIGHT MLG, FWD TRUNNION FITTING, UPPER INBD LUG FACE CORRODED. REPAIRED FITTING IAW EA.

Part: FITTING — CORRODED (LT MLG) · airframe 33,544 hrs · 19,729 cycles

LEFT MLG FWD TRUNNION FITTING UPPER INBD LUG FACE CORRODED. REPAIRED FITTING IAW EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 32,553 hrs · 19,136 cycles

R1 DOOR NR 5 FRAME WEB CRACKED. R & R DOOR IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 31,961 hrs · 18,788 cycles

R2 DOOR EMER EXIT LIGHT LENS FELL OFF. R & R LIGHT ASSEMBLY IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 30,212 hrs · 17,770 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 30,212 hrs · 17,770 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 29,387 hrs · 17,299 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 28,979 hrs · 17,049 cycles

R2 DOOR SLIDE LOOSE. SECURED SLIDE & GIRT BAR IAW MM.

Part: LENS — UNSECURE (CABIN) · airframe 28,370 hrs · 16,674 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. R & R LENS IAW AMM.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 28,281 hrs · 16,618 cycles

LT LOWER EXTERIOR OVERWING EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. SECURED WIRE IAW WDM & MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 28,281 hrs · 16,618 cycles

AFT RT EXIT SIGN BY OVERWING EXIT DOOR INOPERATIVE. CONNECTED WIRES IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 28,281 hrs · 16,618 cycles

AFT WALL EMERGENCY EXIT LIGHT ON LAVATORY A LENS BROKEN. R&R LIGHT ASSEMBLY IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 28,281 hrs · 16,618 cycles

LT NR 3 WINDOW FRAME CRACKED AT THE 2ND LOWER CORNER FASTENER HOLE ALONG POST E-F. REPAIRED FRAME IAW SWA EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,281 hrs · 16,618 cycles

INTERCOSTAL CRACKED AT BS 352, BL 0. R&R INTERCOSTAL IAW DRAWING & SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,281 hrs · 16,618 cycles

LONGITUDINAL FLOOR BEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD IAW EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 28,281 hrs · 16,618 cycles

RT HORIZONTAL STABILIZER RIB AT STATION 92.70, 2ND VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,281 hrs · 16,618 cycles

INTERCOSTAL CRACKED AT BS 306, RBL 16. REPAIRED INTERCOSTAL IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 28,281 hrs · 16,618 cycles

MAIN WW VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN LBL 34 TO LBL 35. REPAIRED WEB IAW SRM.

Part: BALLAST — FAULTY (CABIN) · airframe 27,441 hrs · 16,115 cycles

DECLARED EMERGENCY, F/A AND PASSENGERS REPORT ACRID SMELL (ELECTRICAL) AND SMOKE IN CABIN. R & R LT EMERGENCY EXIT DOOR BALLAST IAW MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 27,316 hrs · 16,040 cycles

LT OVERWING LOWER EMERGENCY EXIT SIGN LENS MISSING. R & R LENS IAW MM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 25,727 hrs · 15,103 cycles

RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL PER MM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 25,727 hrs · 15,103 cycles

FLIGHT COMPARTMENT L1 WINDOW C-D POST CRACKED 1.25" AT UPPER END. REPAIRED PER EA# 1-753-211-96, ALSO SEE TSR # 201205393.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,461 hrs · 14,345 cycles

LEFT EEPLS INOP AT ROW 1. RELAMPED EEPLS PER AMM.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 23,606 hrs · 13,867 cycles

LEFT EMERGENCY LIGHT CAP MISSING AT ROW 7. INSTALLED CAP PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 21,547 hrs · 12,685 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 138.70. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 24,602 hrs · 14,427 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 19,251 hrs · 11,372 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 8 TO ROW 22. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 19,251 hrs · 11,372 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 7. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,804 hrs · 11,119 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 18,706 hrs · 11,066 cycles

EEPLS COVER LOOSE AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LENS — CRACKED (CABIN) · airframe 18,106 hrs · 10,710 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS LENS CRACKED AT ROW 20. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,106 hrs · 10,710 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS INOP AT ROW 18. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 17,321 hrs · 10,260 cycles

FWD EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,013 hrs · 10,072 cycles

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

Part: COVER — MISSING (CABIN) · airframe 16,536 hrs · 9,790 cycles

FWD EEPLS COVER MISSING AT ROW 2. INSTALLED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 16,508 hrs · 9,773 cycles

LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 15,468 hrs · 9,143 cycles

FWD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 14,755 hrs · 8,689 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,815 hrs · 8,100 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD EEPLS LIGHT INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 12,703 hrs · 7,418 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. REMOVED AND REPLACED SLIDE ASSY PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 12,068 hrs · 7,029 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 10,933 hrs · 6,345 cycles

FOUND L1 DOOR SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 6,796 hrs · 5,667 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 2 DEF. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,796 hrs · 5,667 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: ACTUATOR — FAULTY (FUEL CROSSFEED) · airframe 8,613 hrs · 4,967 cycles

DIVERSION/DECLARED EMERGENCY. AT CRUISE FUEL IMBALANCE REPORTED, NR 2 TANK CONTINUED DECREASING WITH PUMPS OFF. REMOVED AND REPLACED CROSSFEED VALVE ACTUATOR PER MM.

Part: LENS — CRACKED (CABIN) · airframe 7,507 hrs · 4,289 cycles

DURING SCHEDULED HC1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 16 ABC. REMOVED AND REPLACED LENS PER MM.

Part: CAP — LOOSE (CABIN) · airframe 7,285 hrs · 4,163 cycles

EEPLS END CAP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 7,197 hrs · 4,112 cycles

EEPLS LENS LOOSE AT ROW 3 ABC. SECURED LENS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 7,110 hrs · 4,057 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 5,134 hrs · 2,928 cycles

EEPLS LENS MISSING AT ROW 17. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 4,620 hrs · 2,636 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 2,843 hrs · 1,638 cycles

EEPLS LIGHT COVER MISSING AT ROW 17 ABC. INSTALLED EEPLS LIGHT COVER PER MM.