N7838A

Part: BATTERY PACK — BURNED (ZN 200 FUS TOP) · airframe 64,028 hrs · 39,504 cycles

R/H FWD EMERGENCY LIGHT BATTERY CHARGER SMOKING<[01] R+R?D R/H FWD EMERGENCY LIGHT BATTERY AND CHARGER IAW MM 33-51-06

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,299 hrs · 39,008 cycles

EMERGENCY AISLE LIGHT BETWEEN ROW 18 AND 19; FO SIDE INOP<[01] RELAMPED AISLE LIGHT @18R PER AMM 33-51-03 OPS CHECK GOOD

Part: POWER SUPPLY — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,164 hrs · 38,902 cycles

3 AFT EMERGENCY LIGHTS OUT<[01] R&R POWER SUPPLY REF AMM 33-51-06 OPS CHECK GOOD NO OTHER DEFECTS NOTED AT THIS TIME

Part: POWER SUPPLY — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,108 hrs · 38,864 cycles

OVER-DOOR EXIT SIGN; EMERGENCY LIGHTS INOP<[01] REPLACED M1672 CHARGER POWER SUPPLY IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 33-51-06; OPS CHECKED GOOD.

Part: LATCH — LOOSE (ZN 800 DOOR) · airframe 62,404 hrs · 38,416 cycles

FWD SERVICE GIRT BAR LATCH LOOSE<[01] ADJUSTED FS DOOR (R-1) GIRT BAR LATCH PER SIP.

Part: NONE — BROKEN (L/H DOOR) · airframe 61,393 hrs · 37,722 cycles

F.O. ASSIST HANDLE BROKE ON LEFT SIDE / [01] R&R F.O ASSIST HANDLE PER SIP

Part: NONE — CRACKED (CABIN FLOOR) · airframe 61,378 hrs · 37,713 cycles

PASSENGER CABIN: FORWARD SERVICE DOOR (R 1). AFT SLIDE BRACKET ISOLATOR CRACKED. / [01] REMOVED AND REPLACED ISOLATOR ON FWD SERVICE DOOR PER SRM 51-40-02;[02] C/W INSPECTION PER SRM 51-40-02.

Part: FLEX LINE — LEAKING (AFT CARGO) · airframe 60,884 hrs · 37,386 cycles

DURING DESCENT PASSING FL 280 THE CABIN ALT WARNING HORN WENT OFF. THE CABIN ALT WAS 14;000. WE INITIATED A RAPID DESCENT. EMER. DECLARED & LANDING WAS UNEVENTFUL INTO OAK. / [01] PERFORMED EXCESSIVE CABIN PRESSURE LEAKAGE INSPECTION REF AMM 05-51-91. REF L/P 2335179 FOR REPLACEMENT OF VACUUM WASTE BLOWER FLEXIBLE LINE AND R/H PACK WATER SEPARATOR BAND CLAMP. C/W MT 721-00-01. OK FOR SERVICE.

Part: PACKING — MISSING (R/H CABIN) · airframe 60,884 hrs · 37,386 cycles

DURING DESCENT PASSING FL 280 THE CABIN ALT WARNING HORN WENT OFF. THE CABIN ALT WAS 14;000. WE INITIATED A RAPID DESCENT. EMER. DECLARED & LANDING WAS UNEVENTFUL INTO OAK. / [01] PERFORMED EXCESSIVE CABIN PRESSURE LEAKAGE INSPECTION REF AMM 05-51-91. REF L/P 2335179 FOR REPLACEMENT OF VACUUM WASTE BLOWER FLEXIBLE LINE AND R/H PACK WATER SEPARATOR BAND CLAMP. C/W MT 721-00-01. OK FOR SERVICE.

Part: FLEX LINE — TORN (R/H CABIN) · airframe 60,884 hrs · 37,386 cycles

DURING DESCENT PASSING FL 280 THE CABIN ALT WARNING HORN WENT OFF. THE CABIN ALT WAS 14;000. WE INITIATED A RAPID DESCENT. EMER. DECLARED & LANDING WAS UNEVENTFUL INTO OAK. / [01] PERFORMED EXCESSIVE CABIN PRESSURE LEAKAGE INSPECTION REF AMM 05-51-91. REF L/P 2335179 FOR REPLACEMENT OF VACUUM WASTE BLOWER FLEXIBLE LINE AND R/H PACK WATER SEPARATOR BAND CLAMP. C/W MT 721-00-01. OK FOR SERVICE.

Part: WARNING BELL — ACTIVATED (WHEEL WELL) · airframe 59,766 hrs · 36,629 cycles

WHEEL WELL FIRE LIGHT & BELL CAME ON DURING CRUIZE AT FL340 / [01] R&R M270 WHEEL WELL SENSOR ELEMENT PER MM 26-18-02

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 59,491 hrs · 36,468 cycles

CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2022-58310 / [01] REPAIRED BY WELDS AFT CORNER SCUFF PLATE OF FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1; REPAIR 1 PARAGRAPH 4.B. STEPS ( 2 ) TO ( 7 ) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPAIRED BY WELDS AFT CORNER SCUFF PLATE OF FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1; REPAIR 1 PARAGRAPH 4.B. STEPS ( 2 ) TO ( 7 ) AND BAC 5975.

Part: LIGHT — MISSING · airframe 59,491 hrs · 36,468 cycles

MISSING STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 LT SIDE AT PASSENGER CABIN (10 EA) 2022-58157 / [01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 LT SIDE AT PASSENGER CABIN (10 EA) IAW SOPM-20-50-12 AND DWG 33500007 REV.2;[02] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 LT SIDE AT PASSENGER CABIN (10 EA) IAW SOPM-20-50-12 AND DWG 33500007 REV.2

Part: LIGHT — MISSING (CABIN FLOOR) · airframe 59,491 hrs · 36,468 cycles

MISSING STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 LT SIDE AT PASSENGER CABIN (10 EA) 2022-58159 / [01] INSTALLED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 LT SIDE AT PASSENGER CABIN (10 EA) IAW SOPM-20-50-12 AND DWG 33500007 REV.2;[02] INSTALLED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 LT SIDE AT PASSENGER CABIN (10 EA) IAW SOPM-20-50-12 AND DWG 33500007 REV.2

Part: LIGHT — MISSING · airframe 59,491 hrs · 36,468 cycles

MISSING STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 RT SIDE AT PASSENGER CABIN (10 EA) 2022-58154 / [01] INSTALLED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 RT SIDE AT PASSENGER CABIN (10 EA) IAW SOPM-20-50-12 AND DWG 33500007 REV.2;[02] INSTALLED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 RT SIDE AT PASSENGER CABIN (10 EA) IAW SOPM-20-50-12 AND DWG 33500007 REV.2

Part: LIGHT — MISSING · airframe 59,491 hrs · 36,468 cycles

MISSING STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 RT SIDE AT PASSENGER CABIN (10 EA) 2022-58155 / [01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 RT SIDE AT PASSENGER CABIN (10 EA) IAW SOPM-20-50-12 AND DWG 33500007 REV.2;[02] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 RT SIDE AT PASSENGER CABIN (10 EA) IAW SOPM-20-50-12 AND DWG 33500007 REV.2

Part: STRINGER — CRACKED · airframe 59,491 hrs · 36,468 cycles

CRACK STRINGER 26L LOCATED BS.540 AT FWD CARGO COMPARTMENT 2022-58135 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 03-FEB-22; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 03-FEB-22.;[03] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022236 ; DUE DATE: 02-JUN-22;[04] TOOL USED: CALIPER; PN: 700-113-10; SN: 0023246; DUE DATE: 23-SEP-22.;[05] PERFORMED REPAIR ON STRINGER 26L BTW BS 500D TO BS.540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1; DRAWING # 143A3230 REV. A AND DRAWING #143A0060 REV. -.;[06] PERFORMED REPAIR ON STRINGER 26L BTW BS 500D TO BS.540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1; DRAWING # 143A3230 REV. A AND DRAWING #143A0060 REV. -.<BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: STRINGER — CRACKED (FWD CARGO BAY) · airframe 59,491 hrs · 36,468 cycles

CRACK STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT 2022-58140 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 03-FEB-22.;[03] TOOL USED: CALIPER; PN: 700-113-10; SN: 0023246; DUE DATE: 23-SEP-22.;[04] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 500D; S/N: N500X12101V022235; DUE DATE: 0-JUN-22.;[05] PERFORMED PERMANENT REPAIR ON STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 SEE INDIVIDUAL SIGN-OFF BELOW;[06] PERFORMED PERMANENT REPAIR ON STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 SEE INDIVIDUAL SIGN-OFFS BELOW RII

Part: STRINGER — CRACKED (FWD CARGO BAY) · airframe 59,491 hrs · 36,468 cycles

CRACK STRINGER 25R LOCATED BS. 540 AT FWD CARGO COMPARTMENT 2022-58138 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 03-FEB-22.;[03] TOOL USED: CALIPER; PN: 500-464; SN: B17030925; DUE DATE: 23-SEP- 22.;[04] TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 210138003 DUE DATE 05-MAR-22.;[05] TOOL USED: CALIPER; PN: 500-197-30; SN: A21043164; DUE DATE: 01-SEP-22.;[06] CALIPER; PN: 500-464; SN: B17030925; DUE DATE: 23-SEP-22.;[07] TOOL USED PRECISION BALANCE P/N PPC-200W S/N 38246 DUE DATE 28-JUL-22.;[08] PERFORMED REPAIR ON STRINGER 25R BTW BS 500C TO BS.540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.;[09] CORRECTED STEP 8.<BR>PERFORMED REPAIR ON STRINGER 25R BTW BS 500C TO BS.540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[10] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: STRINGER — CRACKED (FWD CARGO BAY) · airframe 59,491 hrs · 36,468 cycles

CRACK STRINGER 27R LOCATED BS. 540 AT FWD CARGO COMPARTMENT 2022-58137 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] CORRECT STEP: NOMINAL THICKNESS IS: 0.056? PER NDT MANUAL 51-00-00 PART 4; PROCEDURE 3.;[03] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[04] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 03-FEB-22.;[05] TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 210138003 DUE DATE 05-MAR-22.;[06] PERFORMED PERMANENT REPAIR ON STRINGER 27R LOCATED BS. 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 SEE INDIVIDUAL SIGN-OFF BELOW;[07] PERFORMED PERMANENT REPAIR ON STRINGER 27R LOCATED BS. 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 SEE INDIVIDUAL SIGN-OFF BELOW AS RII

Part: STRINGER — CRACKED · airframe 59,491 hrs · 36,468 cycles

CRACK STRINGER 27L LOCATED BS. 540 AT FWD CARGO COMPARTMENT 2022-58136 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 03-FEB-22; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 03-FEB-22.;[03] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 200048001; CAL DUE DATE: 24-FEB-22;[04] CALIPER; PN: DIGITAL 150; SN: AE-412610; DUE DATE: 21-MAY-22.;[05] PERFORMED PERMANENT REPAIR ON STRINGER 27L LOCATED BS. 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 SEE INDIVIDUAL SIGN-OFF BELOW;[06] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 59,491 hrs · 36,468 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION ; 2022-58102 / REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02 PART USED: 143A5240-35 B/N: SW2022000185; [02] CORRECTED STEP 1 : REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02 PART USED: 143A5240-35 B/N: SW2022000185 SEE INDIVIDUAL SIGN OFF BELOW; [03] REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 59,491 hrs · 36,468 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION 2022-58102 / [01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02 PART USED: 143A5240-35 B/N: SW2022000185;[02] CORRECTED STEP 1 : REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02 PART USED: 143A5240-35 B/N: SW2022000185 SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02 PART USED: 143A5240-35<

Part: STIFFENER — CRACKED · airframe 59,491 hrs · 36,468 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED BETWEEN BL0 AND RBL24.88 BS540 CENTER SECTION ; 2022-58101 / [01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BETWEEN BL0 AND RBL24.88 BS540 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02; PART USED: P/N: 143A5240-36 B/N: SW2021002969; [02] CORRECTED STEP 1 : REPLACED STIFFENER FLOOR STRUCTURE LOCATED BETWEEN BL0 AND RBL24.88 BS540 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02; PART USED: P/N: 143A5240-36 B/N: SW2021002969 SEE INDIVIDUAL SIGNS OFF BELOW; [03] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BETWEEN BL0 AND RBL24.88 BS540 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02; PART USED: P/N: 143A5240-36<BR>RII ACCOMPLISHED <BR> SEE INDIVIDUAL SIGNS OFF BELOW

Part: BULKHEAD — CRACKED · airframe 59,491 hrs · 36,468 cycles

CRACK BULKHEAD PANEL 141PW AT AFT CARGO COMPARTMENT 2022-58107 / [01] EVALUATED CRACK BULKHEAD PANEL 141PW AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 AMM 25-52-00-200-806 PARAGRAPH 6.D.(6). DAMAGE SIZE: L= 1.0?; W= 0.25?. AND REPAIRED AS PER B737-700 AMM 25-52-01-300-804 PARAGRAPH 3.F. TOOL USED= CALIPER P/N: 500-197-30; S/N: A21042057; DUE DATE: 11-AUG-22;[02] EVALUATED CRACK BULKHEAD PANEL 141PW AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 AMM 25-52-00-200-806 PARAGRAPH 6.D.(6). DAMAGE SIZE: L= 1.0?; W= 0.25?. AND REPAIRED AS PER B737-700 AMM 25-52-01-300-804 PARAGRAPH 3.F. TOOL USED= CALIPER P/N: 500-197-30; S/N: A21042057; DUE DATE: 11-AUG-22

Part: BULKHEAD — CRACKED (AFT CARGO BAY) · airframe 59,491 hrs · 36,468 cycles

CRACK BULKHEAD PANEL 141UW AT AFT CARGO COMPARTMENT 2022-58105 / [01] EVALUATED CRACK BULKHEAD PANEL 141UW AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 AMM 25-52-00-200-806 PARAGRAPH 6.D.(6). DAMAGE SIZE: L= 1.5?; W= 0.3?. AND REPAIRED AS PER B737-700 AMM 25-52-01-300-804 PARAGRAPH 3.F. TOOL USED= CALIPER P/N: 500-197-30; S/N: A21042057; DUE DATE: 11-AUG-22;[02] EVALUATED CRACK BULKHEAD PANEL 141UW AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 AMM 25-52-00-200-806 PARAGRAPH 6.D.(6). DAMAGE SIZE: L= 1.5?; W= 0.3?. AND REPAIRED AS PER B737-700 AMM 25-52-01-300-804 PARAGRAPH 3.F. TOOL USED= CALIPER P/N: 500-197-30; S/N: A21042057; DUE DATE: 11-AUG-22

Part: PANEL — CRACKED (FUSELAGE) · airframe 59,491 hrs · 36,468 cycles

CRACK ACCESS PANEL 194E BODY FAIRING AROUND HOLES AT LOWER FUSELAGE 2022-58095 / [01] TOOL USED CALIPER P/N 500-464 S/N 15331932 DUE DATE 26/OCT/22.;[02] TOOL USED HOTBONDER P/N HCS9200B S/N 18175478 DUE DATE 05-AUG-22;[03] TOOL USED SCALE P/N: CL5000 S/N: AE-37099 DUE DATE: 16-AUG-22.;[04] TOOL USED: HOT BONDER P/N HCS9200B S/N 15102320 DUE DATE 16-JAN-23.;[05] REPAIRED ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 REPAIR 8. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] TASK COMPLETED.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 59,491 hrs · 36,468 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED BETWEEN BL0 AND RBL24.88 BS540 CENTER SECTION 2022-58101 / [01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BETWEEN BL0 AND RBL24.88 BS540 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02; PART USED: P/N: 143A5240-36 B/N: SW2021002969;[02] CORRECTED STEP 1 : REPLACED STIFFENER FLOOR STRUCTURE LOCATED BETWEEN BL0 AND RBL24.88 BS540 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02; PART USED: P/N: 143A5240-36 B/N: SW2021002969 SEE INDIVIDUAL SIGNS OFF BELOW;[03] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BETWEEN BL0 AND RBL24.88 BS540 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02; PART USED: P/N: 143A5240-36<BR>RII ACCOMPLISHED <BR> SEE INDIVIDUAL SIGNS OFF BELOW

Part: ANGLE — CRACKED (CABIN FLOOR) · airframe 59,491 hrs · 36,468 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 693 AT BL 0 AT PASSENGER CABIN 2022-58012 / [01] REPLACED ANGLE AND FASTENERS LOCATED ON BS 693 AT BL 0 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 273A9110 REV. A SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE AND FASTENERS LOCATED ON BS 693 AT BL 0 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 273A9110 REV. A SEE INDIVIDUAL SIGN OFF BELOW<BR>RII ACCOMPLISHED

Part: ANGLE — CRACKED (CABIN FLOOR) · airframe 59,491 hrs · 36,468 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 690 AT BL 0 AT PASSENGER CABIN 2022-58007. REPLACED ANGLE LOC. ON FLOOR STRUCTURE BS 690 AT BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 REV. A;[03] CORRECTED STEP 2: REPLACED ANGLE LOC. ON FLOOR STRUCTURE BS 690 AT BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 REV. A. SEE INDIVIDUAL SIGN OFF BELOW;[04] CORRECTED STEP 2 <BR>REPLACED ANGLE LOC. ON FLOOR STRUCTURE BS 690 AT BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 REV. A.

Part: SUPPORT BRACKET — CRACKED (VERTICAL STAB) · airframe 59,491 hrs · 36,468 cycles

CRACK LEADING EDGE SUPPORT BRACKET LOCATED AT BS 1016 BETWEEN S-2R AND S-2L AT VERTICAL STABILIZER 2022-58053 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.;[02] REPLACED SUPPORT BRACKET (SPRING) AND FASTENERS LOCATED AT BS 1016 BETWEEN S-2R AND S-2L AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ; B737-700 SRM 51-40-02 AND DRAWING #176A3101 REV.-;[03] REPLACED SUPPORT BRACKET (SPRING) AND FASTENERS LOCATED AT BS 1016 BETWEEN S-2R AND S-2L AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ; B737-700 SRM 51-40-02 AND DRAWING #176A3101 REV.-

Part: SUPPORT BRACKET — CRACKED (VERTICAL STAB) · airframe 59,491 hrs · 36,468 cycles

CRACK LEADING EDGE SUPPORT BRACKET LOCATED AT BS 1016 BETWEEN S-2R AND S-2L AT VERTICAL STABILIZER ; 2022-58053 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.; [02] REPLACED SUPPORT BRACKET (SPRING) AND FASTENERS LOCATED AT BS 1016 BETWEEN S-2R AND S-2L AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ; B737-700 SRM 51-40-02 AND DRAWING #176A3101 REV.-; [03] REPLACED SUPPORT BRACKET (SPRING) AND FASTENERS LOCATED AT BS 1016 BETWEEN S-2R AND S-2L AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ; B737-700 SRM 51-40-02 AND DRAWING #176A3101 REV.-

Part: DOOR — CRACKED (L/H MLG) · airframe 59,491 hrs · 36,468 cycles

CRACK CENTER DOOR ON LT MAIN LANDING GEAR 2022-57916 / [01] TOOL USED DIGITAL CALIPER P/N: 700-113-10 S/N:0016732 DUE DATE:01-APR -22;[02] TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 60009161631 DUE DATE 03-DEC-22.;[03] TOOL USED: DIGITAL CALIPER: P/N: 500-193-30; S/N: 0000291; DUE DATE: 16-SEP-22.;[04] TOOL USED: DIGITAL CALIPER: P/N: 500-193-30; S/N: 0000291; DUE DATE: 16-SEP-22.;[05] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC600D; S/N: 60007161486; CAL DUE DATE: 06-DEC-22;[06] PERFORMED PERMANENT REPAIR ON CENTER DOOR ON LT MAIN LANDING GEAR IAW B737-700 SRM 52-80-02-2R-3 REPAIR 3 FIGURE 202;[07] PERFORMED PERMANENT REPAIR ON CENTER DOOR ON LT MAIN LANDING GEAR IAW B737-700 SRM 52-80-02-2R-3 REPAIR 3 FIGURE 202 SEE INDIVIDUAL SIGN-OFF BELOW;[08] PERFORMED PERMANENT REPAIR ON CENTER DOOR ON LT MAIN LANDING GEAR IAW B737-700 SRM 52-80-02-2R-3 REPAIR 3 FIGURE 202 SEE INDIVIDUAL SIGN-OFF BELOW

Part: SEAL PLATE — CRACKED (LH HOR STAB) · airframe 59,491 hrs · 36,468 cycles

CRACK SEAL - PLATE ACCESS PANEL 333AT AT LT HORIZONTAL STAB. REPLACED THE SEAL PLATE ACCESS PANEL 333AT IAW SRM 51-10-02 ITEM 9 AND 51-40-02.

Part: SEAL PLATE — CRACKED (RH HOR STAB) · airframe 59,491 hrs · 36,468 cycles

CRACK SEAL - PLATE ACCESS PANEL 343AT AT RT HORIZONTAL STAB. REPLACED THE SEAL PLATE ACCESS PANEL 343AT IAW SRM 51-10-02 ITEM 9 AND 51-40-02.

Part: BULKHEAD — CRACKED (AFT CARGO BAY) · airframe 59,491 hrs · 36,468 cycles

CRACK BULKHEAD PANEL 142NWB AFT CARGO COMPARTMENT 2022-57806 / [01] EVALUATED BULKHEAD PANEL 142NWB AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR IAW B737-700 AMM 25-52-00-200-806 PAR. 6.D (3) DAMAGE SIZE L= 3? W= 0.08? AND REPAIRED PANEL IAW AMM 25-52-01-300-805 PAR.4.F TOOL USED CALIPER P/N 500-196-30 S/N A20226522 DUE DATE 11-AUG-22.;[02] EVALUATED BULKHEAD PANEL 142NWB AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR IAW B737-700 AMM 25-52-00-200-806 PAR. 6.D (3) DAMAGE SIZE L= 3? W= 0.08? AND REPAIRED PANEL IAW AMM 25-52-01-300-805 PAR.4.F TOOL USED CALIPER P/N 500-196-30 S/N A20226522 DUE DATE 11-AUG-22.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,798 hrs · 35,475 cycles

OVERWING ESCAPE ILLUMINATION LIGHT BS 757 INOPERATIVE. R & R THE BATTERY PACK CHARGER ASSY IAW AMM 33-51-06-960-805. FAILED INSTALLATION TEST. BATTERY PACK AND PERFORMED SATISFACTORY INSTALLATION TEST IAW AMM 33-51-06-960-805, PERFORMANCE SATISFACTORY IAW AMM 33-51-06-960-805.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,798 hrs · 35,475 cycles

LEFT AFT L2 EXTERIOR EMERGENCY EXIT LIGHT INOP ; / REMOVED AND REPLACED BAD BULB AS PER AMM 33-51-04-960-801.; INSPECTED

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,361 hrs · 35,193 cycles

INOP EMERGENCY LIGHT 6ABC,6DEF,9ABC,14ABC, FWD ENTRY DOOR AND FWD SERVICE DOOR AT PASSENGER CABIN. REPLACED FUSE IN EMERGENCY LIGHT PACK M1674 AND M2335 IAW AMM 33-51-06-960-804

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,361 hrs · 35,193 cycles

RT SIDE EMERGENCY EXIT DOOR EMERGENCY LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 57,361 hrs · 35,193 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB ON FRONT VERTICAL STIFFENER CRACKED AT STAB. STA. 120.30. R & R STIFFENER IAW SRM & DWG.

Part: RIB — ELONGATED (HORIZONTAL STAB) · airframe 57,361 hrs · 35,193 cycles

ELONGATED HOLE INSPAR RIB STAB STA 120.30 AT RT HORIZONTAL STABILIZER / REPAIRED RH HORIZONTAL STABILIZER RIB AT STAB STA 120.30 IAW EA N.1-755-4613 REV IR EA#55-5088-19 REV 0

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 57,361 hrs · 35,193 cycles

CORROSION STRAP LOCATED BETWEEN BS 767 TO BS 787 AND STR 25L / STR 25R AT AFT CARGO COMPARTMENT / REPLACED STRAP LOCATED BETWEEN BS 767 TO BS 787 AND STR25L 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A7500 REV C

Part: GUSSET — CRACKED (FUSELAGE) · airframe 57,361 hrs · 35,193 cycles

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

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 57,361 hrs · 35,193 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 RH SIDE AT AFT CARGO COMPARTMENT_WL 162.1 / REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS 767 RH SIDE AT AFT CARGO COMPARTMENT IAW B737- 700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG # 146A7502

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 57,361 hrs · 35,193 cycles

AFT CARGO COMPARTMENT SUPPORT ZEE CORRODED BETWEEN BS 727 TO BS 827, STR 25L. R&R SUPPORT ZEE IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 57,361 hrs · 35,193 cycles

FORWARD CARGO COMPARTMENT CRACKED GUSSET AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,361 hrs · 35,193 cycles

AFT CARGO COMPARTMENT WEB - INTERCOSTAL CRACKED BETWEEN BS 794 TO BS 847, STR 25R. R&R WEB-INTERCOSTAL IAW SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 57,361 hrs · 35,193 cycles

CORROSION STRAP LOCATED BETWEEN BS 727D TO BS 727E AND STR 25L / STR 2 5R AT AFT CARGO COMPARTMENT / REPLACED STRAP LOCATED BETWEEN BS727D TO BS727E AND STR 25L TO STRR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02 DRAWING 146A7500 REV

Part: PLATE — CORRODED (FUSELAGE) · airframe 57,361 hrs · 35,193 cycles

FORWARD CARGO COMPARTMENT CHANNEL SIDE PLATE CORRODED BETWEEN BS 492 TO BS 500A, STR 26R. R&R CHANNEL SIDE PLATE IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 57,361 hrs · 35,193 cycles

L/H OVERHEAD EMERGENCY EXIT STOWAGE BIN BULL NOSE LIGHT LENS BROKEN. / R&R LENS IAW AMM.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 57,361 hrs · 35,193 cycles

TIE CLIP CRACKED AT BS. 277, STR. 10R. / R&R TIE CLIP IAW SRM AND DWG.

Part: DOOR SILL — CORRODED · airframe 57,361 hrs · 35,193 cycles

CORROSION EXTERNAL SKIN SCUFF PLATE AREA LOCATED BETWEEN BS794.5 AND BS847 AND BETWEEN STR24R AND STR25R AT LOWER FUSELAGE / REPAIRED FUSELAGE EXTERNAL SKIN AT SCUFF PLATE AREA LOCATED BTW BS794.9 TO BS847 BTW STR 24R TO STR 25R IAW EA # 1-753-36408 REV IR AND EA # 53-0019-20 REV 0

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,361 hrs · 35,193 cycles

FRAME CRACKED AT BS 520, BETWEEN STR 11L TO STR 12L. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,361 hrs · 35,193 cycles

ANGLE CRACKED AT BS. 277, BETWEEN STR. 2L TO STR. 3L. / R&R ANGLE IAW SRM AND DWG.

Part: ACCESS PANEL — CRACKED (AFT ENTRY DOOR) · airframe 57,361 hrs · 35,193 cycles

CRACK ACCESS PANEL 834DZ AFT ENTRY DOOR AT PASSENGER CABIN / REPLACED ACCESS PANEL 834DZ AFT ENTRY DOOR AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9

Part: PANEL — CRACKED (AFT SERVICE DOOR) · airframe 57,361 hrs · 35,193 cycles

CRACK ACCESS PANEL 844DZ AFT SERVICE DOOR AT PASSENGER CABIN / REPLACED ACCESS PANEL 844DZ AFT SERVICE DOOR AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 DUE TO ALLOWABLE DAMAGE NO FOUND ON SRM DATA B737-700

Part: SUPPORT ANGLE — CRACKED (AFT SERVICE DOOR) · airframe 57,361 hrs · 35,193 cycles

CRACK ACCESS PANEL 844DZ SUPPORT ANGLE AFT SERVICE DOOR AT PASSENGER CABIN (2 EA) / NO ACTION REQUIRED DUE TO ACCESS PANEL 844DZ WAS COMPLETELY REPLACED (2E/A) IS DOCUMENTED ON LOG PAGE L158002

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 57,361 hrs · 35,193 cycles

MAIN WHEEL WELL COMPARTMENT VAPOR BARRIER WEB CRACKED AT BS. 663.5, LBL 14. REPAIRED WEB IAW SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 57,361 hrs · 35,193 cycles

AFT GALLEY AREA EMERGENCY EXIT LENS BROKEN. / R&R LENS IAW AMM.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 57,361 hrs · 35,193 cycles

CRACK BODY FAIRING GROUND AIR CONDITIONING SERVICE PLATE LOCATED BETWEEN BS520 TO BS540 AND BETWEEN STR28L TO STR28R AT LOWER FUSELAGE / REPLACED PLATE ON BODY FAIRING GROUND AIR CONDITIONING LOC. BTW B5520 TO B5540 AND BTW STR28L TO STR28R AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 57,361 hrs · 35,193 cycles

R/H HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB. STA. 120.30, 28 INCH FROM FRONT SPAR. REPAIRED RIB IAW EA.

Part: ACCESS PANEL — DELAMINATED (FUSELAGE) · airframe 57,361 hrs · 35,193 cycles

DELAMINATED BODY FAIRING ACCESS PANEL 192BL AT LOWER FUSELAGE / REPAIRED BODY FAIRING ACCESS PANEL 192BL AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED CALIPER P/N 2340A11 S/N B17119057 DUE DATE 18-DEC-19; HOT BONDER P/N HCS9200B S/N 13061394 DUE DATE 25-JAN-20; SCALE P/N CL5000 S/N AE-39089 DUE DATE 02-MAY-20; HOT BONDER P/N HCS9200B S/N 12041156 DUE DATE 17-JUL-20; SCALE P/N CL5000 S/N AE-408753 DUE DATE 15-FEB-20; HOT BONDER P/N HCS9000B-AV S/N 18164925 DUE DATE 14-MAY-20.

Part: ACCESS PANEL — DELAMINATED (R/H WING) · airframe 57,361 hrs · 35,193 cycles

DELAMINATED ACCESS PANEL 621CB LEADING EDGE RT WING / REPAIRED ACCESS PANEL 621CB LEADING EDGE RT WING ASPER B737-700 SRM 51-70-05-2R-10 REPAIR 10. TOOL USED CALIPER PN 2340A11 SN B17119057 DUE DATE 18-DEC-19; HOT BONDER PN HCS7800 SN 01154419 DUE DATE 25-JAN-20; HOT BONDER HCS9200B SN 13061394 DUE DATE 25-JUN-20; HOT BONDER SN HCS9200B SN 12041156 DUE DATE 17-JUL-20; SCALE PN CL5000 SN AE-407340 DUE DATE 03-JUL-20

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 57,361 hrs · 35,193 cycles

MAIN WHEEL WELL COMPARTMENT PRESSURE DECK WEB CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN RBL 30 TO RBL 60. / REPAIRED WEB IAW SRM.

Part: ACCESS PANEL — ELONGATED (R/H WING) · airframe 57,361 hrs · 35,193 cycles

ELONGATED HOLE ACCESS PANEL 621DB LEADING EDGE AT RT WING / REPAIRED ACCESS PANEL 621DB LEADING EDGE AT RT WING ASPER B737-700 SRM 51-70-04-2R-9 REPAIR 9. TOOL USED CALIPER PN 2340A11 SB B17119057 DUE DATE 18-DEC-19; HOT BONDER PN HCS9200B SN 13061394 DUE DATE 25-JAN-20; SCALE PN CL5000 SN AE-39089 DUE DATE 02-MAY-20; SCALE PN CL5000 SN AE-407340 DUE DATE 03-JUL-20

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 57,149 hrs · 35,056 cycles

R/H AND L/H OVERWING EMERGENCY EXIT LOWER INTERNAL HANDLE HOUSING NOT SECURED. / SECURED HANDLE IAW SIP.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 57,149 hrs · 35,056 cycles

FORWARD ENTRY & FORWARD SERVICE LOWER EMERGENCY EXIT LIGHT LENS MISSING DIRECTIONAL ARROW. / INSTALLLED DIRECTIONAL ARROW ON FORWARD ENTRY & SERVICE DOORS.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 57,148 hrs · 35,056 cycles

FASTNER HOLES ELONGATED AT #1;#2;#3;#4;#5;#6;#7;#10 #13;#22 ON 193B PANEL / REMOVED AND REPLACED NUTPLATES PER SRM 51-40-02

Part: BUSHING — MISSING (L2 DOOR GIRT BAR) · airframe 56,871 hrs · 34,862 cycles

L2 DOOR SLIDE GIRT BAR RETAINING BUSHING MISSING. INSTALLED BUSHING PER AMM & SIP.

Part: FASTENER — LOOSE (EVAC SLIDE) · airframe 56,619 hrs · 34,687 cycles

L2 DOOR SLIDE HAD A LOOSE FASTENER. SECURED FASTENER PER SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,078 hrs · 34,337 cycles

EMERGENCY BATTERY POWER SUPPLY M1672 FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.

Part: FLOOR PANEL — CRACKED (AFT CARGO COMPT) · airframe 55,628 hrs · 34,063 cycles

TWO CRACKS WERE FOUND WITH TWO INCHES OF EACH OTHER ON FLOOR PANEL 120BF IN THE AFT CARGO PER MM 25-52-00-200-803. ONE CRACK IS 12' LONG AND THE OTHER IS 15.8' MOD / REMOVED AND REPLACED CARGO FLOOR PANEL PER B737 AMM 25-52-10

Part: COVER — LOOSE (L2 DOOR) · airframe 54,857 hrs · 33,587 cycles

L2 DOOR SLIDE COVER LOOSE. SECURED COVER IAW AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 54,001 hrs · 33,043 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SUPPORT FITTING — CRACKED (L2 DOOR) · airframe 53,908 hrs · 32,981 cycles

L2 DOOR LOWER LINER SUPPORT ATTACH FITTINGS BOTH CRACKED. R&R FITTINGS PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 53,825 hrs · 32,936 cycles

AFT GALLEY OVERHEAD EXIT SIGN BROKEN. R&R LIGHT ASSEMBLY IAW AMM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,836 hrs · 32,327 cycles

THERE IS DAMAGE TO STRINGER 182 WHICK INCLUDES A DENT. DEFORMATION AND A CRACK AT AREA BETWEEN STA 879-881. / CUT AND REMOVED BAD SECTION OF STRINGER BETWEEN STA 879-881 S18L AND REPLACED AND INSTALLED NEW STRINGER SPLICE AT STA 881 PER SRM 53-00-03-2R-1 REF SA-M 326 A1085489

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 52,836 hrs · 32,327 cycles

CREASE BEAM OUTER CHORD DAMAGED BETWEEN BS 817 TO BS 894, STR 17L. R&R CHORD PER EA.

Part: SHEAR WEB — DAMAGED (FUSELAGE) · airframe 52,836 hrs · 32,327 cycles

CREASE BEAM SHEAR WEB DAMAGED BETWEEN BS 867 TO BS 887. R&R CHORD PER EA.

Part: DOOR FRAME — CRACKED (BS 294) · airframe 51,984 hrs · 31,780 cycles

FORWARD GALLEY DOORWAY FORWARD FRAME CRACKED AT BS 294, WL 208.5. REPAIRED THE DOOR FRAME IAW ER AND EA.

Part: DOUBLER — CRACKED (BS 663 BULKHEAD) · airframe 51,984 hrs · 31,780 cycles

BULKHEAD, SEAL DOUBLER AT BS 663, RBL 15 CRACKED. R & R THE DOUBLER IAW SRM & DWG.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 51,984 hrs · 31,780 cycles

HORIZONTAL STIFFENER CRACKED AT BS 663, LBL 9. R & R THE STIFFENER IAW DWG AND SRM.

Part: SHEAR TIE — CRACKED (BS 947) · airframe 51,984 hrs · 31,780 cycles

SHEAR TIE CRACKED AT BS 947, STRINGER 4L. R & R THE SHEAR TIE IAW SRM & DWG.

Part: WEB — CORRODED (BS 767-787) · airframe 51,984 hrs · 31,780 cycles

AFT CARGO BAY WEB CORRODED BETWEEN BS 767 TO 787, RBL 25. R & R THE WEB IAW DWG & SRM.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 51,984 hrs · 31,780 cycles

VERTICAL STIFFENER CRACKED AT BS 663, LBL 25. R & R THE STIFFENER IAW SRM AND DWG.

Part: PLATE — CRACKED (LT WING) · airframe 51,984 hrs · 31,780 cycles

LEFT WING LOWER TRAILING EDGE WIGGLE PLATE CRACKED AT ORSS 261. R & R THE PLATE IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 51,984 hrs · 31,780 cycles

RIGHT WING LOWER TRAILING EDGE WIGGLE PLATE CRACKED AT ORSS 261. R & R THE PLATE IAW SRM.

Part: RETAINER — CRACKED (RT WING) · airframe 51,984 hrs · 31,780 cycles

RT WING SEAL RETAINER ABOVE #2 PYLON AFT TIP IS CRACKED / REMOVED AND REPLACED RT WING SEAL RETAINER ABOVE #2 PYLON P/N. 115A2953-2 IAW SRM 51-40-02. AND AIPC. 57-50-00-25. 88920U 10MAR18

Part: SIDEWALL SUPPORT — CORRODED (BS 727B-787) · airframe 51,984 hrs · 31,780 cycles

AFT CARGO BAY LEFT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727B TO 787. R & R THE SIDEWALL SUPPORT IAW DWG & SRM.

Part: SUPPORT — CORRODED (BS 500A-500C) · airframe 51,984 hrs · 31,780 cycles

SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO 500C, RBL 24. R & R THE SUPPORT IAW DWG AND SRM.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 51,984 hrs · 31,780 cycles

***CORROSION*** ACB FLOOR T-STRAP AT STA 887 HAS CORROSION ON UPR & LWR SURFACES / REMOVED ACB FLOOR T-STRAP AT BS 887 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM. REPLACED T-STRAP. FROM MAT. BNC1505-100543 #7075- T6511 LOT# 1271808 PER REF DWG NBR. 146A9401; 146A7500 AND SRM 51-40-02-0G

Part: FLOOR SUPPORT — CRACKED (BS 747-767) · airframe 51,984 hrs · 31,780 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 747 TO 767, RBL 22. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 727B-767) · airframe 51,984 hrs · 31,780 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727B TO 767. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: FITTING — SHEARED (R1 DOOR GIRT BAR) · airframe 51,984 hrs · 31,780 cycles

R1 DOOR ESCAPE SLIDE PACK AFT GIRT BAR RETAINING FITTING, SHEARED MOUNTING RIVET. R & R THE FITTING IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 500) · airframe 51,984 hrs · 31,780 cycles

SIDEWALL SUPPORT SHIELD CORRODED AT BS 500, RBL 24. R & R THE SIDEWALL SUPPORT IAW SRM AND DWG.

Part: SUPPORT BRACKET — CORRODED (AFT CARGO) · airframe 51,984 hrs · 31,780 cycles

AFT CARGO BAY AFT BULKHEAD RT LOWER CURVED SUPPORT BRACKET CORRODED AT RBL 22. R & R THE BRACKET IAW DWG AND SRM.

Part: TRANSITION PANEL — CORRODED (BS 767-787) · airframe 51,984 hrs · 31,780 cycles

AFT CARGO BAY DOOR FORWARD TRANSITION PANEL CORRODED BETWEEN BS 767 TO 787. R & R THE TRANSITION PANEL IAW DWG & SRM.

Part: SLIDE — FRAYED (R1 DOOR) · airframe 51,984 hrs · 31,780 cycles

R1 DOOR ESCAPE SLIDE PACK GIRT FRAYED. R & R THE SLIDE IAW MT.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 51,984 hrs · 31,780 cycles

AFT PASSENGER FLOOR PANEL 242VF HAS UPPER SURFACE SKIN DELAMINATION / AFT PASSENGER FLOOR PANEL 242UF UPPER SURFACE SKIN DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1 56144U 03/01/2018

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 51,984 hrs · 31,780 cycles

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

Part: FLOOR SUPPORT — CRACKED (BS 277-294.5) · airframe 51,984 hrs · 31,780 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294.5, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 51,984 hrs · 31,780 cycles

AFT PASSENGER FLOOR PANEL 241AEF IS BROKEN ON UPPER SURFACE / AFT PASSENGER FLOOR PANEL 241AEF BREAKAGE ON UPPER SURFACE WAS REPAIRED IAW SRM 53-00-50-2R-1 56144U 03/01/2018

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 51,984 hrs · 31,780 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, RBL 29. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 51,984 hrs · 31,780 cycles

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

Part: BULKHEAD — CRACKED (BS 663) · airframe 51,984 hrs · 31,780 cycles

RIGHT WHEEL WELL BULKHEAD CRACKED BS 663, INBOARD CORNER OF PACK EXHAUST CUT OUT. REPAIRED IAW EA.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 51,984 hrs · 31,780 cycles

AFT PASSENGER FLOOR PANEL 242XF IS BROKEN / AFT PASSENGER FLOOR PANEL 242XF THAT IS BROKEN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO REPAIR COSTS.

Part: SKIN — DENTED (AFT FUSELAGE) · airframe 51,984 hrs · 31,780 cycles

(QC) DENT LOCATED 4' FWD OF BS 927; APPROX. 2' BELOW STR 19R REQUIRES RE-EVALUATION; DENT DOT DAMAGED. (MARKED) / REPAIRED SKIN AT BS 927 STR 19R IAW ER 18-01788 REV IR AND EA 1-753-32456 REV IR

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 51,984 hrs · 31,780 cycles

PANEL 195CL AFT LOWER CORNER CRACKED / PANEL 195CL AFT LOWER CORNER CRACK REPAIRED IAW SRM 51-70-05-2R-6 20549U 03/02/18

Part: FLOOR PANEL — PULLED (CABIN) · airframe 51,984 hrs · 31,780 cycles

FWD PASSENGER CABIN FLOOR PANEL 221DF HAS PULLED STRANDS ON UPPER SURFACE FWD EDGE / FWD PASSENGER CABIN FLOOR PANEL 221DF WITH PULLED STRANDS ON UPPER SURFACE FWD EDGE WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF DAMAGE OVER ENTIRE PANEL

Part: SKIN — CRACKED (SLAT) · airframe 51,984 hrs · 31,780 cycles

SLAT NOSE SKIN CRACKED AT FASTENER AT #6 SLAT ACTUATOR RIB (MARKED) / TRIMMED CRACK OUT 6.5' X 3'; NDI NO DEFECTS NOTED; REPAIRED IAW SRM 57-42-01-2R-8 #6 SLAT LOWER NOSE SKIN AT ACTUATOR RIB

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,984 hrs · 31,780 cycles

R2 DOOR EXTERNAL EMERGENCY EGRESS LIGHT INOPERATIVE. R & R THE LIGHT IAW AMM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,490 hrs · 30,173 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE POWER SUPPLY FUSE IAW MM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,490 hrs · 30,173 cycles

R1 DOOR LOWER EXIT LIGHT INOPERATIVE. R & R THE POWER SUPPLY FUSE IAW MM.

Part: FLAP — DELAMINATED (RIGHT WING) · airframe 49,490 hrs · 30,173 cycles

RH WING OUTBD TRAILING EDGE FLAP INBD AFT EDGE DELAM INATED / REPAIRED R/H OUTBD TRAILING EDGE FLAP INBD AFT EDGE I/A/W 737-700 51-70-10-2R-1 PAR 3. D-F REV 61. (A518 45) EC3333 PASTE ADHESIVE

Part: SKIN — CRACKED (LE SLAT) · airframe 49,490 hrs · 30,173 cycles

RT WING NR 8 LE SLAT LOWER SKIN CRACKED AT ACTUATOR CUTOUT. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,912 hrs · 29,835 cycles

RT OVERWING EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 48,002 hrs · 29,303 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 48,002 hrs · 29,303 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 48,002 hrs · 29,303 cycles

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

Part: RETAINING CLIP — OUT OF ADJUST (R1 DOOR) · airframe 47,926 hrs · 29,249 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR RETAINING CLIP OUT OF ADJUST. ADJUSTED CLIP IAW SIP.

Part: COFFEEMAKER — ODOR (AFT GALLEY) · airframe 47,590 hrs · 29,051 cycles

ODOR REPORTED BY A FLIGHT ATTENDANT AND ODOR IN AFT GALLEY POSSIBLY FROM COFFEE MAKER. FOUND AFT INBOARD COFFEE MAKER BURNER CAUSED ODOR. R&R AFT COFFEE MAKER PER AMM.

Part: WINDOW — ARCED (COCKPIT) · airframe 47,583 hrs · 29,045 cycles

R1 WINDSHIELD ARCED. R & R R1 WINDOW IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 46,019 hrs · 28,108 cycles

AFT ENTRY CENTER EXIT LIGHT DAMAGED. R & R LIGHT IAW AMM.

Part: SUPPORT — BENT (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT BENT, BETWEEN BS 500A - 500B LT. R & R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CRACKED (LT WING) · airframe 46,019 hrs · 28,108 cycles

LEFT WING LOWER TE PANEL SUPPORT, JUST OTBD OF PYLON CRACKED ON INBD END. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

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

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY CLIP UNDER FLOOR TO SIDEWALL, SUPPORT FRAME CRACKED AT BS 500C, RT SIDE. R & R SUPPORT IAW SRM.

Part: BAFFLE — BENT (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT BENT, BETWEEN BS 440 - 460 LT. R & R BAFFLE IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY CLIP CRACKED AT BS 500C, UNDER FLOOR TO SIDEWALL SUPPORT LT AFT SIDE OF FRAME. R & R CLIP IAW SRM & DWG.

Part: BAFFLE — BENT (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT BENT, BETWEEN BS 460 - 480 LT. R & R BAFFLE IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727 TO BS 767 PUSHUPS, R & R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 767 - 794, RBL 21. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727 - 847, LBL 21. R & R SUPPORT IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

STRINGER CLIP CORRODED AT BS 967, STRINGER 20R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

STRINGER CLIP CORRODED AT BS 967, RBL 5. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

STRINGER CLIP CORRODED AT BS 947, STRINGER 18R. R & R CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

CREASE BEAM WEB CORRODED AT BS 727+12, STRINGER 17R. REPAIRED WEB IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED, BETWEEN BS 867 - 887, RBL 21. REPAIRED PLATE IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

AFT CARGO BAY ON THRESHOLD WEB CORRODED, BETWEEN BS 794 - 847, BETWEEN RBL 20 - 28. R & R WEB IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

AFT CARGO BAY ON FLOOR PANEL SPLICE STRAP CORRODED AT BS 887, BETWEEN RBL 21 TO LBL 10. R & R FLOOR PANEL SPLICE STRAP IAW SRM.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 46,019 hrs · 28,108 cycles

AFT CARGO BAY CARGO TIE DOWN TRACK CRACKED AT BS 747, RBL 14. R & R TRACK IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED, BETWEEN BS 420 - 440, RBL 23. R & R PLATE IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN, BS 492 - 500A, RBL 23. R & R SUPPORT IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY ON THRESHOLD WEB CORRODED, BETWEEN BS 440 - 492, BETWEEN RBL 23 - 30. R & R WEB IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY ON LT LOWER CURVED BULKHEAD SUPPORT ANGLE CORRODED, AT BS 500D, LBL 25. R & R ANGLE IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED, BETWEEN BS 396 - 420, RBL 23. R & R PLATE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED, BETWEEN 500A - 500D, RBL 23. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED, BETWEEN BS 887 - 947, RBL 21. R & R SUPPORT IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY AFT ATTACH ANGLE CRACKED AT BS 500B, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY FWD ATTACH ANGLE CRACKED AT BS 400, STRINGER 26L. REPAIRED ANGLE IAW DWG & SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

AFT CARGO BAY BULKHEAD LINER SUPPORT CHANNEL BRACKET CRACKED AT BS 727+3, RBL 3. R & R BRACKET IAW DWG & SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED, BETWEEN BS 396 - 500D, LBL 23. R & R PLATE IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY ON LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN RBL 24 TO LBL 24. R & R ANGLE IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FORWARD CARGO BAY AFT ATTACH ANGLE CRACKED AT BS 500C, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: PLATE — CORRODED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED, BETWEEN BS 847 - 867, RBL 21. R & R SUPPORT IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

LEFT LOWER FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED WEB IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

RIGHT FLIGHT DECK WINDOW FRAME, FIRST LOWER FASTENER HOLE IN E-F POST CRACKED. REPAIRED POST IAW SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 46,019 hrs · 28,108 cycles

LEFT FLIGHT DECK WINDOW FRAME, FOURTH LOWER FASTENER HOLE IN LT E-F POST CRACKED. REPAIRED POST IAW SI.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

RIGHT FLIGHT DECK WINDOW FRAME, THIRD LOWER FASTENER HOLE IN E-F POST CRACKED. REPAIRED POST IAW SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FUSELAGE FRAME CRACKED AT STATION 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: POST — CRACKED (COCKPIT) · airframe 46,019 hrs · 28,108 cycles

THE 2ND LOWER FASTENER HOLE IN THE LT E-F POST CRACKED. REPAIRED POST IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: POST — CRACKED (COCKPIT) · airframe 46,019 hrs · 28,108 cycles

THE 2ND LOWER FASTENER HOLE IN RT SIDE E-F POST CRACKED. REPAIRED POST IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FUSELAGE FRAME CRACKED AT STATION 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

LEFT FLIGHT DECK WINDOW FRAME, THIRD LOWER FASTENER HOLE IN LT E-F POST CRACKED. REPAIRED POST IAW SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FUSELAGE FRAME CRACKED AT STATION 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

LEFT FLIGHT DECK WINDOW FRAME, FIRST LOWER FASTENER HOLE IN LT E-F POST CRACKED. REPAIRED POST IAW SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

FUSELAGE FRAME CRACKED AT STATION 440, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,019 hrs · 28,108 cycles

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