N754SW

Part: FAIRING — DAMAGED (LT NACELLE) · airframe 78,673 hrs · 46,589 cycles

FOUND 2 LOCK FASTENER HOLES ON THE LT STRUT FAIRING ELONGATED ON THE LT SIDE. REPAIRED THE DAMAGEIAW EA 22-154-03528.

Part: PANEL — DAMAGED (NOT REPORTED) · airframe 78,152 hrs · 46,238 cycles

193B FASTENER HOLES AT POSITIONS 7; 8; 18; 20; 25; 26 AND 33 HAVE BEEN ELONGATED. 193B FASTENER HOLES AT POSITIONS 7 8 18 20 25 26 AND 33 HAVE BEEN ELONGATED. / [01] PANEL REPLACED ON N/R TTG8Q00F0UYM;[02] C/W

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 78,089 hrs · 46,199 cycles

L1 DOOR SLIDE NEEDS REPOSITIONED / [01] REPOSITIONED L1 DOOR SLIDE PER S.I.P.

Part: COVER — LOOSE (R2 DOOR) · airframe 77,728 hrs · 45,959 cycles

RIGHT AFT ESCAPE SLIDE PULL STRAP IS NOT SECURED. / [01] RESECURED AFT RH ESCAPE SLIDE PULL STRAP COVER AS REQUIRED PER SIP.

Part: MEGAPHONE — FAILED (FWD GALLEY) · airframe 77,046 hrs · 45,498 cycles

FWD GALLEY MEGAPHONE BATTERY IS DEPLETED / [01] R&R FWD MEGAPHONE AS NEEDED AMM 25-64-00. OPS CHK GOOD.

Part: MEGAPHONE — FAILED (FWD GALLEY) · airframe 77,046 hrs · 45,498 cycles

FWD GALLEY MEGAPHONE BATTERY IS DEPLETED / [01] R&R FWD MEGAPHONE AS NEEDED AMM 25-64-00. OPS CHK GOOD.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,935 hrs · 44,224 cycles

CRACK LEADING EDGE SKIN ACCESS PANEL 341B AT STA 95.96 AT RT HORIZONTAL STABILIZER (1 EA) ; 2021-368797 / [01] TOOK MEASURES OF CRACK RIB LEADING EDGE SKIN ACCESS PANEL 241B AT STA 95.96 RT HORIZONTAL STABILIZER MEASURES ARE: L:0.245 TOOL USED IS CALIPER P/N: 500-197-30 ; S/N: 15242824 DUE DATE: 17-JUN-22.; [02] REMOVED RIB LEADING EDGE SKIN ACCESS PANEL 341B AT STA 95.96 AT RT HORIZONTAL STABILIZER (1 EA) AND PERFORMED VISUAL INSPECTION AREA AND NOT FOUND MORE DAMAGE.; [03] COMPLETED STEP 1 AND 2; [04] EXACTLY LOCATION OF CRACK IS ON RIB STA 95.96 AT LEADING EDGE ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER; [05] STEP 4 COMPLETED.; [06] PERFORMED DRILL ON NEW RIB STA 95.96 AT LEADING EDGE ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER AND APPLIED PROTECTIVE TREATMENT ON HOLES IAW B737-700 SRM 51-40-05 AND SRM 51-20-01; [07] OK TO INSTALL NEW RIB AND FASTENER ON STA 95.96 AT LEADING EDGE ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER GRANTED; [08] STEP 6 AND 7 COMPLETED; RII.<BR><BR>OK TO INSTALL GRANTED.; [09] INSTALLED NEW RIB AND FASTENER ON STA 95.96 AT LEADING EDGE ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 ;SRM 51-10-02 ITEM 9 AND DWG 186A1001 REV: A; [10] STEP 9 COMPLETED RII; [11] REPLACED RIB ON STA 95.96 AT LEADING EDGE ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 ;SRM 51-10-02 ITEM 9 AND DWG 186A1001 REV: A P/N USED 186A1352-6 PO 2021 184921 1; [12] JOB COMPLETED AS RII.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,935 hrs · 44,224 cycles

CRACK LEADING EDGE SKIN ACCESS PANEL 341B AT STA 105.26 AT RT HORIZONTAL STABILIZER (1 EA) ; 2021-368798 / [01] TOOK MEASURES OF CRACK RIB LEADING EDGE SKIN ACCESS PANEL 241B AT STA 105.26 AT RT HORIZONTAL STABILIZER MEASURES ARE: L:0.235 TOOL USED IS CALIPER P/N: 500-197-30 ; S/N: 15242824 DUE DATE: 17-JUN-22.; [02] REMOVED RIB LEADING EDGE SKIN ACCESS PANEL 341B AT STA 105.26 AT RT HORIZONTAL STABILIZER (1 EA) AND PERFORMED VISUAL INSPECTION AREA AND NOT FOUND MORE DAMAGE.; [04] EXACTLY LOCATION OF CRACK IS ON RIB STA 105.26 AT LEADING EDGE ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER; [05] STEP 4 COMPLETED.; [06] PERFORMED DRILL ON NEW RIB LOCATED AT STA 105.26 AT LEADING EDGE ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER AND APPLIED PROTECTIVE TREATMENT ON HOLES IAW B737-700 SRM 51-40-05 AND SRM 51-20-01; [09] INSTALLED NEW RIB AND FASTENER LOCATED AT STA 105.26 AT LEADING EDGE ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 ;SRM 51-40-02 AND DWG 186A1001 REV: A; [11] REPLACED RIB STA 105.26 AT LEADING EDGE ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 ;SRM 51-40-02 ;DWG 186A1001 REV: A AND DWG 186A1304 REV: - P/N USED 186A1352-8 PO 2021 184775 1; [12] REPLACED RIB STA 105.26 AT LEADING EDGE ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 ;SRM 51-40-02 ;DWG 186A1001 REV: A AND DWG 186A1304 REV: - P/N USED 186A1352-8 PO 2021 184775 1. RII

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,935 hrs · 44,224 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-368760 / [01] TOOK MEASURE OF CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IS L: 0.452 AND NO FOUND ALLOWABLE DAMEGE ON SRM MUST BE REPAIR .; [07] PERFORMED CUT AND REMOVED THE DAMAGE FROM LOWER CORD OF THE INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER. I.A.W B737-700 SRM 55-10-09-2R-5 REPAIR 5 AND PERFORMED VISUAL INSPECTION AND NOT FOUND MORE DAMEGE .; [11] MARKED HAND LAY OUT ON REPAIR AREA INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5REPAIR 5 FIGURE 204; [13] MADE AND DRILLED REPAIR PARTS T-SECTION (1E/A) ANGLE (1E/A) AND SHIM (2E/A) AND FILLER (1E/A) OF INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 TABLE 201 FIGURE 204. AND SRM 51-40-05. [19] INSTALLED REPAIR PARTS T-SECTION (1E/A) ANGLE (1E/A) AND SHIM (2E/A) AND FILLER (1E/A) AND FASTENERS ON INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 TABLE 201 FIGURE 204; AND B737-700 SRM 51-40-02; [20] REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 TABLE 201 FIGURE 204; [21] CERTIFIED STEP 19 RII

Part: ANGLE — CRACKED (APU INLET) · airframe 74,935 hrs · 44,224 cycles

CRACK ON ANGLE AT PLENUM RT APU AIR INLET ; 2021-368759 / [01] REMOVED ANGLE AND FASTENERS AT PLENUM RT APU AIR INLET IAW B737-700 SRM 51-40-02 AND PERFORMED VISUEL INSPECTION AND NOT FOUND MORE DAMAGE ON ADJACENT AREA AND DUE TO NOT FOUN ALLOWABLE DAMAGE ANGLE MUST BE REPLACED; [02] STEP 1 COMPLETE; [03] PERFORMED DRILL HOLES ON NEW ANGLE AT PLENUM RT APU AIR INLET IAW B737-700 SRM 51-40-05 AND OK TO INSTALL NEW ANGLE GRANTED.; [04] STEP 3 COMPLETE; [05] INSTALLED NEW ANGLE AND FASTENERS LOC AT PLENUM RT APU INLET. IAW B737-700 SRM 51-40-02 AND DWG #353A2010 SHEET 8 REV _.; [06] REPLACED ANGLE LOC. AT PLENUM RT APU AIR INLET. IAW B737-700 SRM 51-40-02 AND DWG # 353A2010 SHEET 8 REV _.; [07] STEP 5 COMPLETED.; [08] JOB COMPLETED.

Part: SPAR — CORRODED (LT WING) · airframe 74,935 hrs · 44,224 cycles

CORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROX; LOWER AREA AT LT WING ; 2021-368745 / [01] TOOL USED/ EDDY CURRENT PN/ NORTEC 600D; SN/ 2000053402; DUE DATE/ 23APR22.; [02] TOOL USED: ULTRASONIC THICKNESS GAUGE ; PN/ 25DL PLUS;SN/ 071504410; DUE DATE/ 20NOV21; [03] TOOL USED : CALIPER P/N:700-113-10 S/N:0016656 DUE DATE: 11-MAY-22; [04] TOOL USED CALIPER P/N :500-464 S/N : 15331936 DUE DATE : 05-OCT-21; [05] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 500D; S/N: N500X1693P030456 DUE DATE: 30-NOV-21.; [06] REPAIRED FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROX; LOWER AREA AT LT WING IAW EA 21-157-02490; [07] STEP 6 CORRECTED <BR>REFER TO FAULT TTG8Q00617WM WHERE EA 21-157-02490 WAS ADDED AS A SUBTASK.; [08] TASK CARD COMPLETED; [09] TASK CARD COMPLETED<BR>RII

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 74,935 hrs · 44,224 cycles

CRACK FRONT SPAR SUPPORT ANGLE LOCATED AT IFSS 120 AT LT WING ; 2021-368744 / [01] REMOVED SUPPORT ANGLE LOCATED FRONT SPAR WEB AT IFSS 120 AT LT WING IAW B737-700 SRM 51-40-02 DUE TO NOT FOUND ALLOWBLE DAMAGE IN SRM SUPPORT ANGLE MUST BE REPLACED ; CRACK LENGTH IS : 0.620 TOOL USED : DIGITAL CALIPER P/N:500-197-20 S/N:12141486 DUE DATE:03-JAN-22 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NOT FOUND DAMAGE; [02] STEP 1 COMPLETE; [03] MACHINED ANGLE SUPPORT (1 E/A) MATERIAL USED 7050T7451 AMS 4050 IAW 737-700 SRM 57-20-10-1A-3 AND DWG 116A3939 REV B TOOL USED DIGITAL CALIPER P/N 500-193-30 S/N 0000285 DUE DATE 22-NOV-21.; [14] INSTALLED SUPPORT ANGLE AND FASTENERS LOCATED FRONT SPAR WEB AT IFSS 120 AT LT WING. IAW B737-700 SRM 57-20-10-1A-3 ALLOWABLE DAMAGE 3 AND DWG # 116A3001 REV:-; [15] STEP 14 COMPLETED AND CERTIFIED AS RII.; [27] PERFORMED FUEL LEAK CHECK (11 EA FASTENERS EXTERNAL AREA) FRONT SPAR SUPPORT ANGLE LOCATED AT IFSS 120 AT LT WING IAW B737-700 AMM 28-11-00-300-803 AND AMM 28-11-00-790-801 STEP 4.N NOT FOUND LEAK; [28] STEP 27 CERTIFIED; [30] REPLACED SUPPORT ANGLE LOCATED FRONT SPAR WEB AT IFSS 120 AT LT WING. IAW B737-700 SRM 57-20-10-1A-3 ALLOWABLE DAMAGE 3 AND DWG # 116A3001 REV:- MATERIAL USED 7050T7451 AMS4050 PO 0 0 0 BATCH 201953125200102.. RII ITEM

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 74,935 hrs · 44,224 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARMENT ; 2021-368743 / [01] WELDED CRACKS LOCATED AT FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. STEP (4) AND BAC 5975 WELD ROD USED: AMS 4190K P.O. 2021 118316; [02] REPAIRED BY WELD FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. AND BAC 5975 TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N 15120589; DUE DATE 14/SEP/21; [03] REPAIRED BY WELD FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. AND BAC 5975 TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N 15120589; DUE DATE 14/SEP/21

Part: SUPPORT ANGLE — CRACKED (AFT GALLEY DOOR) · airframe 74,935 hrs · 44,224 cycles

CRACK ANGLE - SUPPORT ON ACCESS PANEL 834DZ AFT ENTRY DOOR AT AFT GALLEY AREA ; 2021-368699 / [01] REMOVED ANGLE LOC. ON ACCESS PANEL 834DZ AFT ENTRY DOOR AT AFT GALLEY AREA IAW 737-700 SRM 51-40-02 ANGLE MUST BE REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS AND VISUAL INSPECTION AND NOT FOUND ADDITIONAL DAMAGE.; [02] DRILLED NEW ANGLE LOC. ON ACCESS PANEL 834DZ AFT ENTRY DOOR AT AFT GALLEY AREA IAW 737-700 SRM 51-40-05; APPLIED PROTECTIVE TREATMENT ON NEWS HOLES IAW B737-700 SRM 51-20-01 AND OK TO INSTALL.; [03] STEP 1 AND 2 COMPLETE; [04] INSTALLED ANGLE LOC. ON ACCESS PANEL 834DZ AFT ENTRY DOOR AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 411A2119 SHEET 72 REV-.; [05] REPLACED ANGLE LOC. ON ACCESS PANEL 834DZ AFT ENTRY DOOR AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 411A2119 SHEET 72 REV-.; [06] STEP 4 COMPLETED; [07] TASK CARD COMPLETED

Part: SUPPORT ANGLE — CRACKED (R2 DOOR) · airframe 74,935 hrs · 44,224 cycles

CRACK ANGLE - SUPPORT ON ACCESS PANEL 844DZ AFT SERVICE DOOR AT AFT GALLEY AREA ; 2021-368698 / [01] REMOVED ANGLE LOC. ON ACCESS PANEL 844DZ AFT SERVICE DOOR AT AFT GALLEY AREA IAW 737-700 SRM 51-40-02 ANGLE MUST BE REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS AND VISUAL INSPECTION AND NOT FOUND ADDITIONAL DAMAGE.; [02] DRILLED NEW ANGLE LOC. ON ACCESS PANEL 844DZ AFT SERVICE DOOR AT AFT GALLEY AREA IAW 737-700 SRM 51-40-05; APPLIED PROTECTIVE TREATMENT ON NEWS HOLES IAW B737-700 SRM 51-20-01 AND OK TO INSTALL.; [03] STEP 1 AND 2 COMPLETE; [04] INSTALLED ANGLE LOC. ON ACCESS PANEL 844DZ AFTSERVICE DOOR AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 411A2119 SHEET 72 REV-.; [05] REPLACED ANGLE LOC. ON ACCESS PANEL 844DZ AFT SERVICE DOOR AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 411A2119 SHEET 72 REV-.; [06] STEP 4 COMPLETED; [07] TASK CARD COMPLETED

Part: STUB FRAME — CRACKED (BS 294 S9R) · airframe 74,935 hrs · 44,224 cycles

CRACK ON STUB FRAME LOCATED AT BS 294.5 AT LEVEL STR 9R FWD GALLEY DOOR AREA ; 2021-368691 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 21-JAN-22; [02] REPLACED STUB FRAME LOC. BS 294.5 AT LEVEL STR 9R FWD GALLEY DOOR IAW B737-700 SRM 51-40-02 AND DRAWING # 141A8370 REV. D.; [03] CERTIFIED RII WORK PERFORMED.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 74,935 hrs · 44,224 cycles

CUSTOMER REQUEST CRACK SCUFF PLATE AFT CORNER FWD ENTRY DOOR AT FWD GALLEY AREA ; 2021-368688 / [01] EVALUATED AFT CORNER SCUFF PLATE AT FWD ENTRY DOOR GALLEY AREA FOUND CRACK (1EA) MEASURE IS:L=01450 INCH;THE CRACK IS WITHIN LIMIT OF REPAIR IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2.TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189526;DUE DATE:22-NOV-21.; [02] VERIFIED STEP 1; [03] WELDED CRACK LOCATED ON SCUFF PLATE AFT CORNER FWD ENTRY DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B STEPS (3) AND (4) FIGURE 203 AND BAC 5975 USING AMS 4954 WELD ROD.; [04] VERIFIED STEP 3; [05] PERFORMED LIQUID PENETRANT INSPECTION ON SCUFF PLATE AFT CORNER FWD ENTRY DOOR WELDED AREAS AS PER BSOPM 20-20-02 NO CRACKS WERE FOUND.; [06] APPLIED ONE LAYER OF BMS 10-11 TYPE 1 PRIMER ON THE INNER SURFACES OF THE SCUFF PLATE AFT CORNER FWD ENTRY DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B STEPS (6)(8).; [07] VERIFIED STEP 6; [08] REPAIRED SCUFF PLATE AFT CORNER FWD ENTRY DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B AND BAC 5975.; [09] REPAIRED SCUFF PLATE AFT CORNER FWD ENTRY DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B AND BAC 5975.

Part: SCUFF PLATE — CRACKED (PAX DOOR) · airframe 74,935 hrs · 44,224 cycles

CUSTOMER REQUEST CRACK SCUFF PLATE FWD CORNER FWD ENTRY DOOR AT FWD GALLEY AREA ; 2021-368687 / [01] EVALUATED SCUFF PLATE FWD CORNER FWD ENTRY DOOR AT FWD GALLEY AREA FOUND CRACK (1EA) MEASURE IS:L=0.4300 INCH.THE CRACK MUST BE REPAIR IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2.TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189526;DUE DATE:22-NOV-21.; [02] VERIFIED STEP 1; [03] WELDED CRACK LOCATED ON SCUFF PLATE FWD CORNER FWD ENTRY DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B STEPS (3)(4) FIGURE 203 AND BAC 5975 USING AMS 4954 FILLER ROD.; [04] VERIFIED STEP 3; [05] PERFORMED LIQUID PENETRANT INSPECTION ON SCUFF PLATE; FWD CORNER FWD ENTRY DOOR AREA ON WELDED AREAS AS PER BSOPM 20-20-02 NO CRACKS WERE FOUND.; [06] APPLIED ONE LAYER OF BMS 10-11 TYPE 1 PRIMER TO THE INNER SURFACES OF THE SCUFF PLATE FWD CORNER FWD ENTRY DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B STEPS (6)(8).; [07] VERIFIED STEP 6; [08] REPAIRED SCUFF PLATE FWD CORNER FWD ENTRY DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B AND BAC 5975.; [09] REPAIRED SCUFF PLATE FWD CORNER FWD ENTRY DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B AND BAC 5975.

Part: ANGLE — CRACKED (BS 827 S25R) · airframe 74,935 hrs · 44,224 cycles

CRACK ANGLE - SUPPORT LOCATED BS 827 STR 25R AT AFT CARGO COMPARTMENT ; 2021-368685 / [01] REMOVED ANGLE - SUPPORT LOCATED BS 827 STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0; ANGLE SUPPORT MUST BE REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM B737-700 AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND MORE DAMAGE.; [02] STEP 1 COMPLETE; [03] DRILLED NEW ANGLE - SUPPORT LOCATED BS 827 STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-05-0G-0 AND APPLIED PROTECTIVE TREATMENT ON OPENED HOLES IAW B737-700 SRM 51-20-01-0G-0.; [04] DRILLED NEW ANGLE - SUPPORT LOCATED BS 827 STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-05-0G-0 AND APPLIED PROTECTIVE TREATMENT ON OPENED HOLES IAW B737-700 SRM 51-20-01-0G-0. COMPLIED WITH STEP 3 <BR>RII; [05] OBTAINED OK TO INSTALL NEW ANGLE - SUPPORT AND FASTENERS LOCATED BS 827 STR 25R AT AFT CARGO COMPARTMENT; [06] COMPLIED WITH STEP 5 . OK TO INSTALL NEW ANGLE<BR>RII; [07] INSTALLED ANGLE-SUPPORT AND FASTENERS LOCATED BS 827 STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A8120 SHEET 10 REV A: AND DWG 146A8120 SHEET 11 REV A:; [08] COMPLETED STEP 7 RII; [09] REPLACED ANGLE-SUPPORT LOCATED BS 827 STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A8120 SHEET 10 REV A: AND DWG 146A8120 SHEET 11 REV A: PART NUMBER USED: 146A8125U13 PO: 2021 184959; [10] VERIFIED STEP 9; TASK COMPLETE; [11] CORRECTED STEP 10: VERIFIED STEP 9; TASK COMPLETE RII

Part: SCUFF PLATE — CRACKED (FWD SERVICE DOOR) · airframe 74,935 hrs · 44,224 cycles

CUSTOMER REQUEST CRACK SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA ; 2021-368684 / [01] EVALUATED SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA FOUND CRACKS (4EA) MEASURES ARE #1=1.4390 INCH;#2=2.2750 INCH;#3=2.5025 INCH;#4=1.8400 INCH;THESES CRACKS MUST BE REPAIR IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2.TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189526;DUE DATE:22-NOV-21.; [02] VERIFIED STEP 1; [03] WELDED CRACKS (4EA) LOCATED ON SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B STEPS (3)(4) FIGURE 203 AND BAC 5975 USING AMS 4954 FILLER ROD.; [04] VERIFIED STEP 3; [05] PERFORMED LIQUID PENETRANT INSPECTION ON SCUFF PLATE; FWD SERVICE DOOR AT FWD GALLEY AREA ON WELDED AREAS AS PER BSOPM 20-20-02 NO CRACKS WERE FOUND.; [07] APPLIED ONE LAYER OF BMS 10-11 TYPE 1 PRIMER OF THE INNER SURFACE OF THE SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B STEPS (6)(8).; [08] VERIFIED STEP 7; [09] REPAIRED SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B AND BAC 5975.; [10] REPAIRED SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B AND BAC 5975.

Part: ANGLE — CRACKED (BS 907-927) · airframe 74,935 hrs · 44,224 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS 907 TO BS 927 AND STR 27R TO STR 25R FWD POSITION AFT CARGO COMPARTMENT ; 2021-368686 / [01] TOOK MEASURE OF CRACK ON SUPPORT ANGLE: L=5.854 TOOL USED: CAPLIPER P/N: DIGITAL 150; S/N: AE-412597; DUE DATE: 25-MAY-22 NOT FOUND ALLOWABLE DAMAGE IN SRM SUPPORT ANGLE MUST BE REPLACED; [02] REMOVED ANGLE - SUPPORT LOCATED BETWEEN BS 907 TO BS 927 AND STR 27R TO STR 25R FWD POSITION AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AND NOT FOUND MORE DAMAGE; [03] COMPLETED STEP 1 AND 2; [04] FORMED AND DRILLED SUPPORT ANGLE LOC BTW BS 907 TO BS 927 AND STR 27R TO STR 25R FWD POSITION AFT CARGO COMPARTMENT MATERIAL USED EXTRUSION BAC 1493-318 PO #2021 186690 IAW B737-700 SRM 51-40-05 AND DRAWING 147A7221 SHEET 17 REV D.; [10] INSTALLED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 907 TO BS 927 AND STR 27R TO STR 25R FWD POSITION AFT CARGO COMPARTMENT IAW B737- 700 SRM 51-40-02 AND DWG 147A7221 SHEET 71 REV D.; [11] CERTIFIED STEP 10<BR>RII; [12] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 907 TO BS 927 AND STR 27R TO STR 25R FWD POSITION AFT CARGO COMPARTMENT IAW B737- 700 SRM 51-40-02 AND 51-10-02 AND DWG 147A7221 SHEET 71 REV D.; [13] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 907 TO BS 927 AND STR 27R TO STR 25R FWD POSITION AFT CARGO COMPARTMENT IAW B737- 700 SRM 51-40-02 AND 51-10-02 AND DWG 147A7221 SHEET 71 REV D.<BR>TASK COMPLETED RII

Part: SUPPORT ANGLE — CRACKED (BS 907-927) · airframe 74,935 hrs · 44,224 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS 907 TO BS 927 AND STR 25R TO STR 27R AFT POSITION AFT CARGO COMPARTMENT ; 2021-368689 / [01] TOOK MEASURE OF CRACK ON SUPPORT ANGLE: L=3.465 TOOL USED: CAPLIPER P/N: DIGITAL 150; S/N: AE-412597; DUE DATE: 25-MAY-22 NOT FOUND ALLOWABLE DAMAGE IN SRM SUPPORT ANGLE MUST BE REPLACED; [02] REMOVED ANGLE - SUPPORT LOCATED BETWEEN BS 907 TO BS 927 AND STR 27R TO STR 25R AFT POSITION AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AND NOT FOUND MORE DAMAGE; [05] FORMED AND DRILLED SUPPORT ANGLE LOC BTW BS 907 TO BS 927 AND STR 25R TO STR 27R AFT POSITION AFT CARGO COMPARTMENT MATERIAL USED EXTRUSION BAC 1493-318 PO #2021 186690 IAW B737-700 SRM 51-40-05 AND DRAWING 147A7221 SHEET 17 REV D.; [06] APPLIED PROTECTIVE TREATMENT ON SUPPORT ANGLE IAW B737-700 SRM 51-20-01; [11] INSTALLED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 907 TO BS 927 AND STR 25R TO STR 27R AFT POSITION AFT CARGO COMPARTMENT IAW B737- 700 SRM 51-40-02 AND DWG 147A7221 SHEET 71 REV D.; [12] CERTIFIED STEP 11<BR>RII; [13] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 907 TO BS 927 ANDSTR 25R TO STR 27R AFT POSITION AFT CARGO COMPARTMENT IAW B737- 700 SRM 51-40-02 AND 51-10-02 AND DWG 147A7221 SHEET 71 REV D.; [14] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 907 TO BS 927 ANDSTR 25R TO STR 27R AFT POSITION AFT CARGO COMPARTMENT IAW B737- 700 SRM 51-40-02 AND 51-10-02 AND DWG 147A7221 SHEET 71 REV D.<BR>TASK COMPLETED RII

Part: BRACKET — CRACKED (FAN COWL) · airframe 74,935 hrs · 44,224 cycles

CRACK OUTBOARD FAN COWL SUPPORT BRACKET LOC. INTERNAL AREA ACCESS DOOR 424AR ON ENGINE 2 ; 2021-368631 / [01] MEASURED OF CRACK OUTBOARD FAN COWL SUPPORT BRACKET LOC. INTERNAL AREA ACCESS DOOR 424AR ON ENGINE 2. L: 0.625 INCH TOOL USED P/N: 500-172-30; S/N: 15237811; DUE DATE: 11MAY22; [02] REMOVED OUTBOARD FAN COWL SUPPORT BRACKET LOC. INTERNAL AREA ACCESS DOOR 424AR ON ENGINE 2 DUE TO NOT FOUND ALLOWABLE DAMAGE IN STM B737-700 FOR CRACK ON SUPPORT BRACKET MUST BE REPLACE AND PERFORMED VISUAL INSPECTION NOT FOUND MORE DAMAGE; [03] STEP 1 AND STEP 2 COMPLETE; [06] INSTALLED OUTBOARD FAN COWL SUPPORT BRACKET LOC. INTERNAL AREA ACCESS DOOR 424AR ON ENGINE 2 IAW CMM 71-13-30; [07] STEP 6 COMPLETED; [08] CORRECTED STEP 2 REMOVED OUTBOARD FAN COWL SUPPORT BRACKET LOC. INTERNAL AREA ACCESS DOOR 424AR ON ENGINE 2 IAW B737-700 SRM 51-40-02. DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM B737-700 FOR CRACK ON SUPPORT BRACKET MUST BE REPLACE AND PERFORMED VISUAL INSPECTION NOT FOUND MORE DAMAGE; [09] STEP 8 COMPLETE; [10] REPLACED OUTBOARD FAN COWL SUPPORT BRACKET LOC. INTERNAL AREA ACCESS DOOR 424AR ON ENGINE 2 IAW CMM 71-13-30 AND SRM 51-40-02 P/N USED 314-2259-4 PO 2021-183887 1; [11] REPLACED OUTBOARD FAN COWL SUPPORT BRACKET LOC. INTERNAL AREA ACCESS DOOR 424AR ON ENGINE 2 IAW CMM 71-13-30 AND SRM 51-40-02 P/N USED 314-2259-4 PO 2021-183887 1 TASK COMPLETED

Part: BEAR STRAP — CRACKED (BS 293) · airframe 74,935 hrs · 44,224 cycles

CRACK INDICATION FOUND AROUND FASTENERS ON BEAR STRAP (2EA) LOCATED BETWEEN BS 293 TO BS 293.5 AND BETWEEN STR 8 AND STR 9 RH SIDE IN FWD GALLEY AREA LENGTH (1) CRACK 0.260 INCH; LENGTH (2) CRACK IS 0 ; 2021-368567 / [01] TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022240; DUE DATE: 01-DEC-21.; [02] TOOL USED PN: NORTEC 600D; SN: 210138503; CAL DUE DATE: 05-MAR-22; [03] TOOL USED CALIB PIE DE REY P/N : DIGITAL 150 S/N : AE- 412599 DUE DATE : 21-MAY-22; [04] TOOL USED: MICROMETER P/N: 293-831; S/N: 35031311; DUE DATE: 18-AUG-21; SMALL HOLE GAUGES P/N: 154-901; S/N: AE-412972; DUE DATE: 28-JUL-22; [05] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22.; [06] TOOL USED CALIPER PN: 500-172-20 SN: B21015879 DUE DATE : 10-AUG-22; [07] ULTRASOUND MEASURED ON AFFECTED AREA OF BEARSTRAP IAW NDT MANUAL PART 4 51-00-00 PROCEDURE 3 THICKNESS= 0.090 INCH. TOOL USED ULTRASONIC GAGE P/N: 45MG; S/N: 130060401; DUE DATE: 22-APR-22.; [08] TOOL USED: BENCH TOP SCALE P/N: DSY-1100 ; S/N: 37057 DUE DATE : 07-MAY-22; [09] REPAIRED BEAR STRAP LOCATED BETWEEN BS 293 TO BS 293.5 AND BETWEEN STR 8 AND STR 9 RH SIDE IN FWD GALLEY AREA IAW EA 21-153-02363; [10] TASK CARD COMPLETED <BR>RII

Part: RIB — CRACKED (VERTICAL STAB) · airframe 74,935 hrs · 44,224 cycles

CRACK DORSAL FIN RIB FWD POSITION AT VERTICAL STABILIZER ; 2021-368570 / [01] REMOVED RIB LOC. DORSAL FIN FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 DUE TO NOT FOUND ALLOWED DAMAGE ON SRM ; RIB MUST BE REPLACED CRACK LENGTH IS : 0.625 TOOL USED : CALIPER P/N: DIGITAL 150 S/N: AE-412007 DUE DATE : 21-JUN-22 AND PERFORMED VISUAL INPECTION ON AREA AND NOT FOUND ADDITIONAL DAMAGE; [02] REMOVED BRACKET (2E/A) AND FILLER (2E/A) LOC. ON RIB DORSAL FIN FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INPECTION AND NOT FOUND ADDITIONAL DAMAGE; [04] STEPS 2 AND 3 COMPLETED.; [05] OK TO INSTALL RIB; BRACKET (2E/A); FILLER (2E/A) AND FASTENERS LOC. DORSAL FIN FWD POSITION AT VERTICAL STABILIZER; [06] STEP 5 COMPLETED; [07] STEP 5 COMPLETED RII ITEM; [08] INSTALLED RIB; BRACKET (2E/A); FILLER (2E/A) AND FASTENERS LOC. DORSAL FIN FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A0103 REV A. AND DWG 174A1008 REV -; [09] REPLACED DORSAL FIN RIB FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 174A0103 REV A; DWG 174A1008 REV -; [10] STEP 8 COMPLETED <BR>RII; [11] TASK CARD COMPLETED<BR>RII

Part: SUPPORT ANGLE — CRACKED (BS 540) · airframe 74,935 hrs · 44,224 cycles

CRACK SUPPORT ANGLE LOCATED ON BS540 AND BL0 TO LBL24.5 AT PASSENGER CABIN ; 2021-368610 / [01] REPLACED SUPPORT ANGLE LOCATED ON BS540 AND BL0 TO LBL24.5 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 STEP 9 ; SRM 51-40-02 AND DWG 143A5240 SHEET 1 REV -; [02] REPLACED SUPPORT ANGLE LOCATED ON BS540 AND BL0 TO LBL24.5 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 STEP 9 ; SRM 51-40-02 AND DWG 143A5240 SHEET 1 REV - (UPDATED CORRECTIVE ACTION TO ADD PART INSTALLED); [03] CORRECTED STEP 1 AND 2 REMOVED SUPPORT ANGLE LOCATED ON BS540 AND BL0 TO LBL24.5 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AND NOT FOUND MORE DAMAGE; [04] DRILLED NEW SUPPORT ANGLE LOCATED ON BS540 AND BL0 TO LBL24.5 AT PASSENGER CABIN IAW B737-700 SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT ON HOLES IAW B737-700 SRM 51-20-01; [05] OK TO INSTALL NEW SUPPORT ANGLE LOCATED ON BS540 AND BL0 TO LBL24.5 AT PASSENGER CABIN AND FASTENERS; [06] INSTALLED NEW SUPPORT ANGLE LOCATED ON BS540 AND BL0 TO LBL24.5 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A5240 SHEET 1 REV -; [07] REPLACED SUPPORT ANGLE LOCATED ON BS540 AND BL0 TO LBL24.5 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 STEP 9; SRM 51-40-02 AND DWG 143A5240 SHEET 1 REV -; [08] STEP 3 VERIFIED AND NO FOUND MORE DAMAGE; [09] STEP 4; 5; 6 AND 7 VERIFIED; RII ACCOMPLISHED AND TASK COMPLETED

Part: SUPPORT ANGLE — CRACKED (BS 695) · airframe 74,935 hrs · 44,224 cycles

CRACK SUPPORT ANGLE LOCATED BS 695 AND BL0 LH SIDE AT PASSENGER CABIN ; 2021-368563 / [01] REMOVED SUPPORT ANGLE LOC. BS 695 AND BL0 LH SIDE AT PASSENGER CABIN IAW SRM B737-700 SRM-51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700; ANGLE MUST BE REPLACED. LENGTH OF CRACK: 0.797 TOOL USED: CALIPER P/N: 500-197-20 S/N: 121486DUE DATE: JAN-03-2022 AND PERFORMED VISUAL INSPECTION AND NOT FOUND MORE DAMAGE.; [08] FORMED AND DRILLED NEW SUPPORT ANGLE LOCATED BS 695 AND BL0 LH SIDE AT PASSENGER CABIN IAW DRAWING 273A9112 SHEET 3 REV B IAW B737-700 SRM 51-40-05; [09] APPLIED PROTECTIVE TREATMENT NO NEW SUPPORT ANGLE AIW B737-700 SRM 51-20-01-0G-0; [10] APPLIED PROTECTIVE TREATMENT ON NEW SUPPORT ANGLE AIW B737-700 SRM 51-20-01-0G-0 (CORRECTED TYPO OF CORRECTIVE ACTION #9); [11] STEP 8 COMPLETE RII AND STEP 10 COMPLETE; [14] INSTALLED NEW SUPPORT ANGLE AND RIVETS LOCATED BS 695 AND BL0 LH SIDE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG 273A9111; [15] STEP 14 COMPLETED RII.; [16] REPLACED SUPPORT ANGLE LOCATED BS 695 AND BL0 LH SIDE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG 273A9111 MATERIAL USED 7075-T0-0.050 IN PO# 2021 139514 1 HEAT TREATED AND CONVERTED FROM 7075-T0 TO CONDITION T73 IAW BAC5602 TABLE IV PAGE 22 AND TABLE XI PAGE 36 TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 21-JAN-22; [17] TASK CARD COMPLETED RII.

Part: PRESSURE DECK — CRACKED (BS 663) · airframe 74,935 hrs · 44,224 cycles

CRACK WEB PRESSURE DECK HORIZONTAL AT MAIN WHEEL WELL COMPARTME (2 EA) (CRACK 1 LOC. AT RBL 41 AND BS 663; L= 1.125 INCH APPROX; AND CRACK 2 LOC. AT RBL 42 AND BS 675; L= 1 INCH APPROX) ; 2021-368568 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC500D; S/N: N500X1693P030456; CAL DUE DATE: 30-NOV-21.; [02] TOOL USED CALIPER P/N 700-113-10 S/N 0016656; CAL DUE DATE 11-MAY-22.; [03] REPAIRED WEB PRESSURE DECK HORIZONTAL AT MAIN WHEEL WELL COMPARTMENT AT RBL 41 BS 663 AND RBL 42 BS 675 IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 MATERIAL USED ALUMINUM SHEET P/N 2024-T3 CLAD 0.80 PO 2021 138114; STIFFENER 7075-T6511 P/NBAC1505-100052 PO 2021 129586; ALUMINUM SHEET P/N 2024T3-063 PO 2020 202354; [04] TASK CARD COMPLETED RII

Part: ANGLE — CRACKED (RT WING TE) · airframe 74,935 hrs · 44,224 cycles

CRACK ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 RT WING ; 2021-368530 / [01] REMOVED ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 RT WING IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON AREA NOT FOUND MORE DAMAGE DUE TO NOT FOUND ALLOWABLE DAMAGE MUST BE REPLACED; [02] OK TO INSTALL NEW ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 RT WING AND FASTENERS; [03] COMPLETED STEP 1 AND 2; [04] INSTALLED NEW ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 RT WING IAW B737-700 SRM 51-40-02; [05] REPLACED ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM B737-700 51-40-02 AND DRAWING 115A2930 SHEET 7 REV-; [06] COMPLETED STEP 4 AND 5 <BR>TASK COMPLETED

Part: SUPPORT BRACKET — CRACKED (LT WING TE) · airframe 74,935 hrs · 44,224 cycles

CRACK SUPPORT BRACKET TRAILING EDGE DEFLECTION CONTROL RIB ORSS 271 AT LT WING ; 2021-368553 / [01] REMOVED SUPPORT BRACKET TRAILING EDGE DEFLECTION CONTROL RIB ORSS 271 AT LT WING IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON AREA NOT FOUND MORE DAMAGE DUE TO NOT FOUND ALLOWABLE DAMAGE MUST BE REPLACED; [02] OK TO INSTALL NEW SUPPORT BRACKET TRAILING EDGE DEFLECTION CONTROL RIB ORSS 271 AT LT WING AND FASTENERS; [03] COMPLETED STEP 1 AND 2; [04] INSTALLED NEW SUPPORT BRACKET TRAILING EDGE DEFLECTION CONTROL RIB ORSS 271 AT LT WING IAW B737-700 SRM 51-40-02; [05] REPLACED NEW SUPPORT BRACKET TRAILING EDGE DEFLECTION CONTROL RIB ORSS 271 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM B737-700 SRM 51-40-02; [06] COMPLETED STEP 4 AND 5<BR>TASK COMPLETED

Part: SUPPORT ANGLE — CRACKED (BS 695) · airframe 74,935 hrs · 44,224 cycles

CRACK SUPPORT ANGLE LOCATED BS 695 AND BL0 RH SIDE AT PASSENGER CABIN ; 2021-368562 / [01] REMOVED SUPPORT ANGLE LOC. BS 695 AND BL0 RH SIDE AT PASSENGER CABIN IAW SRM B737-700 SRM-51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700; ANGLE MUST BE REPLACED. LENGTH OF CRACK: 1.430 TOOL USED: CALIPER P/N: 500-197-20 S/N: 121486DUE DATE: 03-JAN-22 AND PERFORMED VISUAL INSPECTION AND NOT FOUND MORE DAMAGE.;[06] FORMED SUPPORT ANGLE LOC. BS 695 AND BL0 RH SIDE AT PASSENGER CABIN IAW B737-700 DWG # 273A9112 REV:- [07] STEP 6 COMPLETED; [10] DRILLED NEW SUPPORT ANGLE LOCATED BS 695 AND BL0 RH SIDE AT PASSENGER CABIN IAW B737-700 SRM 51-40-05; [11] APPLIED PROTECTIVE TREATMENT ON NEW SUPPORT ANGLE IAW B737-700 SRM 51-20-01-0G-0; [12] STEP 10 COMPLETE RII AND STEP 11 COMPLETE; [15] INSTALLED NEW SUPPORT ANGLE AND RIVETS LOCATED BS 695 AND BL0 RH SIDE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG 273A9111 REV:-; [16] STEP 15 COMPLETED RII; [17] REPLACED SUPPORT ANGLE LOCATED BS 695 AND BL0 RH SIDE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG 273A9111 REV:-

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,935 hrs · 44,224 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-368396 / [01] TOOK MEASURE OF CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IS L: 0.435. AND NO FOUND ALLOWABLE DAMAGE ON SRM MUST BE REPAIR .; [03] PERFORMED CUT AND REMOVED THE DAMAGE FROM VERTICAL STIFFENER AND WEB OF THE INSPAR RIB LOC . INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER. I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4 . [07] PERFORMED CUT AND REMOVED THE DAMAGE FROM LOWER CORD OF THE INSPAR RIB . LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER. I.A.W B737-700 SRM 55-10-09-2R-5 REPAIR 5 . AND PERFORMED VISUAL INSPECTION AND NOT FOUND MORE DAMEGE .; [08] VERIFIED STEP 7;NOT FOUND ADDITIONAL DAMAGE;[20] INSTALLED REPAIR PARTS T-SECTION (1E/A) ANGLE (1E/A) AND SHIM (2E/A) AND FILLER (1E/A) OF INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 TABLE 201 FIGURE 204 AND IAW B737-700 SRM 51-40-02; [21] REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 TABLE 201 FIGURE 204; [22] CERTIFIED STEP 20 AND COMPLETED TASK CARD; [23] CERTIFIED STEP 20 RII

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 74,935 hrs · 44,224 cycles

CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT ; 2021-368319 / [01] TOOL USED; DIGITAL CALIPER P/N:500-197-30 S/N: B20189526 DUE DATE 22-NOV-21; [02] REPAIRED BY WELD FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4.B AND BAC5975 TOOL USED: DIGITAL CALIPER P/N 500-197-30; S/N B20189526; DUE DATE 22-NOV-21.; [03] REPAIRED BY WELD FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4.B AND BAC5975 TOOL USED: DIGITAL CALIPER P/N 500-197-30; S/N B20189526; DUE DATE 22-NOV-21.

Part: SPAR — CORRODED (LT WING) · airframe 74,935 hrs · 44,224 cycles

CORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROX AT LT WING ; 2021-368354 / [01] TOOL USED/ EDDY CURRENT PN/ NORTEC 600D; SN/ 2000053402; DUE DATE/ 23APR22.; [02] TOOL USED: ULTRASONIC THICKNESS GAUGE ; PN/ 25DL PLUS;SN/ 071504410; DUE DATE/ 20NOV21; [03] TOOL USED CALIPER P/N :500-464 S/N : 15331936 DUE DATE : 05-OCT-21; [04] TOOL USED : CALIPER P/N:700-113-10 S/N:0016656 DUE DATE: 11-MAY-22; [05] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 500D; S/N: N500X1693P030456 DUE DATE: 30-NOV-21.; [06] REPAIRED FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROX AT LT WING IAW EA 21-157-02490; [07] TASK CARD COMPLETED <BR>RII

Part: LIGHT — BROKEN (GALLEY AREA) · airframe 74,935 hrs · 44,224 cycles

BROKEN GALLEY 1 EMERGENCY LIGHT ASSY AND LENS AT FWD GALLEY AREA ; 2021-368307 / [01] REPLACED GALLEY 1 EMERGENCY LIGHT ASSY AND LENS AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802.; [02] TASK CARD COMPLETED

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 74,935 hrs · 44,224 cycles

CUSTOMER REQUEST CRACK BODY STATION 663.75 VAPOR BARRIER APPROX LBL 14 AT MAIN WHEEL WELL COMPARTMENT ; 2021-368398 / [01] TOOL USED CALIPER: P/N:500-197-20 S/N:13083235 DUE DATE:18-AUG-21.; [02] HOT BONDER P/N HCS9200B-AV S/N 18196127 DUE DATE 11-DEC-21; [03] SCALE: P/N: SCA-301 S/N:AE-412120 DUE DATE:24-FEB-22; [04] TOOL USED SCALE P/N:SCA-301; S/N: AE-412133; DUE DATE: 24-FEB-22; [05] COMPLETED STEP 9. ITEM RII.; [06] REPAIRED VAPOR BARRIER LOCATED AT BS 663.75 APPROX. LBL 14 AT MAIN WHEEL WELL COMPARTMENT AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10.; [07] RII ACCOMPLISHED : <BR>REPAIRED VAPOR BARRIER LOCATED AT BS 663.75 APPROX. LBL 14 AT MAIN WHEEL WELL COMPARTMENT AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,935 hrs · 44,224 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-368397 / [01] TOOK MEASURE OF CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IS L: 0.435 NO FOUND ALLOWABLE DAMAGE ON SRM MUST BE REPAIR .; [03] STEP 2 COMPLETE; [04] PERFORMED CUT AND REMOVED THE DAMAGE FROM VERTICAL STIFFENER AND WEB OF THE INSPAR RIB LOC . INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER. I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4 . [05]PERFORMED CUT AND REMOVED THE DAMAGE FROM LOWER CORD OF THE INSPAR RIB . LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER. I.A.W B737-700 SRM 55-10-09-2R-5 REPAIR 5 . [12] MARKED HAND LAY OUT ON REPAIR AREA INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 FIGURE 204; [14]MADE AND DRILLED REPAIR PARTS T-SECTION (1E/A) ANGLE (1E/A) AND SHIM (2E/A) AND FILLER (1E/A) OF INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 TABLE 201 FIGURE 204. AND SRM 51-40-05. [22] INSTALLED REPAIR PARTS T-SECTION (1E/A) ANGLE (1E/A) AND SHIM (2E/A) AND FILLER (1E/A) AND FASTENERS ON INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 TABLE 201 FIGURE 204; AND B737-700 SRM 51-40-0

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 74,935 hrs · 44,224 cycles

BROKEN FLOOR PANEL 140CF SPLICE PLATE FWD CUT OUT OF DOOR AT AFT CARGO COMPARTMENT ; 2021-368266 / [01] REPLACED PANEL 140CF SPLICE PLATE FWD CUT OUT OF DOOR AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 PART NUMBER USED 453A2611-1 PO 2020 181966; [02] TASK COMPLETED

Part: ACCESS PANEL — CRACKED (WNG-BDY FAIRING) · airframe 74,935 hrs · 44,224 cycles

CRACK ACCESS PANEL 193D BODY FAIRING HOLES AT LOWER FUSELAGE ; 2021-368286 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: B17030925; DUE DATE: 06-AUG-21.; [02] TOOL USE SCALE: P/N: SCA-301; S/N:AE-412130; DUE DATE: 24-FEB-22.; [03] TOOL USED P/N: FLUKE87-5. S/N: 32040131. DUE DATE: 18-AUG-21.; [04] REPAIRED ACCESS PANEL 193D BODY FAIRING HOLES AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9. TOOL USED HOT BONDER: P/N: HCS9200B S/N: 18165044 DUE DATE: 15/FEB/22; SCALE: P/N: SCA-301 S/N AE-412137 DUE DATE: 24/FEB/22; SCALE: P/N: SCA-301; S/N:AE-412130; DUE DATE: 24-FEB-22; HOT BONDER PN: HCS9200B-AV SN:18196127 DUE DATE: 11/DEC/21; MULTIMETER P/N: FLUKE87-5. S/N: 32040131. DUE DATE: 18-AUG-21; [05] REPAIRED ACCESS PANEL 193D BODY FAIRING HOLES AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9. TOOL USED HOT BONDER: P/N: HCS9200B S/N: 18165044 DUE DATE: 15/FEB/22; SCALE: P/N: SCA-301 S/N AE-412137 DUE DATE: 24/FEB/22; SCALE: P/N: SCA-301; S/N:AE-412130; DUE DATE: 24-FEB-22; HOT BONDER PN: HCS9200B-AV SN:18196127 DUE DATE: 11/DEC/21; MULTIMETER P/N: FLUKE87-5. S/N: 32040131. DUE DATE: 18-AUG-21.

Part: ACCESS PANEL — CRACKED (WNG-BDY FAIRGIN) · airframe 74,935 hrs · 44,224 cycles

CRACK ACCESS PANEL 194E BODY FAIRING FASTENER HOLES AT LOWER FUSELAGE ; 2021-368288 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: B17030925; DUE DATE: 06-AUG-21.; [02] TOOL USE SCALE: P/N: SCA-301; S/N:AE-412130; DUE DATE: 24-FEB-22.; [03] TOOL USED: HOT BONDER PN: HCS9200B-AV SN:18196119 DUE DATE: 27JAN22.; [04] REPAIRED ACCESS PANEL 194E BODY FAIRING HOLES AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9. TOOL USED: HOT BONDER P/N: HCS9200B S/N: 18165044 DUE DATE: 15/FEB/22; SCALE: P/N: SCA-301 S/N AE-412137 DUE DATE: 24/FEB/22;; [05] REPAIRED ACCESS PANEL 194E BODY FAIRING HOLES AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9. TOOL USED: HOT BONDER P/N: HCS9200B S/N: 18165044 DUE DATE: 15/FEB/22; SCALE: P/N: SCA-301 S/N AE-412137 DUE DATE: 24/FEB/22;

Part: ACCESS PANEL — BROKEN (WNG-BDY FAIRING) · airframe 74,935 hrs · 44,224 cycles

BROKEN ACCESS PANEL 192BR WING TO BODY FAIRING STUDS AT LOWER FUSELAGE (8 EA) ; 2021-368265 / [01] REPLACED STUDS ACCESS PANEL 192BR WING TO BODY FAIRING AT LOWER FUSELAGE (8 EA) IAW B737-700 SRM 51-40-02-0G; [02] REPLACED STUDS ACCESS PANEL 192BR WING TO BODY FAIRING AT LOWER FUSELAGE (8 EA) IAW B737-700 SRM 51-40-02-0G

Part: BULKHEAD WEB — DAMAGED (BS 663) · airframe 74,798 hrs · 44,134 cycles

STIFFENER FASTENER HOLES IN VAPOR BARRIOR WEB ELONGATED AT ST 663 IN LH MLG W/W BETWEEN LBL 6 AND LBL 11. / [01] REPAIRED FASTENER HOLES PER SRM 51-70-04 REF. FROM SRM 57-10-10.

Part: STIFFENER — CRACKED (BS 663) · airframe 74,798 hrs · 44,134 cycles

STIFFENER CRACKED ; DIAGONAL STIFFENER CRACKED IN LH AC BAY LOCATED ON WING CENTER SECTION REAR SPAR FIBERGLASS VAPOR BARRIER BETWEEN LBL 6.15 AND LBL 31.83. / [01] REMOVED CRACKED STIFFENER. LOCATED; DRILLED AND INSTALLED NEW STIFFENER PER SRM 51-40-02.; [02] CAP SEALED FASTENERS PER SOPM 20-50-19.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 74,798 hrs · 44,134 cycles

VAPOR BARRIER INTERIM REPAIR APPLIED PER SRM 51-10-10-1A-2 ; APPLIED INTERIM SEAL OVER THE CRACK AT LBL 11.9; 45 FROM PRESSURE DECK THA IN PER SRM 57 -10-10 PARAGRAPH 2.C.(4)/ALLOWABLE DAMAGE 2. VISUAL INSPECTION REQUIRED OF THE REPAIR AREA AT 1200 FLIGHT CYCKLE INTERVALS OR MORE FREQUENTLY. / [01] APPLIED INTERIM REPAIR PER SRM 57-10-10-1A-2 STEP 2 (C) 4. ACCOMPLISH VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY PER SRM 57-10-10-1A-2.; [02] APPLIED INTERIM REPAIR PER SRM 57-10-10-1A-2 STEP 2 (C) 4. ACCOMPLISH VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY PER SRM 57-10-10-1A-2.

Part: BARRIER — CRACKED (L/H MLG W/W) · airframe 73,726 hrs · 43,544 cycles

5.5' LONG CRACK IN GLASS REINFORCED FIBER VAPOR BARRIER @ LBL 11.9'; 45' FROM PRESSURE DECK IN L/H MLG W/W / 5.5' LONG CRACK ALSO FOUND SECOND CRACK 4.5' IN GLASS REINFORCED FIBER VAPOR BARRIER @ LBL 11.9'; 45' FROM PRESSURE DECK IN L/H MLG W/W COMPLIED WITH EA 1-A57-13410 TIME LIMITED DEFERRAL REPETITIVE INSPECTION DUE EVERY 100 CYCLES REMOVE ALUMINUM FOIL SPEED TAPE AND INSPECT CRACK(S) FOR ADDITIONAL GROWTH. IF NO ADDITIONAL GROWTH; REAPPLY SPEED TAPE. IF CRACK HAS GROWN BUT STILL WITHIN LIMITS OF STEP 1 OF THIS EA; STOP DRILL THE CRACK PER 737-700/800 SRM 51-10-02 AND APPLY SPEED TAPE. PERMANENT REPAIR REQUIRED WITHIN 600 CYCLES. ACCOMPLISH A PERMANENT REPAIR AS GIVEN IN 737-700/800 SRM 51-70-04; REPAIR 10 OR AS AN ALTERNATIVE; REPAIR PART OF CRACK SO THAT THE CRACK LENGTH IS LESS THAN OR EQUAL TO THE MAXIMUM ALLOWABLE DAMAGE LIMIT. APPLY THE INTERIM SEAL OVER THE CRACK THAT IS LEFT AS GIVEN IN 737-700/800 SRM 57-10-10 PARAGRAPH 2.C.(4)/ALLOWABLE DAMAGE 2.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,726 hrs · 43,544 cycles

CABIN EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY CHECK AT LOCATIONS M01669; M01672 AND M01675 / REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS M01669; M01672 AND M01675 PER AMM 33-51-06

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,706 hrs · 42,940 cycles

RT OVERWING EMERGENCY LIGHT INOPERABLE. RELAMPED RT OVERWING EMERGENCY LIGHT PER AMM 33-51-04. OPERATIONS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,077 hrs · 41,900 cycles

L/H EMERGENCY LIGHT INOP AT ROW 16. RELAMPED EMERGENCY LIGHT PER AMM.

Part: PLATE — CRACKED (RT WING) · airframe 70,745 hrs · 41,714 cycles

R/H WING WIGGLE PLATE CRACKED. / R&R WIGGLE PLATE SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,739 hrs · 41,711 cycles

R/H EMERGENCY EXIT DOOR SIDEWALL LIGHT INOP AT ROW 12. / RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 70,150 hrs · 41,334 cycles

EXIT SIGN INOP. RELAMPED PER AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 70,150 hrs · 41,334 cycles

EXIT SIGN INOP LIGHT BULBS. RELAMPED PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,150 hrs · 41,334 cycles

EMERGENCY EXIT LIGHT HAS BURNED OUT LIGHT BULBS. RELAMPED PER AMM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 70,150 hrs · 41,334 cycles

EMERGENCY BULLNOSE LIGHT INOP AT ROW #1 LEFT. DISCONNECTED AND RECONNECTED CONNECTOR PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 70,150 hrs · 41,334 cycles

EMERGENCY EXTERIOR LIGHT INOP. RELAMPED GOOD OPS CHECK PER AMM.

Part: CONNECTOR — DISCONNECTED (EXIT SIGN) · airframe 70,150 hrs · 41,334 cycles

EMERGENCY EXIT SIGN INOP. RECONNECTED CONNECTOR PER AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

AFT CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 927 TO BS 947, RBL 21. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, RBL 21. REPAIRED INTERCOSTAL IAW SRM & DWG.

Part: NONE — CRACKED (AFT CARGO COMPT) · airframe 70,150 hrs · 41,334 cycles

SUPPORT CLIP AT BS 867 LBL 10 W/L 160 (WASTE TANK ENCLOSURE) IS CRACKED / REMOVED & REPLACED THE DAMAGE SUPPORT CLIP AT BS 867 LBL 10 W/L 160 WITH A NEW SUPPORT CLIP IAW SRM 51-40-02-0G & DWG #149A8103

Part: STRAP — CORRODED (CENTRE FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

***CORROSION*** ON LEFT WING EMERGENCY EXIT LOWER SILL STRAP AT BS 639 LBL 68 WL 222 / EVALUATED; FOUND NO ALLOWABLE DAMAGE PER SRM REMOVED AND REPLACED LEFT WING EMERGENCY EXIT LOWER SILL STRAP AT B.S. 639 LBL 68 WL 222 IAW SRM'S 51-40-02; SRM 51-40-05; SRM 51-10-02; DWG'S 144A6201 AND DWG 411A2802; SOPM'S 20-43-03; SOPM 20-41-02; SOPM 20-41-05

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

AFT CARGO BAY WATER TANK TO BULKHEAD SUPPORT FITTING CRACKED AT BS. 947.5, LBL 10. REPAIRED FITTING IAW SRM & DWG.

Part: PANEL — DEBONDED (LOWER EXT FUSELA) · airframe 70,150 hrs · 41,334 cycles

PANEL 193D OUTER SKIN IS DISBONDED ALONG AFT EDGE. (MARKED) / PANEL 193D OUTER SKIN DISBONDED ALONG THE AFT EDGE WAS REPAIRED. IAW SRM 51-70-05-212-1

Part: PYLON — CRACKED (L/H WING) · airframe 70,150 hrs · 41,334 cycles

LEFT WING FIXED L/E RIB JUST I/B OF PYLON IS CRACKED. PART NUMBER 116A4530-1 / REMOVED AND REPLACED LEFT WING FIXED L/E RIB I/B OF PYLON PER SRM 51-40-02; SRM 51-40-05; AND DWG 116A4008.

Part: BULKHEAD — CORRODED (AFT FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

***CORROSION*** IN MULTIPLE AREAS ON APU INLET PLENUM FLANGE ON BULKHEAD FWD FACE STA 1088 (MARKED) RBL 21-32; WL 231-246 / REPAIRED APU INLET PLENUM FLANGE ON BULKHEAD FWD FLANGE IAW EA 1-753-35570 REV IR AND ATS ER 19-04587 REV IR

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

PASSENGER CABIN SEAT TRACK CORRODED BETWEEN BS. 540 TO BS. 727B, LBL 45. R&R SEAT TRACK IAW DWG & SRM.

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 70,150 hrs · 41,334 cycles

CABIN SEAT TRACK CORRODED BETWEEN BS. 540 TO BS. 727B, RBL 45. / REPAIRED SEAT TRACK PER SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 70,150 hrs · 41,334 cycles

CABIN SEAT TRACK CORRODED BETWEEN BS. 540 TO BS. 727B, LBL 24.5. / R&R SEAT TRACK IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 500C, LBL 25. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 500A, LBL 25. R&R ANGLE IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D RBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 500C, RBL 25. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 400 TO BS 420, RBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

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

Part: GUSSET — CRACKED (FWD CARGO LH) · airframe 70,150 hrs · 41,334 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-21L WL177. MARKED / REMOVED AND REPLACED NEW GUSSET AT FCB B/S 500D; STR 21L WL177. PER SRM 51-40-02-00-0. DWG # 143A7902. 92892U 04SEP19.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

FORWARD CARGO BAY ON AFT LOWER BULKHEAD PANEL SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 22 TO RBL 22. R&R SUPPORT ANGLE IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 440 TO BS 500C, LBL 23. REPAIRED SUPPORT IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 500B, LBL 25. REPAIRED INTERCOSTAL IAW EA AND ER.

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 70,150 hrs · 41,334 cycles

***CORROSION*** ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS887 LBL7 - RBL19 WL168. / CORROSION ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS 887; LBL7-RBL19 FOUND TO BE OT OF LIMITS; NO ALLOWABLE DAMAGE GIVEN; REPAIR BY REPLACEMENT IAW SRM 53-00-53 AND SRM 51-10-02. LOCATED AND DRILLED AND INSTALLED FASTENERS IAW SRM 51-40-05; SRM 51-40-02 AND DWG 146A9401 SH 12; REV F

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 767, RBL 21. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 827, LBL 21. R&R SUPPORT PER SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

FORWARD SHIELD AT AFT CARGO BAY CORRODED BETWEEN BS 767 TO BS 787, RBL 21. R&R SHIELD IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

***CORROSION*** ON EWIS SUPPORT ANGLE STA 1021.27+19 STR 2L WL 307 / REMOVED AND REPLACED SUPPORT ANGLE AT BS 1021.27+19 BETWEEN S2L TO S2R IAW SRM 51-40-02 AND DWG # 148A3110 51049U 07SEP19

Part: JOINT — CRACKED (VERT. STAB.) · airframe 70,150 hrs · 41,334 cycles

CRACK IN 'JOINT ASSY - EXPANSION VERT. FIN ' STA 1021.27 WL 308 (P/N 176A3101-26) ON L/H SIDE (MARKED) / REMOVED & REPLACED JOING ASSY - EXPANSION VERTICAL FIN AT STA 1027.27 WL 308 IAW SRM 51-40-02-0G-01 AIPC 53-33-11-02

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

***CORROSION*** IN MULTIPLE AREAS OF FUSELAGE SKIN FROM STA 1021.27-1088 STR 3L-3R / REPAIRED FUSELAGE SKIN B.S 1021.27 - 1088 STR 3L - 3R IAW EA 1-753-35609 REV IR AND ATS ER 19-04581 REV IR

Part: PANEL — CRACKED (VERT. STAB.) · airframe 70,150 hrs · 41,334 cycles

VERTICAL STAB PANEL 324AR LOWER RETAINER IS CRACKED / REMOVED & REPLACED VERTICAL STAB PANEL 324AR LOWER RETAINER IAW SRM 51-40-02-0G-0.

Part: FORMER — CRACKED (LWR FUSELAGE) · airframe 70,150 hrs · 41,334 cycles

FAIRING FORMER IS CRACKED ON INBOARD END OF LEFT WING LEADING EDGE AT B.S. 500D. / FAIRING FORMER AT INBD L/W FIXED LE REMOVED AND REPLACED IAW B737 SRM 51-40-02 AND DWG 116A3010 AND 116A3110

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 70,150 hrs · 41,334 cycles

RIB ASSEMBLY 4 ON LT HORIZONTAL STABILIZER #3 STIFFENER CRACKED, LOWER RADIUS STAB STA 120.30. REPAIRED #3 STIFFENER IAW SRM & DWG.

Part: PANEL — DELAMINATED · airframe 70,150 hrs · 41,334 cycles

PANEL 194FL HAS TOOL MARKS WITH POSSIBLE DELAMINATION AT FASTENER HOLE (MARKED) / REPAIRED DELAMINATION DAMAGE AT FASTENER HOLE ON PANEL 194FL IAW SRM 51-70-05-2R-1.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 70,150 hrs · 41,334 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS. 663 TO BS. 674, BETWEEN LBL 30 TO LBL 62. REPAIRED PRESSURE DECK IAW SRM2.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 70,150 hrs · 41,334 cycles

LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE CRACKED AT BS 663, BETWEEN RBL 6 TO RBL 19. REPAIRED ATTACH ANGLE IAW SRM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 70,150 hrs · 41,334 cycles

VAPOR BARRIER CRACKED AT BS 663, RBL 10. R&R VAPOR BARRIER IAW SRM & DWG.

Part: PANEL — DELAMINATED (FU) · airframe 70,150 hrs · 41,334 cycles

PANEL 194FR HAS POSSIBLE DELAMINATION ON OUTER SKIN (MARKED) / PANEL 194FR WITH DELAMINATION ON OUTER SKIN WAS REPAIRED IAW SRM'S 51-70-05-2R-2 AND 51-70-05-2R-11. 59702U 08/29/19

Part: BEAM — CRACKED (R1 DOOR) · airframe 70,150 hrs · 41,334 cycles

R1 DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. REPAIRED #4 LOWER BEAM ON RO.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 70,150 hrs · 41,334 cycles

R/H HORIZONTAL STABILIZER REMOVABLE LEADING EDGE #6 RIB CRACKED. R&R #6 RIB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 70,150 hrs · 41,334 cycles

R/H HORIZONTAL STABILIZER REMOVABLE LEADING EDGE #2 RIB CRACKED. / R&R #2 RIB IAW SRM AND DWG.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,051 hrs · 40,644 cycles

EXTERIOR EMERGENCY LIGHT @ R2 DOOR INOP (AFT SERVICE DOOR) RELAMPED EXTERIOR EMERGENCY LIGHT @ R2 DOOR. REF. B-737 AM 33-51-04. (AFT SERVICE DOOR)

Part: WEB — DAMAGED (FUSELAGE) · airframe 68,535 hrs · 40,328 cycles

FLIGHT DECK FLOOR WEB SHARP CREASE THAT AT BS 328, FROM LBL 15.33. TO BL 0. REPAIRED WEB IAW EA AND ER.

Part: LENS — BROKEN (EXIT SIGN) · airframe 68,136 hrs · 40,071 cycles

FORWARD BULKHEAD EXIT SIGN BROKEN. R&R LENS PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,256 hrs · 39,507 cycles

RT EXTERIOR OVERWING EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: MOUNT — BROKEN (L2 DOOR) · airframe 66,928 hrs · 39,296 cycles

L2 DOOR FORWARD MOUNT FOR DOOR SLIDE NUT PLATES BROKEN. R&R MOUNTS PER SRM.

Part: SKIN — CRACKED (TE FLAP) · airframe 66,572 hrs · 39,054 cycles

RT WING INBD AFT FLAP LOWER SKIN CRACKED AT STA 96.5. R&R FLAP PER MM.

Part: RETAINER — OUT OF ADJUST (GIRT BAR) · airframe 66,395 hrs · 38,941 cycles

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

Part: SLIDE — LOOSE (L1 DOOR) · airframe 65,044 hrs · 38,081 cycles

L1 DOOR SLIDE FOUND LOOSE. SECURED THE SLIDE IAW SIP AND AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 63,947 hrs · 37,392 cycles

AFT LOWER CORNER OF EXTERNAL POWER DOOR DOUBLER CRACKED. REPAIRED DOUBLER IAW SRM AND EA.

Part: SLIDE — CORRODED (L2 DOOR) · airframe 63,536 hrs · 37,123 cycles

L2 DOOR EMERGENCY EVAC SLIDE CORRODED. R&R SLIDE PER MM AND MT.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 63,532 hrs · 37,122 cycles

CENTER CABIN OVERHEAD EMERGENCY EXIT SIGN BROKEN. R & R THE LIGHT HOUSING PER AMM.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 63,524 hrs · 37,117 cycles

AFT EMERGENCY SIGN LOOSE. R & R THE LIGHT ASSEMBLY IAW CMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

AFT PIT INTERCOSTAL CORRODED BETWEEN BS 747 TO BS 767, RBL 21. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 63,472 hrs · 37,083 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 63,472 hrs · 37,083 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

PASSENGER CABIN FLOOR CREASE BEAM WEB CORRODED AT BS 927, LBL 55. R&R CREASE BEAM IAW SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,472 hrs · 37,083 cycles

FWD WET AREA FLOOR PANEL 222CF UPPER FACESHEET HAS FIBER DAMAGE / REPAIRED DAMAGE TO 1PLY ON UPPER FWD SURFACE ON PANEL 222CF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1; SRM53-00-50-2R-0 REPAIR GENERAL; AIPC 53-21-00-20; B737 NDT 51-05-01 PART 1

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,472 hrs · 37,083 cycles

FWD WET AREA FLOOR PANEL221GF IS DISBONDED ON FWD OUTBOARD END / REPAIREDFWD WET AREA FLOOR PANEL 221GF FWD OUTBOARD END I/A/W SRM 53-00-50-2R-9 PAR4.C-K (1);L(1);M(1) REV 62.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,472 hrs · 37,083 cycles

AFT WET AREA FLOOR PANEL 241ABF UPPER AND LOWER FACESHEETS ARE DAMAGED / REPAIRED AREAS ON UPPER & LOWER SURFACES AS MARKED WITH DAMAGE TO SKIN ON PANEL 241 ABF IAW B737-700 SRM 53-00-50-2R-0 REPAIR GENERAL SRM 53-00-50-2R-1 REPAIR 1 NDT 51-05-01 PART 1

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,472 hrs · 37,083 cycles

AFT WET AREA FLOOR PANEL 242UF LOWER FACESHEET IS DAMAGED ON OUTBOARD END IN 2 PLACES / PREPPED; CLEANED AND REPAIRED DAMAGE TO LOWER FACE SHEET AT AFT O/B CORNER ON FLOORBOARD 242UF IAW B737 SRM 53-00-50-2R-4; PARA 3(A-K1; L1-M1) REV 62.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO BAY FLOORBOARD TRANSITION STRIP AT STA 770 AREA IS CORRODED TOP AND BOTTOM SIDES AS MARKED / AFT CARGO COMPARTMENT FLOORBOARD TRANSITION STRIP AT BS 770 + 2.0';ORIGINAL 'T' .070; LOSS .070. REMAINING MATERIAL 0. OUT OF LIMITS IAW SRM 53-00-53-1A-2. VERIFIED NEW STRIP 'TEE' P/N 146A9401 -4 ATAG OPO565.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,472 hrs · 37,083 cycles

AFT WET AREA FLOOR PANEL 242VF UPPER AND LOWER FACESHEETS ARE DAMAGED / REPAIRED DAMAGE ON FLOOR PANEL 242 VF BONDED REPAIR PLIES ON UPPER AND LWR SURFACES AND CURED TAP TEST GOOD IAW B737-700 SRM 53-00-50-2R-6 REPAIR 6 & SRM 53-00-50-2R-0 GENERAL

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 63,472 hrs · 37,083 cycles

LAV WASTE DOOR HAS CORROSION ON TOP EDGE AND INSIDE / REMOVED CORROSION AND VERIFIED LIMITS AT LAV WASTE DOOR (ORIGINAL T .100') (LOSS = .033') (REMAINING .067') OUT OF LIMITS IAW SRM 52-40-01-1A-4 STEP 4B FIG 103 DETAIL 1 ) REMOVED AND REPLACED LAV WASTE DOOR IAW AMM 52-49-07-000-801 / AMM 52-49-07-400-801 STEP 3C (BONDING CHECK GOOD .001 OHMS) ATAG # OP0528 TOOL ID # (36308 CAL DUE 08-31-17) (30361 CAL DUE 05-31-18)

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,472 hrs · 37,083 cycles

CABIN FLOOR PANEL 242CF AFT INBOARD END IS DAMAGED / REPAIRED DAMAGE CORE ON AFT I/B END OF PANEL 242CF IAW B737 SRM 53-00-50-2R-10 REV62

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,472 hrs · 37,083 cycles

FWD WET AREA FLOOR PANEL 222DF IS DISBONDED ON FWD INBOARD END / REPAIRED FWD WET AREA FLOOR PANEL 222 DF AT FWD INBD CORNER IAW SRM 53-00-50-2R-1 PAR C-K (10 L (1) M (1) REV 62

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,472 hrs · 37,083 cycles

PASSENGER CABIN FLOOR PANEL 242AF LOWER FACESHEET IS DAMAGED IN 4 PLACES / REPAIRED MULTIPLE AREAS OF PANEL 242AF IAW B737 SRM 53-0-50-2R-10AND 53-00-50-2R-1 REV 62

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,472 hrs · 37,083 cycles

AFT WET AREA FLOOR PANEL 242WF UPPER AND LOWER FACESHEETS ARE DAMAGED NEAR EDGE / REPAIRED AREA ON LOWER SURFACE WITH DAMAGE TO ISKIN PANEL 242WF. WITH NO DAMAGE NOTED TO UPPER SURFACE. IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1; SRM 53-00-50-2R-0 REPAIR GENERAL; NDT 55-05-01 PART 1

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,472 hrs · 37,083 cycles

PASSENGER CABIN FLOOR PANEL 241BF IS DAMAGED ON AFT END / REPAIRED FLOOR PANEL 241BF IAW B737-700 SRM 53-00-50-2R-10 PARA3 REV62

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 63,472 hrs · 37,083 cycles

FWD WET AREA FLOOR PANEL 221BF AFT OUTBOARD CORNER IS BROKEN OFF / PREPPED; CLEANED AND REPAIRED MISSING/BROKEN EDGE AT AFT O/B CORNER; UPPER AND LOWEWR SURFACE ON FLOORBOARD 221BF IAW B737 SRM 53-00-50-2R-6; PAR 3 (A-G1; H1;I1; J-K1;L1;M1) REV 62

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,472 hrs · 37,083 cycles

PASSENGER CABIN FLOOR PANEL 241EF AFT OUTBOARD END IS DAMAGED / REPAIRED FLOORPANEL 241EE IAW B737-700 SRM 53-00-50-2R-10 PARA 3 REV62

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO BAY FLOOR STRAPS MARKED #1 L/H AND #2 L/H HAS MULTIPLE AREAS OF CORROSION TOP AND BOTTOM SURFACES / OBTAINED NEW AFT PIT CARGO BAY FLOOR STRAPS LH #1 AND #2 IAW IPC 25-52-10-02 P/N 453A2611-8 ATAG WN3753 P/N 453A2611-10 ATAG A86990

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO BAY FLOOR PNL # 140AF FWD METAL RETAINER STRIP FOR FWD CORNER EDGE OF BOARD IS CORRODED BOTH SIDES AS MARKED / OBTAINED AFT CARGO BAY FLOOR PNL #140AF FWD METAL RETAINED STRIP IAW AIPC 25-52-10+02 PG 45 ATAG: A86554

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,472 hrs · 37,083 cycles

PASSENGER CABIN FLOOR PANEL 241FF IS DAMAGED ON FWD END IN 2 PLACES / REPAIRED FLOOR PANEL 241FF IAW B737-700-SRM 53-00-50-2R-10 PARA 3 REV62

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO BAY FLOOR PNL # 140DF SIDE RETAINER STRIP IS CORRODED ON BOTTOM SIDE AS MARKED / OBTAINED AFT CARGO BAY FLOOR PNL #140DF SIDE RETAINED STRIP IAW AIPC 52-52-10-02 ATAG: A46104

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO BAY FLOOR PNL # 140CF TOP AND BOTTOM SIDES OF FLOOR BOARD IS CORRODED IN SEVERAL AREAS AS MARKED / EVALUATED PANEL 140CF FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-53-1A-1 STEP 5A. VERIFIED MATERIAL FABRICATED ALONIDID AND PRIMED NEW PANEL #140CF IAW EA 1-A53-2446 REV 1;AMM 51-21-41-370-802;AMM 51-21-41-370-804

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 63,472 hrs · 37,083 cycles

RT WING INBOARD LEADING EDGE WING TO BODY FAIRING SUPPORT BRACKET CRACKED. R&R BRACKET IAW SRM AND DWG.

Part: WEB — CORRODED (RIGHT WING) · airframe 63,472 hrs · 37,083 cycles

RIGHT WING FRONT SPAR AFT OF #3 KREUGER FLAP; SPAR H AS CORROSION AT FUEL BOOST PUMP UPPER AND LOWER BOND ING STRAPS. / RIGHT WING FRONT SPAR AFT OF #3 KREUGER FLAP SPAR HA S CORROSION AT FUEL BOOST PUMP UPPER AND LOWER BONDI NG STRAPS. REPAIRED I/A/W EA 170312 REV IR AND EA 1- 757-14127 REV IR

Part: TRACK — GOUGED (CABIN) · airframe 63,472 hrs · 37,083 cycles

PASSENGER CABIN; SEAT TRACK; 45L; STA. 520 CROWN WORN. / SEAT TRACK STA 520 LBL 45 CROWN WORN. BLENDED OUT GOUGE I/A/W SRM 51-10-02-0G-0; MATERIAL LOSS AT BLENDED AREA IS .025 MAX L IMITS IS .020 'OUT OG LIMITS' I/A/W SRM 53-00-52-1A-1 FIG 103. CUT; TRIMMED; FABRICATED NEW SEAT TRACK WITH -2 CHANNEL I/A/W SRM 53-00-52-2R-4. INSTALLED; ALODINED; PRIMED; APPLIED SEALANT; CIC I/A/W SRM 53-00-52-2R-4 REPAIR 4.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

MAIN CABIN FLOOR STRUCTURE FLOOR SUPPORT WEB CORRODED AT BS 1012, RBL 38. REPAIRED WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

CREASE BEAM INNER CHORD CORRODED BETWEEN BS 293 TO BS 344, RBL 58. REPAIRED CHORD IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (BS 277-294) · airframe 63,472 hrs · 37,083 cycles

FLOOR SUPPORT CRACKED, BS 277 TO 294, RBL 1. R & R THE FLOOR SUPPORT IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

CREASE BEAM WEB INNER CHORD ATTACH ANGLE CRACKED AT BS 295, RBL 54. R&R ANGLE IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

MAIN CABIN FLOOR STRUCTURE R2 CREASE BEAM CHORD CORRODED BETWEEN BS 950 TO BS 993. R&R CREASE BEAM IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (CABIN) · airframe 63,472 hrs · 37,083 cycles

MAIN CABIN FLOOR STRUCTURE STA 947 TO STA 967 LBL 46 FLOOR SUPPORT HAS CORROSION AT FLOORBOARD HOLE. / REMOVED CORROSION ON FLOOR SUPPORT INTER COSTAL AT MAIN CABIN FLOOR STA 947 TO STA 967 RBL 46 AND FOUND IT OUT OF LIMITS IAW B737 SRM 53-70-51-1A-1 REMOVED AND REPLACED INTER COSTAL IAW BAC DRAWING 140A9870 REV A AND B737 SRM 51-40-02-0G-0 ISSUE TAG A83556

Part: BRACKET — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

PASSENGER CABIN FLOOR STRUCTURE GIRT BAR MOUNT BRACKET CORRODED AT BS 344, LBL 60. R&R BRACKET IAW DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

MAIN CABIN FLOOR STRUCTURE FLOOR SUPPORT CORRODED AT BS 955, BETWEEN RBL 9 TO RBL 30. R&R INTERCOSTAL IAW DWG AND SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

FLOORBEAM UPPER FLOOR FLANGE CRACKED AT BS 294.5, RBL 53. REPAIRED FLOOR BEAM IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

R1 DOOR FRAME CRACKED AT BS 295 BOTTOM INBOARD FLANGE. REPAIRED FRAME ASSEMBLY IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

PASSENGER CABIN CREASE BEAM INNER CHORD CORRODED BETWEEN BS 312 TO BS 360, LBL 58. R&R L1 CREASE BEAM IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (BS 297) · airframe 63,472 hrs · 37,083 cycles

FLOOR SUPPORT CORRODED AT BS 297, RBL 11. R & R THE FLOOR SUPPORT IAW SRM.

Part: ANGLE — CORRODED (FED THRESHOLD) · airframe 63,472 hrs · 37,083 cycles

R1 DOOR THRESHOLD SUPPORT ANGLE IS CORRODED STA 309- 313. / R1 DR THRESHOLD ANGLE IS CORRODED STA 309 TO STA 313 . BLENDED TO REMOVE CORROSION I/A/W SRM 51-10-02-0G- 0. MATERIAL LOSS AT BLEND IS .023. MATERIAL THICKNES S IS .090 REMAINING .077 ' OUT OF LIMITS' I/A/W SRM 53-10-15-1-01-2. LOCATED AND DRILLED ALL FASTENER HO ES I/A/W SRM 51-40-05-0G-0 ALSO BOEING DWG 141A8310 REV B. INSTALLED I/A/W BOEING DWG 141A8310 REV B AND SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 63,472 hrs · 37,083 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

MAIN CABIN FLOOR STRUCTURE L2 CREASE BEAM CHORD CORRODED BETWEEN BS 927 TO BS 986. R&R CREASE BEAM IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (BS 727-727A) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO BAY, CARGO TRACK CORRODED BETWEEN BS 727+15 - 727A+10, RBL 13. R & R THE CARGO TRACK IAW SRM & DWG.

Part: ANGLE — CORRODED (BS 727-767) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO BAY FLOOR SUPPORT RT SIDE ZEE ANGLE CORRODED BETWEEN BS 727+4 TO 767. R & R THE ZEE ANGLE IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED BETWEEN BS 927 TO BS 947, RBL 13. R&R FLOOR TRACK IAW DWG & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED AT BS 772, LBL 8. REPAIRED FLOOR TRACK IAW EA.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE R/H SIDE SHIELD (Z ANGLE) STA 767 TO STA 792 RBL 22 HAS CORROSION / BLENDED OUT CORROSION AT AFT CARGO COMPARTMENT FLOOR STRUCTURE R/H SIDE SHIELD STA 767 TO 792 RBL 22 IAW B737-700 SRM 51-10-02-0G-0 MAT LOSS WAS 0.008' ORIGINAL THICKNESS 0.050' THE MATERIAL REMAINING 0.042' THE AREA FOUND TO BE OUT OF LIMITS '10%' - 0.005' IAW B737-700 SRM 53-00-53-1A-2 LOCATED AND DRILLED AND INSTALLED NEW SHIELD IAW DWG 146A0081 REV B ATAG WN2836

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

FORWARD CARGO COMPARTMENT, LT CARGO FLOOR Z ANGLE CORRODED BETWEEN BS 435 TO BS 482. R&R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT FLOOR STRUCTURE R/H SIDE Z ANGLE HAS CORROSION STA 867 TO 947 / AFT CARGO COMPARTMENT FLOOR STRUCTURE RH SIDE ANGLE HAS CORROSION STA 867-947 BLENDED CORROSION AND FOUND FROM STA 867-887 ORIGINAL THICKNESS TO BE 032' REMOVED -101' REMAINING .022' FOUND TO BE OUT OF LIMITS - IAW SRM 53-00-53-1A-2 FROM STA 887-947 FOUND ORIGINAL T TO BE .032' REMOVED .002' REMAINING .030' FOUND TO BE IN LIMITS IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED Z ANGLE FROM STA 867-887 IAW SRM 53-00-53-2R-3 REPAIR 3

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED AT BS 878, RBL 3. REPAIRED FLOOR TRACK IAW SRM.

Part: ANGLE — CORRODED (FWD CARGO COMPT) · airframe 63,472 hrs · 37,083 cycles

FWD CARGO COMPT; CARGO FLOOR RH Z ANGLE CORRODED FROM BS 493 TO BS5OOA. / REMOVED CORROSION AND EVALUATE DAMAGE FOUND TO BE OUT OF LIMITS WITH 100% OF MAT LOSS OF FWD CARGO COMPT CARGO FLOOR RH Z ANGLE STA 493 TO 500A REMOVED AND REINSTALLED INTER COSTALL AND INSTALLED NEW SHIELD P/N 7531855 IAW SRM 53-30-15-1A-1 FIG 103 AND SRM 51-40-02 SOPM 20-41-05 ATAG # WN1433

Part: ANGLE — CORRODED (BS 727-727E) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO BAY FLOOR SUPPORT LT ZEE ANGLE CORRODED BETWEEN BS 727+4 TO 727E+10. R & R THE ZEE ANGLE IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED AT BS 772, RBL 3. REPAIRED FLOOR TRACK IAW EA.

Part: FLOOR PANEL — CRACKED (FWD CARGO COMPT) · airframe 63,472 hrs · 37,083 cycles

FWD CARGO COMPT; FLOOR PNL 120BF IS CRACKED. MARKED / RECEIVED NEW FORWARD CARGO COMPARTMENT FLOOR PANEL 120BF; P/N 453A1610-4 ATAG OPO507 IAW AIPC 25-52-10-01 AND BOEING DRAWING. PANEL 120BF FOUND TO BE OUT OF LIMITS;CRACK EXCEED 3.0 INCHES IN LENGTH. IAW B737 SRM 53-00-53-1A-1 5 (A) (BOEING DRAWING 453A1610-4)PANEL 120BF WILL BE INSTALL ON 36156-1400-0011 AND CARD # JPANEL 121 CLOSE.

Part: STRAP — CORRODED (FWD CARGO RH) · airframe 63,472 hrs · 37,083 cycles

FWD CARGO COMPT; RH SIDEWALL TO FLOOR STRAPS ARE CORRODED. / REMOVED CORROSION ON R/H SIDEWALL TO FLOOR STRAPS; EVALUATED MATERIAL LOSS ON FLOOR STRAPS; FOUND TO BE OUT OF LIMITS WITH 100% LOSS OF MATERIAL IAW SRM 53-00-53-1A-2 OBTAINED NEW FLOOR STRAP FOR FWD COMPARTMENT; RH SIDEWALL IAW 8 RM 53-30-15-0I-A

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT FLOOR STA 847 TO 867 R/H SIDE SHIELD (Z ANGLE) HAS CORROSION / REMOVED CORROSION AT AFT CARGO STA 847 TO 867 SIDE SHIELD IAW SRM 51-10-02-0G-0 ORIG T .050 REM T .030 LOSS OF .020 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED SIDE SHIELD PN 146A8127YS IAW SRM 51-40-02-0G-0 AND DWG 146A8127 REV C.

Part: STRAP — CORRODED (BS 790-812) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO DOOR SURROUND STRUCTURE STRAP CORRODED BETWEEN BS 790 TO 812, RBL 20. R & R STRAP IAW SRM AND DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CRACKED BETWEEN BS 727E TO BS 767, RBL 13. R&R TRACK IAW SRM.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE R/H SIDE SHIELD (Z ANGLE) STA 767 TO STA 792 RBL 22 HAS CORROSION / BLENDED OUT CORROSION AT AFT CARGO COMPARTMENT FLOOR STRUCTURE R/H SIDE SHIELD STA 767 TO 792 RBL 22 IAW B737-700 SRM 51-10-02-0G-0 MAT LOSS WAS 0.008' ORIGINAL THICKNESS 0.050' THE MATERIAL REMAINING 0.042' THE AREA FOUND TO BE OUT OF LIMITS '10%' - 0.005' IAW B737-700 SRM 53-00-53-1A-2 LOCATED AND DRILLED AND INSTALLED NEW SHIELD IAW DWG 146A0081 REV B ATAG WN2836

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT FLOOR PANEL SPLICE STA 887 HAS CORROSION / AFT CARGO COMPARTMENT FLOOR PANEL SPLICE STA 887 HAS CORROSION BLENDED CORROSION AND FOUND 100% MATERIAL LOSS FOUD TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED SPLICE WITH NEW SPLICE IAW SRM 51-40-02-0G-0 AND BOEIG DGW # 146A9401

Part: STRAP — CORRODED (FWD CARGO LH) · airframe 63,472 hrs · 37,083 cycles

FWD CARGO COMPT; LH SIDEWALL TO FLOOR STRAPS ARE CORRODED. / EVALUATED CORROSION LENGTH MORE THAN 3.0 INCHES;FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-53-1A-1 5(B)1) RECEIVED NEW FLOOR STRAPS P/N 453A1611-10 AND -11;AAGS WN3649;A92316 IAW BOEING DRAWING 453A1611 REV B

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED AT BS 772, LBL 3. REPAIRED FLOOR TRACK IAW EA.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT AFT BULKHEAD STA 947 LOWER BULKHEAD SUPPORT ANGLE HAS CORROSION ON TOP AND BOTTOM SURFACE / REMOVED CORROSION/VERIFIED LIMITS(FOUND TO BE 100% OUT OF LIMITS) IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED AFT BULKHEAD STA 947 LOWER BULKHEAD SUPPORT ANGLE IAW BOEING DWG#149A8118 REV D/SRM 51-40-02-0G-0 STEP 4 AND 7 ATAG #WN4242

Part: STRIP — DEFORMED (AFT CARGO) · airframe 63,472 hrs · 37,083 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT FWD BULKHEAD STA 727+4 LOWER BULKHEAD SUPPORT P/N 453A2611-25 IS GOUGED AND DEFORMED / REMOVED AND REPLACED AFT CARGO CPMPARTMENT FWD BULKHEAD STA 727+4 LOWER SUPPORT CAP STRIP P/N: 453A2611-25 AND STIFFNER PLATE P/N: 453A2611-12 IAW B737IPC:25-52-10-02. ISSUE TAGS: A90551 AND OPO 484

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO FLOOR TRACK CORRODED BETWEEN BS 927 TO BS 947, LBL 3. R&R SUPPORT TRACK IAW DWG AND SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED AT BS 772, LBL 17. REPAIRED FLOOR TRACK IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,472 hrs · 37,083 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED AT BS 772, RBL 8. REPAIRED FLOOR TRACK IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,472 hrs · 37,083 cycles

LT WING NR 3 LEADING EDGE SLAT LOWER SURFACE OF THE LE NOSE SKIN AT ACTUATOR CRACKED AT FASTENER HOLE. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,391 hrs · 37,030 cycles

LT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB IAW SRM.

Part: PANEL — DELAMINATED (TE FLAP) · airframe 63,110 hrs · 36,851 cycles

LT WING INBOARD MAIN FLAP OUTBOARD AFT WEDGE PANEL UPPER SURFACE DELAMINATED. REPAIRED MAIN FLAP PER EA.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 62,030 hrs · 36,242 cycles

L1 DOOR EXIT SIGN LENS NEAR FORWARD CABIN JUMPSEAT FELL OFF. R&R LENS PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,944 hrs · 36,183 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R THE BULB IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 59,630 hrs · 34,789 cycles

R1 DOOR EMER EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: MOUNT — BROKEN (R1 DOOR) · airframe 58,798 hrs · 34,300 cycles

R1 DOOR EMER EVAC SLIDE CONTAINER AFT ATTACH POINT SHOCK MOUNTS BROKEN. R & R MOUNTS IAW SRM.

Part: FLAP — FAULTY (LT WING) · airframe 57,840 hrs · 33,740 cycles

AIR RETURN, NR 1 KRUEGER INDICATOR DOWN IN FLIGHT WITH ASSOCIATED LE FLAP TRANSIT LIGHT. R & R NR 1 KRUEGER FLAP IAW MM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 57,267 hrs · 33,402 cycles

LEFT HORIZONTAL STABILIZER, 3RD RIB VERTICAL STIFFENER, CRACKED AT STAB STATION 129.5. AT LOWER END. R & R STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 57,267 hrs · 33,402 cycles

RIGHT HORIZONTAL STABILIZER, FWD RIB VERTICAL STIFFENER CRACKED AT STAB STATION 92.7 LOWER END. REPAIRED STIFFENER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,267 hrs · 33,402 cycles

RIGHT HORIZONTAL STABILIZER AFT RIB CRACKED, VERTICAL STIFFENER AT STAB STATION 92.7, AT LOWER END. REPAIRED RIB IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 57,267 hrs · 33,402 cycles

LEFT HORIZONTAL STABILIZER, 3RD RIB VERTICAL STIFFENER AT STAB STATION 92.7, CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,267 hrs · 33,402 cycles

RIGHT HORIZONTAL STABILIZER FWD RIB CRACKED, VERTICAL STIFFENER AT STAB STATION 129.57, AT LOWER END. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,267 hrs · 33,402 cycles

RIGHT HORIZONTAL STABILIZER RIB, LOWER HORIZONTAL STIFFENER, AT STAB STATION 129.5 CRACKED. REPAIRED RIB IAW EA & ER.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,267 hrs · 33,402 cycles

RIGHT HORIZONTAL STABILIZER 2ND RIB CRACKED, VERTICAL STIFFENER AT STAB STATION 92.7, AT LOWER END. REPAIRED RIB IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 57,267 hrs · 33,402 cycles

LEFT HORIZONTAL STABILIZER, 2ND RIB VERTICAL STIFFENER AT STAB STATION 92.7, CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 57,267 hrs · 33,402 cycles

LEFT HORIZONTAL STABILIZER, FWD RIB VERTICAL STIFFENER AT STAB STATION 92.7, CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,267 hrs · 33,402 cycles

RIGHT HORIZONTAL STABILIZER 3RD RIB CRACKED, VERTICAL STIFFENER AT STAB STATION 92.7, AT LOWER END. REPAIRED RIB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 9R. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

FRAME CRACKED AT BS 907, RT SIDE. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

LEFT FRAME CRACKED AT BS 787. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,267 hrs · 33,402 cycles

FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 57,267 hrs · 33,402 cycles

VERTICAL WEB CRACKED AT BS 663, RBL 38. REPAIRED WEB IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 56,887 hrs · 33,193 cycles

EMERGENCY LIGHT BATTERY M1675 FAILED CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 56,887 hrs · 33,193 cycles

EMERGENCY LIGHT BATTERY M1670 FAILED CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 56,887 hrs · 33,193 cycles

EMERGENCY LIGHT BATTERY M1673 FAILED CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 56,887 hrs · 33,193 cycles

EMERGENCY LIGHT BATTERY M1668 FAILED CHECK. R & R BATTERY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,025 hrs · 31,551 cycles

LEFT EMER EXIT SIDEWALL LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,635 hrs · 31,326 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,537 hrs · 31,265 cycles

LEFT EMER EXIT SIDEWALL LIGHT INOPERATIVE. RE-LAMPED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,038 hrs · 29,789 cycles

FWD EMERGENCY EXIT LIGHTS INOPERATIVE. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,038 hrs · 29,789 cycles

AFT EMERGENCY EXIT LIGHTS INOPERATIVE. RELAMPED IAW MM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,776 hrs · 29,633 cycles

RT NR 3 WINDOW E-F POST CRACKED AT NR 8 FASTENER HOLE. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,776 hrs · 29,633 cycles

RT NR 3 WINDOW E-F POST CRACKED AT NR 7 FASTENER HOLE. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,776 hrs · 29,633 cycles

LT NR 3 WINDOW E-F POST CRACKED AT NR 7 FASTENER HOLE. REPAIRED POST IAW EA.

Part: SLAT — CRACKED (RT WING) · airframe 50,776 hrs · 29,633 cycles

RT WING NR 7 SLAT CRACKED AT FASTENER AT ACTUATOR ATTACH POINT. REPAIRED SLAT IAW SRM.

Part: SLAT — CRACKED (RT WING) · airframe 50,776 hrs · 29,633 cycles

RT WING NR 8 SLAT CRACKED AT FASTENER AT ACTUATOR ATTACH POINT. REPAIRED SLAT IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,776 hrs · 29,633 cycles

LT NR 3 WINDOW E-F POST CRACKED AT NR 8 FASTENER HOLE. REPAIRED POST IAW EA.

Part: SUPPORT — CRACKED (RT WING) · airframe 50,775 hrs · 29,632 cycles

RT WING INBD AFT SPAR FWD ATTACH BRACKET FOR WING TO BODY LONGITUDINAL SUPPORT CRACKED. R & R SUPPORT IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,775 hrs · 29,632 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT RIB BETWEEN BS 129.5, 10' TO 17.5". REPAIRED RIB IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 50,775 hrs · 29,632 cycles

LT HORIZONTAL STABILIZER SKIN CRACKED AT RIB BS 29.5 TO BS 138.7 FWD OF AFT SPAR. REPAIRED RIB IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,420 hrs · 29,404 cycles

FWD RT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. R&R BATTERY PACK IAW AMM.

Part: COVER — BROKEN (CABIN) · airframe 48,872 hrs · 28,513 cycles

ENTRY DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,230 hrs · 27,549 cycles

RIGHT OVERHEAD BIN EMERGENCY LIGHT INOP AT ROW 8. RELAMPED LIGHT ASSY IAW MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 43,944 hrs · 25,622 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED SIGN IAW MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,944 hrs · 25,622 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 43. REMOVED AND REPLACED T-CAP IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,944 hrs · 25,622 cycles

DURING SCHEDULED 2Y CHECK, FOUND AFT CARGO COMPARTMENT RT Z-ANGLE CORRODED BETWEEN BS 767 TO BS 797. REMOVED AND REPLACED Z-ANGLE IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 43,944 hrs · 25,622 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLIGHT DECK FLOOR CORRODED BETWEEN BS 260 TO BS 270, LBL 10 TO RBL 10. REPAIRED FLOOR IAW SRM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 43,944 hrs · 25,622 cycles

DURING SCHEDULED 12Y CHECK, FOUND CAPTAINS SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW MM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 43,944 hrs · 25,622 cycles

DURING SCHEDULED 12Y CHECK, FOUND FIRST OFFICERS SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,944 hrs · 25,622 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,944 hrs · 25,622 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,944 hrs · 25,622 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 43,938 hrs · 25,617 cycles

DURING SCHEDULED HC1 CHECK, LT AFT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 43,938 hrs · 25,617 cycles

DURING SCHEDULED HC1 CHECK, LT FWD BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 43,938 hrs · 25,617 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED AT I/B TRAILING EDGE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 41,183 hrs · 23,984 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: COVER — LOOSE (CABIN) · airframe 40,267 hrs · 23,479 cycles

FWD EEPLS COVER LOOSE. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,111 hrs · 23,388 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT EMERGENCY EXIT BULLNOSE LIGHT INOP. RELAMPED PER MM.

Part: FUSE — BLOWN (CABIN) · airframe 38,742 hrs · 22,637 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FUSE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,558 hrs · 21,895 cycles

RT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 10. RELAMPED PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 36,963 hrs · 21,540 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. REMOVED AND REPLACED FITTING PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 19Y CHECK, FOUND AFT CARGO COMPT FLOORBEAM CORRODED AT BS 773, RBL 5. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 770, RBL 10. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 771, BL 0. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 771, LBL 10. REPAIRED BEAM PER EA.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FITTING CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FITTING CRACKED AT BS 540, RBL 31. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING O/B AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FITTING CRACKED AT BS 540, RBL 54. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FITTING CRACKED AT BS 540, RBL 42. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FITTING CRACKED AT BS 540, LBL 31. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FITTING CRACKED AT BS 540, LBL 7.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER BOX) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FITTING CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,939 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FITTING CRACKED AT BS 540, RBL 7.5. REMOVED AND REPLACED FITTING PER SRM.

Part: FLAP — CRACKED (RT WING) · airframe 36,939 hrs · 21,527 cycles

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

Part: FITTING — LOOSE (GIRT BAR) · airframe 36,938 hrs · 21,527 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT FLOOR GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 36,432 hrs · 21,199 cycles

L1 DOOR EMERGENCY EXIT LIGHT LOWER SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,063 hrs · 20,979 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,780 hrs · 20,789 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT FITTING LUGS CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,780 hrs · 20,789 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT FITTING LUGS CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 35,131 hrs · 20,392 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 31,304 hrs · 18,034 cycles

RIGHT AFT CABIN EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 27,412 hrs · 15,742 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,948 hrs · 15,477 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,948 hrs · 15,477 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 16 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,948 hrs · 15,477 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 11 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — DISCHARGED (AFT GALLEY) · airframe 19,996 hrs · 11,565 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY IN AFT RT GALLEY DISCHARGED. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,869 hrs · 11,499 cycles

DURING SCHEDULED RON CHECK, FOUND LT & RT FWD EMERGENCY BULLNOSE LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,727 hrs · 10,805 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 13,967 hrs · 8,098 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. REMOVED AND REPLACED SLIDE PER MM.

Part: FASTENER — LOOSE (ENTRY DOOR) · airframe 11,940 hrs · 6,974 cycles

DURING SCHEDULED BC3 CHECK, FOUND LOOSE FASTENER AT FWD ENTRY DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK. REMOVED AND REPLACED FASTENER PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 10,588 hrs · 6,201 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING DOOR. REINSTALLED SLIDE PER MM.

Part: WIRE — EXPOSED (SERVICE DOOR) · airframe 6,063 hrs · 3,597 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE HAS EXPOSED WIRES. SECURED EMERGENCY EVAC SLIDE WIRES PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 6,063 hrs · 3,597 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. Removed and replaced LIGHT BALLAST PER MM.

Part: HINGE — WORN (RT ELEVATOR TAB) · airframe 5,712 hrs · 3,378 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 RT ELEVATOR TAB HINGE FITTING ASSY PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 4,973 hrs · 2,952 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT ROW 10. RECONNECTED WIRING PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 2,448 hrs · 1,454 cycles

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY AS PROVISONER WAS OPENING DOOR. REINSTALLED SLIDE ASSY PER MM.

Part: CONNECTOR — BURNED (E/E BAY) · airframe 2,265 hrs · 1,351 cycles

DURING SCHEDULED RON WHILE TROUBLESHOOTING APU INOP, FOUND APU START CONVERTER CONNECTOR D11114B BUNRNED. MX FERRIED ACFT TO DALLAS FOR REPAIR AND FOUND APU STARTER CONVERTER BOX CENTER MALE END CONNECTOR PARTIALLY BURNED, FEMALE CONNECTOR AT RACK ASSY TOTALLY BURNED WITH PIECES OF INSULATION MATERIAL MISSING AROUND PINS, AND WIRING MELTED BEHIND CONNECTOR. REMOVED AND REPLACED APU STARTER CONVERTER BOX AND RACK ASSY WITH WIRING HARNESS.

Part: DOOR — UNSECURED (PAX DOOR)

DURING CLIMB, AIRCRAFT WOULD NOT PRESSURIZE AND LOUD NOISE HEARD AROUND FWD ENTRY DOOR. DISCOVERED FWD ENTRY DOOR NOT FULLY CLOSED. OPERATED DOOR SEVERAL TIMES, OPS CHECK GOOD.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR)

AIR TURNBACK, AFT CARGO DOOR LIGHT ILLUMINATED DURING TAKEOFF AND CABIN PRESSURE RATE OF CLIMB SLOW. ADJUSTED AND LUBRICATED AFT CARGO DOOR LIGHT SWITCH PER MM. PRESSURIZED ACFT, NO LEAKS NOTED. OPS CK GOOD PER MM.