N752SW

Part: TIRE — LOOSE (ZN 700 LANDING G) · airframe 77,797 hrs · 45,777 cycles

LEFT NOSE WHEEL TREAD RECAP CAME LOOSE ON TAKEOFF AND DEPARTED THE AIRCRAFT. LANDED AT LAX WITH A SMOOTH TOUCHDOWN AND GENTLE BRAKING. AIRCRAFT DID NOT LAND OVERWEIGHT. / [01] REMOVED/ REPLACED LH NOSE WHEEL ASSEMBLY PER AMM 32-45-21.;[02] R&R'ED NOSE LANDING GEAR POSITION 2 (B) TIRE PER AMM 32-45-21; TIRE PRESSURE NORMAL.

Part: WHEEL — LOOSE (ZN 700 LANDING G) · airframe 77,797 hrs · 45,777 cycles

LEFT NOSE WHEEL TREAD RECAP CAME LOOSE ON TAKEOFF AND DEPARTED THE AIRCRAFT. LANDED AT LAX WITH A SMOOTH TOUCHDOWN AND GENTLE BRAKING. AIRCRAFT DID NOT LAND OVERWEIGHT. / [01] REMOVED/ REPLACED LH NOSE WHEEL ASSEMBLY PER AMM 32-45-21.;[02] R&R'ED NOSE LANDING GEAR POSITION 2 (B) TIRE PER AMM 32-45-21; TIRE PRESSURE NORMAL.

Part: DOOR — CRACKED (R1 DOOR) · airframe 77,415 hrs · 45,527 cycles

POSIBLE CRACK IN AFT. LOWER DOOR STOP FITTING ON THE FWD. SERVICE DOOR. / [01] PERFORMED NDTM PART 6 51-00-00 PROCEDURE 23. FOUND PART TO BE CRACKED;[02] REMOVED AND REPLACED GALLEY SERVICE DOOR IAW 737 AMM 52-41-00

Part: COVER — EXPOSED (L1 DOOR) · airframe 77,249 hrs · 45,411 cycles

FORWARD ENTRY DOOR SLIDE HAS YELLOW CAUTION FLAP EXPOSED / [01] PLACED VELCRO COVER BACK OVER L1 DOOR ESCAPE SLIDE HANDLE PER SIP

Part: COVER — LOOSE (FWD CABIN) · airframe 77,160 hrs · 45,348 cycles

FWD ENTRY DOOR EMERGENCY LIGHT LENS COVER LOOSE / [01] SECURED WITH TAPE. OK TO CONTINUE ON TLD PER EA M-21-133-00720.

Part: SLIDE & SLEEVE — OUT OF ADJUST (R1 DOOR) · airframe 77,123 hrs · 45,327 cycles

FWD SERVICE DOOR HAS A LOOSE STRAP / [01] REMOVED FWD SVC DOOR ESCAPE SLIDE ASSY; ADJUSTED SLIDE MATERIAL FOR GIRT BAR ; INSTALLED SLIDE ASSY IAWMM 25-66-01

Part: SIGN — LOOSE (FWD ENTRY DOOR) · airframe 76,674 hrs · 45,036 cycles

LOWER EXIT PLACARD AT FORWARD ENTRY DOOR LOOSE / [01] RESECURED LOWER EXIT SIGN COVER @ FWD ENTRY DOOR PER SIP

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,079 hrs · 44,641 cycles

ROWS 8 THRU 11 DEF OVERHEAD BIN EMERGENCY LIGHTS INOP / [01] REPLACED BATTERY CHARGER AND PACK PER AMM 33-51-06. OPS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,079 hrs · 44,641 cycles

ROWS 8 THRU 11 DEF OVERHEAD BIN EMERGENCY LIGHTS INOP / [01] REPLACED BATTERY CHARGER AND PACK PER AMM 33-51-06. OPS GOOD.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 75,483 hrs · 44,261 cycles

FWD ENTRY SLIDE NOT SEATED PROPERLY ON GIRT BAR ; / [01] REMOVED AND REPLACED GIRT BAR FASTENERS PER SRM 51-40-02-0G-0

Part: FAIRING — CRACKED (FUSELAGE) · airframe 74,647 hrs · 43,751 cycles

SUPPLEMENTAL INFORMATION: LEFT WING TO BODY FAIRINGS 191AL-191FL; SUPPORT ASSEMBLY CRACKED ; / [01] R&R LEFT WING TO BODY FAIRINGS 191AL-191FL; SUPPORT ASSEMBLY PER SRM 51-10-02 & SRM 51-40-02.

Part: ANGLE — CRACKED (RT WING SLAT) · airframe 74,046 hrs · 43,386 cycles

CRACK SLAT 6 ON COVE CHORD (ANGLE) STA 202.45 MORE 4.5 INCH AT RT WING ; 2021-319881 / [01] REMOVED COVE CHORD (ANGLE) LOC ON SLAT 6 IAW SRM B737-700 51-40-02; [02] REMOVED COVE CHORD (ANGLE) LOC ON SLAT 6 IAW SRM B737-700 51-40-02; [03] REPLACED COVE CHORD ANGLE P/N : 114A8331-2 AND FASTENERS LOC. ON SLAT #6; BETWEEN STA 144.4500 AND STA 260.4500; RT WING. IAW B737-700 SRM 51-40-02 AND DWG 114A5030 REV: A AND IAW B737-700 SRM 51-10-02 PARAGRAPH 9. TOOL USED CALIPER P/N: 700-113-10; S/N :0019306; DUE DATE: 14-OCT-21; [04] REPLACED COVE CHORD ANGLE P/N : 114A8331-2 AND FASTENERS LOC. ON SLAT #6; BETWEEN STA 144.4500 AND STA 260.4500; RT WING. IAW B737-700 SRM 51-40-02 AND DWG 114A5030 REV: A AND IAW B737-700 SRM 51-10-02 PARAGRAPH 9. TOOL USED CALIPER P/N: 700-113-10; S/N :0019306; DUE DATE: 14-OCT-21 VERIFIED AS RII

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 74,046 hrs · 43,386 cycles

CRACK FRONT SPAR SUPPORT ANGLE LOCATED AT IFSS 120 AND WBL 94.24 AT RT WING ; 2021-319839 / [01] REPLACED FRONT SPAR SUPPORT ANGLE LOCATED AT IFSS 120 AND WBL 94.24 AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02 AND DWG # 116A3001 REV: --; [02] REPLACED FRONT SPAR SUPPORT ANGLE LOCATED AT IFSS 120 AND WBL 94.24 AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02 AND DWG # 116A3001 REV: --<BR>RII INSPECTION DONE.

Part: SUPPORT — CORRODED (BS 807) · airframe 74,046 hrs · 43,386 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727E AND BS 807 S-25L AT WL 156 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727E AND BS 807 S-25L AT WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING # 146A7502 REV A.

Part: SUPPORT ANGLE — CRACKED (BS 400 S26L) · airframe 74,046 hrs · 43,386 cycles

CRACK ANGLE - SUPPORT LOCATED BS 400 AFT FACE STRINGER 26L FWD CARGO COMPARTMENT ; 2021-319856 / [01] REPLACED ANGLE - SUPPORT LOCATED BS 400 AFT FACE STRINGER 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG 143A7505 REV.B PN USED 143A7502U155 PO 2020 212944; [02] CERTIFIED RII WORK PERFORMED.

Part: SUPPORT — CRACKED (BS 400-420) · airframe 74,046 hrs · 43,386 cycles

CRACK SUPPORT ZEE LOCATED BS 400 AND BS 420 AND S-26R AT FWD CARGO COMPARTMENT ; 2021-319855 / [01] TOOL USED: DIGITAL 150 S/N: AE-412602 DUE DATE: 31-MAY-22; [02] REPLACED SUPPORT ZEE LOCATED BS 400 AND BS 420 AND STR 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND SRM 53-30-53-0L-2 FIGURE 2 ITEM 1 TABLE 2 DWG 143A7500 REV. A MATERIAL USED BAC 1496-444 PO 2020 185898; [03] REPLACED SUPPORT ZEE LOCATED BS 400 AND BS 420 AND STR 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND SRM 53-30-53-0L-2 FIGURE 2 ITEM 1 TABLE 2 DWG 143A7500 REV. A MATERIAL USED BAC 1496-444 PO 2020 185898<BR>RII

Part: SUPPORT — CORRODED (BS 727-767) · airframe 74,046 hrs · 43,386 cycles

CORROSION SUPPORT ZEE LOACTED BETWEEN BS 767 AND BS 727 S-25R AT WL 156 AT AFT CARGO COMPARTMENT ; 2021-319853 / [01] TOOL USED P/N DIGITAL 150;S/N AE-412602;CAL DUE DATE 31 MAY-2022; [02] REPLACED SUPPORT ZEE LOACTED BETWEEN BS 727 AND BS 767 S-25R AT WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DWG 146A7500 SHEET 26 REV A; [03] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 767 S-25R AT WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DWG 146A7500 SHEET 26 REV A; [04] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 767 S-25R AT WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DWG 146A7500 SHEET 26 REV A. RII

Part: ANGLE — CRACKED (LT WING) · airframe 74,046 hrs · 43,386 cycles

CRACK ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 276 LT WING ; 2021-319810 / [01] REPLACED ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 276LT WING IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 115A62 REV : A; [02] REPLACED ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 276LT WING IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 115A6200 REV : A

Part: ANGLE — CRACKED (BS 1088-1121) · airframe 74,046 hrs · 43,386 cycles

CRACK CLOSURE ANGLE LOCATED BETWEEN BS1088 TO BS1121 RH SIDE AT UPPER FUSELAGE ; 2021-319799 / [01] TOOL USED PN: NORTEC 600D; SN: 210138503; CAL DUE DATE: 05-MAR-22; [02] PRECISION RADIUS P/N: 2204A3 S/N:AE-408651 DUE DATE: 02-FEB-22; [03] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22.; [04] REPAIRED CLOSURE ANGLE LOCATED BETWEEN BS1088 TO BS1121 RH SIDE AT UPPER FUSELAGE IAW B737-700 SRM 53-80-71-2R-6 REPAIR 6 MATERIAL USED 2024-T0 0.063 P.O. 2021-138368 REPAIR ANGLE (1 E/A) 2024T0/0.063 HEAT TREATED AND CONVERTED FROM 2024T0 TO 2024T42 IAW BAC5602; TABLE IV; TABLE X. TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22.; [05] REPAIRED CLOSURE ANGLE LOCATED BETWEEN BS1088 TO BS1121 RH SIDE AT UPPER FUSELAGE IAW B737-700 SRM 53-80-71-2R-6 REPAIR 6 MATERIAL USED 2024-T0 0.063 P.O. 2021-138368 REPAIR ANGLE (1 E/A) 2024T0/0.063 HEAT TREATED AND CONVERTED FROM 2024T0 TO 2024T42 IAW BAC5602; TABLE IV; TABLE X. TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22.AS RII.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,046 hrs · 43,386 cycles

CRACK LEADING EDGE RIB AT LEADING EDGE STATION 86.66 AT LT HORIZONTAL STABILIZER ; 2021-319790 / [01] REPLACED RIB LOC LEADING EDGE STA 86.66 AT LT HORIZONTAL STABILIZER . I.A.W B737-700 SRM 51-10-02 ;SRM 51-40-02 AND DWG 186A1001 REV B.; [02] REPLACED RIB LOC LEADING EDGE STA 86.66 AT LT HORIZONTAL STABILIZER . I.A.W B737-700 SRM 51-10-02 ;SRM 51-40-02 AND DWG 186A1001 REV B.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,046 hrs · 43,386 cycles

CRACK LEADING EDGE RIB AT LEADING EDGE STATION 105.25 AT LT HORIZONTAL STABILIZER ; 2021-319441 / [01] TOOL USED CALIPER PN: DIGITAL 150 SN: AE 412599 DUE DATE 21-MAY 22; [02] REPLACED LEADING EDGE RIB AT LEADING EDGE STATION 105.25 AT LT HORIZONTAL STABILIZER IAW B737-700 DWG 186A1001 REV. A SRM 51-10-02 AND SRM 51-10-02 ITEM 9 P/N USED 186A1304-1 PO 2021-172657; [03] REPLACED LEADING EDGE RIB AT LEADING EDGE STATION 105.25 AT LT HORIZONTAL STABILIZER IAW B737-700 DWG 186A1001 REV. A SRM 51-10-02 AND SRM 51-10-02 ITEM 9 P/N USED 186A1304-1 PO 2021-172657

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,046 hrs · 43,386 cycles

CRACK LEADING EDGE RIB AT LEADING EDGE STATION 95.96 AT LT HORIZONTAL STABILIZER ; 2021-319791 / [01] TOOL USED CALIPER PN: DIGITAL 150 SN: AE 412599 DUE DATE 21-MAY 22; [02] REPLACED LEADING EDGE RIB AT LEADING EDGE STATION 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 DWG 186A1303 REV.A SRM 51-10-02 ITEM 9 AND SRM 51-40-02 P/N USED 186A1352-5 PO 2021-172982; [03] REPLACED LEADING EDGE RIB AT LEADING EDGE STATION 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 DWG 186A1303 REV.A SRM 51-10-02 ITEM 9 AND SRM 51-40-02 P/N USED 186A1352-5 PO 2021-172982

Part: FLOORBEAM — CRACKED (BS 540 BL0-RBL24) · airframe 74,046 hrs · 43,386 cycles

CRACK STIFFENER FLOOR STRUCTURE BS 540 AND BL0 TO RBL 24.5 CENTER SECTION ; 2021-319751 / [01] TOOL USED P/N: 500-197-20 S/N: 12141486 DUE DATE: 31-JAN-21; [02] REPLACED STIFFENER FLOOR STRUCTURE BS 540 AND BL0 TO RBL 24.5 CENTER SECTION I.A.W B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02-0G-0 AND DWG:143A0060 REV B; [03] REPLACED STIFFENER FLOOR STRUCTURE BS 540 AND BL0 TO RBL 24.5 CENTER SECTION I.A.W B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02-0G-0 AND DWG:143A0060 REV B<BR>RII

Part: SUPPORT ANGLE — CRACKED (BS 807) · airframe 74,046 hrs · 43,386 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS807 AND RBL 19 APPROX. AFT CARGO COMPARTMENT ; 2021-319750 / [01] REPLACED ANGLE-SUPPORT LOCATED ON BS807 AND RBL19 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;51-10-02 AND DWG # 146A8120 REV A ;146A0081 REV C; [02] REPLACED ANGLE-SUPPORT LOCATED ON BS807 AND RBL19 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;51-10-02 AND DWG # 146A8120 REV A ;146A0081 REV C AND TOOL USED: CALIPER 0-6; P/N: 700-113-10; S/N: 0019289; DUE DATE: 25-MAR-22; [03] REPLACED ANGLE-SUPPORT LOCATED ON BS807 AND RBL 19 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;51-10-02 AND DWG # 146A8120 REV A ;146A0081 REV C AND TOOL USED: CALIPER 0-6; P/N: 700-113-10; S/N: 0019289; DUE DATE: 25-MAR-22<BR>RII ACCOMPLISHED

Part: STRINGER — CRACKED (BS 540 S26L) · airframe 74,046 hrs · 43,386 cycles

CRACK STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT ; 2021-319732 / [01] TOOL USED: UT EQUIPMENT P/N: 45MG; S/N: 130060401; DUE DATE: 22/APR/22; [02] TOOL USED P/N:NORTEC 500D; S/N:N500X1693P030456; CAL DUE DATE:30-NOV-21; [03] TOOL USED RADIUS GAUGE P/N S167C S/N AE-35943 CAL DUE DATE: 04 JAN 22.; [04] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE.; [05] REPAIRED STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R 1 REPAIR 1 MATERIAL USED 7075-0.045 PO 2021 134008 AND 7075-T0-0.040 PO 2021 109926 STRINGER SECTION;CHANNEL AND REPAIR ANGLES (2EA) MATERIAL 7075-T0/0.040*/0.045* HEAT TREATED AND CONVERTED FROM 7075-T0 TO CONDITION T6 IAW BAC5602 TABLE IV PAGE 22 AND TABLE X PAGE 33. TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [06] TASK CARD COMPLETED. RII

Part: STRINGER — CRACKED (BS 540 S24R) · airframe 74,046 hrs · 43,386 cycles

CRACK STRINGER 24R LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-319734 / [01] TOOL USED: P/N: 35 DL; S/N: 091419910; DUE DATE: 30-NOV-21.; [02] TOOL USED P/N: NORTEC 500D; S/N: N500X11290U021704; DUE DATE: 08-OCT-21; [03] TOOL USED : RADIUS GAUGE PN: S167C; SN: AE-27309 DUE DATE 05-AUG-21.; [04] PERFORMED PERMANENT REPAIR ON STR 24R LOCATED BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED 7075-T6.045 PO# 2021 152098 AND 7075-T6-0.050; PO# 2921 139514; [05] PERFORMED PERMANENT REPAIR ON STR 24R LOCATED BS 500D BTW BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED 7075-T6.045 PO# 2021 152098 AND 7075-T6-0.050; PO# 2921 139514; [06] PERFORMED PERMANENT REPAIR ON STR 24R LOCATED BS 500D BTW BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED 7075-T6.045 PO# 2021 152098 AND 7075-T6-0.050; PO# 2921 139514 <BR>RII INSPECTION DONE.

Part: STRINGER — CRACKED (BS 540 S25R) · airframe 74,046 hrs · 43,386 cycles

CRACK STRINGER 25R LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-319735 / [01] TOOL USED PN: 45MG; SN: 130064101; DUE DATE: 11 MAR 22.; [02] TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022240; DUE DATE: 01-DEC-21.; [03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22.; [04] PERFORMED PERMANENT REPAIR ON STR 25R LOCATED BTW BS 500C TO BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 MATERIAL USED 7075-T6.036 PO# 2021 131796 AND 7075-T6-0.040; PO# 2921 108926; [05] PERFORMED PERMANENT REPAIR ON STR 25R LOCATED BTW BS 500C TO BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 MATERIAL USED 7075-T6.036 PO# 2021 131796 AND 7075-T6-0.040; PO# 2921 108926 <BR>RII INSPECTION DONE.

Part: STRINGER — CRACKED (BS540 S27R) · airframe 74,046 hrs · 43,386 cycles

CRACK STRINGER 27R LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-319737 / [01] TOOL USED PN: 45MG; SN: 130064101; DUE DATE: 11 MAR 22.; [02] TOOL USED: P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 24-FEB-22; [03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [04] REPAIRED STRINGER 27R LOCATED BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; MATERIAL USED : STRINGER SECTION 7075/0.056/T0 PO# 2021 127971 ; CHANNEL(1E/A);ANGLE (2E/A) 7075/0.063/T0; PO# 2021 120486 STRINGER SECTION;CHANNEL AND REPAIR ANGLES (2EA) MATERIAL 7075-T0/0.056*/0.063* HEAT TREATED AND CONVERTED FROM 7075-T0 TO CONDITION T6 IAW BAC5602 TABLE IV PAGE 22 AND TABLE X PAGE 33. TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [05] TASK CARD COMPLETED. RII

Part: STRINGER — CRACKED (BS 540 S26R) · airframe 74,046 hrs · 43,386 cycles

CRACK STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-319736 / [01] TOOL USED: P/N: 35 DL; S/N: 091419910; DUE DATE: 30-NOV-21.; [02] TOOL USED P/N: NORTEC 500D; S/N: N500X11290U021704; DUE DATE: 08-OCT-21; [03] PERFORMED PERMANENT REPAIR ON STR 26R LOCATED BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED 7075-T6.045 PO# 2021 152098 AND 7075-T6-0.050; PO# 2921 139514; [04] PERFORMED PERMANENT REPAIR ON STR 26R LOCATED BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED 7075-T6.045 PO# 2021 152098 AND 7075-T6-0.050; PO# 2921 139514<BR>RII

Part: STRINGER — CRACKED (BS 540 S24L) · airframe 74,046 hrs · 43,386 cycles

CRACK STRINGER 24L LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-319729 / [01] TOOL USED: UT EQUIPMENT P/N: 45MG; S/N: 130060401; DUE DATE: 22/APR/22; [02] TOOL USED P/N:NORTEC 500D; S/N:N500X1693P030456; CAL DUE DATE:30-NOV-21; [03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [04] REPAIRED STRINGER 24L LOCATED BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R 1 REPAIR 1 MATERIAL USED 7075-0.045 PO 2021 152098 STRINGER SECTION;CHANNEL AND REPAIR ANGLES (2EA) MATERIAL 7075-T0/0.045*/0.050* HEAT TREATED AND CONVERTED FROM 7075-T0 TO CONDITION T6 IAW BAC 5602 TABLE IV PAGE 22 AND TABLE X PAGE 33. TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [05] TASK CARD COMPLETED. RII

Part: SHEAR TIE — CRACKED (BS 277 S10R) · airframe 74,046 hrs · 43,386 cycles

CRACK TIE CLIP LOCATED AT BS 277 LEVEL STR 10R AT PASSENGER CABIN ; 2021-319725 / [01] REPLACED TIE CLIP LOC. BS 277 AT LEVEL STRINGER 10R AT PASSENGER CABIN. IAW B737-700; SRM 51-10-02; SRM 51-40-02 AND DWG #141A1110 SHEET 18 REV -.; [02] TASK COMPLETED; VERIFIED AS RII.<BR><BR>INSTALLED NEW TIE CLIP AND FASTENERS LOC. BS 277 LEVEL STRINGER 10R AT PASSENGER CABIN. IAW B737-700; SRM 51-40-02 AND DWG #141A1110 SHEET 18 REV -.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 74,046 hrs · 43,386 cycles

CRACK FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT ; 2021-319615 / [01] FABRICATED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 STEP 1 (C) (F) DWG 453A2310 SHEET 4 REV C. MATERIAL USED A90RG1W 48144 PO 2021-152338.; [02] CERTIFIED WORK PERFORMED.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 74,046 hrs · 43,386 cycles

CRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT ; 2021-319616 / [01] FABRICATED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 STEP 1 (C) (F) DWG 453A2610 SHEET 3 REV C MATERIAL USED A90RG1W 48144 PO 2021-152338.; [02] CERTIFIED WORK PERFORMED.

Part: HANDLE — BROKEN (R1 DOOR) · airframe 74,046 hrs · 43,386 cycles

BROKEN EMERGENCY DOOR COVER HANDLE RH SIDE AT PASSENGER CABIN (1 EA) ; 2021-319518 / [01] REPLACED EMERGENCY DOOR COVER HANDLE RH SIDE AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 52-22-51-400-801; [02] REPLACED EMERGENCY DOOR COVER HANDLE RH SIDE AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 52-22-51-400-801 STEP 3; C; 2(H)

Part: SKIN — CRACKED (RT WING SLAT) · airframe 74,046 hrs · 43,386 cycles

CRACK EXTERNAL SKIN SLAT 6 LOCATED AROUND THE FASTENER THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 202.45. AT RT WING ; 2021-319499 / [01] TOOL USED DIGITAL CALIPER P/N: 500-172-30; S/N: 15237811; DUE DATE: 11-MAY-22; [02] TOOL USED P/N: NORTEC500D; S/N: N500X12101V022236; DUE DATE: 02-JUN-22.; [03] PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN SLAT 6 LOCATED AROUND THE FASTENER THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 202.45. AT RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8.; [04] PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN SLAT 6 LOCATED AROUND THE FASTENER THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 202.45. AT RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8. VERIFIED AS RII.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 74,046 hrs · 43,386 cycles

CRACK EXTERNAL SKIN SLAT 8 LOCATED AROUND THE FASTENER THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 451.97. AT RT WING ; 2021-319497 / [01] TOOL USED DIGITAL CALIPER P/N: 500-172-20;S/N: 12141486; DUE DATE: 31-JAN-22; [02] TOOL USED P/N: NORTEC500D; S/N: N500X12101V022236; DUE DATE: 02-JUN-22.; [03] RAISED NEW FAULT TTG8Q005QV50 TO REPLACE SLAT 8 DUE TO NOT FOUND ALLOWABLE DAMAGE FOR CRACK ON THE ACTUATOR RIB FITTING; [04] RAISED NEW FAULT TTG8Q005QV50 TO REPLACE SLAT 8 DUE TO NOT FOUND ALLOWABLE DAMAGE FOR CRACK ON THE ACTUATOR RIB FITTING

Part: HANDLE — BROKEN (COCKPIT) · airframe 73,455 hrs · 43,052 cycles

CAPT. ASSIST HANDLE IS BROKEN. R&R CAPT. ASSIST HANDLE AMM 561111.

Part: SKIN — CRACKED (ZONE 200) · airframe 73,382 hrs · 43,012 cycles

INDICATION OF CRACK S4R STA 500C +8 APPOX 1.5'LONG. NDT REF PART 6 53-30-25; VERIFIED PART 6 53-30-09 / ACCOMPLISHED REPAIR IAW EA 1-A53-10228 REV 1 SA-M 326:A1308728

Part: SKIN — CRACKED (ZONE 200) · airframe 73,382 hrs · 43,012 cycles

CRACK INDICATION S4R STA 500D + 10 APPROX 1/2' LONG. NDT REF PART 6 53-30-25; VERIFIED PART 6 53-30-09 / ACCOMPLISH REPAIR EA NO. 1-A53-10228 REV. 1 SEE SA-M A1308731

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,382 hrs · 43,012 cycles

CRACK INDICATOR STR STA 500 D & 7 APPROX 1' IN LENGTH NDT REF PART 6 53-30-25; VERIFIED PART 6 53-30-09 / ACCOMPLISHED REPAIR EA NO. 1-A53-10228 REV 1 SA-M 326:A1308730

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 73,162 hrs · 42,889 cycles

PILOT REPORT RF SLIDE INSPECTION STICKER BLOCKS PRESSURE GUAGE / R&R'D SLIDE ASSY PER MT 725-61-06 RAR# 91643 P/N OFF/ON 63550-101; S/N OFF 0311F _____________________S/N ON 0177F

Part: ROLLER — BROKEN (L2 DOOR) · airframe 73,039 hrs · 42,810 cycles

AFT ENTRY DOOR GUIDE ROLLER OUTER RACE BROKEN. / REMOVED AND REPLACED PER AMM 52-13-21.

Part: SKIN PANEL — CORRODED (FUSELAGE CROWN) · airframe 73,008 hrs · 42,792 cycles

SURFACE CORROSION FOUND ON CROWN SKIN AT ADF ANTENNA MOUNT HOLES 1-12 MARKED / REPAIRED PER EA #21-153-00299

Part: SKIN — CRACKED (ZONE 200) · airframe 73,008 hrs · 42,792 cycles

FOUND 2 EACH CRACK INDICATIONS AT CHEM-MILL STEP AT STR 1 BETWEEN STA 675 AND STA 706 AT L/H SIDE OF ADF ANTENNA. DETECTED WITH PART 6; 53-30-09 AND VERIFIED WITH PART 4; 53-30-07. AFT CRACK MEASURES 2' IN LENGTH APPROX; FWD CRACK MEASURES APPROX 1' IN LENGTH / SA-M 326 #A1308443 COMPLIED WITH EA. 21-153-00299. PART 1;2;4;5;6 AND REV IR

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,597 hrs · 42,544 cycles

9ABC AND 12ABC AISLE EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED M1670 BATTERY PACK. OPERATIONS CHECK GOOD, REF AMM 33-51-06.

Part: TRANSMITTER — FAILED (LT TE FLAPS) · airframe 72,597 hrs · 42,544 cycles

ON 5 MILE FINAL HAD TO SLOW FOR PRECEEDING AIRCRAFT, WENT FROM FLAPS 30 TO FLAPS 40. FLAPS STOPPED SYMMETRICALLY AT 35 DEGREES W/FLAP HANDLE IN THE 40 DEGREE POSITION. WENT AROUND RAN TRAILING EDGE FLAP DISAGREE QRH. DECLARED EMERGENCY LANDED. AFTER LANDING FLAPS MOVED TO 40 DEGREES ON THEIR OWN. AT THE GATE 'B' SYSTEM HYD READ 68%. LEFT GEG 'B' SYST HYD READ 91%, FOUND BAD LEFT TRAILING EDGE FLAP POSITION FAILED, PER FSCU. REMOVED LEFT TRAILING EDGE FLAP POSITION TRANSMITTER AND INSTALLED SERVICEABLE UNIT, PER AMM 27-58-01. C/W TRAILING EDGE FLAPS AND LEADING EDGE FLAPS/SLAT SYSTEM LOCKOUT, PER 727-PRD-01-03 RAR 78726 POS LT P/N OFF/ON 18-1738-10 S/N OFF 3152 S/N ON 3919.

Part: COVER — LOOSE (L2 DOOR SLIDE) · airframe 70,485 hrs · 41,250 cycles

AFT SCREW, HOLDING ESCAPE SLIDE ON AFT ENTRY DOOR, STRIPPED. SECURED COVER IAW AMM.

Part: HANDLE — MISSING (L2 DOOR SLIDE) · airframe 70,181 hrs · 41,074 cycles

L2 DOOR MANUAL ESCAPE SLIDE PULL HANDLE COVER MISSING. / REPOSITIONED PULL HANDLE IAW AMM.

Part: HOOK AND LOOP — WORN (COVER) · airframe 69,901 hrs · 40,893 cycles

R/H EMERGENCY EXIT OVER WING COVER VELCRO WORN. / R&R VELCRO PER SIP.

Part: LIGHT — DAMAGED (CABIN) · airframe 69,256 hrs · 40,475 cycles

G1 GALLEY EMERGENCY EXIT LIGHT ASSEMBLY DAMAGED. / R&R LIGHT ASSEMBLY IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,256 hrs · 40,475 cycles

R/H FORWARD SLIDE LIGHT INOP. R&R LAMP PER AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 69,256 hrs · 40,475 cycles

ACB AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED ACB AFT CORNER SCUFF PLATE PER REF EA 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 69,256 hrs · 40,475 cycles

AFT CARGO BAY; FORWARD CORNER SCUFF PLATE IS CRACKED. / REPLACED FWD CORNER SCUFF PLATE PER REF AMM 53-11-02-420-801

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 69,256 hrs · 40,475 cycles

FORWARD CARGO BAY; AFT CORNER SCUFF PLATE IS CRACKED. / RECIEVED ACB AFT CORNER SCUFF PLATE (P/N 7530065). TO BE INSTALLED ON CUSTOMER CARD # 753-646-63-01. 59577U 09AUG19

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 69,256 hrs · 40,475 cycles

FORWARD CARGO BAY; FORWARD CORNER SCUFF PLATE IS CRACKED. / RECIEVED FCB FORWARD CORNER SCUFF PLATE (P/N 7530406). TO BE INSTALLED ON CUSTOMER CARD # 753-646-63-01. 59577U 09AUG19

Part: PLATE — BROKEN (R/H WING) · airframe 69,256 hrs · 40,475 cycles

R/W T/E WIGGLE PLATE BROKEN COMMON TO FORWARD EDGE OF PANEL 651BB / REMOVED AND REPLACED WIGGLE PLATE ASSY R/W T/E COMMON TO FORWARD EDGE OF PANEL 651BB IAW SRM 51-40-02-0G-0; DWG 115A2781 AND IPC 57-50-00-27 83802U 10AUG19

Part: FLOOR SUPPORT — CRACKED (BS 400-420) · airframe 69,256 hrs · 40,475 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS. 400 TO BS. 420, LBL 22. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: ANGLE — CORRODED (AFT FUSELAGE) · airframe 69,256 hrs · 40,475 cycles

***CORROSION*** ANGLE ON FUSELAGE CROWN; AT BS1036; STR-2L TO STR-2R / REMOVED AND REPLACED ANGLE ON FUSELAGE CROWN; AT BS 1036; STR-2L TO STR-2R IAW SRM 51-40-02-0G-0 AND DWG 148A3110 83802U 05AUG19

Part: DOUBLER — CORRODED (BS 1036-1043) · airframe 69,256 hrs · 40,475 cycles

FUSELAGE CROWN DOUBLER PLATE CORRODED BETWEEN BS. 1036 TO BS. 1043, BETWEEN STR. 2L TO STR. 2R. / R&R DOUBLER PLATE IAW SRM AND DWG.

Part: STRINGER — CRACKED (LT WING) · airframe 69,256 hrs · 40,475 cycles

L/H WING FIXED LEADING EDGE STRINGER CRACKED JUST INBOARD OF PYLON. R&R STRINGER IAW SRM & DWG.

Part: SKIN — CORRODED (EMPENNAGE CROWN) · airframe 69,256 hrs · 40,475 cycles

***CORROSION*** UNDER VERTICAL STABILIZER; ALONG PERIMETER OF LH AND RH REAR SPAR STRUCTURAL SUPPORT ANGLES; APPROX. STA 1035-1076; LBL 11-RBL 9 (UPPER CROWN) - MARKED / CORROSION ALONG PERIMETER OF LH & RH REAR SPAR STRUCTURAL SUPPORT ANGLES AT BS 1035-1076; LBL 11- RBL 9 WAS REPAIRED IAW ATS ER 19-04138 REV IR DATED 12AUG19 AND EA 1-753-35388 REV IR

Part: FLOOR SUPPORT — DAMAGED (BS 685) · airframe 69,256 hrs · 40,475 cycles

FLOOR SUPPORT ANGLE DAMAGED AT BS. 685+4, LBL 9. / R&R ANGLE IAW SRM AND DWG.

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 69,256 hrs · 40,475 cycles

PANEL 194GR HAS A DELAMINATED DENT ON THE EXTERNAL SKIN / PANEL 194GR HAD DELAMINATED DENT ON THE EXTERNAL SKIN WERE REPAIRED IAW SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,256 hrs · 40,475 cycles

FLOOR SUPPORT STRUCTURE CRACKED AT BS. 540, LBL 1. R&R FLOOR SUPPORT STRUCTURE IAW SRM & DWG.

Part: WEB — DAMAGED (FUSELAGE) · airframe 69,256 hrs · 40,475 cycles

MAIN E-BAY DOOR CUTOUT LT VERTICAL WEB DAMAGED AT BS. 335, LBL 5. R&R WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (BS 313) · airframe 69,256 hrs · 40,475 cycles

CRACKED RADIUS OF FRAME ABOVE ENTRY DOOR AT BS. 313, STR. 5L. / REPAIRED FRAME IAW ER AND EA.

Part: BULKHEAD — CORRODED (APU COMPARTMENT) · airframe 69,256 hrs · 40,475 cycles

***CORROSION*** ON FWD BULKHEAD AT APU COMPARTMENT JUST UNDER FUEL SUPPLY LINE BS1088 LBL14 WL215. MARKED. / CORROSION ON FWD BULKHEAD AT APU COMPARTMENT AT BS 1088 LBL 14 WL 215 WAS REPAIRED IAW ATS ER 19-04139 REV IR DATED 29JUL19 AND EA 1-753-35316 REV IR

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 69,256 hrs · 40,475 cycles

PANEL 192AL HAS A DELAMINATED DENT ON THE EXTERNAL SURFACE; 9' FROM THE AFT EDGE; 8' FROM THE LOWER EDGE / REPAIRED DELAMINATED DENT ON EXTERNAL SURFACE OF PANEL 192AL IAW SRM 51-70-05-2R-2. 59049U 07-20-19

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,256 hrs · 40,475 cycles

LOWER COMPOSITE BULKHEAD SUPPORT ANGLE CRACKED AT BS. 663, RBL 27. R&R ANGLE IAW SRM AND DWG.

Part: RETAINER — CRACKED (WING CENTER SECT) · airframe 69,256 hrs · 40,475 cycles

REAR SPAR WING CENTER SECTION SEAL RETAINER ASSY AT RH SIDE IS CRACKED / REPLACED REAR SPAR WING CENTER SECTION SEAL RETAINER ASSY AT RH SIDE BS 663 I.A.W SRM 51-40-02-0G-0 AND DRAWING # 111A1000.

Part: SHIELD — CORRODED (BS 492-500A) · airframe 69,256 hrs · 40,475 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 492 TO BS. 500A, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,256 hrs · 40,475 cycles

FORWARD CARGO BAY ON LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 500 TO BS. 500D, LBL 22. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CRACKED (BS 400) · airframe 69,256 hrs · 40,475 cycles

CRACKED INTERCOSTAL TO FRAME ANGLE SUPPORT AT BS. 400, LBL 24. / R&R SUPPORT IAW SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 69,256 hrs · 40,475 cycles

FRAME TO STRINGER INTERCOSTAL SUPPORT CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET PER SRM AND DWG.

Part: SHIELD — CORRODED (BS 420-440) · airframe 69,256 hrs · 40,475 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 420 TO BS. 440, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: RETAINER — CRACKED (LT WING) · airframe 69,256 hrs · 40,475 cycles

LT WING FWD FAIRING 542AB O/B SEAL RETAINER CRACKED. / REMOVED CRACKED LT WING FWD FAIRING 542AB O/B SEAL RETAINER IAW 20-50-01 AND INSTALLED NEW SERVICEABLE LT WING FWD FAIRING 542AB O/B SEAL RETAINER IAW SOPM 20-50-01 59617U 19JUL19

Part: STRINGER SPLICE — CORRODED (BS 1016) · airframe 69,256 hrs · 40,475 cycles

AFT CARGO BAY STRINGER SPLICE FITTING CORRODED AT BS. 1016, RBL 21. / R&R FITTING PER DWG AND SRM.

Part: FLOORBEAM — CORRODED (BS 887) · airframe 69,256 hrs · 40,475 cycles

AFT CARGO BAY FLOOR PANEL SUPPORT SPLICE CORRODED AT BS. 887, BETWEEN RBL 20 TO LBL 7. / R&R SPLICE IAW SRM.

Part: SHIELD — CORRODED (BS 847-867) · airframe 69,256 hrs · 40,475 cycles

AFT CARGO BAY AFT SHIELD AT CORRODED BETWEEN BS. 847 TO BS. 867, RBL 21. R&R SHIELD IAW SRM & DWG.

Part: FLANGE — CHAFED (BS 294 FRAME) · airframe 69,256 hrs · 40,475 cycles

CHAFING ON FRAME STA 294.5 STR 3 LT HAND LOWER FLANGE (MARKED) / BS 294.5. STR 3L FRAME CHAFING WAS REPAIRED IAW ATS ER 19-04127 REV IR DATED 07AUG19 AND EA 1-753-35370 REV IR

Part: SPLICE — CORRODED (AFT CARGO) · airframe 69,256 hrs · 40,475 cycles

***CORROSION*** ON FLOOR PANEL SUPPORT SPLICE AT AFT CARGO BAY BS767+6 LBL20 - RBL19 WL156. / RECIEVED NEW REPLACEMENT SUPPORT SPLICE TO REPLACE CORRODED SPLICE AT ACB BS 767+6 LBL20-RBL19 IAW SRM 51-10-02-0G-0; SUPPORT SPLICE TO BE INSTALLED ON CUSTOMER CARD # JPANEL-141-CLOSE BETWEEN FLOOR PANEL 140BF & 140CF

Part: SHIELD — CORRODED (BS 767-787) · airframe 69,256 hrs · 40,475 cycles

AFT CARGO BAY ON FORWARD SHIELD CORRODED BETWEEN BS. 767 TO BS. 787, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: RAIL — CORRODED (BS 767) · airframe 69,256 hrs · 40,475 cycles

AFT CARGO BAY RAIL CORRODED AT BS. 767+6, LBL 8. REPAIRED FLOOR BEAM IAW EA.

Part: FLOORBEAM — CORRODED (AFT CARGO BAY) · airframe 69,256 hrs · 40,475 cycles

***CORROSION*** ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS927+8 RBL13 WL176. / REMOVED AND REPLACED ACB FLOOR TRACK AT BS 887-947 RBL 13 WL 176 IAW SRM 53-00-53-1A-2 SRM 51-40-02; SRM 51-40-05 AND DWG # 147A7500. 59647U 29JUL19

Part: SUPPORT — CORRODED (BS 727C-847) · airframe 69,256 hrs · 40,475 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727C TO BS. 847, LBL 20. R&R SUPPORT IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 69,256 hrs · 40,475 cycles

AFT CARGO BAY RAIL CORRODED AT BS. 767+6, LBL 3. REPAIRED RAIL IAW EA.

Part: FLOOR SUPPORT — CORRODED (BS 847-867) · airframe 69,256 hrs · 40,475 cycles

AFT CARGO BAY ON LOWER BULKHEAD TO FLOOR PANEL SUPPORT CORRODED BETWEEN BS. 847 TO BS. 867, LBL 20. / R&R SUPPORT PER SRM & DWG.

Part: FRAME — CRACKED (BS 727D) · airframe 69,256 hrs · 40,475 cycles

CABIN FRAME CRACKED AT BS. 727D, STR. 8R BIN RAIL SUPPORT. / REPAIRED FRAME IAW EA.

Part: SUPPORT — CORRODED (BS 727C-767) · airframe 69,256 hrs · 40,475 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727C TO BS. 767, RBL 20. / R&R SUPPORT IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (AFT CARGO BAY) · airframe 69,256 hrs · 40,475 cycles

***CORROSION*** ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS927+8 LBL3 WL176. / REMOVED CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS 927+8 LBL 3 I.A.W SRM 51-10-02-0G-0 AND ELEVAULATED MAX. MATERIAL REMOVED. L=2.5' X W=1.0' X MINIMUM REMAINING THICKNESS 0.073' FROM ORIGINAL THICKNESS=0.080' AND FOUND TO BE WITHIN LIMITS I.A.W. SRM 53-00-53-1A-2 PARAGRAPH 4.B.(2) FIGURE 103 DETAIL 'G'; APPLIED CHEMICAL CONVERSION COATING AND PRIMER I.A.W. SRM 51-20-01-0G-0 ON BLENDED AREA.

Part: RAIL — CORRODED (BS 767) · airframe 69,256 hrs · 40,475 cycles

AFT CARGO BAY RAIL CORRODED AT BS. 767+6, RBL 3. / REPAIRED FLOOR BEAM IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,256 hrs · 40,475 cycles

FRAME CRACKED AT BS. 440, STR 8L BIN RAIL SUPPORT. REPAIRED FRAME PER EA.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 69,256 hrs · 40,475 cycles

AFT CARGO BAY RAIL CORRODED AT BS. 767+6, RBL 8. / REPAIRED RAIL IAW EA.

Part: BEAM — CRACKED (R1 DOOR) · airframe 69,256 hrs · 40,475 cycles

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

Part: STRINGER FITTING — ELONGATED (MAIN CABIN) · airframe 69,256 hrs · 40,475 cycles

AFT BULKHEAD AFT STR END FITTING HOLE OUT OF LIMITS MEASURES .319 AT 8L STR 3L / REAMED HOLE 8L AT STR 3L TO A HOLE DIAMETER OF 0.3286' AND INSTALLED BOLT IAW SI# 12107-53

Part: PRESSURE DECK — CRACKED (BS 663-375) · airframe 69,256 hrs · 40,475 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS. 663 TO BS. 675, LBL 32. REPAIRED PRESSURE DECK IAW ER AND EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 69,256 hrs · 40,475 cycles

RT WING TRAILING EDGE SUPPORT ANGLE CRACKED BELOW PROGRAM ROLLER SUPPORT ARM JUST O/B OF #2 PYLON AFT TIP. R&R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 69,256 hrs · 40,475 cycles

RT WING TRAILING EDGE COVE SEAL SUPPORT ANGLE CRACKED ABOVE #2 PYLON AFT TIP. R&R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 69,256 hrs · 40,475 cycles

LT WING TRAILING EDGE COVE SEAL SUPPORT ANGLE CRACKED ABOVE #1 PYLON AFT TIP. R&R ANGLE IAW SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 69,256 hrs · 40,475 cycles

LOWER COMPOSITE BULKHEAD CRACKED AT BS. 663, RBL 10. R&R BULKHEAD IAW SRM & DWG.

Part: ATTACH FITTING — OUT OF TOLERANCE (EMPENNAGE) · airframe 69,256 hrs · 40,475 cycles

AFT BULKHEAD VERTICAL FIN ATTACHMENT FITTING HOLE OUT OF LIMITS MEASURES .384' AT 5L STR 2L / REAMED HOLE 5L AT STR 2L TO A HOLE DIAMETER OF 0.4067' AND INSTALLED BOLT IAW SI#12107-53

Part: ATTACH FITTING — OUT OF TOLERANCE (EMPENNAGE) · airframe 69,256 hrs · 40,475 cycles

AFT BULKHEAD VERTICAL FIN ATTACHMENT FITTING HOLE OUT OF LIMITS MEASURES .384' AT 6L STR 2L / REAMED HOLE 6L AT STR 2L TO A HOLE DIAMETER OF 0.4067' AND INSTALLED BOLT IAW SI#12107-53

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 68,605 hrs · 40,049 cycles

AFT CARGO CENTER SCUFF PLATE HAS A CRACK MEASURING 5' LONG FROM FWD EDGE OF SCUFF PLATE AND DENT 6' FWD FROM AFT EDGE MEASURING 1.25' LONG .055' DEEP AND .25' WIDE MOD / RECEIVED NEW PART 146A8342-8 OK TO INSTALL WAS ACCOMPLISHED ON CUSTOMER CARD NBR 753-140-00-02Y STEP 3 INSTALLED AFT CARGO CENTER SCUFF PLATE. PER REF. AMM 53-11-02-420-801

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 68,283 hrs · 39,848 cycles

RT SIDE AFT OF COCKPIT DOOR EMERGENCY BATTERY PACK M1674 WILL NOT CHARGE. R&R BATTERY PACK IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 66,975 hrs · 39,022 cycles

LT FWD EMERGENCY BATTERY FAILED TEST. R&R BATTERY ASSY PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 66,069 hrs · 38,445 cycles

AFT GALLEY EMERGENCY EXIT SIGN LENS MISSING. REPLACED THE LENS IAW SIP.

Part: BEZEL — CRACKED (EMERGENCY EXIT) · airframe 65,860 hrs · 38,310 cycles

LT OVERWING EMERGENCY EXIT LOWER HANDLE BEZEL CRACKED. R&R HANDLE BEZEL PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,860 hrs · 38,310 cycles

LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 64,914 hrs · 37,702 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01672. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 64,914 hrs · 37,702 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01670. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 64,914 hrs · 37,702 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01675. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 64,914 hrs · 37,702 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01673. R&R BATTERY PACK PER MM.

Part: BATTERY — OUT OF POSITION (FLASHLIGHT) · airframe 63,641 hrs · 36,920 cycles

LT WIND SCREEN EMERGENCY FLASHLIGHT OUT OF POSITION. R&R BATTERY PER AMM.

Part: FLOORBEAM — CORRODED (BS 727D) · airframe 63,641 hrs · 36,920 cycles

AFT CARGO BAY FLOORBEAM TEE CORRODED AT BS 727D+5.6. R & R THE TEE IAW SRM AND DWG.

Part: SPLICE — CORRODED (BS 772) · airframe 63,641 hrs · 36,920 cycles

AFT CARGO BAY FLOOR TEE SPLICE CORRODED AT BS 772. R & R THE TEE SPLICE IAW SRM & DWG.

Part: SIGN — BROKEN (OVERWING) · airframe 63,641 hrs · 36,920 cycles

CENTER OVERWING CEILING EMERGENCY EXIT SIGN LIGHT BROKEN. R & R THE SIGN ASSEMBLY IAW AMM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,641 hrs · 36,920 cycles

AFT CARGO BAY BULKHEAD SUPPORT CORRODED AT BS 947 RT. R&R SUPPORT PER SRM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 63,641 hrs · 36,920 cycles

LT HORIZ. STAB UPPER FWD SLIDE SEAL IS CRACKED. / REPLACED LT HORIZ. STAB UPPER FWD SLIDE SEAL IAW SRM 51-40-02-0G-0 STEP 4.

Part: TRACK — DAMAGED (CABIN) · airframe 63,641 hrs · 36,920 cycles

ACB; CARGO TIE DOWN TRACK; BS 727+4 TO BS 887; RBL 18; WL 155; REQUIRES REPLACEMENT DUE TO THE EXTENT OF DAMAGE. / ACB; CARGO TIE DOWN TRACK; B.S. 727+4 TO BS 887; RBL 18; WL 155 REQUIRES REPLACEMENT DUE TO THE EXTENT OF DAMAGE. REMOVED DAMAGED SECTION OF TIE DOWN TRACK PER SRM 51-40-02. RECIEVED NEW TIE DOWN TRACK; LOCATED; DRILLED AND INSTALLED PER SRM 53-00-53-2R-3 AND PER DWG 146A7500.

Part: GUSSET — CRACKED (BS 500D) · airframe 63,641 hrs · 36,920 cycles

FORWARD CARGO BAY CRACKED GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 1006-1016) · airframe 63,641 hrs · 36,920 cycles

FLOOR SUPPORT CORRODED BETWEEN BS. 1006 TO BS. 1016, LBL 36. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: BRACKET — CRACKED (BS 947 BULKHEAD) · airframe 63,641 hrs · 36,920 cycles

AFT CARGO BAY BULKHEAD BACKSIDE BRACKET CRACKED AT BS. 947, LBL 9. R & R THE BRACKET IAW SRM.

Part: SHIELD — CORRODED (BS 767-787) · airframe 63,641 hrs · 36,920 cycles

AFT CARGO BAY SHIELD CORRODED BETWEEN BS 767 - 787, RBL 21. R & R THE SHIELD IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,641 hrs · 36,920 cycles

CREASE BEAM WEB CORRODED AT BS 380, RBL 68. REPAIRED WEB IAW EA & ER.

Part: SHEAR WEB — CORRODED (BS 1016) · airframe 63,641 hrs · 36,920 cycles

SHEAR WEB CORRODED AT BS 1016, LBL 36. R & R THE SHEAR WEB IAW SRM.

Part: WEB — CORRODED (AFT CARGO COMPT) · airframe 63,641 hrs · 36,920 cycles

***CORROSION*** ACB BS 927 WL148 O/B STR27L FRAME WEB SURFACE HAS CORROSION. / ACB BS 927; WL 148; OB STR 27L FRAME WEB HAS SURFACE CORROSION REPAIRED PER ATS ESR 17-03115 REV IR AND SWA EA 1-753-31439 REV IR

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · airframe 63,641 hrs · 36,920 cycles

AFT CARGO BAY BULKHEAD PANEL SUPPORT CORRODED AT BS 947, WL 155. R&R SUPPORT PER SRM.

Part: FRAME SPLICE — CORRODED (BS 787) · airframe 63,641 hrs · 36,920 cycles

AFT CARGO BAY FRAME SPLICE CORRODED AT BS 787, STRINGER 25R. R & R THE FRAME SPLICE IAW SRM & DWG.

Part: SHEAR WEB — CORRODED (BS 1016) · airframe 63,641 hrs · 36,920 cycles

SHEAR WEB CORRODED AT BS 1016, RBL 36. R & R THE SHEAR WEB IAW SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 727 & 767) · airframe 63,641 hrs · 36,920 cycles

AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 727 & 767, RBL 21. R & R THE SIDEWALL SUPPORT IAW SRM & DWG.

Part: BAFFLE — CORRODED (AFT CARGO COMPT) · airframe 63,641 hrs · 36,920 cycles

***CORROSION*** ACB BS 947 RBL21 WL155 INTERCOSTAL BAFFLE CLIP HAS CORROSION. / CORROSSION ON ACB BAFFLE CLIP 947 RBL21 WL155 FOUND OUT OF LIMITS DUE TO NO LIMITS ESTABLISHED IN SRM REMOVED & REPLACED CLIP ON CUSTOMER CARD T671390. 56040C 03JUL17

Part: STRAP — CORRODED (BS 781-847) · airframe 63,641 hrs · 36,920 cycles

AFT CARGO BAY DOOR CUTOUT STRAP CORRODED BETWEEN BS 781 TO 847, RBL 21. R & R STRAP IAW SRM & DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-807) · airframe 63,641 hrs · 36,920 cycles

AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO 807, LBL 21. R & R THE SIDEWALL SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 63,641 hrs · 36,920 cycles

***CORROSION*** ACB BS 867-947 RBL21 WL155 SIDEWALL PANEL SUPPORT HAS NUMEROUS CORROSION. / REMOVED CORROSION ON SIDEWALL SUPPORT 807-847 RBL 21 - WL 155 MULTIPLE LOCATIONS 1' X 1' X 2' FOUND OUT OF LIMITS DUE TO GOING OVER MORE THAN 3 IN 10 FASTENERS REMOVED FLOOR TO SIDEWALL SUPPORT LOCATED; DRILLED USING BAC 1496-377 7075T6 LOT # 1283962 ALODINED PRIMED & INSTALLED PER SRM 51-40-02; SRM 51-20-01; SRM 53-00-53-1A-2; SRM 53-70-53-01-02 & DWG 147A7500

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 63,641 hrs · 36,920 cycles

***CORROSION*** ACB BS 787 WL155 ABOVE STR25L FRAME SIDEWALL SUPPORT HAS CORROSION. / REMOVED & REINSTALLED NEW FRAME SIDEWALL SUPPORT DUE TO CORROSION PER SRM 51-40-02-0G-0 & DWG #146A1262

Part: WEB — CORRODED (DOOR FRAME) · airframe 63,641 hrs · 36,920 cycles

AFT CARGO DOOR CUTOUT SUB WEB THRESHOLD CORRODED AREAS. R & R THE SUB WEB THRESHOLD PER SRM & DWG.

Part: WEB — CORRODED (FWD CARGO DOOR) · airframe 63,641 hrs · 36,920 cycles

FORWARD CARGO DOOR OPENING SUB WEB CORRODED. R & R THE SUB WEB PER SRM.

Part: INTERCOSTAL — CRACKED (AFT CARGO COMPT) · airframe 63,641 hrs · 36,920 cycles

ACB BS 947 RBL21 WL155 INTERCOSTAL BAFFLE IS CRACK. / ACB B.S 947 RBL 21 WL 155 INTERCOSTAL BAFFLE IS CRACKED & FOUND OUT OF LIMITS REMOVED & REPLACED PER DWG 147A7500 & SRM 51-40-02

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,641 hrs · 36,920 cycles

FLOORBEAM CORRODED AT BS 328, RBL 42. REPAIRED FLOORBEAM PER ER & EA.

Part: SHIELD — CORRODED (BS 847-867) · airframe 63,641 hrs · 36,920 cycles

AFT CARGO BAY SIDEWALL SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 21. R & R THE SHIELD IAW SRM & DWG.

Part: ANGLE — CRACKED (RIGHT WING) · airframe 63,641 hrs · 36,920 cycles

(RIGHT WING) T/E COVE SEAL SUPPORT ANGLE CRACKED ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED T/E CORE SEAL SUPPORT ANGLE ABOVE #2 PYLON AFT TIP IAW SRM 51-40-02-0G-0 84036_24JUN17

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,641 hrs · 36,920 cycles

CORROSION ON FLOORPANEL INSERTS 221DF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON FLOOR PANEL 221DF IAW SRM 53-00-50-2R-1. 56749U 27JUN17

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 63,641 hrs · 36,920 cycles

FCB; AFT CORNER SCUFF PLATE CRACKED. / REPAIRED AFT CORNER SCUFF PLATE IAW EA 1-A53-2076 REV 11

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,641 hrs · 36,920 cycles

INTERCOSTAL FLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R&R SUPPORT IAW SRM.

Part: INTERCOSTAL — CORRODED (AFT PX BULKHEAD) · airframe 63,641 hrs · 36,920 cycles

CORROSION ON PRESSURE DOME SEAL DEPRESSOR ANGLE BS 1016 RBL 26 WL 210 / REMOVED AND REPLACED PRESSURE DOME SEAL DEPRESSOR ANGLE (INTERCOSTAL) AT BS 1016 RBL 26-RBL 49 WL 210 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 65-54862; 148A0922

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,641 hrs · 36,920 cycles

CORROSION ON CABIN FLOORPANEL INSERTS 241ABF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON CABIN FLOOR PANEL 241ABF IAW SRM 53-00-50-2R-9. 56749U 26JUN17

Part: NONE — CORRODED (CABIN) · airframe 63,641 hrs · 36,920 cycles

CORROSION ON INNER CHORD 'MOPSILL' BS 947-986 LBL57 WL 208 / REMOVED AND REPLACED INNER CHORD 'MOPSIL' ON AFT ENTRY DOOR LOWER MAINSILL 1.D.W. SRM 51-40-20-0G-0 AND BOEING DWG 147A8501.

Part: SUPPORT — CORRODED (BS 400-420) · airframe 63,641 hrs · 36,920 cycles

FORWARD CARGO BAY RT SIDE PLATE SUPPORT CORRODED BETWEEN BS 400 TO 420. R & R THE SUPPORT IAW SRM & DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,641 hrs · 36,920 cycles

CORROSION ON CABIN FLOORPANEL INSERTS 242UF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON CABIN FLOOR PANEL 242UF IAW SRM 53-00-50-2R-9. 56749U 26JUN17

Part: CREASE BEAM — CORRODED (BS 706) · airframe 63,641 hrs · 36,920 cycles

CREASE BEAM CORRODED AT BS 706, LBL 55. REPAIRED THE CREASE BEAM IAW ER AND EA.

Part: SIDEWALL SUPPORT — CORRODED (BS 500D) · airframe 63,641 hrs · 36,920 cycles

FORWARD CARGO BAY SIDE WALL PANEL SUPPORT CORRODED 500D RT BULKHEAD. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: ANGLE — CRACKED (RIGHT WING) · airframe 63,641 hrs · 36,920 cycles

(RIGHT WING) UPPER T/E PANEL U SUPPORT BEAM TO REAR SPAR ATTACH ANGLE IS CRACKED; RSS80 / REMOVED RT WING UPPER TE PANEL U SUPPORT BEAM TO SPAR ATTACH CLIP IAW SRM 51-40-02 56790 06/21/17 3074 C 21JUN17 INSTALLED A NEW T/E PANEL U SUPPORT BEAM TO SPAR ATTACH CLIP IAW SRM 51-40-02-0G-0 STEP 7

Part: PLATE — CORRODED (FWD CARGO RH) · airframe 63,641 hrs · 36,920 cycles

***CORROSION*** FCB BS500A-500D RBL 25 SIDE PLATE HAS CORROSION IN SEVERAL AREAS / REMOVED AND REPLACED FCB BS 500A-500D RBL 25 SIDE PLATE IAW SRM 51-40-02 AND DWG 143A7500

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 63,641 hrs · 36,920 cycles

INTERCOSTAL FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, RBL 31. R & R THE FLOOR SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (BS 400-500D) · airframe 63,641 hrs · 36,920 cycles

FORWARD CARGO BAY SIDE PLATE CORRODED BETWEEN BS 400 & 500D, LBL 25. R & R THE SUPPORT PLATE IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 63,641 hrs · 36,920 cycles

LEFT WING UPPER TRAILING EDGE PANEL LOWER SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT. R & R THE ANGLE IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,641 hrs · 36,920 cycles

CORROSION ON FLOORPANEL INSERTS 221BF / DAMAGE FOUND ON UPPER AND LOWER SKINS OF FLOOR PANEL 221BF AT INSERT LOCATION P45; AND ALL CORRODED INSERTS; WERE REPLACED IAW SRM 53-00-50-2R-1; SRM 53-00-50-2R-2; AND DWG 141A5810-56 56563U 26JUN17

Part: FLOOR PANEL — CORRODED · airframe 63,641 hrs · 36,920 cycles

CORROSION ON FLOORPANEL INSERTS 221GF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON FLOOR PANEL 221GF IAW SRM 53-00-50-2R-9. 56749U 27JUN17

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,641 hrs · 36,920 cycles

CORROSION ON FLOORPANEL INSERTS 222BF / REPAIRED DAMAGE ON FLOOR PANEL 222BF; INSTALLED NEW INSERTS PER SRM 53-00-50-2R-9 AND SRM 53-00-50-2R-0.

Part: WEB — CRACKED (FWD CARGO LH) · airframe 63,641 hrs · 36,920 cycles

FCB BS 500B -500C LBL 25 SIDE PLATE SUPPORT WEB CRACKED. / REMOVED AND REPLACED FCB B.S. 500B-500C LBL 25 SIDE PLATE SUPPORT WEB 143A7510-11/ NEW PER SRM 51-40-02 SRM 51-10-02 DWG 143A7505

Part: WEB — CRACKED (RIGHT WING) · airframe 63,641 hrs · 36,920 cycles

(RIGHT WING) TRANSVERSE WEB IS CRACKED AT O/B END UPPER LEG JUST I/B OF PROGRAM ROLLER SUPPORT ARM ATTACH POINT / REMOVED AND REPLACED TRANSVERSE WEB FITTING OF O/B END AND I/B OF PROGRAM ROLLER ARM SUPPORT IAW SOPM 20-50-01 84036 22JUN17

Part: ANTENNA — CORRODED (LOWER INT FUSELA) · airframe 63,641 hrs · 36,920 cycles

***CORROSION*** FCB BILGE BETWEEN BS500A AND 500B BL0 ANTENNA INTERNAL BASE CORRODED / REMOVED AND REPLACED ANTENNA BASE ASSY FCB BILGE BETWEEN B.S. 500A AND 500B BL0 PER DWG 143A3230 DWG 143A3233 SRM 51-40-02 .040 CLAD LOT # 1252458

Part: ANTENNA — CORRODED (LOWER INT FUSELA) · airframe 63,641 hrs · 36,920 cycles

***CORROSION*** FCB BILGE BETWEEN BS 500-500A BL0. ANTENNA INTERNAL BACE CORRODED / REMOVED AND REPLACED ANTENNA BASE ASSY FCB BILGE BETWEEN 500-500A BL0 PER DWG 143A3230 DWG 143A3233 SRM 51-40-02 .040 T6 CLAD LOT # 1252458

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,641 hrs · 36,920 cycles

CORROSION ON CABIN FLOORPANEL INSERTS 241ADF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON CABIN FLOOR PANEL 241ADF IAW SRM 53-00-50-2R-1. 56749U 26JUN17

Part: WEB — CRACKED (FWD CARGO LH) · airframe 63,641 hrs · 36,920 cycles

FCBBS 500 LBL 25 SIDE PLATE SUPPORT WEB CRACKED / REMOVED AND REPLACED FCB BS 500 LBL 25 SIDE PLATE SUPPORT WEB ASSY 143A7510-15/ NEW FOR SRM 51-40-02 SRM 51-10-02 DWG 143A7505

Part: SHIELD — CORRODED (BS 492-500A) · airframe 63,641 hrs · 36,920 cycles

FORWARD CARGO BAY SHIELD ASSEMBLY CORRODED BETWEEN BS 492 & 500A, RBL 25. R & R THE SHIELD ASSEMBLY IAW SRM.

Part: SHIELD — CORRODED (BS 420-440) · airframe 63,641 hrs · 36,920 cycles

FORWARD CARGO BAY RT SIDE SHIELD ASSEMBLY CORRODED BETWEEN BS 420 & 440. R & R THE SHIELD ASSEMBLY IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,641 hrs · 36,920 cycles

INTERCOSTAL FLOOR SUPPORT CRACKED BETWEEN BS 328 TO BS 344, LBL 46. R&R SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,641 hrs · 36,920 cycles

INTERCOSTAL FLOOR SUPPORT CRACKED; BS 277 - 294; BL 0; WL 207. / REMOVED AND REPLACED INTERCOSTAL FLOOR SUPPORT AT BS. 277-294 BL0; WL 207 PER SRM 51-40-05-0G-0

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 63,641 hrs · 36,920 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, BL 0. R & R FLOOR SUPPORT IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 500) · airframe 63,641 hrs · 36,920 cycles

FORWARD CARGO BAY SIDEWALL PANEL SUPPORT CORRODED AT BS 500, LBL 28. R & R THE SIDEWALL SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 344) · airframe 63,641 hrs · 36,920 cycles

L1 DOOR AFT GIRT BRACKET SUPPORT CORRODED AT BS 344, LBL 59. R & R THE SUPPORT IAW SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,641 hrs · 36,920 cycles

CORROSION ON FLOORPANEL INSERTS 222CF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON FLOOR PANEL 222CF IAW SRM 53-00-50-2R-1 56749U 27JUN17

Part: NONE — CORRODED (CABIN) · airframe 63,641 hrs · 36,920 cycles

CORROSION ON INNER CHORD 'MOPSILL' BS 947-986 RBL57 WL 208 SEE SA-M 326 FOR REJECTIONS A1111758 ATS340INSP 6-28-17 / REMOVED AND REPLACED INNER CHORD 'MOPSILL' AT AFT SERVICE DOOR IAW SRM 51-40-02 AND DWG 147A8501 SHT 69 & 70. COMPLETED REJECTED ITEMS ON SAM326 A1111758 INSTALLED CORRECT FASTENERS IN FRAMES BS 907; 927; 951 & 992 PER DWG 147A8501 SHT 69 & 70. 7138C 6/28/17

Part: SUPPORT ANGLE — CORRODED (BS 500D) · airframe 63,641 hrs · 36,920 cycles

FORWARD CARGO BAY BOTTOM BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 25 RBL 25. R & R THE SUPPORT ANGLE IAW SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 63,641 hrs · 36,920 cycles

ACB; FWD. CORNER SCUFF PLATE CRACKED. / REPAIRED AND INSTALLED ACB; FWD. CORNER SCUFF PLATE IAW EA 1-A53-2076 REV 11 AND AMM 53-11-02-420-801

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,641 hrs · 36,920 cycles

CORROSION ON CABIN FLOORPANEL INSERTS 242WF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON CABIN FLOOR PANEL 242WF IAW SRM 53-00-50-2R-9 56749U 26JUN17

Part: BEAM — CORRODED (CABIN) · airframe 63,641 hrs · 36,920 cycles

CORROSION BS 986 BEAM UPPER CHORD PREVIOUS REPAIR LBL55-RBL55 WL 208 / REMOVED AND REPLACED UPPER CHORD PER ATSER-07-3558 AND REMOVED AND REPLACED REPAIR FASTENERS PER 737-700 SRM 51-40-02 AS SHOWN IN ATS ER 07-3558 (REFERENCE. ESR #17-03029)

Part: ANGLE — CRACKED (RIGHT WING) · airframe 63,641 hrs · 36,920 cycles

(RIGHT WING) UPPER T/E SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED UPPER T/E SUPPORT ANGLE AT THE TRANSVERSE WEB ABOVE #2 PYLON IAW SOPM 20-50-01 84036 24JUN17

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 63,641 hrs · 36,920 cycles

LT WING UPPER TRAILING EDGE PANEL LOWER U SUPPORT BEAM REAR SPAR ATTACH ANGLE CRACKED AT RSS 80. R&R ANGLE IAW SRM.

Part: ANGLE — CORRODED (FSD THRESHOLD) · airframe 63,641 hrs · 36,920 cycles

***CORROSION*** ON FWD SERVICE DOOR THRESHOLD SUPPORT ANGLE; BS 298 - 330; RBL 57; WL 208. / REMOVED OUT OF LIMITS FWD SERVICE DOOR THRESHOLD SUPPORT ANGLE AT BS 298-330 RBL57 WL 208 AND INSTALLED NEW THRESHOLD SUPPORT ANGLE IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0; DWG 141A8310 REV.D

Part: CREASE BEAM — CORRODED (BS 706) · airframe 63,641 hrs · 36,920 cycles

CREASE BEAM CORRODED AT BS 706, RBL 55. REPAIRED THE CREASE BEAM IAW ER AND EA.

Part: RETAINER — BROKEN (EMERGENYC LIGHT) · airframe 63,641 hrs · 36,920 cycles

L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY LENS RETAINER CLIP BROKEN. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: FRAME — CORRODED (FAIRING) · airframe 63,641 hrs · 36,920 cycles

FAIRING FRAME CORRODED AT BS 727C, BETWEEN RBL 4 TO RBL 11. R & R THE FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,112 hrs · 36,608 cycles

INTERCOSTAL ANGLE CRACKED AT BS 528 AIRCRAFT DISTRIBUTION AREA. R&R ANGLE PER SRM.

Part: BULKHEAD WEB — CRACKED (RT MLG WW) · airframe 61,339 hrs · 35,558 cycles

RIGHT MLG WHEEL WELL PRESSURE DECK, CRACKED AT BS 665, RBL 43. REPAIRED THE BULKHEAD WEB IAW EA.

Part: SKIN — CRACKED (L1 DOOR) · airframe 60,825 hrs · 35,242 cycles

L1 DOOR UPPER AFT CORNER DOOR SKIN CRACKED. R & R THE DOOR IAW AMM.

Part: ANGLE — OUT OF ADJUST (GIRT BAR) · airframe 60,754 hrs · 35,205 cycles

L1 DOOR EMERGENCY SLIDE GIRT BAR HOLDING ANGLE FOUND OUT OF ADJUST. ADJUSTED THE ANGLE IAW SIP.

Part: HMU — FAULTY (NR 2 ENGINE) · airframe 60,247 hrs · 34,920 cycles

DIVERSION, DECLARED EMERGENCY FUEL FLOW ON NR 2 ENGINE DROPPED 100 POUNDS N1 DECREASED 5 PERCENT. ENGINE RECOVERED. MINUTE LATER THE FUEL FLOW DROPPED AGAIN OVER 100 POUNDS WITH N1 & N2 DROP. R & R NR 2 ENGINE HYDRO MECHANICAL UNIT IAW MAINTENANCE.

Part: SIGN — BROKEN (CABIN) · airframe 59,883 hrs · 34,719 cycles

FORWARD GALLEY EXIT SIGN HOUSING LOWER CLIP BROKEN. R & R SIGN IAW AMM.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 58,733 hrs · 347,044 cycles

DIVERSION, FUEL CROSS FEED CB POPPED. R & R FUEL CROSS FEED VLV ACTUATOR IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,763 hrs · 33,483 cycles

EXTERNAL EMER LIGHT INOPERATIVE, BETWEEN BS 986.5 - 1006, BETWEEN STRINGER 11R - 12R. R & R LIGHT IAW AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,763 hrs · 33,483 cycles

RIGHT HORIZONTAL STABILIZER, RIB CRACKED AT STAB STATION 92.70 & 38" OF FRONT SPAR. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,763 hrs · 33,483 cycles

RIGHT HORIZONTAL STABILIZER CRACKED AT STAB STATION 92.70, 29" OF FRONT SPAR. REPAIRED RIB IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 57,763 hrs · 33,483 cycles

WEB CRACKED AT BS 663.75, LBL 10. REPAIRED WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

SUPPORT ANGLE CRACKED AT BS 663.75, LBL 10. R & R ANGLE IAW SRM & DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,763 hrs · 33,483 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 101.90, 10" OF FRONT SPAR. REPAIRED RIB IAW EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FORWARD CARGO DOOR CUT OUT CTR SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,763 hrs · 33,483 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT 92.70, 29" OF FRONT SPAR. REPAIRED RIB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FRAME CRACKED AT BS 440, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FRAME CRACKED AT BS 827, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,763 hrs · 33,483 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT 92.70, LOCATED 10" FRONT SPAR. REPAIRED RIB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FRAME CRACKED AT BS 787, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,763 hrs · 33,483 cycles

LEFT WING OTBD AFT FLAP DELAMINATED ON TE AREA. R & R AFT FLAP IAW AMM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 57,763 hrs · 33,483 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, LBL 29. REPAIRED WEB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,763 hrs · 33,483 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT 92.70, 19" OF FRONT SPAR. REPAIRED RIB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FRAME CRACKED AT BS 867, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FRAME CRACKED AT BS 500A, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FRAME CRACKED AT BS 747, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FRAME CRACKED AT BS 907, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 57,763 hrs · 33,483 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, LBL 34. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FRAME CRACKED AT BS 360, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 57,763 hrs · 33,483 cycles

RIGHT WING OTBD AFT FLAP TE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FRAME CRACKED AT BS 480, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,763 hrs · 33,483 cycles

LEFT WING TE INBD FLAP DELAMINATED. REPAIRED FLAP IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 57,763 hrs · 33,483 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,763 hrs · 33,483 cycles

FRAME CRACKED AT BS 400, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 57,763 hrs · 33,483 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, RBL 41. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 57,763 hrs · 33,483 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, RBL 28.5. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,763 hrs · 33,483 cycles

LEFT WING LE SLAT, NOSE SKIN CRACKED ON LOWER SURFACE AT THE ACTUATOR RIB, SLAT STATION 451.97. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,763 hrs · 33,483 cycles

RIGHT WING LE NR 5 SLAT SKIN CRACKED ON LOWER SURFACE AT ACTUATOR RIB STATION 85.19. REPAIRED SLAT SKIN IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 54,136 hrs · 31,434 cycles

LEFT EMER EXIT BULLNOSE LIGHT LENS LOOSE BETWEEN ROW 11 TO 12. R & R LENS IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,085 hrs · 31,402 cycles

BULKHEAD CHORD CRACKED AT BS 540 BETWEEN STRINGER 22R TO 23R. REPAIRED CHORD IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,193 hrs · 30,320 cycles

RT EMERGENCY EXIT BULLNOSE LIGHT INOPERATIVE AT ROW 18. R & R LIGHT IAW MM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 51,061 hrs · 29,659 cycles

SEAT TRACK CRACKED AT BS 727B RBL 45.5 FWD OTBD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 51,061 hrs · 29,659 cycles

LT NR 3 FWD WINDOW POST CRACKED FASTENER HOLE NR 2 FROM BOTTOM, AT 3 & 9 O'CLOCK POSITION. REPAIRED POST IAW EA.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 51,061 hrs · 29,659 cycles

RT NR 3 FWD WINDOW POST CRACKED FASTENER HOLE NR 2 FROM BOTTOM, AT 3 & 9 O'CLOCK POSITION. REPAIRED POST IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 51,061 hrs · 29,659 cycles

SEAT TRACK CRACKED AT BS 727B RBL 45.5, FWD INBD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 51,060 hrs · 29,658 cycles

LT NR 3 FWD WINDOW POST FASTENER HOLE NR 4 FROM BOTTOM CRACKED AT 3 O'CLOCK POSITION. REPAIRED POST IAW SWA EA.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 51,060 hrs · 29,658 cycles

LT NR 3 FWD WINDOW POST FASTENER HOLE NR 5 FROM BOTTOM CRACKED AT 3 O'CLOCK POSITION. REPAIRED POST IAW SWA EA.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 51,060 hrs · 29,658 cycles

LT NR 3 FWD WINDOW POST FASTENER HOLE NR 3 FROM BOTTOM CRACKED AT 3 O'CLOCK & 9 O'CLOCK POSITION. REPAIRED POST IAW SWA EA.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 51,061 hrs · 29,659 cycles

RT NR 3 FWD WINDOW POST CRACKED FASTENER HOLE NR 3 FROM BOTTOM, AT 3 O'CLOCK POSITION. REPAIRED POST IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 51,061 hrs · 29,659 cycles

LT HORIZONTAL STABILIZER SKIN CRACKED AT OTBD STAB BS 92.70. REPAIRED SKIN IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,404 hrs · 29,281 cycles

RT EMERGENCY EXIT LIGHT BATTERIES FAILED TEST. R&R BATTERY PACKS IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,404 hrs · 29,281 cycles

LT EMERGENCY EXIT LIGHT BATTERIES FAILED TEST. R&R BATTERY PACKS IAW AMM.

Part: MOUNT — DAMAGED (L1 DOOR) · airframe 49,200 hrs · 28,588 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER AFT ATTACH BOLT DAMAGED. REMOVED & REPLACED MOUNT ASSY PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 48,138 hrs · 27,950 cycles

RIGHT AC BAY AFT BULKHEAD HORIZONTAL STIFFENER IS CRACKED. REMOVED AND REPLACED PER SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 48,138 hrs · 27,950 cycles

E&E COMPT LEFT FLOOR SUPPORT BRACKET CRACKED AT FASTENER LOCATED LEFT OF CENTER BETWEEN BS 312 TO 328. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,887 hrs · 27,799 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SLEEVE — DELAMINATED (THRUST REVERSER) · airframe 48,220 hrs · 28,007 cycles

NR 1 TR I/B TRANSLATING SLEEVE TRAILING EDGE OUTER SKIN DAMAGED/DELAMINATED 3/4" X 2 1/2 " MOD. REPAIRED NR 1 ENGINE I/B T/R TRANSLATING SLEEVE AS PER SEM 51-70-05-2R-1.

Part: LENS — BROKEN (EXIT SIGN) · airframe 47,307 hrs · 27,433 cycles

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

Part: SENSOR — CORRODED (E&E BAY) · airframe 47,123 hrs · 27,311 cycles

DECLARED EMERGENCY -- FLAP INDICATION UP (WITH SPLIT) FLAPS DID NOT EXTEND FOR APPROACH OR LANDING. REMOVED AND REPLACED NR 3 SENSOR AND NR 2, 3, 4, 5, 6, 7 AND 8 SKEW SENSOR CONNECTORS PER MM.

Part: STRUCTURE — CRACKED (RT HORIZ STAB) · airframe 46,941 hrs · 26,951 cycles

RIGHT HORIZONTAL STABILIZER CRACKED AT STA 101.9 9. REPAIRED STABILIZER IAW SRM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 45,270 hrs · 26,245 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,460 hrs · 25,764 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 44,407 hrs · 25,735 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,222 hrs · 25,629 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 44,222 hrs · 25,629 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED CHARGER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 44,189 hrs · 25,612 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 44,189 hrs · 25,612 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLIGHT DECK FIRST OFFICERS FWD I/B SEAT TRACK CRACKED. REMOVED AND REPLACED TRACK IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,189 hrs · 25,612 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME IAW EA.

Part: COVER — CRACKED (R2 DOOR) · airframe 42,510 hrs · 24,667 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE VIEWER COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: LENS — CRACKED (R2 DOOR) · airframe 42,510 hrs · 24,667 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE COVER LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 42,169 hrs · 24,472 cycles

FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: CONNECTOR — LOOSE (MLG) · airframe 41,168 hrs · 23,907 cycles

AIR TURNBACK / DECLARED EMERGENCY. AFTER TAKEOFF GEAR WOULD NOT COME UP. RECYCLED MANUAL GEAR. HORN WOULD NOT SILENCE WITH FLAPS RETRACTED. FOUND WHEEL WELL CONNECTOR NOT SECURED. SECURED CONNECTOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,334 hrs · 22,848 cycles

DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 15. RELAMPED PER MM.

Part: LIGHT — WORN (CABIN) · airframe 38,971 hrs · 22,638 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS WORN AT ROW 9. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 38,644 hrs · 22,446 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LIGHT — CORRODED (CABIN) · airframe 37,947 hrs · 22,020 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS CORRODED BETWEEN ROW 22 TO ROW 23. REMOVED AND REPLACED EEPLS PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 37,044 hrs · 21,498 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 548, LBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 37,044 hrs · 21,498 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 548, RBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 37,044 hrs · 21,498 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING OB/ AFT FLAP I/B AFT CORNER DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SPAR — CRACKED (CENTER WING) · airframe 37,044 hrs · 21,498 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING SECTION REAR SPAR WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB PER AAR EA.

Part: SPAR — CRACKED (CENTER WING) · airframe 37,044 hrs · 21,498 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING SECTION REAR SPAR WEB CRACKED AT BS 663, LBL 41. REPAIRED WEB PER AAR EA.

Part: SUPPORT — CRACKED (CARGO BAY) · airframe 37,044 hrs · 21,498 cycles

DURING SCHEDULED 10Y CHECK, FOUND BULKHEAD SUPPORT CRACKED AT BS 727, RBL 4, WL 163.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,044 hrs · 21,498 cycles

DURING SCHEDULED 10Y CHECK, FOUND EMERGENCY LIGHT INOP AT 12 DEF. RELAMPED PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 36,595 hrs · 21,229 cycles

FWD EMERGENCY EXIT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,736 hrs · 20,696 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,736 hrs · 20,696 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 35,072 hrs · 20,317 cycles

AN ODOR WAS PRESENT IN CABIN, SMELLED ELECTRIC/BURNT COFFEE ODOR. SHUTOFF RECIR/GASPER FAN, SMELL WENT AWAY IMMEDIATELY. NO REOCCURRENCE OF SMELL. REMOVED AND REPLACED GASPER FAN PER MM.

Part: WEDGE — BROKEN (RT WING SLAT) · airframe 34,673 hrs · 20,084 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT WING NR 4 SLAT UPPER T/E WEDGE INBD CORNER BROKEN. REMOVED AND REPLACED SLAT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,802 hrs · 18,934 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,165 hrs · 18,558 cycles

DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,165 hrs · 18,558 cycles

DURING SCHEDULED HC2 CHECK, RIGHT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,165 hrs · 18,558 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,165 hrs · 18,558 cycles

DURING SCHEDULED HC2 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 32,165 hrs · 18,558 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,977 hrs · 17,228 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 15 TO RBL 25. REPAIRED FLOORBEAM PER ER.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 23,266 hrs · 13,418 cycles

DECLARED EMERGENCY, NR 2 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED ALONG WITH "B" SYSTEM HYDRAULIC FAILURE. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,355 hrs · 12,880 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 6 ABC. RELAMPED LIGHT PER MM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 22,201 hrs · 12,805 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (LT WING FLAP) · airframe 18,469 hrs · 10,734 cycles

DURING SCHEDULED 5Y CHECK, FOUND LT WING INBOARD AFT T/E FLAP CRACKED. REPAIRED LT WING INBOARD AFT FLAP PER SRM.

Part: DOOR — OUT OF ADJUST (L1) · airframe 16,394 hrs · 9,568 cycles

AIRTURN BACK, AFTER TAKEOFF FAILED TO PRESSURIZE AND THERE WAS A LOUD AIR NOISE AROUND L1 DOOR AREA. DOOR HANDLE WAS DOWN AND L1 DOOR LIGHT WAS OUT. ADJUSTED L1 DOOR PER MM.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 13,570 hrs · 8,001 cycles

FWD ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATION OUT OF LIMITS. REMOVED AND REPLACED FWD ENTRY DOOR SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 10,746 hrs · 6,378 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: COVER — BROKEN (CABIN) · airframe 10,159 hrs · 6,064 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS COVERS BROKEN AT ROW NR 1 AND 11. REMOVED AND REPLACED COVERS PER MM.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 9,925 hrs · 5,917 cycles

AIR TURNBACK, L/E FLAP TRANSIT LIGHT REMAINED ON WITH ALL L/E DEVICES EXTENDED. REMOVED AND REPLACED NR 1, 6, 7 AND 8 L/E SLAT ACTUATORS PER MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 7,863 hrs · 4,766 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT PRESS BULKHEAD OIL CANNED, BS 1016, FIRST CIRCUMFERENTIAL STRAP. MX FERRY TO PAE, REPAIRED BULKHEAD PER SRM.

Part: WIRE — EXPOSED (CABIN) · airframe 4,516 hrs · 2,776 cycles

EEPLS WIRING EXPOSED AT OVERWING EXIT. SECURED WIRING PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 4,526 hrs · 2,783 cycles

EEPLS WIRING EXPOSED AT OVERWING EXIT. SECURED EEPLS WIRING PER MM.

Part: ROD — BROKEN (SPOILER) · airframe 4,236 hrs · 2,582 cycles

AIR TURNBACK - DURING TAKEOFF, RECEIVED T/O CONFIG WARNING, GEAR HANDLE WOULD NOT RETRACT AND A/C WOULD NOT PRESSURIZE. MX FERRY TO PHX. REMOVED AND REPLACED SPOILER INTERLOCK VALVE ROD ASSY PER MM.

Part: GIRT BAR — OUT OF ADJ (PAX DOOR SLIDE) · airframe 2,003 hrs · 1,213 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUSTMENT. REINSTALLED SLIDE ASSY PER MM.