N7829B

Part: HANDLE — BROKEN (PAX DOOR) · airframe 64,891 hrs · 33,165 cycles

FWD ENTRY DOOR ASSIST HANDLE BROKE OFF. REMOVED AND REPLACED HANDLE IAW AMM 52-11-00.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 64,565 hrs · 32,952 cycles

LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED THE LIGHT ASSY IAW MM 33-51-01.

Part: NONE — BROKEN (R2 DOOR) · airframe 63,974 hrs · 32,545 cycles

AFT SERVICE DOOR EMERGENCY EXIT SIGN COVER BROKEN / [01] REPLACED AFT SERVICE DOOR EMERGENCY EXIT SIGN COVER PER AMM 33-51-01

Part: LIGHT — INOPERATIVE · airframe 63,011 hrs · 31,907 cycles

AFT OH CEILING LIGHT ABEAM LAST ROW INOP AFT OH CEILING LIGHT ABEAM LAST ROW / [01] RELAMPED AFT OVERHEAD CEILING LIGHTS OPS CHECK GOOD REFERENCE AMM33-22-00.

Part: LIGHT — INOPERATIVE · airframe 62,425 hrs · 31,545 cycles

LH ROW 1 CENTER CEILING FLOURECENT LIGHT INOP / [01] R&R LIGHT ASSY IAW AMM 33-22-00

Part: INDICATOR — INOPERATIVE (L/H OVERWING) · airframe 62,166 hrs · 31,386 cycles

LT. OVERWING LOWEREMERGENCY EXIT SIGN INOP. ; / [01] R & R INDICATOR ASSY I/A/W M/M 33-51-04.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 61,436 hrs · 30,960 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT ; 2021-466316 / [01] EVALUATED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT FOUND CRACK ( 1 EA )L=0.5820 INCH. CRACK MUST BE REPAIRED BY WELDING IAW BOEING 737-700 SRM 53-60-15-2R-1; REPAIR 1. PARAGRAPH 4.B. TOOL USED; DIGITAL CALIPER P/N:500-193-30 S/N:0000288 DUE DATE 23/NOV/21; [02] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.; [03] STEP 1 ENTRY BY ERROR; [04] TASK COMPLETED; [05] TASK COMPLETED

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMEN ; 2021-466315 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N B20189362; DUE DATE 23-NOV-21.; [02] REPAIRED CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.; [03] TASK COMPLETED.

Part: BRACKET — CRACKED (L/H WING) · airframe 61,436 hrs · 30,960 cycles

CRACK ON BRACKET LOC ON FRONT SPAR CUT OUT FWD BOOST PUMP IFFSS 120 AND WBL 94.24 AT LT WING. REPLACED BRACKET AND FASTENERS IAW SRM 51-40-02 AND DWG 112A2004 REV DWG 116A3001 REV .

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 61,436 hrs · 30,960 cycles

SUPPLEMENTAL INFORMATION: DELAMINATED FLOOR PANEL 231AF AT PASSENGER CABIN 2021-466201 / FAULT WAS RAISED IN ERROR. REFERENCE TTG8Q006UQGP FAULT WAS RAISED IN ERROR. REFERENCE TTG8Q006UQGP

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 61,436 hrs · 30,960 cycles

SUPPLEMENTAL INFORMATION: DELAMINATED FLOOR PANEL 232DF AT PASSENGER CABIN 2021-466206 / FAULT WAS RAISED IN ERROR. REFERENCE TTG8Q006UQJ8 FAULT WAS RAISED IN ERROR. REFERENCE TTG8Q006UQJ8

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

CRACK ACCESS PANEL 194E BODY FAIRING AROUND FASTENERS HOLES AT LOWER FUSELAGE ; 2021-466191 / [01] TOOL USED HOT BONDER P/N:HCS9200B-AV; S/N: 18196021; DUE DATE: 14-DEC-21.; [02] REPAIRED ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 REPAIR 8. TOOL USED CALIPER P/N:500-197-30 S/N:A18234364 DUE DATE: 25-SEP-22; HOT BONDER P/N:HCS9200B-AV; S/N: 18196021; DUE DATE: 14-DEC-21; HOTBONDER P/N:HCS9200B S/N:18165044 DUE DATE: 15-FEB-22; SCALE P/N; SCA-301 S/N: AE-412121 DUE DATE; 16-SEP-22. REFER TO INDIVIDUAL SIGN OFFS BELOW.; [03] TASK COMPLETED

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

CRACK FLOOR PANEL 221GF AT PASSENGER CABIN ; 2021-466215 / [01] REPLACED FLOOR PANEL 221GF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST; [02] CORRECTED STEP 1; REPLACED FLOOR PANEL 221GF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST IAW B737-700 AMM 53-21-00-400-801; [03] REPLACED FLOOR PANEL 221GF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST IAW B737-700 AMM 53-21-00-400-801

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

CRACK FLOOR PANEL 221EF AT PASSENGER CABIN ; 2021-466216 / [01] REPLACED FLOOR PANEL 221EF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST; [02] CORRECTED STEP 1; REPLACED FLOOR PANEL 221EF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST IAW B737-700 AMM 53-21-00-400-801; [03] REPLACED FLOOR PANEL 221EF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST IAW B737-700 AMM 53-21-00-400-801

Part: WEB — CRACKED (FWD GALLEY) · airframe 61,436 hrs · 30,960 cycles

CRACK WEB LOCATED BTW BS277 TO BS294.5 AND BL0 AT FWD GALLEY AREA ; 2021-466135 / [01] REPLACED WEB AND FASTENERS LOCATED BTW BS277 TO BS294.5 AND BL0 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. DRAWING 141A5400 REV. A.LENGTH OF CRACK IS: 3 INCHES TOOL USED CALIPER P/N:500-464; S/N:11452551; DUE DATE:13-FEB-22. SEE INDIVIDUAL SIGNOFFS BELOW; [02] CERTIFIED WORK PERFORMED RII.<BR>SEE INDIVIDUAL SIGNOFFS BELLOW.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

CRACK ENTRY DOOR CUT OUT STRINGER 7L AND BS 294.5 AT FWD GALLEY AREA ; 2021-466120 / [01] TOOK MEASURE OF THE CRACK IS L: 1.056 INCH ; LOCATED ENTRY DOOR CUT OUT STRINGER 7L AND BS 294.5 AT FWD GALLEY AREA ; P/N STRINGER AFFECTED IS 141A3120-12 IAW SRM B737-700 53-10-03-0I -1 FIG 2 ; TABLE 2 ;TOOL USED : CALIPER ; P/N : 700-113-10 ; S/N : 0016732 ; DUE DATE : 01/APR/22; CORRECTED STEP 37: PERFORMED REPAIR ON ENTRY DOOR CUT OUT STRINGER 7L AND BS 294.5 AT FWD GALLEY AREA IAW B737-700 SRM 53-00-03-2R-1. THIS REPAIR IS CATEGORY B AND FUTURE INSPECTION MUST BE REQUIRED. TOOL USED CALIPER ; P/N : 700-113-10 ; S/N : 0016732 ; DUE DATE : 01/APR/22. PERFORMED ULTRASONIC THICKNESS MEASURE DONE ON STRINGER 7L BS 294.5 IS 0.056 INCH. IAW NDT MANUAL 51-00-00 PART 4 PROCEDURE 3. TOOL USED: ULTRASONIC THICKNESS GAGE, P/N: 45MG, S/N: 130064101, CAL DUE DATE: 11-MAR-22 AND HFEC INSPECTION DONE ON CUT OUT EDGE AS PER BOEING NDT MANUAL 51-00-00 PART 6 PROCEDURE 23. CRACK INDICATIONS NOT FOUND. TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X1693P030456 DUE DATE: 30-NOV-21.MATERIAL USED: STRINGER SECTION(1E/A) IS: 7075T0-0.056 P/O: 2021 127971 AND CHANNEL(1E/A) , ANGLE(2E/A) IS: 7075T0-0.063 P/O: 2021 129486 SEE INDIVIDUAL SIGNOFFS BELOW.

Part: NONE — CRACKED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

CRACK INNER CHORD LOCATED BS303.9 AND STRINGER 17L AT FWD GALLEY AREA ; 2021-466134 / [01] TOOK MEASURE OF THE CRACK ON INNER CHORD IS L : 0.850 INCH LOCATED BS303.9 AND STRINGER 17L AT FWD GALLEY AREA ; P/N INNER CHORD AFFECTED IS 141A8112-1 IAW B737-700 SRM 53-10-15-0I-1 FIGURE 5 ; TABLE 4 AND DRAWING # 141A8110 REV - ; TOOL USED : CALIPER ; P/N : 700-113-10 ; S/N : 0023208 ; DUE DATE : 31/DEC/21; [22] REPLACED INNER CHORD LOC BTW BS 270 TO BS 360 STR 17L IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 140A9810 REV: - AND 141A8110 REV: -; [23] STEP 21 COMPLETED; [24] CERTIFIED WORK PERFORMED RII

Part: NONE — CRACKED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

SUPPLEMENTAL INFORMATION: CRACK FLOOR BEAM LOCATED BS294.5 AND RBL57 AT FWD GALLEY AREA 2021-466136 / EVALUATED ALLOWABLE DAMAGE FOR CRACK ON FLOOR BEAM LOCATED BS294.5 AND RBL57 AT FWD GALLEY AREA AND NO FOUND REFERENCE ALLOWABLE DAMAGE FOR CRACK ON FLOOR BEAM UPPER CHORD, FLOOR BEAM MUST BE REPAIR. PERFORMED CUT AND REMOVED DAMAGED PART OF THE UPPER CHORD OF THE FLOOR BEAM 294.5 AND BTW RBL 25 TO RBL 60 IAW SRM B737-700 53-10-51-2R-16 REPAIR 16 ALTERNATIVE 2 FIG 202 DETAIL G AND PERFORMED VISUAL INSPECTION ON ADJACENT STRUCTURES AND NOT FOUND DAMAGE. MADE, DRILLED AND COUNTERSINKS REPAIR PARTS: [1] REPAIR CHORD, [2] ANGLES 2E/A, [3] STRAP, [4] TAPERED FILLER 2E/A, [5] TAPERED FILLER 2E/A, [6] FILLER, [7] SHIM AND [8] SHIM IAW SRM B737-700 53-10-51-2R-16 REPAIR 16 ALTERNATIVE 2. INSTALLED REPAIR PARTS: [1] REPAIR CHORD, [2] ANGLES 2E/A, [3] STRAP, [4] TAPERED FILLER 2E/A, [5] TAPERED FILLER 2E/A, [6] FILLER, [7] SHIM AND [8] SHIM IAW SRM B737-700 51-40-02 AND 53-10-51-2R-16 REPAIR 16 ALTERNATIVE 2. INSTALLED FASTENERS AND INTERCOSTAL AND STIFFENER BTW BS 294.5 TO BS 312, RBL 25 AND RBL 43 AND ANGLE LOC FLOOR BEAM BS 294.5 BTW RBL 15 TO RBL 60 IAW SRM B737-700 51-40-02 AND 53-10-51-2R-16 REPAIR 16 ALTERNATIVE 2 AND DRAWING 141A5400 REV.- AND 141A5502 REV.-

Part: PLATE — CRACKED (L/H WING) · airframe 61,436 hrs · 30,960 cycles

CRACK CORRUGATED PLATE TRAILING EDGE AT LT WING (1 EA) ; 2021-466113 / [01] REPLACED CORRUGATED PLATE AND FASTENER LOC.TRAILING EDGE AT LT WING (1 EA). IAW B737-700 SRM 51-10-02 ITEM: 9 AND DWG:115A2001 REV: - PART USED: 115A2781-13ATSMRO.; [02] CORRECTED STEP 1.<BR>REPLACED CORRUGATED PLATE AND FASTENER LOC.TRAILING EDGE AT LT WING (1 EA). IAW B737-700 SRM 51-10-02 ITEM: 9 AND DWG:115A2001 REV: - PART USED: 115A2781-13ATSMRO. SEE INDIVIDUAL SING OFF BELOW.; [03] TASK COMPLETED ; INDIVIDUAL SING OFF BELOW.

Part: ACCESS PANEL — BROKEN (VERTICAL STAB) · airframe 61,436 hrs · 30,960 cycles

BROKEN ACCESS PANEL 324AL ANGLE AT VERTICAL STABILIZER. REPLACED ACCESS PANEL 324AL ANGLE AT VERTICAL STABILIZER IAW SRM B737-700 51-40-02 AND 51-10-02 ITEM 9.

Part: STUB FRAME — CRACKED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

CRACK FLOOR STRUCTURE STUD FRAME LOCATED BS 294.5 AND STRINGER 17R AT FWD GALLEY AREA ; 2021-466119 / [01] CRACK FLOOR STRUCTURE STUD FRAME LOCATED BS 294.5 MUST BE REPAIR DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700; [21] INSTALLED CLIP FLOOR STRUCTURE STUD FRAME LOCATED BS 294.5 AND STRINGER 17R AT FWD GALLEY AREA IAW B737-700SRM 51-40-02 AND DWG 141A370 SHEET 9 REV D.; [22] CRRECTED STEP 21. INSTALLED CLIP FLOOR STRUCTURE STUD FRAME LOCATED BS 294.5 AND STRINGER 17R AT FWD GALLEY AREA IAW B737-700SRM 51-40-02 AND DWG 141A8370 SHEET 9 REV D.; [23] COMPLETE STEP 22 RII; [24] REPAIR FLOOR STRUCTURE STUD FRAME LOCATED BS 294.5 AND STRINGER 17R AT FWD GALLEY AREA IAW B737-700 SRM 53-10-15-2R-7.; [25] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELLOW

Part: ANGLE — CRACKED (L/H WING) · airframe 61,436 hrs · 30,960 cycles

CRACK ANGLE TRAILING EDGE BETWEEN WS 236 TO WS 285 ON REAR SPAR LT WING ; 2021-466068 / [01] REPLACED ANGLE LOCATED ON TRAILING EDGE BETWEEN WS 236 TO WS 285 ON REAR SPAR LT WING. IAW B737-700 SRM 51-40-02 AND IPC 57-50-00-25.; [02] COMPLETE TASK CERTIFIED

Part: GUSSET — CRACKED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

CRACK GUSSET STR 19R BS 500D FWD CARGO COMPARTMENT ; 2021-466067 / [01] REMOVED GUSSET AND FASTENER IAW SRM 51-40-02 LOC AT STR 19R BS 500D; DUE TO NO FOUND ALLOWABLE DAMAGE ON SRM; AND GUSSET MUST BE REPLACED. PERFORMED VISUAL INSPECTION ON AREA AND NO FOUND MORE DAMAGE.; [02] REPLACED GUSSET AND FASTENERS LOCATED STR 19R BS 500D FWD CARGO COMPARTMENT I.A.W B737-700 51-40-02 AND DRAWING 143A7902 REV. A MEASURE OF CRACK IS L=0.472 INCHES; [03] ENTERED IN ERROR STEP 1; [04] REPLACED GUSSET AND FASTENERS LOCATED STR 19R BS 500D FWD CARGO COMPARTMENT I.A.W B737-700 51-40-02 AND DRAWING 143A7902 REV. A.; [05] CORRECTED STEP 4 ; REPLACED GUSSET AND FASTENER LOCATED STR 19R BS 500D FWD CARGO COMPARMENT I.A.W B737-700 51-40-02 AND DRAWING 143A7902 REV.A ; SEE INDIVIDUAL SIGNOFFS BELLOW.; [06] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELLOW

Part: PANEL — ELONGATED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

ELONGATED HOLE ACCESS PANEL 194E AT LOWER FUSELAGE ; 2021-466076 / [01] REPAIRED ACCESS PANEL 194E AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 REPAIR 8. TOOL USED: CALIPER P/N:500-197-30; S/N:A18234364; DUE DATE: 25-SEP-22; HOT BONDER P/N:HCS9200B-AV; S/N: 18196021; DUE DATE: 14-DEC-21; HOTBONDER P/N:HCS9200B S/N:18165044 DUE DATE: 15-FEB-22; SCALE P/N; SCA-301 S/N: AE-412121 DUE DATE; 16-SEP-22. REFER TO INDIVIDUAL SIGN OFFS BELOW.; [02] TASK COMPLETED

Part: PANEL — ELONGATED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

ELONGATED HOLE ACCESS PANEL 193B AT LOWER FUSELAGE ; 2021-466063 / [01] TOOL USED: CALIPER P/N:500-197-30; S/N:A18234364; DUE DATE: 25-SEP-22.; [02] TOOL USED HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 15-FEB-22; [03] TOOL USED: MULTIMETER P/N: FLUKE 87; S/N: 95740102; DUE DATE: 24-OCT-22; [04] REPAIRED ACCES PANEL 193B AS PER B737-700 SRM 51-70-05-2R-8 REPAIR 8 SEE INDIVIDUAL SIGNOFFS BELOW.; [05] TASK COMPLETED.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

DELAMINATED ACCESS PANEL 192AR AT LOWER FUSELAGE ; 2021-466054 / [01] APPLIED CONDUCTIVE COATING ON REPAIR AREAS ON ACCESS PANEL 192AR AS PER B737-700 SRM 51-70-05-2R-1 REPAIR 1 PARA. 4.G. AND B737-700 SRM 51-70-05-2R-0 REPAIR GENERAL PARA. 4.O. TOOL USED: MULTIMETER P/N: FLUKE 87 S/N: 95100198. DUE DATE: 15-JAN-22.; [02] REPAIRED ACCESS PANEL 192AR AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-1 REPAIR 1. TOOL USED CALIPER P/N: 500-197-30; S/N:A18234364; DUE DATE: 25/SEP/22; HOT BONDER P/N HCS9200B; S/N 18175478; DUE DATE: 05-AUG-22; HOTBONDER:P/N:HCS9200B-AV S/N:18196126 DUE DATE:27-JAN-22; MULTIMETER P/N: FLUKE 87 S/N: 95100198. DUE DATE: 15-JAN-22. SEE INDIVIDUAL SIGN OFFS BELOW.; [03] INSPECTED AND VERIFIED TASK.SEE INDIVIDUAL SIGN OFFS BELOW

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

CRACK SUPPORT ANGLE LOCATED AT BS 690 BL 0 FWD SIDE CENTER SECTION ; 2021-466000 / [01] REMOVE SUPPORT ANGLE LOCATED AT BS 690 BL 0 FWD SIDE CENTER SECTION IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO FOUND MORE DAMAGE.; [02] STEP 1 ENTER IN ERROR; [03] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: 38615K71; S/N: AE-40585; DUE DATE: 07-JUL-22.; [04] REPLACED SUPPORT ANGLE LOCATED AT BS 690 BL 0 FWD SIDE CENTER SECTION IAW B737-700 51-40-02.<BR>SEE INDIVIDUAL SIGNOFFS BELOW.; [05] REPLACED SUPPORT ANGLE LOCATED AT BS 690 BL 0 FWD SIDE CENTER SECTION IAW B737-700 51-40-02. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SKIN — DEBONDED (L/H WING) · airframe 61,436 hrs · 30,960 cycles

CUSTOMER REQUEST - DEBONDED OB AFT FLAP EXTERNAL SKIN LOWER SURFACE LOCATED AT INBOARD CORNER ON LT WING ; 2021-466030 / [01] EVALUATED DAMAGED ON OUTBOARD AFT FLAP EXTERNAL SKIN LOWER SURFACE LOCATED AT INBOARD CORNER ON LT WING AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 SRM 57-53-01-2R-14 REPAIR 14 PARAGRAPH 1 ITEM C AND TABLE 201 AND MUST BE REPAIR IAW B737-700 51-70-10-2R-4 REPAIR 4 FIGURE 202 SHHET 3 AND B737-700 SRM 51-70-10 -2R-0 GENERAL REPAIR DAMAGE SIZE IS L:1.28INCH W:1INCH TOTAL DAMAGE AREA IS 1.28SI TOOL USED CALIPER P/N:500-197-30 S/N:15121570 DUE DATE: 01AUG22; [23] REPAIRED OB AFT FLAP EXTERNAL SKIN LOWER SURFACE LOCATED AT INBOARD CORNER ON LT WING AS PER,NG,NRC,2021-10-16 19:17:07,18Y,Y,MX,0,0,,CUSTOMER REQUEST - DEBONDED OB AFT FLAP EXTERNAL SKIN LOWER SURFACE LOCATED AT INBOARD CORNER ON LT WING ; 2021-466030"

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

CRACK SUPPORT ANGLE LOCATED AT BS 690 RBL 24.5 CENTER SECTION ; 2021-466004 / [01] REMOVE SUPPORT ANGLE LOCATED AT BS 690 RBL 24.5 CENTER SECTION IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO FOUND MORE DAMAGE; [02] STEP 1 ENTER ERROR .; [03] MADE REPAIR SUPPORT ANGLE AND PERFORM DRILL LOCATED AT BS 690 RBL 24.5 CENTER SECTION IAW B737-700 SRM 51-40-05 AND DWG 273A9112 ITEM 45 SHEET 3AND SHEET 7-8 REV H AND BAC1490-2782 PO 202119255000101; [04] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: 38615K71; S/N: AE-40585; DUE DATE: 07-JUL-22.; [05] STEP 3 ENTER BY ERROR; [06] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT BS 690 RBL 24.5 CENTER SECTION IAW B737-700 SRM 51-40-02 DWG 111A6000 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.; [07] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT BS 690 RBL 24.5 CENTER SECTION IAW B737-700 SRM 51-40-02 DWG 111A6000 REV -. SEE INDIVIDUAL SIGN OFFS BELOW. COMPLETED.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 61,436 hrs · 30,960 cycles

SUPPLEMENTAL INFORMATION: DELAMINATED FLOOR PANEL 242CF AT PASSENGER CABIN 2021-465808 / REPLACED FLOOR PANEL 242CF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST IAW B737-700 AMM 53-21-00-400-801 CERTIFIED WORK PERFORMED

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 61,436 hrs · 30,960 cycles

CRACK INSPAR RIB LOCATED AT STAB STA 92.70 AND 21 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER. REPAIRED INSPAR RIB LOCATED AT STAB STA 92.70 AND 21 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 55-10-09-2R-4 CORRECTED STEP 5: REPAIRED INSPAR RIB LOCATED AT STAB STA 92.70 AND 21 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 55-10-09-2R-4.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

DELAMINATED FLOOR PANEL 241FF AT PASSENGER CABIN ; 2021-465816 / [01] REPLACED FLOOR PANEL 241FF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST IAW B737-700 AMM 53-21-00-400-801; [02] CORRECTED STEP 1; REPLACED FLOOR PANEL 241FF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST IAW B737-700 AMM 53-21-00-400-801; SEE INDIVIDUAL SIGNOFFS BELLOW; [03] REPLACED FLOOR PANEL 241FF AT PASSENGER CABIN DUE TO CUSTOMER REQUEST IAW B737-700 AMM 53-21-00-400-801; SEE INDIVIDUAL SIGNOFFS BELLOW. RII

Part: FLOOR PANEL — ELONGATED (FUSELAGE) · airframe 61,436 hrs · 30,960 cycles

ELONGATED HOLE FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT ; 2021-465625 / [01] FABRICATED NEW PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-05 ; 51-40-08 AND DWG 453A2610 SHEET 20 REV E. MATERIAL USED: 2024T3 THICKNESS: 0.071 INCHES; PO: 2021-111049. SEE INDIVIDUAL SIGN OFFS BELOW.; [02] TASK COMPLETED <BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: FITTING — CORRODED (L/H MLG W/W) · airframe 61,322 hrs · 30,886 cycles

LT MLG FWD TRUNNION SUPPORT FITTING; LOWER OTBD (#3);INNER FACE HAS EVIDENCE OF CORROSION. ; / [01] REPAIRED PER. EA 1-A57-3246 REV. 14

Part: SUPPORT FITTING — CORRODED (L/H MLG W/W) · airframe 61,322 hrs · 30,886 cycles

LT MLG FWD TRUNNION SUPPORT FITTING; LOWER INBD (#4);INNER FACE HAS EVIDENCE OF CORROSION. ; / [01] REPAIRED PER. EA 1-A57-3246 REV. 14

Part: FITTING — CORRODED (L/H MLG W/W) · airframe 61,322 hrs · 30,886 cycles

LT MLG FWD TRUNNION SUPPORT FITTING; LOWER OTBD (#3);INNER FACE HAS EVIDENCE OF CORROSION. ; / [01] REPAIRED PER. EA 1-A57-3246 REV. 14

Part: FITTING — CORRODED (L/H MLG W/W) · airframe 61,322 hrs · 30,886 cycles

LT MLG FWD TRUNNION SUPPORT FITTING; LOWER INBD (#4);INNER FACE HAS EVIDENCE OF CORROSION. ; / [01] REPAIRED PER. EA 1-A57-3246 REV. 14

Part: HOOK AND LOOP — LOOSE (R1 DOOR SLIDE) · airframe 60,231 hrs · 30,279 cycles

FWD SERVICE DOOR ESCAPE SLIDE VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF. ; / REATTACHED FWD SERVICE DOOR ESCAPE SLIDE VELCRO STRIP ON THE GIRT TO VELCRO STRIP ON THE BACKING PAN SHELF PER AMM 25-66-01.

Part: HOOK AND LOOP — LOOSE (R2 DOOR SLIDE) · airframe 60,231 hrs · 30,279 cycles

AFT SERVICE DOOR ESCAPE SLIDE VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF. ; / RE-ATTACHED AFT SERVICE DOOR ESCAPE SLIDE VELCRO STRIP ON THE GIRT TO VELCRO STRIP ON THE BACKING PAN SHELF PER AMM 25-66-01.

Part: HOOK AND LOOP — LOOSE (L2 DOOR SLIDE) · airframe 60,231 hrs · 30,279 cycles

AFT ENTRY DOOR ESCAPE SLIDE VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF. ; / REATTACHED AFT ENTRY DOOR ESCAPE SLIDE VELCRO STRIP ON THE GIRT TO VELCRO STRIP ON THE BACKING PAN SHELF PER AMM 25-66-01.

Part: WEB — CRACKED (RT WING) · airframe 58,807 hrs · 29,461 cycles

RIGHT WING WEB AT FIXED TRAILING EDGE PANEL APPROXIMATELY WS 270 HAS CRACKED FITTING. R & R RIGHT WING WEB, IAW SRM 51-40-02.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 57,469 hrs · 28,629 cycles

LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 57,469 hrs · 28,629 cycles

RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM53-31-31.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,913 hrs · 28,285 cycles

L2 DOOR UPPER EMERGENCY EXIT LIGHT INOP. / R&R BATTERY PACK M1672 PER AMM.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 56,913 hrs · 28,285 cycles

R/W ON DEFLECTOR PANEL; ATTACH TO TRANSVERSE WEB AFT BRACKET BULB SEAL IS CRACK. / REMOVED CRACK DAMAGED BRACKET AT R/W DEFLECTOR PANEL IAW SOPM 20-50-01 REMOVED SEAL RETAINER IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-05-0G-0 INSTALLED SEAL RETAINER ON BRACKET IAW SRM 51-40-02-0G-0 INSTALLED AT R/W DEFLECTOR PANEL IAW SOPM 20-50-01 1356R 16NOV19

Part: BATTERY CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,913 hrs · 28,285 cycles

R2 DOOR UPPER EMERGENCY EXIT LIGHT INOP. / R&R BATTERY PACK M1672 PER AMM.

Part: PLATE — CRACKED (AFT CARGO) · airframe 56,913 hrs · 28,285 cycles

AFT CARGO BAY STIFFENER PLATE COMMON TO FWD FLOOR PANEL BS 727+8' RBL 2 WL 156 IS CRACKED / REMOVED AND REPLACED AFT CARGO PLATE COMMON TO FWD FLOOR PANEL 135 727+8' RBL 2 WL 156 RECEIVED NEW STIFFENER ON PO 769532 INSTALLED PER AMM TASK 25-52-10-400-800 92849U 14NOV19

Part: FRAME — CRACKED (BS 312) · airframe 56,913 hrs · 28,285 cycles

FRAME CRACKED AT BS. 312, ABOVE STR. 5L. / REPAIRED FRAME PER ER AND EA.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 56,913 hrs · 28,285 cycles

P18 MOUNT SUPPORT CLIP CRACKED AT BS 259 STRINGER 8 LT. / REMOVED AND SUPPORT CLIP AT BS 259 STR 8 LT IAW SRM 51-40-02 AND DWG# 141A9502.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 56,913 hrs · 28,285 cycles

R/H HORIZONTAL STABILIZER RIB ASSEMBLY 5 STAB. STA. 129.50 UPPER CHORD CRACKED JUST FORWARD OF 3RD VERTICAL STIFFENER. / REPAIRED RIB ASSEMBLY PER ER & EA.

Part: SUPPORT — CORRODED (BS 947) · airframe 56,913 hrs · 28,285 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED AT BS. 947, RBL 21. / R&R SUPPORT PER SRM, AMM, & DWG.

Part: SUPPORT — CORRODED (BS 727-767) · airframe 56,913 hrs · 28,285 cycles

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

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 56,913 hrs · 28,285 cycles

VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT BS. 663, BETWEEN LBL 30 TO LBL 70. / R&R ANGLE IAW SRM.

Part: MOUNT — CORRODED (GIRT BAR) · airframe 56,913 hrs · 28,285 cycles

GIRT BAR MOUNT CORRODED AT BS 312 LBL 50 WL 208 IS / R&R MOUNT PER DWG.

Part: WEB — CORRODED (BS 440-494) · airframe 56,913 hrs · 28,285 cycles

FORWARD CARGO BAY SUB WEB THRESHOLD CORRODED BETWEEN BS. 440 TO BS. 494, RBL 27. / R&R WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 420-440) · airframe 56,913 hrs · 28,285 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 420 TO BS. 440, RBL 24. / R&R SUPPORT IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 56,913 hrs · 28,285 cycles

FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO LBL 25. R&R FLOOR SUPPORT PER SRM AND DWG.

Part: FRAME — CRACKED (BS 259) · airframe 56,913 hrs · 28,285 cycles

FRAME WEB CRACKED AT BS. 259, STR. 9L AT STRINGER CUTOUT. / REPAIRED FRAME WEB PER ER AND EA.

Part: SKIN — CORRODED (TAIL) · airframe 56,913 hrs · 28,285 cycles

***CORROSION*** ON FUSELAGE SKIN; UNDER DORSAL FIN; AT B.S. 887-1007; W.L. 306.5. / REPAIRED CORROSION DAMAGE ON FUSELAGE SKIN UNDER DORSAL FIN; AT BS 887-1007. WL 306.5 PER ER# 19-05337 REV IR AND EA #1-753-35956 REV IR.

Part: SUPPORT — CORRODED (BS 500D) · airframe 56,913 hrs · 28,285 cycles

FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED AT BS. 500D, LBL 14. / R&R SUPPORT PER SRM & DWG.

Part: SUPPORT — CORRODED (BS 400-495) · airframe 56,913 hrs · 28,285 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 400 TO BS. 495, LBL 24. / R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 56,913 hrs · 28,285 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 500A TO BS. 500D, RBL 24. / R&R SUPPORT PER SRM & DWG.

Part: SUPPORT — CORRODED (BS 494-500A) · airframe 56,913 hrs · 28,285 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 494 TO BS. 500A, RBL 24. / R&R SUPPORT IAW SRM AND DWG.

Part: CAP — CORRODED (AFT CARGO) · airframe 56,913 hrs · 28,285 cycles

***CORROSION*** ON AFT CARGO BAY L/H CAP STRIP STA 727-847 LBL 22 WL 156 / RECEIVED NEW AFT CARGO L/H CAP STRIPS STA 727-847 LBL 22 ON P.O# 767125; 755744; 609504; 760807; 766755 FOR AFT CARGO INSTALL WELL BE WORK ON CARD #JPANEL-141-CLOSE

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 56,913 hrs · 28,285 cycles

RT HORIZ. STAB RIB ASSY. 5 (STAB STA 129.50) 3RD VERT STIFFENER IS CRACKED. / REPAIRED RT HORIZONTAL STABILIZER INSPAR RIB ASSY 5 (STAB STA 129.50) 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R REPAIR 4. SRM 51-40-02-0G-0, AMM 27-31-41-400-801, DRAWING #182A1500, 182A3001, 182A4001.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 56,913 hrs · 28,285 cycles

L/H HORIZONTAL STABILIZER 4 RIB ASSEMBLY STAB. STA. 120.30, 4TH VERTICAL STIFFENER CRACKED. / REPAIRED INSPAR RIB IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 56,913 hrs · 28,285 cycles

FLOORPANEL 241ABF HAS AREA OF DELAM AND DAMAGED INSERTS / REPAIRED AREA OF DELAM AND REPLACED DAMAGED INSERTS IAW SRM 53-00-50-2R-1 ON FLOORPANEL 241ABF.

Part: SHIELD — CORRODED (BS 847) · airframe 56,913 hrs · 28,285 cycles

AFT CARGO BAY AFT SHIELD CORRODED AT BS. 847+12, RBL 20. / R&R SHIELD IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 56,913 hrs · 28,285 cycles

AFT CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT LOWER ANGLE CORRODED AT BS. 947, BETWEEN RBL 19 TO LBL 7. / R&R ANGLE PER SRM & DWG.

Part: SUPPORT — CORRODED (BS 727-847) · airframe 56,913 hrs · 28,285 cycles

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

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 56,913 hrs · 28,285 cycles

TRACK AROUND FASTENER HOLE AT AFT CARGO BAY CORRODED BETWEEN BS. 727 TO BS. 887, RBL 14. / R&R TRACK SECTIONS PER SRM & DWG.

Part: WEBBING — CORRODED (BS 795-847) · airframe 56,913 hrs · 28,285 cycles

AFT CARGO BAY ON SUB THRESHOLD WEB CORRODED BETWEEN BS. 795 TO BS. 847, RBL 25. / R&R WEB PER SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 727-867) · airframe 56,913 hrs · 28,285 cycles

AFT CARGO BAY FLOOR TRACK TIE DOWN CORRODED BETWEEN BS. 727 TO BS. 867, LBL 17. / R&R TIE DOWN TRACK PER SRM & DWG.

Part: TAB — MISSING (R/H ELEVATOR) · airframe 56,913 hrs · 28,285 cycles

RT ELEVATOR TAB UPPER SURFACE HAS MISSING PAINT. / REMOVED; PAINTED; BALANCED; AND REINSTALLED THE RT ELEVATOR TAB IAW MM 27-31-31-000-801; MM 51-21-99-300-801; SRM 51-61-06-0G-0; MM 27-31-31-400-801; MM 27-31-00-700-806; AND MM 27-31-00-700-802. OPS CHECK GOOD

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 56,913 hrs · 28,285 cycles

MOPSILL CHORD THRESHOLD SUPPORT FLANGE CORRODED BETWEEN BS. 900 TO BS. 1006, RBL 50. / R&R CHORD IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,913 hrs · 28,285 cycles

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

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 56,913 hrs · 28,285 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,913 hrs · 28,285 cycles

FLOOR SUPPORT CRACKED BETWEEN BS. 312 TO BS. 328, RBL 31. / R&R FLOOR SUPPORT PER SRM AND DWG.

Part: CAP — CORRODED · airframe 56,913 hrs · 28,285 cycles

CORROSION ON UPPER CHORD BS 986 RBL45 AND LBL45 AT NUTPLATE LOCATION / ON BS986 UPPER CHORD LBL 45 REPAIRED I.A.W SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 1 FIG 205 DUE TO FOUND OUT LIMIT AND BS 986 UPPER CHORD RBL 45 REMOVED CORROSION ON 2' X 1' AREA ORIGINAL MATERIAL THICKNESS IS 0.150' REMAINING MATERIAL THICKNESS IS. 0.145 FOUND TO BE IN LIMITS. I.A.W SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1

Part: TAB — MISSING (L/H ELEVATOR) · airframe 56,913 hrs · 28,285 cycles

LT ELEVATOR TAB UPPER SURFACE HAS MISSING PAINT. / REMOVED; PAINTED; BALANCED AND REINSTALLED LT ELEVATOR TAB IAW MM 27-31-31-000-801; MM 27-31-31-400-801; MM 51-21-99-300-801; SRM 51-61-06-0G-0; MM 27-31-00-700-802; AND MM 27-31-00-700-806. OPS CHECKED GOOD.

Part: THRESHOLD — CRACKED (FWD CARGO BAY) · airframe 56,913 hrs · 28,285 cycles

FWD CARGO BAY FWD CORNER THRESHOLD CRACKED. / RECEIVED; LOCATED AND DRILLED FWD CARGO BAY FWD THRESHOLD AND WILL BE INSTALLED IAW CARD N. 753-140-00-01Y. 59847U; 01NOV19; SRM 51-40-05-0G-0 59847U; 01NOV19.

Part: RIB — CRACKED (LT WING) · airframe 55,733 hrs · 27,487 cycles

L/H WING INBOARD FIXED TRAILING EDGE UPPER SEAL RIB CRACKED. R&R RIB PER SRM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 55,733 hrs · 27,487 cycles

L/H WING INBOARD FIXED TRAILING EDGE LOWER SEAL RIB SUPPORT BRACKET CRACKED. / R&R BRACKET PER SRM.

Part: SENSOR — FAULTY (LE SLAT) · airframe 55,534 hrs · 27,363 cycles

DECLARED EMERGENCY, FLAPS SELECTED TO 1 NO FLAP MOVEMENT. R&R NR 2 FLAP SKEW SENSOR PER MM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 53,967 hrs · 26,360 cycles

R1 DOOR SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 52,735 hrs · 25,582 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. REINSTALLED SLIDE PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 52,266 hrs · 25,287 cycles

R1 DOOR EGRESS SLIDE INADVERTENTLY PULLED OUT PARTWAY, DID NOT DEPLOY, STILL OPERATIONAL. R&R SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,694 hrs · 24,924 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: COVER — CRACKED (CABIN) · airframe 50,121 hrs · 23,955 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER CRACKED. R&R COVER PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 50,121 hrs · 23,955 cycles

RT WING OUTBOARD AFT FLAP INBOARD TRAILING EDGE DELAMINATED. R&R AFT FLAP PER AMM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,121 hrs · 23,955 cycles

L/H STABILIZER RIB; THIRD FROM FRONT VERTICAL FLANGE; CRACKED AT LOWER RADIUS AT STAB. STA. 129.50 (I/B SURFACE) / REPAIRED PER SRM 55-10-09-2R-4 AND EA 1-755-3864. SEE NON-ROUTINE G492414 FOR INSTALLATION OF 4 FASTENERS COMMON TO LOWER SKIN.

Part: FAIRING — CRACKED (LT WING) · airframe 50,121 hrs · 23,955 cycles

# 1 ENGINE PYLON STRUT FAIRING FOUND TO BE CRACKED ON TRAILING EDGE WEDGE. / REPAIRED # 1 ENGINE PYLON STRUT FAIRING TRAILING EDGE WEDGE PER EA 1-754-2224.

Part: WEB — CRACKED (FWD CARGO BAY) · airframe 50,121 hrs · 23,955 cycles

FWD CARGO DOOR THRESHOLD WEB CRACKED AT STA 488 RBL 33. / REMOVED AND REPLACED DAMAGED THRESHOLD WEB; AS PER SRM 51-40-02 . REMOVED AND REINSTALLED SCUFF PLATE AS PER AMM 25-52-10 AND SRM 51-40-02.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,121 hrs · 23,955 cycles

L/H STABILIZER RIB; SECOND FROM FRONT VERTICAL FLANGE; CRACKED AT LOWER RADIUS AT STAB. STA. 129.50 (I/B SURFACE) / REPAIRED CRACKED RIB PER SRM 55-10-09-2R-4. SEE NON-ROUTINE G492414 FOR INSTALLATION OF 4 FASTENERS COMMON TO LOWER SKIN.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 50,121 hrs · 23,955 cycles

AFT CARGO LEFT HAND TRANSITION ANGLE HAS CORROSION AT STA 767 + 6. / REMOVED DAMAGED L/H TRANSITION ANGLE AND INSTALLED NEW L/H TRANSITION ANGLE STA 727-847 PER SRM 53-00-53-2R-5; SRM 51-40-02; AND SRM 53-60-53-01-2. SEE INDIVIDUAL SIGNOFFS FOR WORK ACCOMPLISHED.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 50,121 hrs · 23,955 cycles

AFT CARGO AFT CORNER THRESHOLD PLATE IS CRACKED. / REPAIRED ON REPAIR ORDER 7530062-65R. PLATE TO BE INSTALLED ON ROUTINE TASK CARD 753-721-10-01.

Part: BEAM — BROKEN (LEFT WING) · airframe 50,121 hrs · 23,955 cycles

LEFT WING LWR FIXED PANEL BEAM BROKE JUST AFT OF LWER SUPPORT BRACKET AT 281ORSS / REPLACED SUPPORT BEAM PER SRM 51-40-02.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 50,121 hrs · 23,955 cycles

AFT CARGO LEFT HAND TRANSITION ANGLE HAS CORROSION AT STA 727D. / REMOVED DAMAGED L/H TRANSITION ANGLE AND INSTALLED NEW L/H TRANSITION ANGLE STA 727-847 PER SRM 53-00-53-2R-5; SRM 51-40-02; AND SRM 53-60-53-01-2. SEE INDIVIDUAL SIGNOFFS FOR WORK ACCOMPLISHED.

Part: BRACKET — ELONGATED (LEFT WING) · airframe 50,121 hrs · 23,955 cycles

LOWER SHELF PANEL SUPPORT BRACKET ELONGATED HOLE LEFT WING AT ORSS 281. / REMOVED AND RELPLACED SUPPORT BRACKET PER SRM 51-40-02.

Part: PLATE — CRACKED (LEFT WING) · airframe 50,121 hrs · 23,955 cycles

WAFFLE PLATE CRACKED LEFT WING ABOVE AFT STRUT FAIRING AT ORSS 261 / REMOVED AND REPLACED WUFFLE PLATE AT ORSS 261 PER SRM 51-40-02

Part: PLATE — CRACKED (RIGHT WING) · airframe 50,121 hrs · 23,955 cycles

RIGHT WING REAR SPAR STA 271 WAFFLE PLATE CRACKED AT RIVET OUTBD OF NACELLE STRUT FAIRING / REMOVED AND REPLACED WIGGLE PLATE IAW SRM 51-40-02.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 50,121 hrs · 23,955 cycles

FORWARD CARGO THRESHOLD IS CRACKED AT STOP PIN DIVOT. / INSTALLED THRESHOLD PER A/M/M/ 53-11-02

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,160 hrs · 22,754 cycles

LT AFT LOWER EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 46,352 hrs · 21,654 cycles

RIGHT EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. R & R BALLAST ASSEMBLY IAW MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 45,195 hrs · 20,975 cycles

R1 EMER EXIT LIGHTED SIGN COVER LOOSE. R & R SIGN IAW AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 44,532 hrs · 20,591 cycles

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

Part: FITTING — LOOSE (L2 DOOR) · airframe 43,450 hrs · 19,952 cycles

L2 DOOR EMER EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING IAW AMM.

Part: FITTING — LOOSE (R2 DOOR) · airframe 43,450 hrs · 19,952 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING IAW AMM.

Part: WIRE — DAMAGED (CABIN) · airframe 43,450 hrs · 19,952 cycles

EMERGENCY AISLE LIGHT L1065 INOPERATIVE AT BS 520, RBL 30. INSTALLED WIRE IAW MM.

Part: FITTING — LOOSE (L1 DOOR) · airframe 43,450 hrs · 19,952 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR FITTINGS LOOSE. REPAIRED FITTING IAW AMM.

Part: FITTING — LOOSE (R1 DOOR) · airframe 43,450 hrs · 19,952 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING IAW AMM.

Part: FITTING — LOOSE (L1 DOOR) · airframe 43,450 hrs · 19,952 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING IAW AMM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 43,450 hrs · 19,952 cycles

L2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 43,450 hrs · 19,952 cycles

LEFT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STATION 92.7, NR 2 & 3 VERTICAL STIFFENERS. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 43,450 hrs · 19,952 cycles

LEFT HORIZONTAL STABILIZER INSPAR RIB FLANGE, CRACKED AT STAB STATION 101.9, LOWER HORIZONTAL SURFACE. REPAIRED RIB IAW ER & EA.

Part: POST — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME E - F POST, 2ND HOLE FROM LOWER CORNER FOUND CRACKED. REPAIRED POST IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

LEFT NR 3 FLIGHT DECK WINDOW FRAME E-F POST, 2ND HOLE FROM LOWER CORNER FOUND CRACKED. REPAIRED FRAME IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

AFT SEAT TRACK OTBD FLANGE CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA & ER.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

BS 727B, LBL 45.5 AFT SEAT TRACK, CRACKED AT BS 727B, LBL 45.5. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

FORWARD SEAT TRACK, OTBD FLANGE CRACKED AT BS 727B, RBL 24.75, AFT FASTENER HOLE. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

FORWARD SEAT TRACK, OTBD FLANGE CRACKED AT BS 727B, LBL 45.5, FWD & AFT FASTENER HOLES. REPAIRED FLANGE IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, RBL 45.5, INBD FLANGE AT AFT FASTENER HOLE. REPAIRED FLANGE IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 727 - 727A, LBL 63. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 727 - 727A, RBL 63. REPAIRED WEB IAW EA & ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

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

Part: FITTING — CHAFED (R2 DOOR) · airframe 43,450 hrs · 19,952 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR STOWAGE CLIPS CHAFED. R & R CLIPS IAW SRM.

Part: FITTING — CHAFED (L2 DOOR) · airframe 43,450 hrs · 19,952 cycles

L2 DOOR EMER EVAC SLIDE GIRT BAR STOWAGE CLIPS CHAFED. R & R CLIPS IAW SRM.

Part: FITTING — CHAFED (R1 DOOR) · airframe 43,450 hrs · 19,952 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR STOWAGE CLIPS CHAFED. R & R CLIPS IAW SRM.

Part: FITTING — CHAFED (L1 DOOR) · airframe 43,450 hrs · 19,952 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR STOWAGE CLIPS CHAFED. R & R CLIPS IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,450 hrs · 19,952 cycles

RIGHT WING LOWER SURFACE OF LE, NR 6 SLAT NOSE SKIN AT ACTUATOR RIB CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,450 hrs · 19,952 cycles

RIGHT WING LOWER SURFACE OF LE NR 7 SLAT NOSE SKIN AT ACTUATOR RIB, CRACKED. REPAIRED SKIN IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727C+1 - 767, RBL 21. R & R SUPPORT IAW SRM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 43,450 hrs · 19,952 cycles

EMERGENCY EXIT LIGHT WIRE CONNECTOR BROKEN AT BS 757, BETWEEN STRINGER 21L - 22L. R & R CONNECTOR IAW SOPM & WDM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

INTERCOSTAL ATTACH CLIP, CRACKED AT BS 500C, LBL 24. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

INTERCOSTAL ATTACH CLIP, CRACKED AT BS 500A, LBL 24. R & R INTERCOSTAL IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727 - 727E+13, LBL 21. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

FLOOR TO SIDE WALL SUPPORT CORRODED, BETWEEN BS 500A+12 - 500C+13, LBL 23. R & R SUPPORT IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

RIGHT KEEL BEAM VERTICAL ATTACH ANGLE, CRACKED AT BS 727+8, RBL 6 ON INBD SIDE. R & R ANGLE IAW SRM & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,450 hrs · 19,952 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT BS 500B, LBL 24. R & R INTERCOSTAL IAW SRM.