N8604K

Part: BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 38,645 hrs · 17,832 cycles

CRACK ON BRACKET LOCATED TRAILING EDGE INBOARD SIDE AT LH WING 2023-650227<[01] REPLACED BRACKET LOCATED ON TRAILING EDGE INBOARD SIDE AT LH WING IAW B737-800 SRM 51-40-02 AND DWG 115A2510 SHEET 2 REV A. SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK ON SUPPORT BRACKET ASSY LOCATED BETWEEN BS540 TO BS559 RT SIDE AT AIR CONDITION BAY 2023-650179<[01] REPLACED SUPPORT BRACKET ASSY LOCATED BETWEEN BS540 TO BS559 RT SIDE AT AIR CONDITION BAY; IAW B737-800 SRM 51-40-02; SRM 51-10-02 MEASURE OF CRACK IS: L=1.130? TOOL USED: CALIPER P/N: 700-113-10;S/N: 0033152; DUE DATE: 10-SEP-24;[02] JOB COMPLETED

Part: FLOOR PANEL — ELONGATED (ZN 200 FUS TOP) · airframe 38,645 hrs · 17,832 cycles

ELONGATED HOLE FLOOR PANEL 211AF AT COCKPIT 2023-650172<[01] REPLACED FLOOR PANEL 211AF AT COCKPIT IAW B737-800 SRM 51-10-02 PARAGRAPH 9 AND DWG NO. 141A5133; SHEET 2; REV. C. MATERIAL USED 2024-T3/0.040? PO:2023-180996.<BR>SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED FLOOR PANEL 211AF AT COCKPIT IAW B737-800 SRM 51-10-02 PARAGRAPH 9 AND DWG NO. 141A5133; SHEET 2; REV. C. MATERIAL USED 2024-T3/0.040? PO:2023-180996.<BR>SEE INDIVIDUAL SIGNOFFS BELOW.<BR>RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK ANGLE LOCATED BS727B AT LEVEL STR18L UPPER SIDE AT AFT CARGO COMPARTMENT 2023-650156 (CRACK ANGLE LOCATED BS727B AT LBL 50.08 UPPER SIDE AT AFT CARGO COMPARTMENT )<[01] REPLACED ANGLE LOCATED ON BS 727A TO BS 727D MORE 16 INCH AT LEVEL STR18L UPPER SIDE AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 DWG 149A9490 SHEET 24 REV-.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORECTED STEP REPLACED ANGLE LOCATED ON BS 727A TO BS 727D MORE 16 INCH AT LBL 50.08 UPPER SIDE AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 DWG 149A9490 SHEET 24 REV-.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] JOB COMPLETED.

Part: LIGHT — DETERIORATED (ZN 200 FUS TOP) · airframe 38,645 hrs · 17,832 cycles

DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG AT PASSENGER CABIN (5 EA) 2023-650137<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG AT PASSENGER CABIN (5 EA IAW B737-700 AMM-35-51-15-400-802 AND DWG-33510501 REV.IR;[02] TASK CARD COMPLETED

Part: SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK SUPPORT ZEE LOCATED BETWEEN BS727J TO BS747 AND RBL21.80 AFT CARGO COMPARTMENT 2023-650112<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS727J TO BS747 AND RBL21.80 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 146A7500 SHEET 213 REV -<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED SUPPORT ZEE LOCATED BETWEEN BS727J TO BS747 AND RBL21.80 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 146A7500 SHEET 213 REV -<BR>SEE INDIVIDUAL SIGNOFF BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK ANGLE LOCATED BS867 AT LEVEL LBL12.5 AND WL156 AFT CARGO COMPARTMENT 2023-650120<[01] REPLACED ANGLE LOCATED BS867 AT LEVEL LBL12.5 AND WL156 AFT CARGO COMPARTMENT IAW B737-800 SR; 51-10-02 AND DRAWING 149A8102 SHEET 19 REV A;[02] CORRECTED STEP 1<BR>REPLACED ANGLE LOCATED BS867 AT LEVEL LBL12.5 AND WL156 AFT CARGO COMPARTMENT IAW B737-800 SRM; 51-10-02 ITEM 9; SRM 51-40-02; AND DRAWING 149A8102 SHEET 19 REV A;[03] REPLACED ANGLE LOCATED BS867 AT LEVEL LBL12.5 AND WL156 AFT CARGO COMPARTMENT IAW B737-800 SRM; 51-10-02 ITEM 9; SRM 51-40-02; AND DRAWING 149A8102 SHEET 19 REV A

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK WEB - INTERCOSTAL LOCATED BS947 AND RBL21.5 AT AFT CARGO COMPARTMENT 2023-650121<[01] REPLACED WEB-INTERCOSTAL LOCATED BS 927 TO BS947 AND RBL21.5 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 147A7500 REV -.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED WEB-INTERCOSTAL LOCATED BS 927 TO BS947 AND RBL21.5 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 147A7500 REV -JOB COMPLETED.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS747 TO BS807 LBL21.8 AND WL156 AFT CARGO COMPARTMENT 2023-650119<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] REMOVED AND EVALUATED CORROSION SUPPORT ZEE LOCATED BETWEEN BS747 TO BS807 LBL21.8 AND WL156 AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS I.A.W B737-800 SRM 53-00-53-1A-2 PARAGRAPH 4.A (2) FIGURE 103 DETAIL E AND SRM 51-10-02. SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 38,645 hrs · 17,832 cycles

CRACK CORRUGATED PLATE TRAILING EDGE ORSS 295 AT RT WING 2023-650113<[01] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED AT TRAILING EDGE AREA ON ORSS 295 AT RT WING IAW B737-800 SRM 51-40-02 AND DWG# 115A3700-36; SHEET: 32; REV: -<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1. INSTALLED NEW CORRUGATED PLATE AND FASTENERS LOCATED AT TRAILING EDGE AREA ON ORSS 295 AT RT WING IAW B737-800 SRM 51-40-02 AND DWG# 115A3700; SHEET: 32; REV: -;[03] CORRECTED STEP 2. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED AT TRAILING EDGE AREA ON ORSS 295 AT RT WING IAW B737-800 SRM 51-40-02 AND DWG# 115A3700; SHEET: 32; REV: -.<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[04] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED AT TRAILING EDGE AREA ON ORSS 295 AT RT WING IAW B737-800 SRM 51-40-02 AND DWG# 115A3700; SHEET: 32; REV: -.<BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 38,645 hrs · 17,832 cycles

CORROSION FLOOR BEAM LOCATED BS986.5 AT RBL43 AND WL208.1 AT AFT GALLEY AREA 2023-650085<[01] TOOL USED EDDY CURRENT EQUIPMENT PN:NORTEC 600D; SN: 60007161486; DUE DATE: 20-JUL-24;[02] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138503 AND DUE DATE: 21-JUL-24.;[03] PERFORMED PERMANENT REPAIR LOC ON FLOOR BEAM BS986.5 AT RBL43 AND WL208.1 AT AFT GALLEY AREA I.A.W SRM 53-70-51-2R-6 REPAIR 6.SEE INDIVIDUAL SIGN OFFS BELOW.;[04] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 38,645 hrs · 17,832 cycles

CORROSION FLOOR BEAM LOCATED BS947.5 BETWEEN RBL49 TO RBL53 AND WL208.1 AT AFT GALLEY AREA 2023-650083<[01] PERFORMED PERMANENT REPAIR FLOOR BEAM UPPER CHORD BS947.5 AND BETWEEN RBL 2 TO RBL 60 AFT GALLEY AREA. (-1)T CHORD 1E/A MATERIAL USED: AND10136-3006; PO: 2023 125392. (-2) ANGLE 2 E/A MATERIAL USED:BAC1490-2885; PO:2022 163880. (-3)STRAPS 2E/A MATERIAL USED: 7075-T6 0.125; PO: 2022 147476.(-4) FILLER 3E/AMATERIAL USED: 7075-T6 0.100; PO:2012 531818. (-5)CLIP 2 E/A MATERIAL USED: BAC1503-101021; PO: 2023 121945. (-6) CLIP 2 E/A MATERIAL USED: BAC1503-101025; PO: 2023 121944 IAW SRM B737-800 53-70-51-2R-5 REPAIR 5 ALTERNATIVE 2 FIGURE 206 DETAIL B EA# 23-153-03331 [TTG8Q00PUH4D]; EA# 23-153-03331-WIP1 [TTG8Q00PM3XB] AND EA# 23-153-03331-WIP2 [TTG8Q00PPRRS] SEE INDIVIDUAL SIGN OFF BELOW.;[02] PERFORMED PERMANENT REPAIR FLOOR BEAM UPPER CHORD BS947.5 AND BETWEEN RBL 2 TO RBL 60 AFT GALLEY AREA. (-1)T CHORD 1E/A MATERIAL USED: AND10136-3006; PO: 2023 125392. (-2) ANGLE 2 E/A MATERIAL USED:BAC1490-2885; PO:2022 163880. (-3)STRAPS 2E/A MATERIAL USED: 7075-T6 0.125; PO: 2022 147476.(-4) FILLER 3E/AMATERIAL USED: 7075-T6 0.100; PO:2012 531818. (-5)CLIP 2 E/A MATERIAL USED: BAC1503-101021; PO: 2023 121945. (-6) CLIP 2 E/A MATERIAL USED: BAC1503-101025; PO: 2023 121944 IAW SRM B737-800 53-70-51-2R-5 REPAIR 5 ALTERNATIVE 2 FIGURE 206 DETAIL B EA# 23-153-03331

Part: FRAME — CRACKED (ZN 200 FUS TOP) · airframe 38,645 hrs · 17,832 cycles

CRACK FRAME ON BS 312 AT STR6L AT FWD GALLEY AREA 2023-650096<[01] REMOVED CRACK LOCATED ON FRAME BS312 AT STR6L AT FWD GALLEY AREA IAW EA M-22-153-01244;[02] CERTIFIED STEP 1 COMPLETED

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK ON SUPPORT BRACKET ASSY LOCATED BTW BS540 TO BS 559 LT SIDE AT AIR CONDITIONING BAY 2023-650084<[01] REPLACED SUPPORT BRACKET ASSY LOCATED BTW BS540 TO BS 559 LT SIDE AT AIR CONDITIONING BAY IAW B737-800 SRM 51-40-02-0G-0;[02] REPLACED SUPPORT BRACKET ASSY LOCATED BTW BS540 TO BS 559 LT SIDE AT AIR CONDITIONING BAY IAW B737-800 SRM 51-40-02-0G-0

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 38,645 hrs · 17,832 cycles

CRACK ON CORRUGATED PLATE LOCATED IRSS 214 TRAILING EDGE AT LT WING 2023-650095<[01] REPLACED CORRÏ¿½GATED PLATE AND FASTENERS LOCATED IRSS 214 TRAILING EDGE AT LT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A2713 SHEET: 6 REV: A.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED CORRÏ¿½GATED PLATE AND FASTENERS LOCATED IRSS 214 TRAILING EDGE AT LT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A2713 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CORRODED (ZN 200 FUS TOP) · airframe 38,645 hrs · 17,832 cycles

CORROSION INNER CHORD LOCATED BS927 TO BS992.8 AT RBL51 AND WL208.1 AFT GALLEY AND LAV 2023-650087<[01] TOOL USED; ULTRASONIC THICKNESS GAGE. PN:45MG; SN: 130060401; DUE DATE: 20-MAR-24;[02] REPLACED INNER CHORD AND FASTENERS LOCATED BS907 TO BS992.8 AT RBL51 AND WL208.1 AFT GALLEY AND LAV I.A.W. B737-800 SRM 51-40-02 AND SRM B737-800 SRM 51-10-02 ITEM 9 AND DRAWING #147A8540; SHEET 5; REV B. AND #147A850; SHEET 93; REV A.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED INNER CHORD AND FASTENERS LOCATED BS907 TO BS992.8 AT RBL51 AND WL208.1 AFT GALLEY AND LAV I.A.W. B737-800 SRM 51-40-02 AND SRM B737-800 SRM 51-10-02 ITEM 9 AND DRAWING #147A8540; SHEET 5; REV B. AND #147A850; SHEET 93; REV A.<BR>SEE INDIVIDUAL SIGN OFF BELOW<BR><BR>ITEM RII

Part: ACCESS PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK ACCESS PANEL 191CR BODY FAIRING AT LOWER FUSELAGE 2023-650078<[01] TOOL USED: HOT BONDER P/N HCS9200B-AV; S/N: 18196127; DUE DATE: 22-JAN-24;[02] TOOL USED: SCALE: P/N: SPX621 S/N 8340225451 DUE DATE: 16/AUG/24.;[03] TOOL USED: HOT BONDER : P/N:HCS9200B-AV S/N: 18185781 DUE DATE: 24/JAN/24.;[04] TOOL USED: ULTRASONIC EQUIPMENT PN: EPOCH 6LT; SN: 230529908; DUE DATE: 22-AUG-24;[05] TOOL USED: SCALE: P/N: SPX621 S/N 8340225451 DUE DATE: 16/AUG/24.;[06] TOOL USED: HOT BONDER PN: HCS9200B-AV; SN: 18185733; DUE DATE: 23-JAN-24.;[07] REPAIRED ACCESS PANEL 621PB LEADING EDGE AT RT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.SEE INDIVIDUAL SIGNOFF BELOWS.;[08] CORRECTED STEP 7 REPAIRED ACCESS PANEL 191CR LEADING EDGE AT RT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.SEE INDIVIDUAL SIGNOFF BELOWS.;[09] CORRECTED STEP 8 REPAIRED ACCESS PANEL 191CR BODY FAIRING AT LOWER FUSELAGE B737-800 SRM 51-70-04-2R-10 REPAIR 10.SEE INDIVIDUAL SIGNOFF BELOWS.;[10] REPAIRED ACCESS PANEL 191CR BODY FAIRING AT LOWER FUSELAGE B737-800 SRM 51-70-04-2R-10 REPAIR 10.SEE INDIVIDUAL SIGNOFF BELOWS.

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 38,645 hrs · 17,832 cycles

CRACK FLOOR STRUCTURE ANGLE LOCATED BETWEEN BS291.5 TO BS294.5 AND STR17R AT FWD GALLEY AREA 2023-650049<[01] REPLACED ANGLE LOCATED BETWEEN BS291.5 TO BS294.5 AND STR17R AT FWD GALLEY AREA IAW B737-800 SRM 51-10-02 Ï¿½TEM 9; AND DRAWING 141A8310; SHEET 33; REV -;[02] REPLACED ANGLE LOCATED BETWEEN BS291.5 TO BS294.5 AND STR17R AT FWD GALLEY AREA IAW B737-800 SRM 51-10-02 Ï¿½TEM 9; AND DRAWING 141A8310; SHEET 33; REV -

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 38,645 hrs · 17,832 cycles

CRACK ON RIB LOCATED LE STA 105.26 OF PANEL 331B AT LT HORIZONTAL STABILIZER 2023-650054<[01] REPLACED RIB LOCATED LE STA 105.26 OF PANEL 331B AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02 AND DWG 186A1001 SEE INDIVIDUAL SIGN OFF BELOW.;[02] STEP 1 CORRECTED <BR>REPLACED RIB LOCATED LE STA 105.26 OF PANEL 331B AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02 AND DWG 186A1001 SHEET 19 REV - SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED RIB LOCATED LE STA 105.26 OF PANEL 331B AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02 AND DWG 186A1001 SHEET 19 REV - SEE INDIVIDUAL SIGN OFF BELOW. RII.

Part: WEB — CRACKED (ZN 200 FUS TOP) · airframe 38,645 hrs · 17,832 cycles

CRACK WEB LOCATED BETWEEN BS344 TO BS360 AND BL0 FWD GALLEY AND LAV 2023-650047<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS344 TO BS360 AND BL0 FWD GALLEY AND LAV IAW B737-800 SRM 51-10-02 AND SRM 51-40-02 AND DWG 141A5400;SHEET 32; REV.- .SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 38,645 hrs · 17,832 cycles

CRACK ON RIB LOCATED LE STA 244.72 OF PANEL 331B AT LT HORIZONTAL STABILIZER 2023-650053<[01] REPLACED RIB LOCATED LE STA 244.72 OF PANEL 331B AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02 AND DWG 186A1001 SHEET 19 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[02] STEP 1 CORRECTED <BR>REPLACED RIB LOCATED LE STA 244.72 OF PANEL 331B AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02 SRM 51-10-02 AND DWG 186A1001 SHEET 19 REV - SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED RIB LOCATED LE STA 244.72 OF PANEL 331B AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02 SRM 51-10-02 AND DWG 186A1001 SHEET 19 REV - <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: WEB — CRACKED (ZN 200 FUS TOP) · airframe 38,645 hrs · 17,832 cycles

CRACK WEB LOCATED BETWEEN BS344 TO BS360 AND LBL11 FWD GALLEY AND LAV 2023-650048<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS 344 TO BS 360 AND LBL 11 FWD GALLEY AND LAV IAW B737-800 SRM 51-10-02 AND SRM 51-40-02 AND DWG 141A5400 SHEET 46 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS 344 TO BS 360 AND LBL 11 FWD GALLEY AND LAV IAW B737-800 SRM 51-10-02 AND SRM 51-40-02 AND DWG 141A5400 SHEET 46 REV A. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK GUSSET LOCATED BS500I AND STR19R AT FWD CARGO COMPARTMENT 2023-650013<[01] REPLACED GUSSET AND FASTENERS LOCATED BS500I AND STR19R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 SRM 51-10-02 Ï¿½TEM 9; AND DRAWING # 143A7902 REV : B<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED GUSSET AND FASTENERS LOCATED BS500I AND STR19R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 SRM 51-10-02 Ï¿½TEM 9; AND DRAWING # 143A7902 REV : B<BR>SEE INDIVIDUAL SIGN OFF BELOW<BR>CERTIFIED RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK ANGLE - CLIP LOCATED BS500G AND STR26L FWD FACE AT FWD CARGO COMPARTMENT 2023-650019<[01] REPLACED ANGLE - CLIP LOCATED BS500G AND STR26L FWD FACE AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7505; SHEET 108; REV - <BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1. REPLACED ANGLE - CLIP LOCATED BS500G AND STR26L FWD FACE AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7505; SHEET 108; REV - <BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: HANDLE — DETERIORATED (ZN 800 DOOR) · airframe 38,645 hrs · 17,832 cycles

DETERIORATED LINING ENTRY DOOR ASSIST HANDLES NUT (4 EA) AND COLLAR AT FWD GALLEY AREA (4 EA) 2023-649991<[01] REPLACED LINING ENTRY DOOR ASSIST HANDLES NUT (4 EA) AND COLLARS AT FWD GALLEY AREA (4 EA) IAW B737-800 AMM 52-11-31-400-802 STEP 3G(2);[02] TASK CARD COMPLETED

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK ANGLE - CLIP LOCATED BS500D AND STR26L FWD FACE AT FWD CARGO COMPARTMENT 2023-650020<[01] REPLACED ANGLE - CLIP LOCATED BS500D AND STR26L FWD FACE AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A750; SHEET 108; REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1. REPLACED ANGLE - CLIP LOCATED BS500D AND STR26L FWD FACE AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02; SRM 51-40-02 AND DWG 143A750; SHEET 108; REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK GUSSET LOCATED BS500I AND STR21L AT FWD CARGO COMPARTMENT 2023-650016<[01] REPLACED GUSSET AND FASTENERS LOCATED BS500I AND STR21L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET: 257 REV: B.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED GUSSET AND FASTENERS LOCATED BS500I AND STR21L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET: 257 REV: B.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.<BR>CERTIFIED RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK ANGLE - CLIP LOCATED BS500H AND STR26L FWD FACE AT FWD CARGO COMPARTMENT 2023-650018<[01] REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500H AND STR26L FWD FACE AT FWD CARGO COMPARTMENT.IAW B737-800 SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 ITEM 9 AND DWG 143A7505 SHEET 109 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500H AND STR26L FWD FACE AT FWD CARGO COMPARTMENT.IAW B737-800 SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 ITEM 9 AND DWG 143A7505 SHEET 109 REV-. SEE INDIVIDUAL SIGN OFF BELOW.ITEM RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK ANGLE - CLIP LOCATED BS500H AND AT LEVEL STR26L AFT FACE AT FWD CARGO COMPARTMENT 2023-650017<[01] REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500H AND AT LEVEL STR26L AFT FACE AT FWD CARGO COMPARTMENT.IAW B737-800 SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 AND DWG 143A7505 SHEET 109 REV-. SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1. REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500H AND AT LEVEL STR26L AFT FACE AT FWD CARGO COMPARTMENT.IAW B737-800 SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 ITEM 9 AND DWG 143A7505 SHEET 109 REV-. SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500H AND AT LEVEL STR26L AFT FACE AT FWD CARGO COMPARTMENT.IAW B737-800 SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 ITEM 9 AND DWG 143A7505 SHEET 109 REV-. SEE INDIVIDUAL SIGN OFF BELOW. ITEM RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK ANGLE - CLIP LOCATED BS500H AND AT LEVEL STR26R AT FWD CARGO COMPARTMENT 2023-650014<[01] REPLACED ANGLE-CLIP; LOCATED ON BS500H AT LEVEL STR26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET 20 REV B. SEE INDIVIDUAL SIGNS OFF BELOW;[02] REPLACED ANGLE-CLIP; LOCATED ON BS500H AT LEVEL STR26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET 20 REV B. SEE INDIVIDUAL SIGNS OFF BELOW

Part: ACCESS PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

DELAMINATED ACCESS PANEL 191D AT LOWER FUSELAGE 2023-649973<[01] TOOL USED CALIPER P/N: 500-196-30; S/N B22072476; DUE DATE: 14-JUL-24.;[02] TOOL USED: THERMOGRAPHY CAMERA P/N: FLIR-T530; S/N: 79316001; DUE DATE: 23-JAN-24.;[03] TOOL USED: HOTBONDER PN: HCS9200B-AV; SN: 18196127; DUE DATE: 22-JAN-24.;[04] TOOL USED SCALE P/N CR5200; S/N 8343110867; DUE DATE: 21-FEB-24.;[05] REPAIRED ACCESS PANEL 191D INNER SKIN LOWER FUSELAGE IAW B737-800 SRM 53-30-70-2R-1 REPAIR 1 AND B737-800 SRM 51-70-04-2R-2 REPAIR 2 SEE INDIVIDUAL SIGN OFFS BELOW.;[06] REPAIRED ACCESS PANEL 191D INNER SKIN LOWER FUSELAGE IAW B737-800 SRM 53-30-70-2R-1 REPAIR 1 AND B737-800 SRM 51-70-04-2R-2 REPAIR 2 SEE INDIVIDUAL SIGN OFFS BELOW.

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK BRACKET ASSY LOCATED BS540 AND BETWEEN BL0 TO RBL24.75 AT CENTER WING BOX 2023-649920<[01] REPLACED BRACKET ASSY AND FASTENERS LOCATED BS540 AND BETWEEN BL0 TO RBL24.75 AT CENTER WING BOX I.A.W. B737-800 SRM 51-40-02 ;SRM 51-10-02 ITEM 9 AND DRAWING #143A0060; SHEET 36 REV A.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK BRACKET ASSY LOCATED BS540 AND BETWEEN RBL45.5 TO RBL64 AT CENTER WING BOX 2023-649922<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE: 15-FEB-24 WAS USED.;[02] REMOVED AND RE-INSTALLED BRACKET ASSY LOCATED BS540 AND BETWEEN RBL45.5 TO RBL64 AT CENTER WING BOX IAW B737-800 SRM 51-40-02-0G-0; DWG 143A5240 SHEET 23 REV -.<BR>SEE INDIVIDUAL SIGN-OFFS BELOW;[03] REMOVED AND RE-INSTALLED BRACKET ASSY LOCATED BS540 AND BETWEEN RBL45.5 TO RBL64 AT CENTER WING BOX IAW B737-800 SRM 51-40-02-0G-0; DWG 143A5240 SHEET 23 REV -.<BR>SEE INDIVIDUAL SIGN-OFFS BELOW

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-649926<[01] TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N B20189527 DUE DATE 26-DEC-23;[02] TOOL USED: RADIOMETER PHOTOMETER HIGH TECH P/N:XRP 3000; S/N:1859843; DUE DATE:05-DEC-23.;[03] REPAIRED THE CENTER SCUFF PLATE OF AFT CARGO COMPARTMENT IAW BOEING 737-800 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.C. STEPS ( 2 ) AND STEPS ( 4 ) TO ( 7 ) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] TASK COMPLETED.

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 38,645 hrs · 17,832 cycles

CRACK BRACKET ASSY LOCATED BS540 BETWEEN BL0 AND LBL24.75 AT CENTER WING BOX 2023-649921<[01] REPLACED BRACKET ASSY AND FASTENERS LOCATED BS540 AND BETWEEN BL0 TO LBL24.75 AT CENTER WING BOX I.A.W. B737-800 SRM 51-40-02 ;SRM 51-10-02 ITEM 9 AND DRAWING #143A0060; SHEET 36 REV A.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: FLAP — DEBONDED (ZN 500 LEFT WING) · airframe 38,642 hrs · 17,831 cycles

DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT OB SIDE LT WING 2023-649849<[01] TOOL USED: HOTBONDER P/N: HCS9200B S/N: 18165044 DUE DATE: 26-MAR-24; CALIPER P/N: 500-197-30 S/N: A18135081 DUE DATE: 21-JUL-24.;[02] TOOL USED: HOT BONDER PN:HCS9000B ; SN:15092096; DUE DATE: 25-APR-24.;[03] TOOL USED: AUDIBLE BOND TESTER. PN: S-3; SN:064. DUE DATE: 11-AUG-24 AND ULTRASONIC EQUIPMENT PN: EPOCH 650; SN: 190984811; DUE DATE: 24-JAN-24;[04] REPAIRED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT OB SIDE LT WING IAW B737-800 SRM 57-53-01-2R-18 REPAIR 18. SEE INDIVIDUAL SIGNOFFS BELOW;[05] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 38,645 hrs · 17,832 cycles

CRACK TRAILING EDGE ON ANGLE LOCATED ORSS269 AT RT WING 2023-649833<[01] REMOVED AND REPLACED TRAILING EDGE ON ANGLE LOCATED ORSS269 AT RT WING I.A.W. B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9. THE MEASURE OF CRACK IS= (1.125?) TOOL USED DIGITAL P/N:700-113-10 S/N: 0033152 DUE DATE: 10-SEP-24.;[02] REMOVED AND REPLACED TRAILING EDGE ON ANGLE LOCATED ORSS269 AT RT WING I.A.W. B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9. THE MEASURE OF CRACK IS= (1.125?) TOOL USED DIGITAL P/N:700-113-10 S/N: 0033152 DUE DATE: 10-SEP-24.

Part: WEB — CRACKED (ZN 600 RIGHT WIN) · airframe 38,645 hrs · 17,832 cycles

CRACK TRAILING EDGE ON WEB LOCATED ORSS269 AT RT WING 2023-649832<[01] REPLACED WEB AND FASTENERS LOCATED ON TRAILING EDGE ORSS269 AT RT WING IAW B737-800 SRM 51-10-02-0G-0; SRM 51-40-02-0G-0; DWG 115A2512 SHEET 16 REV -.;[02] CORRECTED STEP 1<BR>REPLACED WEB LOCATED ON TRAILING EDGE ORSS269 AT RT WING IAW B737-800 SRM 51-10-02-0G-0; SRM 51-40-02-0G-0; DWG 115A2512 SHEET 16 REV -.<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] COMPLETE TASK CERTIFIED

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 38,071 hrs · 17,501 cycles

LH OVERWING INTERIOR EMERGENCY LIGHTS INOP<[01] R/R BATTERY PACK AND CHARGER ASSEMBLY IAW 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 36,747 hrs · 16,757 cycles

RH OVERWING EXIT EMERGENCY LIGHTS INOP<[01] R&R R/H OVERWING EXIT EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-00.

Part: FSEU — FAULT MESSAGE (ZN 100 FUS LOWER) · airframe 36,018 hrs · 16,336 cycles

T.O. OUT OF MDW - WIND & TURB CAUSED FLAP OVERSPEED DURING FLAP 25 T.O. APPROX 210KTS W/ FLAP 25. WHEN WE RETRACTED FLAP TO 0 THEY WOULD NOT MOVE BELOW 2. WE MOVED FLAP HANDLE TO 5 THEN 10 THEN 0 - FLAPS WOULD NOT MOVE FROM 2. WE UTILIZED ALT FLAP SWITCH PER QRH - SET FLAP HANDLE TO 15 TO MATCH ALT FLAP SETTING AND LANDED FLAP 15.<[01] FOUND FAULT FSEU 27-51351. PERFORMED TRAILING EDGE UNCOMMANDED MOTION PROBLEM TASK TO RESTORE NORMAL FLAP OPERATION REFERENCE FIM 27-51 TASK 830;[02] PERFORMED PHASE I FLAP OVERSPEED INSPECTION REFERENCE MM 05-51-08 AND FOUND NO DISCREPANCIES.;[03] ADDED INFORMATION;[04] ADDED TOOLING<BR>P/N 101-01175<BR>S/N 00319;[05] ADDED TOOLING

Part: RIB — CRACKED (L/H WING) · airframe 34,513 hrs · 15,472 cycles

#3 KRUGER FLAP ON LH WING; OUTBOARD MIDDLE HINGE RIB CRACKED. CRACK IS ON FASTENER ATTACH SURFACE EXTENDING INTO RIB BODY. / [01] DAMAGED RIB TO BE REPLACED IAW SRM 5-10-02-0G-0 DUE NO DATA FOUND ON SRM.;[02] DAMAGED RIB TO BE REPLACED IAW SRM 51-10-02-0G-0 DUE NO DATA FOUND ON SRM.;[03] REPLACED NEW RIB P/N 116A4161-1;LOCATED AND DRILLED AND OK TO INSTALL;[04] REPLACED NEW RIB P/N 116A4161-1;LOCATED AND DRILLED IAW SRM 51-40-05-0G-0; DWG 116A4008 AND OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 4.;[06] INSTALLED NEW RIB EXCEPT AREAS COMMON TO SKIN IAW SRM 51-40-02-0G-0 AND BOEING DWG 116A4008;114A4006;[07] VERIFIED CORRECTIVE ACTION 6.;[08] INSTALLED NEW RIB NO.6 COMMON TO THE SKIN AT KRAS 137.75 IAW SRM 51-40-02 AND BOEING DWG 116A4008.;[09] VERIFIED CORRECTIVE ACTION #8;[10] COMPLETED INSTALL OF NEW #3 K FLAP OUTBOARD MIDDLE HINGE RIB PER BOEING DWG 116A4008;114A4006;[11] VERIFIED CORRECTIVE ACTION #10;[12] TASK COMPLETE;[13] CERTIFIED

Part: LIGHT — BROKEN (R/H CABIN) · airframe 33,961 hrs · 15,157 cycles

EMERGENCY LIGHT LENS COVER MISSING OVER BAG BIN AT ROW 17 DEF. 05/08 MKE HOUSING IS ALSO BROKEN... LENS WILL NOT ATTACH. REQ ASSEMBLY ADDED TO RUN. / [01] OK TO CONTINUE ON MEL 33-15-02.SP 1;[02] RPL EMERGENCY LITE ASSY AT 17 DEF PER AMM 33-51-03

Part: LIGHT — INOPERATIVE · airframe 32,724 hrs · 14,473 cycles

EMERGENCY EXIT LIGHTS HAVE INOP BULBS AT AFT OF AED; AFT OF FWD LH OWE; AND FWD OF FWD LH OWE ; / [01] REPLACED BULBS (LAMPS) EXIT SIGNS AFT OF AED; AFT OF FWD LH OWE; AND FWD OF FWD LH OWE AND PERFORMED A GOOD TEST OF THE LAMPS AS PER AMM 33-51-01-960-801; [02] VERIFIED CORRECTIVE ACTION 1

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 32,612 hrs · 14,410 cycles

FWD CABIN EMER ISLE LTS INOP LEFT + RT SIDE / REMOVED + REPLACED EMER LTS BATTERY PACKS M2335 AND M1676. LIGHTS TEST GOOD PER AMM 33-51-06

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 32,598 hrs · 14,402 cycles

FLOOR PANEL 241GF IS DELAMINATED AND SPONGY. / REMOVED AND REPLACED CABIN FLOOR PANEL 241GF WITH A NEW PANEL PER AMM 53-21-00.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 32,598 hrs · 14,402 cycles

PASSENGER CABIN FLOOR PANEL 241KF IS DELAMINATED AND SPONGY. / REMOVED AND REPLACED CABIN FLOOR PANEL 241KF PER AMM 53-21-00.

Part: PANEL — DEBONDED (FUSELAGE) · airframe 32,598 hrs · 14,402 cycles

PANEL 192 F DME ANTENNA FWD ATTACH BRASE DISBONDED. / PREPPED AND BONDED PANEL 192F DME 1 ANTENNA FWD ATTACH BASE PER AMM 51-31-00

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 32,598 hrs · 14,402 cycles

EMERGENCY EXIT LIGHTS INOP AT FWD SERVICE DOOR / REMOVED + REPLACED FWD EMER LTS BATTERY PACK M2816. TESTS GOOD PER AMM 33-51-06.SA-M 326 ATTACHED: A1362135

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,184 hrs · 13,115 cycles

SERVICE ENTRY EMERGENCY LIGHTS WOULD NOT ILLUMINATE / REMOVED AND REPLACED SVC ENTRY EMERGENCY BATTERY PACK PER 33-51-06 - OPS CHECK GOOD

Part: SKIN — CRACKED (POWER DOOR) · airframe 26,916 hrs · 11,521 cycles

CUSTOMER REQUEST: JM EXTERNAL POWER DOOR CUTOUT LOWER SKIN CRACKED. / REMOVED DAMAGE; AND REPAIRED EXTERNAL POWER DOOR CUTOUT LOWER SKIN (SURROUND DOUBLER) I/A/W B737 SRM 53-10-15-2R-4 REPAIR 4

Part: BRACKET — CRACKED (L2 DOOR) · airframe 26,916 hrs · 11,521 cycles

BRACKET CRACKED ON L2 DOOR SWEEPER SEAL PAN ASSY. / L2 DOOR SWEEPER SEAL PAN ASSY BRACKET REPLACEMENT ACCOMPLISHED ON NRC 40231/8700/0009 DEFECT #Y137462

Part: ANGLE — CRACKED (AFT CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

AFT CARGO STA 727 LOWER FLOOR BULKHEAD ANGLE CRACKED / VERIFIED NEW AFT CARGO STA 727 LOWER FLOOR BULKHEAD ANGLE P/N 453A2611-25 IAW AIPC 25-52-10-19. INSTALLED IAW AMM 25-52-10-400-801. WN 8039

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 26,415 hrs · 11,286 cycles

AFT GALLEY G4 R/H SIDE EMERGENCY LIGHT COVER BROKEN. / R&R COVER IAW AMM.

Part: INTERCOSTAL — CORRODED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN; STA 947 LBL 25 WL 208; UPPER SURFACE OF INTERCOSTAL HAS CORROSION UNDER LAV MOUNT / REMOVED CORROSION ON INTERCOSTAL UPPER SURFACE STA 947 LBL 25 FOUND ORIG T .210' WITH .053' LOSS AND .155' REMAINING TO BE OUT OF LIMITS IAW B737 SRM 53-70-51-1A-1. REMOVED AND REPLACED INTERCOSTAL 147A5660-21 IAW B737 SRM SRM 51-40-02 AND DWG 147A5650 ID 0054 REV A

Part: SUPPORT — CRACKED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN. STA 277+10; BL0; WL 208; LONGITUDINAL FLOOR SUPPORT HAS CRACKS AT NUT PLATE HOLES (2EA) / REMOVED AND REPLACED CRACKED PASSENGR CABIN STA 277-10 BL0 WL 208 LONGITUDE FLOOR SUPPORT WITH NEW PART P/N 141A5410 U3 AAR SRM 51-40-02; SRM 51-40-05 DWG 141A5400 REV - AND AMM 01-00-02-SWA-002 ATAG #WN 6748

Part: FLOOR PANEL — PULLED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN FLOOR PANEL 222BF; UPPER FACE SHEET HAS MISSING FIBERS. / REPAIRED UPPER SKIN ON FLOOR PANEL 222BF AS REQ IAW B737 SRM 53-00-50-2R-1 REPAIR 1 AND SRM 53-00-50-2R-0 REPAIR GEN REV 68

Part: FLOOR PANEL — PULLED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN FLOOR PANEL 222DF; UPPER FACE SHEET HAS MISSING FIBERS. / REPAIRED PASSENGER CABIN FLOOR PANEL 222DF OF UPPER FACE SHEET MISSING FIBERS IAW B737-700 SRM 53-00-50-2R-0 REV 68 AND B737-800 SRM 53-00-50-2R-1 REV 68

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 26,415 hrs · 11,286 cycles

PASSENGER CABIN FLOOR PANEL 221AF HAD SECTION OF PANEL BROKEN OFF 9" FROM FORWARD EDGE AT RH OUTBOARD EDGE BETWEEN BS. 270 TO BS. 420. / REPAIRED R/H OUTBOARD EDGE OF PANEL 221AF IAW SRM.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN FLOOR PANEL 221AF HAS SECTION OF PANEL BROKEN OFF 9' FROM FWD EDGE AT RH O/B EDGE / REPAIRED R/H O/B EDGE OF PANEL 221AF . IAW B737-800 SRM 53-00-50-2R-4; SRM 53-00-50-2R-0

Part: FLOOR PANEL — PULLED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN; FORWARD WET AREA; FLOOR PANEL 222CF; FIBERS PULLED LOOSE/MISSING ACROSS ENTIRE UPPER SURFACE OF PANEL. / REPAIRED PASSENGER CABIN FWD WET AREA FLOOR PANEL 222CF ON ENTIRE UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 REV 68 AND B737 SRM 53-00-50-2R-0 REV 68. A09236 A13438

Part: FLOOR SUPPORT — CRACKED (BS 277) · airframe 26,415 hrs · 11,286 cycles

LONGITUDINAL FLOOR SUPPORT CRACKED AT NUT PLATE HOLES ATA BS. 277+10, BL 0. / R&R FLOOR SUPPORT IAW SRM, DWG, AND AMM.

Part: INTERCOSTAL — CORRODED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN; STA 947 LBL 50 WL 208; UPPER SURFACE OF INTERCOSTAL HAS CORROSION UNDER LAV MOUNT / REMOVED CORROSION ON INTERCOSTAL STA 947 LBL 50 ORIG T .230' LOSS .075' REMAINING .155' OUT OF LIMITS IAW B737 SRM 53-70-51-1A-1. REMOVED AND REPLACED INTERCOSTAL 147A5660-3 SRM 51-40-02 AND DWG 147A5650 ID 0054 REV A

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 26,415 hrs · 11,286 cycles

PASSENGER CABIN FLOOR PANEL 242D CRACKED AT OUTBOARD AFT EDGE NEXT TO CUTOUT. / R&R FLOOR PANEL PER SRM.

Part: BEAM — CORRODED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN STA 947+10 TO 986; RBL 57; WL 208. INNER CREASE BEAM CORD IS CORRODED ON UPPER SURFACE / REMOVED CORROSION ON R2 CREASE BEAM AT STA 947+10 TO 986.0 ORIG 'T' .080' REMAINING .050' LOSS OF .030' OUT OF LIMITS REMOVED & REPLACED R2 CREASE BEAM IAW SRM 51-10-02-0G-0; 51-40-02-0G-0; 51-40-05-0G-0; 53-70-15-1A-1; AMM 51-21-91-620-802; & WG 147A8501 SHT 93 REV INNER CHORD PN 147A854OU8

Part: CAP — CORRODED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN ; STA 947; LBL 50; WL 208; UPPER SURFACE OF T-CAP HAS CORROSION RUNNING UNDER LAU MOUNT / REMOVED CORROSION STA 947 T-CAP UPPER SURFACE LBL50 ORIG T .180' LOSS .040' REMAINING .140' OUT OF LIMITS IAW SRM 53-70-51-1A-1 REPAIRED T-CAP FROM LBL 7 TO LBL 60 IAW SRM 53-20-51-2R-5 REPAIR 5

Part: FLOOR PANEL — PULLED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN FLOOR PANEL 241ABF UPPER FACE SHEET HAS MISSING FIBERS / REPLACED PASSENGER CABIN FLOOR PANEL 241ABF UPPER FACESHEET IAW B737-800 SRM 53-00-50-2R-0 REV 68 53-00-50-2R-1 REV 68(A36551) (A87145)

Part: CREASE BEAM — CORRODED (BS 947-986) · airframe 26,415 hrs · 11,286 cycles

PASSENGER CABIN INNER CREASE BEAM CHORD CORRODED ON UPPER SURFACE BETWEEN BS. 947+10 TO BS. 986, RBL 57. / R&R R2 CREASE BEAM IAW SRM & DWG.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 26,916 hrs · 11,521 cycles

FLOOR PANEL 241D; UPPER FACE SHEET HAS MISSING FIBERS / REPLACED DAMAGE ON PANEL 241D. BONDED REPAIR PLIES AND CURED. TAP TEST GOOD. IAW B737-800 SRM 53-00-50-2R-1 REV 68; SRM 53-00-50-2R-0 REV 68

Part: FLOOR PANEL — PULLED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN FLOOR PANEL 242E HAS MISSING FIBERS ON UPPER FACE SHEET. / REPAIRED PASSENGER CABIN FLOORPANEL 242E UPPER FACESHEET AS MARKED IAW 737-800 SRM 53-00-50-2R-1 REV 68; 737-800 SRM 53-00-50-2R-0 GENERAL REV 68.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 26,415 hrs · 11,286 cycles

UPPER SURFACE OF T-CAP CORRODED RUNNING UNDER LAV MOUNT AT BS. 947, LBL 50. / REPAIRED T-CAP IAW SRM.

Part: ANGLE — CORRODED (BS 500B-500I) · airframe 26,415 hrs · 11,286 cycles

FORWARD CARGO COMPARTMENT FLOOR STRUCTURE R\H Z-ANGLE CORRODED BETWEEN BS. 500B TO BS. 500I, RBL 23 AT NUT PLATE HOLES. / R&R Z ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 500I) · airframe 26,415 hrs · 11,286 cycles

FORWARD CARGO COMPARTMENT FLOOR STRUCTURE, STRINGER CLIP CRACKED AT BS. 500I, STR. 26R. / R&R STRINGER CLIP IAW SRM & DWG.

Part: STRAP — BROKEN (AFT CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

AFT CARGO; STA 847; RBL 21; 2 EA NUT PLATES ARE BROKEN FOR FLOOR PANEL. / ON AFT CARGO STA 847; RBL 21; REMOVED & INSTALLED NUTPLATES STRAP AND REPLACED NUTPLATES IAW SRM 51-40-02-0G-0

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN FLOOR PANEL 242D; AFT O/B CORNER OF PANEL IS BROKEN OFF / RECIEVED NEW FLOOR PANEL TO REPLACE DAMAGED FLOOR PANEL 242D; P.N# 147A5810-345 REF IPC 53-21-51-46 A72035

Part: ATTACH ANGLE — CRACKED (FWD CARGO RH) · airframe 26,916 hrs · 11,521 cycles

FWD CARGO COMPARTMENT FLOOR STRUCTURE; STRINGER CLIP AT STA 500I; STR 26R CRACKED. / REMOVED AND REPLACED FWD CARGO COMPARTMENT FLOOR STRUCTURE STRINGER CLIP STA 500I STR 26R IAW SRM 51-40-02-0G-0 DWG 143A1234 ID: 0020 REV-

Part: FLOOR PANEL — PULLED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN FLOOR PANEL 242D; UPPER FACE SHEET HAS MISSING FIBERS / RECIEVED NEW FLOOR PANEL TO REPLACE DAMAGED FLOOR PANEL 242D; P.N# 147A5810-345 REF IPC 53-21-51-46 A702035

Part: FLOOR PANEL — PULLED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN FLOOR PANEL 241E HAS MISSING FIBERS ON UPPER FACE SHEET. / BONDED REPAIR ON PANEL 241E MISSING AND FRAYED FIBERS ON UPPER FACE SHEET IAW B737-800 SRM 53-00-50-2R-1 REV 68; SRM 53-00-50-2R-0 REV 68 A93557 A36551

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN FLOOR PANEL 242D; LOWER FACE SHEET IS DELAMINATED AND CRACKED AT AFT O/B CORNER / RECIEVED NEW FLOOR PANEL TO REPLACE DAMAGED FLOOR PANEL 242D; P.N# 147A5810-345 REF IPC 53-21-51-46 A72035

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN FLOOR PANEL 242D IS CRACKED AT O/B AFT EDGE NEXT TO CUTOUT (2EA PLACES) / RECIEVED NEW FLOOR PANEL TO REPLACE DAMAGED FLOOR PANEL 242D; P.N# 147A5810-345 REF IPC 53-21-51-46 A72035

Part: FLOOR PANEL — PULLED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN FLOOR PANEL 242RF HAS MISSING FIBERS ON UPPER SURFACE / REPAIRED PASSENGER CABIN FLOOR PANEL #242RF OF PULLED FIBERS ON UPPER SURFACE WITH NO DAMAGE TO COMPOSITE SUBSTRATE IAW B737-800 SRM 53-00-50-2R-0 REV 68 AND B737-800 SRM 53-00-50-2R-1 REV 68.

Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 26,916 hrs · 11,521 cycles

AFT CARGO DOOR CUTOUT LOWER THRESHOLD WEB HAS CORROSION STA 794 TO 847 RBL 21 TO 27 WL 163 / REMOVED CORROSION FROM AFT CARGO DOOR CUTOUT LOWER THRESHOLD WEB STA 794 TO 847 RBL 21 TO 27WL 163 AND CHECKED LIMIT FOUND TO BE OUT OF LIMIT ORIG 'T' OUR LOSS .020' REMAIN .025' INSTALLED NEW PART P/N 146A8123U6 IAW SRM 51-10-02 SRM 53-60-15-1A-1 SRM 51-40-02 DWG 146A8340 REV- AND AMM 51-21-91-620-802 ATAG #WN4221

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

AFT PIT SHIELD CORRODED AT BS 767 TO 787; RBL22; WL 153. / REMOVED DAMAGE. ORIGINAL MATERIAL .050' ; LOSS. 006'; MATERIAL REMAINING .044' FWD FOUND TO BE OUT OF LIMITS PER 53-60-15-1A-1. REMOVED AND INSTALLED A NEW SHIELD AT AFT PIT BS767 TO BS 787 RBL 12 I/A/W SRM 51-40-02-0G-0 AND BOEING DRAWING 146A8127

Part: ANGLE — CORRODED (FWD CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

FWD CARGO COMPARTMENT FLOOR STRUCTURE STA 500I; RBL 24 TO LBL 24; WL 153 BULKHEAD LOWER SUPPORT ANGLE HAS CORROSION. / REMOVED CORROSION FWD CARGO COMPARTMENT FLOOR STRUCTURES STA 500I; RBL 24 TO LBL 24; WL BULKHEAD LOWER SUPPORT ANGLE; NO PUBLISHED LIMITS OUT OF LIMITS 14918 22NOV2019 REMOVED AND REPLACED BULKHEAD LOWER SUPPORT IAW SRM 51-40-02-0G-0 & DWG 143A 14918 22NOV2019 7902 REV;B APPLIED CIC TO ANGLE IAW AMM 51-21-91-620-802

Part: INTERCOSTAL — CORRODED (AFT CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

AFT PIT WEB CORROSION AT BS 747 TO 767; RBL 22; WL 153 / AFT CARGO WEB CORROSION AT B.S. 747 TO B.S. 767 RBL 22; WL 153. BLENDED AND REMOVED CORROSION I/A/W SRM 51-10-02-0G-0 AND CHECKED WITH 10X MAG. MATERIAL THICKNESS IS .040. MAT LOSS IS .016 REMAINING THICKNSS IS .024 'OUT OF LIMITS' I/A/W SRM 53-00-53-1A-2. DRILLED AND REMOVED INTERCOSTAL WEB I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW INTERCOSTAL WEB I/A/W SRM 51-40-05-0G-0 ALSO BOEING DWG 146A7500 REV: - . INSTALLED NEW INTERCOSTAL WEB I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 146A7500 REV: -. APPLIED C.I.C TO AREA I/A/W AMM 51-21-91-620-802

Part: WEB — CORRODED (AFT CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

AFT PIT WEB CORRODED AT BS 927 TO 931; RBL 2; WL 147 / AFT PIT WEB CORRODED AT BS 927 TO 931 RBL 2 WL 147 REPLACED WEB WITH P/N: 147A7500-6 IAW BOEING DWG# 147A7500 REV- ID: 0044 AND SRM 51-40-02-0G-0 CORROSION FOUND TO BE 'OUT OF LIMITS' OF ORIGINAL: .045' REMAINING .019' REMOVED .026' IAW SRM 53-00-53-1A-2

Part: FLOOR PANEL — PULLED (CABIN) · airframe 26,916 hrs · 11,521 cycles

PASSENGER CABIN FLOOR PANEL 242UF; UPPER FACE SHEET HAS MISSING FIBERS / BONDED PNL 242UF UPPER FACESHEET MISSING AND FRAYED FIBERS. IAW B737-800 SRM 53-00-50-2R-1 REV 68; SRM 53-00-50-2R-0 REV 68 A36551 A 09236

Part: FLOOR PANEL — PULLED (CABIN) · airframe 26,916 hrs · 11,521 cycles

FLOOR PANEL 241AAF HAS MISSING FIBERS ON UPPER FACE SHEET. / REPAIRED I/A/W PANEL 241AAF ON UPPER FACE SHEET IAW B737-800 SRM 53-00-50-2R-0 REV 68; 53-00-50-2R-1 REV 68

Part: SHIELD — CORRODED (BS 767-787) · airframe 26,415 hrs · 11,286 cycles

AFT PIT SHIELD CORRODED BETWEEN BS. 767 TO BS. 787, RBL 22. / R&R SHIELD IAW SRM AND DWG.

Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 26,916 hrs · 11,521 cycles

FWD CARGO COMPARTMENT FLOOR STRUCTURE R\H Z-ANGLE STA 500B TO 500I; RBL 23; WL 153 HAS CORROSION AT NUTPLATE HOLES. / REMOVED CORROSION ON FWD CARGO COMPARTMENT FLOOR STRUCTURE RH Z ANGLE STA 500B TO 500I RBL23 WL153 IAW SRM 51-10-02-0G-0. VERTICAL WITH 10X MAG. VERIFIED LIMITS IAW SRM 53-00-53-1A-2. ORIGINAL THICKNESS 0.040' REMAINING 0.029'. LOSS OF 0.011' FOUND OUT OF LIMITS. REPLACED Z-ANGLE STA 500B+10' TO 500I IAW SRM 51-40-02-0G-0; SRM 53-00-53-01-2; SRM 57-40-05-06-0; AMM 51-21-41-370-803 AND AMM 51-21-72-370-804. P/N BAC 1496-444 ATAG A47617. REPLACED SECTION IAW SRM 53-00-53-2R-5 REPAIR 5.

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

FWD CARGO FLOOR PANEL 120CF HAS CORROSION / REMOVED CORROSION FROM FWD CARGO FLOOR PANEL 120CF REPLACED PANEL WITH NEW PART P/N 453A1610-103 IAW SRM 51-10-02; CHECKED LIMIT FOUND TO BE OUT OF LIMIT OVER 30% OF PANEL IAW SRM 53-00-53-1A-1; IPC 25-52-11-17 PANEL TO BE INSTALLED IN WO 578706 ATAG#WN1763

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

FWD CARGO FLOOR PANEL 120BF HAS GOUGES AND CORROSION / REMOVED CORROSION FROM FWD CARGO FLOOR PANEL 120BF AND CHECKED LIMIT FOUND TO BE OUT OF LIMITS 30% OF PANEL REPLACED PANEL WITH NEW PART P/N 453A1610-16 IAW SRM 51-10-02 SRM 53-00-53-1A-1 AND IPC 25-52-11-17 PANEL TO BE INSTALL IN W/O 578706 ATAG# WN0130

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

FWD CARGO FLOOR PANEL 120DF HAS CORROSION / REMOVED CORROSION FROM FWD CARGO FLOOR PANEL 120DF AND CHECKED LIMIT FOUND TO BE OUT OF LIMIT 30% OF PANEL REPLACED PANEL WITH NEW PART P/N 453A1610-20 IAW SRM 51-10-02; SRM 53-00-53-1A-1; IPC 25-52-10-17 PANEL TO BE INSTALLED IN WO 578706 ATAG#WN1476

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

FWD CARGO FLOOR PANEL 120AF HAS CORROSION / REMOVED CORROSION FROM FWD CARGO FLOOR PANEL 120AF AND CHECKED LIMIT FOUND TO BE OUT OF LIMITS OVER 30% OF PANEL REPLACED PANEL WITH NEW PART P/N 453A1610-14 IAW SRM 51-10-02; SRM 53-00-53-1A-1; IPC 25-52-11-17 PANEL TO BE INSTALLED IN WO 578706 ATAG#WN6643

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

AFT CARGO COMPARTMENT PANEL 140DF HAS LIGHT CORROSION ON EDGES OF PANEL. / AFT CARGO COMPARTMENT PANEL 140DF CORROSION EXCEEDS 20' IN LENGTH OUT OF LIMITS IAW SRM 53-00-53-1A-1; NEW PANEL RECIEVED IAW BOEING DWG 453A2610 REV: K ATAG WN3473

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

AFT CARGO COMPARTMENT PANEL 140CF HAS LIGHT CORROSION ON EDGES OF PANEL. / AFT CARGO COMPARTMENT PANEL 140CF CORROSION EXCEEDS 20' IN LENGTH OUT OF LIMITS IAW SRM 53-00-53-1A-1; NEW PANEL RECIEVED IAW BOEING DWG 453A2610 REV: K ATAG WN2693

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

AFT CARGO COMPARTMENT PANEL 140AF HAS LIGHT CORROSION ON EDGES OF PANEL. / AFT CARGO COMPARTMENT PANEL 140AF CORROSION EXCEEDS 20' IN LENGTH OUT OF LIMITS IAW SRM 53-00-53-1A-1; NEW PANEL RECIEVED IAW BOEING DWG 453A2610 REV: K ATAG WN1272

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 26,916 hrs · 11,521 cycles

AFT CARGO COMPARTMENT PANEL 140EF HAS LIGHT CORROSION ON EDGES OF PANEL. / AFT CARGO COMPARTMENT PANEL 140EF CORROSION EXCEEDS 20' IN LENGTH OUT OF LIMITS IAW SRM 53-00-53-1A-1; NEW PANEL RECIEVED IAW BOEING DWG 453A2610 REV: C ATAG WN5310

Part: SUPPORT — CORRODED (BS 947) · airframe 26,415 hrs · 11,286 cycles

UPPER SURFACE OF INTERCOSTAL CORRODED UNDER LAV MOUNT AT BS. 947, LBL 25. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 947) · airframe 26,415 hrs · 11,286 cycles

UPPER SURFACE OF INTERCOSTAL CORRODED UNDER LAV MOUNT AT BS. 947, LBL 50. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: GIRT BAR — STUCK (L1 DOOR) · airframe 25,522 hrs · 10,862 cycles

FORWARD ENTRY DOOR GIRT BAR WAS STUCK IN UNARMED POSITION. / REINSTALLED GIRT BAR IAW SIP.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 23,258 hrs · 9,880 cycles

MID CABIN CEILING EXIT SIGN LIGHT COVER LENS FELL OFF. REINSTALLED LENS PER AMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 20,810 hrs · 8,839 cycles

RT WING OVERWING EXIT EMERGENCY EXIT SIGN LIGHT COVER LOOSE. R&R LENS ASSEMBLY PER MM.

Part: FAIRING — CRACKED (RIGHT WING) · airframe 19,949 hrs · 8,431 cycles

#6 MID 642BB FLAP TRACK FAIRING HAS CRACK ON FWD LOWER O/B CORNER / REPAIRED CRACK ON FWDLWR O/B CORNER OF #6 MID FLAP TRACK FAIRING 642BB IAW REPAIR - 57 EA-04473 REV IR AND ER-17-05136 REV PL

Part: FAIRING — CRACKED (TE FLAP) · airframe 19,020 hrs · 8,011 cycles

RT WING NR 6 MID 642BB FLAP TRACK FAIRING CRACKED ON FORWARD LOWER OUTBOARD CORNER. REPAIRED FAIRING IAW EA AND ER.

Part: BRACKET — BROKEN (LT WING) · airframe 19,949 hrs · 8,431 cycles

PANEL 511FB HAS A BROKEN BRACKET ATTACHED TO SEAL RETAINER. / REMOVED AND REPLACED BRACKET P/O 287A9152 IAW SRM 51-40-02-OG-0 80525 11-18-17 CONT: IAW BOEING DWG 115A2710 NEW BRACKET ITEM # 287A9152 P.O. # 658183

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 19,020 hrs · 8,011 cycles

AFT CARGO LT ZEE CHANNEL CORRODED BETWEEN BS 727+4 TO BS 847. R&R ZEE CHANNEL IAW SRM.

Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 19,949 hrs · 8,431 cycles

***CORROSION*** *CORROSION* AFT CARGO; R/H ZEE CHANNEL HAS CORROSION AND PULLED RIVETS ALONG ITS ENTIRE LENGTH FROM FWD BULKHEAD TO BS 767. / AFTER EVALUATION CORROSION AT STA 727+4 TO 767 ON R/H SIDE WAS FOUND TO BE OUT OF LIMITS. IAW SRM 53-00-53-1A-2 FIG 103 DETAIL D. REMOVED RH ZEE PER SRM 51-40-02-0G-0; FABRICATED; LOCATED; AND DRILLED NEW ZEE CHANNEL FROM BAC 1496-377-7075 T62 LOT #5051578 PER SM 53-00-53-2R-5; SRM 51-40-05-0G-0; AND DWG 146A7502 TREATED AND PRIMED IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804; INSTALLED REPLACEMENT RH ZEE CHANNEL AT 727+4 TO 767 IAW SRM 51-40-02-0G-0 AND BOEING DUB146A7502

Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 19,949 hrs · 8,431 cycles

***CORROSION*** *CORROSION* AFT CARGO; R/H ZEE CHANNEL HAS CORROSION BS 767 TO CARGO DOOR CUTOUT. / REMOVED DAMAGED SHIELD & REPLACED WITH NEW R/H SHIELD IAW SRM 51-40-02-OG-0; 51-40-05-OG-O & BOEING DWG 146A0081

Part: VAPOR BARRIER — CRACKED (RT WHEEL WELL) · airframe 19,949 hrs · 8,431 cycles

R/H VAPOR BARRIER STA. 663 IS CRACKED AT RBL 40.00 / REPAIRED R/H VAPOR BARRIER STA. 663 AT RBC 40.00 IAW SRM 57-10-10-2R-2 AND IAW 51-70-01 REPAIR 10. ALLOWABLE LIMITS IAW OTHER-57EA-03738REPAIRED RIGHT WHEEL WELL VAPOR WEB CRACK AT RBL 40.00 IAW SRM 57-10-10-2R-2 AND IAW SRM 51-20-04 REPAIR 10. AMD OTHER -57-EA-03738

Part: FRAME — CRACKED (AFT CARGO BAY) · airframe 19,949 hrs · 8,431 cycles

WHILE REMOVING WORKING FASTENER IN TRANSITION STRIP AT BS 727H LBL 21.5 WL 155.5 FOUND FASTENER HOLE CRACKED IN FRAME / REPAIRED BS727 H FRAME BETWEEN STR 25L + 26L IAW SWA REPAIR-53EA-00498 REV 1

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 19,020 hrs · 8,011 cycles

BULKHEAD WEB CRACKED AT BS 663, RBL 40. REPAIRED THE BULKHEAD IAW SRM.

Part: CHANNEL — CORRODED (BS 727-767) · airframe 19,020 hrs · 8,011 cycles

AFT CARGO RT ZEE CHANNEL CORRODED BETWEEN BS 727+4 TO 767. R & R THE CHANNEL IAW SRM AND DWG.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 19,949 hrs · 8,431 cycles

*CORROSION* AFT CARGO; L/H ZEE CHANNEL HAS CORROSION AND PULLED RIVETS ALONG ITS ENTIRE LENGTH FROM FWD BULKHEAD TO BS 807. / AFT CARGO L/H ZEE CHANNEL HAS CORROSION FROM STA. 727+4 TO STA 807 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED ZEE CHANNEL FROM STA 727+4 TO STA 847. LOCATED AND DRILLED NEW ZEE CHANNEL LOT #5051578 MATERIAL ID BAC 1496-377-7075-T6 IAW IAW SRM 51-40-02-0G-0 AND SRM 53-00-53-2R-5.

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 19,949 hrs · 8,431 cycles

**CORROSION** FORWARD CARGO STA. 500 +10' TO STA. 500E; LBL 24; FLOOR TO SIDEWALL TRANSITION ANGLE CORRODED AT SEVERAL FASTENER HOLES / AFTER EVALUATION CORROSION ON STA 500+10 TO 500E. LBL 24 FOUND TO BE OUT OF LIMITS. SRM 53-00-53-1A-2; F15103; DETAIL D. REMOVED PER SRM 51-40-02-0G-0 FABRICATED; LOCATED AND DRILLED NEW 2 EA CHANNEL REPLACEMENT; PER SRM 53-00-53-2R-05 SRM 51-40-05-0G-0 USING BAC 1Y96-444-7075T6; LOT #5061427-3. TREATED AND PRIMED PER AMM 51-21-72-370-204; INSTALLED REPLACEMENT AEE CHANNGEL ON LBL24 STA 500+10 TO 50I; IAW SRM 53-00-53-2R-6. SRM 51-40-02-0G-0. SWG 143A7500

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 19,949 hrs · 8,431 cycles

**CORROSION** FORWARD CARGO; STA. 520; LBL24 - RBL24; FLOOR TO AFT BULKHEAD SUPPORT ANGLE CORRODED IN SEVERAL PLACES. / CORROSION ON FWD CARGO AFT BULKHEAD STA 500I LBL24-RBL24 LWR SUPPORT ANGLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS FOUND IN THE SRM. REMOVED DAMAGE ANGLES FABRICATED NEW ANGLE USING BAC1517-2810 T62 LOT #5047971. INSTALLED NEW SUPPORT ANGLE AT THE FWD CARGO AFT BULKHEAD LWR SECTION. REF SRM 51-40-02; 51-40-05; AND BOEING DWG 143A9485. 57575U 11/16/17

Part: ANGLE — CORRODED (BS 500A-500E) · airframe 19,020 hrs · 8,011 cycles

FLOOR TO SIDEWALL TRANSITION ANGLE CORRODED BETWEEN BS. 500A TO BS. 500E, RBL 24. R & R THE ANGLE IAW SRM & DWG.

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 19,949 hrs · 8,431 cycles

**CORROSION** FORWARD CARGO STA. 490-500A; RBL 24; FLOOR TO SIDEWALL TRANSITION ANGLE CORRODED AT SEVERAL FASTENER HOLES / CORROSION ON R/H FWD CARGO SHIELD AT STA 490-500A RBL 24 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM. REMOVED CORRODED SHIELD. FABRICATED SHIELD USING 7075-0 .032' LOT# 5029090. RECIEVED FROM HEAT TREAT PO# 658226 INSTALLED FABRICATED SHIELD AT THE FWD CARGO R/H SIDE STA 490-500A RBL 24. IAW SRM 51-40-02; 51-30-01-06-0; 51-40-05; AND BOEING DWG 143A8126. 57575U 11/17/17

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 19,949 hrs · 8,431 cycles

**CORROSION** FORWARD CARGO STA. 500H TO STA. 500I; LBL 24; FLOOR TO SIDEWALL TRANSITI ON ANGLE CORRODED AT SEVERAL FASTENER HOLES / REPLACEMENT OF SIDEWALL TRANSITION ANGLE STA. 500+10' TO 500I LBL 24 TO BE ACCOMPLISHED ON CUSTOMER CARD N109247. CORROSION AT STA 500H-500I LBL 24 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DETAIL D

Part: NONE — CORRODED (FWD CARGO BAY) · airframe 19,949 hrs · 8,431 cycles

**CORROSION** FORWARD CARGO STA. 500A-500E; RBL 24; FLOOR TO SIDEWALL TRANSITION ANGLE CORRODED AT SEVERAL FASTENER HOLES / REMOVED MAMAGED SECTION OF R/H FLOOR TO SIDEWALL ZEE FROM STA 500D-500I AND REPLACED WITH FABRICATED REPLACEMENT PER SRM 51-40-02; 53-00-53-2R-6 AND DWG 143A7501

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 19,020 hrs · 8,011 cycles

RIGHT EMERGENCY LIGHT LENS CRACKED BETWEEN ROWS 10 TO 14. R & R THE LENS IAW AMM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 19,020 hrs · 8,011 cycles

BULKHEAD WEB CRACKED AT BS 663, RBL 40. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: HOOK — MISSING (R1 DOOR) · airframe 19,640 hrs · 8,289 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK MISSING. INSTALLED HOOK PER EA.

Part: FUEL TANK — LEAKING (BS 612) · airframe 16,875 hrs · 7,122 cycles

FOUND FUEL LEAK AT FASTENER IN CENTER WING TANK LOWER SKIN AT BS 612, RBL 1. REPAIRED FUEL TANK IAW SWA EA.

Part: VALVE — LEAKING (FUEL SYSTEM) · airframe 16,875 hrs · 7,122 cycles

DIVERSION, KEEL BEAM FUEL LEAK ODOR IN CABIN. R&R NR 2 VALVE PER MM.

Part: SIGN — DETACHED (CABIN) · airframe 16,594 hrs · 6,999 cycles

OVERHEAD AISLE EMERGENCY EXIT SIGN DETACHED FROM ABEAM EXIT ROW. SECURED SIGN PER MM.

Part: COVER — CRACKED (CABIN) · airframe 13,131 hrs · 5,464 cycles

CEILING EMER LIGHT COVER 3 CRACKED. R & R COVERS IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 13,131 hrs · 5,464 cycles

CEILING EMER LIGHT COVER 6 CRACKED. R & R COVERS IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 13,131 hrs · 5,464 cycles

CEILING EMER LIGHT COVER 1 CRACKED. R & R COVERS IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 13,131 hrs · 5,464 cycles

CEILING EMER LIGHT COVER 5 CRACKED. R & R COVERS IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 13,131 hrs · 5,464 cycles

CEILING EMER LIGHT COVER 2 CRACKED. R & R COVERS IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 13,131 hrs · 5,464 cycles

CEILING EMER LIGHT COVER 9 CRACKED. R & R COVERS IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 13,131 hrs · 5,464 cycles

CEILING EMER LIGHT COVER 7 CRACKED. R & R COVERS IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 13,131 hrs · 5,464 cycles

CEILING EMER LIGHT COVER 4 CRACKED. R & R COVERS IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 13,131 hrs · 5,464 cycles

CEILING EMER LIGHT COVER 8 CRACKED. R & R COVERS IAW MM.

Part: LENS — MISSING (CABIN) · airframe 12,383 hrs · 5,142 cycles

RIGHT EMER LIGHT LENS MISSING, BETWEEN ROW 21 - 25. INSTALLED LENS IAW SIP.

Part: RETAINER — MISSING (L1 DOOR) · airframe 10,699 hrs · 4,455 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR RETAINER MISSING. INSTALLED RETAINER IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 10,404 hrs · 4,326 cycles

OVERHEAD OVERWING EMER LIGHT AT EXIT DOOR LOOSE. R & R SIGN IAW MM.

Part: LENS — MISSING (CABIN) · airframe 8,902 hrs · 3,645 cycles

RIGHT EEPLS LENS COVER MISSING AT ROW 10. INSTALLED COVER IAW MM.

Part: COVER — MISSING (CABIN) · airframe 8,902 hrs · 3,645 cycles

RT EEPLS LENS COVER MISSING AT ROW 10. R & R COVER IAW SIP.

Part: LENS — MISSING (CABIN) · airframe 8,214 hrs · 3,322 cycles

RIGHT OVERHEAD BIN EMER LIGHT LENS MISSING AT ROW 14. R & R LIGHT ASSEMBLY IAW SIP.

Part: LENS — BROKEN (CABIN) · airframe 6,092 hrs · 2,417 cycles

ENTRY WAY EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 5,751 hrs · 2,276 cycles

R1 DOOR EMERGENCY EVAC SLIDE LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 3,957 hrs · 1,524 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGN BROKEN. REPAIRED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,142 hrs · 1,186 cycles

RIGHT AFT EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.