N913WN

Part: APU — SHUTDOWN (ZONE 100) · airframe 56,419 hrs · 34,436 cycles

AT CRUISE FL 400 RECEIVED APU LOP LIGHT. APU DID AUTO SHUTDOWN NH30. PERFORMED OPERATONAL TEST OF APU AND TEST PASS IAW AMM 49-11-00.

Part: CONTROL MODULE — FAULTY (ZN 100 FUS LOWER) · airframe 53,762 hrs · 32,736 cycles

ENG1 OVHT; ENG2 OVHT; ENG 1&2&APU FIRE HANDLES ILLUMINATED & WHEEL WELL LIGHT ILLUMINATED ON TAKEOFF ROLL WITH ASSOCIATED FIRE WARNING BELLS ON TAKEOFF ROLL (125KT)<[01] R&R ENG & APU FIRE CONTROL PANEL IAW AMM 26-00-01;[02] PERFORMED THE FOLLOWING OPERATIONAL CHECKS OF ENG & APU FIRE CONTROL PANEL:<BR><BR>-FIRE AND OVERHEAT DETECTION SYSTEM - OPERATIONAL TEST; PER AMM TASK 26-10-00-710-801 OPS CHECK GOOD.<BR>-ENGINE FIRE EXTINGUISHING BOTTLE SQUIB - CIRCUIT TEST; AMM TASK 26-21-00-730-801 OPS CHECK GOOD.<BR>-ENGINE FIRE EXTINGUISHING BOTTLE PRESSURE SWITCH CIRCUIT TEST; AMM TASK 26-21-00-730-802 OPS CHECK GOOD.<BR>-APU FIRE EXTINGUISHING BOTTLE PRESSURE SWITCH CIRCUIT TEST; AMM TASK 26-22-00-730-802 OPS CHECK GOOD.<BR>-WHEEL WELL; WING AND LOWER AFT BODY OVERHEAT DETECTION SYSTEM - OPERATIONAL TEST; AMM TASK 26-18-00-710-801 OPS CHECK GOOD.<BR><BR>REMAINING OPERATIONAL SUBTASKS STILL REQUIRED:<BR>-SUBTASK 26-00-01-720-002 (ENG FIRE SWITCH SHUT DOWN)<BR>-SUBTASK 26-00-01-720-004 (APU FIRE SWITCH SHUT DOWN)<BR>-SUBTASK 26-00-01-720-005 (APU SQUIB CIRCUIT TEST);[03] C/W REMAINING OPS CHECKS PER 26-00-01. OPS CHECK GOOD. REMOVED AND REPLACED APU AND ENGINE FIRE DETECTION CONTROL MODULE IAW AMM 26-10-01. OPS CHECK GOOD.

Part: CONTROL PANEL — FAULTY (ZN 100 FUS LOWER) · airframe 53,762 hrs · 32,736 cycles

ENG1 OVHT; ENG2 OVHT; ENG 1&2&APU FIRE HANDLES ILLUMINATED & WHEEL WELL LIGHT ILLUMINATED ON TAKEOFF ROLL WITH ASSOCIATED FIRE WARNING BELLS ON TAKEOFF ROLL (125KT)<[01] R&R ENG & APU FIRE CONTROL PANEL IAW AMM 26-00-01;[02] PERFORMED THE FOLLOWING OPERATIONAL CHECKS OF ENG & APU FIRE CONTROL PANEL:<BR><BR>-FIRE AND OVERHEAT DETECTION SYSTEM - OPERATIONAL TEST; PER AMM TASK 26-10-00-710-801 OPS CHECK GOOD.<BR>-ENGINE FIRE EXTINGUISHING BOTTLE SQUIB - CIRCUIT TEST; AMM TASK 26-21-00-730-801 OPS CHECK GOOD.<BR>-ENGINE FIRE EXTINGUISHING BOTTLE PRESSURE SWITCH CIRCUIT TEST; AMM TASK 26-21-00-730-802 OPS CHECK GOOD.<BR>-APU FIRE EXTINGUISHING BOTTLE PRESSURE SWITCH CIRCUIT TEST; AMM TASK 26-22-00-730-802 OPS CHECK GOOD.<BR>-WHEEL WELL; WING AND LOWER AFT BODY OVERHEAT DETECTION SYSTEM - OPERATIONAL TEST; AMM TASK 26-18-00-710-801 OPS CHECK GOOD.<BR><BR>REMAINING OPERATIONAL SUBTASKS STILL REQUIRED:<BR>-SUBTASK 26-00-01-720-002 (ENG FIRE SWITCH SHUT DOWN)<BR>-SUBTASK 26-00-01-720-004 (APU FIRE SWITCH SHUT DOWN)<BR>-SUBTASK 26-00-01-720-005 (APU SQUIB CIRCUIT TEST);[03] C/W REMAINING OPS CHECKS PER 26-00-01. OPS CHECK GOOD. REMOVED AND REPLACED APU AND ENGINE FIRE DETECTION CONTROL MODULE IAW AMM 26-10-01. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 51,181 hrs · 31,180 cycles

M1672 EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST<[01] REMOVED AND REPLACED M1672 EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 51,181 hrs · 31,180 cycles

WING CENTER SECTION REAR SPAR VAPOR BARRIER HAS SINGLE VERTICAL CRACK 15.8 INCH IN LONG BETWEEN STIFFENER AT LBL 45.64 & LBL 31.83.<[01] REPAIRED WING CENTER SECTION REAR SPAR VAPOR BARRIER VERTICAL CRACK 15.8 INCH IN LONG BETWEEN STIFFENER AT LBL 45.64 & LBL 31.83 IAW SRM 57-10-10-1A-2-A00534. REPAIR UNDER PARA 2.C.(3)(A) WAS USED/ACCOMPLISHED. REINSPECTION REQUIRED AT EACH 600 FLIGHT CYCLE INTERVAL.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 51,181 hrs · 31,180 cycles

LH HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LH HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL PER AMM 53-31-31;[02] C/W INSPECTION

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 51,181 hrs · 31,180 cycles

RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED.<[01] R&R RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL. IAW AMM 53-31-31;[02] C/W INSPECTION REQUIREMENT

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2023-431323<[01] TOOL USED CALIPER P/N: 500-196-30; S/N: A20231842; DUE DATE: 21-FEB-24;[02] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV -.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNS-OFF BELOW

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CRACK WEB - INTERCOSTAL BTW BS847 TO BS867 WL208 FLOOR LEVEL AT AFT CARGO COMPARTMENT 2023-431308<[01] OPEN FAULT HAS AN ERROR AND IS BEING CORRECTED BY RAISING A NEW FAULT; SEE [TTG8Q00M7MDZ];[02] CORRECTED STEP 1:FAULT SOLVED IN OTHER FAULT DUE TO REPLACED PART ASSY SEE TTG8Q00M7MDZ;[03] FAULT SOLVED IN OTHER FAULT DUE TO REPLACED PART ASSY SEE TTG8Q00M7MDZ

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 49,236 hrs · 29,953 cycles

CRACK SUPPORT ANGLE LOC. BS 847 BETWEEN BS867 LBL 21 AT AFT GALLEY AREA AT PASSENGER CABIN 2023-431309<[01] REPLACED SUPPORT ANGLE LOC. BS 847 BETWEEN BS867 LBL 21 AT AFT GALLEY AREA AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 149A8100 SHEET 1 REV -;[02] REPLACED SUPPORT ANGLE LOC. BS 847 BETWEEN BS867 LBL 21 AT AFT GALLEY AREA AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 149A8100 SHEET 1 REV -

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 49,236 hrs · 29,953 cycles

CRACK ON UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND BL 0 WL 208 AT FWD GALLEY AREA 2023-431290<[01] REPLACED ANGLE INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND BL 0 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 92 REV -;[02] REPLACED ANGLE INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND BL 0 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 92 REV - RII CERTIFIED

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 49,236 hrs · 29,953 cycles

CRACK RIB 8 ON ACCESS PANEL 321A AT VERTICAL STABILIZER 2023-431281<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED RIB 8 LOCATED ON ACCESS PANEL 321A AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-10-02 AND DWG 174A0103 REV -.<BR>SEE INDIVIDUAL SINGOFFS BELOW;[03] CORRECTED STEP 2: REPLACED RIB 8 LOCATED ON ACCESS PANEL 321A AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-10-02 AND DWG 174A0103 REV -.<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[04] CORRECTIVE ACTION STEP 3 CERTIFIED

Part: STRINGER — CORRODED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CORROSION STRINGER 25R LOCATED BS540 WL155.3 AT FWD CARGO COMPARTMENT 2023-431287<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24.;[03] TOOL USED: EDDYCURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N:60009161631; DUE DATE: 31-JAN-24;[04] PERFORMED PERMANENT REPAIR STR 25R LOC. BTW BS 500C TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 <BR>SEE INDIVIDUAL SIGN OFFS BELOW;[05] RII JOB COMPLETED

Part: STRINGER — CORRODED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CORROSION STRINGER 23R LOCATED BS540 WL164.1 AT FWD CARGO COMPARTMENT 2023-431283<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 200048001; CAL DUE DATE: 01-MAY-24;[03] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24.;[04] REPAIRED STR 23R LOC. BTW BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 <BR>SEE INDIVIDUAL SIGN OFFS BELOW;[05] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: STRINGER — CORRODED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CORROSION STRINGER 27R LOCATED BS540 WL150.1 AT FWD CARGO COMPARTMENT 2023-431285<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220272712; CAL DUE DATE: 17-DEC-23;[03] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24.;[04] PERFORMED PERMANENT REPAIR STR 27R LOC. BTW BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 <BR>SEE INDIVIDUAL SIGN OFFS BELOW;[05] RII JOB COMPLETED;[06] RII JOB COMPLETED

Part: CARGO TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CRACK TRACK RBBL 13.84 LOCATED BS727C AFT CARGO COMPARTMENT 2023-431274<[01] REPAIRED TRACK AT RBL 13.84 AND BSTA 727B & BSTA 767 AFT CARGO COMPARTMENT IAW EA 23-153-02226 REV1 AND EA 23-153-02226-WIP1 REV2 SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1<BR>REPAIRED TRACK AT RBL 13.84 AND BSTA 727B & BSTA 767 AFT CARGO COMPARTMENT IAW EA 23-153-02226 REV1 TTG8Q00MH0J7 AND EA 23-153-02226-WIP1 REV2 TTG8Q00MCV5Z SEE INDIVIDUAL SIGN OFF BELOW;[03] REPAIRED TRACK AT RBL 13.84 AND BSTA 727B & BSTA 767 AFT CARGO COMPARTMENT IAW EA 23-153-02226 REV1 TTG8Q00MH0J7 AND EA 23-153-02226-WIP1 REV2 TTG8Q00MCV5Z SEE INDIVIDUAL SIGN OFF BELOW. AS RII

Part: FITTING — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CRACK FLOOR STRUCTURE FITTING LOCATED BS947.5 AND STR26R AT AFT CARGO COMPARTMENT 2023-431262<[01] REPLACED FITTING AND FASTENERS LOCATED BS947.5 AND STR26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 Ï¿½TEM 9 AND DWG 149A8103 SHEET 7 REV A. SEE INDIVIDUAL SING-OFFS BELOW;[02] REPLACED FITTING AND FASTENERS LOCATED BS947.5 AND STR26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 Ï¿½TEM 9 AND DWG 149A8103 SHEET 7 REV A. SEE INDIVIDUAL SING-OFFS BELOW ITEM RII

Part: CARGO TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CRACK TRACK RBBL 13.84 LOCATED BS727E AFT CARGO COMPARTMENT 2023-431273<[01] REFER TO FAULT TTG8Q00M3RDR WHERE EA 23-153-02226 WAS ADDED AS A SUBTASK.;[02] REFER TO FAULT TTG8Q00M3RDR WHERE EA 23-153-02226 WAS ADDED AS A SUBTASK.

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CRACK FLOOR STRUCTURE SUPPORT BRACKET LOCATED BS827 AND STR25R AT AFT CARGO COMPARTMENT 2023-431271<[01] REPLACED FLOOR STRUCTURE SUPPORT BRACKET LOCATED BS827 AND STR25R AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 146A8120 REV:- AND DWG 146A0081 REV:- SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CRACK FLOOR STRUCTURE LOCATED BS867 AND STR26L AT AFT CARGO COMPARTMENT 2023-431270<[01] REPLACED BRACKET AND FASTENERS LOCATED FLOOR STRUCTURE BS867 AND STR26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 149A8102 REV:- <BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CRACK FLOOR STRUCTURE SUPPORT BRACKET LOCATED BTW BS907 TO BS927 AND STR26L AT AFT CARGO COMPARTMENT 2023-431264<[01] REPLACED SUPPORT BRACKET LOCATED BTW BS907 TO BS927 AND STR26L AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 147A7221 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT BRACKET LOCATED BTW BS907 TO BS927 AND STR26L AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 147A7221 REV:- SEE INDIVIDUAL SIGN OFF BELOW<BR>RII

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CRACK FLOOR STRUCTURE SUPPORT BRACKET LOCATED BS807 AND STR25R AT AFT CARGO COMPARTMENT 2023-431272<[01] REPLACED SUPPORT BRACKET LOCATED FLOOR STRUCTURE BS807 AND STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 146A8120 REV:- AND 146A0081 REV:- <BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] COMPLETE TASK CERTIFIED RII

Part: FRAME — CRACKED (ZN 200 FUS TOP) · airframe 49,236 hrs · 29,953 cycles

CRACK ON FRAME LOCATED BS 312AT LEVEL STR 5LAT FWD GALLEY AREA 2023-431241<[01] PERFORMED REPAIR ON BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L IAW EA M-22-153-01244 <BR>SEE TASK CARD: TTG8Q00M3J6Z;[02] PERFORMED REPAIR ON BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L IAW EA M-22-153-01244 <BR>SEE TASK CARD: TTG8Q00M3J6Z

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CRACK FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2023-431239<[01] REPLACED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 453A2610 REV: E;[02] CORRECTED STEP 1.<BR>REPLACED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 453A2610 REV:E. MATERIAL USED 2024T3 0.080? P.O:2023 148020;[03] REPLACED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 453A2610 REV:E. SHEET 9 ;MATERIAL USED 2024T3 0.080? P.O:2023 148020

Part: PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 49,236 hrs · 29,953 cycles

CRACK ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2023-431184<[01] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18196126; DUE DATE: 26-MAR-24.;[02] TOOL USED HOT; BONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 26-MAR-24;[03] TOOL USED: SCALE: P/N:CR5200 S/N:8343110772 DUE DATE:20-FEB-24.;[04] TOOL USED: MULTIMETER P/N: FLUKE-87 S/N: 43050133 DUE DATE: 05-MAR-24.;[05] TOOL USED: CALIPER P/N: 500-197-30; S/N:B20189527; DUE DATE: 26 DEC 23.;[06] TOOL USED: SCALE P/N: CR5200; S/N: 8343110809; DUE DATE: 21-FEB-24.;[07] TOOL USED: MULTIMETER P/N: FLUKE-87 S/N: 43050133 DUE DATE: 05-MAR-24.;[08] REPAIRED ACCESS PANEL 661BB IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGN OFF BELOW.;[09] JOB TASK COMPLETED.

Part: PANEL — CRACKED (ZN 500 LEFT WING) · airframe 49,236 hrs · 29,953 cycles

CRACK ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2023-431181<[01] TOOL USED CALIPER P/N 500-197-30 S/N:B20189527 DUE DATE 26 DEC23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18196126; DUE DATE: 26-MAR-24.;[03] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 26-MAR-24;[04] TOOL USED: SCALE: P/N:CR5200 S/N:8343110772 DUE DATE:20-FEB-24.;[05] TOOL USED: MULTIMETER P/N: FLUKE-87 S/N: 43050133 DUE DATE: 05-MAR-24.;[06] TOOL USED: SCALE P/N: CR5200; S/N: 8343110809; DUE DATE: 21-FEB-24.;[07] REPAIRED ACCESS PANEL 561BB IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGN OFF BELOW.;[08] JOB TASK COMPLETED.

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 500D BTW STR 18R AND STR 19R WING-TO-BODY FAIRING SUPPORT STRUCTURE 2023-431183<[01] REPLACED SUPPORT ANGLE LOCATED BS 500D BTW STR 18R AND STR 19R WING-TO-BODY FAIRING SUPPORT STRUCTURE IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 116A3010 ; SHEET 39 ; REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT ANGLE LOCATED BS 500D BTW STR 18R AND STR 19R WING-TO-BODY FAIRING SUPPORT STRUCTURE IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 116A3010 ; SHEET 39 ; REV -. <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 500D BTW STR 18L AND STR 19L WING-TO-BODY FAIRING SUPPORT STRUCTURE 2023-431193<[01] REPLACED SUPPORT ANGLE LOCATED BS 500D BTW STR 18L AND STR 19L WING-TO-BODY FAIRING SUPPORT STRUCTURE IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 116A3010; SHEET 39; REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT ANGLE LOCATED BS 500D BTW STR 18L AND STR 19L WING-TO-BODY FAIRING SUPPORT STRUCTURE IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 116A3010; SHEET 39; REV -. <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 49,236 hrs · 29,953 cycles

CRACK ON INTERCOSTAL LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO RBL 24.75 AT CENTER SECTION 2023-431107<[01] INSTALLED NEW INTERCOSTAL AND FASTENERS LOC.FLOOR STRUCTURE BS 540 BTW BL 0 TO RBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 46 REV -;[02] CORRECTED STEP 1 <BR>REPLACED INTERCOSTAL AND FASTENERS LOC.FLOOR STRUCTURE BS 540 BTW BL 0 TO RBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 46 REV -;[03] CORRECTED STEP 2 <BR>REPLACED INTERCOSTAL AND FASTENERS LOC.FLOOR STRUCTURE BS 540 BTW BL 0 TO RBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 36 REV A;[04] RII ITEM <BR>REPLACED INTERCOSTAL AND FASTENERS LOC.FLOOR STRUCTURE BS 540 BTW BL 0 TO RBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 36 REV A

Part: FLAP — DEBONDED (ZN 600 RIGHT WIN) · airframe 49,233 hrs · 29,952 cycles

CUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT RT WING 2023-431125<[01] TOOL USED CALIPER P/N 500-197-30 S/N 15120589 DUE DATE 13 FEB 24;[02] THE DAMAGE WAS REPAIRED PER 737-700 SRM-57-53-01-2R-18 REPAIR 18 WITH A DEVIATION DUE TO THE REPAIR SIZE APPROVED PER EA 23-157-02208. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] TASK COMPLETED. RII COMLETED.

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 49,236 hrs · 29,953 cycles

CRACK STIFFENER 2 INSPAR RIB 129.50 AT LT HORIZONTAL STABILIZER 2023-431111<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 210138103; CAL DUE DATE: 02-MAY-24;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DATE: 12 MAR 24.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[04] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N:130066701; CAL DUE DATE: 09-JUN-24;[05] PERFORMED PERMANENT REPAIR LOCATED ON STIFFENER 2 INSPAR RIB 129.50 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-5 REPAIR 5 AND DWG 182A3001 REV F. SEE INDIVIDUAL SIGN-OFF BELOW.;[06] PERFORMED PERMANENT REPAIR LOCATED ON STIFFENER 2 INSPAR RIB 129.50 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-5 REPAIR 5 AND DWG 182A3001 REV F. RII; SEE INDIVIDUAL SIGN-OFF BELOW.

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 49,236 hrs · 29,953 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 CENTER SECTION 2023-431116<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112811019; DUE DATE: 25-JAN-24 AND TEMPERATURE CONTROLLER: P/N: 38615K71; S/N: AE-40586; DUE DATE: 09-AUG-23.;[02] REPLACED ANGLE LOCATED AT BSTA 695 RBL 24.75 CENTER SECTION IAW SRM B737-700 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 273A9110 REV-A<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[03] CERTIFIED STEP 2 COMPLETED

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 49,236 hrs · 29,953 cycles

CRACK ON INTERCOSTAL LOCATED FLOOR STRUCTURE BS 540 BTW RBL 24.75 TO RBL 45.5 AT CENTER SECTION 2023-431113<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BS 540 BTW RBL 24.75 TO RBL 45.5 AT CENTER SECTION IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 36 REV A;[02] REPLACED INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BS 540 BTW RBL 24.75 TO RBL 45.5 AT CENTER SECTION IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 36 REV A RII CERTIFIED

Part: FLOOR SUPPORT — CRACKED (ZN 200 FUS TOP) · airframe 49,236 hrs · 29,953 cycles

CRACK ON INTERCOSTAL LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO RBL 24.75 AT CENTER 2023-431106<[01] OPEN FAULT HAS AN ERROR AND IS BEING CORRECTED BY RAISING A NEW FAULT; SEE TTG8Q00M1CBD;[02] TASK CARD COMPLETED <BR>FAULT HAS AN ERROR AND IS BEING CORRECTED BY RAISING A NEW FAULT; SEE TTG8Q00M1CBD

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 49,236 hrs · 29,953 cycles

CRACK ON INTERCOSTAL LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO LBL 24.75 AT CENTER SECTION 2023-431108<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO LBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02 -0G-0 ITEM 9. SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED AS RII <BR>REPLACED INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO LBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02 -0G-0 ITEM 9. SEE INDIVIDUAL SIGN OFF BELOW

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 49,236 hrs · 29,953 cycles

CRACK INSPAR RIB STIFFENER 2 STAB STA 129.50 AT RT HORIZONTAL STABILIZER 2023-431114<[01] TOOL USED P/N NORTEC 600D S/N 60009161631 DUE DATE 31/JAN/24;[02] TOOL USED EDDY CURRENT EQUIPMENT PN:NORTEC 600D; SN:210138103; DUE DATE:02-MAY-24;[03] TOOL USED EDDY CURRENT EQUIPMENT PN:NORTEC 600D; SN:210138103; DUE DATE: 02-MAY-24;[04] PERFORMED PERMANENT REPAIR LOCATED ON INSPAR RIB STIFFENER 2 STAB STA 129.50 AT RT HORIZONTAL STABILIZER. I.A.W. B737-700 SRM 55-10-09-2R-4 REPAIR 4.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[05] PERFORMED PERMANENT REPAIR LOCATED ON INSPAR RIB STIFFENER 2 STAB STA 129.50 AT RT HORIZONTAL STABILIZER. I.A.W. B737-700 SRM 55-10-09-2R-4 REPAIR 4. <BR>SEE INDIVIDUAL SIGN OFF BELOW<BR><BR>ITEM RII

Part: SLAT — CRACKED (ZN 600 RIGHT WIN) · airframe 49,236 hrs · 29,953 cycles

CRACK LOWER SURFACE SLAT 5 LOCATED SLAT STATION 85.19 RT WING 2023-431043<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203 AND DUE DATE: 09-JUN-24.;[02] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 6OOD; S/N:210138003 AND DUE DATE: 27-MAR-24.;[03] PERFORMED PERMANENT REPAIR LOC LOWER SURFACE SLAT 5 STATION 85.19 RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 SEE INDIVIDUAL SIGN-OFF BELOW;[04] PERFORMED PERMANENT REPAIR LOC LOWER SURFACE SLAT 5 STATION 85.19 RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 SEE INDIVIDUAL SIGN-OFF BELOW

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 49,236 hrs · 29,953 cycles

CUSTOMER REQUEST EVALUATE CRACK ON VAPOR BARRIER LH SIDE BSTA 663 2023-431016<[01] TOOL USED CALIPER P/N 500-197-30 S/N B20189527 DUE DATE 26/DEC/23.;[02] TOOL USED: HOTBONDER: P/N:HCS9200B-AV S/N:18175478 DUE DATE:24-SEP-23;[03] TOOL USED: SCALE: P/N:CR5200 S/N:8342514597 DUE DATE:21-FEB-24;[04] TOOL USED HOT BONDER P/N:HCS9200B-AV S/N:18175478 DUE DATE:24-SEP-23;[05] TOOL USED: SCALE: P/N: 91847 S/N: AE-409315 DUE DATE: 08/JUN/24.;[06] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18175478; DUE DATE: 24-SEP-23.;[07] REPAIRED VAPOR BARRIER LH SIDE BSTA 663 IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: SLAT — CRACKED (ZN 600 RIGHT WIN) · airframe 49,236 hrs · 29,953 cycles

CRACK LOWER SURFACE SLAT 8 LOCATED SLAT STATION 451.97 RT WING 2023-431044<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DATE: 12 MAR 24.;[02] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022237; DUE DATE: 26-JAN-24.;[03] PERFORMED PERMANENT REPAIR LOC. LOWER SURFACE SLAT 8 LOCATED SLAT STATION 451.97 RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 SEE INDIVIDUAL SIGN-OFF BELOW;[04] PERFORMED PERMANENT REPAIR LOC. LOWER SURFACE SLAT 8 LOCATED SLAT STATION 451.97 RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 SEE INDIVIDUAL SIGN-OFF BELOW

Part: DOOR — CRACKED (ZN 100 FUS LOWER) · airframe 49,233 hrs · 29,952 cycles

CUSTOMER REQUEST CRACK ON INTERNAL SURFACE OF CENTER MLG DOOR RT SIDE. 2023-431015<[01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X11290U021704; DUE DATE: 12 MAR 24;[02] TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N: A21125526; DUE DATE: 05-NOV-23;[03] REPAIRED INTERNAL SURFACE OF CENTER MLG DOOR RT SIDE IAW B737-700 SRM 52-80-02-2R-3 FIG 202 SHEET 5; SHEET 6 AND SHEET 7. SEE INDIVIDUAL SIGNOFFS BELOW;[04] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: FRAME — CRACKED (ZN 800 DOOR) · airframe 49,233 hrs · 29,952 cycles

CUSTOMER REQUEST CRACK ON CUT OUT OF EXTERNAL GROUND SERVICE DOOR 114AR LOWER FUSELAGE 2023-431020<[01] ET TOOL USED PN NORTEC 600D; SN 210138203; DUE DATE 09-JUN-24;[02] REPAIRED CUT OUT OF EXTERNAL GROUND SERVICE DOOR 114AR LOWER FUSELAGE IAW B737-700 SRM 53-10-15-2R-4 REPAIR 4 . SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPAIRED CUT OUT OF EXTERNAL GROUND SERVICE DOOR 114AR LOWER FUSELAGE IAW B737-700 SRM 53-10-15-2R-4 REPAIR 4 . SEE INDIVIDUAL SIGNS-OFF BELOW RII

Part: CONTACT — INOPERATIVE (ZN 200 FUS TOP) · airframe 49,148 hrs · 29,901 cycles

LEFT AFT EMERGENCY EXTERIOR GROUND ILLUMINATION LIGHT INOP<[01] R&R FUSE AND CONTACT ON LH AFT EMERGENCY LIGHT REF AMM 33-51-00. OPS CHKS GOOD

Part: FUSE — INOPERATIVE (ZN 200 FUS TOP) · airframe 49,148 hrs · 29,901 cycles

LEFT AFT EMERGENCY EXTERIOR GROUND ILLUMINATION LIGHT INOP<[01] R&R FUSE AND CONTACT ON LH AFT EMERGENCY LIGHT REF AMM 33-51-00. OPS CHKS GOOD

Part: COVER — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 48,559 hrs · 29,518 cycles

R1 DOOR LINER AND SLIDE COVER STAINED<[01] CLEANED R1 DOOR LINER & SLIDE COVER IAW AMM 25-00-00.;[02] C/W

Part: PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 48,282 hrs · 29,337 cycles

AFT CARGO AFT CORNER THRESHOLD PLATE CRACKED NEEDS TO BE REPLACED<[01] REMOVED COATINGS AND WELDED SCUFF PLATE REF DWG146A8341 AND SRM 53-00-01;[02] 1. CHAD BLOTSKE (TECHNICIAN); 09-MAR-2023 15:04 UTC<BR>REMOVED COATINGS AND WELDED SCUFF PLATE REF DWG146A8341 AND SRM 53-00-01. REF SRM 53-00-01-2R-21 PAGE 3 OF 16 PARAGRAPH O. (1); (B). REFER TO BAC 5975 FOR WELD REPAIR OF SCURFF PLATES;[03] REINSTALLED AFT CARGO AFT CORNER THRESHOLD PLATE REF AMM 53-11-02

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 48,282 hrs · 29,337 cycles

AFT CARGO FORWARD THRESHOLD CORNER PLATE CRACKED NEEDS TO BE REPLACED AFT CARGO FORWARD THRESHOLD PLATE CRACKED NEEDS TO BE REPLACED<[01] AFT CARGO FORWARD THRESHOLD CORNER PLATE REPLACED REF AMM 53-11-02

Part: VAPOR BARRIER — CRACKED (BS 663 BULKHEAD) · airframe 47,675 hrs · 28,928 cycles

CENTER WING REAR SPAR VAPOR BARRIER HAS A 3 INCH CRACK LOCATED IN L/H WHEEL WELL FWD WALL BETWEEN LBL 24.92 AND 31.83 STARTING APPROXIMATELY 16 INCHES FROM BOTTOM ON WHEEL WELL. APPLIED INTERIM SEAL TO FORWARD SIDE OF CRACK IAW 37.7-0602 PAGE 101 AND SRM 57-10-10-1A-2.

Part: LIGHT — LOOSE (CABIN) · airframe 44,816 hrs · 27,092 cycles

EMERGENCY LIGHT GLOW STRIP NOT SECURED TO FLOOR AT GALLEY AREA ; / [01] RESECURED EMERGENCY LIGHT GLOW STRIP PER SWA DRAWING #33500007.SAF-T-GLO PHOTOLUM INSTALL; [02] C/W; [03] C\W

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 43,304 hrs · 26,170 cycles

R/H OVERWING EMERGENCY EXIT LIGHT (FWD LOWER ASSY.) INOP ; / [01] REPAIRED JIFFY SPLICE ON LIGHT ASSY. AS PER SWPM 20-30-12 AND PERFORMED GOOD FUNCTIONAL AS PER AMM 33-51-01-960-801 STEP 2.(2)<BR>TERM KIT:<BR>ID: T800-004<BR>S/N: E-3166; [02] VERIFIED REPAIRED JIFFY SPLICE ON LIGHT ASSY. AS PER SWPM 20-30-12 AND PERFORMED GOOD FUNCTIONAL AS PER AMM 33-51-01-960-801 STEP 2.(2).

Part: SPLICE STRAP — CORRODED (BS 727D) · airframe 43,304 hrs · 26,170 cycles

CORROSION BS727D LBL19- RBL1 9SPLICE STRAP HAS SEVERAL AREAS OF CORROSION AROUND FASTENER HOLES / [01] REMOVED AND REPLACED ACB SPLICE STRAP AT BS 727D LBL 19 TO RBL 19 DUE TO NO ALLOWABLE LIMIT IN THE SRM FOR THIS PART ; IAW SRM 51-10-02-0G-0 ; STEP 9 (C) AND DWG # 146A7500; [02] REMOVED AND REPLACED ACB SPLICE STRAP AT BS 727D LBL 19 TO RBL 19 DUE TO NO ALLOWABLE LIMIT IN THE SRM FOR THIS PART ; IAW SRM 51-10-02-0G-0 ; STEP 9 (C) AND DWG # 146A7500; [03] VERIFIED ACB SPLICE STRAP AT BS 727D LBL 19 TO RBL 19 CORROSION IS OUT OF LIMITS DUE TO NO ALLOWABLE LIMIT IN THE SRM FOR THIS PART IAW SRM 51-10-02-0G-0 ; STEP 9 (C)<BR>VERIFIED REMOVAL AND REPLACEMENT OF ACB SPLICE STRAP AT BS 727D LBL 19 TO RBL 19 IAW SRM 51-10-02-0G-0 ; STEP 9 (C) AND DWG # 146A7500

Part: SKIN — DEBONDED (LT WING) · airframe 43,304 hrs · 26,170 cycles

LEFT HAND WING INBOARD SPOILER LOWER SURFACE SKIN IS DISBONDED AT THE INBOARD FORWARD CORNER. / [01] IDENTIFIED I/B SPOILER IAW SRM 57-70-01-0I-1.FIG 2; ITEM[1]. REMOVED FINISH IAW AMM 51-21-99-300-802.PARA 3.C.(3).(A)-(D). FOUND DAMAGE WAS UNBONDED FILLER. OK TO APPLY FILLER AND REFINISH.; [02] VERIFIED IDENTIFIED I/B SPOILER IAW SRM 57-70-01-0I-1.FIG 2; ITEM[1]. REMOVED FINISH IAW AMM 51-21-99-300-802.PARA 3.C.(3).(A)-(D). FOUND DAMAGE WAS UNBONDED FILLER. OK TO APPLY FILLER AND REFINISH GIVEN.; [03] DAMAGED AREA ON # 6 SPOILER LOWER SURFACE WILL BE REPAIRED ON CC # TTG8Q005PF9U; [04] DAMAGED AREA ON # 6 SPOILER LOWER SURFACE WILL BE REPAIRED ON CC # TTG8Q005PF9U PER EA # M-21-157-00744; [05] VERIFIED WILL BE REPAIRED ON CUSTOMER CARD TTG8Q005NNGQ.

Part: SUPPORT — CORRODED (BS 807) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 807+15; LBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 807+15; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 1' W= 0.700' D= 0.004' MATERIAL REMAINING IS 0.036' FOUND TO BE WITHIN LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [02] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 807+15; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 1' W= 0.700' D= 0.004' MATERIAL REMAINING IS 0.036' ORIGINAL THICKNESS 0.040' FOUND TO BE WITHIN LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [03] VERIFIED IN LIMITS PER SRM 53-00-53-1A-2; [04] FLOOR TO SIDEWALL TO BE REPLACED ON FAULT TTG8Q005NLFV; [05] VERIFIED PART TO BE REPLACED ON FAULT# TTG8Q005NLFV

Part: SHIELD — CORRODED (BS 433) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FORWARD SHIELD BS 433; RBL 25; WL 157 (MARKED). ; / [01] NOT HAVE ENTRIES FOR ALLOWABLE DAMAGE IN SRM. THE PART MUST BE REPAIRED BY REPLACEMENT PER SRM. 51-10-02 ITEM 9.C.; [02] VERIFIED PART WILL BE REPLACE PER SRM 51-10-02 STEP 9; [03] LOCATED AND DRILLED SHIELD P/N 143A8126-21; LOT.#146355;IAW SRM.51-40-05; DWG#143A0080.; [04] VERIFIED LOCATE AND DRILL OF NEW FWD SHIELD PER SRM 51-40-05; DWG#143A0080; [05] OK TO INSTALL ON FCB. FORWARD SHIELD BTW BS.420-440 RBL 25 WL 157; [06] OK TO INSTALL; [07] INSTALLED ON FCB. FORWARD SHIELD BTW BS.420-440 RBL 25 WL 157 PER SRM 51-40-02. DWG#143A0080; [08] REMOVED AND REPLACED ON FCB. FORWARD SHIELD P/N143A8126-21 BTW BS.420-440 RBL 25 WL 157 PER SRM 51-10-02. ITEM9.C. DWG#143A0080.; [09] STEP 7 AND 8 COMPLETED; [10] VERIFIED INSTALLATION OF FORWARD SHIELD P/N143A8126-21 BTW BS.420-440 RBL 25 WL 157 PER SRM 51-10-02. ITEM9.C. DWG#143A0080

Part: SHIELD — CORRODED (BS 767) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB FWD SHIELD; BS 767+4; RBL 23; WL 157 (MARKED) ; / [01] THIS ITEM DOES NOT HAVE ALLOWABLE DAMAGE THEREFORE HAVE TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 STEP 9; [02] THIS ITEM DOES NOT HAVE ALLOWABLE DAMAGE THEREFORE HAVE TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 STEP 9; [03] ACB FORWARD SHIELD AT BS 767+4; RBL 23 WL157 WILL BE REPLACED ON CUSTOMER FAULT# TTG8Q005NKRA; [04] VERIFIED ACB FORWARD SHIELD AT BS 767+4; RBL 23 WL157 WILL BE REPLACED ON CUSTOMER FAULT# TTG8Q005NKRA

Part: SHIELD — CORRODED (BS 767) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB FWD SHIELD; BS 767+8; RBL 22; WL 157 (MARKED) ; / [01] THIS ITEM DOES NOT HAVE ALLOWABLE DAMAGE THEREFORE HAVE TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 STEP 9; [02] LOCATED AND DRILLED NEW ACB FWD SHIELD BS 767-794 RBL 22 WL 157 IAW SRM 51-40-05 ; AND DWG # 146A8127 OK TO INSTALL; [03] LOCATED AND DRILLED NEW ACB FWD SHIELD BS 767-794 RBL 22 WL 157 ; IAW SRM 51-40-05 AND DWG# 146A8127 OK TO INSTALL; [04] THIS ITEM DOES NOT HAVE ALLOWABLE DAMAGE THEREFORE HAVE TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 STEP 9; [05] LOCATED AND DRILLED NEW ACB FWD SHIELD BS 767-794 RBL 22 WL 157 ; IAW SRM 51-40-05 AND DWG# 146A8127 OK TO INSTALL; [06] CORRECTED MEASUREMENTS; [07] VERIFIED LOCATED AND DRILLED NEW ACB FWD SHIELD BS 767-794 RBL 22 WL 157 ; IAW SRM 51-40-05 AND DWG# 146A8127 OK TO INSTALL GIVEN.; [08] INSTALLED NEW ACB FWD SHIELD BS 767-794 RBL 22 WL 157 ; IAW SRM 51-40-02 AND DWG#146A0081; [09] COMPLETED NRC; [10] VERIFIED CORRECTIVE ACTIONS ITEM 8; INSTALLATION OF NEW ACB FWD SHIELD BS 767-794 RBL 22 WL 157 ; IAW SRM 51-40-02 AND DWG#146A0081; [11] VERIFIED FAULT COMPLETE

Part: SUPPORT — CORRODED (BS 407) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 407; RBL 24; WL 156.5 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53--1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION FROM FCB FLOOR TO SIDEWALL SUPPORT BS407; RBL24; WL156.5; P/N 143A7501-184 IN AREA 0.9''X0.3''X0.010'' DEEP; ORIGINAL THICKNESS 0.040''; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; PAR. 4.A(2) FIG. 103 .<BR>TOOL USED DEPTH GAGE; ID:ATS2473; N/S/N; [03] FCB FLOOR TO SIDEWALL SUPPORT BS407; RBL24; WL156.5; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD #TTG8Q005N9P3; [04] VERIFIED CORRECTIVE ACTIONS 1-3.<BR><BR>CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2<BR><BR>PART TO BE REPLACED ON TTG8Q005N9P3; [05] FCB FLOOR TO SIDEWALL SUPPORT BS407; RBL24; WL156.5; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD #TTG8Q005N9P3; [06] VERIFIED REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD #TTG8Q005N9P3

Part: SUPPORT — CORRODED (BS 446 LBL25) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 446.25; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS446.25'';LBL25;WL157; P/N:143A7501-1; IN AREA 2''X1''X0.018''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] REMOVED FCB FLOOR TO SIDEWALL SUPPORT BS400-BS500D; LBL25; WL157 IAW SRM 51-40-02-0G-0; [04] VERIFIED APPLICABILITY STATEMENT; DIMENSION; AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [05] CORRECTED MEASUREMENTS; [06] CORRECTION: REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS446.25'';LBL25;WL157; P/N:143A7501-183 [07] FABRICATED FLOOR TO SIDEWALL SUPPORT ZEE CHANNEL SIDEPLATE FROM BAC1496--444-7075T6 CLAD LOT#1457306-1. TREATED IAW SRM 53-00-53-2R-6 REPAIR 6. OK TO PRIME;

Part: SUPPORT — CORRODED (BS 500A) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500A+10.5; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS500A+10.5'';LBL25;WL157; P/N:143A7501-1; IN AREA 0.9''X0.8''X0.012''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500A+10.5''; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 727C) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 727C+6; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB R/H SIDEWALL SUPPORT AT BS 727C+6 RBL 21 WL 157; REWORKED AREA; L: 1.3' W: 0.750' ORIGINAL THICKNESS 0.040' REMOVED MAT. 0.008' REMAINING MAT. 0.032' FOUND TO BE OUT LIMIT IAW SRM 53-00-53-1A-2; TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 727C+6 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 767) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 767+15; LBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 767+15; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 1.400' W= 1' D= 0.002' MATERIAL REMAINING IS 0.038' FOUND TO BE WITHIN LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [02] 1. GILBERTO AGUILAR (TECHNICIAN); 04-JUL-2021 19:57 UTC <BR>REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 767+15; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 1.400' W= 1' D= 0.002' MATERIAL REMAINING IS 0.038' ORIGINAL THICKNESS 0.040' FOUND TO BE WITHIN LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [03] VERIFIED IN LIMITS PER SRM 53-00-53-1A-2; [04] FLOOR TO SIDEWALL TO BE REPLACED ON FAULT TTG8Q005NLFV; [05] VERIFIED PART TO BE REPLACED ON FAULT# TTG8Q005NLFV

Part: SUPPORT — CORRODED (BS 747) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 747+2; RBL 21; ; / [01] REMOVED CORROSION ON SIDEWALL SUPPORT AT BS 747+2 RBL 21 WL 157; REWORKED AREA; L:1.2' W: 0.500' ORIGINAL THICKNESS 0.040' REMOVED MAT; 0.007' REMAINING MAT; 0.033' FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 747+2 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 727C) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 727C+2; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB R/H SIDEWALL SUPPORT AT BS 727C+2 RBL 21 WL 157; REWORKED AREA; L: 1.4' W: 0.650' ORIGINAL THICKNESS 0.040' REMOVED MAT. 0.010' REMAINING MAT. 0.030' FOUND TO BE OUT LIMIT IAW SRM 53-00-53-1A-2; TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 727C+2 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 747) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 747+6; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON SIDEWALL SUPPORT AT BS 747+6 RBL 21 WL 157; REWORKED AREA; L:1.2' W: 0.750' ORIGINAL THICKNESS 0.040' REMOVED MAT; 0.008' REMAINING MAT; 0.032 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 747+6 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 727B) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 727B+10; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB R/H SIDEWALL SUPPORT AT BS 727B+10 RBL 21 WL 157; REWORKED AREA; L: 1.1' W: 0.550' ORIGINAL THICKNESS 0.040' REMOVED MAT. 0.007' REMAINING MAT. 0.033' FOUND TO BE OUT LIMIT IAW SRM 53-00-53-1A-2; TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 727B+10 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 500C) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500C+14.5; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FLOOR TO SIDEWALL SUPPORT BS500C+14.5;LBL25;WL157; P/N:143A7501-1; IN AREA 0.8''X0.4''X0.012''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500C+14.5''; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 727B) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 727B+13 - 727B+18; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB R/H SIDEWALL SUPPORT AT BS 727B+13 - 727B+18 RBL 21 WL 157; REWORKED AREA; L: 5'' W: 0.700' ORIGINAL THICKNESS 0.040' REMOVED MAT. 0.008' REMAINING MAT. 0.032' FOUND TO BE OUT LIMIT IAW SRM 53-00-53-1A-2; TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 727B+13 - 727B+18 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 727C) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 727C+10; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB R/H SIDEWALL SUPPORT AT BS 727C+10 RBL 21 WL 157; REWORKED AREA; L: 1.2' W: 0.650' ORIGINAL THICKNESS 0.040' REMOVED MAT. 0.010' REMAINING MAT. 0.030' FOUND TO BE OUT LIMIT IAW SRM 53-00-53-1A-2; TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 727C+10 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 747) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 747+18; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON SIDEWALL SUPPORT AT BS 747+18 RBL 21 WL 157; REWORKED AREA; L:1.5' W: 0.650' ORIGINAL THICKNESS 0.040' REMOVED MAT;0.008 ' REMAINING MAT; 0.032 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 747+18 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 727C) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 727C+14; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB R/H SIDEWALL SUPPORT AT BS 727C+14 RBL 21 WL 157; REWORKED AREA; L: 1.1' W: 0.600' ORIGINAL THICKNESS 0.040' REMOVED MAT. 0.009' REMAINING MAT. 0.031' FOUND TO BE OUT LIMIT IAW SRM 53-00-53-1A-2; TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 727C+14 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 727E) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 727E+2; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON SIDEWALL SUPPORT AT BS 727B+2 RBL 21 WL 157; REWORKED AREA; L:1.1' W: 0.700' ORIGINAL THICKNESS 0.040' REMOVED MAT; 0.009' REMAINING MAT; 0.031 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 727C+18 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] ACB R/H SIDEWALL SUPPORT AT BS 727E+2 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [04] BS CORRECTION=REMOVED CORROSION ON SIDEWALL SUPPORT AT BS 727E+2 RBL 21 WL 157; REWORKED AREA; L:1.1' W: 0.700' ORIGINAL THICKNESS 0.040' REMOVED MAT; 0.009' REMAINING MAT; 0.031 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 TOOL ID: ATS1671 DUE DATE: 01/2022; [05] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON CC TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 727-747) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 747+14 - 727+16; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON SIDEWALL SUPPORT AT BS 747+14 RBL 21 WL 157; REWORKED AREA; L:1.5' W: 0.700' ORIGINAL THICKNESS 0.040' REMOVED MAT; 0.009' REMAINING MAT; 0.031' FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 747+14 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 500C) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500C+6.5; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS500C+6.5;LBL25;WL157; P/N:143A7501-1; IN AREA 0.9''X0.7''X0.012''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500C+6.5''; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 500C) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500C+2; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS500C+2;LBL25;WL157; P/N:143A7501-1; IN AREA 0.8''X0.4''X0.012''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500C+2''; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 454.5) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 454.5; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS454.5'';LBL25;WL157; P/N:143A7501-1; IN AREA 1.5''X1''X0.015''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] FCB FLOOR TO SIDEWALL SUPPORT BS454.5; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [04] CORRECTED MEASUREMENTS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 727D) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+7; LBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+7; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 0.7OO' W= 0.0670' D= 0.017' ALLOWABLE MATERIAL REMAINING IS 0.023' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [02] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+7; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 0.7OO' W= 0.0670' D= 0.017' MATERIAL REMAINING IS 0.023' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [03] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+7; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 0.7OO' W= 0.0670' D= 0.017' MATERIAL REMAINING IS 0.023' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [04] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; [05] FLOOR TO SIDEWALLL TO BE REPLACED ON FAULT NUM. TTG8Q005NLFV; [06] VERIFIED WORK TO BE ACCOMPLISHED ON FAULT# TTG8Q005NLFV

Part: SUPPORT — CORRODED (BS 747) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 747+11; LBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 747+11; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 0.900' W= 0.0750' D= 0.016' MATERIAL REMAINING IS 0.024' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [02] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 747+11; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 0.900' W= 0.0750' D= 0.016' MATERIAL REMAINING IS 0.024' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [03] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 747+11; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 0.900' W= 0.0750' D= 0.016' MATERIAL REMAINING IS 0.024' ORIGINAL THICKNESS 0.040'FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [04] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; [05] FLOOR TO SIDEWALL TO BE REPLACED ON FAULT TTG8Q005NLFV; [06] VERIFIED PART TO BE REPLACED ON FAULT# TTG8Q005NLFV

Part: SUPPORT — CORRODED (BS 767) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 767+7; LBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 767+7; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 1.125' W= 0.0750' D= 0.013' MATERIAL REMAINING IS 0.027' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [02] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 767+7; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 1.125' W= 0.0750' D= 0.013' MATERIAL REMAINING IS 0.027' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [03] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; [04] FLOOR TO SIDEWALL TO BE REPLACED ON FAULT TTG8Q005NLFV; [05] VERIFIED PART TO BE REPLACED ON FAULT# TTG8Q005NLFV

Part: SUPPORT — CORRODED (BS 727D) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+19; LBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+19; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 1' W= 0.0580' D= 0.018' ALLOWABLE MATERIAL REMAINING IS 0.022' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [02] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+19; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 1' W= 0.580' D= 0.018' MATERIAL REMAINING IS 0.022' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [03] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+19; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 1' W= 0.580' D= 0.018' MATERIAL REMAINING IS 0.022' ORIGINAL THICKNESS 0.040'FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [04] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; [05] FLOOR TO SIDEWALL TO BE REPLACED ON FAULT TTG8Q005NLFV; [06] VERIFIED PART TO BE REPLACED ON FAULT# TTG8Q005NLFV

Part: SUPPORT — CORRODED (BS 505) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 505; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS505;LBL25;WL157; P/N:143A7501-1; IN AREA 1.2''X0.5''X0.012''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS505; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 747) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 747+11; LBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 747+11; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 0.900' W= 0.0750' D= 0.016' MATERIAL REMAINING IS 0.024' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [02] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] FLOOR TO SIDEWALL TO BE REPLACED ON FAULT TTG8Q005NLFV; [04] VERIFIED PART TO BE REPLACED ON FAULT# TTG8Q005NLFV

Part: SUPPORT — CORRODED (BS 807) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 807+11; LBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 807+11; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 0.980' W= 0.750' D= 0.007' MATERIAL REMAINING IS 0.033' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [02] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 807+11; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 0.980' W= 0.750' D= 0.007' MATERIAL REMAINING IS 0.033' N ORIGINAL THICKNESS 0.040' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [03] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; [04] FLOOR TO SIDEWALL TO BE REPLACED ON FAULT TTG8Q005NLFV; [05] VERIFIED PART TO BE REPLACED ON FAULT# TTG8Q005NLFV

Part: SUPPORT — CORRODED (BS 410) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 410.5; RBL 25; WL 157, VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53--1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION FROM FCB FLOOR TO SIDEWALL SUPPORT BS410.5; RBL25; WL157; P/N 143A7501-184 IN AREA 1.3''X0.4''X0.015'' DEEP; ORIGINAL THICKNESS 0.040''; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; PAR. 4.A(2) FIG. 103 .<BR>TOOL USED DEPTH GAGE; ID:ATS2473; N/S/N; [03] FCB FLOOR TO SIDEWALL SUPPORT BS410.5; RBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD #TTG8Q005N9P3; [04] VERIFIED CORRECTIVE ACTIONS 1-3. CORROSION DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2<BR><BR>PART TO BE REPLACED ON TTG8Q005N9P3; [05] FCB FLOOR TO SIDEWALL SUPPORT BS410.5; RBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD #TTG8Q005N9P3; [06] REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD# TTG8Q005N9P3

Part: SUPPORT — CORRODED (BS 402) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 402; RBL 24; WL 156.5 (MARKED). ; / [01] REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS.402; RBL 24; WL156.5 PER SRM 51-10-02 MAX. MAT. LOSS L=1.5' X W=.6' X D=0.020' REMAINING THICKNESS IS 0.020' . FOUND OUT OF LIMITS REWORKED AREA IAW. SRM 53-00-53-1A-2 PARAG. 4.A.(2) DETAIL D FIG 103. AND SRM 53-30-53-0I-2 IDENTIFICATION 2 TABLE 2 ITEM 1 BAC1496-444 ORIG.THICKNESS 0.040'. USED TOOL ID:ATS1672;S/N 65092939;DUE DATE:03/2022.; [02] REMOVED FCB FLOOR TO SIDEWALL SUPPORT BS400 BS420; RBL24; WL156.5 IAW SRM 51-40-02-0G-0; [03] VERIFIED CORRECTIVE ACTIONS 1 AND 2.<BR><BR>CORROSION DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [10] INSTALLED ON FCB FLOOR TO SIDEWALL SUPPORT BTW BS.400- 420; WL;156.5; RBL.24; PER SRM 51-40-02;DWG#143A7500.; [11] REMOVED AND REPLACE ON FCB FLOOR TO SIDEWALL SUPPORT P/N 143A7501-184 PER SRM51-10-02; ITEM 9.C. DWG# 143A7500.

Part: SUPPORT — CORRODED (BS 727B) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 727B+6; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON SIDEWALL SUPPORT AT BS 727B+6 RBL 21 WL 157; REWORKED AREA; L:1.1' W: 0.500' ORIGINAL THICKNESS 0.040' REMOVED MAT; 0.008' REMAINING MAT; 0.032 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 727B+6 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 727C) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 727C+18; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB R/H SIDEWALL SUPPORT AT BS 727C+18 RBL 21 WL 157; REWORKED AREA; L: 1.4' W: 0.700' ORIGINAL THICKNESS 0.040' REMOVED MAT. 0.008' REMAINING MAT. 0.032' FOUND TO BE OUT LIMIT IAW SRM 53-00-53-1A-2; TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 727C+18 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE INSTALLED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 514.25) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 514.25; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS514.25'';LBL25;WL157; P/N:143A7501-1; IN AREA 1''X0.9''X0.018''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS514.25; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 727D) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+15; LBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+15; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 1`' W= 0.600' D= 0.018 ALLOWABLE MATERIAL REMAINING IS 0.022' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [02] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+15; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 1' W= 0.600' D= 0.018' MATERIAL REMAINING IS 0.022' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [03] 2. GILBERTO AGUILAR (TECHNICIAN); 04-JUL-2021 20:41 UTC <BR>REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+15; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 1' W= 0.600' D= 0.018' MATERIAL REMAINING IS 0.022' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [04] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; [05] FLOOR TO SIDEWALL TO BE REPLACED ON FAULT TTG8Q005NLFV; [06] VERIFIED PART TO BE REPLACED ON FAULT# TTG8Q005NLFV

Part: SUPPORT — CORRODED (BS 500C) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500C+12; LBL 24; WL 156.5 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS500C+12;LBL24;WL157; P/N:143A7501-1; IN AREA 0.8''X0.5''X0.012''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500C+12''; LBL24; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: STRAP — CORRODED (BS 787) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB TENSION STRAP; BS 787+12; RBL 19; WL 157 (MARKED) ; / [01] EVALUATED ACB TENSION STRAP BS 787+12 RBL 19 WL 157 AND FOUND TO BE OUT OF LIMITS DUE TO EXCEEDS THE ALLOWABLE LIMITS IAW SRM 53-60-15-1A-1 PART 4G(3); PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; MEASURES L=1.0'' X W=0.8'' X D=0.030'' TOOL USED DIGITAL CALIPER P/N ATS2318 S/N B19006095 DEPTH GAUGE P/N ATS2472 S/N UNKNOWN; [02] VERIFIED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1.<BR><BR>PART TO BE REPLACED.; [03] REMOVED ACB TENSION STRAP BS 787+12'' RBL 19 WL 157;<BR>IAW SRM 51-40-02-0G-0; [04] REMOVED ACB TENSION STRAP BS 770-860 RBL 19 WL 157;IAW SRM 51-40-02-0G-0; [05] RECIVED NEW STRAP ITEM 7530562 LOT 1457399-1 P/N 146A8128-14 LOCATED AND DRILLED NEW STRAP AT BS 787+12 RBL 19; WL 157; IAW B 737-700 SRM 51-40-05-OG-0 DWG 146A8120; [06] OK TO INSTALL STRAP; [07] VERIFIED NEW TENSION STRAP RECEIVED AND LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 146A8120; [08] INSTALLED NEW TENSION STRAP AT BS 767+8 - 847+15 RBL 19 WL 157 . IAW 773-700 SRM 51-40-02-0G-0; DWG 146A8120 AND DWG 146A0081 .; [09] VERIFIED INSTALLATION OF THE NEW TENSION STRAP AT BS 767+8 - 847+15 RBL 19 WL 157 . IAW 773-700 SRM 51-40-02-0G-0; DWG 146A8120 AND DWG 146A0081; [10] ALL ITEMS ARE COMPLETE; [11] UPDATED PARTS USAGE; [12] VERIFIED FAULT COMPLETE

Part: SUPPORT — CORRODED (BS 887) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 887+11; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB R/H SIDEWALL SUPPORT AT BS 887+11 RBL 21 WL 157; REWORKED AREA; L: 1.5' W: 0.700' ORIGINAL THICKNESS 0.040' REMOVED MAT. 0.009' REMAINING MAT. 0.031' FOUND TO BE OUT LIMIT IAW SRM 53-70-53-1A-2; TOOL ID: ATS1671 DUE DATE: 01/2022; [02] REMOVED ACB R/H SIDEWALL SUPPORT AT BS 887 TO BS 947 RBL 21 IAW SRM 51-40-02-0G-0; [03] FABRICATED ACB R/H FLOOR TO SIDEWALL SUPPORT AT BS 887 TO BS 947 RBL 21; FROM MATERIAL BAC1496-377#7075-T62 LOT # 1454325-1; IAW DWG 147A7501 LOCATED AND DRLLED NEW SIDEWALL SUPPORT IAW SRM 51-40-05- 0G-0; [04] VERIFIED FABRICATION/LOCATE AND DRILL OF R/H FLOOR-TO-SIDEWALL SUPPORT; BS 887-947; RBL 21 IAW SRM 51-40-05-0G-0; [05] APPLIED A CHEMICAL CONVERSION COATING AND PRIMED THE NEW ACB FLOOR TO SIDEWALL SUPPORT R/H BS 847 TO BS 947 RBL 21; IAW SOPM 20-43-03 & SOPM 20-44-04 OK TO INSTALL; [06] APPLIED A CHEMICAL CONVERSION COATING AND PRIMED THE NEW ACB FLOOR TO SIDEWALL SUPPORT R/H BS 847 TO BS 947 RBL 21; IAW SOPM 20-43-03 & SOPM 20-44-04 OK TO INSTALL; [07] CORRECTED MEASUREMENT; [08] VERIFIED APPLICATION OF CONVERSION COATING AND PRIMER. <BR>IAW SOPM 20-43-03 & SOPM 20-44-04<BR><BR>OK TO INSTALL; [09] INSTALLED FLOOR TO SIDEWALL SUPPORT AT ACB BS 847-947; RBL21; WL157 PER SRM 51-40-02-0G-0; SRM 53-00-53-2R-6; AND BOEING DRAWING #146A7500.

Part: SUPPORT — CORRODED (BS 517) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 517; LBL 24; WL 156.5 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS517'';LBL24;WL156.5; P/N:143A7501-1; IN AREA 0.9''X0.5''X0.015''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS517; LBL24; WL156.5; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 500B) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500B+14.5; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS500B+14.5'';LBL25;WL157; P/N:143A7501-1; IN AREA 1''X0.8''X0.012''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A. CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500B+14.5''; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 518.5) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 518.5; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS518.5'';LBL25;WL157; P/N:143A7501-1; IN AREA 0.9''X0.8''X0.015''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS518.5; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 727E) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 727E+5; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON SIDEWALL SUPPORT AT BS 727E+5 RBL 21 WL 157; REWORKED AREA; L:1.5' W: 0.650' ORIGINAL THICKNESS 0.040' REMOVED MAT; 0.009' REMAINING MAT; 0.031 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 727E+5 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 510.25) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 510.25; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS510.25'';LBL25;WL157; P/N:143A7501-1; IN AREA 1.1''X0.7''X0.015''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS510.25; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 474.5) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 474.5; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS474.5;LBL25;WL157; P/N:143A7501-1; IN AREA 1.3''X1''X0.015''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS474.5; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 727E) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 727E+8 - 727E+14; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON SIDEWALL SUPPORT AT BS 727E+8 - 727E+14 RBL 21 WL 157; REWORKED AREA; L:6' W: 0.800' ORIGINAL THICKNESS 0.040' REMOVED MAT; 0.008' REMAINING MAT; 0.032 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 727E+8-727E+14 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: SUPPORT — CORRODED (BS 470.5) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 470.5; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS470.5;LBL25;WL157; P/N:143A7501-1; IN AREA 1''X0.8''X0.015''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS470.5; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 500C) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500C+14.5; RBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500C+14.5''; RBL25; WL157; P/N 143A7501-86; IN AREA: 1.5''X1''X0.020'' DEEP; ORIGINAL THICKNESS 0.040''; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; PAR.4.A(2) FIG. 103.; [03] REMOVED FCB FLOOR TO SIDEWALL SUPPORT BS500C+14.5'';RBL25;WL157;IAW SRM 51-40-02-0G-0; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500C+14.5;RBL25;WL157; REPLACEMENT ACCOMPLISHED ON TASK CARD# TTG8Q005NA5E; [05] VERIFIED CORROSION DAMAGE OUT OF LIMITS PER SRM 53-00-53-1A-2.<BR><BR>PART TO BE REPLACED ON TTG8Q005NA5E; [06] FCB FLOOR TO SIDEWALL SUPPORT BS500C+14.5;RBL25;WL157; REPLACEMENT ACCOMPLISHED ON TASK CARD# TTG8Q005NA5E; [07] VERIFIED REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD# TTG8Q005NA5E

Part: SUPPORT — CORRODED (BS 500C) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500C+13; RBL 24; WL 156.5 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500C+13''; RBL24; WL156.5; P/N 143A7501-86; IN AREA: 2''X1''X0.015'' DEEP; ORIGINAL THICKNESS 0.040''; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; PAR.4.A(2) FIG. 103.; [03] REMOVED FCB FLOOR TO SIDEWALL SUPPORT BS500C+13'';RBL24;WL156.5;IAW SRM 51-40-02-0G-0; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500C+13'';RBL24;WL156.5; REPLACEMENT ACCOMPLISHED ON TASK CARD# TTG8Q005NA5E; [05] VERIFIED CORROSION DAMAGE OUT OF LIMITS PER SRM 53-00-53-1A-2.<BR><BR>PART TO BE REPLACED ON TTG8Q005NA5E; [06] FCB FLOOR TO SIDEWALL SUPPORT BS500C+13'';RBL24;WL156.5; REPLACEMENT ACCOMPLISHED ON TASK CARD# TTG8Q005NA5E; [07] VERIFIED REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD #TTG8Q005NA5E

Part: SUPPORT — CORRODED (BS 500A) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500A+14.5; RBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500A+14.5''; RBL25; WL157; P/N 143A7501-86; IN AREA: 2''X0.8''X0.018'' DEEP; ORIGINAL THICKNESS 0.040''; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; PAR.4.A(2) FIG. 103.; [03] REMOVED FCB FLOOR TO SIDEWALL SUPPORT BS500A+14.5'';RBL25;WL157;IAW SRM 51-40-02-0G-0; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500A+14.5;RBL25;WL157; REPLACEMENT ACCOMPLISHED ON TASK CARD# TTG8Q005NA5E; [05] VERIFIED CORROSION DAMAGE OUT OF LIMITS PER SRM 53-00-53-1A-2.<BR><BR>PART TO BE REPLACED ON TTG8Q005NA5E; [06] FCB FLOOR TO SIDEWALL SUPPORT BS500A+14.5;RBL25;WL157; REPLACEMENT ACCOMPLISHED ON TASK CARD# TTG8Q005NA5E; [07] VERIFIED REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD #TTG8Q005NA5E

Part: SHIELD — CORRODED (BS 514) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB AFT SHIELD BS 514; RBL 24; WL 156.5 (MARKED). ; / [01] NOT HAVE ENTRIES FOR ALLOWABLE DAMAGE IN SRM. THE PART MUST BE REPAIRED BY REPLACEMENT PER SRM. 51-10-02 ITEM 9.C.; [02] VERIFIED PART WILL BE REPLACE PER SRM 51-10-02 STEP 9.; [03] LOCATED AND DRILLED SHIELD P/N 143A8126-21; LOT.#146355;IAW SRM.51-40-05; DWG#143A0080.; [04] VERIFIED LOCATED AND DRILLED NEW SHIELD PER SRM 51-40-05; DWG#143A0080.; [05] CORRECTED PART Y LOT NUMBER OF THE SHIELD P/N 143A8126-31; LOT.#1461424;IAW SRM.51-40-05; DWG#143A0080.; [06] OK TO INSTALL ON FCB AFT SHIELD BTW BS.500-500A;RBL24;WL156.5; [07] OK TO INSTALL; [08] INSTALLED ON FCB AFT SHIELD P/N143A8126-31 BTW BS.500-500A;RBL24;WL156.5 PER SRM.51-40-02;DWG#143A0080.; [09] REMOVED AND REPLACED ON FCB AFT SHIELD P/N143A8126-31 BTW BS.500-500A;RBL24;WL156.5 PER SRM.51-10-02 ITEM 9.C. DWG#143A0080; [10] STEP 8 AND 9 COMPLETED; [11] VERIFIED INSTALLATION OF FCB AFT SHIELD P/N143A8126-31 BTW BS.500-500A;RBL24;WL156.5 PER SRM.51-10-02 ITEM 9.C. DWG#143A0080; [12] COMPLETE

Part: SUPPORT — CORRODED (BS 500B) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500B+10.5; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS500B+10.5'';LBL25;WL157; P/N:143A7501-1; IN AREA 0.9''X0.7''X0.012''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500B+10.5''; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 500A) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500A+14.5; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS500A+14.5'';LBL25;WL157; P/N:143A7501-1; IN AREA 1''X0.9''X0.015''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500A+14.5''; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 500A) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500A+6.5; LBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS500A+6.5'';LBL25;WL157; P/N:143A7501-1; IN AREA 0.8''X0.7''X0.018''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500A+6.5''; LBL25; WL157; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 727D) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 727D+6; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB R/H SIDEWALL SUPPORT AT BS 727D+6 RBL 21 WL 157; REWORKED AREA; L: 4' W: 0.800' ORIGINAL THICKNESS 0.040' REMOVED MAT. 0.008' REMAINING MAT. 0.032' FOUND TO BE OUT LIMIT IAW SRM 53-00-53-1A-2; TOOL ID: ATS1671 DUE DATE: 01/2022; [02] LOCATED AND DRILLED NEW ACB R/H FLOOR TO SIDEWALL SUPPORT BS 727 - 767 RBL 21 WL 157 IAW SRM 51-40-05 AND SRM 53-60-53-0I-2 OK TO TREAT AND PRIME; [03] LOCATED AND DRILLED NEW ACB R/H FLOOR TO SIDEWALL SUPPORT BS 727 - 767 RBL 21 WL 157; MATERIAL USED BAC1496-377 #7075T62 LOT#1459405-1 IAW SRM 51-40-05 AND SRM 53-60-53-0I-2 OK TO TREAT AND PRIME; [04] VERIFIED CORROSION DAMAGE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [05] VERIFIED PART FABRICATED; LOCATED AND DRILLED PER DWG 146A7502; SRM 51-40-05 AND SRM 53-60-53-0I-2.<BR><BR>OK TO TREAT AND PRIME.; [06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON NEW SIDEWALL SUPPORT AT BS 727 TO BS 767 ACB RBL 21 WL 157; IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02; [07] VERIFIED APPLICATIONS CHEMICAL CONVERSION COATING AND PRIMER PER SRM 51-20-01-0G; SOPM 20-41-02.; [08] OK TO INSTALL THE NEW ACB SIDEWALL SUPPORT AT BS 727 TO BS 767 ACB RBL 21 WL 157;

Part: SUPPORT — CORRODED (BS 727B) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727B+15; LBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727+15; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 0.760' W= 0.0700' D= 0.018 ALLOWABLE MATERIAL REMAINING IS 0.022' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [02] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727B+15; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 0.760' W= 0.700' D= 0.018' MATERIAL REMAINING IS 0.022' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [03] REMOVED CORROSION ON ACB L/H FLOOR-TO-SIDEWALL SUPPORT; BS 727B+15; LBL 21; WL 157 WITH FOLLOWING MEASURES L= 0.760' W= 0.700' D= 0.018' MATERIAL REMAINING IS 0.022' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT LIMITIS PER SRM 53-00-53-1A-2 TOOL USE ID: ATS1671 S/N 65093024 DATE 04/2021 DUE 01/2022; [04] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; [05] REMOVED SIDEWALL SUPPORT ACB AT BS 727 TO BS 847 LBL 21 WL 157 IAW SRM 51-40-02-0G-0; [06] FABRICATED NEW L/H FLOOR TO SIDEWALL SUPPORT ITEM BAC1496-377#7075T62 C LOT # 1459405-1 BS 727-847; LBL 21; WL 154; IAW PER SRM 51-40-05 DWGS: 146A7502 AND FABRICATED SPLICE FROM BAC1496-377#7075T62C B.S727E +10 IAW SRM 53-00-53-2R-6; OK TREAT AND PRIMER; [07] VERIFIED FABRICATION OF FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-05; SRM 53-00-53-2R-6. OK TO CHEMICALLY TREAT AND PRIMER PARTS.

Part: SUPPORT — CORRODED (BS 500B) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500B+17.75; LBL 24; WL 156.5 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION O FCB FLOOR TO SIDEWALL SUPPORT BS500B+17;LBL24;WL156.5; P/N:143A7501-1; IN AREA 0.9''X0.5''X0.012''DEEP; ORIGINAL THICKNESS 0.040'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR.4(2) FIG. 103; DETAIL A.<BR>TOOL USED: DEPTH GAGE ID:ATS2473; N/S/N; [03] CORRECTED MEASUREMENTS; [04] FCB FLOOR TO SIDEWALL SUPPORT BS500B+17.75''; LBL24; WL156.5; REPLACEMENT TO BE ACCOMPLISHED ON TASK CARD TTG8Q005NAAS; [05] VERIFIED CUSTOMER CARD TTG8Q005NAAS WILL BE REPLACE.

Part: SUPPORT — CORRODED (BS 500A) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500A+10.5; RBL 25; WL 157 (MARKED). ; / [01] VERIFIED APPLICABILITY OF SRM 53-30-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE; [02] REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500A+10''; RBL25; WL157; P/N 143A7501-86; IN AREA: 2''X1''X0.018'' DEEP; ORIGINAL THICKNESS 0.040''; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; PAR.4.A(2) FIG. 103.; [03] REMOVED FCB FLOOR TO SIDEWALL SUPPORT BS500A+10.5'';RBL25;WL157;IAW SRM 51-40-02-0G-0; [04] VERIFIED CORROSION DAMAGE OUT OF LIMITS PER SRM 53-00-53-1A-2; [05] LOCATED AND DRILLED CHANNEL WITH P/N 143A7501-186. BAC1496-444; LOT.#1446325-1; 143 LOCATED ON FCB BTW. BS.500A-BS500D;RBL.25;WL.157 IAW. SRM 51-40-05;SRM.53-30-53-0I-2 IDENTIFICATION2;DWG#143A7501. OK TO TREAT AND PRIMER.; [06] VERIFIED LOCATE AND DRILL OF NEW FLOOR-TO-SIDEWALL SUPPORT SRM 51-40-05; SRM.53-30-53-0I-2; AND DWG#143A7501; OK TO TREAT AND PRIMER; [07] APPLIED CHEMICAL CONVERSION COATING AND PRIMER PER SRM.51-20-01; SOPM.20-43-03.; [08] VERIFIED APPLICATION OF CHEMICAL CONVERSION COATING AND PRIMER PER SRM 51-20-01 AND SOPM 20-43-03; [11] INSTALLED ON FCB FLOOR TO SIDEWALL SUPPORT BTW. BS500A-500D; RBL.25;WL.157; PER SRM 51-40-02; DWG#143A7500.; [12] REMOVED AND REPLACED ON FCB FLOOR TO SIDEWALL SUPPORT WITH P/N 143A7501-186; BTW BS.500A - 500D; RBL.25; WL.157 PER SRM 51-10-02. ITEM 9.C. AND DWG#143A7500;

Part: SUPPORT — CORRODED (BS 747) · airframe 43,304 hrs · 26,170 cycles

CORROSION ON ACB R/H FLOOR-TO-SIDEWALL SUPPORT; BS 747+10; RBL 21; WL 157 (MARKED) ; / [01] REMOVED CORROSION ON SIDEWALL SUPPORT AT BS 747+10 RBL 21 WL 157; REWORKED AREA; L:1.2' W: 0.650' ORIGINAL THICKNESS 0.040' REMOVED MAT; 0.007' REMAINING MAT; 0.033 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 TOOL ID: ATS1671 DUE DATE: 01/2022; [02] ACB R/H SIDEWALL SUPPORT AT BS 747+10 RBL 21 WL 157 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q005NKNY; [03] VERIFIED OUT OF LIMITS AND TO BE REPLACED ON FAULT# TTG8Q005NKNY

Part: PRESSURE DECK — DENTED (BS 255) · airframe 43,304 hrs · 26,170 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. ; / [01] EVALUATED DENTED AREA ON FLIGHT DECK FLOOR BS 255 RBL 4 - LBL4 L=6.0 ; W=4.0 ; Y= .060 ; Y/W=66 ; FOUND TO BE OUT OF LIMITS IAW SRM 53-1051-1A-1 STEP 4;J;(3) FIG 105 ; DETAIL D ; DEPTH GAGE USED ID# ATS400 ; S/N UNKNOWN DUE DATE 04/2022; [02] VERIFIED - EVALUATED DENTED AREA ON FLIGHT DECK FLOOR BS 255 RBL 4 - LBL4 L=6.0 ; W=4.0 ; Y= .060 ; Y/W=66 ; FOUND TO BE OUT OF LIMITS IAW SRM 53-1051-1A-1 STEP 4;J;(3) FIG 105 ; DETAIL D ; DEPTH GAGE USED ID# ATS400 ; S/N UNKNOWN DUE DATE 04/2022; [03] REPAIRED FLIGHT DECK FLOOR DENT BS255 RB L4-LBL 4 PER EA M-21-153-00734; [04] VERIFIED FLIGHT DECK FLOOR IS REPAIRED AT BS225 RBL4-LBL4 EA M-21-153-00734.; [05] VERIFIED FLIGHT DECK FLOOR IS REPAIRED AT BS225 RBL4-LBL4 EA M-21-153-00734.

Part: STIFFENER — CRACKED (HORIZOTNAL STAB) · airframe 43,304 hrs · 26,170 cycles

LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STAB STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] TRIMMED OUT THE DAMAGED PART OF THE RIB 129.50 3RD VERTICAL STIFFENER L/H HORIZONTAL STAB. IAW SRM 55-10-09-2R-4; [02] UPDATED MEASUREMENT CHART; [03] VERIFIED DAMAGED REMOVAL AS PER SRM 55-10-09-2R-4.; [04] HFEC INSPECTION OF THE CUT OUT EDGES OF THE STIFFENER; WEB AND ALL EXISTING FASTENERS HOLES WITHIN THE REPAIR AREA TO ENSURE NO CRACKS EXIST.; [05] HFEC INSP CUTOUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [06] HFEC INSP OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; 2 EA CRACKS NOTED AT 2 EA FASTENER HOLES COMMON TO THE REPAIR AREA; AREAS MARKED. EQUIP ID#: IS000450 S/N: N500D000M120071 EQUIP ID#: ATS2407 S/N: MM1591DD064104; [07] TRIMMED OUT THE DAMAGED PART AT LOWER FLANGE OF THE RIB IAW SRM 55-10-09-2R-5; [11] FABRICATED REPAIR PARTS (1) T-SECTION FROM 60-5872 7075 T76511 LOT# 1427519-1 (2) ANGLE FROM BAC 1490-2793 7075 T62 CLAD LOT# 1461745-1 (3)FILLER FROM 7075 T6 0.050' CLAD LOT# 1407842-2 (4) SHIM FROM 7075 T6 0.020' CLAD LOT# 1381332-1; APPLIED CHEMICAL CONVERSION COATING IAW SRM 55-10-09-2R-5 OK TO PRIME.; [18] REPAIR OF L/H HORIZ. STAB. INSPAR RIB STA 129.50 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-5 COMPLETED ON ITEMS 1-17;

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 43,304 hrs · 26,170 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STAB STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] TRIMMED OUT THE DAMAGED PART OF THE RIB 129.50 3RD VERTICAL STIFFENER R/H HORIZONTAL STAB. IAW SRM 55-10-09-2R-4; [02] UPDATED MEASURMENT CHART; [03] VERIFIED DAMAGED REMOVAL AS PER SRM 55-10-09-2R-4.; [04] HFEC INSPECTION OF THE CUT OUT EDGES OF THE STIFFENER; WEB AND ALL EXISTING FASTENERS HOLES WITHIN THE REPAIR AREA TO ENSURE NO CRACKS EXIST.; [05] HFEC INSP CUT OUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [06] 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; [07] FABRICATED REPAIR PARTS (1) T-SECTION FROM 60-5872 7075 T76511 LOT# 1427519-1 (2) ANGLE FROM BAC 1490-2793 7075 T62 CLAD LOT# 1461745-1 (3) SHIM FROM 7075 T6 0.020' CLAD LOT# 1381332-1; APPLIED CHEMICAL CONVERSION COATING IAW SRM 55-10-09-2R-4 OK TO PRIME.[11] VERIFIED PRIMED REPAIR PARTS PER SRM 55-10-09-2R-4. OK TO INSTALL.; [12] INSTALLED REPAIRS PARTS AT R/H HORIZ. STAB. INSPAR RIB STA 129.50 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 43,304 hrs · 26,170 cycles

EXTERNAL POWER DOOR CUTOUT BARE STRAP ALONG AFT EDGE IS CRACKED AT PREVIOUS REPAIR ; / [01] SRM 53-10-15-2R-4 REPAIR 4 IS APPLICABLE TO THIS A/C; [02] VERIFIED APPLICABILITY OF SRM 53-10-15-2R-4 REPAIR 4. IS APPLICABLE.; [03] REMOVED PREVIOUS -1 REPAIR DOUBLER IAW SRM 51-40-02; [04] FABRICATED -1 REPAIR DOUBLER FROM 2024T3#0.050' CLAD LOT#1453158-1. TREATED IAW SRM 53-10-15-2R-4 REPAIR 4 TABLE 201. OK TO PRIME; [05] VERIFIED FABRICATION OF NEW -1 REPAIR DOUBLER FROM 2024T3#0.050' CLAD LOT#1453158-1. VERIFIED PART TREATED IAW SRM 53-10-15-2R-4 REPAIR 4 TABLE 201. OK TO PRIME; [06] PRIMED REPAIR PART AND REWORKED AREA IAW SRM 53-10-15-2R-4 REPAIR 4 STEP 4L.... OK TO INSTALL; [07] VERIFIED PRIMER APPLICATION IAW SRM 53-10-15-2R-4 REPAIR 4 STEP 4L. OK TO INSTALL.; [08] INSTALLED -1 REPAIR DOUBLER AT EXTERNAL POWER DOOR CUTOUT PER SRM 53-10-15-2R-4 REPAIR 4; [09] VERIFIED INSTALLATION -1 REPAIR DOUBLER AT EXTERNAL POWER DOOR CUTOUT PER SRM 53-10-15-2R-4 REPAIR 4.; [10] APPLIED FILLED SEAL GAPS AND APPLIED TOPCOAT AREA AT EXTERNAL POWER DOOR CUTOUT PER SRM 53-10-15-2R-4 REPAIE 4; [11] ALL ITEMS COMPLETED; [12] VERIFIED APPLIED FILLED SEAL GAPS AND APPLIED TOPCOAT AREA AT EXTERNAL POWER DOOR CUTOUT PER SRM 53-10-15-2R-4 REPAIR 4.; [13] VERIFIED ALL STEPS COMPLETE.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 42,220 hrs · 25,540 cycles

CABIN EMERGENCY LIGHT BATTERY FAILED LONG TEST (MID L/H) / REMOVED AND REPLACED PER AMM.33-51-06

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 40,639 hrs · 24,545 cycles

LEFT HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED. / R&R LEFT HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL REF AMM 53-31-31.

Part: VALVE — INOPERATIVE (FUSELAGE) · airframe 38,371 hrs · 23,086 cycles

DIVERSION, ANTI SKID INOP LIGHT ILLUMINATED DURING TAKEOFF - STAYED ON FOR 2-3 MIN IN CLIMB THEN ILLUMINATED INTERMITTENTLY FOR ANOTHER 2-3 MIN THEN EXTINGUISHED FOR REMAINDER OF FLIGHT. R&R RIGHT ALTERNATIVE AIR SPEED VALVE PER AMM.

Part: FLOOR SUPPORT — CRACKED (BS 460-480) · airframe 38,235 hrs · 22,990 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS. 460 TO BS. 480, LBL 21. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (BS 947.5) · airframe 38,235 hrs · 22,990 cycles

AFT CARGO BAY AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED ON LOWER SURFACE AT BS. 947.5, BETWEEN RBL 4 TO RBL 20. / R&R SUPPORT IAW DWG & SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 38,235 hrs · 22,990 cycles

FCB AFT SCUFF PLATE IS CRACKED / REPAIRED FWD CARGO BAY AFT SCUFF PLATE IAW SRM 1-A53-2076 REV 11

Part: NONE — CRACKED (CABIN) · airframe 38,235 hrs · 22,990 cycles

BS 540 PANEL BREAK CRACKED AT RBL 1 / REMOVED AND REPLACED WITH NEW; PANEL BREAK BS 540 BL 0. - RBL 24.75 PER SRM 51-40-05 AND 51-40-02 AND DWG # 143A0060 REV:- 88911U 30JUL19

Part: STRIP — CRACKED (FWD CARGO RH) · airframe 38,235 hrs · 22,990 cycles

FWD CARGO BAY RH FWD CAP STRIP IS CRACKED / REPLACED FWD CARGO BAY RH FWD CAP STRIP IAW AMM 25-52-10-400-801 3E.(11) 59581U 07AUG19

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 38,235 hrs · 22,990 cycles

LOWER COMPOSITE WEB UPPER ATTACH ANGLE CRACKED AT BS. 663, LBL 43. / REPAIRED ANGLE PER ER AND EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 38,235 hrs · 22,990 cycles

LT HORIZONTAL STAB REMOVABLE LEADING EDGE 5TH RIB FROM INBOARD END CRACKED. R&R RIB IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,235 hrs · 22,990 cycles

CABIN FLOOR PANEL 231AF HAS DELAMINATION ON FWD EDGE / CABIN FLOOR PANEL 231AF WITH DELAMINATION OF FWD EDGE WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A.(1)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 38,235 hrs · 22,990 cycles

CABIN FLOOR PANEL 231KF IS DELAMINATING / DUE TO THE EXTENT OF DAMAGE REPLACED CABIN FLOOR PANEL 231FK IAW SRM 51-10-02-0G-0 PARA 9A(1) AND AIPC 53-21-51-81 ITEM 165. 7066U 7/15/19

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,235 hrs · 22,990 cycles

CABIN FLOOR PANEL 231UF IS DELAMINATING / DAMAGED FLOOR PANEL 231UF WAS REPLACED WITH A SERVICEABLE PART IAW SRM 51-10-02-0G-0 PAR. 9

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,235 hrs · 22,990 cycles

CABIN FLOOR PANEL 232BF HAS DELAMINATION ON FWD EDGE / CABIN FLOOR PANEL 232BF WITH DELAMINATION ON FWD EDGE WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0. PARA 9.A.(1)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,235 hrs · 22,990 cycles

CABIN FLOOR PANEL 231GF IS DELAMINATING / DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW CABIN FLOOR PANEL 231GF USING BMS4-17 TY6 LOT#1399952-1; INSTALLED INSERTS USING BMS 5-107 LOT#AK8KD4895K; APPLIED TAPE TO LOWER SURFACE AND PART MARKED IAW SRM 53-00-50-2R-0 PARA 1A(NOTE) AND DWG 143A5810-575 57066U 7/18/19

Part: SERVICE DOOR — CORRODED (LWR FUSELAGE) · airframe 38,235 hrs · 22,990 cycles

***CORROSION*** (MULTIPLE POINTS) ON TOILET SERVICE DOOR (145AL) - MARKED / REMOVED & REPLACED TOILET SERVICE DOOR (145AL) IAW AMM 52-49-07-400-801 59191U 01AUG19

Part: PLATE — CORRODED (LAV SERV CUT OUT) · airframe 38,235 hrs · 22,990 cycles

***CORROSION*** ON HINGE CLOSEOUT PLATE AT CUTOUT FOR TOILET SERVICE DOOR (145AL) - MARKED / ACCOMPLISHED REPAIR EA 1-752-2595 REV IR AND ER 19-04268 REV IR.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 38,235 hrs · 22,990 cycles

RT HORIZONTAL STABILIZER CRACKED ON A RIB AT LOWER RADIUS THIRD FROM FORWARD STA. 120.3. REPAIRED STIFFENER IAW SRM.

Part: SUPPORT — CORRODED (BS 440-500D) · airframe 38,235 hrs · 22,990 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 440 TO 500D, LBL 23. R & R THE SUPPORT IAW SRM & DWG.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 38,235 hrs · 22,990 cycles

LOWER COMPOSITE BULKHEAD CRACKED AT BS. 663, LBL 47. REPAIRED BULKHEAD IAW SRM.

Part: SHIELD — CORRODED (BS 420-440) · airframe 38,235 hrs · 22,990 cycles

FORWARD CARGO BAY FORWARD SHIELD CORRODED BETWEEN BS 420 TO 440, RBL 23. R & R SHIELD IAW DWG & SRM.

Part: WEB — CORRODED (THRESHOLD) · airframe 38,235 hrs · 22,990 cycles

AFT CARGO BAY SUB-THRESHOLD WEB CORRODED. R&R WEB ASSEMBLY IAW SRM & DWG.

Part: ANGLE — CORRODED (BS 767-787) · airframe 38,235 hrs · 22,990 cycles

AFT CARGO BAY FORWARD SHIELD SUPPORT WEB ANGLE CORRODED AT FASTENER HOLES, BETWEEN BS. 767 TO BS. 787, RBL 21. / R&R ANGLE PER SRM AND DWG.

Part: STRINGER CLIP — DAMAGED (BS 727B) · airframe 38,235 hrs · 22,990 cycles

AFT CARGO BAY STRINGER CLIP DAMAGED AT BS. 727B. R&R STRINGER CLIP IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 38,235 hrs · 22,990 cycles

AFT CARGO BAY RT FLOOR-TO-SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 767, RBL 23. R&R SUPPORT IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 38,235 hrs · 22,990 cycles

LT WING TRAILING EDGE FOUND CRACKED ATTACH ANGLE UNDER FIXED TRAILING EDGE PANEL JUST AFT OF THE #1 PYLON ORSS. 277. R&R ANGLE IAW SRM.

Part: FRAME — CORRODED (BS 947.5) · airframe 38,235 hrs · 22,990 cycles

AFT CARGO BAY LOWER FRAME CORRODED AT BS. 947.5, BETWEEN LBL 9 TO LBL 11. / R&R FRAME IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 767-787) · airframe 38,235 hrs · 22,990 cycles

AFT CARGO BAY FORWARD FLOOR-TO-SIDEWALL SHIELD CORRODED BETWEEN BS. 767 TO BS. 787, RBL 23. / R&R SHIELD IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FWD CARGO BAY) · airframe 38,235 hrs · 22,990 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS 400 LBL25 WL156. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE CLIP AT FWD CARGO BAY BS 400 LBL 25 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 ID: 0081 REV:-

Part: GUSSET — CRACKED (FUSELAGE) · airframe 38,235 hrs · 22,990 cycles

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

Part: SUPPORT — CORRODED (BS 727-847) · airframe 38,235 hrs · 22,990 cycles

AFT CARGO BAY L/H FLOOR-TO-SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 847, LBL 23. R&R SUPPORT IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 38,235 hrs · 22,990 cycles

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

Part: STRAP — CORRODED (BS 887) · airframe 38,235 hrs · 22,990 cycles

AFT CARGO BAY FLOORBEAM STRAP CORRODED AT BS. 887, BETWEEN LBL 10 TO RBL 21. / R&R STRAP IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,235 hrs · 22,990 cycles

FORWARD CABIN INTERCOSTAL CRACKED AT BS. 277+6, BL 0. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 38,235 hrs · 22,990 cycles

AFT CABIN INTERCOSTAL CORRODED AT BS. 947+5, RBL 48. R&R INTERCOSTAL PER SRM & DWG.

Part: STRUCTURE — CORRODED (BS 753-893) · airframe 38,235 hrs · 22,990 cycles

PASSENGER CABIN INNER CHORD CORRODED BETWEEN BS. 753 TO BS. 893, RBL 63. / R&R INNER CHORD PER SRM & DWG.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 38,235 hrs · 22,990 cycles

AFT CABIN FLOOR BEAM CORRODED AT BS. 986, LBL 43. / REPAIRED FLOOR BEAM PER EA AND ER.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 38,235 hrs · 22,990 cycles

AFT CABIN WEB CORRODED BETWEEN BS. 986 TO BS. 1016, RBL 38. R&R SHEAR WEB IAW SRM AND DWG.

Part: STRAP — CORRODED (MAIN CABIN) · airframe 38,235 hrs · 22,990 cycles

***CORROSION*** ON TENSION STRAP AT AFT CABIN BS1016 LBL3 WL208. MARKED / CORROSION ON TENSION STRAP BS1016 LBL3 WL208 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN IN SRM REPAIRED PER ATS ER 19-04030 REV IR AND EA 1-753-35322 REV IR

Part: BEAM — CRACKED (R1 DOOR) · airframe 38,235 hrs · 22,990 cycles

R1 DOOR NR 4 LOWER BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. R&R NR 4 BEAM PER AMM.

Part: WEB — CORRODED (MAIN CABIN) · airframe 38,235 hrs · 22,990 cycles

***CORROSION*** ON 1016 WEB AT AFT CABIN BS1016 LBL19 WL208. MARKED / CORROSION ON WEB BS1016 LBL19 WL208 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN IN SRM REPAIRED PER ATS ER 19-04030 REV IR AND EA 1-753-35322 REV IR

Part: STRAP — CORRODED (MAIN CABIN) · airframe 38,235 hrs · 22,990 cycles

***CORROSION*** ON TENSION STRAP AT AFT CABIN BS1016 RBL3 WL208. MARKED / CORROSION ON TENSION STRAP AT BS1016 RBL3 WL208 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN IN SRM REPAIRED PER ATS ER 19-04030 REV IR AND EA 1-753-35322 REV IR

Part: STRAP — CORRODED (MAIN CABIN) · airframe 38,235 hrs · 22,990 cycles

***CORROSION*** ON TENSION STRAP AT AFT CABIN BS1016 +13 RBL18 WL208. MARKED / CORROSION ON TENSION STRAP BS1016+13 RBL18 WL208 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN IN SRM REPAIRED PER ER 19-04030 REV UR AND EA 1-753-35322 REV IR

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,235 hrs · 22,990 cycles

FORWARD CABIN INTERCOSTAL CRACKED AT BS. 312+6, RBL 31. R&R INTERCOSTAL IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,235 hrs · 22,990 cycles

FORWARD ENTRY DOOR MOP SILL CORRODED AT BS. 328+7, LBL 58. R&R MOPSILL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (MAIN CABIN) · airframe 38,235 hrs · 22,990 cycles

***CORROSION*** ON FLOOR BEAM AT AFT CABIN BS986 RBL37 WL208. / BLENDED CORROSION ON BS986 FLOOR BEAM RBL37 WL208; 3' X .25' X .014' ORIGINAL THICKNESS .150' FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1 REPAIRED PER EA 1-A53-8241 REV 3

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,235 hrs · 22,990 cycles

FORWARD CABIN INTERCOSTAL CRACKED AT BS. 312+6, LBL 47. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR PANEL — WORN (CABIN) · airframe 38,235 hrs · 22,990 cycles

FWD CABIN FLOOR PANEL 221BF WORN. REPAIRED FLOOR PANEL PER SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 38,235 hrs · 22,990 cycles

FORWARD CABIN FLOOR PANEL 221DF HAD DAMAGED UPPER SURFACE SKIN. REPAIRED FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 38,235 hrs · 22,990 cycles

FORWARD CABIN FLOOR PANEL 222DF DAMAGED UPPER SURFACE SKIN PLIES, BETWEEN BS. 270 TO BS. 420. REPAIRED FLOOR PANEL IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 38,235 hrs · 22,990 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS. 665, LBL 31. REPAIRED DECK PER SRM, MM, & DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 38,235 hrs · 22,990 cycles

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

Part: SPAR — CRACKED (LT HORIZ STAB) · airframe 37,537 hrs · 22,524 cycles

TRANSFERRED FROM LOGBOOK PAGE 0857790 'REF LP0857789 LEFT HORIZONTAL STAB FWD SPAR LOWER FLANGE OF T CAP CRACKED AT STA258.2 11.5' LONG AT RADIUS' / REMOVED & REPLACED L/H HORZ. STAB ASSY IAW B737 AMM 27-41-11-000-801 & AMM 27-41-11-400-801. HORIZONTAL STAB TRAVEL CHECK IS GOOD IAW B737 AMM 27-41-11-400-801. ALL NECESSARY OPS CHECKS ARE GOOD IAW B737 AMM 27-41-11-400-801; AMM 27-31-00-700-815 & AMM 33-49-00-960-802. NO ELEVATOR POWER-OFF TEST REQ PER AMM 27-31-00-710-803 STEP 26.A(3). RECEIVED SERVICABLE HORZ. L/E. REF. NRC N206210 FOR INSTALLATION. (POS:L/H STAB

Part: SLIDE — WORN (R2 DOOR) · airframe 36,945 hrs · 22,133 cycles

R2 DOOR EMERGENCY SLIDE GIRT BAR SKIRT WORN. R&R SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 36,585 hrs · 21,899 cycles

L2 DOOR EVAC SLIDE OUT OF POSITION. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 36,347 hrs · 21,751 cycles

L2 DOOR EMERGENCY SLIDE PRESSURE GAUGE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 35,262 hrs · 21,064 cycles

L2 DOOR SLIDE GAUGE OUT OF ADJUST. ADJUSTED SLIDE PER AMM AND MT.

Part: BATTERY — FAILED (CABIN) · airframe 34,740 hrs · 20,729 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 34,740 hrs · 20,729 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 34,740 hrs · 20,729 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 34,740 hrs · 20,729 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 34,740 hrs · 20,729 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 34,740 hrs · 20,729 cycles

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

Part: SLIDE — LOOSE (R1 DOOR) · airframe 32,471 hrs · 19,289 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER AMM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 32,385 hrs · 19,232 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 32,385 hrs · 19,232 cycles

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

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 32,332 hrs · 19,202 cycles

CABIN FLOOR BREAK ASSY. PANEL @ APPROX. STA. 540 FROM BL 0 TO LBL 24.75 IS BROKEN / REMOVED AND REPLACED CABIN FLOOR BREAK ASSY. PANEL @ APPROX. STA. 540 FROM BL 0 TO LBL 24.75 PER SRM 51-40-02.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 32,332 hrs · 19,202 cycles

RUDDER COUNTER BALANCE WEIGHT SHOWS SIGNS OF CORROSION. / REMOVED AND REPLACED RUDDER BALANCE ARM WEIGHT PER CMM 55-40-09. SEE SUBTASKS AND WIPS FOR INDIVIDUAL SIGNOFFS

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 32,332 hrs · 19,202 cycles

CABIN FLOOR PANEL 232SF HAS PEELING FIBERS AND EDGE DAMAGE / FLOOR PANEL 232SF TO BE REPLACED WITH NEW FLOOR PANEL ASSY. AND TO BE INSTALLED ON ROUTINE JPANEL-231-CLOSE

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 32,332 hrs · 19,202 cycles

CABIN FLOOR PANEL 231ZF HAS MULTIPLE LAYERS OF FIBER MISSING/PEELING OVER A LARGE AREA / FLOOR PANEL 231ZF TO BE REPLACED WITH NEW FLOOR PANEL ASSY. AND TO BE INSTALLED ON ROUTINE JPANEL-231-CLOSE

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 32,332 hrs · 19,202 cycles

CABIN FLOOR PANEL 241DF HAS MULTIPLE LAYERS OF FIBER MISSING/PEELING OVER A LARGE AREA / FLOOR PANEL 241DF TO BE REPLACED WITH NEW FLOOR PANEL ASSY. AND TO BE INSTALLED ON ROUTINE JPANEL-231-CLOSE

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 32,332 hrs · 19,202 cycles

CABIN FLOOR PANEL 231XF HAS SEVERAL LAYERS OF FIBER MISSING/PEELING OVER A LARGE AREA / INSTALLED NEW PANEL ON ROUTINE CARD JPANEL-231-CLOSE

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 32,332 hrs · 19,202 cycles

CABIN FLOOR PANEL 241AF HAS MULTIPLE LAYERS OF FIBER MISSING/PEELING OVER A LARGE AREA / FLOOR PANEL 241AF TO BE REPLACED WITH NEW FLOOR PANEL ASSY. AND TO BE INSTALLED ON ROUTINE JPANEL-231-CLOSE

Part: PRESSURE WEB — CRACKED · airframe 32,332 hrs · 19,202 cycles

CABIN STA 663 VERTICAL PRESSURE WEB CRACKED AT RBL 35 AT WL 194 APPROX. 1 INCH LONG VERIFIED WITH HFEC / FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 32,040 hrs · 19,015 cycles

L1 DOOR SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED THE SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 30,856 hrs · 18,301 cycles

L2 DOOR EMERGENCY ESCAPE SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: BOTTLE — LOW PRESSURE (R2 DOOR SLIDE) · airframe 30,608 hrs · 18,152 cycles

R2 DOOR SLIDE PRESSURE GAUGE ON THE LOW SIDE. R & R THE SLIDE IAW MT.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 29,497 hrs · 17,504 cycles

FORWARD CABIN LT PHOTO LUMINESCENT LIGHT INOP BETWEEN BS 370 TO BS 380. R&R STRIP IAW AMM.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 29,497 hrs · 17,504 cycles

FORWARD CABIN RT PHOTO LUMINESCENT LIGHT INOP AT BS 360. R&R LIGHT IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 29,497 hrs · 17,504 cycles

FORWARD GALLEY R/H LOWER EMERGENCY EXIT LENS COVER BROKEN. R&R COVER IAW AMM.

Part: HOOK — LOOSE (L1 DOOR SLIDE) · airframe 28,386 hrs · 16,821 cycles

L1 DOOR EMERGENCY EVACUATION SLIDE CONTAINER GIRT BAR HOOK LOOSE. SECURED THE HOOK IAW SRM.

Part: HOOK — LOOSE (R1 DOOR SLIDE) · airframe 28,386 hrs · 16,821 cycles

R1 DOOR EMERGENCY EVACUATION SLIDE CONTAINER GIRT BAR HOOK LOOSE. SECURED THE HOOK IAW SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 27,088 hrs · 16,029 cycles

R2 FLIGHT DECK WINDOW, HEATING ELEMENT ARCED. R & R R2 WINDOW IAW MT.

Part: SLIDING WINDOW — ARCED (COCKPIT) · airframe 26,591 hrs · 15,757 cycles

CAPTAIN'S SLIDING WINDOW ARCED. R & R WINDOW IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 26,105 hrs · 15,465 cycles

G4 GALLEY EMER EXIT LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 26,105 hrs · 15,465 cycles

AFT LAVATORY EMER LIGHT BASE OTBD OF ATTENDANT SEAT CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 26,105 hrs · 15,465 cycles

LONGITUDINAL FLOORBEAM FWD SEAT TRACK FLANGE, CRACKED AT BS 727B, LBL 45.5, INBD AFT & OTBD AFT HOLES NR 8 & 10. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 26,105 hrs · 15,465 cycles

LONGITUDINAL FLOORBEAM FWD SEAT TRACK FLANGE, CRACKED AT BS 727B, LBL 24.75, INBD AFT HOLE NR 8. REPAIRED FLANGE IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 26,105 hrs · 15,465 cycles

RIGHT CREASE BEAM CORRODED, BETWEEN BS 952 - 990. R & R CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (R1 DOOR) · airframe 26,105 hrs · 15,465 cycles

R1 DOOR CREASE BEAM INNER CHORD, CORRODED BETWEEN BS 291 - 344, STRINGER 17R. REPAIRED CHORD IAW SRM DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 26,105 hrs · 15,465 cycles

LONGITUDINAL FLOORBEAM FWD SEAT TRACK FLANGE, CRACKED AT BS 727B, RBL 45.5, AFT OTBD & BOTH INBD. REPAIRED FLANGE IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,105 hrs · 15,465 cycles

FORWARD CARGO COMPARTMENT, Z ANGLE WEB CORRODED, BETWEEN BS 493 - 497, RBL 25. R & R WEB IAW SRM.

Part: FITTING — DAMAGED (L1 DOOR) · airframe 26,105 hrs · 15,465 cycles

L1 DOOR EMER EGRESS ESCAPE SLIDE GIRT BAR FITTING DAMAGED. R & R FITTING IAW AMM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 26,105 hrs · 15,465 cycles

MAIN WW SPAR VERTICAL PRESS WEB, CRACKED AT BS 663, BETWEEN LBL 40 - 43. REPAIRED WEB IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,709 hrs · 15,242 cycles

FORWARD UPPER EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW CMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 23,737 hrs · 14,103 cycles

FORWARD ENTRY EMER EXIT SIGN MISSING. R & R LENS ASSEMBLY IAW MM.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 22,867 hrs · 13,586 cycles

CENTER AISLE OVERWING CABIN EXIT SIGN LIGHT ASSEMBLY LOOSE FROM MOUNT. R & R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,580 hrs · 12,858 cycles

LEFT OVERHEAD BIN EMER LIGHT INOPERABLE AT ROW 12. RELAMPED LIGHT IAW SIP.

Part: FITTING — LOOSE (R1 DOOR) · airframe 21,539 hrs · 12,834 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR CLIP LOOSE. SECURED CLIP IAW SIP.

Part: LIGHT — BROKEN (CABIN) · airframe 20,309 hrs · 12,130 cycles

FORWARD ENTRY EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 19,789 hrs · 11,830 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 175.5 RIB 10 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 19,789 hrs · 11,830 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 129.5 RIB 34 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 19,789 hrs · 11,830 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 120.30 RIB 10 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 19,789 hrs · 11,830 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 89 REAR SPAR. REPAIRED SKIN IAW SRM.

Part: FLAP — DAMAGED (RT WING) · airframe 19,789 hrs · 11,830 cycles

RT WING OTBD AFT FLAP DAMAGED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 19,789 hrs · 11,830 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 92.7 RIB 10 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 18,045 hrs · 10,786 cycles

FORWARD EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS IAW SIP.

Part: LENS — CRACKED (CABIN) · airframe 15,151 hrs · 9,105 cycles

CABIN FLOOR EEPLS LENS CRACKED. REMOVED AND REPLACED LENS PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 15,151 hrs · 9,105 cycles

CABIN EMERGENCY EXIT SIGN LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERIES PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 14,946 hrs · 8,980 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,427 hrs · 8,043 cycles

FWD ENTRY EEPLS INOP. RELAMPED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 13,418 hrs · 8,037 cycles

LT EMERGENCY FLOOR LIGHT LENS MISSING AT ROW 4. REMOVED AND REPLACED LENS PER MM.

Part: BLADE — VIBRATION (NR 1 ENGINE) · airframe 12,883 hrs · 7,736 cycles

DIVERSION - DURING CLIMBOUT PASSING FL 380, NR 1 ENG VIBRATION WENT 4.0 WITH VIBRATION FELT. PERFORMED QRH ITEMS, VIBRATION STABILIZED AT 2.6 IN CRUISE. AGAIN SLIGHT VIBRATION FELT. REMOVED AND REPLACED BLADES PER MT.

Part: COVER — CRACKED (CABIN) · airframe 12,797 hrs · 7,684 cycles

LT EEPLS COVER CRACKED AT ROW 23. REMOVED AND REPLACED COVER PER AMM.

Part: COVER — CRACKED (CABIN) · airframe 12,797 hrs · 7,684 cycles

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

Part: LENS — CRACKED (CABIN) · airframe 11,690 hrs · 7,050 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS LENS CRACKED AT ROW 11. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 11,690 hrs · 7,050 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 11,273 hrs · 6,806 cycles

R1 DOOR EMERGENCY EXIT LIGHT LEN LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 9,043 hrs · 5,504 cycles

DURING SCHEDULED MV1 CHECK, FOUND OVERHEAD MID CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LENS — BROKEN (CABIN) · airframe 9,028 hrs · 5,496 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 8,775 hrs · 5,340 cycles

MID CABIN OVERHEAD EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: COVER — MISSING (CABIN) · airframe 8,259 hrs · 5,037 cycles

EEPLS COVER MISSING AT ROW 22. INSTALLED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 7,814 hrs · 4,757 cycles

R2 DOOR EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CAP — MISSING (CABIN) · airframe 4,996 hrs · 3,024 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS END CAP MISSING AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 4,758 hrs · 2,879 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 4,630 hrs · 2,807 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS BASE BROKEN. REMOVED AND REPLACED LAMP PER MM.

Part: COVER — MISSING (CABIN) · airframe 4,309 hrs · 2,606 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT LENS COVER MISSING AT ROW 1. INSTALLED COVER PER MM.

Part: CAP — BROKEN (CABIN) · airframe 4,309 hrs · 2,606 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 3,286 hrs · 1,964 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 2,912 hrs · 1,742 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 2,738 hrs · 1,645 cycles

L1 DOOR SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 1,063 hrs · 653 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. R&R LIGHT BULB PER MM.